EFTA01326217

Ord to 2120<<20 Electron Track ng Eiveitet 0 MAJOR REPAIR AND ALTERATION Ed tr31ICI B USOwarteen haniiponiu,. or (Airframe, Powerplant, Propeller, or Appliance) For FAA Use Only . rent Amp. mimmiratim INSTRUCTIONS: Print or type all entries. See Title 14 CFR §43.9, Pan 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. §44701). Failure to report can result in a civil penally for each such violation. (49 U.S.C. §46301(a)) Naeorekty end Registration Mark! N120JE Setter NI: 10aS I. Aircraft Make. GULFSTREAM Model! OW Sykes: WA Name (As shown on reoisration cerlificare) Address (As shown on reoistratiOn cortittafe) JEGE LLC Ad*a.a: MOO RED R.304 DARTER 03 2. Owner Oty ST. TMOWS SW. CORDON Sc 00002 go.roy VIRGIN MINOS 3. For FM Use Only • 4. Type & Unit Identification Regsr Meseta. UM Make Model Sorel Number O 0 AIRFRAME (As descnbed if teem I abOYO) • O POWERPLANT O PROPELLER o 1taa El . APPLIANCE wituraceser S. Conformity Statement A. Annoys Name and Address B. K nd 01Agency Name Stevens AdItC4p8O• Ma Delostir System. SC a U.S. Certificated Mechanic 0 Manacturer se 103 Ent Din O Foreign Certificated Mechant C. Cent-ante No. City Mow Sum GoOrom 0 Certificated Repak Swam Sc St2te Coeds United &Stela Amente O Careficated Maintenance Organdatcn VIB8368K 0. 1i:entry dal the repair erclror alteration made kr tie unti(.) 'denoted In item 5 above and OW..nbild on the reverse or aeactrnents hereto new been nestle In accordance with die rettirements of Pant) 430! the US. Federal Anton Regulatans and that the Intrinabon Ravished herein is true and correct iti tie best of my knowtedge. Extended rarqe Fuel Sionstvernate of &Shafted kedual Per 14CFR Pan 43 App. B O Mike Shaw , • June 03, 2019 . —7 , 4.1141 7. Approval fof cum to Service Pursuant to the autharity green persons specified below. the twit Identified in item 5 was irepected n tie manner peSSOIbed by the AdminIStrator el the Federal Adidas Adrnindliaten ard IS 0 APPROVED . REACTED FM FP Standards Person APING'S by Canadian Manufacturer Maintenne Orgarizaban inspect& Department of Transport BY Otter (50900.7 FM Designee X Repair Stamm Inspecton Aulltarizettm Carthate Of Signature/Date of ALthonzed IntS4dual Oesqnsuco No. CRS$ VII18388K Dendall Wood June 03.2019 iatAuttlat w6 09.0 FM Form 337 oo-om SDNY_Glil_02753702 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240624 EFTA01326217 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An a,Yeration must be cornpabble with allprevious atterahons ro assure continued conformity with the applicable airworthiness requirement& 8. Description of Work Accomplished (If more space Is required, attach additional sheets. Identify with se-craft nationakly and registration mark and date work completed.) N120JE June 03-2019 Nationality and Registration Mark Dale KaiserAir, Inc STC ST03422CH 1. Installed KalserAt, Inc. SIC ST03422CH - by installation of a Universal Avionics UNS•I Espw flight management system oath Unlink UL•801 datalink system and CVR-120A cockpit voice recorder to meet airworthiness requirements for FANSUA+ and optional Automatic Surveillance — Broadcast (ADS-B) Out in accordance with Master Data List. Document No. JRW1279-MDL. Revision A dated October 26. 2018 or later FAA approved revision. 2. The following FM approved Flight Manual Supplements: Universal Avionics Systems Corporation CVR-120A Codtpit Voice Recorder. Document No. JRW1280.FMS-01, Revision A. dated May 25. 2015. Automatic Dependent Surveillance Broadcast Out (ADS-B Out). Document No. JRW1260-FMS-03, Revision A. dated October 06. 2015. Universal Avionics UNS•tEspw FMS and UL• 801 Unlink Datalink Communication System, Document No. JRW1280-FMS-04. Revision IR. dated October 30. 2018 and the Unvemal Avionics Corporation CVR Operation Report No. 23-70-08-01, Rev. 2. Dated March 10. 2016. has been inserted Into the Aircraft Flight Manual. 3. Instructions for Continued Airworthiness Document No. JRW1283-ICA Revision E. Appendix A Svu E. dated June 18. 2018 has been inserted into the Customer's Supplemental Maintenance Manual. FM 8110-3 Approvals: Iridium Antenna Instalati08 FM 8110.3 • CI 490-490 indium Antenna Doubler Design B Inslalabon, Identification No. N120JE-052310-1-ECNOI. Revision N/C. dated May 23.2019 and Damage Tolerance Analysis for the Gulfstream Cy-IV CI 490-490 Iridium Antenna Doubler Insulation, Repot No. N120JE-052319-OT01, Revision N/C. dated May 23. 2019. Approved by FM Structures DERT-605818.NAL Trevor J. Sarong. Instructions for Continued Airworthiness Document No. N120JE-ICAW-052319, Revision IR. dated May 23. 2019 LED Cabin Effects Liohting FM 8110-3 - installed direct replacement LEO Caton Lighting. Identification No. Drawing No. 06-328-W03 Rev IR pages 1.9. dated May 30. 2019. Approved by FM Systems & Equipment DERT-832582-CE. Michael Casper. VHF/Comm Antenna Installation and LH Mfd Foul**. Feadthru Installation FM 81101- VHF/Communication Antenna Installation. Drawing No. 06-560-001. Revision IR. dated May 16.2019 and LH Feed•thru installation 06-560-002, revision IR. dated May 23. 2019. Approved by FM Structures DERT-605818-Mil. Trevor J. Strong. 'es Performed aircraft reweigh. updated Equipment List and inserted data into the Weight 8. Balance Manual and Flight Manual as required. FAA-8110-3 and dramngs have been inserted into the Stevens Aerospace. Customer's Supplemental Maintenance Manual. ENO cgAdditional Sheets Are Attached FM Form 337 110-06) SDNY_GM_02753703 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240625 EFTA01326218 KAISERAIR, Letter Of Authorization May 14, 2019 KaiserAir, Inc. authorizes Stevens Aerospace and Defense Systems LLC the one time use of KaiserAir, Inc STC ST03422CH for the installation of Universal Flight Management System, Unilink and CVR for the requirements for FANS In Guifstream Model IV Serial Number 1085 current Tail Number N120JE. AndreaJtujan Chief Inspector KaiserAir, Inc. 2240 Airport Blvd. Santa Rosa. CA. 95492 707.528.7400 SDNY_GM_02753704 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240626 EFTA01326219 SDNY_GM_02753705 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240627 EFTA01326220 numb Shan of America Ptparhttent of tgrausportntion — Acbcral Attention Abittinistration Supplemental Zgpe Certificate AGnien, ST03422CH .Y/ti fly/Awn KaiserAir, Inc. 8735 Emhart Road Oakland, CA 946214547 rent//J 441.44, doer e:s ensi4.../ewhet /-14-wsillys-siwy/wvat averaieh.d rowirebierboo4 //muter frJ 4aareleadaCarytva ~NJ de reterreete:ionw private-Si 1:4e/ 25 r/46 Federal Aviation .W.cownchb..4. (See Page 3 of4 for complete certification basis) / 1;yjyafcci:Oww4w/. • .-3,2,y vely/Awn Wwweer.• Al2EA Oulfstraan 04V. GV CerlierOdeava 1.4*.iowe P.r.ifivor Installation of a Universal Avionics C/NS-IDPW night management system "WI UnilAnk UL-1501datalink system and CVR-120A cockpit voice record". to moat aim:inhalant requirements for FANS 1/A+ and optional Automatic Depaulan Surveillana — Broadassi (ADS-3) Oct in accordance with KaiscrAir, Inc. Master Dula List JR9/1279-MDL.Revision J, dated October 30.2018. or later FAA approved revision. Vatenthe/tiva owegveativaa: 1. The installa must determine nib:Ilia this design change is compatible with previoirdy approved modifications. 2. FAA approved Hight Manual Supplements, KaiscrAir, Inc. !bemoan No. JRW 1280-FMS-0I RevisMn A, approved May 25, 2015, JRW I280-FMS-02. Revision B. anwoval Octoba 6, 2015. JRW 12804MS-03, Revision A dated October 6, 2015 and JRW 12804-MS414, Revision -. dated Octoba 30. 2018 or later FAA approved revisions me required onboard the modified aircraft 3. The modified aircraft must be maintained in Accordance with Ainvorthinois Limitations containedin KairerAir.'Ine. Document No. JRW1283-ICA, Chapter 10 0 Airworthiness Limitations. Revision approved October 30, 20I It, or later FAA approval revision, in addition to the basic aircmft niaintenance manuals. 4.11the holder agrees to permit another person to int this certificate to alts the product, the hoWer must give the other paron written evidence of that pimnbsion. arronwayt snide 4.yerretiese AA, evf he a.I p, A, 4440nweeir fir Werbeehrite Josavvmdarei mawavoini: errnevire or Arneriteehave .4,4 r Arebrib ouleinatin," /dr •Alaimaivaillow/or .Zialetv/. Zivie/navo . tefitraidasalaira. late Vor,r4;whiv. :July23.2014. Jamey 27. 2015 lir* wecbavy/.. Vark et:maaaanry• :WWI 03. 2015 Vark 'naval May 25. 2015. °ciao 30.20t8 /Ay" r//4. Zetintividnv/er Armature) Brenda L. tilditickl ODA Admiiiigralor ElflOy Aerospace. LIZ OCA431240-CE Aar afopiat too et iris aaa• It!.?.,. 1, itsnirbrd• ay a fib of b. brridler ropirioonset not onallag 1 bars, or tot". TM raw PAGI I at I PARS Ibis .vat/lean ay b canasta In better* with ratt ZI.47. SDNY_Glvl_02753706 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240628 EFTA01326221 SDNY_GM_02753707 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240629 EFTA01326222 ltnite Stoke of Aumito peparbumf of transportation - Adorn( A0 butittist tion Suppletztental type ffertifirate Mantinuation Ailed) ...441t/10,170 ST03422CH firok rAZatoovor: March 03, 2015 %eft smov4, May 25, 2015 miww4./ October 30, 2018 eitAwlint .92w4: The certification basis for the changed Gulfstream G4 V aircraft as described in this certificate is as follows: a. The type certification basis for Gulfstrenm G4V ninslanes is shown on TCDS Al2EA for parts not changed or not affected by the change. b. The certification basis for parts changed or affected In the change since the reference dai of application, July 23, 2014, is shown on TCDS Al2EA. In addition. the npphcant has complied with 14 CFR Part 25 as specified in the sections listed below. Regulations as shown on TCDS Al2EA [Amendment 25-0 through 25-56i: 25.301(a), (b); 25.303; 25.305(a), (b); 25.307(a); 25.341(a); 25.365(a), (b), (O, (d); 25.561(e); 25.581(a), (b), (e); 25.601: 25.60300. (b). (a); 25.606(a); 25609(a). (b): 25.611; 25.613(a). (b). (d): 25.615(a); 25.619(a), (b). (c); 25.625(a). 25.771(a); 25.777(a), (e); 25.789(a); 25.1301(a), (b), (o), (d); 25.1309(a), (b), (e), (d), (a), (g); 25.1322(a), 0O, (e). (d); ;5.1333(a). (b), (c): 25.1353(a), (b); 25.1357(a), (e); 25.1431(a), (b), (e); 25.1501(a), (b); 25.1523(n), (b); 25.1529; 25.1585(a), (b). Regulations at a later amendment level than specified In TCDS Al2EA: 23.29 [Am& 25.721; 2.5.571(a). (b) [Arndt 25-45j; 25.86900(4) [Arndt 25.1131; 25.1307(e) [Arndt 25-721; 25.1329(e), (i) [Arndt 25.1191: 25.1351(a) [Muth 25.721: 25.138100, (b) (Amdt 25-72); 25.1457(a), (b), (c), (d)(1)0),(2),(3).(6), (e), (g) 'Arndt 25-124); 25.1581(a), (b), (d)(Amdt 25-72), 25.1583(h) (Am& 23-72). Spotlit Conditions 25-665-SC, Special Conditions: Gulfstream Aerospace Cotpomtion, Model GV-SP Airplane; Non-Rechargeable Lithium Battery Installations, Docket No. FAA-2017-0367 (Applicability Limited to Universal Avionics UNS- 'Espy Flight Management System installed in Configurations -04 and -05). The certification basis for the changed Gulfstream GV aircraft as described in Ibis certificate is as follows: a. The type certification basis for Gulfstream GV airplanes is shown on TCDS Al2EA for pans not changed or not affected by the change. b. The certification basis for pans changed or affected by the change since the reference date of application. January 27, 2015, is shown on TCDS AI2EA. In addition, the applicant has complied with 14 CFR Pad 25 as specified in the sections listed below. (Continued on µage 4) Any eltorotion of this artlelooco Is panish.41* by • has of eat Oireupelaf $1.000. or trivisaist Inc Inroatizoo 3 rues, w Cerra. DA Tam 0110.:.1(30.4,) IASI 3 of I PAGES This corcltleat• wy b• troduncroci Zr. 110741tifill,W ZAR 21.47. SDNY_GM_02783708 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240630 EFTA01326223 SDNY_GM_02753709 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 I EFTA_00240631 EFTA01326224 %Whit *Ws of pAmerita !apartment of ggranspo dation - eberati Ablation Abministration $upplementui Zgpe Certificate (Continuation Alpe° Verk r/f:"MeMet: March 03, 2015 %ter- 07.4.:4;44se May 25, 2015 rink ittivowtf./ October 30, 2018 en.e0;w4;34 • 4.4.46rvi/4w”.9.- Regulations as shown oa TCDS Al2EA 'Amendment 254 through 25411: 25.29; 2$.301(a), (b); 25.303; 25.305(a). (b); 25.307(a); 25.341(a); 25.365(x), (b), (c), (d); 25.561(e), (d); 25.571(a), (b); 25.581(a), (b), (e); 25.601; 25.603(a), (b). (a); 25.60500; 25.60900. (b); 25.611; 25.613(a), (b), (c), (d); 25.610(a). (b), (c); 2362500: 2527100; 25177(4 (a); 25.789(a); 25.1301(a), (b) K2 (d); 25.1307(c); 25.1309(0), (b), (e), (d), (e), (0, (g% 25.B16(b), (a); 25.1322(a), (6), (e). (d); 25.1333(4 (b), (o); 25.1351(a); 25.135300. (b); 25.1357(a), (a); 25.138100, (b); 25.1431(a), (b), (c); 25.1501(a), (b); 25.1523(o), (b); 25.1529; 25.1581(o), (b), (d); 25.158309; 25.1585(a), (b). Regulations at a later amendment level than specified In TCDS A l2EA: 25.869(ng4) [Am& 25.113); 25.1329(c), (i) (Arndt 25.1191: 25.1457(a), 00, (c), (d)(IX0,(2),(3).(6), (a), (0, (g) [Arndt 25-124) Special Conditions 25-ANM-I08, Special Conditions; Gulfstream Aerospace Corporation, Model Gulfstream CV, High Altitude Operations. Docket No. NM-112; Paragraphs 1(aXbX4 25465-SC, Special Conditions:. Gul fstream Aerospace Coq/oration, Model GV-SP Airplane, NonIFIechargeabk Lithium Battery Installations. Picket No. FAA-20I7-0367. (Applicability Limited to Universal Avionics UNS- lEspw Flight Management System installed in Configurations 44 and .05). —END-- My ****** tam of ells cortlelomo L puelaluebe by • tine or we 114*.enril *Lear or IsprUpon tut esesollag I imam. or both. FM Feu I110-2-10.4•11 Pia 4 of 4 Pal This corn/lost* ,say to trossferrod Is *mordant Ida yet 11.0. SDNY_GM_02753710 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240632 EFTA01326225 SDNY_GM_02753711 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240633 EFTA01326226 feeteme e Eliontne crew,ream 0 US Dremnort MAJOR REPAIR AND ALTERATION wagon 21100010 sot eiliA uneasy e Ting:futon (Airframe, Powerplant, Propeller, or Appliance) &woe esaotion Ads1risibton INSTRUCTIONS hull or type as entries. See Title 14 CFR §43.9. Part 43 Appendix 8. and AC 4194 (or subsequent foremen thereof) for instructions and disposition of this form This report is required by law (49 U.S.C. §44701). Failure to report can road? in a ovil penaky for each such violation. (49 U.S.0 §46301(a)) Nationality and Registration Mark Serial No. N120JE 1085 1. Aircraft Make Model Sores Gulfstream Aerospace G-IV Name (As shown on regostraDon certificate) Address (As Shown on registration carnivore) Morin 6100 RED HOOK QUARTER 83 a. Owner JEGE LLC cry St. Thomas sm. Foreign be 00802 cage, Virgin Islands 3. For FAA Use Only 4. Type 6. Unk Identlfkatifin Repair AllefillIOn Unit Make Model Serial NO. al 0 AIRFRAME (As CIOSChbed ifl MINI I above) 0 ID POWERPLAt4T 0 0 PROPELLER Type 0 APPLIANCE 0 Alenutectiger I. Conformity Statement A. Agency's Name and Address B Kind of AgenCy ismsGunstream Aerospace Services COrpOration U S Collated Mecherie I laerulacturer &Ss 7 Char Drive Fetal:, Centagel Methane C. Certificate No. cie Westfield am MA i Coble:al Repair Sieben be 01085 own, USA Cans:sew maintenance Organs/bon LEGRO39G D. I candy that he repair andlor alteration made to the unit( ) identified in item S above and described on the reverse or attachments hereto have been made in accordance with the requiremee4s of Pan 43 of the U.S. Federal Aviation Regulations and that the information Nmished herein is true and cared to the best of my knowledge. re Extended range fuel Signature/0mo of Authorized Intkviduat , Per 14 CFR Pin 43 0 APP. 8 Benjamin Thomas Jones z ....4—.... -- 09 November 2018 7. Approval fo Wurn to Se Pursue I to the authority given persons &Pealed below, the unit identified in item 5 was nseecteo in the manner presorted by Me Administrator of the Federal Aviation Administration and is Approved 2 0 Rejected FAA Flt Standards Persons Appeared by Canavan Maintenance Organization Department or Transport Inspect« BY Other (Specify) FM Designee I Repair Station Inspection Au cation Corti ale Of Signature/Date of Aumon 1101 Designation No. Dean Mathew Dickman c.... --09_November 2018 LEGRO39G FAA Fenn 3370041i SDNY_GM_02753712 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240634 EFTA01326227 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record An alteration must be Compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. S. Description of Work Accomplished Minor° space is ragweed attach addrional shears Idenlify min soccer nahonabty and regOkation mark and dale work comaierca) N120JE 159 November 2018 Nationale), and Registration Mark Date Performed Major Repair to the Forward Lower Side of the Baggage Door in accordance with 1159RD13459-3 and Forward Upper Side of the Baggage Door in accordance with 1159RDB459.5 Standard Repair Intl - Frame Cracks. Baggage Door. Gulfstream Standard Repair Drawing 1159RDB459 Rev. J is FAA Approved per Gulfstream GIV SRM 52-00-02 Rev. 16 Dated December 15. 2017 and Engineenng Disposition 50019580.1.1 by Stephen Alois Dated November 7, 2018. This Repair Does Not Impact Aircraft Weight and Balance or the ICA. END Additional Sheets Are Attached FAA Fenn 137 (Wai SDNY_GM_02753713 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240635 EFTA01326228 ee /41....,7703 core Eleceobc Weeny Nun. MAJOR REPAIR AND ALTERATION 2.21/2011 erFAA UN Only us oftwonn et Orntoenol on (Airframe, Powerplant. Propeller, or Appliance) Federal Aviation winawasten INSTRUCTIONS: Pnnt or type all entnes. See Tele 14 CFR $43.9. Parl 43 APperdix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is requred by law (49 V.S.C. $44701). Fatale report can resiA in a civil penalty for each such holabcn. (49 U S C §46301(a)) Nationality and NegntrabOn Mark Serer No. N120JE 1085 1. Aircraft Model Senes Make GULFSTREAM AEROSPACE G-IV N/A Name (As shown on teolfration cerflficate) Address (As shown on/migration contralto) Meese 8100 RED HOOK QUARTER 83 t. Owner JEGE LW G., ST THOMAS sew FOREIGN z,,, 00802 cony VIRGIN ISLANDS 3. For FAA USO 0 ly 4. Type a Unit Identification Repair Alteration Unit Make Model Serial NO. O AIRFRAME (As descnbect in nem 1above) IZI O O PON£RPLANT El CI PROPELLER Type O . APPLIANCE mraacia, 6 Conformity Statement A. Agency: Name and Address B. Kind of Agency an Galmmargigaenaces ration u 5 corencesee Mechanic I lAanuhaurer man. 7 Char Drive Foreign CerlaCated Mechem C. Certificate No. cq Westfield Sine MA / Cannoties Raper 3NbOn a. 01085 Canty USA Certif.:ad atenterence Organzatan LEGRO39G O. [certify that tne repair and/or aeration made to the unlit ) identified in item 5 above and described on the reverse or attachrnems hereto have been made in accordance with the restatements of Part 43 of the U.S. Federal Aviation Regulahons and that the intortnatson furnished herein is Ina and correct to the heft of my knowledge. Extended range fuel SignaturerDate of Authorized Ince/ -1 per 14 CFR Part 43 • App. B Benjamin T. Jones „.,..-- t_--_... 26/JUIJ2018 . pproval for R - talcs Pursuant to the authority given persons specified below. the Linn identified in item 5 was inspected n the manner prescribed by the Administrator of the Federal Aviation Administration and is Approved 2O Rejected FM Fit. Standards Person, ANNOYS by Censaen manufacturer Maintenance Organization orpartmen of Transport inspector BY Other (Sporty) FM Designee 1 Repar Station Inspection Authorization Certificate or Signature/Date reed indwismil Designation No. Dean M. Di ___ 26/JUL/2018 LEGRO39G FAA Forrn 337 rioter SDNYGM02753714 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240636 EFTA01326229 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record An alteration must be compatible with all previous alterations to assure continued contort* with the applicable einvorthiness requirements. a. Description of Work Accomplished (It more space is required. attach additional sheets. Identify wen aircraft nationality and reetstrabon mark and date work completed.) N120JE 26/JUU2018 Nationality and RegitratiOn Mark Date 1.) Reworked the LH Thrust Reverser P/N 1159P41460-3 S/N A088 LH Fwd Mount Holes 2L - 4L and 7L - 11L. Installed The Following Repair Bushing Part Numbers In Locations Listed; 21. - GSL405420001.11-5474 31. - GSL405420001-11-5312 4L - GSL405420001-11-5474 7L - GSL405420001.11-5312 8L - GSL405420001.11-5940 9L - GSL405420001-11-5312 10L - GSL405420001-11.5940 11L - GSL405420001-11.5312 2.) Reworked the RH Thrust Reverser P/N 1159P41460-4 S/N A088 RH Fwd Mount Holes 3R,7R,13R -10R. Installed The Following Repair Bushing Pan Numbers In Locations Listed; 2R - GSL405420001.11.5746 3R - GSL405420001.11.5320 4R - GSL405420001-11-5781 5R - GSL405420001-11-5322 7R - GSL405420001-11-5312 BR - GSL405420001-11-5946 9R - GSL405420001-11-5312 10R - GSL405420001-11-5754 11R - GSL405420001-11-5312 Repairs Accomplished in Accordance with and Substantiated By Gulfstream General Service Letter GSL405420001 Rev B., Engineering Disposition SC18934.14.9.1.1 and SC18934.16.1.1.1 This Repair Does Not Impact Aircraft Weight And Balance. Or The ICA. 3.) Reworked the LH Inlet P/N 1159P41100-69 S/N A086 LH Fwd Mount Holes 13L. 151. - 20L and 231. - 25L then Installed Repair Bushings PIN GSDD405411001-11 as required. 4.) Reworked the RH Inlet PIN 1159P41100-71 SIN A086 RH Fwd Mount Holes 6R, 12R, 17R - 19R and 24R then Installed Repair Bushings PIN GSDD405411001.11 as required. Repairs Accomplished in Accordance with and Substantiated By Gulfstream General Service Letter GSL405411001 Rev C., Engineering Disposition SC18934.14.10.1.1 and SC18934.16.11.1.1 This Repair Does Not Impact Aircraft Weight And Balance. Or The ICA. END Addnional Sheets Are Attached FAA Form 337 {torn SDNY_GM_02753715 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240637 EFTA01326230 Fr, Amos! Elena"K Treaing Nuen: pre No 1000020 91 Ilbf vs oromurer MAJOR REPAIR AND ALTERATION moon .. FAS Use Puy a transponsess (Airframe, Powerplant. Propeller, or Appliance) From Annie, Aantatistration INSTRUCTIONS: Pont or type aN entries. See Tele 14 CFR §43.9. Pan 43 Appendix 8. and AC 43.9.1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 544701). Failure to report can result in a civd penalty for each suCh violation. (49 U.S.C. §46301(a)) Nationality and Registration Mark $erial No. N120JE 1085 1. Aircraft Make Model GULFSTREAM AEROSPACE G4V N/A Name (As shown on mixers:ion certracate) Address (As shown on registration certificate' Mann 6100 RED HOOK QUARTER B3 2. Owner JEGE LLC cc, ST THOMAS sm. FOREIGN 20 00802 cowr y VIRGIN ISLANDS 3. For FAA Use Only 4. Type S. Unit Identification Reis* Alteration Unit I Make Model Serial No 0 AIRFRAME (As clescncecl on Item 1 above) Z El • POWERPLANT El • PROPELLER type 0 APPLIANCE El Merestectiew 6. Conformity Sta ernent A. Agency's Name and Address B. Kind of Agen y ere Gulfstream Aerospace Services Corporation u. s. Garlaraterl Meehan I Sran...ackrer Mons 7 Char Drive Foreign Cathcatee Mechanic G Certificate No Ger Westfield Si." MA i Certificated Repair Staten a• 01085 cwwv USA Coreficateo Ulaimenance OrgarCakin LEGR039G O. I certify that the repair andior alteration made to the unit( ) id nofied in item 5 above and described on the reverse or attachments hereto have been made in accordance vett the requirements of Part 43 of the U.S Federal Aviation RegAations and that the information furnished herein is true and Coned to the best of my knowledge. Extended range fuel &puha Authorized Indi per 14 CFR Part 43 El n00. B tmin ej- ; ----T---" 26/JUN/2018 7. Approval for Return to Service Pursuant to the authority g ven persons specified below. the unit identified in item 5 was -nspected in the manner prescnbed by the Adnwestralor 01 the Federal Aviation Administration and is Approved 9 IMI Rejected FAA Fn. Standards Manufacturer MaintenanceOrganization Meintenan Persons Approved by Gainsays Inspedor Department of Transport BY Other (Savory) FAA Designee I Repair Station Inspection Autnonzation Ceti Kate or Signature/Date of Authorized Individual Designation No. Wiliam Stucklen 26/JUN/2018 LEGR039G FAA Form 337 norm SDNY_GM_02753716 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0O240638 EFTA01326231 NOTICE Weight and balance or operating limitation changes shall be entered in the appropnate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. I. Description of Work Accomplished (IImore space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) N120JE 26/JUN/2018 Nationality and Registration Mark Date Performed rework of rudder actuator forward attach fitting - F.S. 757.562 in accordance with Gulfstream drawing No. 1159RDB729, No Revision, -901 inst. This major repair is substantiated by FAA form 8100-9. dated 06/15/2018, Project No. TR-07-2018-0014. from Gulfstream Savannah Authorization# ODA-511131-CE. cert 0336099. This repair has no effect on current ICA. Weight and Balance effect: None AFM Supplement: None Performed the following repairs to flight control hinge fittings in accordance with Gulfstream drawing No. SE05000102. Rev. E. STD. Repair - Control Surface Hinge Fittings: 1) Performed repair SE05000102-913D6-20 to UH #3 Aileron hinge fitting P/N 1159WM20202-5. Bore measures .4065", installed 5E05000901-913D6-20 bushing. 2) Performed first increment 0/S repair to UH Aileron #1 hinge holes (3 places). Bores measure .3280". installed NAS6605D4OX. NAS6605D54X, AND NAS6605066X 0/S hardware. 3) Performed repair SE05000102-911P5-21 to UH Elevator hinge #4. Bores measure .3906" - .3911", installed SE05000102-911P5-21 repair sleeve. 4) Performed repair SE05000102-912S88-1 to UN Elevator trim tab hinge# 1 inboard lug. bore measures 3905". installed SE05000102-912588.1 bushing. 5) Performed repair SE05000102-911P2-5 to UH Elevator trim tab hinge# 1 outboard lug, bore measures .4063", installed SE05000102-911P2-5 sleeve. 6) Performed repair SE05000102-911P1-5 to R/H Elevator trim tab hinge# 1 outboard lug, bore measures .3905", installed SE05000102-911P1-5 bushing. 7) Performed repair SE05000102-911P1-5 to R/H Elevator trim tab hinge# 2 outboard lug, bore measures .3905", installed SE05000102-911P1.5 bushing. 8) Performed repair 5E05000102-914P1-28 to Rudder top hinge and fitting. bores measure .389r. installed 5E05000901.914P1-28 bushing. 9) Performed repair SE05000102.914P1-27 to Rudder middle hinge and fitting, bores measure .3898", installed SE05000901.914P1.27 bushing. Et Additional Sheets Are Attached FAA Form 337 i loos) SDNY_GM_02753717 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240639 EFTA01326232 T1O4 DEPARIWO CR TRASSPC*TAIX.4410IIPLU. AY.A7O.1•ZAI0SSTRA STANDARD AIRWORTHINESS CERTIFICATE polinounams a ists/if Fearempalk I sow!. Maus N$201 1 OUUSTREMINEM(SAGE MN revert . K••••••21 linsennisini•••• tiSileteerna•laillsnois• aSC 114111.••••••• • I es -Owe One 'Mb s ••••••••••••Manlailatermal••• atininte.nto ow in owl•••••••••• •INtent••••••••••Ytaii•leeniss • NONE •••teratem• Maori* MOS 90./00 test Raw. waste Flews, ZarSer2S ROSIV2CCO az:Az, as, wealle rtptivi sturtrattildratil 11•SCOMICATIMST “ClUth/0•11•11A/00// reit,e ~Jig ••• SDNY_GM_02753718 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00240640 EFTA01326233 _ SONY_GA.4_02753719 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 0024064I EFTA01326234 0.40 VS/ I CO illOisca CEPARTMEN1 Of TRANSPORTATION MEWL AVIATOIMMISTRATION STANDARD AIRWORTHINESS CERTIFICATE alevort op I sntiniCitata NO litCtl I MOW/ KRA& I unwire i WSTWO.1 100. Walla N212JE Gultatreas G-IV 1085 Tramline t AVICW, MOVISI Twessaim sea maw •••••••14C 6001011.140••••••••••••sto nil DSO /anat. mad Dan leadele YM st= Imintossis ern ant* pep is 0.0moiningapsiOnlialson•Ina innatenem es • plait wits NONE • toms mensal** nal aphigypelpiakkiowns mini — —a at ®yeti h. wit Pete.Wel b1101bFYKI teSOIP.M.5w It 05/23/2000 S019 A.S.S•ppla • Arm minus". 4.* nese. V rwisms• an" henna marital WE MI IPMAPVIIIIJAMPL PIPPallaW06 1.0.• non 4 9141$1,1 SDNY_GM_02753720 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00240642 EFTA01326235 SDNY_GM_02753721 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00240643 EFTA01326236 to co UNITED STATES OF AMERICA H DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION 0 STANDARD AIRWORTHINESS CERTIFICATE Xl o 1 NATIONALITY AND 2 MANUFACTURER AND MODEL .- ft.. ..;.: 3 AIRCRAFT SERIAL NUMBER 4 CATEGORY H REGISTRATION MARKS N120JE GULFSTREAM AEROSPACE -a:IV 1085 Transport 5 AUTHORITY AND BASIS FOR ISSUANCE / c:"..-\ ••• - ..„. , / •. , t m This airworthiness certificate is issued pursuant to 49 U.S.C. § 44704 and certifies that, as of the date otissuance, this aircraft has been inspected and found to O conform to its type certificate and be in a condition for safe operation. This aircraft meets the requirementief the applicable airworthiness standards in Annex 8 Xi to the Convention . on International Civil Ariabon. except as fellows: CI i. • 70 1 NONE Xl ;f t'fl C) 70 ea. 6 TERMS AND CONDITIONS LE) Unless sooner surrendered, suspend,revoked, or a termination date is otherwise established by the FAA, this airworthiness certificate is effec ive as long as maintenance, preventative maintenance, and alterations are performed per the applicable FederatAviation Regulations and the. aircraft is registeredin the United States. DATE OF ISSUANCE FAA REPRESENTATIVE DESIGNATION NUMBEF .10 R 05/23/2000 AEA-FSDO-25 Co PZ-L: ag t. cm a Any alteration, misuse, or reproduction of this certificate for a fraudulent purpose may be punishable by certificate revocation, fine, and I or imprisonment UT THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT PER THE APPLICABLE FEDERAL AVIATION REGULATIONS. o ; AA Form 8100.2 (11-2016) Previous Edition Dated 0.4-11 May be Used Until Depleted La, CL ,13 m A p EFTA01326237 a p VIIONV1)10 Alto VINOHY1)10 Se Tr WEI 6 90U Uhl US NOUNii/S10311 141,210WV V114 HIIA1 031Id SDNY_GM_02753723 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240645 EFTA01326238 co m -o 0 m n •- , UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION . STANDARD AIRWORTHINESS CERTIFICATE , mr,e,m„,I.,NC a IMOSACTU.0 NO Oa ,'...........—• -rinv i e,. .: —: cartoore 1. ractorionar Doty roes 0," -C ' • 7 A • N 120JE . GULFSTREAM AE, RDSFACE—G:IV Transport / eLs,, ...en. ri ,.. 0 Mt ennnesarteceb b WI Fame faille i "Ma menu Weeannet Si eye ha tan ithAtm eaWV in Cotten b Owe mica skl le basalts Wide art No Sint se telleillitit tor liplcatio inners zurdn•kne. II m .b as -wets,a" irinabv Oil .... sall • law % -0 • tr NONE • IteallmOccoarail • • ,.' UMW MOW suntnar rye.; el • lontate. skis is ~So ~ALSO try to FM. Ea entrthepose ands is Seiko a bie mm' grey., Wawa al Sett on pricaned serfs woke* ireplrithissal anion aim as nil irre0.10. 1 . Wiwi Stela . -o WM CIilliatba OA.etitsemera ' f,, . 0....:I.Alle.PONS 80523/2000 cajt, •J; • OS.i • AEA.FSDO-25 AffiNnim eat a twneosio. at IN* was,Poe WsamMi ts eing.by ream,motion rm. Ardis Inebsellent ..."-....-....._.,.....-.- DIM CERTIFICATE 41ST IIE OiSPLAYED ti ME PaalAFT PER THE APPLICAKI FECtIV4 AVIATION REGULA11048. ftham II1C04 01401M Orwais San Ofted04.116,/ tio UndUndlOsprobill 9° 9) E p a) •@, P, ••-•1 EFTA01326239 All0 V1)40 so u nu LIU as N • lignSI0311 14 8W Ind HAIM 031Id SDNY_GM_02753725 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240647 EFTA01326240 Orni APPOY00 on< Ime.00 ionow 0,2007 OMB No. 2120-0020 MAJOR REPAIR AND ALTERATION ' 117 0 (Airframe, Powerplant, Propeller, or Appliance) For Pm um OW US Deortmont of Tronsocnssol 'Odin, Animon mminstroson INSTRUCTIONS: Pnnt or type as entries. See FAR 43.9 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition o this form This report is required by law (49 U S C 44701) Failure to report can result in a civil penalty for each such violation (49 U.S C. 46301(a)) Nationally and Registration Mark Serial No. USA N212JE 1085 1. Aircraft Model Series Make G-IV GULFSTREAM AEROSPACE Name (As storm on registration certificate) Address (As shown on registration certificate) Mans 6100 Red Hook Quarter 83 2. Owner JEGE LLC ay ST Thomas Stud Zo 00802 ciikrov Virgin Islands 3. For FAA Use Only 4. Type 5. Unit Identification Repair Alteration Unit Make Model Serial No. 0 9 AIRFRAME (As described in item 1 above) 0 0 POWERPLANT 0 0 PROPELLER APPLIANCE is 0 0 Maitaciett 6. Conformity Statement A Agency's Name and Address B Kind of Agency I Manufacturer International Jet Interiors _U.S. Certificated Mechanic C. Certificate No. 2221 Smithtown Ave Foreign Certificated Mechanic Ronkonkoma, New York 'Mc Certificated Repair Station CRS I1JR439Y 11779 USA Certificated Maintenance Organization D. I certify that the repair and/or alteration made to the unit s) identified in item 5 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Extended range fuel per Signature/Date of Authorized Individual . 14 CFR Part 43 0 App B Thomas Norden Date. 2/20/2014 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit identified in item 5 was inspected in the manner prescribed by the Administrator of the Federal Aviation ACITiniSIta000 and is tE) APPROVED 0 REJECTED FM Fit. Standards Persons Approved by Canadian Manufacturer Maintenance Organization Department of Transport Inspector BY Other (Specify) FM Designee X Repair Station Inspection Authorization r ...\ Certificate or Signature/Date of Authorized Indrodual Designation No. ,Kl aca e....4._ CRS I1JR439Y Thomas Norden Date: 2/20/2014 • FAA Form 337 rio-osi SDNY_GM_02753726 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240648 EFTA01326241 NOTICE Weight and balance or operating limitalico changes shall be entered in the appropriate aircraft record An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and dale work accomplished.) USA N212JE DATE Nationality and Registration Mark 2/20/2014 KGS ELECTRONICS II5VAC, 60FIZ, I000VA INVERTER SYSTEM INSTALLATION I.) Removed 20. PIN: AK-55140M 28-I2VDC converters. 2ca. PIN: XD600-1 amplifiers, lea. P/N: XD600-6 amplifier, and lea. P/N: BBK-2AH keep alive battery. Installed a KGS Electronics I I SVAC, 60HZ, 1000VA inverter system in accordance with DB Integrations, LLC document No. 140121001 titled I I5VAC 60HZ Inverter Wiring Diagram, revision (0), dated February 5, 2014 which was approved under FAA form 8110.3 dated Febuary 11, 2014 (attached) for systems and equipment. 2.) The structural aspects of the inverter installation were accomplished in accordance with DB Integrations, LLC document No. 140205001 titled 60HZ Inverter Structural Installation, revision (0), dated February 5.2014 which was approved under FAA form 11110-3 dated February 13.2014 (attached) for structures. 3.) The structural aspects of the outlet and circuit breaker installations arc deemed a minor alteration, which were performed in accordance with applicable sections of AC43.13-I B and AC43.13.2G. 4.) The equipment list has been revised. 5.) The weight and balance has been revised. 6.) An electrical toad analysis has been performed and found not to exceed 80% of the full generator capacity. 7.) Instructions for Continued Airworthiness (ICA) are incorporated into DB Integrations. LLC document No. 140213002. revision (IR.). dated February 13, 2014 and have been provided to the operator for incorporation into the aircraft inspection/maintenance program. 8.) A Logbook entry has been made reflecting this modification. 9.) The work described, has been found to be in conformity with the above mentioned approved data and continues to meet the airworthiness criteria under which it was originally certificated. Work Order No. 14104, on file at this agency, covers the above described work. No Further Entries CEI Additional Sheets Are Attached FM Form 337 (10-06) SDNY_GM_02753727 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240649 EFTA01326242 U.S. DEPARTMENT OF TRANSPORTATION 1. DATE FEDERAL AVIATION ADMINISTRATION February 11.2014 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MAKE 3. MODEL NO. 4. TYPE MeV* E Sint PMCOSIV. arc I 5 NAME OF APPLICANT Gultstream Aerostat. G.IV Airplane DS mtegraiions. I.LC LIST OF DATA 6. IDENTIFICATION 7. TITLE Report:0000214.1085. Rev. Wt. 130 Hz T50 Invader Modification' Dale: 02/11/2014 NOTES: t. This approval coven Medial. design aspects onhr on Airplane Model G-IV. sin I 065 ands not intalialion approval. 2. The au0lorted agency retumng the Wadi to sena is responsible to determine compeance *II the above data. 3. This approval is lot ele*foal engineering design data only. It indraiNs IS data listed above densanstees coerces** or* with the regubtions specified by paragraph and subparagraph listed below as 'Applies* Rechirernents" 8. PURPOSE OF DATA To support Major Alteration FM Form 337 for sin 1065. The approval is design data approval only and Is not instate* approval. O. APPLICABLE REQUIREMENTS (List specific sectcas) 14 CFR Pan 25.0; 25.135100M Nerd 25:72; 25.1357 (aKb)(c)Ard 25.123 10. CERTIFICATION • Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under 14 CFR Part 183. data listed above and an alleChed sheets numbered have been examined in accordance with established procedures and found to comply with applicable reenactments of the Airworthiness Standards fisted. 0 Recommend approval of these data I (1M0) Therefore a Approve Mose data II. SIGNATURES) OF DESIGNATED ENG7RING 5 'SENTATivE(SI 12 DESIGNATION NUMBER(S) 13. Cl ASSiFICATION(S) David J Richards .2( , ..............t.k .., 42.../ f DERT 955091-NE Systems and Ethripnera Eleclncal FAA Form 8110-3 (01,10) SUPERSEDES PREVIOUS EDITION SDNY_GM_02753728 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240650 EFTA01326243 SDNY_GM02753729 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240651 EFTA01326244 U.S. DEPARTMENT OF TRANSPORTATION I DATE FEOMAL AVtATiOn ADMINISTRATION 2/13/2014 STATEMENT OF COMRUANCE WITH AIRWORTHINESS STANDARDS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MAKE 3. MODEL a TYPE (Aircraft. Engine. Propeller. etc.) S. NAME OF APPLICANT Gulfstream G-IV Aircraft DB Integrations Aerospace Corporation UST OF DATA 6. IDENTIFICATION 7. TITLE 140205001 60 Hz Inverter Structural Installation, Sheets I through 4, Initial Release, dated February 5, 2014. Notes: 1. This approval is for engineering design data only. It indicates the data listed above demonstrates compliance only with the "Applicable Requirements." Compliance with additional regulations not listed here may be required. This form does not constitute FAA approval of all the engineering data necessary for substantiation of compliance to necessary requirements for the entire alteration. 2. TCDS is Al2EA. 8. PURPOSE Of DATA: Drawing 140205001 installs a 60 Hz inverter on an existing shelf on Gulfstream Aerospace Corporation Model G- IV, A/C S/N: 1085, as a major alteration. 9. APPLICABLE REQUIREMENTS (List specific sections): 14 CFR dated February 1, 1965, including Amendments 25-1 through 25.56: 25.301 Loads, 25.303 Factor of safety, 25.305 Strength and deformation, 25.561 Emergency Landing Conditions —General, 25.601 Design and Construction —General, 25.603 Materials, 25.605 Fabrication methods, 25.607 Fasteners, 25.789 Retention of items of mass in passenger and crew compartments. 10. CERTIFICATION -Under authority vested by direction of the AdrniMstrator and in accordance with conditions and limitations of appointment under 14 CFR Part 183, data listed above and on attached sheets numbered have been ermined in accordance with established procedures and found to comply with applkable requirements of the Airworthiness Standards listed. O ROCOMMadd SPINOVil of these data I (We) therefore a Approve these data 11. SIGNATURE(S) Of DESIGNATED ENGINEERING REFIIESENTATIVE(S1 12. 0CSIGNATION NUMEIER(S) 13. ClASSIFICATION(S) CA T\ CLVN ICi)m)li N- DERT-831129-CE STRUCTURES FAA Fpm $110.3 (O3/1O1SUPERCEDES PREVIOUS REVISION SDNCGM_O275373O SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240652 EFTA01326245 SDNY_GM02753731 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240653 EFTA01326246 U. S. DEPARTMENT OF TRANSPORTATION I DATE FEDERALAVIATION ADMINISTRATION 2/18/2014 STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2.MAKE 3.MODEL NO. 4.TYPEfAhOwre. Craw. Propellor.It) sNAME OF APPLICANT Gulfstream • G-IV Airplane International Jet Interiors LIST OF DATA tit IDENTIFICATION 7,11TLE TP 268821-14 Skandia. Inc. Flammability Test Report Rev A Bunsen Burner Testing Dated 02/18/2014 Test Specimen P/N's 1 (represents floor covering) 2 (represents floor ducts) 3 (represents seat bases) 4 (represents cockpit. sidewalls & pedestal) Notes: 1) Work accomplished under Skandia Inc. WO 0 268821.14, Ref Document ID 94995. 2) Flammability test witnessing only, does not constitute installation approval of materials. 8.PURPOSE OF DATA Demonstration of compliance with material flammability requirements in support of Major Repair & Alteration for SIN 1085 9.APPLICABLE REQUIREMENTS dist specific sections) 14 CFR Pan 25.853 (a) Arndt 25-116 Appendix F Pad I (a)(1Xi) Amdt 25-111 14 CFR Part 25.853 (a) Arndt 25-116 Appendix F Pan I taxixie 10.CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and imitations of appointment under 14 CFR Pail 183. data listed above and on attached sheets numbered have been examined Si accordance with established procedures and found to comply with applicable requirements of the Airworthiness Standards listed. 0 Recommend approval of these data I (ibb)Therefore )tiaprove these data , I I.SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE 12.DESIGNATION NUMBER(S) 13.ctASSIFicATiOmS) )4Q \bObit 'xi 1 gl Ja- Biberstein -FAA DER DERY-832780-CE Structural Special orm 8110-3 (03ile)•SUPERSEDES PREVIOUS EDITION SDNY_GM_02753732 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240654 EFTA01326247 SDNY_GM02753733 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240655 EFTA01326248 ram Approved iEllevonc Trseiro Noce' OMB NO 2120-0020 MAJOR REPAIR AND ALTERATION iirkoncor 0 (Airframe, Powerplant, Propeller, or Appliance) Fee FArtUe•Only US Doperonant of Trecepflon Fedenl Avladon Adminievetion INSTRUCTIONS Print or type all entries See FAR 43 9 Appendix B. and AC 43.9.1 (or subsequent revision thereof) for instructions and disposition o this form. This report is required by law (49 U.S.C. 44701). Failure to report can result in a civil penalty for each such violation (49 U.S C. 46301(a)). Nationality and Registration Mark Serial No. USA N212JE 1085 1. Aircraft Model Series Make G-IV GULFSTREAM AEROSPACE Name (As shown on registration certificate) Address (As shown on registration certificate) Aedess 6100 Red Hook Quarter 2. Owner JEGE LLC cay St Thomas sine A, 00802 corm Virgin Islands 3. For FAA Use On 4. Type 6. Unit Identification Repair Alteration Unit Make Model Serial No El i7i AIRFRAME (As described in item 1 above) 0 0 POWERPLANT 0 PROPELLER APPLIANCE T10F 0 • hiestellOlaW 6. Conformity Statement A. Agency's Name and Address B Kind of Agency I Manufacturer International Jet Interiors U.S. Certificated Mechanic C. Certificate No. 2221 Smithtown Ave Foreign Certificated Mechanic Ronkonkoma, New York k Certificated Repair Station CRS I1JR439Y 11779 USA Certificated Maintenance Organization D. looney that the repair and/or alteration made to the unit(s) identified in item 5 above and described on the reverse or enactments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Extended range fuel per Signature/Date of Authorized Individual 14 CFR Part 43 0 APP. 8 Thomas Norden Date: 9/19/2013 C---- Il aelAl .t ) elra -....1 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit identified in item 5 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is (2) APPROVED 0 REJECTED FM Fit. Standards Persons Approved by Canadian Inspect« Manufacturer Maintenance Organization Department of Transport Y Other (Specify) FM Designee X Repair Station Inspection Authorization Certificate or 'Signature/Date of Authonzed Individual Designation No. CRS I1JR439Y ", . Thomas Norden Date: 9/19/2013 kil a eir FM Form 337 0005) SDNY_GM_02753734 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240656 EFTA01326249 NOTICE Weight and balance or operating limitation changes snail be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required. attach additional sheets, Identify with aircraft nationality and registration mark and date worn accomplished) USA N212JE DATE Nationality and Registration Mark 9/19/2013 Modified the existing Cabin Entertainment System in accordance with Electrical Drawing listed below ( Note: reference FAAIDER approved Structural Drawings for provisions for all Audio and Video equipment installed at this time on FAA 337 Form, this date). Dwe No. Date Rev Title PA-G1V-1085.2501 8/21/13 B CABIN ENTERTAINMENT SYSTEM (MOD) ELECTRICAL DRAWING The above listed wiring diagram is FAA/DER approved by W.C. Janzer (DERT-510187-CE), Systems and Equipment, Electrical Equipment via FAA Form 8110-3 dated 8f2 I /13, attached to this 337 Form. Electrical Load Change is negligible & dots not exceed the 80% electrical power generating system on the aircraft. Complied with a EMI-RFI Test Flight, there were no adverse effects on any other systems. The Aircraft's Scheduled Maintenance Program is not altered by this installation. The cabin entertainment system components are considered to be "On Condition Items". A supplement to the aircraft equipment list and copies of the wiring diagrams listed above has been provided to customer and must be added to the aircraft's records. The work described, has been found to be in conformity with the above mentioned approved data and continues to meet the airworthiness criteria under which it was originally certificated. Work Order No. 13127, on file at this agency, covers the above described work. A Logbook entry has been made reflecting this modification. No Further Env' 0 Additional Sheets Are Attached FM Form 337(10-06) SDNY_GM_02753735 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240657 EFTA01326250 us CenOnigetir CO MAKSPCIOAHON T. WI: rECERAL AVIATION ADWNGTRATIO11 AUG 21, 2013 STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MAKE 2. MODEL NO. 4. TYPE (Aircraft &Kant Aromatic. ate.) S. NAME OF APPLICANT GULFSTREAM G-IV AIRPLANE PRODIGIOUS AVIONICS LIST OF DATA S. menwicknon 7. DILE PRODIGIOUS AVIONICS DRAWING: PA-GIV-1085-2501 CABIN ENTERTAINMENT SYSTEM (MOD) ELECTRICAL DRAWING 9 SHTS REV: B DATE: 8.21.2013 NOTES: I- THIS APPROVAL IS FOR THE ELECTRICAL ASPECTS ONLY. 2- THIS APPROVAL IS FOR THE DESIGN ASPECTS ONLY AND DOES NOT CONSTITUTE INSTALLATION OR OPERATIONAL APPROVAL. 3- IF THIS APPROVAL IS PROVIDED FOR A FOREIGN REGISTERED AIRCRAFT, ACCEPTANCE OF THIS APPROVAL IS AT THE DISCRETION OF THE CIVIL AVIATION AUTHORITY OF THE STATE OF REGISTER. 4- THE INSTALLER MUST DETERMINE THE COMPATIBILITY OF THIS DATA WITH THE AIRCRAFT CONFIGURATION. S. PURPOSE OF DATA TO APPROVE THIS MAJOR ALTERATION ON GULFSTREAM AEROSPACE G-IV AIRCRAFT N423TT SERIAL NUMBER 1085 IN SUPPORT OF FAA FORM 337. I. APPLICABLE REOURIEMENTS (UM *milk IMKtioas) 14CFR25.603(b) Arndt. 25-46 14CFR25 1301(a)(b) Arndt. 25-123 14CFR25.869(a) Arndt. 25-123 14CFR25.1309(a)(b)(c)(e)(g) Arndt 25-123 14CFR25 1353(x) Amdt. 25-123 ID CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under 14 CFR Pan 183, data listed above and on attached sheets numbered XXXXXXXXX have been examined in accordance with established procedures and found to comply with applicable requirements of the Airworthiness Standards listed. O Recommend approval of these data I (We) Therefore L Approve these data 11. SIONATUREIS) OF DESIGNATED ENONEEMNG REPRESENTATIMM D. DESRVIATON NUMSER(S) 13. MASSiFiCATC/410) W.C. Janzer DERT-5 I CH 87-CE Systems & Equipment .....-------- Electrical Equipment GULFSTREAM FAV-ENTERTAINMENT-N42317- ISM FAA Form 81104 SOnteM41ERSEDES PABACus EDTIC•I SDNY_GM_02753736 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA ())24(X158 EFTA01326251 SDNY_GM_02753737 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240659 EFTA01326252 Form Approved .astitonic Trion; NWOP CUB No 2120-0020 MAJOR REPAIR AND ALTERATION 1100/2007 eji (Airframe, Powerplant, Propeller, or Appliance) For FAA On On, us Oningren1 01 Trartgelab3n Federal Mit., AdmInIstralon INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 44701). Failure to report can result in a civil penalty for each such violation. (49 U.S C. 46301(a)). Nationality and Registration Mark Serial No. USA N212JE 1085 1. Aircraft Model Series Make G-IV GULFSTREAM AEROSPACE Name (As shown on registration certificate) Address (As shown on registration certificate) Pants 6100 Red Hook Quarter B3 2. Owner JEGE LLC on ST Thomas sw. zo 00802 co.my Virgin Islands 3. For FAA Use Only 4. Type 5. Unit Identification Repair Altmann Unit Make Model Serial No. 0 Er AIRFRAME (As described in item 1 above) 0 0 POWERPLANT • 0 PROPELLER APPLIANCE n" • 0 OilaMaconer 6. Con ormi Statement A. Agency's Name and Address B. Kind of Agency Manufacturer International Jet Interiors U.S. Certificated Mechanic C. Certificate No. 2221 Smithtown Ave Foreign Certificated Mechanic Ronkonkoma, New York x Certificated Repair Station CRS I1JR439Y 11779 USA Certificated Maintenance Organization D. I certify that the repair and/or alteration made to the unit(s) identified in item 5 above and described on the reverse or attactrnents hereto have been made in accordance with the requirements of Pan 43 of the U.S. Federal Aviation Regulations and that t • tMn furnished herein is true and correct to the best of my knowledge. Extended range fuel per Signature/Date of Authorized Individual Date: 9/19/2013 7. Approval for Return to Sento. Pursuanl to the authority given persons specified below. the unit identified in item 5 was invected in the manner prescribed by the Administrator of the Federal Aviation Administration and is el APPROVED 0 REJECTED FM FN. Standards Persons Approved by Canadian Manufacturer Maintenance Organization Department of Transport Inspector BY Other (Specify) FM Designee X Repair Station Inspection Authorization Certificate or Signature/Date of Authorized Individual Designation No. CRS I1JR439Y Thomas Norden Date: 9/19/2013 e\INWIS FM Form 337 most SDNY_GM_02753738 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240660 EFTA01326253 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with allpreviota alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work accomplished.) USA N212JE DATE Nationality and Registration Mark 9/19/2013 (I) Fireblocked and reupholstered Six (6) existing single cabin chain, two (2) existing double cabin chairs and one (1) existing jump seat with Edelman Leather: Royal Hide RH32. Fireblocked and upholstered one (I) new replacement (Goodrich PN 960014.49) divan with Brentano Fabric: Simplicity- Carrara 1010-01. Rewebbed the existing PAX seat and shoulder harness belts by C&M Marine Aviation Services Inc., CRS V05R749Y, under W.O. 5006. 8130-3 dated 8/8/13. Aircraft seat cushions have been fireblocked as pa the requirements of tine 14 CFR, 25.853(c) Amendment 25 - 116 Appendix F Part II and 14 CFR, 25.853(a) Amendment 25- 116 Appendix F Pan l(aK I x ) Results of Oil Boma Testing arc documented on (attached)Skandia Inc. FAA/D.E.R. approved 8110-3, dated 9/19/13, document ID 94288, WON 25830443, Test Flan 122867 Rev B, dated 8/01/2013, by Jennifer Paluza FAA/DER (DERV-832779-CE). (2) The Crew Scats were snipped and reupholstered with Edelman leather. "Royal Hide, RH32, Dead White" and Aircraft Sheep Skin Co.: Sheepskin 3CCOOI, White. Rewebbed two (2) crew seal Spt seat and shoulder harness belts by C&M Marine Aviation Services Inc, CRS V05R749Y, under W.O. 4991, 8130-3 dated 8/13/13. Flammability Testing (Spec 12) was approved via Skandia Inc. (WO 1257726-13. Test Plan 0 21306) Vertical Flammability Test Results Report dated 6/24/13(attached) by PANDER lane Biberstein. (3) Stripped and recovered Baggage Area / Jeppesen Storage Box in Tapis, Grospoint Black 0091, Lot R. Flammability Testing (Spec /land Spec II) was approved via Skandia Inc. (WON 257726-13, Test Plan SI 21306) Vertical Flammability Test Results Report dated 6124/13 (attached) by FAA/DER Jane Biberstein, (4) Stripped and recovered Forward Closet and Aft Lavatory Storage in Tapis Fabric Grospoint, Muse Blue-FR, 0018. Flammability Testing (Spec (5) was approved via Standee Inc. (WO 0 257726-13. Test Plan N 21306) Venice! Flammability Test Results Report, dated 6/24/13 (attached) by FAA/DER lane Bibermein (5) Fabricated new Entry Rain Curtain in Willowtex list Leather Snow, FR2250A/SKD-I and Ebony Izit Leather, FR2250Bakd-7. Flammability Testing (Spec 0) was approved via Skandia Inc. (WON 257726-13, Test Plan 121306) Vertical Flammability Test Results Report dated 6/24/13 (attached) by FAA/DER lane Bibastein. (6) Recovered the Existing Forward/ Aft Lavatory Side Panel Bulkheads in Willowy Fabric: Snow hit Enhanced A. FR2250A/SKD-L Flammability Testing (Spa N 7) was approved via Skandia Inc. (WON 257726-13, Test Plan N 21306) Vertical Flammability Test Results Report, dated 6/24/13 (attached) by PANDER lane BibersIcin. (7) Recovered the Existing Headliners. Valances and PSU's and Hand Rails in Tams- Ullrasue0e, 3723 Pak Beige. Flammability Testing (Spec 19 and 10) was approved via Skandia Inc. (WON 257726-13. Test Plan a 21306) Vertical Flammability Test Results Report, dated 6/24/13 (attached) by FAA/DER lane Bibersitin (8) Stripped and recovered the existing Window Line Panels and Aft Lay Side Wall panels in Brentano Fabric: Simplicity-Cara 1010-01. Flammability Testing (Spec II l) was approved via Skandia Inc (WO N 257726-13. Test Plan 0 21306) Vertical Flammability Test Results Report, dated 6/24/I) (attached) by PANDER lane Biberstein. (9) Stripped and recovered the existing Lower Side Wall Panels in Edelman Woven Leather. WVNC50. Flammability Testing (Spa 012) was approved via Skala. Inc (WON 257726-13, Test Plana 21306) Vertical Flammability Test Results Report, dated 6/24113 (attached) by FAA/DER Jane Biberstein. (I0) Stripped and recovered the existing Aft Cabin Bithd and Fwd Aft Galley Mild in Acrospecialtia..125 Polycarbonate Minor, 16004102. Flammability Testing (Spec NI 5) was approved via Skandia Inc (WON 257726-13. Test Plan 0 21306) Vertical Flammability Test Results Report. dated 6/24/13 (attached) by PANDER Jane Blear:win. (11) Stripped and recovered the existing Divan End Arms. Divan Lower Doors and Lower Side Walls in Edelman Leather: Royal Hide. RH32, Dead White. Flammability Testing (Spec 116) was approved via Skandia Inc. (WOI 25772643, Test Plan 121306) Vertical Flammability Test Results Report. dated 6/24/13 (attached) by FAA/DER hale Biberstein. (18) Stripped and recovered the Entry Area and Baggage Compartment Floor in A1P: Aermat, 37R/SV/1000/985/20R/54. Flammability Testing (Spec N20) was approved via Skandia Inc. (WON 257726-13. Test Plan 21306) Venial Flammability Test Results Report. dated 6/24/13 (attached) by FAA/DER lane Bibentein. (19) Installed new nplacanau Aft Galley and Lay Countertops with Evans & Paul..187, Designer White Corian. Flammability Testing (Spec121) was approved via Skandia Inc. (WO 125772613, Test Plan It 21306) Vertical Flammability Ten Results Report, dated 6/24/13 (attached) by FAA/DER /the Biberslea. (20) Stripped and recovered the existing Aft Lay Closet Sliding Doers in ACt0SpeCiallieS, .125 Polycarbonate Clear. Minor and Tpis,0018 Muse Blue-FR Grogram, Fabric. Flammability Testing (Spec 122) was approved via Skandia Inc. (WON 257726-13. Test Plan 1 21306) Vertical Flammability Test Results Report, dated 6024/I) (attached) by FAA/DER lane 8ibasttin. Additional Sheets Are Attached FM Form 337 (10-C6) SDNY_GM_02753739 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240661 EFTA01326254 NOTICE Weight and balance or operating limitation Changes shall be entered in the appeopnate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements 8. Description of Work Accomplished (If more space is required, attach additional sheets, Mealy with aircraft nationality and registration mark and date work ished) USA N212JE DATE Nationality and Registration Mark 9/192013 (21) Fabricated and Installed new replacement Baggage Flap in MP. Hematite Red, /80, 0001,Vinyt. Flammability Testing (Spec /23) was approved via Skandia Inc.(W01 257726-13, Test Plans 21306) Vertical Flammability Test Results Report, dated 6/24/ I 3 (attached) by FAA/DER lane Biberslein. (22) Stripped and recovered the existing FWD Cabin Bulkheads in Brentano Fabric: Simplicity-Carrara 1010-01. Flammability Testing (Spec N24) was approved via Skandia Inc. (WO a 257726-13. Test Plan /1 21306) Venial Flammability Test Results Report, dated 6/24/13 (attached) by FAA/DER Jane Biberstein. (23) Stripped and recovered the existing FWD and AFT Potty Seats and Shrouds with Edelman: Woven Leather, WVNC50. AM 3FL. Flammability Toting (Spec I8, N I4) was approved via Skandia Inc. (WON 260097-13, Test Nana 21306) via FAA Form 8110-3 (attached) dated VI VI 3 by FAA/DER lane Biberstein (DERV-1)2780-CE). (24) Fabricated new Conference Table Top using Indiana Architeautal Plywood, laminated with Makore Pom, Veneer. Flammability Testing (Spec 113) was approved via Skandia Inc. (WO N 260097-1). Test Plan N 21306) via FAA Form 8110-3 (attached) dated 8/13/13 by FAA/DER Jim Biberstein (DERY-832780-CE). (25) Installed a new Carpet throughout the cockpit, main cabin. and Floor Ducts areas using ABC Carpet - Wootston Plaid Shoreline. Flammability Testing (Spec I 17./18, 119) was approved via Skandia Inc. Rcfacnce (anached) Skandia Inc. FAA/D.ER. approved 8110-3. dated 9/18/13. document ID 94212, WON 261824-13, Test Plan II 21306 Rev UR by Jennifer Paluzzi FAA/DER (DERV-832779-CE). (26) Modified the following existing cabinetry in accordance with the following FAA/DER approved Drawings ' ;:rtimNo... ! :. A . ter .2", • WIGIVIMS IR INFERIOR INSTL UIGIVIOSSA IR MONITOR MOD INSTL4tH FWD UIGIVII0858 A CONFERENCE TABLE MOD INSTL LIIGIV1085C IR DIVAN INSTL-LH AFT LIIGIV1085D IR LH AFT CLOSET MOD INSTL IJIGIV1085E IR DIVAN ARMREST INST1.4.11 AFT IJIGIV1085F A ENTERTAINMENT EQU1PT MOD INSTL-CREDENZA UIGIVI0850 IR MONITOR MOD INSTL414 AFT UIGIVI08511 IR RH GALLEY MOD INSTL UIGIV101151 IR LH GALLEY MOD INSTL LIIGIVI085K IR VANITY MOO INSTL UIGIVIMI5L IR PSU MOD MIL All above listed structural drawings were approved via attached; FAA PRIM 8110-3, doted Mg 22,2013 Tin Sept 16.2013 by FAA/DER Brian C Adamson, DERT-830137-CE and Donald E. Shepherd. Jr. DERT-230307-CE. Passenger ante width maintained per Title I4 CFR 25.815. A supplemental equipment list has been supplied. A logbook entry has been made reflecting this alteration. All Cabin Interior Fumishings listed above have been Bum Tested in accordance with Title 14 CFR Pan 25.853 (a) Amdl. 25-116 Appendix F Part I (IXI MO Arndt 25-III and Tide 14 CFR Pan 25.853 (a) Am& 25-116 Appendix F Part I (a)( IRO as applicable . This Modification/Repair to the existing Cabin Interior furnishings requires No Scheduled Maintenance Tasks or Ainvonhiness Limitatiens, refer to the Gulfuream Maintenance Manual, and all other existing aircraft ICA's. The Aircraft's Scheduled Maintenance Program is not altered by this installation. The work described, has been found to be in conformity with the above mentioned approved data and continues to meet the airworthiness aitcna under which it was originally certificated Work Order No. 13127, on file at this agency, covers the above described work. No Further Entries 0 Additional Sheets Are Attached FAA Form 337 (10-06) SDNY_GM_02763740 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240662 EFTA01326255 SDNY_GM_02753741 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240663 EFTA01326256 U.S. DEPARTMENT OF TRANSPORTATION 1. DATE FEDERAL AVIANON ADMINISTRATION August 22 2013 STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS AIRCRAFT OR AIRCRAFT COMPONENT umanncAnort 2 MAKE 3 MODEL NO. 4. TYPE Wreak Env* Ropey Pt) 5 NAME OF APPLICANT Gulfstream G-IV Airplane International Jet Interiors, Inc. sin 1085 Ronkonkoma. NY UST of DATA 6 I3DRIFICATION 7 TITLE Drawing: IJIGR/1085 Interior !me sht 1 - 4 Rev (IR) 05/13/2013 IJIGN1005D LH Aft Closet Mod Instl slit 1 - 5 Rev (IR) 06/11/2013 Report: IJIGIV1065DSA Structural Analysis LH Aft Closet Mod Intl Gulfstream G-IV Aircraft Rev (IR) 013/22/2013 Structures Note: 1) The structural aspects only of the above listed data are approved herein. This approval is only for the engineering data. It indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and subparagraph listed below as 'Applicable Requirements". 2) This form does not constitute FAA approval of all the engineering design data necessary for substantiation of compliance to necessary requirements for the entire alteration. The requirements of Flammability are not included in this approval and require separate approval. 3) Aircraft interior compliance inspection is not included in this approval and requires separate approval. S. PURPOSE Of DATA. To provide type data for FAA approval of structure in support of a Major AJteration for Gulfstream G-IV sin1085. A ApPUC48LE REOUREMENTS OM Wed&ma** 14 CFR Part 25, Amdt 25-1 through 25-56 as specified in TCDS Al 2EA; Paragraphs: 25.301(a-b) Amdt 25-23.25.303 Arndt 25-23, 25.305(a, b) Amdt 25-54, 25.307(a. b) Arndt 25-54, 25.341 Arndt 25-0, 25.561(a-c)Amdt 25-23, 25.601 Arndt 25-0.25.603(8c) Arndt 25-46, 25.605(a) Arndt 25-46, 25.609(a) Arndt 25-0, 25.611 Arndt 25-23, 25.613(a, b, d, e) Arndt 25-46, 25.615(a) Arndt 25-23, 25.619(a-c) Arndt 25.23, 25.623 Arndt 25-0, 25.625(8c) Arndt 25-23, 25.769(a) Arndt 25-46. 10. CERTIFICATON - Uncle, autalty vested by Onettlan of the Adrrenstmer and in ecconlinca Me ceetalens and limiteen of *papered under 14 CFR Pat 189. dm Wed abOva end on attached sheets numbered 91a._. nate been exarened h accedence we* esistashed ceacelotes and loved to co.rVy 440 apploalatt readramens of the Airtrolhoen Stilr4Srd, INGO ❑ Recommend approval of those dab I OVIOThetefcce 0 Approve these Oat/ 11. SIGNATURE/S)OF DESCANTED ENGINEERNG REPRESENTATIVE(S) 12. DESSIATON MAMMAS(S) 13. ( 1 ASSLTICATOMS) Brian C. Adamson ofe seLc.0 ,.... DERT-830137-CE Structures ....c.---- FAA Refs 11104 (131I0) SUPERSEDES PREVIOUS EIXT04 3-494-4 SDNY_GM_02753742 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240664 EFTA01326257 SDNY_GM_02753743 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240665 EFTA01326258 U.S. DEPARTMENT OF TRANSPORTATICN i. (»TE FEDERAL AV1ATION ADIAMSTRATICN September 16, 2013 STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS AIREFtAFT OR AIRORAFT COMPONENT IDEN TIFICATION 2. MAKE t IACIDEL MD. 4. TYPE Sttrorali Eniiva Pitrosim. ec.) i MANE OF "CM« Gulfstream G-IV Airplane International Jet Interiors, bc. i s/n 1085 Ronkonkoma. NY UST OF DATA S VENTIRCAT04 2 lime Drawing: - . IJIGIV1085F Entertainment Equipt Mod Instl-Credenza slit 1 - 6 Rev (A) 09/13/2013 Report IJIGIV1085FSA Structural Analysis Entertainment Equipt Mod Instl. Credenza Gulfstream G-N Aic i Rev (A) 09/16/2013 ,.: fi Structures Note: 1) The structural aspetts only of the above listed data are approved herein. Tres approval is oSy for the engineering data. It indicates the data listed above demonstratas compliance onty with the regulations specifled by paragraph and subparagraph listed below as "Applicable Requirements". 2) This form doer not constitute FAA approval of all the engineering design dala necessary for substantiation of compliance to necessary requirements for tie ente alteration. The requirements of Electrical Systems and Equipment and Flammabityae ,- not induded in this approval and require separate approval. 3) Aircraft kilenot compliance inspection is not included m this approval and netaines separate approval. 8. PUFtPOSE OF DATA for Gulfstream 6-1V ski:DE& To provide type data for FAA approval of structure in support of a Major Alteration 9...APPLICABIE REOUIRENENTS (UR Nedla inceini) 14 CFR Part 25, Arndt 25-1 through 25-56 as specified in TCDS AI2EA; Paragraphs: 25.301(a-b) Arndt 25-23, 25.303 Arndt 25-23, 25.305(a, b) Arndt 25-54, 25.307(a, b) Anst r)-54. 25-65, 25.341 Arndt 25-0, 25.561(a-c) Arndt 25-23, 25.601 Arndt 25-0, 25.603(a-c) Arndt 25-46, 25.605(a) Ami 25.619(wcikatt 25.609(a) Arndt 25-0, 25.611 Arndt 25-23, 25.613(a. b, d, e) Arndt 25-48, 25.615(a) Arndt 25-23, 25-23. 25.623 Arndt 25-0, 25.625(a-c) Arndt 25-23, 25.789(a) Arndt 25-48. d 10. OERTIRCATION • under suNortry vred by terecloe d Om Administrator and In aeccidence trim condMons and IiiraMOrd SCI2 e Ill Pan 183. CM* mel *hove and on *trad sheMs nemt:sed uta vere bal dernned in scoordanca sei estioddied eveceatra sed bed t =ME iiai apeacotro requirements ot IMAinvortrinees Standard, 4,164. 0 ReCommend approval of til I (pq? Therekn ISI APprove tinn. data 11. SIGNATIMEiS)OF CESIGNATED ENGINEERNG REPRESENTAI~ 12. DESIGNA/KN NULIBERS(S) 13. EIASSIF~E4 Donald E. Shepherd, Jr. DERT-230307-CE Structures den eid r..$4.4År - i 3 - Mat FM Fordi $1104 (03110) SUPERSEDES PREVIOUS EDITION SDNV_GM_02753744 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240666 EFTA01326259 SIDNYGM 02753745 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240667 EFTA01326260 U.S. DEPARnair OF TRANSPORTATION I. DATE FEDERAL AviimoesOliveSTRAMON August 30.2013 STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MAKE 3 MODEL NO. 4. TYPE To0110. Engu* Moran a) 3. NAME OF APPLICANT Gulfstream G-IV Airplane International Jet Interiors, Inc. sin 1085 Ronkonkoma. NY UST OF DATA 6 DemncAnoN 7. TITLE Drawing: IJIGIV1085B Conference Table Mod InstI see 1 - 5 Rev (A) 08/29/2013 Report UIGIV10858SA Structural Analysis Conference Table Mod InstJ Gulfstream G-IV Aircraft Rev (A) 08/30/2013 Structures Note: 1) The structural aspects only of the above listed data are approved herein. This approval is only for the engineering data. It indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and subparagraph listed below as "Applicable Requirements'. 2) This form does not constitute FM approval of all the engineering design data necessary for substantiation of compliance to necessary requirements for the entire alteration. The requirements of Flammability are not included in this approval and require separate approval. 3) Aircraft interior compliance inspection is not included in this approval and requires separate approval. 4) See sheet 2 for additions drawings supporting drawing WIGIV10858 Rev (A). & PURPOSE OF DATA To provide type data for FM approval of structure in support of a Major Alteration for Gulfstream G-IV s/n1065. 9. APPLICABLE Reotsserts its walk wen) 14 C0R . Part 25, Amdt 25-1 through 25-56 as specified in TCDS Al 2EA: Paragraphs: 25.301(a-b) Amdt 25-23, 25.303 Amdt 25.23, 25.305(a, b) Amdt 25- 54, 25.307(a, b) Amdt 25-54, 25.341 Amdt 25-0, 25.561(a-c) Amdt 25-23, 25.601 Amdt 25-0, 25.603(a-c) Amdt 25-46.25.605(a) Arndt 25-46, 25.609(a) Arndt 25-0. 25.611 Amdt 25-23, 25.613(a, b, d, e) Arndt 25-46, 25.615(a) Amdt 25-23, 25.619(ac) Amdt 25-23, 25.623 Amdt 25-0, 25.625(a-c) Amdt 25-23, 25.789(a) Arndt 25-46. 10. CERTRCATON . Under au/berity reeled by direction of the Adoatnitor and in accordance vats condition rd irmamea of wren oaf la CFR Pan 133. date Wed above and on ached sheets nurnbered 2 o12 haTo poor eom-.ed In woo/dare.. An, esttlAbbed procodufee and bind b comply well applealio requirements of De Alfocoddnesa Standards lama. O Recommend approval of these data I tWo)Therefae 0 Approve Thee data II. 304ATUROSIOF DESIGNATED ENCNEER1NG REPRESENT/LINOS) 12. DESIGNATION fiUMBETASOI 13 CLASSIFICATIONS) Brian O. Adamson ( Oa ts_ DERT-830137-CE Styr:tures FAA Fern, 1110-3 OW SURERscr-Fs PREVIOUS EDITION r2 -001-9 SDNY_GM_02753748 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240668 EFTA01326261 SDNY_GM_02753747 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240669 EFTA01326262 VS. IMPART ENT OF TRANSPORTATION I. DATE FEDERAL AVIATION ADIANiSTRATION August 19.2013 STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS AIRCRAFT Oft AIRCRAFT COMPONENT IDENTIFICATION Z. IMRE 3. MODEL NO. 4. TYPE (Alta Engine. Propstaef, era) S. NAME OF APPLICANT Gulfstream G-IV Airplane Intemabonal Jet Interiors, Mc. s/n 1085 Ronkonkoma, NY UST OF DATA IL IDENTIFCAPON T TIRE Drawing: LlIGIV1085J LH Galley Mod Insti sht 1 - 4 Rev (IR) 07/16/2013 IJIGIV1085H RH Galley Mod Instl sht 1 • 4 Rev (IR) 07/16/2013 Report: IJIGIV1085JSA Structural Analysis LH Galley Mod InsU Gulfstream G-IV Aircraft Rev (IR) 08/12/2013 IJIGIV1085HSA Structural Analysis RH Galley Mod Inst1Gulstream G-IV Aircraft Rev (IR) 08/12/2013 Structures Note: 1) The structural aspects only of the above listed data are approved herein. This approval is only for the engineering data. It indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and ' subparagraph listed below as "Applicable Requirements". 2) This form does not constitute FAA approval of all the engineering design dab necessary for substantiation of compliance to necessary requirements for the ate alteration. The requirements of Flammability are not included in this approval and require separate approval. 3) Aircraft interior compliance inspection is not included in this approval and rterSas separate approval. & PURPOSE OF DATA To provide type data for FM approval of structure in support of a Major Alteration for Guttstream G4V sen10135. ; i tcAPPUCABLE REOUIRDAENFS ,. speak mama) 14 CFR Part 25, Arndt 25-1 through 25-56 as specified In TCDS Al2EA: Paragraphs: 25.301(a-b) Arndt 25-23, 25.303 Amdt 25-23, 25.305(a, b) Amdt 25-54, 25.307(a, b) Arndt 25-&-.. 25.341 Arndt 25-0, 25.561(a-c) Arndt 25-23, 25.601 Amdt 25-0, 25.603(a-c) Arndt 25-46, 25.605(a) AMA 254B. - 25.609(8) Arndt 25-0, 25.611 Arndt 25-23, 25.613(a, b, d, e) Arndt 25-46, 25.615(a) Arndt 25-23, 25.619(a-4A:sit I 25-23, 25.623 Arndt 25-0, 25.625(a-c) Amdt 25-23, 25.789(a) Arndt 25-46. i 10. CERTIFICATION • Una( authority vaned by claccton of the Admidaastm we In madam, MP unarm and InglatIceeMigeeetrmarea -A OR pee Ity, maa ems !bore end On may sea ri,mbcod Mi... Mae been sominad In eccoMance 4eth antennae Resmeares ltd tete C =ate .. wth Amicable reatfiemama a/ the Atwanfiness Standards fisted • Recommend apetovel of ems* deb I (/ft) Thereby Cll APPFave thin data II. SIGNATURES) OF DESIGNATED ENGINEERING REPRESENTATTVELS) 12 DES/GMMONNUMBERS(S) 13. CLASSIRCATOCS Brian C. Adamson _ _.,..-3 „....-- DEBT-630137-CE Structures C...- ------ FMForm $110.3 (03110) SUPERSEDES PREVIOUS EDITION 13-002-4. SDNY_GM_02753748 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240670 EFTA01326263 SDNY_GM_02753749 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240671 EFTA01326264 U.S. DEPARTMENT OF TRANSPORTATION 1. DATE FEDERAL AVIATION ApiEUSSTRATTON August 22 2013 STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 3. Meal NO. A TYPE (Alma EVAN. PNE4407, n7c) 5. NAME OF APPLICANT 2. LAKE Gulfstream G-IV Airplane International Jet Interiors, Inc. s/n 1085 Ronkonkoma, NY UST OF DATA 6 CEINIFICATION 7 TRIE Drawing: IJIGIV1085A Monitor Mod Instl-RH Fwd slit 1 - 3 Rev (IR) 07(16/2013 Report: LIIGIV1085ASA Structural Analysis Monitor Mod Intl-FtH Fwd Gulfstream G-IV Aircraft Rev (IR) 08/21/2013 Structures Note: 1) The structural aspects only of the above listed data are approved herein. This approval is only for the engineering data. It indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and subparagraph listed below as "Applicable Requirements". 2) This form does not constitute FM approval of all the engineering design data necessary for substantiation of compliance to necessary requirements for the entire alteration. The requirements of Flammability are not included in this approval and require separate approval. 3) Aircraft interior compliance inspection is not included in this approval and requires separate approval. S. PURPOSE OF DATA To provide type data for FAA approval of structure In support of a Major Alteration for Gulfstream G-IV s/n1085. 9. APPLICABLE REQUIREMENTS MN soma sceftm) 14 CFR Part 25, Amdt 25-1 through 25-56 as specified in TCDS Al 2EA; Paragraphs: 25.301(a-b) Arndt 25-23, 25.303 Amdt 25-23, 25.305(a, b) Amdt 25-54, 25.307(a. b) Amdt 25-54, 25.341 Amdt 25-0. 25.561(a-c) Amdt 25-23, 25.601 Amdt 25-O. 25.603(a-c)Amdt 25.46.25.605(a) Amdt 25-46, Arndt 25.609(a) Amdt 25-0, 25.611 Amdt 25-23, 25.613(a, b, d, e) Amdt 25-46, 25.615(a) Arndt 25-23. 25.619(a-c) 25-23, 25.623 Amdt 25-0, 25.625(a-c) Amdt 25-23. 25.789(a) Aral 25-46. oremon and Umitakte 01 aNneintinerninclor it CFR 10. CEITDREADON • UM* nullinAly moo, by atecncA of the AdminNINsar end in a:Godard MA PM I83. On GAM ken end on abed abs nettled ale nave been canted in aNtordance MD ellatATITA3 procedures end Nunn to WWI oiM me** roodienwers ol to Almalltwas Damara Wed 0 RoOmmooltd oPproyol Sews@ don I DVIN TAMEN, 0 APPloys those data 11. SIGNATURE(S) OF DESIGNATED ENG04F.EAR40 REPRESENTATIVE(9) 12. DESIGNATION NumitERS(S) ii. ciessinrAnoiks) Brian C. Adamson -c:, .. DERT-830137-CE Structures FAA Form 51104 (01/10) SUPERSEDES PREVIOUS EDITION O-tier t -7 SDNY_GM_02753750 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240672 EFTA01326265 SDNY_GM_02753751 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240673 EFTA01326266 U.S. DEPARTMENT OF TRANSPORTATION I. DATE FEDERAL AVIATKIN ACOMISTRATION August 19, 2013 STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MAKE 1 MODEL NO. 4 TYPE Stara &pink Propeller; art) S. NAME OF APPLICANT Gulfstream G-IV Airplane International Jet Interiors, Inc. s/n 1085 Ronkonkoma. NY LIST OF DATA 6 IDENTIFICAIION 7 TITLE Drawing: IJIGIVI(P35B Conference Table Mod Instl sht 1 - 5 Rev (IR) 06/0512013 IJIGIV1065K Vanity Mod 'mil sht 1 - 4 Rev(IR) 07/05/2013 Report: IJIGIV108513SA Structural Analysis Conference Table Mod Insti Gulfstream G-IV Aircraft Rev(IR) 08/19/2013 IJIGIV1035KSA Structural Analysis Vanity Mod Intl Gulsfteam G-IV Aircraft Rev(IR) 08/1212013 Structures Note: 1) The structural aspects only of the above listed data are approved herein. TMs approval is only for the engineering data. It indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and subparagraph listed below as "Applicable Requirements". 2) This form does not constitute FAA approval of all the engineering design data necessary for substantiation of compliance to necessary requirements for the entire alteration. The requirements of Flammability are not included in this approval and require separate approval. 3) Aircraft interior compliance inspection is not included in this approval and regales separate approval. t PURPOSE OF DATA TO provide type data for FM approval of struchne in support of a Major Alteration for Gulfstream G-fV s/nl0$5. 9. APIMCABLE REQUIREMENTS (UN Met eardkos) 14 CFR Part 25, Amdt 25-1 through 25-56 as specified in TCOS Al2EA; Paragraphs: 25.301(a-b) Arndt 25-23, 25.303 Amdt 25-23, 25.305(e, b) Arndt 25-54, 25.307(a, b) Amdt 25-54 25.341 Arndt 25-0, 25.561(a-c)Amdt 25-23, 25.601 Amdt 25-0, 25.603(a-c) Amdt 25-46, 25.605(a) Arndt 25-48, 25.809(a) Arndt 25-0, 25.611 Amdt 25-23, 25.613(0. b, d, e) Amdt 25-46. 25.615(a) Amdt 25-23, 25.619(apc) Ala 25-23, 25.823 Arndt 25-0, 25.625(a-c) Amdt 25-23, 25.789(a) Arndt 25-48. io. carifiFICATON .Unclor *Mod* tistied by catectice of Re AthnkatiflOr and In accordance MA ccedelorts AM MUM. of morolrenet mar t4 CFR PM In 000 ate] ' led on sheets nunixted Na have been ermines In actordfrea Mn forablfichod maks and lc r 0 CO* 00 000icable multenrs 0 re Meatiness Standards Imo . 0 Recommend approval of these arts I (ele)Thetefoie 0 Morove these OM II. SIONATURE(3)06 DESIOPATED ENGNEERMG REPPESENTAME(S) IT DESIGNATION NUOMSERSMI t3 ci.AssrncAnotest Brian C. Adamson DERT-830137-CE Structures t5s4Z. EVe., — FM Fon. 81104 (MO) SUPERSEDES PREVIOUS EDrniat SDNY_GM_02753752 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240674 EFTA01326267 SDNY_GM_02753753 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240675 EFTA01326268 US. DEPARTMENT OF 1RANSPOITFADON I DATE FEDERAL AVIATION ADIANISTRADON August 21, 2013 STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS AIRCRAFT OR AIRCRAFT COMPONENT 'DEMME/CATION 1 ?WE 3. MOMS NO. a ME (Arend &tee. Now:4e. at! 5. NAME OF APPLICANT GLII1SDOSITI G-IV Airplane International Jet Interiors, Inc. sin 1085 Ronkonkoma, NY UST OF DATA 6 IDENTiRCADON Y. TOSE Drawing: IJIGN1085C Divan Intl-LH Aft sht 1 - 3 Rev(IR) 06/10/2013 IJIGN1085E Divan Armrest instl-LH Aft sht 1 - 4 Rev(IR) 06/28/2013 Report IJIGIV1085GSA Structural Analysis Divan Intl-LH Aft Gulfstream G-IV Aircraft Rev(IR) 08/1W2013 Structures Note: 1) The structural aspects only of the above listed data are approved herein. This approval is only for the engineenng data. It Indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and subparagraph listed below as "Applicable Requirements". 2) This torn does not constitute FAA approval of all the engineering design data necessary for substantiation of compliance to necessary requirements for the enure alteration. The requirements of Flammablity are not included in this approval and require separate approval. 3) Aircraft interior compliance inspection is not Included In this approval and requires separate approval. S. PURPOSE OF OATA To provide type data for FAA approval of structure in support of a Major Alteration for Guffstream G•h/ s/n1085. 9. APAlldJJ3LE REPAREUEMS NMRCM staked) . 14 CFR Part 25, Amdt 25-1 through 25-56 as specified In TCDS Al2EA; Paragraphs: 25.301(a-b) Amdt 25-23, 25.303 Amdt 25.23.25.305(a. b) Amdt 25-54, 25.307(a, b) Amdt 25-54, 25.341 Arndt 25-0, 25.561(a-c) Arndt 25-23, 25.601 Amdt 25-0, 25.603(a-c) Arndt 25-48, 25.005(a) Amdt 25-46, 25.609(a) Amdt 25-0, 25.811 Amdt 25-23, 25.813(a. b. d, a) Arndt 25-46, 25.615(a) Amdt 25-23, 25.819(ac) And 25-23, 25.623 Arndt 25-0, 25.625(a-C) Amdt 25-23, 25.785 (i1.13) Amdt 25-51, 25.789(a) Arndt 25-46. to currocKriou • under aulthety waled by Creedal of the Adak:trate and In moxdance Mt condemns end frnerms of this:thareri sedir SI CIR1t Part 183. data Wed Sae and on arm:fed Mods mnaftbeded Na move bean eminthed in actiordance MU' eatitthice postathes endInflows, i ilith spoest4eroperrents of to A/worminess Standards lett 0 Recommend approval of Mene date I (We) Therefore E Appease these data II. SIGNATURE(S) OF MIGRATED ENGINEERING REPRESENTARYEMLia MIGRATION NUIMERSM II- CLASSIECATIONISI Brian C. Adamson DERT-830137-CE Structures FAA Fan,, *110-3 (02-40 SuPERScosSeREVIOuS 13-4v2 -r SDNY_GM_02753754 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240676 EFTA01326269 SDNY_GM_02753755 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240677 EFTA01326270 U.S. DEPARTMENT OF TRANSPORTATION I. DATE FEDERAL Melee AJMONISTRA110.1 August 20, 2013 STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MAKE 3 MODEL NO 4- TYPE Pee, GAM After. M[.) I NAME OF APPLCANT Gulfstream G-IV Airplane International Jet Interiors. Inc. sin 1085 Ronkonkoma, NY LIST OF DATA 6 CANTIFICATION 7 TITLE Drawing: IJIGIV1085L PSU Mod Intl sht 1 - 4 Rev (IR) 06/27/2013 IJIGIV1085G Monitor Mod Inset-LH Aft sht 1 - 3 Rev (IR) 07/16/2013 Report' IJIGIV1085LSA Structural Analysis PSU Mod Instl Gulfstream G-IV Aircraft Rev (IR) 08./12(2013 IJIGIV1085GSA Structural Analysis Monitor Mod Instl-LH Aft Gulfstream G-IV Aircraft Rev OR) 08/08/2013 Structures Note: 1) The structural aspects only of the above listed data are approved herein. This approval is only for the engineering data. it indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and Subparagraph listed below as 'Applicable Requirements". 2) This form does not Constitute FAA approval of all the engineering design data necessary for substantiation of compliance to necessary requirements for the entire alteration. The requirements of Flammability are not included in this approval and require separate approval. 3) Aircraft interior compliance inspection is not included in this approval and requires separate approval. S. PURPOSE OF DATA To provide type data for FAA approval of structure in support of a Major Alteration for Gulfstream G-IV sin lass. 9. APPUCA9tE REOUIRAJAEITIS (UN some sem) 14 CFR Part 25, Amdt 25-1 through 25-56 as specified in TCDS Al 2EA: Paragraphs: 25.301(a-b) Amdt 25-23. 25.303 Amdt 25-23, 25.305(a, b) Amdt 25-54, 25.307(a. b) Amdt 25-54, 25.341 Amdt 25-0, 25.561(a-c) Amdt 25-23, 25.601 Amdt 25-0, 25.603(a-c)Amdt 25-46, 25.605(a) Amdt 25-46, 25.609(a) Amdt 25-0, 25.611 Amdt 25-23, 25.613(a, b. d, e) Amdt 25-46, 25.615(a) Amdt 25-23. 25.619(a-c) Amdt 25-23, 25.623 Arndt 25-0, 25.625(a-c) Amdt 25-23, 25.789(e) Amdt 25-46. 10. CERTIFICATION • Under awe* eel by diem a( Re AOrrarasnIof and In amorderat MU mete and lealtalens of notentment under 14 CFR Pan 163, data led above and on Shea shaets numbered _e_ have been seined In accoNance eh estakeed PoCeAdUtall and foe to coney MO% onkablorterements d the Almodesse Steeds Idled. 0 Recommend approval of these data I °Ye)Ilmeore 0 Approve thou data 11. SIGNATURE(S) OF DESIGNATED ENGINEEFteIG REPRESENTATNE($1 12. DESMNATION MILMERS(S) 13. CLASSIFCATION(S) Brian C. Adamsof c::e________ DERT-830137-CE Structures FAA Form 6110-3 (00110) SUPERSEDES PREY/DVS EDITION /3-ern.- * SDNY_GM_02753756 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240678 EFTA01326271 SDNY_GM_02753757 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240679 EFTA01326272 U. S. DEPARTMENT OF TRANSPORTATION I OATE FEOERAt. AVIATION ADMINISTRATION 8/1512013 STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2.MAKE 1 NODE,. NO. 4 TyPE(Amame. Engine. Not* ere.) 5 NAME OF APPuCArrr Gultstream G-IV Airplane International Jet Interiors UST Of DATA 6 IDENTIFICATION Design Data $280145 Skandia, Inc Flammability Test Results Rev NC Bunsen Burner Testing Test Specimen P/N S (represents forward/art storage) Notes: 1) Work accomplished under Skandia Inc. WO 0 260145-13. Ref Document ID 94116. 2) Flammability test witnessing only, does not constitute installation approval of materials. 3) IAW Skandia Flammability Streamline Testing Test Plan 21306. Rev IR. Dated 11/03/11 8.PURPOSE OF DATA Demonstration of compliance with material flammability requirements in support of Major Repair & Alteration for S/N 1085 9.APPUCABLE REQUIREMENTS (UM spseibc sections) 14 CFR Part 25.853 (a) Arndt 25-116 Appendix F Pan I (a)M0) Arndt 25-11I 10.CER11FICATION • Under authority vested by direction of Ilse Administrator end in accordance with conditions and limitations of appointment under 14 CFR Pan 183, data listed above and on attached sheets numbered have been examined in accordance with established procedures and found to comply with applicable requirements of the Airworthiness Standards listed. 0 Recommend approval of these data 1(We) Therefore *Approve these dale ii.SiGNATUISE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE 12.0t&IGNATiON NUMBERS) i3.ClASSIFICATION(S) /is, 1.- tkS/1 ck I . i \K-Aili Iti() Jane Bibehtein -FAA DER DERY-032780-CE Structural Special FAA Form 8110-3 (03/10) SUPERSEDES PREVIOUS EDITION SDNY_GM_02753758 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240680 EFTA01326273 SDNY_GM_02753759 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240681 EFTA01326274 U S DEPARTMENT OF TRANSPORTATION ELATE FEDERAL AVIATION ADMINISTRATION 8/13/2013 STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2.MAKE 3.MOOEL NO. 4.TYPE(AtTano. Ear,. Awe*? tic) 5 NAME OF APPLICANT Gulfstream G-IV Airplane International Jet Interiors LIST OF DATA 6 IDENTIFICATION 711T1F Design Data S260097 SKandia, Inc. Flarnmabildy Test Results Rev NC Bunsen Burner Testing Test Specimen P/N's B (represents potty seats. fwd/aft) ' 13 (represents conference table) 14 (represents potty seats. fwd/af0 Notes: 1) Work accomplished under Skandla Inc. WO # 260097.13. Ref Document ID 94098. 2) Flammability test witnessing only, does not constitute installation approval of materials 3) UAW Strand* Flammability Streamline Testing Test Plan 21306. Rev IR. Dated I unit &PURPOSE OF DATA Demonstration of compliance with material flammability requirements in support of Major Repair & Alteration for S/N 1085 1 9.APPLICAEILE REQUIREMENTS (List specific secesns) 14 CFR Pan 25.853 (a) Arndt 25-116 Appendix F Pan I (a)(1)(ii) 14 CFR Part 25.853 (a) Arndt 25.116 Appendix F Pan I (a)(1)(i)Amdt 25.111 tO.CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under 14 CFR Pan 183. data listed above and on attached sheets numbered have been examined in accordance with established procedures and found to comply with applicable requirements of the Airworthiness Standards listed. 0 Recommend approval of these dela 1 (We) Therefore ,... • )2C1pprove these data i 1.SIGNATURE(5) OF DESIGNATED ENGINEERING REPR SENTATIVE 12.06 IONA 10 NUMBER(S) 13.0 IFATION($) ..1..___. \ (') 3.k3. W ug J Jane Stherstet ...FAA DER DERV-832780-CE Structural Special FAA Form 8110.3 (0110) SUPERSEDES PREVIOUS EDITION SDNY_GM_02753760 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240682 EFTA01326275 SDNY_GM_02753761 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240683 EFTA01326276 U. 5_ DEPARTMENT OF TRANSPORTATION I.DATE FEDERAL AVIATION ADMINISTRATION 9/19/2013 STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2.A4AKE 3.MOOEL NO. 4.TYPEMATA44. &Ott Prootate. et) 5.NAME OF APPLICANT Gulfstream G-IV Airplane International Jet Interiors LIST OF DATA ILIDENTIFICATION 7 TIME 1? 22867 Skandia, Inc. Flammability Test Report Rev B Oil Burner Testing and Vertical Burner Testing Dated 08(01/2013 Notes: 1) Work accomplished under Skandia Inc. WO X 258304-13, Ref Document ID 94288. 2) Flammablity test witnessing only, does not constitute installation approval of the materials. 8.PURPOSE OF DATA Demonstration of compliance with material flammability requirements in support of Major Repair 8 Alteration for SIN 1085 SAPPLICABLE REQUIREMENTS Oast specific sections) 14 CFR Part 25.853 (c) Amendment 25118 Appendix F Part II 14 CFR Part 25.853 (e) Arndt 25.118 Appendix F Part I (a)(1)(11) 10.CERTIFICAT1ON - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under 14 CFR Part 183. data listed above and on attached sheets numbered have been examined In accordance with established procedures and found to comply with applicable requirements of the Airworthiness Standards listed. 0 Recommend approval of these data I 04 Therefore 0 Approve these data tt.SIONATURE(S) OF DESIGNATED ENOINEERmo REPRESENTATNE 12.0ESKINATION 'WM8EP(S) 13.CLASSIFICATION(S) pci tyr• t J niferPaluzzi -FAA E FAA Form 81104 (03710) SUPERSEDES PREVIOUS EDMON DERV-832779-CE Structural Special SDNY_GM_02753762 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240684 EFTA01326277 SDNY_GM_02753763 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240685 EFTA01326278 Li S. DEPARTMENT OF TRANSPORTATION I DATE FEDERAL AVIATION ADMINISTRATION 9(19/2013 STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION ?MAKE 3.MODEL NO 4.7 YPE(Avatmo. &Vat PI T etc 1 5. NAME OF APPLICANT Gulfstream G-IV Airplane International Jet Interiors UST OF DATA 6 IDENTIFICATION 7 ITT Design•Data S261931 Skandia, Inc. Flammability Test Results Rev NC Bunsen Burner Testing Test Specimen P/N 17 (represents floor covering being installed unbondedl Notes. 1) Work accompliShed under Skandia Inc. WO # 261931-13, Ref Document ID 94289. 2) Flammability lest witnessing only, does not constitute installation approval of materials. 3) IAW Skandia Flammability Streamline Testing Test Plan 21306, Rev IR, Dated 11103111 8.PURPOSE OF DATA Demonstration of compliance with material flammability requirements in support of Major Repair 8 Alteration for SIN 1085 9APPLICABLE REQUIREMENTS plat SPCCAC WOODS) 14 CFR Part 25.853 (a) Arndt 25-118 Appendix F Part I (a)(1Xii) _.. 10.CERTIFICATION • Under authority vested by direction of the AdmIniShater and in accordance with conditions and limitations of appointment under 14 CFR Part 183, dale listed above and on attached sheets numbered have been examined in accordance with esiebilshed procedures and found to comply with applicable requirements of the Airworthiness Standards listed. 0 Recommend approval of these data I (We) Therefore *Approve these data It SiGNATuRE(S)OF DESIGNATED ENGINEERING REPRESENTATIVE 12.0ESIGNATION NUMBER(S) i3.ClASSiFiCATIOR(S) • t'l i.‘1 ...._ , k /.. .) '1121 1-0—.) Jane Bibtrsteln -FAA DER DERV-832780-CE Structural Special FAA Fo 8110.3 (03110) SUPERSEDES PREVIOUS EDITION SDNY_GM_02753764 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240686 EFTA01326279 SDNY_GM_02753765 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240687 EFTA01326280 IL S DEPARTMENT OF TRANSPORTATION I DATE FEDERAL AVIATION ADMINISTRATION 9/ 18/2013 STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2.MAKE 3 MODEL NO ATYPE/Anw. Foyers. ens etc) SNAME OF APPLICANT Gutfstream G-IV Airplane International Jet Interiors lir OF DATA 8 ICENIWICATION 7 Ern F Design Data 5281824 Skandia, Inc. Flammability Test Results Rev NC Bunsen Burner Testing Test Specimen P/N's 18 (represents floor covering. cockpit) 19 (represents floor covering, ducts) Notes: 1) Work accomplished under Skandia Inc WO # 261824.13. Ref Document ID 94282. 2) Flammability test witnessing only, does not constitute Installation approval of materials 3) IAN/ Skandia Flammability Streamline Testing Test Plan 21306, Rev IR, Dated 11103111 8.PURPOSE OF DATA Demonstration of compliance with material flammability requirements in support of Major Repair 8 Alteration for S/N 1085 9APPLICABLE REQUIREMENTS (List specific seetion11 14 CFR Part 25.853 (a) Arndt 25-116 Appendix F Part I (8)(1)00 10.CERTiFICATION • Under 8UlhOlity yelled by direction or the Administrator and in accordance with Conditions and limitations of appointment under 14 CFR Pao 183, data listed above and on attached sheets numbered have been examined in accordance with established procedures and found to comply with applicable requirements of the Ainvocthiness Standards listed. 0 Recommend approval of these data i 004 Therefore pApprove theSe data 11.81GRATURE(8) OF OESIGNATED ENGINEERING REPRESENTATNE 120ES(GNATION NUMBER(S) Is CU>SSiFICATIONa) 9 , 44fi s fej ein • J niter Paluzzi -FA DER DERY-832779-CE Structural Special FAA Form 81104 (nto) SUPERSEDES PREVIOUS EDITION SDNY_GM_02753766 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240688 EFTA01326281 SDNY_GM02753767 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240689 EFTA01326282 U S. DEPARTMENT OF TRANSPORTATION '.DATE FEDERAL AVIATION ADMINISTRATION 9117/2013 STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2MAKE 3 MOOEL NO. 4.TYPE(MPIms. &WOK Propose. ere) 5.NAME OF APPLICANT Gulfstream G•IV Airplane International Jet Interiors FATA LIS1rnI 6 IDENTIFICATION 7 TITLE Design Data S257726 Skandia, Inc. Flammability Test Results Rev NC Bunsen Burner Testing Test Specimen P/N's 2 (represents crew seats) 3 (represents jeppesen box, aft baggage) 4 (represents aR baggage) 5 (represents Ned closet and Finlay storage) 8 (represents rain curtain) 7 (represents fwd lay side panel, blkhds, aft lay all bulkhd) 9 (represents headliners, valences, pates) 10 (represents hand rails) 11 (represents window line, aft lay side wall) 12 (represents lower side wall panels) 15 (represents aft cabin blkhd. Md aft galley blkhd) 16 (represents divan end arms, divan lower doors, lower side walls) 20 (represents entry area, baggage floor) 21 (represents aft galley, lav countertops) 22 (represents aft, lay closet sliding doors) 23 (represents baggage nap) 24 (represents hod cabin bulkheads) Notes: 1) Work accomplished under Skandia Inc. WO 0 257726-13, Ref Document ID 94278. 2) Flammability test witnessing only, does not constitute installation approval of materials. 3) IAW Skandia Flammability Streamline Testing Test Plan 21306, Rev IR, Dated 11/03/11 8.PURPOSE OF DATA Demonstration of compliance with material flammability requirements in support of Major Repair & Alteration for SIN 1085 9.APPLICABLE REOUIREMENTS(tisi specific sections) 14 CFR Pan 25.853 (a) Arndt 25-116 Appendix F Pan t (a)(t)(i) Amdl 2`5-111 14 CFR Part 26:853 (a) Arndt 25.116 Appendix F Part 1 (a)(1Xii) IOCERTIFICATION • Under authority vested by direction of the Administrator and In accordance with conditions and limitations of appointment under 14 CFR Part 183, data listed above and on attached sheets numbered have been examined in accordance with established procedures and found to comply with applicable requirements of the Airworthiness Standards listed. CI Recommend approval of these data I (We) Therefore y ..Approve these data i i .SIGNATURE(S) Of DESIGNATED ENGINEERING REPRESENTATIVE 12.DESIGWVION NUMBER($) I 3.0 SSI ION(S) c r") / ,1 41- a 1 Ai) Jane Bi4rstern FAA DER DERY-832780-CE Structural Special FAA FOND 8110-3 (03/10)SUPERSEDESPREVIOuS EDITION SDNY_GM_02753768 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA (x124(169() EFTA01326283 SDNY_GM_02753769 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240691 EFTA01326284 wait STATES CF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE NATIONALITY MO 2 OAANUFACIVREA AND MCOEL 1 AIRCRAFT SERIAL 1 CATEGORY, NEW:STRAD:Al MARKS KAISER N212JE Gulf stream G-IV 1085 Transport 5 AUTHORITY AND BASIS FOR ISSUANCE Tm troenness wics1464sn1pocoel ti U SC. 1N101v/ cots ta. dbe On<ISam to mot 44 %No Aug tab* rsmad and bac 99 orkm try to ceSS:V• Dotty. • eln anidoi ti lde toribi.v1W bol *We 11NINilootn015iN Art ceryntrit aNdebNd~Sea Da as "Wad WainIt N Cznyterko MInes CAA ASIA JINN N ION 1446/. SAS NONE 6 TERMS AND CONDITIONS Wets Nay seen6N41 442.4444 Al a a woe ts Menem WatilhOityNAGA As artiothea AMES ad. a in /1At tefrOrl• gre•eirMita Antall a* prima coact AM Pan 1.4.9•40 • SI cl !WANMar 9 as at II IN UMW] SIAN DATE OF ISSUANCE DESIGNATION WISER R 05/23/2000 S019 AllIbrikhrAndanns.se cootait /*be *by.Ite 4ci auttfrq fl12 a a tales 144•192 CEPRFICATE MAT et DISOLA AF DC PI CROWE MTN APPLOStEFECOAL BA PGIAAACK5 FM Form 51004 (044 I ) SW* Ed1:01 • • SDNY_GM_02753770 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240692 EFTA01326285 SDNY_GM_02753771 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240693 EFTA01326286 ...menew ;arc COMTIST a TIWC•0011.010%-etptiltaiL ikna,TIM•0•01.8MATOI STANDARD IURWORTHINESS CERTIFICATE T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 00240694 EFTA01326287 I SDNY_Ghl_02763 3 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00240695 EFTA01326288 weft& 2, 204t20 Emmett Teeming MINX( elsr MAJOR REPAIR AND ALTERATION E*to ino14 wefts wean arOwerwent unsoonnon Fedmil minion (Airframe, Powerplant, Propeller, or Appliance) AdmitAttr•Ilon INSTRUCTIONS- Print or type all entries. See Title 14 CFR §43.9. Pal 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) fOr instructions no disposition of INs form. This report Is required by law (49 U.S.C. §44701). Failure to report un result in a ail penally for each such violation. (49 V.S.C. 146301(a)) Nationality and Registration Mark Serial No. USA N423TT 1085 1. Aircraft make Model Series GULFSTREAM GIV GIV Name (As snown on registration certificate) Address (As shown on registration CLYMCOM) Aeress 2. Owner JEGE LLC or, ST , rows Sole Fonda„ hp 00002 Caney VIRGIN SAWS 3. For FAA Use Only 4. Type S. Unit identification Repair Alteration Vial Make Model Serial No. 0 AIRFRAME (As described in Item 7 above) O O POWERPLANT 0 O O PROPELLER Type O APPLIANCE O Mil/IttliCtOrOf 6. Conformity Statement A. Agencys Name and Address B. Kind of Agency ewe GuLFSTREAU V. S. Certificated Mechanic I MilMEOChiref Agm,... OK PtitelYI00 Foreign Corteretrod Mechenic C. Cenificale No. Car WEST PALM BEACH um FL X CM/4MM Repair Swim z• wee Ca011y USA Confutes Mardimanca Orme/nen PB8R624N O. I certify that the repair and/or alteration made to the unit(s identifier' in item S above and described on the reverse a atlachrneMs hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is but and correct to the best of my Extended range fuel Signature/O rlz per le CkR, n 43 AFP' Bis t bog ❑ WM Thomas J. Choynowski 06/13/2013 7. • oval for Return to Service Pursuant to the autherily g'ven persons specified below. the unit identified in item 5 we! Inspected in the Manner prescribed by the Administrator Of the Federal Aviation Administration and * plApproved riRejected FAA Fit. Sundards Foment APOMved by Canadian Manufacturer Maintenance Organization InSpeCtOr .Desionnient of Tranicen BY Omer (Specify) FAA Designee X Repair Sleben Inspection Authorization CertifiCate or Signature/Dale of ' d Individua Designation No. PB8R624N ,r.77s. oar.; Jim Fishburn 06/13/2013 FAA Form 337 (10/06) Page I it SDNY_GM_02753774 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240696 EFTA01326289 NOTICE Weigh end balance or operating arretation changes shall be entered in the appropriate aircraft record An alteration must be compatible with all previous alterations to assure continued conformity with the sleekest:Oa airworthiness requirements. a. DncripUon of Won Accomplished Of more space i9 required. attach adthbonal MOWS Men* wan aware nabonatly and registration mark and date work completed.) USA mann 0611312013 NolienaltY and negastratein Mark Oat. Aircraft Make: GULFSTREAM AEROSPACE Aircraft Model: GIV Aircraft Serial Number: 1085 Reference Gulfstream PSI Wodc Order: SCI3300 Complied with STC ST04257AT-D - Installation of GAViS System- IAW Gulfstream Aerospace Index List CE513358001, Rev. A dated April 9, 2012 and Gulfstrcam Document CE4960458 dated 06/13/2013. The display for the GAViS System is installed JAW ASC 476A and Customer Engineering Drawing List DL No. CE41 4960458 approved by Gulfstream form 8100-9 dated 06/13/2013. Reference Airplane Flight Manual Supplement CE51335M%14, Rev.-, dated April II, 2012 and Accepted Instructions for Continued Airworthiness CE51335A001, Rev. A, dated April 5, 2012. Items Removed: Qty. Description Manufacturer Pan Number Weight/Lbs. F/S 6 Ea. DU-880 Honeywell 4053000-901 30.4 (Ea.) 90.0 I Ea. FMS Data Loader DL-950 Gables 07226.02 1.17 166.0 2 Ea. CRT Fan Commutating Module Rotron 508534 1.5 147.5 2 Ea. Fan Any. Rottman 508617 1.15 73.0 2 Ea. ATC Transponder Collins 622-9210-309 8.5 (Ea.) 40.5 Items Installed Qty. Description Manufacturer Pan Number Weight/Lbs. F/S 6 Ea. DU-885 Honeywell K9321061A02 19.6 (Ea.) 90.0 I Ea. XM Data Receiver Honeywell 4092743.901 1.5 151.0 I Ea. XM Antenna Honeywell C1420-1 0.2 174.5 I Ea. FM Data Loader DL-I00 Gables G7228.02 1.17 166.0 2 Ea. Cursor Control Device Esterline 73E8202 2.6 109.0 I Ea. Video Amp Audio Intl VA-401-2 0.6 112.0 2 Ea. ATC Transponder Collins 622.9210.409 8.5 (Ea.) 0.5 Notes: I. The electrical load analysis statement is contained in Gulfstream Document CE4 I 4696425. 2. Deviations to STC 476A arc shown in Cull-Stream Document CEA I 6990073. 3. Deviations to Gavis STC ST04257AT-D arc found in Gulfstream Document CE4 I 3350049. 4. A logbook entry reflecting this installation was completed and entered into the aircraft logbook. 5. The aircraft Equipment List has been updated to reflect this installation. 6. Weight and Balance data has been revised and inserted into the Weight and Balance Manual. 7. Maintenance instructions for continued airworthiness are contained in FAA Accepted Instructions for Continued Airworthiness CE51335A00 I Rev. S dated April 05, 2012 (or later). 8. FAA Approved Flight Manual Supplement CE51335M004 A dated April II, 2012 has been inserted into the AFM. ClAdotuonattneets _ 4.,.1 AM Attached FAA Form 337 (10/06) Page 2 SDNY_GM_02753775 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240697 EFTA01326290 Rimhetione marecoic inewhe /*mini Or ha 2NOCON 0 Ora /2007 MAJOR REPAIR AND ALTERATION IAA We Only US Dated Miry aponasan (Airframe, Powerplant, Propeller, or Appliance) Rani Avid... MIEMIstaillon INSTRUCTIONS: Print or type as entries See Title 14 CFR §43.9. Pan 43 Appendix 8. and AC 43.9-1 (or subsequent revision thereof) for Instructions and disposition of this form. This report iS reputed by taw (49 U.S.C. §447O ). Failure to report can result in a civil penally for each such violation. (49 U S.C. §463O1(a)) Nationality and megistrabon Mark Serial NO. USA N423TT 1085 1. Aircraft Make Model beats Gulfstream Aerospace G-IV Name (As shown on registration ceshficate) Address (As sheen on reipsfrolkon testate) Kona 515 N Flagler Drive, STE P400 2. Owner TRT Leasing Car West Palm Beach stew Florida no 33401-4320 Carty USA 3. For FM Use Only applailagra The actrankal date herein gas keen mood to comply wok tirwortif4. P. racjwiredicate and is hon:by enameled MT N69 Cillbr PI tie above described aircraft, subject to conformity tfaaft00840414 a ea anction33.7. , \n, - _- aim tr io,S.AlAit ,S‘x 4. Type S. unit Identification Repair Mention Unit Make Model Serial No. 0 AIRFRAME (As clescnbed in Item 1 abetter) O . POWERPLANT 0 E O PROPELLER Type o O APPLIANCE Uanufackre• 6 Conformity Statement A. Agencys Name and Address B. Kind of Agency iaoki CE Amnia Inc. U. Comecon:I Mechanic I ManAacturve ArMnn 2789 Frightline Avenue Foreign Contralto MeChailiC C. Certificate No. eta Sanford tam FL x Cartnicateci Repay Stanco 32773 twiny USA OE4R411M Al Congested Maimenance Organdaton D. I certify that the repair andlor alteration made to the tine s) Identified in item 5 above and described on the reverse or attachments hereto have been made in accordance with the remarements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Extended range fuel Signe a o Irld.iduat pet 14 CFR Part 43 O APP. B 2 JAN 2 9 1013 7. Approval for R urn to Service PUIllant to the authority given persons specified below. the unit identified in item 5 was inspected in the manner prescribed by the Administrator of Federal Aviation Administration and is I21 Approved El Rejected FAA Fit. Stanclals Poisons Approwed try Canadian Manufacturer Maintenance Organization InSpOCICH OSpartinent Of Trengal BY other (specify) FM Designee X Repair Station Inspection Authorization Certificate or Signature/Date of AlithOrized InteVidell Destgnation No. 0E4R411M — leen..-4 4c/ -. 4" --c----- JAN 2 9 2013 orm 5370040 SONY_GM_02753776 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 1O, 15, and 17 EFTA_00240698 EFTA01326291 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements B. Description of Work Accomplished (If more space is requited. Mach adcktional sheets. mien:Wrath aircraft nationality and reefs:catkin mark and date work completed) USA N423TT JAN 2 9 2013 NationaMy and Registration Mark Date Removed 2 each, CMC Electronics CMA-1100 EFB EEMU's and Part No. 217-601933-215 Cable Assemblies previously installed on FM Form 337 dated April 9, 2007 (CRS X91R092Y). Removed circuit breakers, capped and stowed power wires. Remaining connectors bagged and properly secured. END O Additional Sheets Are Attached 0 Pages FAA FOOT, 3371,0.41 SDNY_GM_02753777 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240699 EFTA01326292 0 wn zwrir Bean Warsaw tweet A°YB Ow MAJOR REPAIR AND ALTERATION 11f'101001 VS Oteatirnee 0/f/lAWS1Sell a Traritieerd01 (A irframe, Powerplant, Propeller, or Appliance) Nerd A* Admisslaretle. INSTRUCTIONS: PAM or type as entries. See TAB 14 CFR §43.9. Part 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for nstruCtions and disposnon of (Ns form. This report is required by law (49 U.S.C. §4470 ).Fein I0 feint CIA Mull in a bvil Panay la earn such violation. (49 U.S.C. §463O1(a)) Nationality and Registration Mark Senal No USA N423TT 1085 1. Aircraft Make MOCtel bents Gulfstream Aerospace G•IV Nun* (As shown on tegostrobon cerfincato) morass (As Shown on regeshalfron certificate) Arms 515 N Flagler Drive, STE P4OO 2. owner TRT Leasing cay West Palm Beach our Florida SO 334O1.432O Qatar USA & For FAA Use Only Ihi essioleal dati herein on t‘z.tia aataa: la MAIO TO eltalYASIO shwoutli,,,c reavivreetents ant iii lamb; topiva.t1 IN IP9 fflil/ itil 'be above atscapal aircraft, subloct to gugonnity ii,Vi0WA W ti a seoloa33.7. rA SS `TM ASU•ADO-15 4. Type 5. Unit Identification Repair Alteration Unit make Moat Serial No g AIRFRAME (As descnoed in Item I above) • • O PONERPLANT 0 0 PROPELLER Type 0 APPLIANCE • laantartebaer 6. Conformity Sta ement A. Agency's Name and Address 8. Kind of Agency caw CE Avionics Inc. U S. Certificated Mechanic I Mantairclumr mews 2789 Flightline Avenue Altair bananas mechanic C. Certificate No. oo Sanford Va.• FL x Ocala; OW re 32773 cony LISA Ceti/dated Pilaintensnc•Oroandaeon OE4R411M D. !certify that the repair and/or alteration made to the unit s) identified in Rent 5 above and described on the reverse a attachments neitio have been made n accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and coned to the best of my knowledge. Extended range fuel Signature/Date of Authorized Individual per 14 CFR Part 43 APP. 8 7 1-z:-/-ie f e7K/ JAN 1 9 NU 7. Approval for Return t Service Pursuant to the authority given persons specified below, the unit identified in item 5 was nspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is Approved 0 RejeCted FAA Fe Standards Manufacturer Maintenance Organization Persons Approved by Canacban Inspect ment of Transport 8v Other (Speedy) FAA Designee X Repair Station Inspection Authorization Certificate ix Signature/Date of Authorized I Designation No OE4R411M 7. JAN 2 9 2013 one 337nocei SDNY_GM_02753778 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240700 EFTA01326293 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. S. Description of Work Accomplished RI more space is required. Misch additional sheets. Identify yarn am a nat y and repstration mark and date non( completed) USA N423TT JAN 2 9 2013 Nationally al Regesiration Mark Date Removed AirCell P12192-002 Corded Handset and replaced with P121357-002 cordless handset. Installed AirCell ATG 4000, Pan Number P13989 Air-To-Ground (ATG) Broadband Transceiver in the aft fuselage equipment bay at F.S. 724 with AirCell ACM. Part Number P14126 Configuration Module in the forward cabin RH equipment bay at F.S. 159. Mounted two each AirCell Pan Number P12344 Remote Diversity Antennas on the inside of the forward right hand storage cabinet at station 193A+7.0. Installed two each. AirCell Pan Number P12949 ATG UHF Antennas on the bottom of the fuselage per DDH Group Drawing Number ER02222-001, Revision 0 (Approved on FM Form 6110-3 dated January 18. 2013 by David E. Haralson, 0ERT-810028-SW. Structural at F.S. 598 and 749. Interfaced the AGT 4000 System per the attached CE Avionics. Inc. Drawing Number 66268-1VVD, Revision IR (Approved on FM Form 8110-3 dated January 18, 2013 by Leslie S. Roblin, DERT-510335-SW, Avionics/Electrical Systems & Equipment). The system is powered by the cockpit controlled cabin bus. Cabin wireless intemet is not enabled at this time pending incorporation of approved STC. Primary AGT 4000 power is connected to il 5-amp circuit breaker and primary ACM power connected to a 1-amp circuit breaker per manufacturer's specifications. Electrical load computed and found to be within acceptable limits. Instructions for continued airworthiness for the ATG 4000 System are contained in the attached CE Avionics Inc. Document Number 64961-1ICA. Installation of the above made in conformance with AirCell ATG 4000 Installation Manual Pan Number 013928. Revision C dated April 2011; AirCell kocess Installation Manual Part Number 012004, Revision E dated March 2010; AirCell Antenna Installation Manual Pan Number 800-10355, Revision E dated May 2009; Gulfstream IV Maintenance Manual. Revision 63 dated September 30. 2012, Chapter 6, Sections 06-00-00 and 06-50-00; Chapter 20, Sections 20-24-00, 20-25-07, 20-28-00, 20-28-09, 20-42.00 and 20-70-11; Chapter 24, Sections 24-004)0. 24-02-00. 24-02-01; 24-03-00 and 24-03-02; Chapter 34. Section 34-02-00; Chapter 51, Section 51-00-00; Gulfstream IV Wiring Manual, Revision 46 dated September 30, 2012, Chapter 20. Sections 20-00-00, 20-24-00. 20-25-00. 20-25-01. 20-25-03. 20-25-05, 20-26-00, 20-26-01, 20-26-03, 20-26-07, 20-2741, 20-27-03, 20-28-01, 20-28-05 and 20-28-07; Chapter 34, Section 34-60-00; and in compliance with FAR 25.1301, 25.1309, 25.1351, 25.1353, 25.1357 and 25.1431. ND El Additional Sheets Axe Attached 11 Pages FAA Form 337neen SDNY_GM_02753779 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024070I EFTA01326294 Attachment FM Form 337 (AGT-4000) Dated January 29. 2013, N42377. Gttlistrearn G-IV. SIN 085 Sheet 0111 hp it E !E ii &! I .-•A ii i Hlli IOW .. n il s "I 9 |||||| iiii if g !Hill Ifilks 1 — • i IF, ..... -- Ati i SDNY_GM_02753780 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240702 EFTA01326295 SDNY_GM_02753781 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240703 EFTA01326296 N C n -0 7a 0 n H 70 7a 70 Gl 1 70 0 -011 -012 00 FWD MRCELL BROADBAND AFT MRCELL BROADBAND ANTENNA INSTALLATION ANTENNA INSTALLATION LD LOWER FUSELAGE SKIN LOWER FUSELAGE SKIN VIEW LOOKING RIGHT LHS VIEW LOOKING RIGHT LHS /- 1 O O I ‘.(11 t •SIOnon ofteate. Wt_ ca.rea .oto. ass twieftnseyiepots /Le soma. a Mil t. csinsoa. ape hts• Doe wan rannata en, rim oil NOW( I ER02222401 I 0 2 OS 4 NJ h a Hs I S 2 EFTA01326297 SDNY_GM_027.783 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240705 EFTA01326298 In co n A0006 COWIT 1.011.0150.01 (Co /0/404/0 am •eist•1MYI.R CMC wont H 00, 02017C101,1k w Inc '4—.— 001 001001.111 k02001.104 A.. L001100.0000•14010 paw i -O 14/0011402T10111.11•100.40•01 COMMA, NOLO V.COMPMD CITIL0 y 0.0 - 00 0 ,1COW* 0 (4 - COMONOt LCCATION Vent 0401,•3 =KW 0118.115 Mr) H rn n Natal MG Arnim& pol H '• •• • ••••• • • • / I. • O O 0 I j 0 0 0 7u • ../ / • ./ G') •• •. „ec .• (4/4 - • It•D i 11 •• ••••••" ••••. -c) ••• I (f) SECTION BB (-011) SECTION 0-0 (412) VIEW LOOKING NORMAL TO Co el'el0640 Oen ANTENNA ATTACH SURFACE. SECTION AA (411) LOWER FUSELAGE COVER PLATE VIEW LOOKING DOWN nW P I-, 10 Nos rte....err me era ors-. are Olirturrar a:mealier am no !PQM Orr. red ter..0.• 0.00. rrO••• ter • 0.0.00./11 6040 interrIO ER02222401 3 OF. Oa '6,4 r 0- EFTA01326299 SDNY GM 02753785 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240707 EFTA01326300 Attachment: FM Form 337 (AGT-4000) Dated January 29. 2013, N423TT. Gut!stream G.IV, SIN 1085, Sheet 4 of 11 SDNY_GM_02753786 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240708 EFTA01326301 SDNY GM 02753787 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240709 EFTA01326302 Attachment FM Form 337 (AGT-4000) Dated January 29. 2013. N423TT. Gu*Stream G.N. S/N 1085. Sheet 5 of I I DATE DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION January 18, 2013 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS MRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE Verdant Redly licaceper.ek.) NAME OF APPLICANT Gulfstream G-IV Airplane CE Avionics. Inc. LIST OF DATA IDENTIFICATION TITLE ER02054-001, Rev — Aircell Antenna Tapered Adapter. 12.4 Deg, Sht 1-4 ER02054.002. Rev— Aircell Antenna Tapered Adapter. 7.4 Deg. Sht 1-4 ER02222-001. Rev 0 Aircell Broadband System Antenna Installation, Sht 1.4 ER02222 Rev 0 Structural Substantiation — Aircell Broadband Antenna Installation for Gulfstream G-IV, sin: 1058 NORM: I) Per FAA Order 8110.37D Chapter 4-12.h. a) This approval is for engineering design data only. It indicates the data listed above demonstrates cornpliance only ugh the regulations spedlled by paragraph and subparagraph listed belOw as Applicable Requirements. b) This bent may not constiluM FAA approval of all ling tearing data necessary to. the substantiation of compliance to necessary requirements for the entire alteration. c) Structural aspects are approved. d) Approval of °lethal aspects and equipment Installed are not included. 2) The instalth must determine the correatibuity S this data with the aircraft configuration. Alter the repak or alteration the aircraft must be retuned to service hymned:tee personnel. PURPOSE OF DATA To approve structural aspects of an alteration to Gulfstream G-IV. sin: 1085 APPLICAIRE REQUIREMENTS (Liu speak armor) 14 CFR 25.301 25.303 25.305(a)(bxc) 25.307(a)(b) 25.601 25.603 25.605 25.607 25.609(a)(b) 25.611 25.613(811) 25.615 25.619 25.625 TCDS Al2EA Certification Basis: 14 CFR Part 25 through Amdt 25-56 (except 25.571 Amdl 25-22) CERTIFICATION • Under authority vested by direction of the Administrator and in accordance with contagions and limitations of appointment under Part 183 of the Federal Aviation Regulations. data ksthd above and on attached sheets numbered 0 have been exemineo in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. Recceimend oppeovelol these delt I ea< Therelom brow,* Item Sm. SIGNATUREIS) OF DESIGNATED ENGINEEFUNG REPRESENTATIVES) DESIGNATION NUMBER(S) CLASSIFICATIONS) David E. Haralsonj:):e eg,.. it - DERT-810028-SW Structural FM Form 8110-3 00) SUPERSIOES PREviOUS !ONION 010222240 oat SDNY_GM_02753788 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002407 10 EFTA01326303 SDNY GM 02753789 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240711 EFTA01326304 Attachment FM. Form 337 (AGT-4000) Dated January 29, 2013, N423TT, Gulfatream Gall, WI 1085, Sheet 6 of 5 a g A a • SDNY_GM_02753790 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002407 12 EFTA01326305 SDNY_GM02753791 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240713 EFTA01326306 Attachment FM Form 337 (AGT.4000) Dated January 29, 2013, Na233T, Gultatmarn G-N. SIN 1085. Sheet 7 all E 9: Fp a O *0! IyyI;I'1 41 SS- 3 Ix SDNY_GM_02753792 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002407 14 EFTA01326307 SDNY_GM_02753793 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002407 15 EFTA01326308 Attachment FAA Form 337 (AGT.4000) Oated January 29, 2013, N423TT, Gulfstream G-11/, SIN 109S, Sheet 8 of II SDNY_GM_02753794 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002407 16 EFTA01326309 SDNY GM 02753795 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002407 17 EFTA01326310 Attachment FM Form 337 (AGT-4000) Dated January 29. 2013. N423TT. Gulfstream Gar. SIN 1085. Sheet 9 of 11 U.S. DEPARTMENT OF TRANSPORTATION L DATE FEDERAL AVIATION ADMINISTRATION January 18, 2013 STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MANE 3. MODEL NO 4 TYPE (Aim,* Err* Proponor, Mc/ 5 NAME OF APPLICANT Gulfstream Aerospace G-IV AIRPLANE CE Avionics Sanford, Fl. LIST OF DATA 6 IDENTIFICATION 7. TITLE 66268-1WD. Rev IR, Aircell ATG 4000 High Speed Internet System dated 12/27/12 END Nola: 1) The electrical aspects way of the above listed data are approved herein This approval is for erigineereg design data only. It Indicates the data listed above demonstrates corerlance onq Writhe regulations specified by paragraph and subparagrarn listed below as 'ARROW* Requirements'. 2) Compliance With stsiionsi regulations not listed may be rewired. This form does not constitute FM approval of all the engineering data necessary for substanballon of compliance to necessary requirements for the entire alteration. The stnicturel aspects are not Inckeded In this approval. 3) Mar the Alteration, the aircraft mull be retuned to senke by FM Authorized personnel. 4) Cabin Wireless Internet capability is NOT enabled; Pending Incorporation of Supplemental Type Cerillication. 5 PURPOSE OF DATA Design approval in support of installation modifications to Gullstream G-IV Series aircraft, serial number 1085. registration no. N423TT. Avionics/Electrical Systems 8 Equipment Design Approval Only. 9 APPLICABLE REOUIREMENTS OF !TILE II CFR (del specific seams) FAR 25.869 (a)(4); Arndt 25-72 FAR 25.1353 (b)(d)(1)(2); Amdt. 25-113 FAR 25.1301 (8)(1)(2)(3); Arndt. 25-123 FAR 25.1357 (a) Amdt. Orig. FAR 25.1307 (c); Amdt. 25-72 ici CERTIFICATION -Under aulhority veiled by direchon Cl Ike Admnislator and in accordance war GOIldia04$ WA Ihrstabons of appointment under 14 CFA Pail 183. WO baled abaVO and on ottecned sheers mantesei None have been examined In aCcordenCe Nth eslatdshed procedures and found lo comply yea applicable IOCMIanlatAll al ma Nrwortirmss Standards kited 0 Recommend approval of these data I pot) Mesita 0 Approve these data II. SIGNATURE(S) OF DESIGNATED ILGNEE RING REP S IJTATIVEISI 12 DESIGNATION NUMBERS(S) 13. CLASSIFICATIONS) Lewd S. Roblin Ire SP 1 DERT-510335-CE Avionics/Electrical Systems 8 Equipment FAA Form 8110-3 (03no)SuPERCEDES PREVIOUS ED4DON (ON recelt4 doe) 13010 SDNY_GM_02753796 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 0024071S EFTA01326311 SDNY_GM_02753797 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240719 EFTA01326312 Attachment: FAA FO1111 337 (AGT-4000) Dated January 29. 2013. N423TT, Gulista:tam G-N. Sm 1085. Sheet 10 01 11 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS, AIRCELL ATG 4000 HIGH SPEED INFLIGHT INTERNET SYSTEM CE Avionics Inc. Document No. 66278-1ICA, Rev. IIR I. Introduction Aircraft that has been altered: Registration No. — N423TT, Make — Gulfstream, Model —G-IV, Serial No. 1085 Content, Scope, Purpose and Arrangement: This document identifies the Instructions for Continued Airworthiness for the modification of the above aircraft by installation Man AirCell ATG 4000. Applicability: Applies to aircraft altered by installation of the AirCell ATG 4000. Definitions and Abbreviations: None, N/A. Precautions: None, N/A. Units of Measurement: None, N/A. Referenced Publications: AirCell ATG 4000 Installation Manual Pan No. D13485. AirCell Antenna Installation Manual Pan No. 800.10355. AirCell ATG Quick Reference Troubleshooting Guide Part No. D14748. Distribution: This document should be a permanent aircraft record. 2. Description of the Alteration Installation of the AirCell ATG 4000 System with interface to the Number 2 Flight Management System. Refer to Section 10 of the AGT 4000 Installation Manual for interconnect infomiation. 3. Control, Operation Information Refer to Section 4 of the AGT 4000 Installation Manual. 4. Servicing Information N/A 5. Maintenance Instructions Maintenance of the AirCell Alt 4000 System is 'on condition' only. Periodic maintenance is not required. 6. Troubleshooting Information Refer to Appendix A of the ACT 4000 Installation Manual. 7. Removal and Replacement Information Section 3 of the AGT 4000 Installation Manual. If the unit is removed and reinstalled, a functional check of the equipment should be conducted in accordance with Section 4 of the AGT 4000 Installation Manual. 8. Diagrams Refer to Section 10 of the AGT 4000 Installation Manual. 9. Special Inspection Requirements N/A 10. Application of Protective Treatments N/A II. Data: Relative to Structural Fasteners N/A 12. Special Tools N/A Page I oft SDNY_GM_02753798 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240720 EFTA01326313 SDNY_GM_02753799 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024072! EFTA01326314 Attachment: FAA Form 337 (AG7-4000) Dated January 29. 2013. N423TT, Gulfstream S/N 1085. Sheet 11 oftt 13. This Section is for Commuter Category Aircraft Only A. Electrical loads: N/A. B. Methods of balancing flight controls: N/A. C. Identification of primary and secondary structures. N/A. D. Special repaii methods applicable to the airplane: N/A. 14. Overhaul Period No additional ovedmul time limitations. IS. Airworthiness Limitation Section N/A. 16. Revision To revise this ICA, a letter must be submitted to the local FSDO with a copy of the revised FAA Form 337, and revised ICA. The FAA inspector accepts the change by signing Block 3 and including the following statement: "The attached revised/new Instructions for Continued Airworthiness (date X X-XX-XX ) for the above aircraft or component major alteration have been accepted by the FAA, superseding the Instructions for Continued Airworthiness (date X X -X X - X X )" 17. Assistance Flight Standards Inspectors have the resources to respond to questions regarding the ICA. 18. Implementation and Record Keeping For major alterations performed in accordance with FAA field approval policy, the owner/operator operating under Part 91 is responsible foi ensuring that the ICA is made part of the applicable section 91.409 inspection program for their aircraft. This is accomplished when a maintenance entry is made in the aircraft's maintenance record in accordance with section 43.9. This entry records the major alteration and identifies the original ICA location (e.g., Block 8 of FAA Form 337, dated X X-XX-XX ) along with a statement that the ICA is now part of the aircraft's inspection/maintenance requirements. Page 2 of 2 SDNY_GM_02753800 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240722 EFTA01326315 SDNYGM02753801 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240723 EFTA01326316 FrmApasual Elmircnic Trader; tancra OMB No 2120=0 Ilan/200? 0 MAJOR REPAIR AND ALTERATION FAA Use Only or Iron...rein,' (Airframe, Powerplant, Propeller, Or Appliance) Friend ANS* Aaninistracien INSTRUCTIONS: Print or type al entries. See Title 14 CFR §43.9. Parl 43 Appendix B, and AC 43.9-1 (ce subsequent revision thereof) for nstructions and disposition of this form. This report is required by law (49 U.S.C. 44470 ). Failure to repel can result in a civ4 penally for each such violation. (49 U S.C. §46301(e)) Nationally and Registrabon Mark senaI NO. USA N42317 1085 1. Aircraft 'Make Series Gulfstream Aerospace G-IV Name (As shown on registration cerbitcate) Address (As shown on tegisfrabon certificate) mwen 515 N Flaoler Drive, STE P40O 2. Owner TRT Leasing ay West Palm Beach Son Florida so 33401-4320 cans USA 3. For FAA Use Only 4. Typo 6. Unit Identification Repa , Morahan Unit Make Model Serial No. g2 AIRFRAME (As described in teem f above) El I:l POO/ERRANT El El ii PROPELLER Type 0 APPLIANCE 0 'Manufacturer 6. Conformity statement A. Ageneys Name and Address 8 Kind of Agency i... CE Avionics Inc. U S Contra...1 mechrmc I Manufacturer ••••••• 2789 Flightlme Avenue ;weir Certhcala0 M•CnanC C. Certificate No. ou Sanford ash FL x _ Cerebrated Reps. Stabta a 32773 ohms USA ceinissite4 maintenance Organization 0E4R411M D. I certify that the repair andior alteration made to the unfi(s) identified in Item 5 above and °escrow on the reverse a attachments hereto have been made in accordance with the requirements of Pad 43 of the U.S. Federal Aviation Regulations and that the inkurnaliOn furnished herein is the and correct to the best of my knowtedge. Extended range fuel SgnalurelDale of Authonz erai per 14 CFR Pat 43 O APO. B 7‘f a tk esaV - -Z — Michael. E. Hughes January 29. 2013 7. Approval for Return to Service Pursuant to the arthartY g yen persons speciierl whs, the unit identified in item 5 was inspected in the manner prescribed by the Administrator of the Federal AVOMIOn Administration and Is Approved 2 • Rejected FM Fit Standards PerionS Append by Canadian Manufacturer Maintenance Organization DepartmeN of Tronspon Inspector BY r (Bleary) FAA Designee X Repair Staban Inspection Authorization Certificate or Sonaluremate ofkuthorized .i. ... I Designation No. OE4R411M es Michael, E. Hughes January 29. 2013 ore 337ncau SDNY_Girl_02753802 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240724 EFTA01326317 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with allprevious alterations to assure continued conformity with the applicable airworthiness requirements. 8. Descent/cm of Work Accomplished of m003 Space is requited. attach additional Sheets aleatory with *Mae nettOrialay and registration mark and date work completed) L SA N423TT Naborialey and RegisUalion Mark Date January 29, 2013 Completed activation of AirCell ATG 4000 Wireless High-speed *nternet in compliance with Duncan Aviation STC Number ST01625W1-D and the following Duncan Aviation Documents: Master Document List Document Number 110121028, Revision E. Follow On Installation and Configuration Document Number 110315014, Revision E. Follow On Ground Test Procedure Document Number 110121020, Revision D. Instructions for Continued Airworthiness Document Number 110121022, Revision C. Duncan Aviation FAA Approved Flight Manual Supplement Document Number 110121021, Revision B placed on board the aircraft in the Approved Airplane Flight Manual Supplements binder. Weight and Balance information not affected. ❑ Additional Steels We reached Pages FAA Form 337 flow SDNY_GISI_02753803 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240725 EFTA01326318 }unlit! Atha of America 4fiepartment of tEransportation Atbernl "thiattion Abininistrution $upplemental 'Type aertifiratt Aam4.ST01625V/I-D STC No. ST01625WI-D FL err4earwar itauentio Duncan Aviation, Inc. Enable WLAN System 3701 Aviation Road for use on Lincoln, NE 68524 Gulfstream G-IV sin 1085 if:4A da/14 okra doinoriviinfraGALAt elatzlihAtikaiw aaaferaiahavat denyevo abl +1041.avera nosa.0 Gee aercontesenu esperthradwa eMent25 e/66 Federal Aviation i iregattrivel. aviatatileluel- -.54,gienceealeiglnds, Al 2EA Gulfstream Aerospace Corporation Aga GV 91110•9•6•.• 0/3;•• fkleic4gra,s11A' Enable Wireless Local Area Network (WLAN) system for use with Transmitting Portable Electronic Devices (TPEDs). Data Required: (I) Duncan Aviation Inc., Document List No. 110121028, Revision A, dated March 18, 2011, (2) AAA Approved Airplane Plight Manual Supplement, Duncan Aviation Inc., Document No., 110121021, Revision A, dated March 18, 2011, or later FAA Approved Revisions to (1) or (2). SeirIdahh•J 044111:•••414W,' This system is intended to provide internist connection and email services using TPEDs. Any other intended function of this equipment will require a re-examination of the certification basis. Compatibility of this design change with previously approved modifications must be determined by the installer. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. FL twes4n4..z.,,,a4myr e,c4,44,add.) [4law gornivaidarreowan 4. r/~idanahe.n.a4id .vereertied meaty a Ardi.eloiva .44 a tdiertoas eatted.,44. Addeuileata.04.5;raigoiates SethAtlina 44 eiscpriaohivs Fans.). 1,2011 git4 taws( .944 *ea:wagon. Moat 11,2011 floks an/waled May 27,2011 4 o) atrick M. Chick, Jr. ODA administrator, ODA-501013-CE Duncan Aviation, Lincoln, Nebraska (Mk) anttr K a4 palJtttra 4 1•• • Sr a ft.ae tag . or y,tallaat nee toscacligmies. Or Leto. ha rah oho-too-4h Ma I or r air tete certified. ••• to convents: in •ecordase• with IAA V. O. SDNY_GM_02753804 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240726 EFTA01326319 SDNY GM 02753805 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240727 EFTA01326320 DINCAN AVIATION I II 1 Authorization of STC use: In reply please reference: 2013-028L Date: January 15, 2013 To: CE Avionics Inc. Attn: Brian Rannie 2789 Flightline Ave Sanford, FL 32773 Authorization is herby given for one time usage of FAA Supplemental Type Certificate Number ST01625WI-D to enable WLAN System. This installation is approved for Gulfstream G-IV sM 1085 1 only. Deviations to this subject data are the sole responsibility of CE Avionics Inc. If your engineering department has any questions about this STC, feel free to contact me at r by email at Douglas Bates Engineering Records Tech Duncan Aviation 3701 Aviation RD Lincoln, NE 68524 USA 1 1 Lincoln Anpoti P.O. Jinx 81887 Lincoln. Nebraska 68501 402.475.2611 Pax 402.475.5541 www.diencannvincion von, SDNY_GM_02753806 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240728 EFTA01326321 SDNY_GM_02753807 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240729 EFTA01326322 Form naretwed Navas imamMuster We to 21204020 el leo traVIO., us Osentro MAJOR REPAIR AND ALTERATION For FAA UR CsiO a Trtnspennon (Airframe, Powerplant, Propeller, or Appliance) Fake& Aetna, 1ids-billed. INSTRUCTIONS: Print or type all envies. See Title 14 CFR §43.9. Part 43 Appendix B. and AC 43.9.1 (or subsequent revision thereon for Instructions and disposition of Mis form. This report is required by law (49 U.S.C. §44701). Failure IC repot can result in a civil penally for each such violation. µ9 U.S.0 448301(0)) Nationality and Registration Mart Serial No. USA N423TT 1085 1. Aircraft Make Model Series GULFSTREAM GIV Name (As shown on regatrabon certificate) Address (As shown on foist:anon Certificate) Mtn 51S Ist Fl Ant FR nR STF PAM 2. Owner O,1 WEST PALM BEACH flee FL TRT LEASING INC no 33401-4320 Cony USA 3. For FAA Use Only 4. Type 5. Unit Identilkation Repair Alteration Una Make Model Serial No. 0 A/RFRAME (As eaSenDed,n nem i abate) El O O POIAERPtAP4T O O PROPELLER Type O APPLIANCE Manutedwar 0 S. Conformity SO ement A. Agency's Name and Address B. Kind of Agency sere (WI FSTRFAM U.S. Cenicated Nahum I mentiouunse AMMO 1500-C PERIMETER RD. Fcreign Cenificese Methane C Cenific.ste No. car WFST PM M REACH en Fl / CertAcezed Repair Stamm Da 33408 co , USA Cerukraect Meneenenoe Organization CRS PB8R624N 0. I eitetey Mal the repair and/or aaeration made to the unit( ) idenlifienl in item S above and descried on the reverse or attachments hereto have been mode In accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished eerekl Is true and correct to the best of my knowledge Extended range fuel Signature/Ds IAuthorized I iveual m pet 14 CFR Part 43 O App. 8 I. 4 Terry Barker 08/15/2012 7. Approval for Return to Service P masa to the authority given specified below. the unit identified in item S was inspected in to manner prescribed by the Administrator of the Federal Aviation ministration and is R Approved ..O Rejected FAA Flt. Standards Manufacturer MairiteMACe Organization Permed APIXO7W by Canaan Inspector ed Transpon 8Y Other (Speedy) FM Designee I Repair Station Inspection Authorization Certificate or Signal° at Authorized Inc* „. Designation No. 0,y t CRS PB8R624N p James Fishburn 08/15/2012 FAA Form 337 noon SDNY_GM_02753808 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240730 EFTA01326323 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. S. Description of Work Accomplished Iona* and repiygapn Tat* and date work completed.) (If more space is required, attach addiffonal sheets. Identity with aircraft net - USA N423TT 08/15/2012 Nationality and Registrabon Mark Date Aircraft Model: Gulfstream GIV Aircraft Serial Number 1085 Reference Gulfstream Pal Work Order: SC11231 Complied with STC ST00544LA - Installation of Concorde Battery sealed lead-acid Battery Model No. RG-380E/44 UAW STC ST00544LA and steps II A 2 & 3 of Concorde Battery Corporation Master Dwg. Number 12 for Model RG-380E144 Lead acid batteries. Rev A dated August 28 2000. Permanently removed the following equipment: 2 ea. Saft Nickel-Cadmium Main Battery, Model 4076-11 Installed the following new equipment: 2 ea. Concorde sealed lead-acid Battery, Model RG-380E-44 No Weight and Balance change required by this action (weight change negligible). No Airplane Flight Manual Supplement required by this action. Airplane records updated to reflect this action. Aircraft electrical load not affected by this action. Instructions for Continued Airworthiness can be found in Concorde document No. 5-0171 Rev. M. dated 03/15/2012. Note: This amendment, dated 08/1512012, supersedes the original 337 dated 08/06/2012, and the amendment dated 08/08/2012. and removes 'Concorde Battery Corporation Master Dwg. Number 12 for Model RG-380E/44 Lead Acid Batteries, Rev. A dated 08/28/2000" from the ICA statement. END ❑ Additlifiel.Shaels Are Attached FAA Form 337 nom SDNY_GM_02753809 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240731 EFTA01326324 \.,--i// MAJOR REPAIR AND ALTERATION form.prowe OMB No 2I2POCQO Wiffai I Eno.* Tredire veneer fee FMUr OW? US eopsersent el TWOKSICA (Airframe, Powerplant, Propeller, or Appliance) Fedstil Mines A•alalwaece INSTRUCTIONS: Print or type all enthes. See Title 14 CFR 643.9. Pan 43 Appendix EL and AC 43.9-1 (or subsequent revision thereof) for Instructions and dIsposeion of this form. This report is required by law (49 U.S.C. §44701). Failure to report an result in a dig penalty for mach such violation. (49 U.S C §48301(a)) Nationality and Repistrason Mark Serial No. USA N423TT 1085 1. Aircraft Make Model Series GULFSTREAM GIV Name (As snown on recestratron certificate) Address (As shown on registration cerbficate) meow Kin N Fl Anl FR nR TIT PAM 2. Owner On WFST PALM BEACH set. FL TRT LEASING INC zo 33401-4320 Cann; USA 3. For FAA tied Iv 4. Type 5. Unit Identification Reps( Alteration Unit Make Model Serial No. IZI AIRFRAME (As deSonbed in an 1 above) El O O POWERPLANT El O PROPELLER Type O APPLIANCE O manwarmer 6 Conformity Statement A. Agency's Name and Address S. Knd of Agency rem MO FSTRFAM U 5 Congealed Mechanc I Naumann:. mew. 1500-C PERIMETER RD. Faeign Calif.:OS Mecmnic C. Certificate No. ow WEST PAI M RFACH sow.Fl / CeMeateii Repair Medal v. 33406 ewe., USA Courcared maintenance Oranizethe CRS PB8R624N D. I Certify that the repair and/or alteration made lo the unit( ) denbried in item 5 Move and described on the reverse or anachments hereto have been made in accordance with the requirements 01Pan 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and cared to the best of my knowledge. Extended range fuel Signature/0 trd Ind ual .. per 14 CFR Penal) II App. 6 p28 Terry Barker 08/08/2012 7. Approval for Return to Service Pursue 1 to me aulhontY 9 en ;sons Specified below, the unit identified in Rem 5 was inducted n the manner presaibed by the Administrate( of the Federal Aviation Administration and a 2 Approved II Rejected FM Ft. Standards Peewee ApPaasee by Can110451 Inspector Manufacturer maintenance Organization Department 04 Tramped BY Other (SpeCify) FM Designee I Repair Station Inspection Aulhonzabon Dedicate or Signature/Date Authorized I Designation No. den t CRS PB8R624N James Fishburn 08/08/2012 FAA Form 337 once) SDNY_GM_02753810 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240732 EFTA01326325 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be Compatible with all previous alterations to assure continued confonniry with the applicable airworthiness requirements. IL Description of Work Accomplished (IImote space p teetered. Mace acklemnal sneers. Identify waft aircraft nattonably and reed:ration mark and date work completer') USA N423TT 08/08/2012 tlitoommy and Repistratco Mark Date Aircraft Model: Gulfstream GIV Aircraft Serial Number: 1085 Reference Guffstream PBI Work Order: SC11231 Complied with STC 51005441A - Installation of Concorde Battery sealed lead-acid Battery Model No. RG-380E144 IAW STC ST00544LA and steps II A 2 & 3 of Concorde Battery Corporation Master Dwg. Number 12 for Model RG-380E144 Lead acid batteries. Rev A dated August 28 2000. Permanently removed the following equipment: 2 ea. Saft Nickel-Cadmium Main Battery, Model 4076-11 Installed the following new equipment: 2 ea. Concorde sealed lead-acid Battery, Model RG-380E-44 No Weight and Balance change required by this action (weight change negligible). No Airplane Flight Manual Supplement required by this action. Airplane records updated to reflect this action. Aircraft electrical load not affected by this action. Instructions for Continued Airworthiness can be found in Concorde Battery Corporation Master Dwg. Number 12 for Model RG-380E/44 Lead Acid Batteries, Rev. A dated 08/28/2000, and Concorde document No. 5-0171 Rev. M. dated 03/15/2012. Note: This amendment, dated 08/0812012, supersedes the original 337 dated 06/06/2012, and adds the Instructions for Continued Airworthiness. END O AQdeIMA4)neets Are Attached FAA Form 337 now Nei SDNY_GM_027538t 1 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240733 EFTA01326326 ran APWIhea EMCItrOC TWOS( I Ninte, 0 mwo me n 3129CO20 MAJOR REPAIR AND ALTERATION 6• yen Vas Orer us DIDIMMOI at Tromoortrion (Airframe, Powerplant, Propeller, Or Appliance) Foam, aviation Aasenlernace INSTRUCTIONS: Prom or type all entries. See Tile 14 CFR 643.9. Part 43 Appendix B. and AC 439.1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 944704 Failure to report can result in a civil penalty br each such vtolabon. (49 U.S.C. §46301(a)) Nationality and Registration Mark Serial mo. USA N423TT 1085 1. Alreraft Make Model Series GULFSTREAM GIV mamk (As ShoWlIOn registration certificate) Address (As shown on registration certificate) Amon MR N Fl Ant FR nR STF Pa00 3. Owner Car WEST PALM BEACH Seri. Fl TRT LEASING INC To 33401-4320 cosh, USA 3. Fa FAA Use Only 4. Type 5. Unit Identification Repair Alteration Unit Make Model Serial No. p AIRFRAME (As describer:tin neon I above) O 0 O POWERPLANT O O PROPELLER hype O APPLIANCE O MarntaClurat 6. Conformity Statement A. Agency's Name and Address B. Kind of Agen y own Fall FSTRFAM U S. Certificated Mechanic I Manufacturer mem 1500-C PERIMETER RD. Forage Cenncares Mechanic C. Certificate No. ow MST PALM BFACH on. FL j Cenecaoss RaPai, Station Le 33406 cam, USA Centered Membrane* Organization CRS PEI8R624N D. I certify that the repair and/or alteration made to the unit( ) identified in item 5 above and described on the rove 'se Or a ttathrnants hereto la been made in accordance with the requirements of Part 43 of the U S Federal Aviation RegullitiOns and "•'.il the I-1ormaliOn furnished hereon is true and correct t0 the best of my itnewledge. Extended range fuel Si nature/Dat0 o fined per is CFR Part 43 MI OF g APP. B Terry Barker 06/06/2012 . Approval for Return to Service Pursuant to the authonty given rsons Specified below. the unit .dented In item 5 was Inspected in the manner prescribed by the Administrator of the Federal MOW Administration and is O Approved O Retooled FAA FR. Standards Persona AFprovad by Camden Manufacturer Maintenance Organization Departmental Transport Ocisartment InSpettOr BY Other (SPearn FAA. Designee ,/ Repse Station Inspection Authorization carificii. or Signature, ate of Au Individual Designation No 03 , CRS P88R624N James Fishburn 06/06/2012 FAA Form 331(loo) SDNY_GM_02753812 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240734 EFTA01326327 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be Compatible with all previous alterations to assure continued Conformity with the applicable airworthiness requirements. S. Description of Work Accomplished (it more space is required, attach additional sheets Identity well entree nationality endregistration mark and dare wore carom Wed USA N423TT 06/06/2012 NaloMMY and Degreiration Mark Oate Aircraft Model: Gulfstream GIV Aircraft Serial Number: 1085 Reference Gulfstream PSI Work Order: SC11231 Complied with STC ST00544LA • Installation of Concorde Battery sealed lead•acid Battery Model No. RG-380E144 IAW STC ST00544LA and steps II A 2 & 3 of Concorde Battery Corporation Master Dwg. Number 12 for Model RG-380E/44 Lead acid batteries. Rev A dated August 28 2000. Permanently removed the following equipment: 2 ea. Saft Nickel-Cadmium Main Battery. Model 4076.11 Installed the following new equipment: 2 ea. Concorde sealed lead-acid Battery, Model RG-380E-44 No Weight and Balance change required by this action (weight change negligible). No Airplane Flight Manual Supplement required by this action. Airplane records updated to reflect this action. Aircraft electrical load not affected by this action. END J heels Are Attached FAA Form 337 yeah SDNY_GM_02753813 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240735 EFTA01326328 Fon" atOmnta Iltetac mixing Mower OM Na 21204020 /30. MAJOR REPAIR AND ALTERATION 0 LIS Doporbwr 11 2007 am FAA1)•• Only oi Inonrpriso” (Airframe, Powerplant, Propeller, or Appliance) roes Artesia Adiekrusein INSTRUCTIONS: Print or type at entries. See Tide 14 CFR §43.9. Pan 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of the teem. This report is required by law (49 U.S.C. §44701). Failure o report can result in a civil penaity for each such violation. (49 U.S.C. §48301(a)) Nationality and Registration Mark Serial No. N423TT 1085 1. Aircraft Make Model Series Gulfstream G -IV Name (As shown on registratton certificate) Address (As shown on registration certificate) Alone 05 N Fiedler Drive Suite P400 2. Owner TRT LEASING INC tier West Palm Beach thus Ft As 33401.4320 _ . tear USA 3. Far FAA Use Only 4. Type 5. Unit Identification Reese Mershon Unit Make Model Serial No. 0 0 AIRFRAME (As descrtbed An Item I above) 0 o powERRANT • 0 PROPELLER Type O APPLIANCE 0 Manulacturs 0 Confonnity StatiesseM __ A. Agency's Name and Address B. Kind of Agency rem tleneral Dynamic, Aviation Services u. S. Condkated Mechanic I htersitscsser *emu 1500-C Perimeter Road FOreign Unmated Latahant C. Certificate No. oft trftitSt Palm Beach lam FL j Caellkalad Repair Station z, 33406 Caw" USA PB8R624N CO41114104 Izamenanee 0rgenvation D. I certify that the repair and/or alteration made to the unit a) identified in item 5 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the intOnneion furnished herein is true and correct to the best of my knowledge. Extended range fiat Signature/Date of Authorized Individual PM 14 CFR Pali 43 O App. 8 Ali, elti.__.--- Stephen G. Paulsen 21 September 2007 7. Approval for Return to Service Pursuant to the authority given persons specified below. the unil identified in Item 5 was Inspected in the manner prescribed by the Administrator of the Federal Aviation AdrrinialnillOn and is O Approved O Rejected FAA Fn. SlandardS Panora ADP.Oved Ist Canadian Manufacturer Maintenance Organization Inspector I Depwtmem of Tranwort BY Other (Specify) FM Designee x Repair Staten Inspection Authorization Certificate or SignaturerDere of Authorized Ince/duel ...XS Designation No. CRS PB8R624N St dit-----.. Stephen G. Paulsen 21 September 2007 FAA Form 337 nee FAA SDNYGfil02753814 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002407 EFTA01326329 NOTICE Weight and balance or operating limilabbn changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (II more space is required. WWII additional sheets. Identify with aircraft nationality andregistration mart and date *orb completed.) USA I N423TT 21 September 2007 Nationality and Registration Mark Date Aircraft Model: G-IV Aircraft Total Time: 6728.0 Aircraft Serial No.: 1085 Aircraft Total Landings: 3057 Work Order No.: 17964 Accomplished upgrade of existing Allied Signal Enhanced Ground Proximity Warning System from a software version 104-104 to 218-218 UAW Gulfstream STC ST01851AT-D and Gulfstream Custom Engineering Drawing List CE41 4960458 and EGPWS Windshear (218-218) (MOD) Electrical Drawing CE41 3490238 approved under FAA Form 8110-3 dated 9/17/07. Updated Flight Manual Supplement with Gulfstream G-IV Flight Manual Supplement No. CE41 349M001 and provided EGPWS Instructions for Continued Airworthiness Report No. CE41 349A001. Change to Electrical Load negligible. No change in Weight or Balance. END 0 Additional Sheets Are Attached FAA Form 337 ilea Fax SDNY_GM_02753815 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA (x)244)737 EFTA01326330 Form Approved 0148 No. 2120-0020 0 MAJOR REPAIR AND ALTERATION For FAA Use Only aronpoowion (Airframe, Powerplant, Propeller, or Appliance) Office Identification Nowa ease Adirenianwee INSTRUCTOONS NM or type as entries. See FM43.9. FM 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. The report 4 required by law (49 U.S.C. 1421). Failure to report can ream in awl penalty not to exceed $1.000 for each Such vioUlion (Section 901 Federal Aviation Act of 1958) Make GULFSTREAM MCdelG-IV 1. Aircraft Serial No. Nationality and Registrabon Mark 1085 N877RP. None (As show, on registration certificate) Address (As shown on egssftation certificate) TRT LEASING INC 515 N FLAGLER OR STE P400 2. Owner WEST PALM BEACH FL 33901-4320 3. For FAA Use Only The alterMien identified henn nas been reviewed and found to be complete with appropriate DER approvals. All aspects of the atterabon(s) are compatible and eligible for use on the above described aircraft, subject to conformity Inspection by a person authorized in FAR 43.7. David Kelm 1---a—...--- 1 Y U.1/4...,_ MA Pr nil DOI 5t-) ‘I — n s o il r Serial 4. Unit Identification 5. Type tint Make Model No. Repair Alteration AIRFRAME (As described in Item I above) X POWERPLANT PRCPELIER Type APPLIANCE Manufacturer 6. Con enmity Statement A. Agency's Nana and Address B. Kind of Agency C. Certificate No. CAPITAL AVIATION. INC. U.S Cortiliesee liKheniC 5500 PHILLIP J. RHOADES Fannon Certificate Nernst MZIR092Y HGR. 2. WILEY POST AIRPORT X Caninesisa ReNir Minion BETHANY OK 73008 Illanidechat D. i Caney mat ea row macs ataneen nude to the unite) denoted neer 4 above and 00•01trier on Inc reverse et erinolvnenrs memo have been mese n 41O:Ordend web Vie requinernenrs or Part 43 or tie V S Federal Mabee Regulate,,, and MN the Somalia, Ournonee hem e tee and COMPC113 the belt or fry sroirieope. Date Signature of Authorized e/ D1-2€297 MICHAEL S. ROPER 1 7. Approval for Return To Service P rsuant to the authority given pe sons specified below, the tint identified in item 4 was i ded en manner preSalbed by Me Administrator of the Federal Aviation Administration and is IM APPROVED O FM Flt. Standards Other (30.O69 Inspector Manufacturer Inspection Authorization BY Person Approved by Transport FM Designee X Repair Station Canada Airworthiness Group Date of Approval or Reaction Certificate or Signature of Authorized I ual Designation No. X91R092Y MICHAEL S. ROPER e le /iai s 24 9, 7 FAA Form 337(1201 EleattriC Yawn(MOW) SDNY_GM_02753816 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240738 EFTA01326331 Work cpndetad tot IN677RE) al NOTICE Weight and balance or Operabng Mrstabon changes Shall be colored in MO SparOpiate mraall MOM M Steredlan musi be Calipabble web apeman alteratiOrb 1001WO COntInUedCOnlarnily WI Me appeals anworthtless reqdrernent5 8. oeso.e..cel el Work Accomplished GULFSTREAM G-IV N677RP S/N 1085 W/O 1658 ELECTRICAL MODS The following is a list of drawings used for dte Mixliftcations and Alterations to the Phone, Entertainment and Electrical Systems: I. Report - ELA 06-10318, Electrical Load Addendum Gulfstrearn G-IV-S/N 1085, Rev.1/R, dated 03.26-2007. (4 Sheets) 2. 06-10319, Lay-Gut-G-IV, sin 1085 Cabin Modifications (4 Sheets) 3. 06-10320. W/D-G-IV S/N 1085 Drawing Notes. Rev.I/R dated 03.26-2007. (I Sheet) 4. 06-10321, W/D-G-IV S/N 1085 Vendor Information, Rev.UR dated 03.26-2007. (I Sheets) 5. 06-10322, W/D-G-IV S/N 1085 Cabin Equipment/Wiring Renitnials, Rev.1/R dated 03-26-2007. (14 Sheets) 6. 06-10323, W/D-G-IV S/N 1085 Ciricut Breaker Panel Mods, Re;/.1/12 dated 03-26-2007. (5 Sheets). ' 7. 06-10324, W/D-G-IV SIN I085.Terminal Block Layout, Rev.1/R dated 03-26-2007. (3 Sheets). 8. 06-10325, W/D-G-IV Sthl 1085 Galley Systems, Rev.1/R dated 03.26-2007. (9 Sheets). 9. 06-10326, W/D-G-IV S/N 1085 Aft Lavatory Systems, Rev.I/R dated 03-26-2007. (3 Sheets). 10. 06-10327, W/D-G-IV SIN 1085 Upwash/Downwash Lighting, Rev.UR dated 03-26-2007. (3 Sheets). 11. 06-10328, W/D-G-IV S/N 1085 Cabin Reading and Table Lihgts, Rev.I/R dated 03-26-2007. (3 Sheets). 12. 06-10329. W/D-G-IV 1085 Cabin Aisle Lighting, Rev.1/R dated 03.26-2007. (3 Sheets). 13. 06-10330, W/D-G-IV SIN 1085 Ordinance Signs, Rev. UR dated 03-26-2007. (3 Sheets). 14.06-10331, W/D-G-IV S/N 1085 Entry Lights, Rev.1/R ditted 03-'26-2007. (2 Sheets). IS. 06-10332, W/D-G-IV SIN 1085 Jump Seat Lihgts,Rev.11R dated 03-26-2007. (2 Sheets). 16.06-10333, W/D-G-IV S/N 1085 Cabin Window Shades, Rev.UR dated 03-26-2007. (4 Sheets). 17.06-10334, W/D-G-IV S/N 1085 Cabin/Lav Call Systems, Rev.1/R dated 03-26-2007. (2 Sheets). 18.06-10335, W/D-G-IV S/N 1085 Crew Lavatory System, Rev.1/R dated 03-26-2007. (2 Sheets). 19.06-10336, W/D-G-IV S/N 1085 Cabin Audio Mods., Rev.1/R dated 03-26-2007. (2 Sheets). 20.06-10337, W/D-C-IV S/N 1085 Entertainment Systems. Rev.1/R dated 03-26-2007. (8 Sheets). 21.06-10338, W/D-G-IV S/N 1085 Assess Phone System, Rev.I/R dated 03-26-2007. (2 Sheets). 22.06-10339, NOT USED. 23. 06-10340, W/D-G-IV S/N 1085 Cabin I I VAC Outlet Mods.,Rev.1/R dated 03-26-2007. (4 Sheets). 24.06-10341, W/D-O-IIV SIN 1085 CMK-1100 Electronic Flight Big Sys., Rev.I/R dated 03-26-2007. (3 Sheets). . . 25.06-10342, W/D-G-IV S/N 1085 Cabin Temp Control Mods, Rev. UR dated 03-26-2007. (2 Sheets). 26.06-10343, W/D-G-IV S/N 1085 XM Weather Receiver, Rev.1/R dated 03-26-2007. (2 Sheets): • 1 Data approved by Systems & Equipment DERT-710196-SW on FAA Form 8110-3 NJEN-07- 027dated April 04,2007. A EMI Test performed in accordance with Capital Aviation. Inc. EMI. Ground Test Procedures, Document No. 04-EMI-10000, Rev. I/R dated 11-22-2004. Document No. 04-EMI-10000 approved by Systems & Equipment - Avionics & Electrical DERT-710796-SW on FAA Form 8110-3, SLIFN-06- 074, dated September 26,2006. • • X 1Matti:nal Shears Aso anacnoo SONY_GM_02753817 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240739 EFTA01326332 Walt Completed for (N677RPI on a Description or work Arrornossreci NOTE: I. All NON-ESSENTIAL systems and equipment installed on existing Non-Essential Busses. Load Sheding covered in Aircraft Flight Manual. 2. See Capital Aviation, Inc. FAA Form 337 entitled "Interior Cabin Mods" for mounting of Electrical Equipment. Log Book Entry made. Weighed Aircraft, computed new C.G. and entered in aircraft records. CONTINUED AIRWORTHINESS - Monitor item(s) for condition. If item(s) become damaged, replace with same make and model. If make / model is not available, notify the local FSDO of part replacement. Refer item(s) to installer or any qualified service center for repair or replacement. Items to be inspected in conjunction with operators approved inspection program to insure secutity, overall condition and proper operation as is required. CULFSTREAM G-11/ N677RP SIN 1085 W/O 1658 )(Additional Sneers Are Attached SDNY_GM_02753818 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240740 EFTA01326333 SDNY_GM_02753819 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240741 EFTA01326334 U.S. DEPARTMENT OF TRANSPORTATION. DATE FEDERAL AVIATOR ADMINISTRATION April 4, 2007 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MODEL NO. TYPE (Aiplans. Reda bisticoeter. Ott) NUM OF APPLICANT MAKE GULFSTREAM G-IV Airplane Capital Aviation Inc LIST OF DATA IDFNTIFICATION TITLE DRAWINGS See sheet 2 of 2 SEE SHEET 2 OF 2 NOTES: ' 1.The Electrical Design Data Aspects Only of these data are approved herein. Approval is In support of a 337 Interior installation modification in a Gulfstream , Model G-IV, SIN 1085 only. 2. EMI test required prior to returning aircraft to service. PURPOSE OF DATA Approve the Electrical Design Data Aspects Only in support of a 337 installation (Major Alteration ) APPUCABLE REOUIREAIENTS (LW sPiscMe sections) FAR 25.1301(aXbXcXd), FAR 25.1309(a)(b), FAR 25. 1351(a), FAR 25.1357(a)(c)(d), FAR 25.1359(a)(b) ma • C:i".3LTIt with conditions and Flattens of appointment CERTIFICATION - Under authority vested by drecbon of the Administrator and In accordance numbered , 2 of 2 have been examined in under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets Federal Aviation Regulatlens accordance with established procedures and found to comply with applicable requirements of the 0 Recommend approval of those data Wore la Approve those data SIGNATU ) FIAT (S) OF 06.7 EERING REPRESENTATIVES) DESIGNATION NUMBERS(S) CLASSIFCATION(S) Joluaik et,_ a DERT-710196-SW Systems & Equipment • Avionics & Electrical 8110-3 JFN-07-027 ELECTRONIC FORMAT (740) FAA Form 8110.3 (11.70) SUPERSEDES PREVIOUS ELATION SDNYGM 02753820 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240742 EFTA01326335 SDNY_GM_02753821 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240743 EFTA01326336 FEDERAL AVIATION ADMINISTRATION FORM 8110 -3 FOR GULFSTREAM, MODEL GIV, S/N 1085 NUMBER: JFN-07-027A DATED 4-4-2007 SHEET 2 OF 2 DRAWING NOMENCLATURE REVJDATE EFFECTIVITY REPORT- ELECTRICAL LOAD ADDENDUM IR- Dtd. 03-2407 S/N 1085 ONLY ELA-10318 GULFSTREAM GIV-S/N1085 06-10319 LAY-OUT-GIV S/N 1085 CABIN I/R- Dtd. 03.26.07 " " MODIFICATIONS 06-10320 W/D-G-IV S/N 1085 MASTER DRAWING 1/R- Ott 03-26-07 " a NOTES - 06-10321 W/D-G-IV S/N 1085 VENDER INFORMATION UR- Dtd. 03-26-07 " " 06-10322 W/D-G-IV S/N 1085 CABIN • UR-Dtd. 03-26-07 " " EQUIPMENT/WIRING REMOVALS 06-10323 W/D-G-IV S/N 108.5 CIRCUIT BREAKER UR- Dud. 03.26.07 a " PANEL MODS 06-10324 W/D-G-IV WI 1015 TERMINAL BLOCK 1/R- Ott 03-26-07 a " LAYOUT 06-10325 W/D-G-IV S/N 1085 GALLEY SYSTEMS I/R- Dtd. 03-26-07. " " 06-10326 W/D-G-IV S/N 1085 AFT LAVATORY I/R- Did. 03-26-07 " SYSTEMS 06-10327 W/D-G-IV S/N 1085 UPWA$11/DOW14WASH UR- Did. 03-26-07 LIGHTING _ " 06-10328 - W/D-G-IV S/N 1085 CABIN READING AND I/R- Dtd. 03-26-07 TABLE LIGHTS " a 06-10329 W/D-G-IV S/N 1085 CABIN AISLE LIGHTING I/R- 06-10330 Dtd. 03-26-07 " W/D-G-IV SIN 1085 ORDINANCE SIGNS I/R- Dtd. 03-26-07 06-10331 W/D-G-IV S/N 1085 ENTRY LIGHTS " " UR-Dtd. 03-26-07 " " 06-10332 W/D-G-IV S/N 1085 JUMPSEAT LIGHTS I/R-Dtd. 03-26-07 " 06-10333 W/D-G-IV S/N 1085 CABIN WINDOW 1/R Dtd. 03-26-07 " " SHADES 06-10334 W/D-C-IV S/N 1085 CABIN/LAV CALL 1/R Did. 03-26-07 " SYSTEM 06-10335 W/D-G-IV S/N 1085 CREW LAVATORY I/R Dtd. 03-26-07 " " SYSTEMS 06-10336 W/D-G-1V S/N 1085 CABIN AUDIO MODS I/R Dtd. 03-26-07 " " 06-10337 W/D-G-IV S/N 1085 CABIN 1/R Dtd. 03-26-07 " " ENTERTAINMENT SYSTEMS 06-10338 W/D-G-IV S/N 1085 AIRCELL AXXESS UR Dtd. 03-26-07 " " PHONE SYSTEM 06-10340 W/D-C-1V S/N 1085 CABIN I1OVAC OUTLET 1/R Dtd. 03-26-07 " MODS 06-10341 W/D-G-IV S/N 10135 CMA-1100 ELECTRON IC UR Dtd. 03-26-07 a FLIGHT BAG SYSTEM 06-10342 W/D-G-IV S/N 1085 CABIN TEMP CONT ROL 1/R Ott 03-26-07 a MODS 06-10343 GIV S/N 1085 XM WEATHER SYSTEM I/R-Dtd. 03-26-07 " " SDNY_GM_02753822 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240744 EFTA01326337 SDNY_GM_027.823 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240745 EFTA01326338 U.S. DEPART/ea OF TRANSPORTATION DATE FEDERAL AVIATION N4SCTRAT1ON SEPTEMBER 26 2006 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDEMTTFC.ATON MAKE t&COEL NO. TYPE (Urprane. Radio. MIlkoplel. etc) NAME OF APPLICANT GulfstrearnAerospace G-iv Airplane Capital Aviation Inc Corporation LIST OF DATA IDENTIFICATION Ina DOCUMENT 04-EMI-10000 EMI GROUND TEST PROCEDURE REVISION 1/R DATED 11-22-2004 NOTES: 1.The Electrical Design Data Aspects Only of these data are approved herein. Approval is for the Gulfstream Aerospace Corp. Aircraft listed in TCDS Al2EA. Rev 29. PURPOSE CF DATA Approve the Electrical Design Data Aspects Only in support of a EMI Ground Test Procedure. APPLICABLE REQUIREMENTS (UNNadia roan) FAR 25.1301(a)(bXc) - FAA 02:C;IVI. CERTIFICATION - undue =Ahern vested by derecton 04 In Aeroflot:2kt and In aoardanc0 volt cannons and Inialions of aPPIATININI under Part 183 of the Federal Aeration Reptaattorts data listed above and on attached fl ats reambeasel have bean rnalnaleal In accordance PUT estabfishod procedures and found to comp/yeah appicalab nequIromenta of Om Federal Aseadon RoISITIona. -- is Recotrunond approval or these data I Tln 0 Approve those data SIGNATU OF DESIGN*, REPRESENTATIVE(S) DE IS/ATM NIAABERSTSI cussincsnotem John F DERT-710198-SW Systems 8 Equipment Avionics 8 EJectical 8110-3 JFN-06-074 Si (1140) SUPERSEDES PREVIOUS ECtnow ILICTROICITORISTT(7441 SDNY_GM_02753824 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240746 EFTA01326339 SDNY_GM_02753825 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240747 EFTA01326340 Form Approved 0 CM No 21204320 MAJOR REPAIR AND ALTERATION us Oemarvera For FAA Use Only Twice:In (Airframe, Powerplant, Propeller, or Appliance) Office Idenbfication Wet 'Waren Mbredetrelee talRUCTIONS. Rh Or type al entries See FAR 43.9. FAR 43 Appendix B. and AC 43 9.1 (or subsequent revelon thereof) for instrucoons and deposition of this form. The report is required by law (49 U.S C. 1421). Facture to report can result a girl penalty not to exceed 51.000 for *Eh such violation (Section 901 Federal Aviation Act of 1958). Make . i MOON GV 1. Aircraft • Sere) No. NabOnalty. and Revocation Mark 1085 N677RP ' Name (As shown on registration caratiCete) Address (As shawl on regisfralion car-tektite) TRT LEASING INC 515 N FLAGLER DR STE P400 t. Owner NEST PALM BEACH FL 33401-4320 3. For FAA Use 0* The alteration identified herin has been reviewed and found to be complete with apPropriate DER approvals All aspects of the alterations) are compatible and eligible for use on the above described aircraft, subiect to conformity inspection by a person authorized in FAR 43.7. . . . • David Kelm r4C=E , \le..1—.. ti nt. —WOOL go—, Li^ '7.s'7 i .• 4. Unit Identification s. Type Ui'S SAM. Moist Sena! No. Repair flotation AIRFRAME (As dasenterf in Ilsm 1 above) X POWERFLANT PROPELLEFt Type APPLWCE Manufacturer a. Conformity Statement 1 ••: A Agency's Nays and AddretS B. Kind of Agency C Certrficale No. CAPITAL AVIATION, INC. us. Commend methane • ! 5500 PHILLIP J. RHOADES sconigin Genital*. ma. so X9114092), FIGR 2, WILEY POST AIRPORT X can/kited Repair Staten BETHANY OK 73008 Marulacturer D. 'Wei trial the Wet anew amnion nude to the men *Wee n diem 4 reeve ace deicnbed en the reverse or attachment; hereto have bee made in atcoleance well the reouiemerts of Pane of ma us Fears Avia6On Rociations end that We Syronaanutio0 ham, and canal to Ma OW Of nag linOwaidd0 Dale Signature of Authorized d -009- 2a97 MICHAEL S. ROPER ' 7. Approval for Return To Service P rsuant to the authority given persons spoofed below. the raid Identified in lair 4 was i n the manner preSCribed by the Administrator of the Federal Aviation Administration and et El APFROW-0 O FAA Flt. Standards Other (Specify) Inspector Manufacturer Inspection Authorization BY FAA Designee Person Approved by Transpart X Repair Station Canada Airworthiness Group, Date of Approval or %alba • - Certificate or . --Spam of Authorizes - ftW DengristIon No. . DV-DI-2.407 FAA Fenn 337 ilzse X91R0112Y MIGHAELS. ROPER earinnevensie(Mee SDNYGA402753826 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240748 EFTA01326341 Week completed for IN677RPI on • !MICE Weight and balance or operating imitabon changes shag be elected Ingle aPliaoPtige morn Mad. An annum must be compatible wan an previous a/wagons to assure comMued conlormity went* appicalste d..wrdwress requirements 8. Descnpuon ot Work Accomplished GULFSTREAM G-IV N6'77FtP S/N 1085 W/O 1658 ANTENNA I. Removed existing Antenna and installed COMANT Antenna CI 420-I , s/n 162608 using existing doubler at F.S.I93C.00+9 as per Strong Aero Engineering drawing N677RP-011107-I, Rev. N/C dated 01-1I-2007. 2. Installed Sensor Systems, Inc. Iridium/GPS Antenna 567-1575-165, s/n 1333 F.S.193C.00+9 as per Strong Aero Engineering drawing N677RP-011107-2, Rev. N/C dated 01-11-2007. Data approved by Structures (A I, A4, PI, P4) DERT605818NM on FAA Form 8110-3 dated 02.19-2007. Weighed aircraft, computed new C.G. and entered in aircraft records. Log Book Entry made. CONTINUED AIRWORTHINESS - Monitor item(s) for condition. If item(s) become damaged, replace with same make and model. If make / model is not available, notify the local FSDO of pan replacement. Refer item(s) to installer or any qualified service center for repair or replacement. Items to be inspected in conjunction with operators approved inspection program to insure secutity, overall condition and proper operation as is required. CND W Additional sheets /me Attached SDNY_GM_02753827 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240749 EFTA01326342 V.S. DEPARTMENT OF TRANSPORTATION DATE 02/19/07 FEDERAL AVIATION AtmivIsTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE cairpiene,4.410. NAME OF APPLICANT Hellorpter.etc.) GULFSTREAM G - IV CAPTIAL AVIONICS, AIRPL ANE INC. LIST or DATA IDENTIFICATION TITLE DRAWING REFS: N677RP -011107 - 1 "ANTENNA REMOVAL AND COMANT CI 420 - 1 ANTENNA REV N/C REPLACEMENT" 01/11/07 N677RP -011107 -2 "S67-1575-165 IRIDIUM/DATA DUAL CHANNEL ANTENNA REV N/C DOUBLER DESIGN & INSTALLATION" 01/11/07 APPROVAL IS FOR ONE AIRCRAFT; S/N 1085, T/N N677RP Notes: •. This approval'is for engineering design data only and is not an installation approval. It indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and subparagraph listed below as 'APPLICABLE REQUIREMENTS'. (Compliance with additional regulations not listed here may be required). PURPOSE OF DATA IN SUPPORT OF A MAJOR ALTERATION TO SHOW COMPLIANCE WITH THE FOLLOWING REGULATIONS APPLICABLE REQUIREMENTS (List specific sections) CFR 14 FAR Part 25.301(a), Amdt 25-23; .303, Amdt 25 - 23; .305(a), Amdt 25 - 86; .307(a), Amdt 25 - 72; .365(a) (b)(c), Amdt 25-87; .601, Amdt 25-0; .603(a), Amdt 25-46; .605(a), Amdt 25-46; .607(a), Amdt 25-23; .609(a), Amdt 25-0; .611, Amdt 25 - 23; .613(a) -(d), Amdt 25-72; .625(a), Amdt 25-72 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Part 181 of the Federal Aviation Regulations, data listed above and on attached sheets numbered N/A have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. El Recommend approval of these data I oditi Therefore Pg Approve these data SIGNATVREISIOF DESIGNATED ENGINEERING RE RESENTATIVE(S) DESIGNATION NOKBERSIS) CLASSIFICATION(SI TREVOR J. STRONQ--- --\ DERT605818NM STRUCTURES(A1,A4,P1,P4) I /U\ VVVicjkTAA - _ ... ...... ( - Clt EDITION GPO 901-41 SDNY_GM_02753828 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA (X)240750 EFTA01326343 SDNY_GM_02753829 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240751 EFTA01326344 Fern Approved 0 0M3 No. 2120-0020 MAJOR REPAIR AND ALTERATION US Overt* For FAA Use Only Crimea , (Airframe, Powerplant, Propeller, or Appliance) Office Identification rens Ann Adriteiblike INSTRUCTIONS: Print or type as entries. See FAR 43.9, FAR 43 Appends B. arid AC 43.9,1 (or subsequent revision thereof) for instructions and deposition of this lone. Ties report is required by law (49 US.C. 1421). Failure to report can resul ti civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model GULFSTREAM G-IM 1. Aircraft Sew No. Nellonality and Registration Mark 1085 MSTIRP /tare (As shown on registrabon carioca) Address //As shown al registration certificate) TRT LEASING INC S15 N FLAMER DR STE P400 2. Owner WEST PALM BEACHFL 33401-4320 , . 3. For FAA Use Only The alteration identified henn has been reviewed and found to be complete with appropriate DER approvals. All aspects of the alteration(S) are compatible and eligible for use on tie above described aircraft. autism to conformity inspection by a person authorized in FAR 43.7. David Kelroc. L ...... _.-41./-...- °Art "II tool <ma LI - I. 0 C) 4. Unit Identification S. Type UM Male • Model Sorel No Repar ArtefMien -: AIRFRWE (As descntial in Muir 1above) X POAERRANT FRCPEMBI Type APPUNCE Manufaciunsi i ALConferseft7 Statement A. Agency's Name and Address ' B. land of Agency C. Certificate No. CAPITAL AVIATION, INC. U.S. Conine:awe nine 5500 PHIUJR J. RHOADES Forpn CeillfiCalled Marthiak X91R0921. MGR. 2, ViALEY POST AIRPORT X Ce(VIICat•O Repair Staten BETHANY. OK 73008 lannewer Ct I reaW Nai no ran ana anon nen be wtissi dented n ilet 4 roam ens decreed on te reverse a allaclinerds lent Nee been made in llosedance wale rte neurone 08 Pen 43 of to U.S. Fein ANSI*" Repeat» end swab mlorrreeco tinned en Sid and b as bit or rrir Wainge. Date Signature of Authorized I g MICHAEL S ROPER 63 / a 2a 77 7. Approval for Return To Service Pursuant to the authority given persons specified below, the and identified in ism 4 was i it manner by the Administrator of the Federal Aviation Admeetration acid's El APPROVED O FAA Rt. Oiler (SPecify) InspectorS1Hi0art1a Manufacturer Inspection Authorization, BY FAA Designee Person Approved by Transom X Repair Station Canada Airworthiness Group • Dale of Approval or Reterzlon Cerlecate or 1 -Span of Authorized Designation No. . X91R092Y MICHAEL S. ROPER A l le4, - FAA Form 337nuo Elseetnevessewesee SDNYGlvi 02753830 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240752 EFTA01326345 .• Walt completed Ice IN677NPI on NOTICE Weill and balance or operating lordaton changes shell be ertered In the appoprerce aircraft record. An Aeration must be ccenpeatile *eh al premotrs Maria.* to assire continued eat/amity vah an *pebble anat*iess imitarements. & Desolation cr Work AocomPashed GIJLFSTREAM G-IV N677RP S/N 1085 W/O 1658 INTERIOR / CABIN MODS, I. Original Interior Configuration and New Interior Configuration are as shown on Capital Aviation, Inc. drawing 07-10018, Rev. URI dated,03-05-2007. (1 Sheet) 2. Modified existing L/H Fwd.Closet as per Capital Aviation, Inc. drawing 07-10019 Rev. 1/R dated 03-05.2007. (2 Sheets) 3. Installed R../14 Fwd. Crew Lay as per Capital Aviation, Inc. drawing 07-10020 Rev. I/R dated 03- 05-2007. (7 Sheets) 4. Installed Windowline as per Capital Aviation, Inc. drawing 07-10021 Rev: I/R dated 03-05-2007. (2 sheets) 5. Installed Credenza as per Capital Aviation, Inc. drawing 07-10023 Rev: I/R dated 03-05-2007. (10 Sheets). 6. Installed SubWoofer Cable( to existing Ft/H AFT Bulkhead as per Capital Aviation, Inc.drawing 07-10024 Rev: I/R dated 03-05-2007. (I Sheet) 7. Modified L/H and R/H Galley as per Capital Aviation Inc. drawing 07-10025 Rev: I/R dated 03-05- 2007. (5 Sheets) • 8. Modified existig Vanity as per Capital Aviation Inc, drawing 07.10026 Rev: I/R dated 03.05-2007. (3 Sheets). 9. Installed 17" Monitor at F.S. 297.0 as per Capital Aviation Inc, drawing 07-10027 Rev: I/R dated 03-05.2007. ( 4 Sheets ). 10. Installed Aircell FUH at FS. 232.5 as per Capitall Aviation Inc, drawing 07-10028 Rev. I/R dated 03-05-2007. ( 4 Sheets ). II. Installed Misc. Equipment as per Capital Aviation Inc, drawing 07-10029 Rev: I/R dated 03-05- 2007. ( 4 Sheets ). Data approved by Structural DERT-710098-SW, on FAA Form 8110-3, NSE-07-004 dated 04-02- 2007. CONTINUED AIRWORTHINESS - Monitor item(s) for condition. If ken(s) becinneydamagel, • replace with same make and model. If make / model is not available, notify the local FSDO of part replacement. Refer item(s) to installer or any qualified service center for repair or replacement. Items to be inspected in conjunction with operators approved inspection program to insure secutity, overall condition and proper operation as is required. Weighed Aircraft computed new C.G. and entered in Aircraft records. Log Book Entry made. ()Ciao:Nome Sheets Aro Attached SDNY_GM_02753831 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240753 EFTA01326346 04/02/2007 ION 1:18 FAA %003/004 US. OELIMMENT OF TRANSPORTATION DATE FEDERAL AVIATIONADMINISTRATION 4-2-07 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MARE MOM Na TYPE (Mast Rad H•OcrS etc) MALE OF APPLICANT Gulfstream Aerospace GIV Airplane Capital Aviation Inc. Corporation LIST OF DATA IDENIVICATON 771E Dwg. No 07-10018 INTERIOR INSTALLATION Rev. VR. dtd 3-6-07 Sheet 1 Dwg. No. 07-10019 LH FWD CLOSET MOD Rev. UR, dtd 3-5-07 Sheets 1 & 2 Dwg. No. 07-10020 RH FWD CREW LAV INSTALL Rev. UR, dtd 3-5-07 Sheets 1Vim 7 Dwg. Na 07-10021 WINDOWLINE INSTALL Rev. UR, dtd 3-5-07 Sheets 18 2 Dwg. No. 07-10023 CREDENZA INSTALL Rev. UR. dtd 3-6-07 Sheets 1 thrU 10 Dwg. No. 07-10024 SURWOOFER CABINET INSTALL Rev. l/R. Md 3-5-07 Sheet 1 NOTES: 1. This FAA approval is for structural aspects of the data only. Additional approvals may be required for other aspects of the data. 2. The inspection of the installation is not being approved 3. The approval Is in support of the noted modet. S/N 1085 only. SE-07-004 Sheet 1 of 2 PURPOSE OF DATA To provide FAA Approved data in support of a Form 337 approval APDI kum F REQUIREMENTS as ip allow) FAR 25.301, 25.303, 25.305, 25.307, 25.603, 25.605, 25.607, 25.813, 25.789(a) at Amendment 25-56 CEP:MACAU:IN . under sumo* vetted by deeded *lima Ammeurator and Ln =meant* wan ~worn WIC1 bIlibitiOrit of appointment urger Pmt 183 of to Fedora anew: Ra- et ans, data Wed above and on aliened crmot nvenearm )0C4 have been manned in =Wan=Ni estiahAled piIXtd4), C'S 411C found to wmpty vall appleatie nattdementa of Ite Federal AvishOn ~In , 0 Recommend approval of them data 4iNekTromeiore 2 Approve thaw data 51 ATI NA 0j te t'SF ' Thee , D S NATO USEFLS(S) CLASSIFiCAT/ON(S) Richard W. Southard PERT-710241-SW Structures FAA Fonm MIMS (I JO) SUPERSEDES PREVIOUS EPROM ELECTRONIC FM:m*3 (790, SDNYGlvl02753832 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0O240754 EFTA01326347 SDNY_GM_02753833 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240755 EFTA01326348 04/02/2007 MON 1;19 FAA ?004/004 OE DEPARTMENT OF IPANSPORTA11014 DATE FEDERAL AVIATION ACGINISTRATION 4-2-07 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT QR AIRCRAFT COMPONENT IDENTFIC•TION NAPE la0DEL NO. TYPE plep/ony RM. Nymootte. No NAME OF APPLICANT Gulfstream Aerospace GIV Airplane Capdal Aviation Inc. CorPOretite UST Or DATA IDENTIRCANON 1TRE Dwg. No 07-10025 Lti AND RH GALLEY MOD Rev. UR. dtd 3-6-07 Sheets 1 thy 5 Dwg. No. 07-10026 VANITY MOD Rev. UR, dtd 3-5-07 Sheets 1 dint 3 Dwg. No. 07-10027 MONITOR INSTALL Rev. UR, dtd 34-07 Sheets 1 Wm 4 Dwg. No. 07-10028 MRCS LL INSTALL Rev. UR, did 3447 Sheets 1 that 4 Dwg. No. 07-10029 MSC EQUIPMENT INSTALL Rev. UR, dtd 3-5-07 Sheets 1 thru 4 NOTES: 1. This FAA approval is for structural aspects of the data only Additional approvals may be required for other aspects of the data. 2 The inspection of the installation is not being approved 3. The approval's in support of the noted model, SIN 1085 only. SE-W-004 Sheet 2 of 2 PURPOIE OF DATA To provide FAA Approved data in support d a Form 337 approval APPUCARE REEMMEMENTS DM weft media* FAR 25.301, 25.303, 25.305, 25.307, 25.603, 25.605, 25.607, 25.613, 25.789(a) at Amendment 25-56 CERTIFICATION - Vnde, mulhonly veered by ciontron of the Adrnitingefter and in •Coonlenon sal andRiCe% awl Imitaffn of appointment Under PM 163 of !In rt...ten, AvtabOn Regt10130r4, Outs rn.ted *Love and On lanChed nen numbered vex hive boon Wit s:4 in accordance w0 MtabezIllee procedures end found to cotnuty DAM meta* Itiqukeelenb of the Federal MAST Repulterte. 0Recomenand approval of ThOs. data I ?hat) Throb, MAMMA. Mara dab IA TWatEMIORlar artFASENTNINE161 OESIGNATMet NIPMERNS) I CIASWICATIONM1 ... .. Richard W. Southard DERT-710241-SW Structures FM Foam 111104 (ii -TO) SUPERSEDES PREMOUS EOMON ELECTROMC FORMAT (7-00) SDNY_GM_02753834 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240756 EFTA01326349 SDNY GM 02753835 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240757 EFTA01326350 OramPOPrOse CO MAJOR REPAIR AND ALTERATION M)NO 21204030 ,.......... U Nyed •Aae. (Airframe, Powerplant, Propeller, or Appliance) let FAA se ORM ........ CfAce kftradien Mare ,NSTRUCTIONS Prot et hoe elPena. See FAR 43 E. MR 43 APP•Ma B. end AC 43 91 crehteepant mimeo teed) S3r Ma eispommm cf um In yhe mon A repuppy oy /•• l49 U SC 1421) Felon anon cmrowan 4 ow yemMY AM to Ammo, SICCO re, Yeti AAA Valallon (Seam or Irvin Paint Am mom Make atom Gultstream GIV 1. Aircraft Sem, No 144nonaly end Rapflebon Mot 1085 N423TT Nwrm (Al Mean OfrAYAStraVari ON/Ecole) Address (As Moen oa mplifilibbn CMIFCMO) Owe 515 N Flag*/ Or STE P400 2 TRT Leasing West Palm Beach, FL 334014320 3. For FAA Um Mk 4. UM 109neficeeon 4 Type UM MOP Mcdel 34041He Rea Miriam X AIRFRAME (As describedIn Hem 1 above) PCP, t RP. ANT PROPELLER lice APPLIANCE lAndscosee 4 ConfomMy Meepre4 A Apncys NY* and MOAN B Kid.:i Agar/ C. Cenficee. No. CE Avionics, Inc. us. CeAlPedNecrenK 0E4R411M 2789 Fightllne Avenue Famign Called Mithant. Sanford, FL 32773 X CP1E•A Roper Saban Monawaset 0 I oweI y tat OM Wee Reba MielefaCa made to to unAls)MInfloclhells atom end lerscrtal on V* mem et enschmens MMO hen been cede in eeeerdame delMe repatments of PM 43 44 the U.9. F eat& Avalon Regalscrs rats IPA • lortsebOi twililhed Bain le sme and coma to Iheeeel elPm WeeMelie Ca &Oran cfluilwreed tilmduel . d oe May 22, 2007 ./: Michael E. Hughes • 7. approval for Rohn to Swam MW MM•..fley ran pram spew beCre Si.MM IderMsd Si am • pas mewled n we warner welarblatfl e• ACINNIVOlot of me Few,. Anew Armen.= et le El APPROVED 0 REJECTED FAA Ft StanPirdt Minaarer inspomanhartamen salw Mayan aapaca. BY FM Dowee X Reeler NOM Pence 90,0•4 TV TremPM Cana Anyonlemis OM. OOP aI Appian' or RESPIOn Cat mem ot st We 4/ Iatreasecilnilatilw)us tioitc . a / s ir d i$ 0.i ...... May 22, 2007 EsPranon He 0E4R411M Michael E. NuoMs amFenn MY mat) SONY GM_02753838 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240758 EFTA01326351 NOTICE Weight and balance or operating limitation changes shall be enteredin the apProOnate aircraft record. An alteration must be compatible with allprevious itterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished Of more space Is required attach additional sheets. Identify with aircraft nationality and registration mark and date work completed) Removed Collins Part Number 822.9210-008 TDR-94D Mode S Diversity Transponders Serial Numbers 2221 and 3672 and Installed factory modified per Service Bulletin 504 to Part Number 822-9210-308 (Enhanced Surveillance) Serial Numbers ICBM and 4J2W. Interfaced the TDR.940 to the Number 1 and Number 2 Honeywell HGT1075AE03 Inertial Reference Systems and made additional voting changes per CE Avionics, Inc. Drawing Number 5893B-t. Revision UR dated March 22, 2007 (Approved on FAA Form 8110-3 dated May 21, 2007 by Leslie S Roblin. DERT-510335-CE - Systems & Equ talent). The installation was made In ccapitance with Gulfstream IV Arming Diagram Manual Revision 52, dated December 31. 2008, Chapter 20. Sections 20-24-00.20.25-07, 20-28-00 and 20-28-09; Chapter 34, Section 34.02-04; and in compliance with FAR 25.1301, 25.1309 and 25.1431. END- El Mani S , l InAllatred (1 Page) US.OPD:1989-0653.171 SDNY_GM_02753837 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240759 EFTA01326352 Armament. FAA Fr 337 Dated May 22, 2007, N4237T.Gulfstream 04V, Mu 1085. Sheet I of DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS May 21, 2007 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO TYPE (Airplane. Rano. Helicopes. sac) . NAME OF APPLICANT CE Avionics, Inc. Gulfstrcam Aerospace Corp. G-IV Airplane Sanford, Fl. LIST OF DATA IDENTIFICATION TITLE 5893B-1, Rev IR, dated 5.21.07 Additional Wiring for Transponder Mode S Surveillance END Notes: I) The electrical gyms only of the above listed dm at approved Main Thissprat is for ensineerns design data only. It ndicaes die dna liseclabove romances retie= only Min the regulations specified by wrap* std subparagraph tided tebw as- Applicable Requirements". 2) Cornplimce vrith addiionalreaula ins Inc listed my to required This trot does not confide FAA approvalorall the coalman's dm nccessry be subset inbn of =Siam to necessary requirements br Meat Se Mention. The a iia unit area s are esst Related in this 'preys]. 3) After the Akar an, thesimnel must be let urned to service by FAAmawcod pained PURPOSE OF DATA: Design approval in support of major attention, installation of Elementary & Advanced ATC Surveillance (Flight ID) Transponder System on Gulfstrearn 0-IVSerics aircraft, serial number 1085, registration no. N42317: Systems & Equipment Design Approval Only. APPLICABLE REQUIREMENTS of Title 14 CFR (List specific sections) FAR 25.869 (aX4) FAR 25.1357 (aXc) FAR 25.1301 (aXbXe)(d) FAR 25.1381 (exb) FAR 25.1353 (bXd) CERTIFICATION - u........ ....t. Sc.. a (................ ,we wawa ass amass Sapp:non aim Psn in sr au F.S.. Amara RAMakm. Pm has Son inlIn.ult. that auiribet•J MOM 'Wigton awash. iit•Odain sub enialAwd pectin end kmad is WW1with illpialis 'Kris.. MM Nana A"... P.O.W. O Recommend eppoval of Mn data I (We) llecrefore eil Amore these data SIGNATUREM OF DESIGNAT ENG ERI RE E REM DESIGNATION NUMBER(S) CLASSIFICATIONIS) Leslie S. Roblin • DERT-510335-CE Systems & Equipment FAA Form 8110-3 (I140)SUPERSEDES PREVIOUS EDITION (0 V Rob alt3 doe) 010509 GPO 901113 SDNY_GM_02753838 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240760 EFTA01326353 SDNY_GM_027.839 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240761 EFTA01326354 *Waved OMBFOrm 0 MAJOR REPAIR AND ALTERATION MO 21204020 tilift......0 Twear For FM 13•4 Over las mum. (Airframe, Powerplant, Propeller, or Appliance) sans. Mob lanfloatien INSTRUCTIONS Rt4 a tope d eines See FAR 419. FAR434cent O. W AC 419.1 a eteeepril melon Owed) Kw ingevakee and dfloslion et en Van Pio neon i~e3 le lea (H1.1C 021) Fein ea repon one* m 4 del penile nab ease III.0)D low each es. *Ake (Seaers901 F40401Aeelen Ao 1959) PAW, Model GULFSTREAM G-N, s. myna sols Ma Petbraff W Rama,Mot 1085 N42317 Nun fAr row on ,.walla,colikeel Amer (A, shown eNoever. oNellceON 1 Omer TRT LEASING INC 515N RACIER DR SUITE P400 WEST PALM BEACH. FL 334014320 3. FeeDA Use Only 4. UMkkalikallen L TIT.* UM IIIS Rea Solid No Ream Metsbat 0 9 AIRFRANE As dissafIndIn awn 1 above El 0 PONERKANT 0 0 INIDPELLER Type 0 M OPPLINCE blenulwitror 0 0 S. Coreenrely Sleernerd A PreisNee in4Addreee S. Fib d AireY C. Carthal• ft ALAN D. REDMON u S Cedes!Mocha 3107552 MP 200 REDMON RIDGE Fasin Ceded Moen DAWSONVILLE, GA 30534 tame two.Han wassAist D I <flyIt WO ewe flee eleraeco ale 43 we eat)Itilelled Mabee tore ere Suited on Irenema ellienneeT hereto hen been as n ecoortlenceIse re •ellterthiels ol Pe 43 cf a U S FlideilMeson Repealer* eelera seconelon WOW ninon a no incl one le Se bog deny Ircaleapi 0414 Syrian of ()drs. 4 APRIL 2007 / ..---...-'•-----."' 7. for ex Antal to to alliOnty Oven moons aged billo,the int MM.,in is 4 wee areplosci in toe worm preacited by IN Adetrailnkt 011/10 rowel MA200)Admedereen Ind a el APPROVED 0 REJECTED FMFS StenderdS O lAwascluw 1 Irabun AW:notion (Spay) ri '—' Inspecior BY O ;SA 000trose O Reps Slam Rep New.440fteed IN Treaty Cale Nreetileito Creep \ Dal* *I Approve/ or Reran °Macs* a Snows s:zr 4 APRIL 2007 Oelepriece NO 3107562 MAN D. /,4_,.-- /) \ %--....." .. _ SDNY_GM_02753840 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240762 EFTA01326355 NOTICE Weight and belance oroperating limitation changes shall be entered in the apProPrIste astiallredard An einem^ must be requirements compabble with all previous alterations to assure continued conlommy with the applicable airworthiness 8. Description of Work Accomplished (0N more Spies is required, at additional sheets. Identify with onsralt nabonakty and registration mark and date work completed) AIRCRAFT MODIFIED: N42377 G-IV SS 1055 4 APRIL 2007 DUAL TRANSPONDERS AND 1. THE FOLLOWING WORK WAS ACCOMPLISHED BY CAPITOL AVIATION SERVICES: REMOVED UPGRADED WITH NEW FUGHT ID UNITS. DUAL TDR940 2. REMOVED DUAL COLONS TOR-94 TRANSPONDERS AM) RTU-4210 CONTROL HEADS AND INSTALLED SA 267 8 Se 1176 PER TRANSPONDERS P/N 622-9210-005 SI 2221 8. S8 3872 WITH CONTROL HEADS RTU-4210 P/N 822-0838-015 COLLINS ROCKWELL COLLINS STC 01142W-0 AND IS SUPPLEMENTED WITH ENHANCED SURVEILLANCE USING ROCKWELL SIL-1.04 ALONG WITH DRAWINGS NO CMM P/N 523-0778502 REV 3 DATED 10 NOV 2008 AND SERVICE INFOR1MT1ON LETTER CC-040407 REV IR APPROVED BYDER ANDREW K. ANDERSON ON FM FORM 8110-3 DATED 4 APRIL 07. SUPPLEMENTARY THE INSTALLED MODES SYSTEM SATISFIES THE DATA REQUIREMENTS OF ICAO DOC 7030/4. REGIONAL PROCEDURES FOR SSR MODES ENHANCED SURVEILLANCE IN DESIGNATED EUROPEAN AIRSPACE. 523-0773070- 3. CONTROL OPERATION INFO.: REFER TO ROCKWELL COLLINS PROUNE II PILOTS GUIDE DOCUMENT NUMBER 004117, DATED JULY 14, 1993, OR LATER APPROVED REVISION. 4. SERVICE INFORMATION: REFER TO COLUNS CMM REFERENCED ABOVE. 5. MAINTENANCE INSTRUCTIONS: REFER TO COLLINS CANA REFERENCED ABOVE. 6. TROUBLESHOOT INFORMATION: REFER TO COLUNS CMM REFERENCED ABOVE. 7. REMOVAL ANO REPLACEMENT: REFER TO COLLINS CMOS REFERENCED ABOVE. 8. DIAGRAMS: N/A 9. SPECIAL INSPECTION REQUIREMENTS: NONE 10. APPLICATION OF PROTECTIVE COATINGS: WA 11. DATA NO HARDWARE WAS REQUIRED. 12. UST OF SPECIAL TOOLS: NONE 13. FOR COMMUTER CATEGORY AIRCRAFT: N/A 14. RECOMMENDED OVERHAUL PERIODS: NO ADDITIONAL LIMITATIONS. 15. AIRWORTHINESS UMITATIONS: NONE AT THIS TIME. -END_A} FORM 337 16. REVISIONS: A LETTER WILL BE SUBMITTED TO THE LOCAL FSDO WITH A COPY OF THE REVISED FM 0 AddilcrelfropS An Allmo's, U.S.OP0:1989-0463-171 SDNY_GM_02753841 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240763 EFTA01326356 Apr 04 07 09:32a Andrew Anderson 770-387-0701 P• 1 U S. OEPARASENT OF TRANSPONTAIION DATE FEDERAL AvallON Aramosnunon Apn1-04-2007 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MANE MODEL NO. 'TYPE tithatm Radm fralitaba et) MANE Of APPUCAXT Gulfstream G-IV Airplane Private Consultant to ATS INC LIST OF DATA MENDFICATION 'RAE CC-040407 Flight VD Installation (Dated 04-04-2007 Rev VR) PURPOSE OF DATA In support of major modification for SIN 1085 ONLY. APPUCABLE RECIUREMEXTS dal mice smut 25.1309 (a)(b)(c)(dXeXg) 25.1351 (a) 25.1357 (aXt4(6)(6)(e)(9) CERTIFICATION - under authal(y el by dlitarti of the AcInnatrafor and In womb= NM oamtdions end lialittorm et OppoirdrUtif Latta Part 103 of N. Ficleral Mallon ReOutrons. au Wed alien and on attached staters numbered r arta hare been auatted In accordance's* astabGalyarl doceduras NM found to =oh Idth alIoNable nutternets of Me Foetal Aviatch Repubsbars. 0 Recommits:1 approval amen data Ipil e Thete in s) (83 Approve Sew data S OF TED EWXNEEFUN(3 RF_PRESERTATNE(5) IDESIGNIIIM7 FliFISERAS) CLASSFrATONA DE RT-510004-CE System & Equipment 4n t. FliaM Analyst Andrew7 Anderson FM Form 11104 (t1.70) SUPERSEDES PREVIOUS ECITION ELECTRONIC FORMAT (7.03) SDNY_GM_02753842 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240764 EFTA01326357 SDNY GM 02753843 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240765 EFTA01326358 fr Fowl Appeased Elicirmt robesMats 0 , L. CSOM.2111)403) 11/30107? : esenrani • MAJOR REPAIR AND ALTERATION • Mc FAA um den tillrannislai ' af . (AI:frame. posemplvd, Propeller. or Appliance) ... .. Alniblillelfaa i -. .‘ INSTRUCTIONS: Print a type all greet Sao Me 14 CFR 4µa. Part 43 Appendix B. and At 43.94 (or etiongse mann thereon for irenctorts end Minabon of It form. Thee report le wined by km (49 U.B.C. .44701) Fans to report cannot. hada prey to tech much Nolen. (49 US.C. §48301(a)) ova scrim No. .' "le-tY and jigiets161:111-441 N677RP i . 1085 I. Aircraft make sea ilothi Gulfsueam G-IV Nana (Ai Man cn reglanden cerillon) Arkbers (/4 Moan on regkorattn oartlAcate) raini,15 N Eisele: Dr. Suite P400 r • • . 2. Owner TRT Leasing Inc. ay • .West Palm Beach are as 33410-4320 ea r USA •• S.PerliAlle UmOnly .. 4. r/Ps 6. Unit Identification . Repot Mallon UM Araks Model Sinai No. IN AIRFRAME . - - (Ait assambeI Magi I above) 0 .. . _. ... . . .. . . . O • ... - . O - . : pRpp,....,t PONSMUJIT RECEIVED .... . . . . • ' ... ---• • •••- - • . • - - .- 'type • El APPLIANCE Lardocaser ASW - FSDO OK : 4 Conformity Ittornort A. Agency's Name and Address B. Ktnd a Agency id. Associated Acro.Sennice u. a. unkaaid Mechanic 1 tranuracon nom PO Box 1310 rarely Carercateci Mechanic C. Certdkate No. ow Oklahoma City an OK ..x Gellman Rena Eamon D, 73008 o w., USA caiiii Enno,.. . —es Orartaten SSWR I 86K D. I astly !het the repair anon alteration made to the unit e) kientleed in Item 6 above aid deacrIbed on the reverse or attachrrants Anti Sive boon nude in amo-danco rah the requirements of Part 43 of the US. Fenn Aviation Regulations and that the inbrmaton fantod hareln le Ina and carob to the tint of my Imosiedge. Extended range hal Sisnahreibets of Authated Incilvklual d i e Awce/A-re.,7> 4. a -4, _COL V 'c, ( per 14CFR Pert 43 E App. El 7.-...g12.- Y. Et/eA r )ty - 1,--- 71,- -;71 7 .77 7. Ape rand for Ran to Site Pursuant to the *Wintry given persona snarled baba. the unk identified in /tern 5 was Impeded h the manner proscribed by the Adenbiletretor of the Federal Antal Adman:atm midis Approved 0 0 Reflected FAA FitStendards - .- Panora ACORMS MiCillibtien -. . . Ilanufachrer Mentenance Organization Ommilmeni a/ Imielpiel illipeCitt ._ . . .. _ . ._ . _ . Other (Specify) - - • FAA Dilignse Repea le r y irssectial Autortzslon Certinte a . 901inglikillafAtentledtralniduel , .. , 7.; ., ;;Z:‘,.. . . I/ . .. . i; di4 - . " " . Otaignatkin M.. tr liA2- 2 3 14‘iel --retN aidte.AOX -' ( o3/e37260-7) SDNYGM02753844 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240766 EFTA01326359 NOTICE • • Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be Compatible with all previous alterations to assure continued confonnitysvith the applicable airworthiness requirements. 8. Description of Work Accomplished alman space fa reyndral. mach additional sheets. identify with aircraft nationality and registration Mark and date work coatpkier1 Aircraft Make GulfAreom.. . Model GIV .Serial Pluinber1085 Reiiiiradoe Nia7RP Date03/00007 . , . . Installed Gulfitream'ingineefecfrepairs at fiVe lOattiOns on ilie upper akin of the floor panels in the cabin area. Reference.thecntlfatteant $E05005902 Rev. IR drawing: : All doubler material is 2024-T3 0.050 thick. All replacement core material is 5.7-3/16-20N 5052. All bonds were made using EA9309.3NA adhesive. Drawing INSTL No. Doubler Diameter F.S. R.B.L. L.B.L.. -1 5.60 489.43 28.22 -3 6.40 476.45 28.57 -5 5.90 . 475.66 16.75 -7 6.70 482.41 28.78 -9 6.90 481.19 16.32 This repair was done in accordance with the GulfstreamSE05005902 Rev. IR drawing and the Gulfstream engineering 8110-3 form, Identification SE40001085 Rev. B, dated 03/07/2007. There is no change to the aircraft Weight and Balance or Equipment List. . For Continued Airworthiness reference the aircraft manufacturer's applicable data. With respect to the work referenced in the Associated Aero Service work order number 4635, this aircraft has been found safe for return to service. END El Additional Sheets Arc Attached S 0 P01990.761.751 SDNY_GM_02 753845 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240767 EFTA01326360 TECHOP STRUC TLIRE '3 PAGE NS 03/12/2007 69:22 25519 0 AG' US. DEPARTMENT OP TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION 03 / /1 19 6 -Ce .3--- STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS ' 'AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION - . MAKE MODEL NO. TYPE: tabus. rues aseresec at -NAME OF APPLICANT . .., .• - .. - . .. .. ..• .. i — . • . .. . ..- .- Gulfstieam 0-tV .-Airplane .. Culfetreani Agit:aspect Conioration • S/N LOSS LIST OF DATA IDENTIFICATION TITLE SE40001085 TOP DRAWING - REPAIR/MODIFICATION, REV B G-IV S/N 1085 --______ --- END OF DATA ------- NOTE: The structural aspects only of the above listed data are approved herein. This approval is only for the Engineering design data and is not installation data. .., • : ' ' • PURPOSE OF DATA • Support major repair for G-IV sin 1085. APPLICABLE REQUIREMENTS (Lin specific sections) FAR 25.601 CERTITICATION - Under authority vested by direction of the Administrator and in accordance with condition and limitations of appointment under Pan I ID of the Federal Aviation Regulations, data listed above and on ached sheets numbered have been examined in accordance with enablishol procedure. and found to comply with applicable requitements oft's< Federal Aviation Regulations. O Recontnattxl approval of these data OWe) Therefore ve these data SIGNATURE(S) OF DESIONA ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) • 1 46 1'44 12 .;-- it. Robert H. Drinnon, Jr. DER Y-51117S-CE Structures FAA Form 8110-3 mane SDNY_GM_02753846 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240768 EFTA01326361 SDNY_GM_02753847 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240769 EFTA01326362 Form Approved 21210020 le MAJOR REPAIR AND ALTERATION OMB No For FAA Use *ray us. owenweili at Tranwartrtol (Airframe, Powerplant, Propeller, or Appliance) Office Idertiticaton FecWsl AA•0on Adesleast-40.n VINN X00 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appal& B, and AC 439-1 (or stbsequerd revision thereof) for inn ions and deposition of this lone. This reports required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty rot to exceed 51.000 for each such violation (Section 931 Federal Aviation Act 1958) mon Gil/stream *al GIV 1. Aircraft Sew tee. 1085 Swear and Rildenten Wen/ N677RP Nwns (As ilwaN on rophbvtlx. Estate) &knee (Ae Moan 0e leeettebee CeteGk) 2. Owner Petersen Aviation 7155 Vatican Ave Van Nuys CA 91406-3917 3. For FM Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As descnbedin item 1above) X POWERPLANT PROPELLER NM APPLIANCE MAMAPCILMIt 6. CoolomitlyStatement A Agency's Name and Address 9. 10nd dAgratcy C. Cerblicale No. Damon Midgette X U.S CsencaltOeortere ASP565174728 4828 Adele Court FralenCereforged mega Woodland Hills. CA 91384 Cerleostes hew satin Menaces D. /certify that the repar and/or alteration made to the urk(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accorda roe with the requirements of Part 43c4 the U.S. Federal Aviation Regulaticns and that the information furnished herein is true and correct to the best of my knowledge. Date 919 Irina ter' /0/23/93 7. Approval for Retum To Service Ptrauard to the a /holey given persons specified below, the wit iderefied in item 4 was inspected in the manner prescribed by the Adminstrator of the Federal Aviation Administration and s a APPROVED RE.ECTED FAA Flt St a rstirds Other (Specify) sr aspect*, Manufacturer X Inspedion Adhestration ca oesion est r iseeron u FM Designee Repair Station Dale clApprowl a Rojection CenkRIA OP SignAlralp Ceelgeollon 1O/13/ 0 3 EA I/Mr /Mr ir FAA Form 337 (12 SDNYGM02753848 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240770 EFTA01326363 SDNY_GM_02753849 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240771 EFTA01326364 NO110E Weight and balance or operating limitation changes shed; be enteredin the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued =O:porgy with the applicable airworthiness requirements. 8. Description of Work Accomplished 01more space is required, each addrtional sheets. (den* vett aircraft nationality end registration mark and date work completed) Reconfigtred cabin interior per STC STO1sssl A See Master Drawing List report SAM -1-02 approved by the FAA on 1021/03. see letter of approval dated 10r20/03 signed by Alan T. Shinseki. Manager, Systems and Equipment Branch. Los Angeles Aircraft Certification Office. ❑ AMIloralmoans Attached FAA Fon337 MN) . US. OP0.1989-0-663-17I SONY_GM_02753850 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240772 EFTA01326365 SDNY_GM_02753851 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240773 EFTA01326366 Q1001 10/21/2003 02:37 FAX 562 827 5210 FAA LAACO 1ST FLA FAX • 3gratebliteeta poreeetta papa:tent of gransportation - eater4,1kEriactires Sthnsististc alier; $uppfnuental Zue dertifirate Afeendes ST01555LA .57 4. c a4ta.dle Syncro Aircraft Interiors, Inc. 7701Woodley /Avenue Van Nays, Ca 91406 , Astizetst.t end .--1/1, axe der agerape d• 4540 04*4A. zdt emearantaaamara 25* 166 co-2 ‘44ro t atray-e$ yrevanionseses emaienyrdeerdirs npierieurearhe 19d Sheet Al2EA Federal Aviation ...98esagsreavo, *Catification basis is set tenth in Type Certificate Data araiTegkacOe .SS.• i f f••••, * Sonde.: Angg Sae: Gulfstream ...a0edet G-1V S/14 1085 in accordance with Syncro &Cyr Cabin interior re-configuration ..§flosvivas, te..fess Siscja r 12, 2003, or later FAA approved revisio n. Master Drawing List SA11-1-02 Rev, NC, dated Octobe modification is considered inadequate for Salnetaaas cadraidaevair Data pertaining to this Serial installation made mthilfstream Cr1V duplication oa other aircraft This approval is limited to the aircraf t. permanent records of the modified Number 1085. A copy of this STC must be included in the entitlerataWi•dtl:, OiD ea, 444 4.444A. 44440arialf delta 4 1.4,4 1 4 tage4e4ak Rea Od• a isornistrays ria.4 a odano4s a+ 44 egaisearammenee Jotassicee 0 Ce Asinsaa(gr.14.v. agessimarnerc744 .rts...c at/Sara'''. August 12, 2003 MTh, isluasse: 0.4 arale .t.paseace.• Arlo• .1.4.iesscace .• October 21, 2003 .53). eravaiw Vo4 -4 4 • Wittaccs) Alan Sbinseki Manager, SYsteass and Equipment, Los Angeles Aircraft Certification Office (rdk) -e ma i••••14rmnartil not MCCAW 3 yea; " SDNY_GM_02753852 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240774 EFTA01326367 SDNY_GM_027.8. SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240775 EFTA01326368 Form Approved OMB No. 2120-0020 MAJOR REPAIR AND ALTERATION tit doormen For FAA Um Only olomnionan (Airframe, Powerplant, Propeller, or Appliance) Office Identification reetermarnmen steam NIN`C F‘.Do INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix (3; and AC 43.9-1(or subsequent revision thereof) for inStruct inn and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed 51.000 for each such violation (Section 901 Federal Aviation Aci of 1950). Make Model GULFSTREAM AEROSPACE CORP. G-IV 1. Aircraft Serial No. Nationality and Registration Mark 1085 N88GA Name (As shown on registration certificate) Address (As shown on registration certificate) BA LEASING & CAPITAL CORP. TWO EMBARCADERO CENTER a. Owner SAN FRANCISCO CA. 94111 3. For FAA Use Only 4. Unit Identification S. Type Unit Make Model Serial No. Repair Alteration AIRFRAME ' (As described in Item I above) xx POWERPLANT PROPELLER Type APPLIANCE Manulacturer 6 Conformity Statement A Agency's Name and Address B. Kind of Agency C. Certificate No. It U.S. Certificated lawNnic LANCE A. MATTESON Forerun Corldicated Mechanic 2407 EAST SHEA BLVD. 04eldicated hew Station AP 1864049 PHOENIX, ARIZONA 85028 Manulacturer 0. I Gerrity that the Waif and/or &Cormier) mad to the un Ifs) identified in item 4 above and described on lhe reverse or attachments hereto have been mule in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of or d Ir‘vid i .— / s 7- ?a K. 7. Approval for Return To Sonic upt. of Maintenance Pursuant to the authority given persons specified below. the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is qii APPROVED 0 REJECTED FAA Flt. Standards Other [Specify) Manufacturer XXvInspection Authorization Inspector BY Person Approved by Transport FAA Designee Repair Station Canada Airworthiness Group Date of Approval or Rejection Certificate or Signature of Authori is fliduai Designation No. /11-re 5267054_94 SDNY_GM_02753854 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240776 EFTA01326369 NOTICE Weight and balance or operating limitation changes shall be entered,n the appropriareaircralt record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. S. Description ol Wont Accomplished (it more space is required. attach additions, sheets ldenldy with aircraft nationality and repostiarion mark and date work completed.) JANUARY 15, 1990, GULFSTREAM AEROSPACE CORPORATION MODEL G-IV, SiN 1085, N88GA, FAA Type Certificate Data Sheet Al2EA. REFER TO: GAC Maintenance Manual, Illustrated Parts Catalog, and Wiring DIAGRAM MANUAL ATA Chapter(s), 22 AUTOPILOT, 24 Electrical Power, 32 LANDING GEAR; HONEYWELL CORP. Maintenance Manual for the SPZ-8000 INTEGRATED FLIGHT MANAGEMENT SYSTEM; GREYHOUND CORP. NUTCRACKER RIGHT MAIN DC AND/OR ESSENTIAL DC MODIFICATION, ELECTRICAL DhU. No. 32122589, dated 12-25-89. see DER APPROVED FAA Form 8110-3 dated January 10, 1990. The purpose of this alteration is to eliminate the failure of Flight Guidance Computer (FIGC] number 2 whenever power is momentarily lost on the 28 Volt DC Essential Bus because of automatic bus switching. Performed all of the "MODIFICATION INSTRUCTIONS" contained on Greyhound Corp. Electrical Dwg. No. 32122589, referred to above, in compliance with FAR 43.13 Performance rules (general) (a)(b). All parts that were installed were new at the time of installation and comply with FAR 21.303 (b)(1)(2)(4). Tested the modification in accordance with all steps titled '"TESTING THE MODIFICATION" contained on Greyhound Corp. Electrical Dwg. No. 32122589, referred to above, and noted no abnormal or unusual results before, during, or after the testing sequence. Recorded compliance with this FAA form 337 in the aircraft's maintenance records, in accordance with FAR 43.9(a)(1)(2)(3)(4) and complied with the requirements of FAR 43 Appendix B (a)(1)(2)(3). It has been determined that the interrelationship between this change and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. This determination included, but was not limited to, consideration that this modification provides power to the nut- cracker relay circuits in a similar manner that the Gulfstream Model G1159 and G1159A non-VSCF aircraft utilize, as a result of this modification the installed FGC equipment can function safely and properly as it was intended, and the following specific sections of the applicable requirements of the Federal Aviation Regulations have been complied with: 25.1301(a)(b)(c)(d), 25.1309(a), 25.1353(a), 25.1357(a)(c), and 25.1359(d). There were no changes to the aircraft's electrical load analysis and the effect upon the aircraft's weight and balance report is negligible. ****END OF THIS SHEET****Greyhound Corp. Dwg. 32122589 is attached ❑ Additional Sheets Are Attached SDNY_GM_02753855 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240777 EFTA01326370 Form Approved .., •. 0 • OMB No. 2120-0020 MAJOR REPAIR AND ALTERATION US Ocorrnee. aeon osmon (Airframe, Powerplant, Propeller, or Appliance) For FAA Use Only Weenellivicifien Office Identification AdOeradreelen Jr PC ParIZ)O INSTRUCTIONS: Print or type all entries. Sea FAR 43.9. FAR 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof)) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to repon can result i acivil penalty nol to exceed $1.000 for each such violation (Section 901Federal Aviation Act 011956). Make Model GULFSTREAM AEROSPACE CORP. G —IV I.. Aircraft Serial No. Nationality and Registration Mark 1085 N88GA Name (As shown on registration certificate) Address (As shown On registration certificate) BA LEASING & CAPITAL CORP. TWO EMBARCADERO CENTER 2. Owner SAN FRANCISCO CA. 94111 3. For FAA Use Only 4. Unlit IdentlfIcalion 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item I above) XX POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6. Conformity Statement A. Agency's Name and Address 8. Kind of Agency C. Certificate No. x US Certificated Mecham< LANCE A. MATTESON Foreign Ceeld'Med liAeCheniC 2407 EAST SHEA BLVD. manufanifICAIMS %VIC StillI011 CO AP 1864049 PHOENIX, ARIZONA 85028 cturer D s certify that the repair and/or alteration made to the un f(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 430f the U.S. Federal Aviation Regulations and that the information furnished herein is true and Correct to the best of my knowledge. Coate Signature of A ed Indwidus T. Approval for Return To Sr*? upt. Ot matntenance Pursuant to the authority given persons specified below. We unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is .4) APPROVED O REJECTED FAA Fit Standards Other (Specify) MWMOr Manufacturer XX IrtepectiOn AuthOreratiOn BY FAA Designee Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Refection Certificate or Signature 01 Authorized idual Designation No. /—/e -90 t 26705494 Orr SDNY_GM_02753856 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240778 EFTA01326371 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. S. Description col Work Accomplished (U more space is required. attach additional sheets Identity With 811Cfel nationality and registration mark and date work compleunt1 JANUARY 15, 1990, GULFSTREAM AEROSPACE CORPORATION MODEL G-IV, S/N 1085, • N88GA, FAA Type Certificate Data Sheet Al2EA. REFER TO: GULFSTREAM AEROSPACE CORP. (GAC] MAINTENANCE MANUAL, ILLUSTRATED PARTS LIST, AND WIRING DIAGRAM MADATAL - ATA CHAPTER 49; GARRETT AIRESEARCH AUXILIARY POWER UNIT MAINTENANCE MANUAL 49-21-89 FOR MODEL GTCP36-1CCG; GREYHOUND CORP. API SURGE VALVE CONTROL MODIFICATION ELECTRICAL CHG. No. 49122489, dated 12-24-89, see D€ APPROVED FAA Form 8110-3 dated January 10, 1990. The purpose of this alteration is to eliminate a nuisance operation of the PPUes surge control valve whenever power is momentarily lost on the 28 Volt Essential Bus because of automatic bus switching. Performed all of the modification instructions contained on Greyhound Corp. Electrical Dwg. No. 49122489, referred to above, in compliance with FAR 43.13 Performance rules (general) (a)(b). All parts that were installed were new at the time of installation and comply with FAR 21.303 (b)(1)(2)(4). Tested the modification in accordance with all steps titled "TESTING THE MODIFICATION" contained on Greyhound Corp. Electrical Dwg. No. 49122489, referred to above, and noted no abnormal or unusual results before, during, or after the testing sequences. Recorded compliance with this FAA form 337 in the aircraft's maintenance records in accordance with FAR 43.9 (a)(1)(2(2)(4) and complied with the requirements of FAR 43 Appendix B (a)(1)(2(3). It has been determined that the interrelationship between this change and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. This determination included, but was not limited to, consideration that this modification provides power from the same power source that the Gulfstream Aerospace Model G1159A (VSCF) (GIII) aircraft uses to control the APU's surge control valve, the installed equipment will function safely and properly as it was intended and the following specific sections of the applicable requirements of the Federal Aviation Regulations have been complied with: 25.1301(a)(b)(c)(d), 25.1309(a), 25.1353(a), 25.1357(a)(c), and 25.1359(d). There were no changes to the aircraft's electrical load analysis and the effect upon the aircraft's weight and balance report is negligible. ****END OF THIS SHEET""Greyhound Corp Dwg. 49122489 is attached ❑ Additional Sheets Are Attached SDNY_GNL02753857 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240779 EFTA01326372 US DEPARTMENT OF TRANSPORTATION Fen. Apron', . , FEDERAL AVIATION ADMINISTRATION Sweet Berne No. as-Ro60.r MAJOR REPAIR AND ALTERATION FOR FAA USE ONLY OFFICE J DENTWICATION (Airframe, Powerplant, Propeller, or Appliance) \N I CSQD INSTRUCTIONS: Print or type all entries. Ste FAR 43.9. F 1R 43 Appendix B. and AC 43.9-I (or for instructions end disposition of this form. subsequent revision chereoll mAn Gulfstream MOOEL Aerospace G -IV 1. AIRCRAFT SERIµ NO. .NATIONALITY AND REGISTRATION MARK 1085 , N88GA NAME (Ai 'Soon on registration nortincoro) i ADDRESS fro shown on registration tertikahlt 2. OWNER I BA Leasing ITwo Embarcadero Ctr, 10th Floor and Capital Corp. San Francisco, CA 94111 3. FOR FAA USE ONLY 4. UNIT IDENTIFICATION 5. TYPE UM? MALI NOM Mem. NO. wee. Wail I MVP. AIRFRAME (A de ;bed tern I obo 0••••••••••••••••••••••• x PoWettlANT PROPELLER TVPI APPLIANCE mthytACTUtal 6. CONFORMITY STATEMENT A. AGENCY'S NAME AND ADDRESS R. KIND Of AGENCY C. CERTIFICATE NO. U.S. ClititiCal0 mux.•.I6 Western Commander, Inc. FOittiON CtaloriCATI0 MCKANIC REPAIR STATION #4221 16300 Daily Drive —11- COITitiCATI0 suits STATION Ail A 4, R-I,2, Al Lila AAP Van Nuys, CA 91406 iiiANUIACTUala D. 1 cenify that the repair and/or alteration made to the unit's) identified in item 4 above musclemen's hereto have been made in accordance with he requirements of Pan 43 of the U.S.and described on the reverse or ead that the information furnished herein is true and correct to the ben of my knowledge. Federal Aviation Regulation! DATE SIGNA I OF AUTHORIUD - INDIVIDUAL September 7, 1989 e . 7. APPROVAL FOR ROM T SERVILE pen uan to the authority given persons specified below the unit identified in item 4 was inspected in the manner prescribed by - the Administrator of the Federal Aviation Adtninittanion and is 0 APPROVED 0 REJECTM P44 TIT. IITANOA191 OMR 4.00,) IMMIPACIIMI INSPOCISON AUTICIUSATION nelfger011 BY CANADIAN DEPARTMENT FAA Cillgatell x WWI STATION OP TM/MOW 'Mallet°. Or [ DATE OP APPROVAL OR CERTIFICATE OR SIGN SIGN E OF AUTHOR?) II:rU artt ocy REJKTION DESIGNATION NO. 9-7-89 #4221 . D ny C. rnham, Chief Inspector (7-en ($320) SDNY_GM_02753858 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240780 EFTA01326373 EFTA01326374 I 8LetZ00- V.L.A3 LT PUB 'ST '01 '6 '8 'L SHdV89V8Vd H3CI8O 3/W331O8d O1103f8fS 629ESLZCINOANEIS NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. DESCRIPTION OF WORK ACCOMPLISHED (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Avionic and Electrical modifications installed per drawings listed on Western Commander Top Drawing #08000012 N/C dated 8-8-88 and approved by DER #NM-476. Installed Sundstrand Mark V Ground Proximity Warning System per data approved by STC SA218850. Minor deviations performed per Western Commander drawing #08069091 N/C dated 2-8-88 approved by DER #NM-476. Installed Honeywell LSZ-850 Lightning Sensor System in accordance with data approved by STC SA2388S0 and Western Commadner Drawing No. 08069157 N/C dated 11-14-88, approved by DER #NM-476. Installed De Vore Logo Lights per data approved by STC SA4749SW Rev. #3 dated 1-21-88. Installed a third Honeywell Inertial Reference System (IRS), a third Honeywell Flight Management System, NZ910 Navigation Computers (3), and a Single Honeywell VLF/OMEGA Sensor in accordance with data approved by STC SA3774NM. Flight Manual supplements provided and Equipment List revised. Aircraft weight and balance report revised. END 6 ADDITIONAL SHEETS ARE ATTACHED C FAA AC/2490A 0 U.S. GOVERNMENT PRINTING OF TICE I966-559.I2I /40260 LIS DEPARTMENT OF TRANSPORTATION Fenn Approi _ . FEDERAL AWATION•ADMINISTRADON B.4410 8 eau.Vet.04 ROO I I FOR FAA USE ONLY 1 MAJOR REPAIR AND ALTERATION IDENTIFICATION (Airframe, Powerplant, Propeller, or Appliance) 7 N‘( INSTRUCTIONS' Pnnt or type ell entries See FAR 4)9. F X R a) Appendix R. and AC 43.9-I lot subsequent revision thereon for instructions and disposition of this form. MAKE I MODEL Gulfstream Aerospace I G - IV I.. AIRCRAFT Mal NO. NATIONALITY AND REGISTRATION MARK 1085 i N88GA NAME (Ai shot', on registration cerrtigrott) ADDRESS (As show" on repoleolion erfiPcoTS) I Two Embarcadero Ctr, 10th Floor 2. On " 1 BA Leasing and Capital Corp. I San Francisco. LA 94111 3. FOR FAA USE ONLY 4. UNIT IDENTIFICATION S. TYPE UNIT MASS /*CPU I Stew. NO. M111 WAN •110N AIRFRAME ••••••••••••••••••••••••• (A de Med I ob two)•••••••••••••••••••••• X POWERKANT PROPELLER POI APPLIANCE ssaminemuest 6. CONFORMITY STATEMENT A. AGENCY'S NAME AND ADDRESS I. KIND Of AGENCY C. CERTIFICATE NO. V.S. CIITOKATID islettANIC Western Commander, Inc. POTION CiatinCATIO AtICitANIC REPAIR STATION #422I 16300 Daily Drive Y wall STATION A-3 84, R1, 2,87 Lit, A & p Van Nuys, CA 91406 atAstuFACTuate D. I certify that the repair and/or e 'on made to the 'mitts) identified in hens 4 above and described on the reverse or enechments hereto have been made in accordance with he requirements of Pan 45 of the U.S. Federal Aviation Regulation, sad that the information furnished herein is inn and correct to the best of my knowledge. DATE GNATURE OF i D INDIVIDU September 8, 1989 7. APPROVAL FOR RETURN TO SERVICE Put uen to the euthoriey given persons specified below the unit identified in item 4 was inspected in the manner prescribed by the Adminietntor of the Federal Aviation Administration and is UAPPROVED OREJEL M./ FAA In STANDARDS 000 agyroW MANVFACTMORS lesSeKTION AUTHORIZATION petrol SY CANN:MAN DEPAIITAMNT SA IMMOtell XX "PAM STATION OF INSAKTOt OM Ala 2 DATE OP APPROVAI OR CERTIFICATE OR SIGMA T E OP AUTHORIZED I DIVIDU ON DESIGNATION NO LI- . 9-8-1989 #4221 nnv C Farnham. Chief Inspector AA Ponn 337 17-on 013201 SDNY_GM_02753860 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240782 EFTA01326375 EFTA01326376 £8LIWZ00ViSa LT Pim 'ST '01 '6 '8 'L SHdtql9V8Vd 2130180 3AI1D3108d 01_031$:ins L99ESLZ0 NO ANDS NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. DESCRIPTION OF WORK ACCOMPLISHED (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Custom interior installed in accordance with Gulfstream Aerospace Report #1159C-GER-023, Revision 02 dated November 14, 1988 and the following reports as listed in Consulting Aerospace Engineers, Inc. reports approved by DER #NM-442 and Aero Interiors, Inc., Drawing RAI-G-1085 dated August 28, 1989. The following major components installed per the reports and specifications as listed: 1. L/H Bar Installation CAE AIN-52-2 2. R/H Galley Installation CAE AIN-52-3 3. R/H Fed Crew Galley CAE AIN-18-3 4. T.V. Entertainment Installation CAE AIN-38-8 5. Vanity Cabinet Installation CAE AIN-41-4 6. L/H & R/H Stereo/ Storage Cabinet Installation CAE AIN-41-8 7. Bulkhead Installation CAE AIN-38-26 8. 539.75 Bulkhead Reinforcement & Net Inst. CAE AIN-GIV-I 9. Aft Toilet Service Panel Installation CAE AIN-GIV-2 10. Floorboard Replacement CAE AIN-GIV-4 11. Water containers & Pedistal Installation CAE AIN-GIV-6 12. Aft Baggage Shelves and Net Installation CAE AIN-GIV-8 13. Drain Mast Installation CAE AIN-GIV-9 14. Service Ladder Instalation CAE AIN-GIV-10 15. Aft Toilet Installation CAE AIN-GIV-12 16. Service Tool Box Installation CAE AIN-GIV-13 17. Seat Track Installation CAE AIN-GIV-14 Insullation and covering materials meet the requirements of FAR 25.853 Appendix F part 1 paragraph (a) through (d) as stated in 1989 Aero Interiors, Inc. Report #AI -1085-FR-45 dated September 7, and substantiated by John Caleo, Inc. FAA DER #NM-682. Aircraft weighed on jacks upon completion of outfitting. Equipment list and weight and balance reports revised. 5, All workmanship accomplished according to A.C. 43-13-1A Chapters 6, & 7 and A.C. 43-13-2A Chapters 1, 9, 12 & 13. END O ADDITIONAL SHEETS ARE ATTACHED C FAA AC724904 *U.S. GOVERNMENT PRiN TING OF FICE 1916-659.12O40260 ;eat of_ 27 4* • Form Approved OMR No. 21200020 OS Datong-mai MAJOR REPAIR AND ALTERATION For FM Use Only celtarsortaion liationi Aviation (Airframe, Powerplant, Propeller, or Appliance) Office IdeabfiCagen„ „ Atrnintar• tiOn tje‘rk air )Jae INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendtx B. and AC43.9-1 (or subsequent revision theme° for instruct/cos and disposition of this fon. This is required by law (49 U.S.C. 1421). Failure o report can result in a civil penalty not lo exceed S 1000 for each such violation (Section 901 Federal Aviation Act of 1958). make model GOLFSTREAM CIV 1. Aircraft Sabi No Nalianaky end Ropisoraien Mark 1085 N677RP Name (As sites on registraton eerbfkale) Address (As shone on registration comitano PETERSEN AVIATION 7155 VALJEAN AVE. 2. Owner VAN NUYS, CA 91406 3. For FAA Use Only The data identified herein compli with a plicable al rthin 5 requirements is approved and only for above describe aircraf •ubject con i;y fie on by a person authorized in FAR 43.7. FAA INSPECTOR WP-FSDO-1 y DATE: dad .15 ..#1;21r e 4. Unit Identification 5. Typo Unit • Serial No. Repair Anenwon AIRFRAME (As described In Item 1 above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer 8. Conformity Statement A. Agency's Name and Address B. /0nd of Agency C. Certificate No. Ire AVIONICS INC. U. S. Certified Mechanic AQ4ROS9N RADIO CI. 2, 3 7035 SOPHIA AVE. Foreign Certified Mechanic LTD INSTR VAN NUYS, CA 91406 X Certified Repair Station LTD AIRPRAHS AQ4R059N Manutachrer D. I certify that the repair and/or alteration made to the can t(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance w tit the requirements of Part 43 of the U. S. Federal Aviation Regulations and that the information furnished herein Is true and correct to the best of my knowledge. Date Signature of Authorized Individual //aS/20cs- etaa17 -‘ 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is g APPROVED O REJECTED FAA Ft Standards Manufacturer in Auttniurition Other (Specify) Impeder BY Person Approved by Transport FMDesiree X Repair Station Canada Anvortrinees Grew Dale of Approval a Rejection Certlficate or Signature of Authorized Individual ........-^c z eta/ Designation No. / AQ4R059till FM Form 337 (1241) SDNY_GM_02753862 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240784 EFTA01326377 1 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alterationmust be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. DESCRIPTION OF WORK ACCOMPLISHED (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) N677RP Installed an Artex C-406-1 ELT P/N 453-5002. Antenna P/N 110-340. and Remote Switch P/N 345-6196-04. The installaben was done Ni accordance with AETEX document number: 570-5001 REV A. Reference 8110-3 Signed by Trevor Strong DER No. DERT60581NM for mounting approval of the antenna. The ELT was mounted at STA. 753.50. the antenna was mounted at STA. 633.00. The ELT Switch was mounted in the cockpit on the copilot's dzus rail at STA. 54.00. A 1 amp circuit breaker labeled 'ELT' was Installed on the copilots circuit breaker panel. Existing spare wires were used for the ELT system. Reference IFR Avkmics document no. ICAW AXE% 406 for Instruction for Continued Airworthiness. Mounting for el 03MpOnents and installation details are in compliance with applicable portions of AC.13-1I3 Chapters 11 and 12; AC 43.13-2A Chapters 2 and 3. The mountings are made on existing previously approved equipment shelves or location in the aircraft and meet strength requirements of AC 43.13-2A Chapter 1. ARTEX Description and operation manual document number 570-5001 was installed in the aircraft The ELT. Antenna. and the NAV interface unit meets TSO requirements C126. A logbook entry has been made. Wiring diagrams. Revised Weight 6 Balance and Equipment list Amendment have been provided as necessary. Work Order 39886 on Neat this agency covers the work describe above. ND El...ADDITIONAL SHEETS ARE ATTACHED • laGe03:1101.0.C46012/40036 SDNY_GIA_02753863 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240785 EFTA01326378 IFR Avionics, Inc. Document No. ICAW ARTEX 406 • : 7035 Sophia Ave. Van Nuys CA. 91406 Instructions For Continued Airworthiness For a Artex ELT This alteration to this aircraft obligates the aircraft operator to include the following maintenance information provided by this document in the owner/operator's Aircraft Maintenance Manual and the ownedoperator's Aircraft Scheduled Maintenance Program. The Artex 406 ELT Line Replaceable Units' (LRU) maintenance is on condition and there is no periodic, preventative or scheduled maintenance required for the continued operation of this unit. Should any failure of the Artex 406 ELT System occur, it should be properly noted, and the unit should be removed from the aircraft. Once a failure has occurred, it is advisable to do a visual inspection of the Artex 406 ELT system. This inspection should include, but is not limited to the Artex 406 ELT mounting, the antenna, the NAV Interface Unit, associated wiring. and any related hardware. This inspection should be performed through elementary means. 1. Maintenance, repair. reinstallation and testing information for the Mex 406 ELT system in this aircraft are contained in the Artex Description, Operation, Installation, and Maintenance Manual document number 570- 5001 REV A. 2. The Line Replaceable Unit (LRU) part numbers and other necessary part numbers contained in the installation data documentation for this modification should be placed into the aircraft's owner/operators appropriate Illustrated Parts Catalog (IPC). 3. Wiring diagram information contained in the installation data documentation for this modification should be placed into the aircraft owner/operators appropriate airplane Wiring Diagram Manual. 4. The scheduled Maintenance tasks required by this modification are to added to the aircraft owner/operators appropriate airplane maintenance program are as follows: a. Perform on at least an annual basis a periodic inspection of the equipment rack, equipment mountings, associated wiring, cables, connectors, hardware, antenna and related aircraft structure for integrity, security, wear. chaffing, and etc. Special attention should be given to the aircraft primary structure with regards to fatigue and stress cracking, corrosion, and etc. NOTE: These inspections may appear as part of opportunity inspections or recommended Zonal inspection tasks. 5. Should it become necessary to remove a component of the Artex 406 ELT system, secure the associated cables and wiring, collar the applicable circuit breakers, placard the aircraft that the unit has been removed. Revise the weight & balance and the equipment list arid make a logbook entry stating the unit has been removed for service (refer to section 91.213 of Title 14 of the Code of Federal Regulations and/or the aircraft's MEL) 6. The Artex 406 ELT System and its related primary components can only be repaired at a factory authorized repair center or an appropriately rated FAA Part 145-repair station. NOTE: Should structural repairs be necessary to the airframe they should be performed in accordance with FAA approved data, the Structural Repair Manual from the Airframe manufacturer (SRM) or guidance contained in Advisory Circular (AC) 43.13-18, if applicable. 7. For additional information regarding this modification and the related equipment refer to the following documents: a. The Artex Description, Operation, Installation, and Maintenance Manual document number 570-5001 REV A. Page 1 of 1 SDNY GM 02753864 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240786 EFTA01326379 V SDNY GM 02753865 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240787 EFTA01326380 _ Form Approved 0 OMB No. 2120-0020 MAJOR REPAIR AND ALTERATION For FAA Use Only arm (Airframe, Powerplant, Propeller, or Appliance) reatnal on ettentureatan Office identification W/4 0 1— gOri CC A 0 INSTRUCTIONS:Print or typo all entries. SeeFAR43.9.FAR43Appendix B.and AC43.9-1(or subsequent rewisionthereol)I or instructions and disposition of thislorm.Thisreport is required by law (49 U.S.C. 1421).Failure toreport can result ina civil penalty not to exceed 51.000 for each such violation (Section 901 Federal Aviation Act of 1958). • Make Model GULFSTREAM G-IV 1. Aircraft Serial No. Nationality and Registration Mark 1085 N677RP Name (As shown on registration certificate) ROOMS (As shown on registration certificate) PETERSEN AVIATION 7155 VALJEAN AVE 2. Owner VAN NUYS CA 914064917 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make . Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer • 8 Conformity Statement A. Aunty's Name and Address B. Kind of Agency C. Certificate No. IFR Avionics Inc. US. Certificated Mechanic AQ4R059M Radio Cl 7035 Sophia Ave. Foreign Cettincatne Mechanic 1.2,3 LTD Instr. Van Nuys CA 91406 x Certificated Repair Station LTD Airframe. Manufacturer LTD Spec Service. D. I certify thattherepairand/or alteration madelotheun t(s)identifiedin itern4aboveanddescribedonthereverseorattachments hereto have been made in accordance with the requirements 01Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized Individual q-k-1, - Loot 7. Approval for Return TojSe tt Pursuant to the authority given persons specified below, the unit Identified in item 4 was inspected In the manner prescribed by the Administrator of the Federal Aviation Administration and is xi APPROVED 0 REJECTED FAA Flt. Standards Other (Specify) Inspector Manufacturer Inspection Authorization By FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval orRejection Certificate or Signature of Autttrize dividual q-(---4,- ,, 2040esignation No. ANR05914 6 FAA Fenn 337 0243a) SDNY_GM_02753866 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240788 EFTA01326381 • .6 NOTICE Weight andbalance or operating limitation changes shallbe enteredin the appropriate aircraft record. Analteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished Of more spaces required, attach adchtlonal sheets. Identify with as:craft nahonalify and reparrafron mark and date work completed.) N677RP Upgraded existing Honeywell TCAS II Traffic Collision Avoidance System (TCAS) to be Minimum Operating Performance Standards (MOPS) 7 version compliant (Change 7), in accordance with Gulfstream STC ST00711AT. Removed existing Honeywell TCAS II Traffic Collision Avoidance System Processor Part Number 4066010-904, SIN 93121994. Sent unit to manufacturer for Change 7 Mod, to be Minimum Operating Performance Standards (MOPS) 7 version compliant (Change 7). Received modified TCAS Processor, new Part Number 4066010-910, unit keeps same Serial Number . Reinstalled modified TCAS Processor in aircraft. Performed ground check of TCAS system. TCAS system passed ground check. Gulfstream Aerospace FM Approved Airplane Flight Manual Supplement Document No. SC41129M04, Rev. A. dated Jan 5, 2001 or later FAA Approved revision, is required with this installation. Instructions for Continued Airworthiness are part of STC contained in Report No. CE41 129A003, Rev. A. dated Jan 5, 2001 This modification does not effect the aircraft's existing Weight & Balance. Log Book entry has been made. Equipment List Amendment has been provided. Work Order 37783 on file at this agency covers the work described above. END 0 Additional Sheets Are Attached OMR. GOVERNMENT ►RINTING OF FICE: 1922-711-012/60157 SONY_GM_02753867 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240789 EFTA01326382 . ... - I - ad - .. Form APPrOved O MAJOR REPAIR AND ALTERATION OMB No. 21200020 US 0•0Celmerd a terecoreere (Airframe, Powerplant, Propeller, or Appliance) For FAA Use Only ows marten Office Identification m Maminblrellen S/P1/- YNY -"AN INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B. and AC43.9-1 (or subsequent revision thereof) lotInstructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed 31.000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model GULFSTREAM G4V 1. Aircraft Serial No. Nationality end Registration Mark 1085 N677RP Name (As shown on registration certificate) Address (As shown on registration certificate) PETERSEN AVIATION 7156 VAI-JEAN AVE 2. Owner VAN NUYS CA 914064917 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As describedIn Item 7 above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer ' 8. Conformity Statement A. Arilincy's Name and Address B. Kind of Agency C. Corti icate No. IFR Avionics Inc. . u.s. catenated Mechanic AtI4R059M Radio C1 7035 Sophia Ave. Foreign Certificated Mechanic 1,2,3 LTD Instr. Van Nuys CA 91406 x Cerlificated Rena Station LTD Airframe. Manufacturer LTD Spec Service. D. I certify thai the repair and/or alteration made to the un t(s) identifiedIn item 4 above and describedon the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Data Signature Authorized Individual 7. Approval lot u To Service /— er Pu suanl to the authority given persons specified below. the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is gl APPROVED 0 REJECTED -, FAA Flt. Standards Other (Specify) Inspector Manufacturer Inspection Authorization EST FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval Or RejeCtion Certificate or Sign e of Authorized Individual Designation No. / 12512,90 I FAA Form 337 met AO4R059 /. 1 l.., 8- SDNY_GM_02753868 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240790 EFTA01326383 NOTICE Weight and balance or operating limitation changes shalt be enteredin the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. a. Description of Work Accomplished (it more space is required, attach additional sheets. Identity with aircraft nationality and registration mark and date work completed.) N677RP Removed eisting NZ-2000 Flight Management System (FMS) Navigational Computer Units (NCU), Part Number (7018879-01002), Serial Numbers (95120678, 95120716, & 95120669) from the aircraft. Sent NCU's to manufacturer for software upgrade from software 4.1 to software 5.2. In accordance with Gulfstream Aerospace Corporation (GAC), Aircraft Service Change (ASC) No. 349AM6. Received modified NCU's from the manufacturer new NCU Part Number is 7018879-03014. NCU's keep their original Serial Numbers. Reinstalled NCU's into the aircraft. Gulfstream Aerospace Corporation FAA Approved Airplane Flight Manual Supplement Number GIV-2000-03, dated July 25, 2000, in accordance with Gulfstream Aerospace Corporation ASC No. 349AM7, is required with this modification. The NZ-2000 system was operationally ground checked in accordance with ASC No. 349AM6. NZ-2000 system passed ground check. The Honeywell FMZ-2000 Pilot's Guide is Installed in the aircraft This modification does not effect the aircraft's eAsting Weight & Balance. No wiring changes were made to the aircraft. A log book entry has been made. An Equipment List Amendment has been provided. Work Order 37626 on file at this agency covers the work described above. END O Additional Sheets Are Attached *U.S. GOVIIRNMENT PRINTING OFFICE: 19112-761-012/50157 SDNY_GM_02753869 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240791 EFTA01326384 Form Approved - 00 MAJOR REPAIR AND ALTERATION OMB No. 2120-0020 tin Orporiment cr TramontalOn (Airframe, Powerplant, Propeller, or Appliance) For FAA Use Only Aviation Office Idenfificat (envoi AdninistratiOn WP-23 INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model Gulfstream Aerospace G-IV 1. Aircraft Serial No. Nationality and Registration Mark 1085 N677RP Name (As shown on registration certificate) Address (As shown on registration certificate) 7155 Valjean Ave. 2. Owner Petersen Aviation Van Nuys, Ca. 91406-3917 3. For FAA Use Only The data identified herein complies with applicable airworthiness requirements and is approved only for the above described aircraft subject to a conformity Inspection by a person authorized In FAR 43.7 IBIC: 40-imiv- —20C4 -4 1" .c.s. LAXIFSDO Dated 3-9-0/ 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in hem 1above) XX POWERPLANT PROPELLER Type APPLIANCE Manufacturer S. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. Garrett Aviation Services U.S. Certificated Mechanic 6201 W Imperial Highway Foreign Certificated Mechanic AN3R377L Los Angeles, Ca. 90045 X Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and cored to the best of my knowledge. Date Signst74,liveri er 03 -0 4 -0) ourchro‘ e dist,h4e-- 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit ides Med In item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is X APPROVED 0 REJECTED FAA Fit. Standards Other (SpecifV) Manufacturer Inspection Authorization Inspector BY Person Approved by Transport FAA Designee X Repair Station Canada Ainvorthiness Group Date of Approval or Rejection Certificate or Signatrely,erso, Designation No. OZ — O4 - di AN3R377L Aficatimi 4 it/Art.1,a", Form 337 (1243) SDNY_Gtv1_02753870 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00240792 EFTA01326385 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished Of more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished. Accomplished an upgrade to the previously installed #1 and #2 transponder systems. The #1 and #2 P/N 622-9210-003 transponders were removed and (2each) transponders that were modified by the equipment manufacture Rockwell/Collins to P/N 622-9210-006 status, in accordance with their service bulletins #13, #17 and #20 were installed. Accomplished an electrical wiring change to the #1 and #2 systems, in accordance with the equipment manufacture Rockwell/Collins Service Information Letter 1-96 dated 10-20-97. The electrical wiring changes mentioned above enables systems to have part number status interchangeability. Accomplished a complete ground operational check of systems and a electromagnetic interference verification with satisfactory results. Tested the #1 and #2 transponder systems for altitude integration, in accordance with FAR Part 43 appendix "E" para. ( c ). No change to weight and balance. END X Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: 1992-769.012160157 SDNY_Glvl_02753871 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00240793 EFTA01326386 kg,' a A7PrOvtd COOIto. 2120l0t0 amei Only MAJOR REPAIR AND ALTERATION Fee FAA Use u S DcywUncal (Airframe, Powerplant,Propeller, or Appliance) Office Identifkadon of Tevoce.wica learnt Arbeee Admit:atriums VitI%-i ••"' 1C K 00 INSTRUCTIONS Print a type al entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision therWt for instrucdons and disposition of thi form. This report is required by taw (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such Notation (Section 901 Federal Aviation Act of 1958). Make Model I. Aircraft GULFSTREAM G-P/ Serial No. Nationality and Registration Mark 1085 N677RP Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner PETERSEN AVIATION 7155 VALJEAN AVE VAN NUYS, CA 91406 - 3917 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make I Model I SerialNo. Repair Alteration Airframe (As described inItem I above) • *********•*****••• X Powerplant fir / V ... Propeller ig st m ei. tat 'MED .. Ill Appliance Tie Fit borhaz nos 6 V Manufacturer FEB 0 9 2001 1 6. Conformity Statement A. Agency's Name and Address B. Kind of YS FSDO C. Certificate No. WESTERN JET AVIATION,INC. U.S. trot echamc W1JR483Y 1750 HAYVENHURST AVE. Foreign Certificated Mechanic VAN NUYS, CA 91406 X Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements ofPart 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowled e Date Signature Authorized Individual . JANUARY 31, 2001 7. royal for Return to Service Pursuant to he authority given persons specified b low, uni ide tilled in item 4 was inspected in the rnanne prescribed by the Administrator of the Federal Aviation Administration and is la APPROVED O REJECTED FAA Flt. Standards Manufacturer Inspection Authorization Other (Specify) BY Inspector FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection Certificate or Signature of Authorized Individnal Designation No. JANUARY 31, 2001 W1JR483Y C D —O41 FAA Form 337 0 1-95) SDNYGlvl02753872 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240794 EFTA01326387 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) PERFORMED THE FOLLOWING CUSTOMER BULLETINS AND AIRCRAFT SERVICE CHANGES: C/B 107 - FLAP "D" TRACT DOWN LOAD HOOKS - INSPECTION. C/B 108 - ACM BYPASS SHUTOFF VALVE - ACTIVATION WIRING - CHAFE PROTECTION. C/B 114 - NOSE LANDING GEAR ACTUATOR ROD END - LIFE LIMIT. C/B 116 - ELEVATOR BALLAST WEIGHT HELICOIL - INSTALLATION. CM 121 - AILERON BOOST BELLCRANK LUG THICKNESS TO LUG RADIUS RATIO - INSPECTION. CB 127 - HE ANTENNA ADAPTER - INSPECTION. C/B 128 - WIRE HARNESS AT F.S. 603 - INSPECTION. ASC 198 A1111 - ACM BYPASS SHUTOFF VALVE ACTIVATION WIRING CHAFE PROTECTION. ASC 403 - WINGLET ATTACHMENT HARDWARE REMOVAL / REPLACEMENT. ASC 414 - NOSE LANDING GEAR ACTUATOR ROD END SERIAL NUMBER. Changes to the Aircraft Weight and Balance has been Determined to be Negligible and Continues to Meet the Airworthiness Criteria Under Which it was Originally Certificated. END • :4r MI\ e I, • I. ' lit %:c!) O Additional Sheets Are Attached SDNY_GIvl_02753873 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240795 EFTA01326388 ,--, ...., of ..- - Form Approved 0 OMB NO. 2120-0020 MAJOR REPAIR AND ALTERATION us cowmen, For FAA Use Only a Loatecornon (Airframe, Powerplant, Propeller, or Appliance) Office Identification feer olAvicitlen Aorilnisffetion alfie - - /0/ -- --,ed>7 a INSTRUCTIONS: Print or type all entries. See FAR 43.9,FAR 43 Appendix B.and AC43.9-1 (or subsequ nt revision thereof),or instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not toexceed51.000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model GULFSTREAM G4V 1. Aircraft Serial No. Nationality and Registration Mark 1085 N677RP Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner PETERSEN AVIATION 7165 VALJEAN AVE VAN NUYS CA 914064917 3. For FAA Use Only The data identified herein complies with a li able al rthiness uirem and is approved only for above described aircraft subject to conformity' s ction n z FAR 43.7. FAA INSPECTOR WP-FSDO-1 li Date:......7Ofe2- 4. Unit Wan IL Typo Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWER PLANT PROPELLER Type APPLIANCE Manufacturer • II Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Ceni icate No. IFR Avionics Inc. • u.s. Certificated Mechanic AQ4Ft059M Radio Cl 7035 Sophia Ave. Foreign Certificated Mechanic 1.2 3. LTD Instr. Van Nuys CA 91406 x Certificated Repair Station LTD Airframe. mannoovref LTD Spec Service. D. I certify that the repair and/or alteration made to(neuritis) 'dentified In item4 above and described on the reverse or attachments hereto have been made In accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date SI tura of Authorized ndlvid I ;--- 2 lf --- ?tat) 7. vat for Rate To Service Pu suant to the authority given persons specified . the unit identified in item 4 was inspected In the manner prescribed by the Administrator of the Federal Aviation Administration and is xl APPROVED 0 REJECTED FAA Fit. Standards Other (Specify) Inspector Manufacturer Inspection Authorization BY FAA Designee X Repair Station Parson Approved by Transport Canada Airworthiness Group Dale of Approval or Rejection Certificate or Sigi lure of Authorized individu ._... Designation No. --- 2 4 - .),,,,,,o AO4ROSSM FAA Form 337 02 eel SDNY_GIvl_02753874 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240796 EFTA01326389 NOTICE Weight and balance or operating limitation changes shall be enteredin the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. IL Description of Work Accomplished and date work completed.) of more space is required, attach additional sheets. Identity with aircraft nationality and registration mark N677RP LCD Monitors. Removed existing lea. Panasonic PV-4662 VCR, and 2ea. Baker Electronics SB1410AAB 14- s Installed two each Samsung Electronics Co. 170MP, 1T' LCD Monitor In accordance with manufacturer Owner's Instructions P/N BN68-00108E-01 dated 1999. Installed a RCA Corp. PROSCAN Model PS8680Z Digital Video Disk Player in accordance with manufacturers Users Manual Manual No. TOCOM 15346010 dated 1998. The LCD monitors are located at arm 151.0, & 443.0, and the DVD is located at arm 145.0. Installation details are in compliance with AC 43.13-1B chapters 11, and 12, AC 43.13-2A Chapter 2, and AC 25-10. AC Post installation ground test were performed in accordance with Manufacturer's installation manual's, and 25-10. All systems operated normally. The above equipment was mounted by Synchro Aircraft Interiors. Van Nuys, Ca. and was structurally approved under FM Form 337, dated May 24, 2000. The above equipment is interfaced to the aircraft's existing cabin entertainment, audio/video switching system. For Continued Airworthiness Instructions for the LCD Monitor see IFR Avionics Inc. Document No. ICAW-170MP, REV. N/C, dated May 23, 2000, for the DVD see IFR Avionics Inc. Document No. ICAW-PS8680Z, REV. N/C, dated March 16, 1999. Revised Weight & Balance performed by Synchro Aircraft Interiors. Van Nuys, Ca. A log book entry has been made. Wiring Diagrams, and Equipment List Amendment have been provided. Work Order 37230 on file at this agency covers the work described above. END ill Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: I102-765-012/601$7 SDNY_GM_02753875 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240797 EFTA01326390 Wt. IFR Avionics, Inc. 1035 Sophia Ave. Document No. ICAW-170MP Dated: May 23, 2000 r Van Nuys Ca. 91406 REV. N/C Instructions For Continued Airworthiness For a Samsung Electronics Co. 170MP 17" LCD Monitor This alteration to this aircraft obligates the aircraft operator to include the following maintenance information provided by this document in the owner/operator's Aircraft Maintenance Manual and the owner/operator's Aircraft Scheduled Maintenance Program. The Samsung Electronics Co. Line Replaceable Unit (LRU) maintenance is on condition and there Is no periodic, preventative or scheduled maintenance required for the continued operation of this unit. Should any failure of the Samsung Electronics Co. 17' LCD Monitor system occur, it should be properly noted, and the unit should be removed from the aircraft. Once a failure has occurred, it is advisable to do a visual inspection of the 17" LCD Monitor system. This inspection should include, but is not limited to the 17' LCD Monitor mounting, associated wiring, and any related hardware. This inspection should be performed through elementary means. 1. Maintenance, repaired, reinstall, and testing information for the 17' LCD Monitor system in this aircraft are contained in the Samsung Electronics Co. Owners Instructions (P/N EIN68-00108E-01 dated 1999, or later). 2. The Line Replaceable Unit (LRU) part numbers and other necessary part numbers contained in the installation data documentation for this modification should be placed into the aircraft's owner/operators appropriate Illustrated Parts Catalog (IPC). 3. Wiring diagram information contained in the installation data documentation for this modification should be placed into the aircraft owner/operators appropriate airplane Wiring Diagram Manual. 4. The scheduled Maintenance tasks required by this modification are to added to the aircraft owner/operators appropriate airplane maintenance program are as follows: Perform on at least an annual basis a periodic inspection of the equipment rack, equipment mountings, associated wiring, cables, connectors, hardware, and related aircraft structure for integrity, security, wear, chaffing, and etc. Special attention should be given to the aircraft primary structure with regards to fatigue and stress cracking, corrosion, and etc. NOTE: These inspections may appear as part of opportunity inspections or recommended Zonal inspection tasks. 5. Should it become necessary to remove the 17" LCD Monitor, secure the associated cables and wiring, collar the applicable circuit breakers, placard the aircraft that the unit has been removed, revise the weight & balance and the equipment list and make a logbook entry the unit has been removed for service refer to section 91.213 of Title 14 of the Code of Federal Regulations and/or the aircraft's MEL). 6. The 20" LCD Monitor and its related primary components can only be repaired at a factory authorized repair center or an appropriately rated F.AA. Part 145 repair station. NOTE: Should structural repairs be necessary to the airframe they should be performed in accordance with F.A.A. approved data, the Structural Repair Manual from the Airframe manufacturer (SRM) or guidance contained In Advisory Circular (AC) 43.13-1A, if applicable. 7. For additional Information regarding this modification and the related equipment refer to the following documents: a. Samsung Electronics Co. 17* LCD Owner's Instructions (P/N BN68:00108E-01 dated 1999, or later). Page 1 of 1 SDNY_GM_02753876 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240798 EFTA01326391 SDNY_GM_02753877 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240799 EFTA01326392 IFR Avionics, Inc. Document No. ICAW-PS8680Z 7035 Sophia Ave. Dated: March 16, 1999 Van Nuys Ca. 91406 REV N/C Instructions For Continued Airworthiness For a ProScan PS8680Z Digital Video Disk (DVD) Player This alteration to this aircraft obligates the aircraft operator to include the following maintenance information provided by this document in the owner/operators Aircraft Maintenance Manual and the owner/operators Aircraft Scheduled Maintenance Program. The ProScan Line Replaceable Unit (LRU) maintenance is on condition and there is no periodic, preventative or scheduled maintenance required for the continued operation of this unit. Should any failure of the ProScan PS8680Z DVD, it should be properly noted, and the unit should be removed from the aircraft. Once a failure has occurred, it is advisable to do a visual inspection of the DVD system. This inspection should include, but is not limited to the DVD mounting, associated wiring, and any related hardware. This inspection should be performed through elementary means. 1. Maintenance, repaired, reinstall, and testing information for the DVD system in this aircraft are contained in the ProScan User's Manual (Manual No. TOCOM 15346010). 2. The Line Replaceable Unit (LRU) part numbers and other necessary part numbers contained in the installation data documentation for this modification should be placed into the aircraft's owner/operators appropriate Illustrated Parts Catalog (IPC). 3. Wiring diagram information contained in the installation data documentation for this modification should be placed into the aircraft owner/operators appropriate airplane Wiring Diagram Manual. The scheduled Maintenance tasks required by this modification are to added to the aircraft owner/operators appropriate airplane maintenance program are as follows: Perform on at least an annual basis a periodic inspection of the equipment mountings, associated wiring, cables, connectors, hardware, and related aircraft structure for integrity, security, wear, chaffing, and etc. Special attention should be given to the aircraft primary structure with regards to fatigue and stress cracking, corrosion, and etc. NOTE: These inspections may appear as part of opportunity inspections or recommended Zonal inspection tasks. 5. Should it become necessary to remove the DVD secure the associated cables and wiring, collar the applicable circuit breakers, placard the aircraft that the unit has been removed, revise the weight & balance and the equipment list and make a logbook entry the unit has been removed for service refer to section 91.213 of Title 14 of the Code of Federal Regulations and/or the aircraft's MEL). 6. The DVD and its related primary components can only be repaired at a factory authorized repair center or an appropriately rated F.A.A. Part 145 repair station. NOTE: Should structural repairs be necessary to the airframe they should be performed in accordance with F.A.A. approved data, the Structural Repair Manual from the Airframe manufacturer (SRM) or guidance contained in Advisory Circular (AC) 43.13-1A, if applicable. 7. For additional information regarding this modification and the related equipment refer to the following documents: a. ProScan Users Manual (Manual No. TOCOM 15346010). Page 1 of 1 SDNY_GM_02753878 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240800 EFTA01326393 SDNY_GM_02753879 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240801 EFTA01326394 G-1-00 Mt 14.8.240ma--- di /R. Form Approved OMB No.2120-0020 f i 4 MAJOR REPAIR AND ALTERATION U.S. Depeetneet For FAA Use Only plTheuppeteme (Airframe, Powerplant, Propeller, or Appliance) Office Identification ham Awaon AdmInIstrollea ?OO 0 a( 557 / 517--/Z 5 Go Po I INSTRUCTIONS: Print or type al entries. See FAR 43.9, FAR 43 Append( B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report Is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act 1958) Stelae GULFSTREAM motet GIV 1. Aircraft Sens]It 1085 NolimarY end Rightists, Mork N677RP Marne (As shoat ea segIstntlan anthem.* Address (As shawl on registration certificate) 2 Owner PETERSEN AVIATION 7155 VAUEAN AVE. VAN NUYS. CA. 91406-3917 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Mention X AIRFRAME (As describedIn Item I above) POWERPLANT PROPELLER Type APPLIANCE Manteactser 6. Co formity Statement A. Agency's Name and Address 8. Kind of Agency C. Certificate No. RICHARD P. JOSEPH JR. 0 U.S. CerlAcated MochaPp MP 245198915 3456 GARNET ST. APT. 0338 0 Foreign Oct-Seated iischaric TORRANCE. CA. 90503 0 CestAxalecl Repair Swan 0 manuracturer D. I certify that the repair and/or alteration made to the unifts Identified in kern 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is bye and correct to the best of my knowledge. Date Signature of Authorized Indvidted--- 6.2q . co n -----' 2 7. Approval for Return To Service `------t----- Pursuant to the authcrey given persons specified below, the u rt identified In kem 4 was inspected in the manner presented by the Administrator of the Federal Aviation Administration and is ] APPROVED 12I REJECTED Other BY 0 FAA Ft aavixds 0 Manufacturer 0 Inspection Authorization (S y) n PersonaPaca:ObiTfbraPad 0 FAA Designee 0 Repair Station LI Canada Alnvorthiress Group Date of oprwal or Rejection Certificate or Designation No. of Inefrvidual b M oo 614356.225" IC(ALacrIA,N FAA Form 337 (12.88) SDNYGlvl_02753880 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240802 EFTA01326395 NOTICE alteration muslin) " Weight end balance or operating limitation changes shall bo entered in the appropriate eitcraftnscord. An compatible with all previous operations to assure continued conformity with the applicable einvorthiness requirements. 8. Description of Work Accomplished completed.) (IImore space is required, attach additional shoe& Identifywith aircraft naffonatily and togistration mark and data work 1.) FIREBLOCKING: WERE REUPHOLSTERED AS REMOVED ALL SINGLE SEATS, DOUBLE SEATS, ATHREE PLACE DIVAN, AND JUMPSEAT. ALL SEATS FOLLOWS: SKANDIA, INC. DAX GRAPHITE/POLY 2611.0 FOR ALL SEATS MENTIONED SEATS EDELMAN LEATHER -ROYAL HIDE P/N RH323 CUSTOM LT GRAY DYE LOT AFLOO FOR (6) SINGLE GARRETT LEATHER C-616 CHATHAM SEAFOG DYELOT 67296 FOR RI EACH DOUBLE SEATS JOB 034)32FOR THREE PLACE ICF/UNIKAVAEV FABRIC 917 COLOR 81 CRANBROOK CRANBROOK GREY TREATED AT SYNCRO REF. DIVAN VAN NUYS AWNING CO. ARABIAN COTTON ARMY DUCX TREATED AT SYNCRO REF. LB 00032 SKANDIA INC. NOMEX BATTING USED ON ALL ABOVE SEATS MENTIONED. FAR 25.853 (CI APPENDIX F PART ALL MATERIALS MENTIONED ABOVE MEET FLAMMABIUTY &FIREBLOCKING REQUIREMENTS PER BOGGS DERV-406020CE ON II AMENDMENT 2583. REFERENCE SKANDIA, INC. TEST PLAN 15823 REV. IR. APPROVED BY JUDY 5/19/00. 2.1 FLAMMABILITY: FABRIC P/N 1797/1 LAV1NA. REMOVED DECOR PANELS AND STRIPPED OFF EXISITNG FABRIC. RECOVERED WITH A BER GAM° RECOVERED WITH A KNOLL TEXTILES LAV AFT BULKHEAD AND DOOR WERE REMOVED AND STRIPPED OF EXISITNG COVERING. FABRIC P/N K183-1 BUM! PEARL. APPENDIX F PART I (el (1) G). ALL MATERIALS MENTIONED ABOVE MEET FLAMMABILITY REQUIREMENTS PER FAR 25.853 (o) INC. TESTPLAN 85902 &81103 APPROVED BY JUDY BOGGS DERV-4050204C E ON 4/25/00. REFERENCE SKANDIA, FLAMMABILITY REQUIREMENTS PER INSTALLED NEW 10016WOOL CARPET THROUGHOUT AIRCRAFT, CARPET MATERIAL MEETS FAR 25.853(A). REFERENCE 81103 PROVIDED BY SCOTT GROUP. TRUSS STRUCTURE AFT BY 4.75 INCHES 3.1THE EXISTING THREE PLACE DIVAN IS MODIFIED BY MOVING THE EXISTING CENTER UNDERNEATH. AND THE FWD TRUSS STRUCTURE FWD BY 4 INCHES FOR THE PURPOSE OF FITTING UFE RAFTS MENTIONED MODIFICATION IS WORK WAS PERFORMED BY DYNAMO AVIATION PER SYNCRO WORK ORDER.THE ABOVE REFERENCE STRUCTURAL APPROVED BY HOWARD L PATTERSON DERT405434MM, PER AN 8110-3 DATED 5/8/00. GALANTE. SUBSTANTIATION REPORT DA41085 REV. "NC* DATED 5/8/03 PREPARED BY SHANAZ REMOVED E)GSITNG RACK FROM 4J ONE PANASONIC VCR MODEL PV4682 WAS EXCHANGED WITH DVO PLAYER MODEL PS88802. L/H FWD COMPARTMENT. MODIFIED TO INCORPORATE NEW DVD PLAYER. MONITORS MODEL 8170MP. ONE IS REMOVED TWO 14' LCD MONITORS FROM STA 193B &STA441INSTALLED TWO 17" LCD LOCATED AT STA 193 AND THE SECOND MOUNTED ONTO THE AFT BULKHEAD ON THE FWD R/H EXISITNG STORAGE CABINET • ONE IS MOUNTED ONTO THE FWD SIDE OF THE AFT L/H BULKHEAD LOCATED AT STA 442. REFERENCE 81103 APPROVED ALL THE ABOVE MODIFICATIONS ARE APPROVED BY HOWARD L. PATTERSON DERT-535434-NM. ON 5/15/00. REPORT DOCUMENT SY.GLIOSSREV. PREPARED BY SHANAZ GALANTE. FORM 337, DATED ON MAY THE ABOVE EQUIPMENT WAS ELECTRICALLY INSTALLED BY IFR AVIONICS, VAN NUYS, CA. SEE FAA 242000 FOR DETAILS. DATED 5/23/01 5.) WEIGHT &BALANCE WAS RECALULATED. REFERENCE WEIGHT &BALANCE REPORT El Add Tonal Sheets Are Attached (1248) U.S. GPO:19893-663-171 FAA Form 337 SDNY_GIvI_02753881 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240803 EFTA01326396 r • Interior Alteration Report Syncro Aircraft Interiors, Inc. Gulfstream GIV Van Nuys, Ca. 91406 N677RP S/N 1085 May 24,2000 Table Of Contents 4— Opposite Page - FAA form 337 1. Compliance with FAR 25.853 (c) for fireblocking of all passenger seats. Skandia, Inc. Test plan #5823 2. Proof of compliance per FAR 25.853 (a) for materials used on: a.) Decor Panel Fabric b.) Lay aft bulkhead c.) Carpet 3. Divan modification 8110-3 and report 4. Structural Substantiation 8110-3 and report 5. Weight & balance report (original inserted into weight & balance book) SDNY_GIvl02753882 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240804 EFTA01326397 SDNYGM02753883 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240805 EFTA01326398 • - U.S. DEPARTMENT OF TRANSPORTATION DAM FEDERAL AVIATION ADMINISTRATION 05/19/00 - STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIK4K/U- I UK AIMUKAI- I IVJPIIMINtN I IULN IIFICA I IUN MAKE MODEL NO. TYPE (Airplane. Ratio. Helicopter NAME OF APPLICANT Me.) OULFSTPEAM ON Stadia, Ine. SIN 1085 Aiwhat SYNCEDAIRCRAFT INTERIORS WI VI- UA IA IDENTIFICAI ION NILE Work Order 0 FIREBLOCKING FLAMMABILITY TEST RESULTS 45812-00 Test ID 23626 REF: Skandia, Inc. Test Plan # 5823 Rev IR Dated: 05/12/00 For PN's 5823-1, 5823-2, 5823-3, 58234 5823-5 & 58234 SKANDIA, INC. DAX GRAPHITE/POLY 26 MD EDELISI LEATHER ROYAL HIDE RH323 CUSTOM LT. GRAY DYE LOT AFI.00 . GARP,EIT LEATHER C-616 CHATHAM SEAFOG DYE LOT 67296 ICF/UNIICA VAEV FABRIC 917 COLOR 81 CRANBROOK CRANBROOK GREY ' TREATED AT SYNCRO REF. JOB 00-032 VAN NUYS AWNING CO. ARABIAN COTTON ARMY DUCK TREATED AT SYNCRO REF. JOB 00-032 SKANDIA, INC. NOMEX BATTING ' • ......-- PURPOSE OF DMA DEMONSTRATION OF COMPLIANCE WITH MATERIAL FLAMMABILITY REQUIREMENTS APPLICABLE REQUIREMENTS (list specific sections) FAR 25.853 (c) Appendix F Part)] Amendment 25-83 FAR 25.853 (a) Appendix F Part I (a) (1) (ii) CERTIFICATION -Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached shorts numbered have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. ecommend approval of these data I (We) Therefore Approve these data ,. TURE(S) OF D _ NATED ENGINEERING REPRESENTATIVE DESIGNATION NUMBER(S) CLASSIFICATION(S) A-El 1 DERY-405020-CE Structural Special Judy oggs FAA Form 81104 (11-70) SUPERSEDES PREVIOUS EDITION SDNYGIvl_02753884 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240806 EFTA01326399 SDNY_GM_02753885 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240807 EFTA01326400 • SKAND1A, lnc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 SYNCRO AIRCRAFT INTERIORS, INC. TEST PLAN #5823 REV IR SKANDIA WO #45812-00 GULFSTREAM GIV S/N 1085 DEMONSTRATION OF COMPLIANCE OF AIRCRAFT SEAT CUSHION ASSEMBLIES TO THE FIREBLOCKING REQUIREMENTS OF FAR 25.853 (C) AMENDMENT 25-83 DATE: REVISION NO. EFFECTIVE PAGE DESCRIPTION 5-12-00 IR PREPARED BY: DATE: S - 7- 7-CD° CHECKED BY: DATE: 5708/0 DICK LAUGHLIN APPROVED DATE: 5 --i -OD PAGE: 1 SDNYGlvl02753886 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240808 EFTA01326401 • 0 SDNY_GM_02753887 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240809 EFTA01326402 • SKAND1A, inc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 TEST PLAN 5823 REV IR INDEX OF PAGES REVISION PAGE 1 INDEX OF PAGES 2 MATERIAL LIST 3 TEST SPECIMEN PROCEDURES 4 PRODUCTIONPROCEDURES 5 TEST DRAWING (P/N 5823-1 & 5823-2) 6 TEST DRAWING (P/N 5823-3 & 5823-4) 7 TEST DRAWING (P/N 5823-5 & 5823-6) 8 PRODUCTION DRAWINGS 9-11 FIREBLOCKING FLAMMABILITY TEST RESULTS 12-14 WEIGHT LOSS STRIP CHART 15-17 DAILY CALIBRATION CHART 18 VERTICAL FLAMMABILITY TEST RESULTS 19-27 TRACEABILITY DOCUMENTS 28-40 PAGE: 2 SDNYG1.1_0275388.13 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240810 EFTA01326403 SDNYGM02753889 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240811 EFTA01326404 • SKANDIA, inc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 TEST PLAN 5823 REV IR MATERIAL LIST DRESS COVER: EDELMAN LEATHER ROYAL HIDE RH323 CUSTOM LT. GRAY DYE LOT AFL00 DRESS COVER: GARRETT LEATHER C-616 CHATHAM SEAFOG DYE LOT 67296 DRESS COVER: ICF/UNIKA VAEV FABRIC 917 COLOR 81 CRANBROOK CRANBROOK GREY TREATED AT SYNCRO REF. JOB 00-032 BATTING: SKANDIA, INC. NOMEX BATTING CANVAS: VAN NUYS AWNING CO. ARABIAN COTTON ARMY DUCK TREATED AT SYNCRO REF. JOB 00-032 ADHESIVE: CORAL ADHESIVES CC1025 ADHESIVE FOAM: SKANDIA, INC. DAX GRAPHITE/POLY 26 ILD, 47 ILD & 55 ILD VELCRO: SKANDIA, INC. PBLK1.00L & PBLK1.00H 1' LOOP AND HOOK BLACK PAGE: 3 SDNYGlvl_02753890 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240812 EFTA01326405 SDNY_GM_02753891 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002408 I 3 EFTA01326406 • SKAND1A, lnc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 TEST PLAN #5823 REV IR TEST CUSHIONS: TEST NO. 1 P/N 5823-1 & 5823-2 Test cushion dress covers are fabricated using 50% Edelman Leather Royal Hide RH323 Custom Lt. Gray Dye Lot AFL00 and 50% Van Nuys Awning Co. Arabian Cotton army duck treated at Syncro ref. Job 00-032. Test cushions are fabricated with Skandia, Inc. DAX Graphite/Poly 26 ILD which qualifies the same foam of a higher density. All cushion assembly components are bonded with Coral Adhesives CC1025 Adhesive. Additionally, test cushions have a layer of Skandia Nomex Batting placed between the dress cover and the foam on the seating surfaces only. Test cushion dresscovers wrap over and around foam with the leather velcroing to leather and canvas velcroing to canvas in a window pane fashion. TEST NO. 2 P/N 5823-3 & 5823-4 Test cushion dress covers are fabricated using 50% Garrett Leather C-616 Chatham Seafog Dye Lot 67296 and 50% Van Nuys Awning Co. Arabian Cotton army duck treated at Syncro ref. Job 00- 032. Test cushions are fabricated with Skandia, Inc. DAX Graphite/Poly 26 ILD which qualities the same foam of a higher density. All cushion assembly components are bonded with Coral Adhesives CC1025 Adhesive. Additionally, test cushions have a layer of Skandia Nomex Batting placed between the dress cover and the foam on the seating surfaces only. Test cushion dresscovers wrap over and around foam with the leather velcroing to leather and canvas velcroing to canvas in a window pane fashion. TEST NO. 3 P/N 5823-5 & 5823-6 Test cushion dress covers are fabricated using 50% ICF/Unika Vaev Fabric 917 Color 81 Cranbrook Cranbrook Grey treated at Syncro ref. job 00-032 and 50% Van Nuys Awning Co. Arabian Cotton army duck treated at Syncro ref. Job 00-032. Test cushions are fabricated with Skandia, Inc. DAX Graphite/Poly 26 ILD which qualifies the same foam of a higher density. All cushion assembly components are bonded with Coral Adhesives CC1025 Adhesive. Additionally, test cushions have a layer of Skandia Nomex Batting placed between the dress cover and the foam on the seating surfaces only. Test cushion dresscovers wrap over and around foam with the fabric velcroing to fabric and canvas velcroing to canvas in a window pane fashion. PAGE 4 SDNYGlvl_02753892 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240314 EFTA01326407 • • SDNY_GM_02753893 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240815 EFTA01326408 • SKAND1A, lnc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 TEST PLAN #5823 REV IR PRODUCTION CUSHIONS 6 PAX SEATS Production cushion dress covers-are fabricated using Edelman Leather Royal Hide RH323 Custom Lt. Gray Dye Lot AFL00. Production cushions are fabricated using a combination of different densities of Skandia, Inc. DAX Graphite/Poly with 26 ILD being the lowest density used. All cushion assembly components are bonded with Coral Adhesives CC1025 Adhesive. Additionally, production cushions have a layer of Skandia Nomex Batting placed between the dress cover and foam on seating surfaces only. There is a layer of Van Nuys Awning Co. Arabian Cotton army duck treated at Syncro ref. Job 00-032 bonded to the back side of the back and bottom side of the bottom utilized as a close out fabric. Production cushion dresscovers wrap over and around foam with the dresscover velcroing to the canvas in a window pane fashion. 2 DOUBLE PAX SEATS AND JUMPSEAT Production cushion dress covers are fabricated using Garrett Leather C-616 Chatham Seafog Dye Lot 67296. Production cushions are fabricated using a combination of different densities of Skandia, Inc. DAX GraphiteJPoly with 26 ILD being the lowest density used. All cushion assembly components are bonded with Coral Adhesives CC1025 Adhesive. Additionally, production cushions have a layer of Skandia Nomex Batting placed between the dress cover and foam on seating surfaces only. There is a layer of Van Nuys Awning Co. Arabian Cotton army duck treated at Syncro ref. Job 00-032 bonded to the back side of the back and bottom side of the bottom utilized as a close out fabric. Production cushion dresscovers wrap over and around foam with the dresscover velcroing to the canvas in a window pane fashion. DIVAN Production cushion dress covers are fabricated using ICF/Unika Vaev Fabric 917 Color 81 Cranbrook Cranbrook Grey treated at Syncro ref. job 00-032. Production cushions are fabricated using a combination of different densities of Skandia, Inc. DAX Graphite/Poly with 26 ILD being the lowest density used. All cushion assembly components are bonded with Coral Adhesives CC1025 Adhesive. Additionally, production cushions have a layer of Skandia Nomex Batting placed between the dress cover and foam on seating surfaces only. There is a layer of Van Nuys Awning Co. Arabian Cotton army duck treated at Syncro ref. Job 00-032 bonded to the back side of the back and bottom side of the bottom utilized as a close out fabric. Production cushion dresscovers wrap over and around foam with the dresscover velcroing to the canvas in a window pane fashion. PAGE 5 SDNYGIvl_02753894 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240816 EFTA01326409 0 • SDNY_GM_02753895 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240817 EFTA01326410 *SIGN APPROVAL REQUESS • FAR 25.853 (c) APPENDIX F PART II TEST SPECIMEN DRAWING NO: 5823 WO# 45812-00 REV IR DATED: 05-12-0Q MAKE: GULFSTREAM MODEL: G1V SIN: 1085 SEAT DESIGN TO BE PER ATTACHED: TEST PLAN UPON COMPLETION F CONFORMITY INSP FOR TESTING IN ACCOR APPROVED TEST PROCEDURES AU. TOLERANCES ! .125 SEAT BACK PIN 5823-1 END VIEW BACK CUSHION SEAT BOTTOM P/N 5823-2 c WITHOUT' DRESS COVER END VIEW BOTTOM CUSHION WITHOUT DRESS COVER . -. . COMPOSITOR MANUFACTURER PART NUMBER COLOR DYE LOT FLAME TREATMENT DRESS COVER CUSTOM A LEATHER 50% EDELMAN LEATHER ROYAL HIDE RH223 LT GRAY AFUO DRESS COVER B CANVAS 50% TREATED AT SYNCRO VAN NUYS AWNING CO. ARABIAN COTTON GREY • REF. JOB C0032 ARMY DUCK C BATTING PLACED BETWEEN DRESS COVER AND SKANDIA, INC. NOMEX BATTING WHITE FOAM ON SEATING SURFACES CI FOAM .75 ' SKANDIA, INC. DAX GRAPIETEROLY MAUVE ' 26 MD E FOAM I.75 SKANDIA, INC. DAX GRAPHITE/POLY MAUVE 26 ILD PBLKI.ODL LOOP BLACK F VELCRO V SKANDIA, INC. ' PBLKI.OOH HOOK ALL CUSHION ASSEMBLY COMPONENTS ARE BONDED WITH CORAL ADHESIVES CCI025 ADHESIVE eather ve woes to leather and canvas ve croes to canvas. Materials on backs and bottoms are identical PAGE 6 SDNYGIvl_02753896 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024081S EFTA01326411 SDNYGM02753897 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240819 EFTA01326412 *SIGN APPROVAL REQUEST. FAR 25.853 (c) APPENDIX F PART II TEST SPECIMEN DRAWING NO: 5823 WO# 45812-00 REV IR DATED: 05-12-00 MAKE: GULFSTREAM MODEL: GIV SRN:: 1085 SEAT DESIGN TO BE PER ATTACHED: TEST PLAN UPON COMPLETION OF CONFORMITY INSPECTOR TEST SPECIMENS TO BE SUBMITTED FOR TESTING IN ACCORDANCE WITH FAA APPROVED TEST PROCEDURES ALL TOLERANCES • .12T END VIEW BACK CUSHION SEAT BACK P/N 5823-3 WITH0UT' DRESS COVER SEAT BOTTOM P/N 5823-4 D E F END VIEW BOTTOM CUSHION WITHOUT DRESS COVER COMPOSITOR MANUFACTURER PART NUMBER COLOR DYE LOT FLAME TREATMENT DRESS COVER CHATHAM . A LEATHER 50% GARRETT LEATHER C-61ft SEAFOG 57996 DRESS COVER ARABIAN COTTON TREATED AT SYNCRO B CANVAS 50% VAN NUYS AWNING CO. • ARMY DUCK GREY REF. JOB CO.= ' PLACED BETWEEN DRESS COVER AND C BATTING SKANDIA, INC. NOMEX BATTING WHITE FOAM ON SEATING SURFACES 0 FOAM .75 SKANDIA, INC. DAX GRAPHITEIPOLY MAUVE 2BILD E FOAM 1.75 SICANDIA, INC. DAX GRAPHITEJPOLY MAUVE 2BILD PBLKI.CCL LOOP BLACK F VELCRO 1' SKANDIA, INC. PBLK1.COH HOOK ALL CUSHION ASSEMBLY COMPONENTS ARE BONDED WITH CORAL ADHESIVES CC1025 ADHESIVE Leather velcroes to leather and canvas velcroes to canvas. Materials on backs and bottoms are identical. PAGE 7 SDNYGlvl_02753898 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240820 EFTA01326413 • SDNYGM02753899 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240821 EFTA01326414 •SIGN APPROVAL REQUES. FAR 25.853 (c) APPENDIX F PART II TEST SPECIMEN DRAWING NO: 5823 WO# 45012-00 REV IR DATED: 05.12-00 MAKE: GULFSTREAM MODEL: GIV Sift. 1085 SEAT DESIGN TO BE PER ATTACHED: TEST PLAN UPON COMPLETION OF CONFORMITY INSPFCTIOWTEST SPECIMENS TO FORIESTING2LACCORDANCE WITH FM APPROVED TEST PROCEDURES ALL TOLERANCES ±.1r SEAT BACK P/N 5823-5 END VIEW BACK CUSHION WITHOUT DRESS COVER SEAT BOTTOM P/N 5823-8 g- E ENO VIEW BOTTOM CUSHION WITHOUT DRESS COVER • COMPOSITOR MANUFACTURER PART NUMBER COLOR DYE LOT FLAME TREATMENT DRESS COVER 917 CRANBROOK TREATED AT SYNCRO A FABRIC 9:396 ICPUNIKA VAEV CRANBROOK GREY 81 REF. JOB COCG2 DRESS COVER TREATED AT SYNCRO B CANVAS 50% VAN NUYS AWNING CO. ARABIAN COTTON GREY REF. JOB CO032 ARMY DUCK PLACED BETWEEN DRESS COVER AND C BATTING SKANDIA, INC. NOMEX BATTING WHITE FOAM ON SEATING SURFACES D FOAM .75 SKANDIA, INC. DAX GRAPHITFJPOLY MAUVE 2811.0 E FOAM 1.75 SKANDIA, INC. DAX GRAPHITEIPOLY MAUVE 28 ILD PBUL1.01LOOP BLACK F VELCRO 1' SKANDIA, INC. P8Ua.COH HOOK ALL CUSHION ASSEMBLY COMPONENTS ARE BONDED WITH CORAL. ADHESIVES CC1025 ADHESIVE Leather velcroes to leather and canvas velcroes to canvas. Materials on backs and ottoms are Identical. PAGE SDNYGI.1_02753900 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240822 EFTA01326415 • SDNYGM02753901 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240823 EFTA01326416 8 A r ' 0 ENO VIEW BA CK:AND BOTTOM CLISH/ON PRODUCTION CUSHIONS A. DRESS COVER: EDELMAN LEATHER ROYAL HIDE TYPICAL 6 PAX SEATS RH323 CUSTOM LT. GRAY DYE LOT AFLOO TEST PLAN 5823 B. BATTING: A LAYER OF SKANDIA, INC. WO# 45812-00 NOMEX BATTING PLACED BETWEEN REV IR DRESSCOVER AND FOAM ON SEATING SURFACES ONLY DATE: 05-12-00 C. FOAM CONSTRUCTION: A COMBINATION GULFSTREAM GIV OF DIFFERENT DENSITIES OF SKANDIA S/N 1085 DAX GRAPHITE/POLY WITH 26 ILO BEING THE LOWEST DENSITY USED D. CLOSE OUT FABRIC: VAN NUYS AWNING CO. ARABIAN COTTON ARMY DUCK TREATED AT SYNCRO REF. JOB 00-032 BONDED TO THE BACK SIDE OF THE BACK AND BOTTOM SIDE OF THE BOTTOM CUSHION E. VELCRO: SKANDIA, INC. PBLK1.00L & PBLK1.00H 1- LOOP AND HOOK ALL COMPONENTS BONDED WITH CORAL ADHESIVES CC1025 ADHESIVE THE BURN TEST REQUIREMENT FOR THIS PRODUCTION ARTICLE IS MET BY TEST SPECIMENS 5823-1 & 5823-2 ' PAGE 9 SDNYGIvl02753902 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240824 EFTA01326417 • r = lk. SDNY_GM_02753903 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240825 EFTA01326418 • e A r D I ENO VIEW BACK:AND BOTTOM CUSHION PRODUCTION CUSHIONS A. DRESS COVER: GARRETT LEATHER C-616 CHATHAM TYPICAL 2 DOUBLE PAX SEAFOG DYE LOT 67296 SEATS & JUMPSEAT B. BATTING: A LAYER OF SKANDIA, INC. TEST PLAN 5823 NOMEX BATTING PLACED BETWEEN WO# 45812-00 DRESSCOVER AND FOAM ON SEATING REV IR SURFACES ONLY DATE: 05-12-00 C. FOAM CONSTRUCTION: A COMBINATION GULFSTREAM GIV OF DIFFERENT DENSITIES OF SKANDIA S/N 1085 DAX GRAPHITE/POLY WITH 26 ILD BEING THE LOWEST DENSITY USED D. CLOSE OUT FABRIC: VAN NUYS AWNING CO. ARABIAN COTTON ARMY DUCK TREATED AT SYNCRO REF. JOB 00-032 BONDED TO THE BACK SIDE OF THE BACK AND BOTTOM SIDE OF THE BOTTOM CUSHION E. VELCRO: SKANDIA, INC. PBLK1.00L & PBLK1.00H 1' LOOP AND HOOK ALL COMPONENTS BONDED WITH CORAL ADHESIVES CC1025 ADHESIVE THE BURN TEST REQUIREMENT FOR THIS PRODUCTION ARTICLE IS MET BY TEST SPECIMENS 5823-3 & 5823-2 PAGE 10 SDNYGIv1_02753904 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240826 EFTA01326419 SDNY_GM_02753905 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240827 EFTA01326420 EO/4 SOTT ND VIEW BACA-- CUSH' -.AND PRODUCTION CUSHIONS A. DRESS COVER: ICF/UNIKA VAEV FABRIC 917 COLOR 81 TYPICAL DIVAN CRANBROOK CRANBROOK GREY TREATED AT SYNCRO TEST PLAN 5823 REF. JOB 00-032 WO# 45812-00 B. BATTING: A LAYER OF SKANDIA, INC. DATE: 05-12-00 NOMEX BATTING PLACED BETWEEN REV IR ' DRESSCOVER AND FOAM ON SEATING GULFSTREAM GIV SURFACES ONLY S/N 1085 C. FOAM CONSTRUCTION: A COMBINATION OF DIFFERENT DENSITIES OF SKANDIA DAX GRAPHITE/POLY WITH 26 ILD BEING THE LOWEST DENSITY USED D. CLOSE OUT FABRIC: VAN NUYS AWNING CO. ARABIAN COTTON ARMY DUCK TREATED AT SYNCRO REF. JOB 00-032 BONDED TO THE BACK SIDE OF THE BACK AND BOTTOM SIDE OF THE BOTTOM CUSHION E. VELCRO: SKANDIA, INC. PBLK1.00L & PBLKI.00H V LOOP AND HOOK ALL COMPONENTS BONDED WITH CORAL ADHESIVES CC1025 ADHESIVE THE BURN TEST REQUIREMENT FOR THIS PRODUCTION ARTICLE IS MET BY TEST SPECIMENS 5823-5 & 5823-6 PAGE II SDNYGlvl_02753906 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240828 EFTA01326421 SDNYGM02753907 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240829 EFTA01326422 • SKAND1A, lnc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 Client : SYNCRO AIRCRAFT INTERIORS Date : 05/19/00 Client P.O. Aircraft: GULFSTREAM GIV S/N: 1085 Test Plan 11: 5823 Rev: IR Skandia WON: 45812-00 FIREBLOCKING FLAMMABILITY TEST RESULTS FAR 25.853 (c) Appendix F Part U Amendment 25-83 Conditioning Room: Time In:05/J7/00 Time Out: 05/19/00 Bum Length (Inches) Weigh Loss Part Number Specimen VERT HORIZ-T HORIZ-B (LBS.) cm Al 5823-1 LEATHER/CANVAS 9.0 5823-2 LEATHER/CANVAS 7.5 3.6 0.25 3.9 #2 5823-1 LEATHER/CANVAS 9.2 5823-2 LEATHER/CANVAS 7.7 4.2 0.26 4.2 #3 5823-1 LEATHER/CANVAS 9.2 5823-2 UMBER/CANVAS 7.2 3.8 0.25 3.9 AVERAGE: 9.1 7.5 3.9 0.25 4.0 Materials: Dress Cover 50% EDELMAN LEATHER ROYAL HIDE RII323 CUSTOM LT. GRAY DYE LOT AFL00 50% VAN NUYS AWNING CO. ARABIAN COTTON ARMY DUCK TREATED AT SYNCRO REF. JOB 00-032 Foam: SICANDIA, INC. DAX GRAPHITE/POLY 261W Other SICANDIA, INC. NOMEX BATTING Comments: PAGE: 12 FIREBLK3-6499 SDNYGIvl_02753908 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240830 EFTA01326423 • • SDNY_GM_02753909 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024083 I EFTA01326424 • SKANDIA, Inc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 Client : SYNCRO AIRCRAFT INTERIORS Date : 05/19/00 Client P.O. #: Aircraft: GULFSIREAM GIV S/N: 1085 Test Plan #: 5823 Rev: IR Skandia WO #: 45812-00 FIREBLOCKING FLAMMABILITY TEST RESULTS FAR 25.853 (c) Appirlix F Part II Amendment 25-83 Conditioning Room: Time In:05/17/00 Time Out: 05/19/00 Burn Length Race Weigh Loss Part Number Specimen VERT HORIZ-T HORIZ-B (LBS.) (%) in 5823-3 LEATHER/CANVAS 8.0 5823-4 LEATHER/CANVAS 7.4 2.6 0.26 4.4 #2 5823-3 LEATHER/CANVAS 8.2 58234 LEATHER/CANVAS 7.0 3.4 0.26 4.4 #3 5823-3 LEATHER/CANVAS 8.4 5823.4 LEATHER/CANVAS 7.5 3.7 0.28 4.7 AVERAGE: 8.2 7.3 3.2 0.27 4.5 Materials: Dress Cover 50% GARRETT LEATHER C-6I6 CHATHAM SEAFOG DYE LOT 67296 50% VAN NUYS AWNING CO. ARABIAN COTTON ARMY DUCK TREATED AT SYNCRO REF. JOB 00-032 Foam: SKANDIA, INC. DAX GRAPHtTE/POLY 26 ED Other. SKANDIA, INC. NOMEX BATTING Comments: PAGE: 13 FIREBLK3.6501 SDNYGIv102753910 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240832 EFTA01326425 • • SDNYGM02753911 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240833 EFTA01326426 • SKAND1A, lnc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227.1611 • Fax 815/227-1920 Client : SYNCRO AIRCRAFT INTERIORS Date : 05/19/00 Client P.O. #: Aircraft: GULFSIREAM GIV S/N: 1085 Test Plan ft 5823 Rev: IR Slcandia WO #: 45812-00 FIBEILOCKING FLAMMABILITY TEST RESULTS FAR 25.853 (c) Appendix F Part II Amendment 25-83 Conditioning Room: Time In:05/9/00 Time Out: 05/19/00 Burn Length (Inches) Weigh Loss Part Number Specimen VERT HORIZ-T HORIZ-B (LBS.) (%) #1 5823-5 FABRIC/CANVAS 8.0 5823-6 FABRIC/CANVAS 7.8 3.4 0.26 4.1 #2 5823.5 FABRIC/CANVAS 7.7 5823-6 FABRIC/CANVAS 7.3 3.3 025 3.9 #3 5823-5 FABRIC/CANVAS 8.4 5823-6 FABRIC/CANVAS 8.0 3.7 0.28 4.3 AVERAGE: 8.0 7.7 3.5 0.26 4.1 Materials: Dress Cover: 50% ICF/UNIKA VAEV FABRIC 917 COLOR 81 CRANBROOK CRANBROOK GREY TREATED AT SYNCRO REF. JOB 00-032 50% VAN NUYS AWNING CO. ARABIAN COTTON ARMY DUCK TREATED AT SYNCRO REF. JOB 00-032 Foam: SICANDIA, INC. DAX GRAPIWIFJPOLY 26 ILD Other: SICANDIA, INC. NOMEX BATTING Comments: PAGE: 14 FIREBLIC3-6502 SDNYGIvl_02753912 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240834 EFTA01326427 • • SDNY_GM_02753913 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240835 EFTA01326428 *O.5 MAY 19 2000 7 -p ci f? .3 ..57? 3 - - 6.33 LB BURN LENGTH 6. 33 LB VERT 6. 33 L HORZ-T 7 T- 6. 22 LB HORZ-B - 6. 11 LB Nit 1.60., • 6. 10 LB gialmemiggin 6.09 LB 6.09 LB 6.08 LB 6.08 LB- • 6. 19 LB CURN LENGTH 9. 6. 20 LB VERT 6. 20 LB---HORZ-T 6. 06 LB HORZ B 5.98 LB WT.L0SS LBS. awe 5.96 LB WV % !omegas 5.95 LB 5.94 LB 5.94 LB , 5.94 6. 40 LB BURN LENGTh 6. 40 LB ERT -9 A 6. 40 L HORZ-T 6. 25 LB HORZ B 6. 18 LB 6. 17 LB' 6. 16 LB 6. 16 LB 6. 15 LB 6. 15 LB--- PAGE: 15 SDNY GM 02753914 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240536 EFTA01326429 • • SDNY_GM_02753915 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240837 EFTA01326430 6PA-401 MAY 19 2000 t p (.5--wp3 Ay 5ra-3- 3 5. 95 LB BURN LENGTH 5.95 LB ERT 5.95 LB HORZ-T 5.83 LB HORZ-B 5. 74 LB 5. 71 LB WrLQ$$ LOS. WTian %nal iEro 5. 70 LB 5. 70 LB 5. 70 LB 5. 69 LB 5. 92 LB BURN LENGTH 5. 92 LB VERT - 55. LB 55 90 780 2 LLF WTHu°1410SRZRZ:TBS 5- 68 LB 5.67 LB Valigi--i6er"'"" 5.67 LB 5.66 LB 5.66 LB---- 5. 92 LB BURN LENGTH 5.92 LB VERT = 5. :978 2 = 5.69 LB nuns Las, = 5.67 LB ma 9601se,sers. 5.66 LB 5.65 LB 5. 64 LB 5. 64 LB PAGE: 16 SDNYGIv1_02753916 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 1O, 15, and 17 EFTA 00240838 EFTA01326431 • • SDNYGM02753917 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240839 EFTA01326432 ri4 6 yer MAY 19 2000 fp t)° ,5- ga 3 3-Se ,, 6. 34 LB CU RN LENGTH 6. 34 LB ERT 6.34 L. HORZ-T 7 -cr 6.21 LB HORZ B 6. 12 LB WT.Lpgg LBO.® 6. 10 LB IMT4wq ienws 6. 09 LB 6. 09 LB 6. 09 LB 6. 08 LBO 6. 47 LB CORN LENGTH 6.48 LB __VERT = 6. 48 LB.' HORZT 6.. 2 36 LB wrJER1 - HO t88. 6. 25 LB wT lismsaimmes 6.24 LB 6.23 LB 6.. 23 LB---" 6. 47 LB r URN LENGTH 6. 47 LB VERT = Q ie 6. 47 HORZ-T V/7 6. 35 LB MORZ-B = 6.24 LB WT.LOSS LBO. 6. 21 LB cep 6. 20 LB Yin WM) 6. 20 LB 6. 19 LB 6. 19 LB , " PAGE: 17 SDNYGlvl02753918 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240840 EFTA01326433 SDNY_GM_02753919 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240841 EFTA01326434 SDNY_GI,1_02753920 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240842 EFTA01326435 SDNY_GM_02753921 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240843 EFTA01326436 • SKAND1A, lnc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 Client WO #: 45812-00 SYNCRO AIRCRAFT INTERIORS Date: 04/24/00 7701 WOODLEY AVENUE Test Plan #: 5823 Rev:IR VAN N(JYS CA 91406 PO #: Aircraft: S/N: GULFSTREAM OW 1085 VERTICAL FLAMMABILITY TEST RESULTS FAR 25.853 (a) Appendix F Part I (a) (1) (ii) Conditioning Room: Time In: 04/21/09 Time Out: 04/24/00 Specimen EDELMAN LEATHER ROYAL HIDE RH323 CUSTOM LT. GRAY DYE LOT AFL00 Desc.: Flame Flame Burn Application Time Length Drippings (seconds) (seconds) (inches) (seconds) 12 0.0 0.3 0.0 12 9.2 0.3 0.0 12 10.3 0.3 0.0 Average: 6.5 0.3 0.0 Comments: Vertical (12 sec.) Bum Test: Average Self-Extinguish time may not exceed 15 sec. Average Bum Length may not exceed 8". Average Dripping may not exceed 5 sec. after falling. Passed: Failed : Signed: PAGE: 19 /ERTI2NW-25381 SDNYGlvl02753922 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002 40844 EFTA01326437 • SDNYGM02753923 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240845 EFTA01326438 • SKAND1A, inc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 Client: WO ft 45812-00 SYNCRO AIRCRAFT INTERIORS Date: 05/04/00 7701 WOODLEY AVENUE Test Plan #: 5823 VAN NUYS CA 91406 PO #: Aircraft: S/N: GULFSTREAM OW 1085 VERTICAL FLAMMABILITY TEST RESULTS FAR 25.853 (a) Appendix F Part I (a) (1) (ii) Conditioning Room: Time In: 05/02J$1 Time Out: 05/04/00 Specimen GARRETT LEATHER C-616 CHATHAM SEAFOG DYE LOT 67296 Dese.: Flame Flame Burn Application Time Length Drippings (seconds) (seconds) (melts) (seconds) 12 0.0 0.5 0.0 12 0.0 0.5 0.0 12 0.0 0.6 0.0 Average: 0.0 0.5 0.0 Comments: Vertical (12 sec.) Burn Test: Average Self-Extinguish time may not exceed 15 sec. Average Burn Length may not exceed 8". Average Dripping may not exceed 5 sec. after falling. • Passed: Failed : Signed: PAGE: 20 ✓ERTI2NW-25382 SDNYGlvl_02753924 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240846 EFTA01326439 SDNY_GM_02753925 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240847 EFTA01326440 • SliAND1A, inc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 Client: WO #: 45812-00 SYNCRO AIRCRAFT INTERIORS Date: 04/24/00 7701 WOODLEY AVENUE Test Plan #: 5823 Rev: IR VAN NUYS CA 91406 PO #: Aircraft: S/N: GULFSTREAM GIV 1085 VERTICAL FLAMMABif T triPcT RESULTS FAR 35.853 (a) Appendix F Part I (a) (1) (ii) Conditioning Room: Tithe In: 04/21/00 Time Out: 04/24/00 Specimen VAN NUYS AWNING CO. ARABIAN COTTON ARMY DUCK TREATED AT SYNCRO REF. Des° JOB 00-032 Flame Flame Bum Application Time Length Drippings (seconds) (seconds) (inches) (seconds) Warp Fill Warp Fill Warp Fill 12 0.0 0.0 2.7 2.0 0.0 0.0 12 0.0 4.7 2.4 4.5 0.0 0.0 12 0.0 13.2 2.6 7.1 0.0 0.0 Average: 0.0 6.0 2.6 4.5 0.0 0.0 Comments: Vertical (12 sec.) Burn Test: Average Self-Extinguish time may not exceed 15 sec. Average Burn Length may not exceed 8". Average Dripping may not exceed 5 sec. after falling. Passed:❑ Failed : Signed: PAGE: 21 ✓ERTI2-6308 SDNYGlvl_02753926 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240848 EFTA01326441 • • SDNYGM02753927 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240849 EFTA01326442 • SKAND1A, inc. • Fax 815/227-1920 Illinois 61109 • Phone 815/227-1611 5181 Falcon Road • Rockford, WO #: 45812-00 Client: Date: 03/23/00 SYNCRO AIRCRAFT INTERIORS if: Test Plan 5823 Rev: IR 7701 WOODLEY AVENUE PO it: VAN NUYS CA 91406 S/N: Aircraft: 1085 GULFSTREAM GIV VERTICAL FLAMMABILITY TEST RESULTS FAR 25.853 (a) Appendix F Part I (a) (1) (ii) 1:30PM Time Out: 03/23/00 1:35PM Conditioning Room: Time In: 03/22/00 81 CRANBROOK CRANBROOK GREY TREATED AT Specimen ICF/UNIKA VAEV FABRIC 917 COLOR Desc.: SYNCRO REF. JOB 00-032 Flame Burn Flame Length Drippings Application Time (seconds) (inches) (seconds) (seconds) Warp Fill Warp Fill Warp Fill 1.3 2.6 0.0 0.0 12 0.0 0.0 2.0 1.4 0.0 0.0 12 0.0 0.0 1.9 1.6 0.0 0.0 12 0.0 0.0 1.7 1.9 0.0 0.0 Average: 0.0 0.0 Comments: guish time may not exceed 15 sec. Average Vertical (12 sec.) Burn Test Average Self-Extin ng may not exceed 5 sec. after falling. Burn Length may not exceed 8". Average Drippi Failed : Passed: I ^j PAGE: 22 tERT12-6306 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, and28 17 SDNY15,027539 EFTA_00240850 EFTA01326443 • SDNY_GM_02753929 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024085 I EFTA01326444 • SKANDIA, inc. 815/227.1920 5181 Falcon Road • Rockford. Illinois 61109 • Phone 815/227.1611 • Fax Client: WO #: 47120-00 SKANDIA (PRODUCTS) Date: 04/25/00 Test Plan #: PO #: Aircraft: S/N: STOCK NA VERTICAL FLAMMABILITY TEST RESULTS FAR 25.853 (a) Appendix F Part I (a) (1) (ii) Conditioning Room: Time In: 04/24/00 11:50AM Time Out: 04/25/00 1:00 PM Specimen SKANDIA, INC.: DAX GRAPHITE/POLY FOAM, 1/2", 26 ILD, LOT #03290 Desc.: Flame Flame Bum Application Time Length Drippings (seconds) (seconds) (inches) (seconds) 12 0.0 2.8 0.0 12 0.0 2.9 0.0 12 0.0 2.8 0.0 Average: 0.0 2.8 0.0 Comments: Vertical (12 sec.) Burn Test: Average Self-Extinguish time may not exceed 15 sec. Average Burn Length may not exceed 8". Average Dripping may not exceed 5 sec. after falling. Passed: Failed : Signed: Litz Carin Demus L. PAGE: 23 VERTI2NW-24914 SDNYGlvl_02753930 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240852 EFTA01326445 SDNYGM02753931 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240853 EFTA01326446 • SKAND1A, lnc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227.1611 • Fax 815/227-1920 Client: WO #: 47120-00 SKANDIA (PRODUCTS) Date: 04/25/00 Test Plan #: PO14: Aircraft: S/N: STOCK NA VERTICAL FLAMMABILITY TEST RESULTS FAR 25.853 (a) Appendix F Part I (a) (1) (ii) Conditioning Room: Time In: 04/24/00 II:50AM Time Out: 04/25/00 1:05PM Specimen SKANDIA, INC.: DAX GRAPHITE/POLY FOAM, UT, 26 MD, LOT #03310 Desc : Flame Flame Burn Application Time Length Drippings (seconds) (seconds) (inches) (seconds) 12 0.0 2.0 0.0 12 0.0 2.3 0.0 12 0.0 2.4 0.0 Average: 0.0 2.2 0.0 Comments: Vertical (12 sec.) Burn Test: Average Self-Extinguish time may not exceed 15 sec. Average Burn Length may not exceed 8". Average Dripping may not exceed 5 sec. after falling. Passed: E Failed : Signed: 7G• Carin Demus PAGE: 24 ERT12NW-24915 SDNY_Glvl_02753932 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240854 EFTA01326447 • SDNY_GM_02753933 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240855 EFTA01326448 • SKAND1A, inc. 5181 Falcon Road • Rockford. 111inois 61109 • Phone 815/227-1 Client: 611 • Fax BIS/227-1920 SKANDIA (PRODUCTS) WO #: 44446-00 Date: 02/16/00 Test Plan #: PO #: Aircraft: STOCK S/N: NA VERTICAL_FLAMMABILITY TEST RESULTS FAR 25.853 (a) Appendix F Part Conditioning Room: Time In: I (a) (1) (ii) 02/15/00 3:15PM Time Out: 02/16/00 4:23PM Specimen SKANDIA, INC.: NOMEX THERMAL BATTING, Desc.: PART 135, LOT #02140 Flame Flame Application Bum Time Length (seconds) (seconds) Drippings (inches) (seconds) 12 12.0 2.3 0.0 12 5.3 1.4 0.0 12 0.0 0.9 0.0 Average: . 5.8 1.5 0.0 Comments: Vertical (12 sec.) Burn Test: Ave rage Self-Extinguish time may not Burn Length may not exceed 8". exce Average Dripping may not exceed 5 ed IS sec. Average sec. after falling. Passed: in Failed : Signed: A: t " / 4 9-nte•o-, Carin Demus zNW-23221 PAGE: 25 SDNYGlvi_02753934 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240856 EFTA01326449 SDNY_GM_02753935 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240857 EFTA01326450 • SKANDIA, Inc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227.1611 • Fax 815/227.1920 Client: WO 41724-99 SKANDIA (PRODUCTS) Date: 12/02/99 Test Plan #: PO #: Aircraft: S/N: STOCK NA VERTICAL FLAMMABILITY TEST RESULTS FAR 25.853 (a) Appendix F Part I (a) (1) (ii) Conditioning Room: Time In: 12/01/99 9:30AM Time Out: 12/02/99 10:00 AM Specimen Desc.: SKANDIA, INC.: 1" BEIGE SEW HOOK FASTENER, SBGEI.00H, LOT #11299-lit Flame Flame Burn Application Time Length Drippings (seconds) (seconds) (inches) (seconds) 12 0.0 3.6 0.0 12 0.0 3.4 0.0 12 ' 0.0 3.2 0.0 Average: 0.0 3.4 0.0 Comments: Vertical (12 sec.) Burn Test: Average Self-Extinguish time may not exceed 15 sec. Average Burn Length may not exceed 8". Average Dripping may not exceed 5 sec. after falling. Passed: Failed : Signed: e.i Carin Demus PAGE: 26 VERT12N'W-21424 SDNY_Glvl_02753936 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240858 EFTA01326451 • w SDNYGM02753937 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240859 EFTA01326452 r SKAND1A, lnc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227.1611 • Fax 815/227-1920 Client: WO #: 40478-99 SKANDIA (PRODUCTS) Date: 10/27/99 Test Plan #: PO #: Aircraft: S/N: STOCK NA VVERTICAL FLAMMABILITY TEST RESUt TS FAR 25.853 (a) Appendix F Part I (a) (1) (ii) Conditioning Room: Time In: 10/26/99 2:30 PM Time Out: 10/27/99 2:55PM Specimen Desc.: SKANDIA INC.: LOOP FASTENER, SBGEI.00L, SEW BEIGE I", RUN # 42112 - Flame Flame Burn Application Time Length Drippings (seconds) (seconds) (inches) (seconds) 12 0.0 2.4 0.0 12 0.0 2.6 0.0 12 0.0 2.6 0.0 Average: 0.0 2.5 0.0 Comments: Vertical (12 sec.) Burn Test: Average Self-Extinguish Burn Length may not exceed 8". Average Drippi time may not exceed 15 sec. Average ng may not exceed 5 sec. after falling. Passed: ri Failed : ri PAGE: 27 RTI 2NW-20642 SDNYGkl_02753938 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240860 EFTA01326453 r SDNY_GM_02753939 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240%61 EFTA01326454 flncVclrPNL2V 8189885 2:334263840;9/NCR° PAGE 84 0W02/280.ps-Cbcp:?.0 , PAGE:01 • Teddy & Arthur Edelman, Limited Order Nos 615346 EDELMAN Pick Date: 04/76/2000 28 HawleyvIlle Road. P. O. Pox 110. Hawlei/villa, CT 06440-0110 Tel: (203) 426-3611. Fax: (203) 426-3840 Sold To: Snipped To; ----- Cust No: 003549 WINCRO AIRCRAFT INTERIORS SYNCRO AIRCRAFT INTERIORS VERONICA ALZAREZ 818 901-9828 7701 WOODLEY AVENUE VAN NUYS, CA 91406 7701 .WOODLEV AVENUE USA VAN NUYS, CA 91406 USA Cust. PO No. Order Date Shyer:. & SIsmn Delivery Terms itttrifireTter — oil/26/2000' — GPS7r KIET—":0—D - AYS- OtY-Ord OtY.Shp Item No. Description Color Lot 606.25 0.00 RH323 ROYAL HIDE. CUSTOM LT GRAY AFLOO Special instructions: JOB noo-b32-4.01 - 600 5/F 4.09 - 55 S/F RESHIPMENT TIE TO RMA 615344 NO CLAIMS FOR NATURAL OR VISIBLE DEFECTS ARE TO BE ALLOWED UNLESS MADE WITHIN 5 DAYS AFTER RECEIPT OF GOODS BY SUTER. RESPONSIKLITY OF THE SELLER FOR ( NATURAL DEFECTS WHICH MAY BE VISIBLE IN LEATHER OR FABRICS AS ORIGINALLY SHIPPED. CEASES AFTER SUCH LEATHER DR FABRIC HAS SEEN CUT OR FABRICATED PICKING TICKET - PAGE 1 PAGE: 28 COPT I SDNYGIvl_02753940 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240862 EFTA01326455 • i SDNY_GM_02753941 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240863 EFTA01326456 05/09/2000 88:28 8189885251 SYNCRO PAGE 67 Garen locrhoc Cap:ma:en GARRETT. 1360 MOM Shoot DvDo13, NY 14213.1305 Toknonco.3 500442.7735 L EAT H E R Far 716.862.9301 7164824358 ACKNOWLEDGMENT 1 Natural Selection. Woo Site yomtgarettlealher.com (THIS IS NOT A BILL) 5 O SYNCRO AIRCRAFT INTERIORS H SYNCRO AIRCRAFT INTERIORS 0 ACCOUNTS PAYABLE P RECEIVING 7701 WOODLEY AVENUE 7701 WOODLEY AVENUE 0 VAN ,NUTS, CA 914.06 0 VAN NUYS, CA 91406 EDER DATE CUSTOMER P.O. SEP VIA FOB. TERMS .)3/30/00 09691 PDX.,21 OVERNITE BUFFALO NY NET 15 DAYS MM DUE DATE LOCATION SALES PERSON currincanoN VERONICA 04/03/00 KENM A T INTRS - TONI THOMAS <CA) FAR 25.553 a/b tJANTITY ORDERED DESCRIPTOR Ea QUANTITY SHIPPED 490 I C-618 CERT Chatham Seafog ** CFA APPROVED 3-30-00 .8110-3 Certificate: 67296 . 9. 4/9(0,tio - I Cert GUI.FSTBAM G IV SN 1085 N884CE • • . FOR WAREHOUSE ONLY St , DATE *EKED BY: 3bl/ 0D NECKED BY: - I FOR SELECTING ORUENNO. JARRETT LEATHER !!! I 37210 on MARKED HIDES ARE NOT RETURNABLE PLEASE INSPECT CAREFULLY. SDNY_GM_02753942 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240864 EFTA01326457 SDNY_GM_02753943 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240865 EFTA01326458 cn Ctevx:Ittlars4 W. ea C Utio New co lo( Comae Orrecond. VI!it Caine.NV tos64 PACKING LIST ICE re:14a 0 iCas ID REPRINT rn Locat 01 191902-00 :r:pee CPO Alt LS na Ens ICE Taftville Warehouse H 006594 S 1 018-901-9828 O SYNCRO AIRCRAFT INTERIORS INC. SYNCRO AIRCRAFT INTERIORS INC. 77 D 7701 WOODLEY AVE 7701 WOODLEY AVENUE • VAN NUYS, CA 91406 VAN NUYS, CA 91406 0 0 0 H L J "0 in rn 3 co OROER DATE "USTOMEsi PUN HASECK,ESNO. SHIP DATE SHIPVA tRIV7 GCE • —i tn) < 3/09/00 ! 09567 3/17/00 !UPS Second Day Air Y 3/10/00 rn 0 PEDAL giSTRUCTIOVS ► BEND OT4ORDERED OTY.SAWED KMUSACKCJOBE0i UN BIN= I NEMNO. DESC.1e7MN 0 rn 1 30.00 30.00 .00 YRD 11.78.7 GRANBROOlts CRANBROOZ GREY JJ 30.00 ,220 ,0 2 JOB NO. ED0-032 4.04 , . 7D 0 8 77 5 .>"j CO c0 • F" o2 Ic) -0 J. j V. 195 W T r (T, MAIRENOECTAD DATE R*0 i PICKED DV PAM() CHECKED aY 0- F" NO7E: 1HIS SHIPMEIC HAS BEEN CHECKED TWICE ANY DISCREPANCIES /MST BE REAMED IIAMEDLUELY. N0 CLAIM VALI/EA EMEDMIER5DAYS EFTA01326459 9980tZ00-V.L43 SDNY_GM_02753945 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240867 EFTA01326460 8188885251 SYNCRO PAGE 35 05/89/2000 10:33 • • This is to certify that the materials described below have been flame-retardant treated in order to meet the flammability requirements of FAR 25.853 (b) Amendment 25-32 by: The treatment process used is in accordance with Syncro Aircraft Interiors Process Specification PSOO1. THE FLAME RETARDANT PROCESS USED WILL BE REMOVED AFTER THREE WASHINGS. DRYCLEANING DOES NOT REMOVE RETARDANT. SDNYGlvl_02753946 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240868 EFTA01326461 • • SDNY_GM_02753947 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240869 EFTA01326462 05/09/2000 10:33 818988525/ SYNCRO PAGE 05 , • • • • ranKildaSINCE AWNING 1ST B CO, INC. 5661 SEPULVEDABLVD.,VANNUTS,CA. 91411 - PHONES:752-5607 - FROMLA. 573-3331 COST. ORDERNo. DATE • -7 = • rn --- NAME tr ADDRESS CA11,21O c •c, I C .-.14)4e4m, 5 SOW SY CAD( CAA. cuA dtmA moStAVD. pm cut. C0MINCTCA S CC • 277 0 0 2 QUANTITY • DESCRIPTION PRICE AMOUNT qiris • c,"O6.. AMOUNT '155. -c: TAX LABOR TOTAL 55'i DEPOSIT 555 77 BALANCE DUE AU. CLAIMSMID RETURNEDGOODS MUST BE ACCOMPANIEDBY THIS BILL 107290 RECD BY .1641C1C0.6••20.. 3I4 PAGE: 32 SDNYGlvl02753948 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240570 EFTA01326463 SDNY_GM_02753949 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024087 I EFTA01326464 SYNCRO PAGE 07 8189885251 85/89/2000 10:33 • • This is to certify that the materials described below have been flame-retardant treated in order to meet the flammability requirements of FAR 25.853 (b) Amendment 25-32 by: The treatment process used is in accordance with Syncro Aircraft Interiors Process Specification PS001. THE FLAME RETARDANT PROCESS USED WILL BE REMOVED AFTER THREE WASHINGS. DRYCLEANING DOES NOT REMOVE RETARDANT: SDNY_GM_02753950 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240572 EFTA01326465 SDNYGM02753951 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240873 EFTA01326466 05/09/2000 18:33 8199885251 SYNCRO PAGE 08 / / ..r" • CORAL INDUSTRIES, INC. N?. 19618 10109 SO. SHOEMAKER AVE. SANTA FE SPRINGS, CA 90670-3495 (562) 944-9971 so' Jan. 28, 2000 Sold CVSIODAEAS GROM To SYNCRO AIRCRAFT 9390 .SAISPAAN 7701 WOODLEY AV. TS.% VAN NUYS, CA 91406 Net 30 Shipped To SFS SMAPCO VIA - Pratt' Trkg • • . . • per gal 2 5-gal. pails CC1025A adhesive, Lot #2521A0 20 90 209 00 ..-- Freight & handling charges, 25 88 .4ek FES 2 5 aCe £(0 W. 04 (5-C>- 6( ) 0 For resa e 51:1 i• c ‘i-ne TOTAL 234 88 LEGAL RATE OF INTEREST WILL BE CHARGED ON OVERDUE ACCOUNTS INVOICE PAGE: 34 SDNYGIvl_02753952 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240874 EFTA01326467 • • SDNY_GM_02753953 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240875 EFTA01326468 • SKAND1A, inc. PAGE: 1 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227.1611 • Fax 815/227-1920 ****** INVOICE ****** ORDER NUMBER:0043599 INVOICE NUMBER: 0056911-IN ORDER DATE: 01/26/00 INVOICE DATE: 01/26/00 CUSTOMER NO: 0001650 SOLD TO: SHIP TO: SYNCRO AIRCRAFT INTERIORS, INC SYNCRO AIRCRAFT INTERIORS, INC 7701 WOODLEY AVENUE 7701 WOODLEY AVENUE VAN NUYS CA 91406 VAN NUYS CA 91406 CONFIRM TO: BRENDA CUSTOMER P.O. SHIP VIA F.0.8 TERMS 9388 FED SAVER DAVIS JUNCTION NET 30 1.5% LATE CHARGE ITEM NO. UNIT ORDERED SHIPPED BACK ORD PRICE AMOUNT SKAHC.25 EACH 1.000 .000 1.000 327.930 .000 .25"X56"X48' ENSOLITE AHC WHSE: 002 DAX26.5 EACH 15.000 15.000 .000 14.520 217.800 DAX 26 1/2"X24"X72" F/R FOAM WHSE: 002 LOT NUMBER: 11019-2 15.000 DAX261.0 EACH 15.000 15.000 .000 29.040 435.600 DAX 26 1"X24"X72" F/R FOAM WHSE: 002 LOT NUMBER: 01100-2 15.000 DAX262.0 EACH 20.000 20.000 .000 58.080 1,161.600 DAX 26 2"X24"X72" F/R FOAM WHSE: 002 LOT NUMBER: 11159-2 20.000 DAX471.0 EACH 15.000 .000 15.000 29.040 .000 DAX 47 1"X24"X72" F/R FOAM WHSE: 002 PAGE: 18 PAGE: 35 CONTINUED SDNYGIvl_02753954 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240876 EFTA01326469 SDNY_GM_02753955 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240877 EFTA01326470 • SKAND1A, PAGE: 2 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 ****** INVOICE ****** ORDER NUMBER:0043599 INVOICE NUMBER: 0056911-IN ORDER DATE: 01/26/00 INVOICE DATE: 01/26/00 CUSTOMER NO: 0001650 SOLD TO: SHIP TO: SYNCRO'AIRCRAFT INTERIORS, INC SYNCRO AIRCRAFT INTERIORS, INC 7701 WOODLEY AVENUE 7701 WOODLEY AVENUE VAN NUYS CA 91406 VAN NUYS CA 91406 CONFIRM TO: BRENDA CUSTOMER P.O. SHIP VIA F.O.B TERMS 9388 FED SAVER DAVIS JUNCTION NET 30 1.5% LATE CHARGE ITEM NO. UNIT ORDERED SHIPPED BACK ORD PRICE AMOUNT DAX472.0 EACH 10.000 .000 10.000 58.080 .000 DAX 47 2"X24"X72" F/R FOAM WHSE: 002 DAX55.5 EACH 25.000 25.000 .000 14.520 363.000 DAX 55 1/2"X24"X72" F/R FOAM WHSE: 002 LOT NUMBER: 10259-30 25.000 DAX551.0 EACH 15.000 15.000 .000 29.040 435.600 DAX 55 1°X24"X72" F/R FOAM WHSE: 002 LOT NUMBER: 12209-5 15.000 DAX552.0 EACH 20.000 20.000 .000 58.080 1,161.600 DAX 55 2"X24"X72" F/R FOAM WHSE: 002 LOT NUMBER: 01030-5 15.000 LOT NUMBER: 10259-5 5.000 FR CANVAS/NAT YARD 10.000 10.000 .000 10.000 100.000 FR CANVAS/NAT 64" X 1 YARD WHSE: 002 LOT NUMBER: 11249 10.000 1OMEX BATTING EACH 2.000 2.000 .000 375.000 750.000 PART 135 THERMAL BAT 40"X2OYDS WHSE: 002 LOT NUMBER: 01050 2.000 PAGE: 19 PAGE: 36 CONTINUED SDNYGlvl02753956 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA ()1240878 EFTA01326471 • • SDNY_GM_02753957 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240879 EFTA01326472 cn CORAL INDUSTRIES, INC. co 19618 10109 SO. SI•1OEMAKER AVE. iCl° SANTA FE SPRINGS, CA 90070-3495 rn n (502) 944-9971 H OAK —I Jan. 28 2000 (WO/4n ORDER Sold 9390 -0 lo SYNCRO AIRCRAFT SME5mAN 7a 0 7701 WOOULEi AV. IERAtS rn • VAN NUYS, CA 91406 • Net 30 n F.O.B. —I srs •• Shippod to UWEDVIA rn Pratt Trkg... . •• • • . 0 per gal 70 C 20 90 209 00 rn 2 5-gal. pails CC102.5A adhesive, Lot 112521A0 7J -a Freight & handling charges 25 88 7a 7a w.6 4 507, (51 ) - 6 1 ' ) For resale 5b ' ). Sitlir to TOTAL 234 88 : t: -CO II LEGAL RATE OF INTEREST WILL BE CHARGED ON OVERDUE ACCOUNTS u, P c, STIF- 0 cu CI_ I-s 0880K0O- V.L.43 EFTA01326473 • • SDNY_GM_02753959 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240881 EFTA01326474 • SKAND1A, Inc. PAGE: 3 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227.1611 • Fax 815/227-1920 ****** INVOICE ****** ORDER NUMBER:0043599 INVOICE NUMBER: 0056911-IN ORDER DATE: 01/26/06 INVOICE DATE: 01/26/00 CUSTOMER NO: 0001650 SOLD TO.: SHIP TO: SYNCRO AIRCRAFT INTERIORS, INC SYNCRO AIRCRAFT INTERIORS, INC 7701 WOODLEY AVENUE 7701 WOODLEY AVENUE VAN NUYS CA 91406 VAN NUYS CA 91406 CONFIRM TO: BRENDA CUSTOMER P.O. SHIP VIA F.O.B TERMS 9388 FED SAVER DAVIS JUNCTION NET 30 1.5% LATE CHARGE ITEM NO. UNIT ORDERED SHIPPED BACK ORD PRICE AMOUNT PBGE2.00L EACH 2.000 2.000 .000 33.000 66.000 PSA BEIGE 2" LOOP WHSE: 002 1.007 NUMBER: 11119-PHL 2.000 PBGE1.OOH EACH 3.000 3.000 .000 19.750 59.250 PSA BEIGE 1" HOOK WHSE: 002 LOT NUMBER: 11229-PHL 3.000 PBGE1.00L EACH 3.000 3.000 .000 19.750 59.250 PSA BEIGE 1" LOOP. WHSE: 002 LOT NUMBER: 01050-PHL 3.000 SBGE2.00H EACH 2.000 2.000 .000 15.750 31.500 SEW BEIGE 2" HOOK WHSE: 002 LOT NUMBER: 09298-HL 2.000 PBLK2.00H EACH 3.000 3.000 .000 33.000 99.000 PSA BLACK 2" HOOK WHSE: 002 LOT NUMBER: 01140-PHL 3.000 PBLK2.OOL EACH 3.000 3.000 .000 33.000 99.000 PSA BLACK 2" LOOP WHSE: 002 LOT NUMBER: 08309-PHL 3.000 PAGE: 21 PAGE: 38 CONTINUED SDNYGlvl_02753960 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240882 EFTA01326475 SDNY_GM_02753961 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240883 EFTA01326476 • PAGE: 4 SKAND1A, lnc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax1515/227-192.0 ****** INVOICE ****** ORDER NUMBER:0043599• INVOICE NUMBER: 0056911-IN ORDER DATE: 01/26/06 INVOICE DATE: 01/26/00 CUSTOMER NO: 0001650 SOLD TO: SHIP TO: SYNCRO AIRCRAFT INTERIORS, INC SYNCRO AIRCRAFT INTERIORS, INC 7701 WOODLEY AVENUE 7701 WOODLEY AVENUE VAN NUYS CA 91406 VAN NUYS CA 91406 CONFIRM TO: BRENDA CUSTOMER P.O. SHIP VIA F.O.B TERMS 9388 FED SAVER DAVIS JUNCTION NET 30 1.5% LATE CHARGE ITEM NO. UNIT ORDERED SHIPPED BACK ORD PRICE AMOUNT PBLK1.00H EACH 3.000 3.000 .000 19.750 59.250 PSA BLACK 1" HOOK WHSE: 002 LOT NUMBER: 01050-PHL 3.000 PBLK1.OOL EACH 3.000 3.000 .000 19.750 59.250 PSA BLACK 1" LOOP WHSE: 002 LOT NUMBER: 01050-PHL 3.000 SBLK2.00H EACH 3.000 3.000 .000 15.750 47.250 SEW BLACK 2" HOOK WHSE: 002 LOT NUMBER: 11309-HL 3.000 SBLK2.00L EACH 2.000 .000 2.000 15.750 .000 SEW BLACK 2" LOOP WHSE: 002 SBLX1.00L EACH 2.000 2.000 .000 7.500 15.000 SEW BLACK 1" LOOP WHSE: 002 LOT NUMBER: 09249-HL 2.000 NET INVOICE: 5,219.95 LESS pirWT: .00 PAGE: V60.85 CRT: SALES TAX: .00 INVOICE TOTAL: 5,780.80 SDNYGlvl_02753962 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240884 EFTA01326477 SONYGAL02753963 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240885 EFTA01326478 SKANDIA FLAMMABILITY PICKING LIST FOR TEST CUSHION FABRICATION MATERIALS MATERIALS QTY. LOT# PICKED BY INSPECTED BY DAX GRAPHITE/POLY 26 ILD BURN BLOCK BACKS 6 at- 2Cn DAX.26.75X25 a 033m. . DAX .75" X 18' X 25* DAX GRAPHITE/POLY 26 ILD BURN BLOCK BOTTOMS DAX261.75X20 DAX261.75' X 18" X 20" ...- it ,03n4 6 ig,,,-.41- 5--, ...• SKANDIA NOMEX BATTING 2.5 YDS O7.1 yo Da- THREAD 69 NYLON X 4 .- SKANDIA VELCRO 1' PBLK1.00L & PBLK1.001-I LOOP AND HOOK BLACK 09? 1- frt. 09119-NI- 0 3 ?go HC 4 CORAL ADHESIVES CC1025 ADHESIVE X TEST PLAN # 5823 WORK ORDER # 45812-00 PREPARED BY: JUDY BOGGS SweAO ft 30 S-17-00 it 30 (7-e" 31115 71g PAGE: 40 SDNYGlvl_02753964 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240866 EFTA01326479 SDNY_GM_02753965 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240887 EFTA01326480 ' • U.S. DEPARTMENT OF TRANSPORTATION UAIt FEDERAL AVIATION ADMINISTRATION 04/25/00 •STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIWACA1- I UK AllitA<Ar I ILUNIVUtitti I IlltNIII-Ila I JUN MAKE MODEL NO. TYPE (Altplene, Radio. Helicopter NAME OF APPLICANT etc.) GULFSTREAM OW Mandl; Inc SIN 1085 Anplane SYNCRO AIRCRAFT INTERIORS Ub I UP VAIA IUnN i IFICANON NILE Work Order # FLAMMABILITY TEST RESULTS 46501-00 Test ID 22923 REF: Skaudia, Inc. Test Plan #5902 Rev NEW Dated: 04/17/00 For PN's 5902-1 P/N 5902-1 Test pan* are r X 12' pieces of Knoll, Inc., Fabric 1(1831 Butai Pearl treated at Syncro Ref. Job #00-032. Both the warp and fill . . . of the fabric are tested • Rev A Dated: 04/24/00 For PN's 5902-3 P/N 5902-3 Test panels are 3" X 12" piece's of Bergamo Fabrics., Fabric 1797-1 Lavin treated at Syncro Ref. Job #00-032. Both the warp and fill of the fabric arc tested. ... PURPOSE Or UM A DEMONSTRATION OF COMPLIANCE WITH MATERIAL FLAMMABILITY REQUIREMENTS APPUCABLE REQUIREMENTS 01st specific sections) FAR 25.853 (a) Appendix F Part I (a) (1) (h) CERTIFICATION -Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. ecoromend approval of these data I (We) Therefore Approve these data SIGNATURE(S) OF a. 0 TED ENGINEERING REPRESENTATIVE DESIGNATION NUMBER(S) CLASSIFICATION(S) • —A \ ) DERY-405020-CE Structural Special Judy B ggs AA FOfi51 8110-3 (11.70) SUPERSEDES PREVIOUS EDITION SDNYGIvl_02753966 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240888 EFTA01326481 • • SDNY_GM_02753967 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240889 EFTA01326482 • SKAND1A, lnc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 SYNCRO AIRCRAFT INTERIORS, INC. TEST PLAN #5902 REV A SKANDIA WO# 46501-00 GULFSTREAM GIV S/N 1085 DEMONSTRATION OF COMPLIANCE OF FAR 25.853 (a) APPENDIX F PART I (a)(1)(ii) DATE: REVISION NO. EFFECTIVE PAGE DESCRIPTION 04/24/00 A ALL ADDITIONAL TESTING CHANGED P/N 5902-2 TO 5902-3 04/17/00 NEW PREPARED BQA-i-a- Lei-) DATE: a4-00 JU CO ER CHECKED BY: A:a DATE: le/2- s-70 DICK LAUGHLIN APPROVED B DATE: c4-- D-5" 00 Page 1 SDNY GM 02753968 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 002401390 EFTA01326483 • SDNY_GM_02753969 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240891 EFTA01326484 • SKAND1A, lnc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 TEST PLAN 5902 REV A MATERIAL LIST: FABRIC: KNOLL, INC.: FABRIC K1.831 BUTAI PEARL TREATED ATZYNCRO REF. JOB #00-032 BERGAMO FABRICS: FABRIC 1797-1 LAVINA TREATED AT SYNCRO REF. JOB #00-032 TEST SPECIMENS TEST NO. 1 P/N 5902-1 Test panels are 3' X 17 pieces of Knoll, Inc., Fabric K1831 Butai Pearl treated at Syncro Ref. Job #00-032. Both the warp and fill of the fabric are tested. Test specimens are representative of fabric that will be used as lay aft bulkhead panel covering. TEST NO. 2 P/N 5902-3 Test panels are 3" X 17 pieces of Bergamo Fabrics., Fabric 1797-1 Lavina treated at Syncro Ref. Job #00-032. Both the warp and fill of the fabric are tested. Test specimens are representative of fabric that will be used as decor panel covering. Page 2 SDNYGlvl02753970 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240892 EFTA01326485 SDNY_GM_0275.71 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240893 EFTA01326486 i tESIGN APPROVAL REQUEST • FAR 25.853 (a) APPENDIX F PART I (a)(I)(ii) TEST SPECIMEN DRAWING NO: 5902 WO #46501-00 REV A DATE: 04/24/00 MAKE: GULFSTREAM MODEL: GIV S/N: 1085 DESIGN TO BE PER ATTACHED: TEST PLAN UPON COMPLETION OF CONFORMITY INSPECTION TEST SPECIMENS TO BE SUBMITTED FOR TESTING IN ACCORDANCE WITH FAA APPROVED TEST PROCEDURES ALL TOLERANCES +/- .030 INCH PANEL 5902-1 2' A 3' COMPOSITION MANUFACTURER PART NUMBER COLOR FLAME TREATMENT A FABRIC KNOLL, INC. K1831 PEARL SYNCRO REF. JOB BUTAI 00-032 ' Page 3 SDNYGIvl_02753972 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240894 EFTA01326487 SDNY_GM_02753973 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240895 EFTA01326488 • • DESIGN APPROVAL REQUEST FAR 25.853 (a) APPENDIX F PART I (a)(0(ii) TEST SPECIMEN DRAWING NO: 5902 WO #46501-00 REV A DATE: 04/24/00 MAKE: GULFSTREAM MODEL: GIV S/N: 1085 DESIGN TO BE PER ATTACHED: TEST PLAN UPON COMPLETION OF CONFORMITY INSPECTION TEST SPECIMENS TO BE SUBMITTED FOR TESTING IN ACCORDANCE WITH FAA APPROVED TEST PROCEDURES • ALL TOLERANCES +1- .030 INCH PANEL 5902-3 12" 3" COMPOSITION MANUFACTURER PART NUMBER COLOR FLAME TREATMENT A FABRIC BERGAMO FABRICS 1797-1 MULTI- SYNCRO REF. JOB LAVINA GREY 00-032 Page 4 SDNYGlvl02753974 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240896 EFTA01326489 r SDNY_GM_02753975 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240897 EFTA01326490 A A. KNOLL, INC. FABRIC K1831 PRODUCTION DRAWING BUTAI, PEARL TREATED AT TYPICAL LAV AFT BULKHEAD SYNCRO REF. JOB 00-032 COVERING TEST PLAN 5902 REV A DATE: 04/24/00 WO# 46501-00 GULFSTREAM GIV S/N 1085 BURR TESTREQUIRSHNT FOR THIS PRODUCTION AR77CLE ISME7'BY ZESTSPECIME'5902-I Page 5 SDNYGlvl_02753976 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240898 EFTA01326491 • SDNYGM02753977 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240899 EFTA01326492 A B. BERGAMO FABRICS: FABRIC 1797-1 PRODUCTION DRAWING LAVINA TREATED AT TYPICAL DECOR PANEL SYNCRO REF. JOB 00-032 COVERING TEST PLAN 5902 REV A DATE: 04/24/00 WO# 46501-00 GULFSTREAM GIV S/N 1085 BURN TES7'REQUTREVENT FOR THIS PRODUCTION ARTICLE1Sil&T BY SPECAIFJ15902-3 Page 6 SDNY GM 02753978 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024090() EFTA01326493 • • SDNY_GM_02753979 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024[1901 EFTA01326494 • SKAND1A, lnc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 Client: WO #: 46501-00 SYNCRO AIRCRAFT INTERIORS Date: 04/18/00 7701 WOODLEY AVENUE Test Plan #: 5902 Rev: A VAN NUYS CA 91406 PO ft: 09724 Aircraft: • • S/N: GULFSTREAM GIV 1085 VERTICAL FLAMMABILITY TEST RESULTS FAR 4853 (a) Appendix F Part I (a) (1) (ii) Conditioning Room: Time In: 04/07/00 Time Out: 04/18/00 Specimen P/N 5902-1 Desc;• Test panels are 3" X 12" pieces of Knoll, Inc., Fabric K1831 Butai Pearl treated at Syncro Ref. Job #00-032. Both the warp and fill of the fabric are tested. Flame Flame Bum Application Time Length Drippings (seconds) (seconds) (inches) (seconds) Warp Fill Warp Fill Warp Fill 12 0.0 0.0 2.3 2.6 0.0 0.0 12 0.0 0.0 2.6 2.6 0.0 0.0 12 0.0 0.0 2.5 2.9 0.0 0.0 ' Average: 0.0 0.0 2.5 2.7 0.0 0.0 Comments: Vertical (12 sec.) Bum Test: Average Self-Extinguish time may not exceed 15 sec. Average Bum Length may not exceed 8". Average Dripping may not exceed 5 sec. after falling. Passed: Failed : ri Signed: • Page 7 VERT12-6124 SDNYG1.1_02753980 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002 40902 EFTA01326495 0 0 SDNY_GM_02753981 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240903 EFTA01326496 • SKAND1A, inc. 5181 Falcon Road • Rockford, Illinois 61109 • Phone 815/227-1611 • Fax 815/227-1920 Client: WO #: 46501-00 SYNCRO AIRCRAFT INTERIORS Date: 04/25/00 7701 WOODLEY AVENUE Test Plan it: 5902 Rev: A VAN NUYS CA 91406 PO #: 09724 Aircraft: SIN: GULFSTREAM OW 1085 VERTICAL FLAMMABILITY TEST RESULTS FAR 2_5.853 (a) Appendix F Part I (a) (1) (h) Conditioning Room: Tine; In: 04/24/00 9:00AM Time Out: 04/25/00 11:00AM Specimen P/N 5902-3 Desc.•• Test panels are 3" X 12" pieces of Bergamo Fabrics., Fabric 1797-1 Lavine treated at Syncro Ref. Job #00-032. Both the warp and fill of the fabric are tested. Flame Flame Burn Application Time Length Drippings (seconds) (seconds) (inches) (seconds) Warp Fill Warp Fill Warp Fill 12 0.0 0.0 0.9 0.7 0.0 0.0 12 0.0 0.0 0.8 0.9 0.0 0.0 12 0.0 0.0 1.0 0.8 0.0 0.0 Average: 0.0 0.0 0.9 0.8 0.0 0.0 Comments: Vertical (12 sec.) Bum Test: Average Self-Extinguish time may not exceed 15 sec. Average Burn Length may not exceed 8". Average Dripping may not exceed 5 sec. after falling. Passed:❑ a Failed : Sign Page 8 ✓ERT12-6125 SDNYGIvl02753982 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002 40904 EFTA01326497 SDNY_GM_02753983 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240905 EFTA01326498 in Page: 2 C Sold To: SYNCRO AIRCRAFT INTERIORS INC CO 770I WOODLEY AVE Knoll, ins Invoice VAN NUYS CA 91406 Knoll Invoice Number Date n H 581029 03/24/00 Purchase Order No. 09638 Purchase Order Release 7a Ln/ 0 Shp Dt Pattern Description Qty List Price Discount Unit Net Price Extended Price 1.000 X1831 BUTAI, PEARL 4.000 54.00 .00 54.00 • 216.00 Per YD Shipped Via: UPS Shipped Date: 32400 B.O.L.: 110248090000046 • n-i 2.000 SHTX Shipping & Handling.- Textile 29.000 \ 1.00 .00 1.00 29.00 Per BA 0 Merchandise Total: 245.00 7:3 C 7z) 7D 7D in • 02 'O ,tri ,E 2 Sales Tax Total Order e, Net Due 04/23/00 Tax Rt 8.250 17.82 262.82 Currency: USD Terms Nital 30 DAYS C/- **-4 4a EFTA01326499 SDNYGM02753985 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240907 EFTA01326500 This is to certify that the materials described below have been flame-retardant treated in order to meet the flammability requirements of FAR 25.853 (b) Amendment 25-32 by: SONY_GM_02753986 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002 40908 EFTA01326501 • • SDNY_GM_02753987 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240909 EFTA01326502 • BERGAMO • FABRICS INVOICE DI 031063 INVOICE * 7 Win 22ND Sr. 2Nu FLOOs inw nits NY 10010 TRANSACTION # FAX 212-462-1080 • 695232-00 ill 212-•02-1010 DATE . 03/29/2000 SOW TO SHIP TO . SYNCRO AIRCRAFT 'SYNCRO AIRCRAFT 7701 WOODLEY AVENUE 7701 WOODLEY AVENUE . VAN NUYS CA 91406, VAN NUYS CA 91406 VERONICA VERONICA/ Ac II "116E-1532 • 7Rffd 3/1/93 CUSTOMER P.O. SALESMAN SNOVIROOM DATE SHIPPED SNIPPED VIA TERMS .50 32015 03/29/2000 FEDEX IPD PROFORMA ITEM NO. DESCRIPTION QUANTITY UNIT PRICE AMOUNT 111#1-:.L. LHVANH/ 14 IOW 111.1...i. /4/10 QTY SHIPPED: 14.00 1795-2 LINUS/ 2.00 95.00 190.0E QTY SHIPPED: 2.00 MATERIAL DISCOUNT MISCELLANEOUS FREIGHT& SALES TAX AMOUNT PAID HANDLING 1660.00 37.50 PAGE 1 ALL ORDERS SHIPPED VIA FEDEX INTERNATIONAL PRIORITY DIRECTDISTRIBUTION'" SERVICE FecEx ORIGINAL SDNYGlvl02753988 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002409 10 EFTA01326503 • • SDNY_GM_02753989 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002409 I I EFTA01326504 This is to certify that the materials described below have been flame-retardant treated in order to meet the flammability requirements of FAR 25.853 (b) Amendment 25-32 by: SONY_GM_02753990 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002409 1 2 EFTA01326505 r • SDNYGM02753991 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002409 13 EFTA01326506 MAY-26-2000 FRI 11:05 AN SCOTT GROUP FAX NO. 616 954 9600 P. 02 • M3.712 P.3/3 MAY.26. 2020 9: 47AN DUNI, AVIATION us DEPARTMENT OF TRANSPORTAMON TAM POEM AMMAN ION 05126/00 STATEMENT OF COMPLIANCE WITH THE FEDERATL AVIATION REGULATIONS ADMITTRA OF Al CRAFT COMPONENT ID FICA- 10N moos Haw THE (MAWS, Ruda HoAtepfe0 NAM OP APPUCAM MAKI. OULFSTREAM AIRPLANE SYNCRO AIRCRAFT amMS MENTIFICATOR TITLE UST OF DATA 0120 SCOTT GROUP CUSTOM CARPETS 0 W16146M GLENCOE O.T. 100% WOOL CARPET DYE LOT 0 333118 PURPOSE OP DATA DEMONSTRATION OF COMPLIANCE WITH FAR MATERIAL FLAMMABILITY REQUIREMENTS APPIJOAKEREQUFREMENT6 (1.61woenacos; FAR MCI (a) AppeadtiR Part I I a )(fi( It ) 12 SECOND VERTICAL BURN MT. cmenrionoN Abider %Ape/ fl uted by direction of tho Adrtinistralor and In accordance WM conditions and limitations of eppointnent under Part 183 of the Federal Aviation .Rnelgeris. data geed above and on attached shoots fl ied wth applicable have been examined ifl accordance with established macadam and found to comply requhemenla of th• Sand Aviation Rognaflons. toreforo 0 RecorMand /pp:OW of those data I Mon AMINO them debt Ci motanueem OF DillinittalTD ramorpeto anttItsettrenvoMI PCSIONCRON MANURES) CIATSVICA110141) rga# 09C . MA DERTMcascg FlAMMAIOLITY it/ ode skis FAA Form 81104 (1140) SUPERSEDES PREVIOUS EDITION SDNYGIvl02753992 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240914 EFTA01326507 SDNYGM02753993 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002409 15 EFTA01326508 Test Number: 991342-1 4: 'independent Textile I rdt g" P.O. Box 1948 Service, Inc. 1503 Murray Ave. Dalton, Georgia 30722-1948 • Phone 706-278-3013 • Fax 706-272.7057 • E-mail: ittslab@daltonmet TEST REPORT Customer Scott Group July 16, 1999 Subject "DOT, FM Title, 14, Part 25 - Airworthiness Standards: Transport Category Airplanes, Paragraph 25.853, Compartment Interiors, Sub-Paragraph (a) Vertical Flammability. ITTS's Certificate of Authority (DER) Designation No. SO.602. Sample Identification: Style: 333101 Town & Country P.O.# 09536 Backing: Wide Cotton Back SCOTT GROUP# 333118 SIZE: 30sqyd!s PIECE: lofl all. TEST RESULTS: ,FlarneTime - ':.. PINSVOR:::'7:-”:, ,; -..-ARRligtro- -. : .Fffimean9-. - :. - PfieeitiO . Pgri) 4M.41! • • .. • . (sechnds). - (Seconds) (seconds) (inches) Length 12 0 0 0 Length 12 0 0 0 Length 12 0 0 0 . „.. . .: • ,-.49010g0)_ - : .; _ ;v.'. -: . - 0; .7: 0 Width 12 0 0 0 Width 12 0 0 0 Width 12 0 0 0 0 Average -• lg - - 0 0 TEST REQUIREMENTS: (PASSES) Maximum Flame Time = 15 Seconds Maximum Flame Time Drippings = 5 Seconds Maximum Burn Length = 8 Inches L Kent Suddeth Executive Vice President Our letters and repot an forth culusive use ofat caucus althorn they an eddressed. and that communication toarryotbas or the useofthe name oflatlependentTaillaestingSark;Inc..must restive currier wrfuenapron/. °uction and rqxctsapply ocily to the uncle used edamnot ntoessarily indicative orate qualities orapparendyidaileal or semauproduct The marts tadam and the nameofthe!navels:lent Tails TeitingService.the..ste not tobe usedunderany tiro:Want:1ln advatisk,g tothepoen! public. L/42 10IA (6A9) - -----, . • • SDNYGIvl_02753994 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240916 EFTA01326509 SDNYGM02753995 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002409 I 7 EFTA01326510 . U.S. DEPART/MR*OF TRANSPORTATION W DATE . FEDERAL AVIATION ADMINISTRATION May 08, 2000 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION AKE MODEL NO. TYPE (Airplane. Radios Helicopter. etc.) NAME OF APPUCANT .oULFSTFtEAM G-IV Airplane PETERSEN AVIATION AEROSPACE UST OF DATA IDENTIFICATION 1171E DOCUMENT' DA-G1085 Rev. "NC" STRUCTURAL SUBSTANTIATION - MINOR MODIFICATION TO 3- PLACE Dated: 5-08-2000 DIVAN, LH FWD. DRAWING: 50100-1085 Rev. "NC" DIVAN MODIFICATION G-IV SIDE FACING Dated: 5-02-2000 This approval indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and subparagraph listed below as Applicable Requirements.' (Compliance to additional regulations not listed here may be required.) This form • (does not) constitute FM approval of all the data necessary for substantiation of compliance to necessary requirements for the entire alteration/repair. (DETAIL DESIGN AND STRUCTURAL APPROVAL ONLY) • PURPOSE OF DATA TO SUBSTANTIATE THE MINOR MODIFICATION TO EXISTING 3-PLACE DIVAN ASSEMBLY ON GULFSTREAM G-IV AIRCRAFT, SIN 1085 ONLY ' ' APPUCABLE REQUIREMENTS (List specific sections) FAR 25.301, 25.303, 25.305, 25.307, 25.561, 25.603, 25.605, 25.607, 25.609, 25.613 and 25.789. CERTIFICATION - Under authority vested by dinmion of the Administrator and at accordance with conditions and limitations of appointment under Part NU of the Federal Aviation Regulations, data listed above and on attached sheets numbered ban boas examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. = Recommend Approval of these data I 04) Matron El Approve those data SIGNATURE'S) OF DESIGNATED ENGINEF_FLING REPRESENTAINEfs) DESIGNATION NUMBER(S) CLASSIFICATION X/c,CZIZZIZel d Ved.477r4d-err‘ -- DERT-605434-NM Structures Howard L Patterson FAA Form 8110-3 !11.701SUPERSEDES PREVIOUS EDITION GPO 901413 SDNYGlvl02753996 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240918 EFTA01326511 • SDNYGM02753997 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240919 EFTA01326512 IV mar AIRCRAFT MODEL• GULFSTREAM G-IV AIRCRAFT REPORT NO. DA-G1085 DATE: 05-09-2000 REV: NC DYNAMO AVIATION STRUCTURAL SUBSTANTIATION- MINOR MODIFICATION TO IDOST1NG 3 -PLACE, DIVAN ASSEMBLY PREPARED BY: SHAHNAZ GALANTE 05-09-2000 APPROVED BY: HOWARD PATTERSON , 05-09-2000 REV DATE DESCRIPTION SDNYGM_02753998 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240920 EFTA01326513 SDNY_GM_02753999 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240921 EFTA01326514 TABLE OF CONTENTS I) References 2) Introduction 3) Structural substantiation — LH Fwd Divan modification Page 1 DA-G1085 Rev NC 05-08-2000 SDNYGIvl_02754000 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240922 EFTA01326515 SDNY_GM_02754001 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240923 EFTA01326516 1) REFERENCES 1 MIL-HDBK-5F Metallic Materials and Elements for Aerospace Vehicle Structures. 2 FAR 25. Page 2 DA- G1085 Rev NC 05-08-2000 SDNY GM 02754002 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240924 EFTA01326517 SDNY_GM_02754003 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240925 EFTA01326518 r • 2) INTRODUCTION This report provides structural substantiation on the modification of the LH Fwd divan on Gulfstream G-IV model aircraft, S/N 1085. The existing three place divan assembly is modified by moving the existing center truss structure aft by 4.75 inches and the fwd truss structure fwd by 4 inches. The center truss structure is connected to the outboard truss structure, however the basic outboard truss design has not changed significantly. The divan framing is made of 6061-T6 SQ tubing (for vertical and horizontal members) and Rectangular tubing for diagonal members. The divan was a TSO item and with this modification, the TSO Tag is removed and the divan is substantiated under a new part no. for the following load conditions. The gust condition of 7.2 G Down and 9.0 G Fwd load. 3.0 g side and 4.5 g up load. Divan new part number is: 50100-1085 I o 40.00- 65.88 1 0 0 fa n VIEW B-B OLD FOOT PATTERN Exism4 a) Page 3 DA- G1085 Rev NC 05-08-2000 SDNYGlvl02754004 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240926 EFTA01326519 • • SDNY_GM_02754005 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240927 EFTA01326520 3) STRUCTURAL SUBSTANTIATION: 3-PLACE DIVAN ASSEMBLY 9.0 O Fwd load Modified 3- Place Divan Weight including cushion, : 78 lbs Occupants : 3 x 170 = 510 lbs Total weight : 510 + 78 = 588 lbs .Total load : 9.0 x •588 = 5;292 lbs Attachment fitting loads The divan is tied down with six seat track fittings(Anchora) to the aircraft seat track. Load per fitting: 5,292 /6=882 lbs (shear) Tension load per fitting: (5,292 lbs x 22 in ) / 2 x 69.87 in = 833 lbs Minimum allowable for Tension for the seat track fitting is : 4000 lbs Minimum allowable for Shear for the seat track fitting is : 2000 lbs 1 MS = 1 —+ 1.05 [(882 / 2000)2 + (833 / 4600 )2] 1/2 X et t'x ( Co ) 40.0 I 69.87 (%) ° (s) 4(5) ° ° (J (t-itotqcmD ConIF Page 4 DA- G1085 Rev NC 05-08-2000 SDNYGlvl02754006 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240928 EFTA01326521 • • SDNYGM02754007 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240929 EFTA01326522 3) STRUCTURAL SUBSTANTIATION: 3-PLACE DIVAN ASSEMBLY 9.0 G Fwd load Cont.d Fwd load on the divan, Outboard frame The Shoulder Harnesses are installed to the outboard divan frame for take off and landing. (The existing configuration). The center truss structurels connected to the outboard truss structure and by moving it to the aft by 4.7 inches resulted in minor redesigning of the outboard truss frame. The changes to the outboard truss structure are that the compression member (a) is longer by 3 inches and the tension member (b) is shortened by 4 inches. Since the basic truss design has not been changed, therefore it is still structurally adequate under fwd load and the change is considered minor. REMOVE LEGS (EX ISM-114G.) A I n tan via to -3 ' Cita ona,4 =WAD tat %IX ar PUY< FV11)..—.) (MODIFIED) Page 5 DA-G1085 Rev NC 05.08-2000 SDNYGlvl_02754008 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240930 EFTA01326523 SDNY_GM_02754009 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024093I EFTA01326524 3) STRUCTURAL SUBSTANTIATION: 3-PLACE DIVAN ASSEMBLY Center inboard/outboard truss structure The center piece moved to the aft and installed back as the original. Fwd . inboard/outboard truss structure The fwd truss structure moved to the most fwd frame. A SQ. Tube bridge is installed between the two top frames (fwd frames) and the existing vertical tube is welded to it and to the base frame. 8 GUSSETS 10 BUSHING 0 groat.. Page 6 DA- G1085 Rev NC 05-08-2000 SDNYGIv1_0275401 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240932 EFTA01326525 SDNY_GM_02754011 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240933 EFTA01326526 31 STRUCTURAL SUBSTANTIATION: 3-PLACE DIVAN ASSEMBLY 7.2 O Down load Pz = 7.2 g x 78 lbs = 562 lbs Load per three truss structures (inboard / out board): 562 lbs / 3 = 187 lbs See the end view (fwd end), load on the vertical post (-1). The post is at 18° Angle. Assume total 187 lbs acting on the -1 tube. Pz = 187 / COS 18° = 197 lbs for SG. Tubing: I= .0324 in4 a A = .2300 in2 L = 12.62 13 inch 1413 /D ai tn) M:177 165 PCR= n2 EI 2 /L 2 VIEW A-A L=13 inch, E= 9.9X 106 PCR= C(712 E x .0324 ) / 132 -4 PCR = 606 lbs MS. = 606 / 197 -1 = + 2.0 -2 10 BUSHING 0 Page 7 DA- G1085 Rev NC 05-08-2000 SDNYGIv102754012 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240934 EFTA01326527 • • SDNY_GM_02754013 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240935 EFTA01326528 3) STRUCTURAL SUBSTANTIATION: 3 PLACE DIVAN ASSEMBLY 7.2 G Down load Cont.(' Strength of the welded joint. The weld area is .176" x .176" x .25" Shear Stress of weld for a 6061-T6 material : 9,000 psi (ref. Lockheed weld design manual). P. = Area x Shear Stress . T .707 S en' \2G Area =tx L • 11 6" P = [(.707 x .176 x .25)1 x 9,000 = 280 lbs weld strength Pz= 197 lbs applied load MS = 280 / 197 -I = + .42 Page 8 DA- G1085 Rev NC 05-08-2000 SDNYGlvl02754014 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240936 EFTA01326529 • • SDNYGM02754015 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240937 EFTA01326530 4 3 2 1 C 4 M =XI MM Row =Man c was APOO .0 C CD V= MORI MOW mlb0 COMM 00100115/11 tatorrou twt L. 07011•01 NM =ACME a UMW, MICR IteaCCI ORMAN Ram Dal WOO CC V Ti. 1 rn n n o H 77 70 0 1. RELOCATE LEGS ON EXISTING H DIVAN TO MAKE ROOM FOR 2 12 rn MAN LIFE RAFTS(61LBS EA), TO n REPLACE ON 12 MAN AND ONE 6 MAN LIFE RAFT. rn 2. CUT LEGGS TO BE RELOCATED CAREFULLY, DO NOT DAMAGE 0 C REMAINING TUBING. 77 3. WELD LEGS PER MIL-W-2219 rn CLASS B, DYE-PEN INSPECT. ALL 70 WELDED AREAS. -o 70 Gl 70 OMMIIIR MS 0511-1 9(T1 waitasmasabinta _ —41 -" 4 -$0 7V X I . 4541-19 B -0 %RIM VA1-11 DIM -8 MR711:. 1- 5 ;OM cr) -7 I'% A' X OM 5XCI 'As") PER 114-1-7:0/4 1. X A. X Of) KV Mt* KR n -!-)Z/4 1 re in -i-70010 -S • 8 1,45. ROL SO l'AC csr K41-11 SO ME KR Vw-l-705/1 Co I' ye', ou SO MI K01-10 KA v•-4M1/1 7 • x 1041-10 'RI NOW OISCROPVI WROACATOR S. , PM WOO PAP, LEVI c) 2 MOM gmG.:eta won, dna 424,2-4011 •••=.0 y l DIVAN MODIFICATION to A C. TAYLOR 5/1/0) A/ 5//11005 cu Ns= GIV SIDE FACING 41/N (480-40 I-- 50100-1085 0_ °,,, P<Y, ASV tee) CM C NOTES: UNLESS OTP.ERMSE SPECIFIED freartivi $.4.1 1/I 1 SAVED AS: Ise I Or 1 1w— 4 3 2• EFTA01326531 • SDNYGM02754017 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240939 EFTA01326532 In 4 3 2 co 4 Cl -O 0 Cl 0 0 -O REMOVE LEGS -O U) VIEW LOOKING OUTBOARD LEFT SIDE OF PLANE BEFORE MODIFICATIONS, 9° REMOVED LEGS NOTED IN BLUE <---AFT FWD N N O 2 MOOS XVI MOIR MIAOW, MINE DIVAN MODIFICATION ON SIDE FACING J -' 501o0—lo&S 1/1 I sno /s: I —.dor 11'w ‘,1 II 3 t 2.' EFTA01326533 SDNY_GM_02754019 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024[1941 EFTA01326534 4 -- tr) 0 z ce I- <▪ iL 0_ co 0 U oo O In L. (.4 G1 ; 3 ▪ Z < --- ‘=' 0 O O c0 0 rnr I n I SDNYGNL02754020 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240942 EFTA01326535 SDNY_GM_02754021 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240943 EFTA01326536 Ln C CO rn 4 3 1 2 1 n H 1SSET ADDED 3 PLACES 0 H rn n H rn 0 O 70 rn 77) -O 587 70 Gl 70 -O O O CO Co (-O O2 B NEW LEG AND ATTACHMENT VYal%Y.0 'O win Lost q 4S 3/4 SCALE I0 DIVAN MODIFICATION tl GIV SIDE FACING o_ 7 50100-1085 — lb L'40 I -S K6 ruc 4 3 ..2 1 EFTA01326537 SDNYGM02754023 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240945 EFTA01326538 VIP MEI S. C. CO O JI Os C) In If) Cll Ifi CI • r, O I Cu 00 r A SONY GI,L 02754024 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240046 EFTA01326539 SDNY_GM_02754025 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240947 EFTA01326540 cr) co Cl H -O 0 0 -9 GUSSET 3 REQUIRED 0 -O -O Go 910.88e C) -12 DOUBLER f-r DIVAN MODIFICATION GIV SIDE FACING g 50100-1085 CD_ 7 r: isvio I... or EFTA01326541 SDNY_GM_02754027 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240949 EFTA01326542 8 I 7 6 I 5 xs mar n “ rm. tam no. s Rolm lo no MI co war.ca stn.= fa. MIN... TRW", =4 SIM 000 DM 141.50.01,41R1,111.11001N frEl KtellI Ma n -0 30.00 0 644,8. 25. n 64.62° -7 DIAGONAL MEMBER 0 19.95 -0 40.7 49.25° 075° 49.2 -6 DIAGONAL MEMBER 3 9.35 42.44° 47.5 lD 7.56° 42.44' p 2 -5 DIAGONAL MEMBER U I ,c,„ EFTA01326543 r SDNY_Gtv1_02754029 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240951 EFTA01326544 In 4 3 2 1 co Cl 12.62 H 4,88 4.06 \-) 71 2 PLS 0 -1 DETAIL Cl -8 GUSSET -7.19 15.00. 00.94 1.50 23.52 0 25.78' 115. 8° -2 DETAIL -3 DETAIL —O 25.08 11.61 6-) -11 DETAIL -O -4 DETAIL V) 1.25 00 00.94 .O 00.62r" N N O -10 BUSHING Nte12800 ...mow., WI OWL II, III 01, Om 1.11411 DIVAN MODIFICATION Iv GM SIDE FACING g 50100-1085 CL (6, 7 i SINEO I". 3 Of 6 riC - 4 3 2 1 IJ In EFTA01326545 SDNY_GM_02754031 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240953 EFTA01326546 • • -4 8 GUSSETS (O 10 BUSHING (O 4- N co 03 A SDNYONL02754032 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240954 EFTA01326547 • • SDNY_GM_02754033 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240955 EFTA01326548 (.1 co n 1 4 3 2 I H 4 4 -O 70 0 A H n H 70 70 B 73 Gl 7J Cr) A Co - 12 DOUBLER WELD TO lO - 3 LEG 2 PLCS VIEW LOOKING OUTBOARD LEFT SIDE O 2 OF PLANE (---AFT FWD I— Jo MAYO " F t= DIVAN MODIFICATION OJ GIV SIDE FACING Cl. - 50100- 1085 .. SOW AS, f se 2 Of 6 PNC 3 2 1 4 EFTA01326549 9c6ortoo-vid9 SDNYGM02754035 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240957 EFTA01326550 lar , iI .3 lei Oil illi . SDNY GM 02754036 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240958 EFTA01326551 • • SDNY_GM_02754037 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240959 EFTA01326552 . ..TT OF TRANSPORTATION U.S. DEPARTIMI W DATE FEDERAL AVIATION ADMINISTRATION May 15, 2000 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio. Helicopter. etc.) NM E OF APPLICANT GULFSTREAM G-IV Airplane PETERSEN AVIATION AEROSPACE LIST OF DATA IDENTIFICATION TITLE - DOCUMENT: • SY-GL1085 Rev. "NC" STRUCTURAL SUBSTANTIATION - TWO 17 INCH LCD MONITOR Dated: 5-15-2000 INSTALLATIONS RH/LH, FWD I AFT AND ENTERTAINMENT SYSTEM MODIFICATION: It This approval indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and subparagraph listed below as 'Applicable Requirements: (Compliance to additional regulations not listed here may be required.) This form (does not) constitute FAA approval of all the data necessary foi substantiation of compliance to necessary requirements for the entire alteration/repair. ,(DETAIL DESIGN AND STRUCTURAL APPROVAL ONLY) PURPOSE OF DATA TO SUBSTANTIATE THE INSTALLATION OF TWO 17 INCH LCD MONITORS AND ENTERTAINMENT SYSTEM MODIFICATION ON GULFSTREAM G-IV AIRCRAFT, S/N 1085 ONLY APPLICABLE REQUIREMENTS (list specific sections) FAR 25.301, 25.303, 25.305, 25.307, 25.561, 25.603, 25.605, 25.607, 25.609, 25.613 and 25.789. CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered • have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. C Recommend Approval of these data I (3.11e) Therefore l= Approve these data . SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION. mania /paraders- DERT-605434-NM Structures Howard L. Patterson FAA Form 8110.3 (11-70) SUPERSEDES PREVIOUS EDITION GPO 901.613 SDNYGlvl02754038 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240960 EFTA01326553 • • SDNYGM02754039 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024[1961 EFTA01326554 • AIRCRAFT MODEL: GULFSTRFAM G-IV • REPORT NO. SY-GL1085 8/N NO. : 1085 DATE: 5-15-2000 SYNCRO AIRCRAFT INTERIORS STRUCTURAL SUBSTANTIATION- 17 INCH LCD MONITOR INSTALLATION RH/LH, FWD/AFT BULKHEAD- MOUNT. AND ENTERTAINMENT SYSTEM MODIFICATION PREPARED BY: SHAHNAZ GALANTE 5-15-2000 APPROVED BY: HOWARD PATTERSON 5-15-2000 REV DATE SDNY GM 02754040 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240962 EFTA01326555 • • SDNY GM 02754041 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240963 EFTA01326556 TABLE OF CONTENTS 1) References 2) Introduction 3) Geometry 4) Structural Substantiation: Fwd and Aft RH/ LH 17" LCD Monitors Installation Page 1 SY-GL1085 Rev NC 5-15-2000 SDNY GM 02754042 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240964 EFTA01326557 • • SDNYGM02754043 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240965 EFTA01326558 1) REFERENCES 1 MIL-HDBK-5F Metallic Materials and Elements for Aerospace Vehicle Structures. 2 FAR Part 25 Page 2 SY-GL1085 Rev NC 5-15-2000 SONY GM 02754044 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240966 EFTA01326559 • • SDNYGM02754045 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240967 EFTA01326560 2) INTRODUCTION This report provides structural substantiation for the installation of twol7 inch LCD Monitors. One is mounted onto the Aft Bulkhead of the Fwd RH existing storage Cabinet (STA193) and the second one is mounted onto the fwd side of the Aft LH Bulkhead(STA442). The Aft LH Bulkhead is more like a divider than a load carrying Bulkhead for the existing Galley. The new 17 inch LCD monitors are installed in place of existing 14 inch monitors in exact locations. Also in the Fwd LH Comp (STA193). One Panasonic VCR Model PV4662, Weight 7.0 lbs is exchanged with DVD player model PS86802 , Weight 7.0. The subject installation and modification is on Gulfstream G-IV model aircraft SIN 1085. The subject installation is analyzed for the most critical load conditions. The following load factors are used herein: 9.0 G Fwd 7.2 G Down 4.5 G Up 3.0 G SIDE All the critical parts have been investigated, those not shown are considered not critical. Page 3 SY-GL1085 Rev NC 5-15-2000 SDNYGIvl_02754046 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240968 EFTA01326561 • • SDNY_GM_02754047 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240969 EFTA01326562 31 GEOMETRY- FWD/AFT RB/LR Bulkhead Mount, 17" LCD Monitor Installation t.P /404 434. •e./r Nett law. ovr-eor art,Pith 0140 JO- tig„.a..12 Ebor ..3(ob ;opt ALIJA. iteu4Fbecibby cOrar Tritirt4ti Seal gevii LCD monin-00- rto Sand °La Mon/ wog- i7-‘43s. *" saitsch.I 7 A041.e £ts4Y Page 4 SY-GL1085 Rev NC 5-15-2000 SDNYGIvl_02754048 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240970 EFTA01326563 • • SDNYGM02754049 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024097I EFTA01326564 • • 4) STRUCTURAL SUBSTANTIATION- FWD/AFT R.H/LH Bulkhead Moon 17" LCD MonitorInstallation The subject LCD Monitor is installed on the Aft Bulkhead of the RH Fwd Cabinet with four Z- Brackets, top and bottom, Inb'd/Outed. The Z- Brackets are installed to the bulkhead with two #10-32 screws and NAS1836-13 inserts. Fwd LCD Installation WEIGHTS: New 17 inch LCD Monitor, Model # 170MP Total : 12.0 lbs Old 14 inch LCD Monitor. Weight 7.9 lbs 9.0 G Fwd load Px = 9.0 x 12 = 108 lbs total fwd load Load per 2-Bracket Px = 108 / 4 = 27 lbs Z- Bracket Supports. 2024-T3. t = .063" L = 5.0 in Rt = Px (2.0 in) / .50 in Rt = 108 lbs (tension in insert) Load per fastener. P = 108 /2 = 54 lbs (Tension) Bending stress of 2-Bracket, jb= 6M /b 12 width, b = 5.0" Max bending moment : 27 lbs x 1.0 in = 27 in-lbs .fro= 6 x27/5.0 in x.0632 =8,163 psi Ftu = 62000 psi for 2024-T3 (ref 1) MS = 62,000 / 8,163 -1 = HIGH Page 5 SY-CL1085 Rev NC 5-15-2000 SDNY Clvl 02754050 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240972 EFTA01326565 • • SDNYGM02754051 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240973 EFTA01326566 • • 4) STRUCTURAL SUBSTANTIATION- FWDIAFT RA/LB Bulkhead Mount, 17"_LCD Monitor Installation Cont'd Fwd LCD Installation. Contd 7.2 G Down load Pz = 7.2 gx (12.0 lbs ) = 86.4 lbs Take the overturn by the upper and lower bracket Rrop= - Racer= (86.4 lbs x 2.0" ) / 12.88" Rrop = - Raman = 13.42 lbs Load per upper and lower bracket Down load Pz bears on the bottom Z-Bracket Rzsocke = 86.4 lbs Load per inserts (NAS 1836-3) Shear load: 86.4 lbs / 2 = 43 lbs Check bendino of the Z- Bracket Bending stress, fb= 6M /b tz width, b = 5.0" Max bending moment 86.4 lbs x 1.0 in = 86.4 in-lbs fb=6 x86.4 / 5 in x.0632 = 26,122 psi Ftu = 62000 psi for 2024-T3 (ref 1) gst...(astree,,) • MS=62,000/26,122 -1= +13 Esti 1.5 a Aft load condition! Px = 1.5 x 12 =18 lbs (this load bears on the aft bulkhead) Page 6 SY-GL1085 Rev NC 5-15-2000 SDNYGlvl_02754052 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002 40974 EFTA01326567 • • SDNY_GM_02754053 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240975 EFTA01326568 • 4) STRUCTURAL SUBSTANTIATION- FWD/APT RHJLII Bulkhead Monnt. 17" LCD Monitor installation Coned Fwd LCD Installation. Contd Check flange bending of the Z- Bracket Bending stress, fb= 6M /b t2 width, b = 5.0" Max bending moment: 13.42 lbs x. .50 in = 7.0 in-lbs fb= 6)(7.0 15 in x .0632 = 2,116 psi Ftu = 62000 psi for 2024-T3 (ref 1) MS = HIGH Check inserts. The largest Shear load and Tension Load on NAS1836-13: Pt = 54 lbs Ps = 43 lbs (Ref. P5,6) Insert Analysis Core shear allowable from: HEXCEL: 150 psi PALLowASLE = (150)(7t)(11 x .40) = 136 lbs Tension Bearing Allowable = Fen, = 121,000 psi (2024-T3) PALLOwASLE Br = (121,000 psi)(.02)(.451) = 1091 lbs Calculation of Margin of Safety Rs = 43/1091= .040 , R-r = 54/136 = .40 MS = 1/Rs + -1= 1/.040 + .40 = +1.27 Page 7 SY-CL1085 Rev NC 5-15-2000 SDNYGIvl_02754054 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240976 EFTA01326569 • • SDNYGM02754055 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240977 EFTA01326570 ) STRUCTURAL SUBSTANTIATION- FWD/AFT RH/LH Bulkhead Mount, 17" LCD Monitor Installation Cont'd Aft LH LCD Installation WEIGHTS: New 17 inch LCD Monitor, Model # 170MP Total : 12.0 lbs Old 14 inch LCD Monitor. Weight 7.9 lbs.. 9.0 G Fwd load Px = 9.0 x 12 = 108 lbs total fwd load This load bears on the bulkhead (this bulkhead is more like a divider than a load carrying bulkhead for the existing Galley, STA 442.). This Monitor installation is identical to the Fwd RH one shown on pages 4,5,6,7 . Page 8 SY-GL1085 Rev NC 5-15-2000 SDNYGIv1_02754056 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240978 EFTA01326571 0 0 SDNYGM02754057 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240979 EFTA01326572 AIRCRAFT INTERIORS, INC. EMPTY WEIGHT RECORD Aircraft type. Gulfstream GIV Serial # 1085 Registration- N677RP Weight Arm Moment Current Empty Weight from Jan. 28, 00 41887.7 460.95 19308255 Removed R/H 1 singe seat -67.5 172 -11610.0 Removed L/H 2 singe seat • . :96.0 225 -21600.0 Removed R/H 2 single seat -97.5 225 -21937.5 Removed R/H 3 singe seat -68.0 370 -25160.0 Removed R/H 4 single seat -68.5 424 -29044.0 Removed L/H 1 singe seat -68.0 172 -11696.0 Removed L/H 4 double seat - -1175 326 -38305.0 Removed L/H 3 double seat .. -119.0 272 -32368.0 Removed divan cushions -56.0 395 -22120.0 Removed galley linoleum -9.0 458 -4122.0 Removed VCR PV-4662 -8.0 145 -1160.0 Removed LCD Monitor SB1410AAB -7.9 ,151 -1192.9 Removed LCD Monitor SB1410AAB -7.9 443 -3499.7 Installed DVD PS8680Z +9.0 145 +1305.0 Installed LCD Monitor 170MP +12.0 151 +1812.0 Installed LCD Monitor 170MP +12.0 443 +5316.0 Installed R/H 1 singe seat +76.0 172 +13072.0 Installed R/H 2 singe salt +105.0 225 +23625.0 Installed R /1-i 3 singe seat +77.0 370 +28490.0 InstalledR/H 4 singe seat +77.0 424 +32648.0 Installed L/H 1 singe seat +77.0 172 +13244.0 Installed L/H 2 singe seat +105.0 225 +23625.0 Installed L/H 3 double seat +143.0 272 +38896.0 Installed L/H 4 double seat +142.0 326 +46292.0 Installed divan cushions • +67.0 395 +26465.0 Installed galley carpet +18.0 458 +8244.0 New Empty Weight ( May 23, 2000) 42129.9 460.16 19386557.775 43.591/4 MAC Hours: ital Landings: 2111 PREPARED BY: Richard P.Jose 245198915 7701 WOODLEY AVENUE.VAN NUYS,CAUFORNIA 91406 • RioNE 818.901.9828 • Fax 818.988.5251 SDNYGlvl02754058 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240980 EFTA01326573 SDNYGM02754059 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240981 EFTA01326574 MATION.INIPR STANDARD AJAW011111INESS COMRCATEOCIN Nmu . I , 'VrTYLT6-se "rsOLlsoni Fs. Form BICP2 SONY_CA1_02754060 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00240982 EFTA01326575 SONYGM_027 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00240983 EFTA01326576 UNITED STATES CF AMERICA cr) • DEPARTMENT OF TRANSPORTATION-FEDERAL AVLAION ADAENISTRATICN C STANDARD AIRWORTHINESS CERTIFICATE co 1 NATIONALITY AND 2 MANUFACIVRERANDMCCEL 3 AIRCRAFT SERIAL 4 CATEGORY REGISTRATIONMARKS NUMBER N677RP GULFSTRP,AM/GIV 1085 TRANSPORT IS AUTHORITY AND BASIS FOR ISSUANCE Ms sirwaltilnesi IMIRCAle Is Issued pursonl 10 to Federal MINIm AD of 1958 and cerlites that as«Ns ebbs of Issumee. ne Goan lo whr.A &wed Pas been Foxe*, aid Mond lo omform lo the type Oillfleolo therefor. b be b comKon fee eale 0 oPersOn and nos teen ire« to real In. req‘fromans of IRO Oppieable areonshensM DM &Mtn! Mr.ontWesa Cae as mote by Area Elo Me CenvenlIcn of Wanorcnef CM Aw/S:n. MØ fes rried Pne -o Exce~ 73 NONE 0 TERMS AND CCCITIONS Wins son sweerOarenl. mspended ietefied. IX a werineikm dW Y etIrelse eSISEININ4 by IM AdmnblRlp. INS tinvorflass torOlc.IM Is elSecOm as Mop es Oro noi-anence. nnweolot49 ermlnlsnetCR Md Illtealkm> are perfenred In iNcaclanos wln Pals 31. 43. end 91 <I Na Fedensl ASIOn Pernik,g as ndomdelat end ha elnyeAl Is fe~:1 M Ine Wiled DATE OF t331/ANCE REPAESENTA As, p re DESIGNATION NUMBER May 23 2000 L. 1,4O1TER WP-FSDO-01 An ~irk" ~nil^ la ~so al mala ~kola Mr be weal~le by a Y. *a wade, §1M9 am &where« rei 0~ 3 non ai bat THIS CERTIPICATE MUST DE DISPLAYED N THE AIRCRAFT N ACCORDANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS FAA Eon 8100.2 (Rod) APSE:can:Me Fain Sy!~ • JolFarn Foials• 12/19913 e as. EFTA01326577 SDNYGM02754063 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240985 EFTA01326578 .e • ' I T: r •I7 • • Form AOPirked 0 - • ' MAJOR REPAIR tp ALTERATION OMII No 2120.0020 USOerotineni (Airframe, Rowerplant Aro enE0 &Arian 10 ...) For FAA Use ONy • oftroaserrako Fedora Aviation Administnalen id \L\ Office Identification GI_ 13 INSTRUCTIONS: Print or type all entries. See FAR 43.9. F 43 Appendix B.,:and AC 43.9- (or subsequent revision thereof) for instructions and disposition o this form. This report is required by law (49 U.S.C. 1411). Failure-70 report can result in a civil penalty not to exceed $1,000 for each vielationiSection 901 of Federal Aviation Act of 1958). Make Model &airstream Aerospace Cow: GM 1. Aircraft SaiaiNo. Nationality and Regetration Mark 1085 N864CE Name lessikoseroirmistatira rarcs tecia1 ... a) Address iershounariniptatearerkkes) Coca Cola Enterprises Inc. 2500 Windy Ridge Rosy SE 2. Owner Atlanta ,GA 30339-5677 3. For FAA Use On y 4. Unit Identification S Type Unit Make Model Serial No. Repair AJteration X AIRFRAME As described in item 1 above) powERriaa PROPELLER TYPO APPLIANCE Manufacturer G. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. Gulfstream Aerospace Corporation U.S. Certikated Mechanic W6365 Discovery Drive Foreign Certificated Mechanic Appleton, WI 54915 X Certified Repo': Station GIFE100Y Manufacturer D. I certify that the repair and/or alteration made to the tin' (s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein Is this and correct to the best of my knowledge. Date Signature erd iii DEC 1 0 1998 . 7. Approval for Return To Service Pursuant to the authority given persons specified below, the unit Identified In item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and IsPlAPPROVED CI REJECTED FAA FIL Standards Manufacturer Inspection Authorization Other (Spee) Inspector BY FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection Certificate Of Signatur odzed Indi r du DEC 1 0 i898 Designation No. GIFR1OOY FAA Form 337 ozak (CamputerGonended) SDNY_GIvl_02754064 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240986 EFTA01326579 NOTICE • • •• • must be compatible Weight and balance limitation changes shall be entered In the appropriate aircraft record. An alteration conformity with the applicable airworthiness requirements . with all previous alterations to assure continued 8. Description of Work Accomplished completed). (If mom space is required, attach additiOrtal sheets. Identify with aircraft nationally and registration mark and date work Repair Repaired L/H Flap "A" track recess I.A.W. Gulfstream Aerospace Corp. (FAA Approved) Structural Flap "A" track recess Manual Drawing 1169RDCS280 Rev. C dated 41-88, -901 Installation. Repaired R/H substituted with per -904 installation same dwg. Note on -904 install, Sea. NAS1921M05-3 fasteners were NAS1919M0 6-3 and lea. OSMLS100M 04-03 per Gulfstream Service Engineering E-mail transmittal tea. same dwg. dated 12-6-98. Reworked L/H and Ft/H °A" flap tracks per -905 and -906 installation END O Additional Sheets are attached. SDNY_GM_02754065 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240987 EFTA01326580 - • " Fare Approved 0 MAJOR REPAIF I I OMB No.2120-0020 uswparrnw (Airframe, Powerpla . t iptValan curranomwm For FAA Use Only Federal Aviation n id Office IdentificaterGL i 3 Administration -. INSTRUCTIONS. Print or type all entries. See FAR 43.9, FAR-48-Appondi. O. oratA0 43r9al(a subsequent revision thereof) for instructions and disposition of this form. This report Is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1.000 for each violationfSecgon 901 of Federal Aviation Act of 1958). Make. . Model Gulfstream Aerospace Corp. GIV 1. Aircraft Serial No. Natonaity and Regatation Mark 1085 N864CE Name (Ass/rowanfristfailonarrAfca.49) Address (AsgooseorI fayStratiofmakes) Coca Cola Enterprises Icc. 2500 Windy Ridge Pkwy SE 2. Owner Atlanta ,GA 30339-5677 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration X AIRFRAME (As described in Item 1 above) POwERMAiir PROPELLER Type APPLIANCE Manufacturer 6. Conformity Statement AL Agency's Name and Address B. Kind of Agency C. Certificate No. Gulfstuam Aerospace Corporation U.S. Certificated Mechanic W6365 Discovery Drive Foreign Certificated Mechanic • Appleton. WI 54915 X Certified Repair Station GIFRIOOY Manufacturer D. I certify that the repair and/or alteration made to the uni (s) Identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the Information furnished herein is true and correct to the best of my knowledge. Date Signature of AutinrizJ, I raidual DEC 1 0 I000 ca. ".4 .4-- 7. Approval for Return To eevlco Pursuant to the authority given persons specified beew, the unit identified In item 4 was Inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is EL APPROVED 0 REJECTED FAA FIL Standards Manufacturer Inspection Authorization Other (Specify) Inspector BY FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection Certificate or 22of Authr I al • DEC 1 0 1998 Designation No. GIFRIOOY AA Form 33 (12-aM (Compute. Generated) SDNY_GIvi_02754066 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240988 EFTA01326581 NOTICE Weight and balance limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Doscription of Work Accomplished. • (If more space is required. attach additional sheets. Identify with aircraft nationality and registration mark and data work completed). Complied with Gulfstream Aerospace Corp. (FAA approved) Aircraft Service Change 400 dated 9-22-98 Structures - Aluminum Collar - Pressure Bulkhead FS 596 - Terminating Action. Aircraft weight and balance, Equipment list, and Electrical load is negligible or unchanged. END CI Additional Sheets are attached. SDNY_GM_02754067 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002 40989 EFTA01326582 - • • II" • ti - •" !it"; f Form Approved 0 MAJOR REPAIR AND ALTERATION -:'. -tn- 1 OMB No. 2120-0020 US Depotrod I •-•• • aratisartaron (Airframe, Powerplant, Propfellebror Appline) For FAA Use Only Federal Aviation Administration 1 it , ; ULU 1 O I. \‘: ) Office IdentificatioG4._ i INSTRUCTIONS: Print or typo all entries. See FAR 43.9, FAR Appendix:ff. altI7(C-439-110mtuiSquent revision thereof) for instructions and disposition o this form. This report is required by law (49 U. 14..F_ailtrileJarnErt EnaesR in a civil penalty not to exceed $1,000 for each violation (Section 901 of Federal Aviation Act of 1958). Make Model Gulfstrearn G-IV 1. Aircraft Serial No. Nallerialit), and RegStraticn Mark 1085 N864CE Name (rtsslotrwaregisfrationtarriffsafe) Address (Assbonnoaregisbaliontertikale) Coca Cola Enterprises, Inc 2500 Windy Ridge Pkwy SE 2. Owner Atlanta, GA 30339.5677 3. For FAA Use On y 'The data/alteration identified herein cowries with the applicable airworthiness requirements and Is approved for the above described aircraft subject to calamity inspection by a person authorized In FAR 43, Section 43.7'. Date iz/9/9( FAA Inspector GL13 4. Unit anti cation 6. Type Unit Make Model Serial No. Repair Alteration AIRFRAME As described in Item 1above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. Culla:tam Aerospace Corporation U.S. Certificated Mechanic W6365 Discovery Drive Foreign Certificated Mechanic GIFR100Y Appleton, WI 54915 X Certified Repair Station Manufacturer D. I certify that the repair and/or alteration made to the uni Cs) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized In • ual /2/9/98 t • 7. Appro r Return To Service Pursuant to the authority given persons specified below, unit identified in Item 4 was inspected In the manner prescribed by the Administrator of the Federal Aviation Administration and is (APPROVED CI REJECTED FAA FR Standards Manufacturer Inspection Authorization Other (Specify) Inspector BY FAA Designee x Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection Certificate or Signature of AVUodiedl ual Designation No. /2-4)-9se -• • - --- - - --- -- r Genera SDNY_Gtvl_02754068 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240990 EFTA01326583 NOTICE aircraft record. An alteration must be compatible Weight and balance limitation changes shall be entered in the appropriate with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. DescdptIon of Work Accomplished mark and date work Completed). Qf more space is required. attach additional sheets. Identity with aircraftnationally and registration r.structure, F.S. STA 56.812, Replaced one AD rivet in clip angle bracket on the under side of right cockpit floo HL18 fastener. Also installed an additional Hi-Lok forward of floor access panel FLR-4 installing a Hi-Lok P/N: P/N: HL18 fastener in adjacent hole of same clip, found missing since production. END O Additional Sheets are attached. SDNY_GM_02754069 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024099I EFTA01326584 - e 7.••• c r1 Ora --• 7 . -7. . 2..0 1 :Form Approved .0 MAJOR REPAIR AND AL I;l OMB No. 2120-0020 USecoretmere 441998 For FAA Use Only ontensooncoon (Airframe, Powerplant, Propelle _ JO. Office Identificatioph., 13 Asepearericasen Admmemmon INSTRUCTIONS:Printer type all entries. See FAR 43.9,FAR43 A subsequent revision thereof) for Instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to repo can result in a civil penalty not to exceed stood tor each such violation (Section 901 Federal Aviation Act of 1958). Make Model GULFSTREAM AEROSPACE G-IV • 1. Aircraft Nationality and Registration Mark Serial No. 1085 N864CE • • Name (As shown on registration certificate) Address (As sltown on registration certilkate) 2. Owner COCA COLA ENTERPRISES, INC. 2500 WINDY RIDGE PKWY SE ATLANTA, GA 30339-5671 3. For FAA Use Only 4. Unit Identification S. Type Unit Make Model Serial No. Repair Alteration X AIRFRAME • (As described in Item I above) . • • . . . ^. POWERPLANT • PROPELLER . Type APPLIANCE Manufacturer . S. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certi kale No. U.S. Certificated Mechanic GULFSTREAM AEROSPACE CORP. Foreign certificated Mechanic W6365 DISCOVERY DR. It Certificated Rees& Station G1FR100Y APPI.PTCK WT T•421% _ issausuturar D. I certify that the repair and/or alteration made to the un t(s) identified In Item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the Information furnished herein Is true and correct to the best of my nowledge. Data • Signatur f Authottect' DEC 1 0 1998 . • 7. Approval for Return To Seneca Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is MAPPROVED 0 REJECTED FAA Fit. Standards Other (Specify) Inspector Mariblacturer Inspection Authorization BY FM Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of AppitNal or Refection Certificate or Signal Authoriz Inds ual Designation No. DEC I 0 1998 ' G1FR100Y • A Form 337 ilVeal SDNY_Givl_02754070 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240992 EFTA01326585 NOTICE Weight and balance oroperating limitation changes shallbe enteredin the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Descdption of Work Accomplished (II more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Modified the existing Third Comm & Nat Systems by removing the Gables G6860-09 Conun/Nav Control Head, and installing a Collins CTL-23 Digital Control Head, P/N 622-9851-001. The third Comm / NAV system's interface was retained as previously installed with the exception of the controller. GAC modifications to the aircraft wiring for the new control head interface is depicted on the GAC revision to Western Commander Inc. wiring diagrams: No. 3 VHF COMM, 08069110; and No. 3 VHF NAV, 08069128, of which the electrical/electronic aspects of the GAC listed revision is DER approved by N. Kopesky, CHI-262. Existing wiring diagrams affected by the above referenced systems are revised to reflect changes iri system design or interface to the newly installed or modified systems as appropriate. All new single conductor wire meets MIL 22759/16 and all new multi-conductor shielded wire meets MIL 27500. All work done IAW AC43.13-2A, Chapters 1, 2 & 3 and manufacturers installation data. Aircraft equipment list and weight & balance manual revised. END ❑ Additional Sheets Are Attached OILS. GOVERNMEET PRINTING OFFICE: t902-760-012/E0I57 SDNY_GM_02754071 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240993 EFTA01326586 .• 6 — — I Form Approved OMB NO. 2120-0020 0 MAJOR REPAIR ANII!I Ailf I us oecerirreni For FAA Use Only co tensonoton (Airframe, Powerplant, PripterWergdgg) Office Identificatior 13 Federal manse Acurmumnian li i. j (.71, k , i INSTRUCTIONS:Print or type all entries. See FAR 43.9.FAILSAppandiatranclACAS.W.US.16bsequent revision thereof) for instructions and disposition of this form. This report is required by law ( 9 U.S.C.1421). Failure to report can result In a civil penalty not to exceed 51.000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model GULFSTREAM AEROSPACE G-IV 1. Akcraft Serial No. Nationality and Registration Mark 1085 N864CE - .. Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner COCA COLA ENTERPRISES, INC. 2500 WINDY RIDGEPKWY SE ATLANTA, GA 30339-5677 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration X AIRFRAME ' In Item 7 above) . .. (As described . . POWERPLANT PROPELLER Type APPLIANCE Manufacturer 8 Conformity Statement A. AgencYs Name and Address B. Kind of Agency C. Ceni kate No. US. Certificated mechanic GULFSTREAM AEROSPACE CORP. Foreign certificated mechanic W6365 DISCOVERY DR It Certificated ROPOtStalion G1FR100Y APPT MICK MGR 5491c Manufacturer D. Icertifythat the repair and/oralteration made to the un Rat Identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with tht requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my nowledge. Date Signatu . Authord I DEC 1 0 1998 WI 7. Approval for Return To • nice Pu suant to the authority given persons specified below, the unit identified In Item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and Is CkAPPROVED O REJECTED FAA Fit. Standards Other (Specify) Inspector Manufacturer Inspection Authorization BY FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection CertlficaM or Signatu Author Nast DEC 1 0 1908 • Designation No. . GIMUDOY - , orm 337 mast SDNYGM_02754072 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240994 EFTA01326587 • r . NOTICE Weight and balance or operating limitation changes shallbe entered in the appropriate effete(t record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. B. Description of Work Accomplished -•. (It more space is required, attach additional sheets. Identify withaircralt nationality and registration mark and date work completed.) Installed an Allied Signal Avionics Enhanced Ground Proximity Warning System (EGPWS), computer P/N 965-0976-003-104-104, as per Guffaws= Aerospace Corporation (GAC) STC ST01445AT. In order to facilitate this installation, the existing MK-V Ground Proximity Warning System (GPWS), computer P/N 965-0676-0010 (installed per Sits SA218850, FAA Form 337 dated 9/7/89 & ST00714AT, FAA Form 337 dated 1/26/96) was roved from the aircraft Additionally, the three (3) each Honeywell SG-884 Symbol Generators, P/N 7008570-904 have been modified to -905 and the two (2) each Honeywell DC-884 Display Controllers, P/N 7007540-942 have been modified to -946 to allow for EGPWS selection and display of the enhancement features. Deviations to STC ST01445AT include: • Utilized existing wiring where practicaL • Retained the previously installed GPWS circuit breakers and some of the annunciation by incorporating them into the new EGPWS system. System interface and wiring as depicted on GAC wiring diagram GIV-31085-34-10 is electrically equivalent to the aforementioned STC. • Mounting the computer in the R/H radio rack extension at the same location as the removed GPWS computer. Expanded the STCd EGPWS Relay Unit design to house system components. Installed this newly fabricated Avionics Interface Unit in the R/H radio rack extension, adjacent to the EGPWS computer, picking up existing structure. FAA Approved Airplane Flight Manual Supplement, SC41 349M37 dated 8/8/97, with Rev. 02 dated 4/8/98 is required for this approval and supersedes all previously issued AFMS' pertaining to GPWS. Maintenance Requirements - Instruction for Continued Airworthiness, GAC Document No. 5C41 349A01, Rev. 1, dated 6/22/97 with attached AlliedSignal.Line Maintenance Manual, Doc. No. 060- 4199-014 is required for this approval. Eating wiring diagrams affected by the above referenced systems are revised to reflect changes in system design or interface to the newly installed or modified systems as appropriate. All new single conductor wire meets MIL 22759/16 and all new multi-conductor shielded wire meets MIL 27500. All work done IAW AC43.13-2A, Chapters 1, 2 & 3 and manufacturers installation data. Aircraft equipment list and weight & balance manual revised. END O Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING °EPICS: 1912-769-012/60IS7 SONY_GM_02754073 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240995 EFTA01326588 " II ) ' i Form Approved 0 MAJOR REPAIR AN fRILT TIO I OMB No. 2120-0020 uscepamert II 1 1 1998 dTrarasatatian (Airframe, Powerplant, Pr wiener, or ApAliance) j For FAA Use Only Federal Aviation Uldi Office klentficationGL /3 Administration INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 4247ZEftendirtralttlertraffitrzybesquent revision thereof) for instructions and disposition of this form. This report M required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each violation(Section 901 of Federal Aviation Act of 1958). Make. Model Gulfstrezun Aerospace Corp. GIV 1. Aircraft Serial Na Nationality and Registraticn Mark Iffil5 P1864CE Name aflame oitapistrattisaceritecak) Address (As shaman faySiMaancefffitak) Coca Cola Enterprises Inc. 2500 Windy Ridge Pkwy SE 2. Owner . Atlanta GA 30339-5677 3. For FAA Use On y 4. Unit Identification 6. Type Unit Make Model Serial No. Repair Alteration X AIRFRAME (As descabcd in Item 1above) POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6. Conformity Statement A. Agency's Name and Address B. IGnd Of Agency C. Certificate No. Oulfstream Aerospace CorpenitiOn ' U.S. Certificated Mechanic W6365 Discovery Drive Foreign Certificated Mechanic Appleton. WI 54915 X Certified Repair Station GIFRI00Y Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified In item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is hue and correct to the best of my knowledge. Date SIgnatu refuel DEC 1 0 1998 . 7. Approval for Return To Service Pursuant to the authority given persons specified below, the unit Identified In item 4 was inspected in the manner prescribed by the AdmInisUator of the Federal Aviation Administration and isySAPPROVED CI REJECTED FAA Flt. Standards Manufacturer Inspection Authorization Other (Specify) Inspector BY FM Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection Certificate or Signal Autho o rni f t DEC. 1 0 1998 Designation No. GIFRIODY nn 337 (1248) (Compote: Generated) SDNY_Gtvl_02754074 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240996 EFTA01326589 NOTICE Weight and balance limitation changes shall be entered tri the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity With the applicable airworthiness requirements. 8. Description of Work Accomplished , (If more space Is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed). Removed Bendix Instrument Landing system (ILS), consisting of 2ea. ILS Receivers, 2ea. racks, and lea. ILS controller. The ILS system was originally installed at the factory. The ILS system was previously disabled I.A.W. AD 89.02-12 R1 dated March 21, 1994. #1 and #2 ILS circuit breakers were previously removed. Connectors are capped, bagged, and stowed. Removed the following equipment: 2ea. Bendix ILS Receivers P/N 2104-1230-3504 lea. Bendix ILS Controller P/N 1159SCAV404-3 lea. ILS Rack P/N 1159AV40369-1 lea. ILS Rack P/N 1159AV40369-2 The weight and balance manual and equipment list were revised. END ❑ Additional Sheets are attached. SDNY_GIvl_02754075 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240997 EFTA01326590 re:-Q7: r : •._,,, ts Form Approved _., OMB NO. 21204020 .0 MAJOR REPAIR ITERATION US Cocain/al • For FAA Use Only orlandomaron Federal Aneden (Airframe, Powerplant, P regal; Ay/ElI&zee Office IdentificationGt 13 Administration INSTRUCTIONS:Print or type all entries. See FAR 43.9, F kR43Appendix 8. an = or ulnas:went revision thereof) for instructions and disposition of this form. This report Is required by lave44946S.G..1421)...Eatakirggenad result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act 011958). Make Model GULFSTREAIA AEROSPACE ' G-IV 1. Aircraft Serial No. Nationality and Registration Mark 1085 N864CE • Name (As shown on registration certificate) Address (As shown on registration certificate) z Owner COCA COLA ENTERPRISES, INC. 2500 WINDY RIDGE PKWY SE ATLANTA, GA 30339-5677 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration X AIRFRAME (As described in item 1 above) • ' . ',.. - P0WERPLANT PROPELLER Tyne APPLIANCE • Manufacturer . 8. Conformity Statement A. Agency's Name and Address B. Kind of Agency C: Certificate No. (U.S. Certificated mechanic • GULFSTREAM AEROSPACE. CORP. Foreign Certificated Mechanic W6365 DISCOVEItY DR. Certificated Repak Station GIFRIOOY ' ADMPION, WI Sal 5, Manufacturer D. I certifythat the repairand/or alteration made to the un t(s)identified in item 4 above and described on thereverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my nowledge. Date Signature of Authorized Indiv u DEC 1 0 1998 • 7. Approval for Return To Send Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and Is [(APPROVED . CI REJECTED FAA Fit. Standards Other (Specify) Inspector Manufacturer Inspection Authorization BY FAA Designee X Repair Station Person A oved by Transport Canada ppr Ainvonhiness GrouP Dale of Approval or Rejection Certificate or Signatu uthorized dd • Designation No. DEC 10 1998' GIFRIDOY - lt FAA Form 337 ordist. SDNY_GI.1_02754076 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00240998 EFTA01326591 NOTICE Weight andbalance or operating limitation changes shall be enterid in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished . (It more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Installed dual digital Collins RTU-4210 Radio Control Units in the center pedestal in accordance with Atlantic Aviation/Delta Engineering STC ST00717NY-D, dated May 19, 1998, replacing the GAC installed Gables Comm/Nav/ATC/ADF / TCAS Control Heads. Newly installed equipment includes: 2 Ea. Collins RTU-4210 Radio Tune Units, P/N 822-0836-005 Removed equipment includes: 2 Ea. Gables 700-D36407A-002 Comm Controls 2 Ea. Gables 700-D36409A-002 Nav Controls 2 Ea. Gables 700-D36411A-002 AIDE Controls 1 Ea. Gables 700-D36413-008 ATC 1 Control 1 Ea. Gables 700-D36413-003 ATC 2 Control 1 Ea. Gables 700-D36415A-003 Marker Control 1 Ea. Gables G6969-04 TCAS Control Refer to GAC drawings: VHF Comm Mods, GIV-31085-23-20; VHF NAV/DME Moth, GIV-31085-34- 26; ADE System Mods, GIV-31085-34-32; ATC System Moth, GIV-31085-34-35; Control Heads, GIV- 31085-34-37; and FMS Mods, GIV-31085-34-58, which is electrically equivalent to the aforementioned STC. FAA Approved Airplane Flight Manual Supplement, 62743606-340 dated 5/19/98, with Rev. — is required for this approval and supersedes the existing AEM and attached supplements only in the areas contained therein. Maintenance Manual Supplement, Delta Engineering Document No. 727-03609-340 dated 5/19/98, with Rev. — is required for this approval. Existing wiring diagrams affected by the above referenced systems are revised to reflect changes in system design or interface to the newly installed or modified systems as appropriate. All new single conductor wire meets MIL 22759/16 and all new multi-conductor shielded wire meets MIL 27500. All work done IAW AC43.13-2A, Chapters 1, 2 & 3 and manufacturers installation data. Aircraft equipment list and weight & balance manual revised. END 0 Additional Sheets Are Attached dV.S. GOVERNMENT PRINTING OFFICE: 1,12-755-017/60I57 SONY GM 02754077 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002 40999 EFTA01326592 U.S. DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATION February 9.1996 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airpkne,Radiodielicopter etc) NAME OF APPLICANT Gulfstream G-IV Airplane The Jet Center LIST OF DATA IDENTIFICATION TITLE Drawing Number Rev. Date 0 Shts Drawing Tide 08069100 A 01/20/96 5 No. 3 FMS 08069324 A 01/20/96 1 No. 1 & No. 2 Global Position 'END' Note: The above data is reviewed and approved as it pertains to electrical systems and equipment only. PURPOSE OF DATA To show compliance with applicable Federal Airworthiness Regulations for minor deviations to S.T.C. SA3774NM for Gultstrearn G-TV, S/N 1085, N88GA ONLY via FAA. Form 337. APPLICABLE REQUIREMENTS Vitt specific sections) FAR's: 25.1301(nkod); 25.1309(a,b,c); 25.1322(be,d); 25.1355(c); 25.1357(a,c,d). CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered none have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. I ewe) Therefore A Recommend approval of these data Approve these data SIGNATURES) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) .gLits,ci re rt nA--- NM-2128 Systems & Equipment Sarlds A ICara,guzian . orm EI 10-3(11.70) SUPERSEDES PREVIOUS EDITION GPO 901-613 SDNYGlvl_02754078 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241000 EFTA01326593 SDNYGM02754079 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241001 EFTA01326594 . A. A ch-cf4:-c-s Form Approval C 1 OMB No. 2120-0020 U.S. Department MAJOR REPAIR AND ALTERATION For FAA Use Only of Transportation (Airframe Powerplant, Propeller, or Appliance) Office Identification 'Federal Aviation Administradon STITS11O.11 .,114STRUCTI0NS. Print or type all antics. See FAR 43.9 FAR 43 Appendix B. and AC43.9-1 (cesubscquent revue= thereof) for =ass and cIsposilkm dais tbrin. Ibis report is required by law(49 U.S.U. 1421). Faun to report can remit illation penalty not to exceed $1,000 for cub nub violation (Section 901 Federal Aviation Actor 1938). Make Model 1. Aircraft Gulfstream (MV Serial No. Nationality and Registration Marks 1085 U.S.A. N864CE Name at shown on registration Certificate) Address (As shown on registration certificate) 2. Owner Coca-C-ola Enterprises Inc. 3931 Ann Dr NW Atlanta, GA 30336-1512 3. For FAA Use Only • 4. 17alt Identification 5. type Unit Make I Model I Serial no. Repairs Alterations Airframe - — (As described in irem I above) P ea— X Powerplant Propeller Type Appliance ManUfaCtUrtr 6. Conformity A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Certificated Mechanic Gulfstream Aerospace Corporation Foreign Certificated Mechanic FAA CRS GR4R216M P.O. Box 2206 - Travis Field X Certificated Repair Station Savannah. GA 31402-2206 Manufacturer D. I cab& that tbe repair andlor alteration made to the =Ns) idadified m item 4 above and!wailed ca the muse or anathacrits bare have been made in accordance with the requirements of Part 43 efthe US. Federal Regulations and that the information garnished benzin is true and ant the bet army knowledge- Date Signature of Authorized Indivi ual 09/05/97 Steven Sweeney 7. Approval for Return To Service Punuant to the authority giveo persons specified below, the unit identified in ban 4 was inspected in the manner prescribed by the Atli:enteral& Federal Aviation Administration and is El APPROVED O REJECTED FAA FIt. Standards Manufacturer Inspection Authorization Other (Specify) BY Inspector- FAA Designee X Repair Station Person Approved by Transport Canada Ai worthiness Group Date o Approval dr Rejection - - Certificate or - - Signature of Assiberized individual Dedgoation No. g 09/05197 FAA CRS GR4R216M Jimmie K. Smith . ' A,.. . ntei, SDNYGlvl_02754080 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241002 EFTA01326595 • NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate tuft retort An alteration must be compatible with altprevious alteration to assure continued conformity with the applicable airworthiness requirements 8. Description of Work Accomplished: (temote space is requited snub soiTstional sheets kleo* vale ainraft Whoa* end registration mark iodate bark completab. Aircraft Model: G-IV Aircraft Time Since New: 2853.9 Aircraft Serial No.: 1085 Aircraft Landings Since New: 1227 Aircraft Registration No.: N864CE Reference: Gulfstream Aerospace Corporation Workorder No.: C04-1085-097-0042 1. Incorporated the following FAA approved major Gulfstream Aircraft Service Changes: ASC No.: Subiect: 135 A2 ECS Pack Sequencing During Engine Start End O Additional Sheets Are Attached SDNY_GM_02754081 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241003 EFTA01326596 -- 8TAWDARISAIRWOMINES8 CITTFICATI II866CZ 0:11.18118Sall/GIV 10115 MUM= • J•I•antr".•••• WWI. ::•••.:::========" " "" Ion • 71:3. 12-16-88 Vitt FMFo, Me" man SDNY_GM_02754682 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 00241004 EFTA01326597 SONY_GM02/59083 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 00241005 EFTA01326598 . _ • !r,7-• •-• • \\ ( Cly t ; • II • Form Approved f • OMB No. 2120-0020 - 6 L.,:,7 MA. R REPAIR AND ALTERATION For FAA Use Only mmn (Airframei Powerplant, Propeller, or Appliance) Office Identification if - AI /3 ClitragtFriRroitype an en des. See FAR 43.9, FAR 43Appendix B. and AC 43S-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed 91,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model— Gulfstream Aerospace -1.,-IV 1. Aircraft Serial No. 7085 Nationality and Registration Mark N Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner Coca-Cola Enterprises, Inc. 2500 Windy Ridge Parkway Atlanta, Georgia 30338 3. For FAA Use Only 4. Unit Identification S. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item I above) X POWERPLANT PROPELLER Type APPUANCE Manufacturer 8 Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Certificated mechanic K-C Aviation, Inc. Foreign Certificated Mechanic 301 Discovery Drive X c•niscanics sops swan Appleton, WI 54915 Manufacturer QK2R112L D. I certify that the repair and/or alteration made to the un t(s) identified in Item 4 above and describedon the reverse or attachments hereto have been made In accordance with the requirements of P n 43 of the U.S. Federal Aviation Regulations and that the Information furnished herein is true and correct to the best of my know edge. Date Signature of Authorized Ina( ual DEC 20 1996 7. Appro I or Return To Service Pursuant to the authority given persons specified below, the unit identified in item 4 was Inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is Ft.APPROVSO - 0 REJECTED FAA Rt. Standards Other (Specify) Inspector Manufacturer Inspection Authorization BY FAA Designee x Repair Station Person Approved by Transport Canada Airworthiness Group Date& Approval or Rejection Certificate or Signature of Authorized Ind' 'dual Designation No. DEC 20 1996 ClK2R112L • (cdseine. FAA Form 337 /2.s SDNYGIvl_02754084 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241006 EFTA01326599 NOTICE Weight andbalance or operating limitation changesshall be enteredin the appiopriate aircraft record. An alteration niust be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (II more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed:) . Fabricated and installed life raft storage provisions for two rafts under divan, F.S. 379 and F.S. 415 in accordance with K-C Aviation, Inc., Structural Drawing GIV-25-01-222, sheet 1. DER approval is in accordance with 8110-3 form dated 12/20/96 by A. Duncan, CHI-424. Fasteners torqued using AC43.13-1A chapter 5 as a guide. Corrosion protection accomplished using AC-43.13-1A chapter 6 as a guide. Materials used meet the requirements of FAR 25.853. END O Additional Sheets Are Attached OILS. 00VICRNMENT PRINTING OPPIGC: I192-749-0I2/101117 SDNY_GM_02754085 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241007 EFTA01326600 Form Approved ' OMB No. 2120-0020 MAJOR REPAIR AND ALTERATION - 6 tlAn 1d rams) Powerplant, Propeller, or Appliance) For FAA Use Only Office Identification Aviation tmrlinn IL" Ch/3 atiglIaLICTIOAMPrig4014490411-sa ries. See FAR 43.9, FAR 43Appendix EL and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result In a civilpenalty not to exceed S1.000 for each such violation (Section 901 Federal Aviation Act of 1958). make Model Gulfstream Aerospace G-IV 1. Aircraft Serial No. Nationality and Registration Mark 1085 N88GA Name (As shown on registration certificate) Address (As shown on registration certificate) t Owner Coca-Cola Enterprises, Inc. 2500 Windy Ridge Parkway Atlanta, Georgia 30338 3. For FAA UVVEINIXIA/ALI trUAIILMIrrilzIJAIti ILltNI II-ICU ItHtinil GUM Itb WI I H I It mar4GAbLt HIFIVVUti I I-IINtbb REQUIREMENTS AND IS APPROVED FOR THE ASOVE DESCRIBEDAIRCRAFT, SUBJECT TO CONFORMITY INSPECTION BYA PERSON AUTHORIZED I AR SECTIO 43. 3IGNA—U 4. Unit 'dentin; IAA MICE FSDO . Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 7 above) X POWERPtAfff PROPELLER Type APPLIANCE Manufacturer 6 Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Cenificated Mechanic K-C Aviation, Inc. Foreign Certificated mechanic 301 Discovery Drive x Certificated Repair Station Appleton, WI 54915 manufacturer QK2R112L D. I certify that the repair and/or alteration made to the un t(s) identified in item 4 above and described on the reverse orattachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein Is true and correct to the best of my knowledge. Date Signature of Authorized Individual DEC 0 9 1996 . -kO 7. App a tor Return To Service Pursuant to the authority given persons specified below, the unit Identified In item 4 was Inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is Q, APPROVED O REJECTED FAA FIL Standards Other (Specify) Inspector Manufacturer Inspection Authorization BY FAA Designee ., Repair Station Person Approved by Transport A Canada AIMOilhintSS Group Date of Approval or Rejection Certificate or Signature of Authorized Individual Designation ignation No. DEC 181996 i 8 1996 0K2R112L Coma ‘....a FAA Form 337 02401 SDNYGIvl_02754086 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241008 EFTA01326601 NOTICE Weight and balance or operating limitation changes shallbe enteredin the appropriate aircraft record. An alteration must be corn/sat/We with all previous alterations to assure continued conformity with the applicable airworthinesi requirements. 8. Description of Work Accomplished (If more space is requited. attach additional sheets. Identify with aircraft nationality and registration mark and dale work completed.)- ... Removed all 10 existing Aircraft Modular Products cabin chairs P/N: 1250-1399-001; P/N: 1250- 1399-002, forward (2 ea.), center group (4 ea.), aft group (4 ea.), retractable tables (6 ea.) and (2 ea.) left and right forward cabin cabinets at F.S. 176. Installed six new single ISO C39a Aircraft Modular Products chairs, two double TSO C39a Aircraft Modular Products chairs and a Tosington side facing three place TSO C39a, Type I divan reconfigured to 13 place passenger cabin in accordance with K-C Aviation, Inc., floor plan drawing GIV-25-05-200, sheet 1 dated 10/29/96. Seats and divan are installed in the conventional manner using new seat track over existing aircraft seat track in accordance with K-C Aviation STC SA1266GL approved drawing GIV-25- 50-205, sheet 1, revision B in the positions listed below: #1 IJH P/N: 2524.014(-866C) Aft Facing F.S. 173 #1 R/H P/N: 2524.014(-866D) Aft Facing F.S. 173 #2 L/H P/N: 2524.014.01(-874B) Forward Facing F.S. 225 #2 R/H P/N: 2524.014.01(-874A) Forward Facing F.S. 225 #3/4 L/H P/N: 2524.015(-167C) Aft Facing F.S. 272 #5/6 L/H P/N: 2524.015(-1678) Forward Facing F.S. 326 #7 R/H P/N: 2524.014(-866A) Aft Facing F.S. 370 #8 R/H P/N: 2524.0141-866A) Forward Facing F.S. 424 Divan P/N: T480-40 Side Facing F.S. 397 All seats installed with new ISO C-22F color coordinated seat belts by C & M Marine. Details of additional interior components depicted and installed in accordance with floor plan drawing are approved on separate FAA form 337's. The floor plan drawing will be referenced for location purposes. Materials used meet the requirements of FAR 25.853. The aircraft weight and balance manual and equipment list revised. Fasteners torqued using AC.43.13-1A chapter 5 as a guide. END ❑ Additional Sheets Are Attached 0 U.S. GOVERNMENT SMINTINO OF NCI: 1M-769-012/60157 SDNY_GM_02754087 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241009 EFTA01326602 in g Lt.,. I,.. Form Approved • OMB No. 21200020 Vat IS MA OR REPAIR AND ALTERATION For FAA Use Only 4 - 6 Iiigrframe Powerplant, Propeller, or Appliance) Office Identificatiory is, Ansa •i await f alif...1 NSTRUCTIO NS: Print or type all e ries. See FAR 43.9. FAR 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions ermicitspositiorrof this . is required by law (49 U.S.C. 1421). Failuret0 Alpert can result Ina civii penaity not to excee351800 for each such violation (Section 901 Federal Aviation Act of 1958). Make ModeL• Gulfstream Aerospace u -IV I. Aircraft Serial No. Nationality and Registration Mark 1085 N88GA Name (As shown on registration certificate) Address (As shown on registration certificate) z Owner Coca-Cola Enterprises, Inc. 2500 Windy Ridge Parkway Atlanta, Georgia 30338 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As describedIn Item 1 above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6 Conformity Statement A. Agency's Name and Address 8. Kind of Agency C. Certificate No. U.S. Certificated Mechanic K-C Aviation, Inc. Foreign Cann-mated Mechanic 301 Discovery Drive y Certificate:1Racal/ Station Appleton, WI 54915 ' Manufacturer OK2R112L O. I certify that the repair and/or alteration made to the un t(s) identified in item 4 above and described on the reverse or attaChmentS hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein Is true and correct to the best of my knowledge. Date Signature of Authorized lndiv ual DEC 18 1996 7. Approv or Return To Service Pursuant to the authority given persons specified below. t unit identified in item 4 was Inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is (APPROVED O REJECTED FAA Flt. Standards Other (Specify) Inspector Manufacturer Inspection Authorization BY FAA Designee x Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection Certificate Or Signature of Authoriz Indi dual Oesignation No. DEC 18 1996 OK2R112L CI A,-4-, c • FAA Form 337 02441 SDNYGIvl_02754088 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241010 EFTA01326603 NOTICE Weight and balance or operatinglimitation changes shall be enteredin the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. S. Description of Wotk Accomplished of more Space is required, attach additional sheets. Identity with aircraft nationality and registration mark and date work completed.) Fabricated and installed the following new interior components in accordance with K-C Avlation, Inc., Floor Plan Drawing GIV-25.05-200, sheet 1 and the below listed Structural Drawings: GIV-25-02-203 Sheet 1 Rev. - Subwoofer Installation GIV-25-01-209 Sheet Rev. - Game Table Leaf Assembly GIV-25-02-209 Sheet 1 Rev. - Enflight Table Installation GIV-25-09-210 Sheet 1-3 Rev. - Galley Aft Right Modification GIV-25-10-210 Sheet 1-2 Rev. - Galley Aft Left Modification GIV-25-07-223 Sheet 1 Rev. - Aft Divan Cabinet Installation GIV-25-08-223 Sheet 1 Rev. - Forward Divan Cabinet Installation GIV-25-06-226 Sheet 1-5 Rev. - Credenza Details and Installation GIV-25-53-286 Sheet 1-2 Rev. - Conference Table Dual Pedestal Installation Subwoofers installation consists of four units installed below cabin window ledges at the following locations: two each forward left and right cabin F.S. 163; one each right aft cabin F.S. 350 and one each right aft cabin 436. Fabricated and installed three stowable game tables in the following locations: two each left and right forward cabin F.S. 198; one each right aft cabin F.S. 397. Fabricated and installed new manual height adjustable conference table in center left cabin F.S. 299. Fabricated and installed new credenza cabinet in right center cabin extending from F.S. 255 to F.S. 345. Credenza contains six drawers in center for miscellaneous storage and hinged compartments on each end for pillow and blanket storage. Fabricated and installed new divan forward and aft divan armrest cabinets located at F.S. 355 and F.S. 434. Cabinets contain drawers for miscellaneous storage. Modified left galley to include removal of decanter cabinet, replacing Sharp microwave oven P/N: R-1M53 with new larger Tappen unit P/N: TMS083U1W and replaced 13" Hitachi TV monitor P/N: CT1386B with new 14" Baker LCD monitor P/N: TW1400. Modified right galley removing hot cup dispenser, replacing circuit breaker panel, adding the following equipment: new Krups coffee maker, hot and cold water spigot and sink, Nordskog Hi- Temp oven P/N: 50231 and new trash receptacle. New trash receptacle is in compliance with the flammability requirements of 14CFR25 (part 25), paragraph 25.853(h), amendment 25-83. DER approval is in accordance with 8110-3 form dated 12/18/96 by A Duncan, CHI-424. Electrical aspects covered separately. Cabin interior compartment placards description detailed in K-C Aviation drawing GIV-25-01-218 and layout per drawing GIV-25-04-218. Fasteners torqued using AC43.13-1A chapter 5 as a guide. Corrosion protection accomplished using AC 43.13-1A chapter 6 as a guide. Weight and balance accomplished using AC43.13-1A chapter 13 and the aircraft manufacturer's weight and balance manual as a guide. Materials used meet the requirements of FAR 25.853. The aircraft weight and balance manual and equipment list revised. END 0 Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: 1192-769-012/60157 SDNY_GM_02754089 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002410I I EFTA01326604 Form Approved I ; Vi L3 . ome No. 2120-0020 0 MAJOR REPAIR AND ALTERATION US Doormen For FAA Use Onty Mitenspermson - 6 Lymnr Powerplant, Propeller, or Appliance) . An Fare' krtallen Office Identificatiwi NJ3 tU Ctl a itlUCTIONS: Print or type alt entries. See FAR 43.9. FAR 43 Appendix B. and AC 43.9.1 (or subsequent revision thereof) for instructions ispositicusoLthWoraatiisseairt Is required by law (49 U.S.C. 1421). Failure to report can result In a civil penalty not to exceed $1.000 - for each such violation (Section 901 federal Aviation Act of 1958). Make Model Gulfstream Aerospace G-IV 1. Aircraft Serial No. Nationality and Registration Mark 1085 N88GA Name (As shown on registration certificate) Address (As shown on registration certificate) Z Owner Coca-Cola Enterprises, Inc. 2500 Windy Ridge Parkway Atlanta, Georgia 30338 3.. For FAmp 4;enotreers, .. . tf. , v4H44.h.7ipptitheipteleaFivvom ,I.t_j,:,,,,rminajtmiurt -.,:r miciEsr l REQUIREMENTS AND IS APPROVED FOR THE ABOVE DESCRIBED AIRCRAFT, SUBJECTTO CONFORMITY INSPECTION BYA PERSON AUTHORIZED IN 43 SECTION 7 ne-re 1 zl In 4. Unit Identification FAA NIKE I-SDO Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6 Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. . US. Certificated Mechanic K-C Aviation, Inc. Foreign Certificated mechanic 301 Discovery Drive x Certificated Repair Station Appleton, WI 54915 Manufacturer CIK2R112L D. I certify that the repair andtor alteration made to the un t(s) identified in item 4 above and described on the reverse or altachrnemts hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Oate Signature of Authorized Individual DEC 0 9 1996 c 7. App for Return To Service Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected In the manner prescribed by the Administrator of the Federal Aviation Administration and is Ck.PPROVED CI REJECTED FAA Flt. Standards Other Meal Inspector Manufacturer Inspection Authorization BY FAA Designee K Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection Certificate or Signature of Authorized Individual No. DEC 18 1996 Des CIK ignation2R112L Qs...-. cd-jd- FAA Form 337 11206) SDNYGIvl02754090 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241012 EFTA01326605 NOTICE Weight andbalance or operating limitation changes shall be enteredin the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required attach additional sheets. Identify with aircraft nationality and registration park and date work completed.) Modified existing forward right vestibule crew cabinet, F.S. 163 in accordance with K-C Aviation, Inc., Structural Drawing GIV-25.05-216, sheet 1 and PS100-26.04-600. Cabinet rework consists primarily of the following changes: Compartment #1 (Upper): 1) Removed existing upper cabinet compartment tambour door installing new hinged door 2) Relocated existing bleed air temp indicator in upper portion of compartment adjacent existing data loader and removed existing water tank from lower portion of compartment. Area now used for miscellaneous storage. 3) Compartment placarded 4.0# maximum Compartment #2: 1) Removed existing Proctor Silex coffee maker P/N: A607 installing new Krups auto fill maker P/N: 321 to existing slide out tray. 2) Installed new Baker 14' LCD TV monitor aft facing and adjacent to coffee maker. Monitor is retained in the cabinet by a removable shroud assembly, fabricated from Norlam aluminum sandwich panel P/N: NL610-10111-375, .75" X .75" X 0.050" 2024-73511 extruded aluminum angles and TYE 2004 thru inserts and TYE 2001 potted into cabinet. Compartment #3 (Drawer): 1) No changes 2) Compartment placarded 5.0# maximum Compartment #4 (Drawer): 1) No changes 2) Compartment placarded 10.0# maximum Compartment #5 (Bottom): 1) Removed two existing drawers installing new single drawer to fit compartment. 2) Compartment placarded 20.0# maximum Replaced all compartment drawer and door latches with new Actron positive type latches P/N: A23060-9 and A23551-35. Electrical aspects covered separately. All metal fabrication practices per K-C Aviation Process Specification 106. All threaded fastener installations per K-C Aviation Process Specification 105. Fabrication of bulkheads, cabinets, drawers and doors per K-C Aviation Process Specification 116. Cabin interior compartment placards description detailed in K-C Aviation drawing GIV-25.01-218 and layout per drawing GIV-25-04-218. Fasteners torqued using AC43.13-1A chapter 5 as a guide. Corrosion protection accomplished using AC 43.13-1A chapter 6 as a guide. Weight and balance accomplished using AC43.13-1A chapter 13 and the aircraft manufacturer's weight and balance manual as a guide. Materials used meet the requirements of FAR 25.853. The aircraft weight and balance manual and equipment list revised. END ❑ Additional Sheets Are Attached nu.s. aote vitamin T PRINTING OFFICE 1991-769-015/40157 SDNY_GM_02754091 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241013 EFTA01326606 . "; \11121 • Form Approved JAN — 6 I997 OR REPAIR AND ALTERATION OMB No. 2120-0020 For FAA Use Only (AM , Powerplant, Propeller, or Appliance) Office Identifies,' ackremmenew, ic)gn lig INSTRUCTIONS:Print or type all entries. SeeFAR 43.9. FAR 43 Appendix Et and AC43.9-1 (or subsequ nt revision thereof) for instructions anddisposition of this form. This report is required by law (49U.S.C. 1421). Failure to report can result in a civil penalty not to exceed 51.000 for each such violation (Section 901 Federal Aviation Act 011958). Make Mode Gulfstream Aerospace IG-IV 1. Aircraft Serial No. Nationality and Registration Mark 1085 N88GA Name (As shown on registration certificate) Address (As shown on registration certificate) 2. owner Coca-Cola Enterprises, Inc. 2500 Windy Ridge Parkway Atlanta, Georgia 30338 ,._ , .,,..,,;.., „,...,, „„,„...,.,,,,,,..„.0‘.,....wicil miziks:IN 3. For FAA Urie(Gartel IFS WITH THE APPI CAR) F AIRIANIRTHIMFRR REQUIREIviENTS AND IS APPROVED FOR THE ABOVE DESCRIBED AIRCRAFT, SUBJECT TO CONFORMITY INSPECTION BY A PERSONAUTHORIZED IN F 43, SECTION 7- DATE. ea- SIGNKRIRF. 4. Unit Identification FAA MKE FSDO S. Type Unit Make Model Serial No. Repair Alteration AIRFRAME . (As clisSeribedin hem 1OM") X POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6 Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Cerli icate No. U.S. Certificated mechanic K-C Aviation, Inc. Foreign Certificated MeChailiC 301 Discovery Drive x Certificated Repair station Appleton, WI 54915 Manufacturer C1K2R112L D. I certify that the repair and/or alteration made to the can t(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the Information furnished herein Is true and correct to the best of my knowledge. Date Signature of Authorized Individual DEC 0 9 1996 (" ......A. . 7. Ap al for Return To Service Pursuant to the authority given persons specified below, the unit identified In Item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is GAPPROVE0 0 REJECTED FAA Flt. Standards Manufacturer Other (Specify) Inspector Inspection Authorization BY FAA Designee Repair Station Person Approved by Transport x Canada AInvorthiness Group °aloof Approval or Rejection Certificate or Signature of Authorized Individual Designation No. DEC 18 1996 12K2R112L C)S`" d e" - " .• FAA Form 337 02.8e) SDNY_CM_02754092 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_0024I0I4 EFTA01326607 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued LOnlOrmily with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required attach additional sheets. Identity with aircraft nationality and registration mark and dale work completed) Removed existing cabin window ledges and lower sidewalls, modified existing vestibule, cabin, aft galley headliner and existing floor conditioned air ducts, installed new window desiccant system, upper sidewall speakers, new ledges and lower sidewalls and two additional oxygen presentation units as detailed below. Interior components located in accordance with K-C Aviation, Inc. floor plan drawing GIV-25-05-200, sheet 1. Cabin peripheral interior rework extends from forward cabin bulkheads F.S. 155 to aft cabin bulkheads F.S. 445. Modified by sectioning existing cabin headliner into five 48.00" long sections using the following K-C Aviation drawings: GIV-25-50-213, sheet 1, rev. A - Headliner Vestibule Assy and Installation; GIV-25-50-213, sheet 2, rev. A - Headliner Main Cabin Bracket Details; GIV-25-01- 213, sheet 1 -Headliner Support Bracket Installation. The five panels interlock together on the forward and aft ends when installed in the aircraft with a flange and slot assembly fabricated from .040" 2024-T3 aluminum flat stock and 5 slots fabricated from 0.75 X .025" X .075" 2024-T3511 extruded aluminum Z angle. The headliner is retained in the aircraft on the outboard edges using existing isolator mounting provisions and ten 34.00" long support angles (5 ea. side) fabricated from 0.063" 2024-T3 aluminum installed between each existing headliner bracket. Added two new Scott dual oxygen presentation units P/N: 833-610 in left headliner F.S. 286.5 and 307.5 and two duel presentation units, one left valance F.S. 213.81 and one in right valance F.S. 213.81. All new units are plumbed to existing system. Additional presentation unit installation and seating configuration does not exceed limitation requirements of Aero Interiors continuous flow supplemental oxygen system STC SA4416NM. Fabricated and installed 11.0" X 5.0" light bracket assemblies in vestibule between F.S. 85.0 and F.S. 97 (1 ea.) and galley (2 ea.) using K-C Aviation, Inc. drawing GIV-25-50-213, sheet 4, rev. A - Headliner Aft Galley Assy and Installation. Each bracket assembly is fabricated from .040" 2024-T3 aluminum. Each assembly is retained by four brackets fabricated from 1" X 1" X .050" 2024-73511 extruded aluminum L angle riveted or hylocked to adjacent frames. Bracket assembly provides mounting surface for dome style lights. Fabricated and.installed mounting provisions for five upper sidewall entertainment system speakers on each side of the cabin between each cabin window, F.S. 200, 250, 301, 350 and 395 in accordance with K-C Aviation Inc., drawings GIV-25.02-211, sheet 1 & 2 - Upper Sidewall Speaker Installation. Each assembly consists two formed angles and four brackets constructed from 0.063" 2024-T3 aluminum to accommodate the 8.50" X 5.00" Baker HF93 speaker assemblies. Each speaker is retained to the aircraft by the four angle brackets riveted to the adjacent frames, four each isolator mounts P/N: 100147-40-062; four each MS21059L3 nutplates and MS227039-1 screws, two each formed angles and hardware provided by the speaker manufacturer. Fabricated and installed replacement left and right ledges using K-C Aviation, Inc., drawings GIV- 25-51-203, sheet 2, rev. A - Lower Sidewall Ledge Assembly and Install; GIV-25.04-203, sheet 1 - Ledge VIP Panel Installation; CL600-25-17-203, sheet 1 - Ledge Lid And Storage Compartment Install Installation consisting primarily of four sections fabricated from NL610-10122-500 and - 250 Norlam sandwich panel; two left and right forward and one right aft section with retractable table provisions; left aft section behind divan. Each section is secured to each side of the cabin below the window line using TYE 2004A3-500 and TYE 2001-08-10 thru and threaded inserts potted into ledge, isolators P/N: B-532-1 and MS hardware into a formed aluminum assembly consisting of a full length intercostal, aluminum gussets, angles, webs and gusset plates riveted together and to the aircraft structure. Ledges contain cup holders and electrical membrane switches at seating locations, VIP panel and Magnastar handset and cell phone storage at #2 left and right forward cabin seats. The lower sidewall panels are fabricated from NL 610-10111-250 Norlam sandwich panel and close-out area below ledges to existing floor conditioned air duct. Panels are sectioned for easy access and retained by the ledge end cap and an aluminum angle running full length of ledge. The lower end of sidewall panel is retained using an aluminum angle blind riveted to existing conditioned air duct and Velcro loop and hook fastener material. rif Additional Sheets Am Attached *U.S. GOVERNMENT PRINTING OFFICIO IS112-761-0ISNSOIS7 SDNY_GM_02754093 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241015 EFTA01326608 Gulfstream GIV, S/N: 1085 N88GA Page 2 Reworked existing floor length left and right cabin conditioned air ducts due to removal of previously installed cabin stowable tables at F.S. 206, 297 and 395 in accordance with K-C Aviation, Inc., drawing GIV-25-01-207, sheet 1 - Conditioned Air Heat Duct Repair. Rework consists of closing out upper duct recesses using a 0.040" 2024-T3 aluminum panel blind riveted with NAS9301B-4 rivets and PR1422 sealant. Relocated existing cabin temperature sensors P/N: 926485-1-1 in accordance with floor plan drawing. Right forward temperature sensor moved from F.S. 219 to F.S. 250 and left from F.S. 436.5 to 345. aft moved Fabricated and installed new left and right cabin window desiccant systems using K-C Aviation, Inc., drawing GIV-25-51-203, sheet 6, rev. A • Lower Sidewall Window Desiccant System Installation. Each desiccant system is constructed of 2.0" X 21.0" long Excelon tube 2.0" PVC end caps bonded on each end with PCV adhesive. One end cap contains bonded with fitting P/N: 125HBL4-4 the other with an MS 20913-4D fill plug. Desiccant tubes area hose barb mounted below window ledges in lower sidewalls at F.S. 200 with two MS21919WH32 clamps and a bracket fabricated from 0.050" 2024-T3 aluminum riveted to the aircraft structure. Each desiccant tube is plumbed to each window with 5052-0 0.25" tubing, Tygon polyethylene tube, Nalgene nylon TEE P/N: 582707C/15221CA and Y P/N: 582747C/13366CA fittings as required. Performed an oxygen drop-out test in accordance with Gulfstream Aerospace Maintenance Manual chapter 35. Electrical requirements for above installations covered on separate form 337. All metal fabrication practices carried out per K-C Aviation Process Specification 106. All threaded fastener installations carried out per K-C Aviation Process Specification 105. Riveting accomplished using AC43.13-1A chapter 2 as a guide. Fasteners torqued using AC43.13-1A chapter 5 as a guide. Corrosion protection accomplished using AC43.13-1A chapter 6 as a guide. Materials used meet the requirements of FAR 25.853. The aircraft weight and balance manual and equipment list revised. END SDNY_GIvl_02754094 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241016 EFTA01326609 SDNY_GM_02754095 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002410 I 7 EFTA01326610 C. • - "'"— --lii 'I migrgoweE• !' : Form Approved ontra— 6 US l itJOR REPAIR AND ici fRato3N6 mg It • OMB NO.2120-0020 For FAA Um Only e, Powerplant, Props or Appliance) II' i' Office identification lit g. iliviniten La I IL' 6 4ia INSTRUCDO.NS:RsinSeotypea entries. See FAR 43.8 FAR 4 Appendix B. and AC 4.371-"Mu s7Vertu nt revision thereof) for instructions —ird disposition of this form. This report is required by law (49U.S.C. 1421). Failure toreport can result i a civil penalty not to exceed $1.000 for each such violation (Section gat Federal Aviation Act of 1958). Make Gulfstream Aerospace M°deb-IV I. Aircraft Serial No. 1085 Nationality and Registration Mark Name (As shown on registration cenifkate) Address (As shown on registration cetlificatel 2. Owner Coca-Cola Enterprises, Inc. 2500 Windy Ridge Parkway Atlanta, Georgia 30338 3. For FAA Use Only 'The data/alteration identified herein complies with the applicable airworthiness requirements and is approved for the above discribed aircraft to conformity inspection by a person authorized in FAR 43, Section 43.r. Date \7 \s::\‘,0 FAA Inspector . k—L \ GL13 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer 8. Conformity Statement A. Agency's Name and Address 8. Kind of Agency C. Certificate No. V.S. Certificated Mechanic K-C Aviation, Inc. Foreign Certificated Mechanic 301 Discovery Drive x Cenificated Repair Station Appleton, WI 54915 Manufacturer QK2R112L D. I certify that the repaira/xi/or alteration made to the un t(s) identified in item 4 above and described on the reverse or attachmentshereto have been made In accordance with the requirements of P n 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date • Signature of Authorized individual DEC 09 1996 7. Approv r Return To Service Pu suant to the authority given persons specified below, the unit Identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and s ja,APPROVED 0 REJECTED FAA FIL Standards Other (Specify) Inspector Manufacturer Inspection Authorization BY FAA Designee Repair Station Person Approved Canada by Transport Airworthiness Group X Date of Approval or Rejection atie or Certificat Signature of Authorized Individual ig on No. Desn DEC 18 1996 QK2R112L gsn,o FAA Form 337 one) SDNY_ GE/1_02754096 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024I0I8 EFTA01326611 NOTICE • • Weight and balance or operating limitatiorrafangesshalf qe entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished of more space Is required. attach additional sheets. Identity with akeraff nationality and registration mark and date work completed.) Remounted interior cabin door at F.S. 155 to hinge from right side. Door installed with new hinge assembly fabricated in accordance with K-C Aviation, Inc., drawing GIV-25-50-229, revision A, sheet 10. Door is retained in the open position by a door stop installed on lower vestibule storage cabinet. Fabricated and installed mounting tray for HPA/LNA on right lower cabin sidewall F.S. 250.5 in accordance with K-C Aviation, Inc., structural drawing GIV-25-51-203, sheet 7. Mounting tray is constructed from 0.040" 2024-T3 aluminum sheet. Tray is mounted using MS24693-10 screws and MS21059L3 nutplates to the aircraft structure between adjacent frames using brackets fabricated from 0.050" 2024-T3 aluminum sheet riveted to the aircraft structure. Fabricated and installed mounting trays for CDBR-2 on center right lower cabin sidewall F.S. 238 and CDBR-2 on left aft cabin below ledge, F.S. 430 in accordance with K-C Aviation, Inc., structural drawing GIV-23.02-301, sheets 1 & 2. Trays are constructed from 0.040" 2024-T3 aluminum mounted to the aircraft structure with four brackets fabricated from 0.050" 2024-T3 aluminum with rivets and MS hardware. Fabricated and installed miscellaneous electrical component mounting trays located on left lower forward cabin below ledge F.S. 170 and right forward cabin behind coat closet F.S. 127. Trays are primarily constructed from 0.050" 2024-T3 aluminum sheet mounted to the aircraft structure with MS hardware to 2.75" X 4.5" brackets fabricated from 0.050" 2024-T3 aluminum sheet riveted to frames or stringers as required. Overall dimensions of left trays (2 ea.) at F.S. 170 are 6.5" wide and 16" wide; 3.5" wide and 12.0" long. Overall dimensions of right forward tray F.S. 127 is 9.0" wide and 19.5" long. Trays provide mounting surface for cabin lighting power supplies, terminal strips and entertainment system controllers. Fabricated and installed new replacement lavatory vanity fluorescent accent light bar, F.S. 502. Unit is constructed from NL610-10111-250 Norlam aluminum honeycomb panel contoured to headliner extending from lavatory door to vanity top. Overall dimensions are 2.125" wide and 58" long. Light bar is mounted to the existing bulkhead using three 1.25" X 1.0" X 0.063" 2024-T3511 extruded aluminum L brackets, TYE threaded inserts potted into bulkhead, MS screws and nutplates. The light bar contains mounting provisions for two fluorescent tubes. Unit constructed using K-C Aviation Process Specification 106 and fasteners installed per Process Specification 105. Fabricated and installed feed thru behind entertainment cabinet for micellaneous electrical cable routing in accordance with K-C Aviation drawing GIV-25-15-293, sheet 1. Fabricated and installed replacement left and right life lines only. Lines fabricated in accordance with K-C Aviation emergency equipment and location drawing GIV-25-00-222, revision C, sheet 1. Life lines attach to existing seat tracks below emergency exits and when in use, to existing eye mounts on each wing. ❑ Additional Sheets Are Attached GOVOINMENT PRINTING OFFICE: IM -769-012/60167 SDNY_GM_02754097 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241019 EFTA01326612 Gulfstream GIV, S/N: 1085 N88GA Page 2 Fabricated and installed a new cockpit curtain and track assembly, F.S. 73. Curtain is constructed from 100% wool pleated and sewn to the dimensions of 67.0" high and 24.0" wide. Curtain slides with nylon curtain guides on a curtain track P/N: 9046 fastened to the headliner MS hardware. Curtain is retained in the open position with two straps fabricated from same material as curtain and snaps. Electrical aspects covered separately. Cabin interior compartment placards description detailed in K-C Aviation drawing GIV-25.01-218 and layout per drawing GIV-25.04-218. Fasteners torqued using AC43.13-1A chapter 5 as a guide. Corrosion protection accomplished using AC 43.13-1A chapter 6 as a guide. Weight and balance accomplished using AC43.13-1A chapter 13 and the aircraft manufacturer's weight and balance manual as a guide. Materials used meet the requirements of FAR 25.853. The aircraft weight and balance manual and equipment list revised. END SDNYGIvl_02754098 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241020 EFTA01326613 SDNY_GM_02754099 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241021 EFTA01326614 T. • i • IiF rM Approved q I I il . • OMB NO. 2120-0020 imb , :0, JAN — 91 6p.?7, il,IAJOR REPAIR AND ALTERATION t0000101 (Airframe, ;v Powerplant, Propeller, or Appliance) Office Ide F:trifi FcaAA Use °ifil ri..13 OCTieff4S-: tsrent or type all entries. See FAR 43.9, FAR 43 Appendix B.andAC 43.9-1 (or subsequent revision thereof) tor instructions and disposition of this form. This report is required by law (49U.S.C. 1421). Fa lure to report can result Ina civil penalty not to exceed S1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make ModelG-IV Gulfstream Aerospace 1. Aircraft Serial No. Nationality and Registration Mark 1085 N88GA Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner Coca-Cola Enterprises, Inc. 2500 Windy Ridge Parkway Atlanta, Georgia 30338 3. For FAA UslrOMt I fUrtl-i ti -U4i 5...filintiJFtliri lOhlq I I hitU FIEHIN t•UlYie Itb Wit H I It AYFLIUMULt AIM/KA-CI HIrsik&S REQUIREMENTS AND IS APPROVED FOR THE ABOVE DESCRIBED AIRCRAFT, SUBJECT TO CONFORMITY INSPECTION BY A PERSON AUTHORIZED IN F 43, SECTION 43.7. -11 VI Vie StuNAt UR . 4. Unit IdenTfiggiart FAA MKE FS • • Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in !tern 1above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer 8 Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. V.S. Certificated mechanic K-C Aviation, Inc. Foreign Certificated Mechanic 301 Discovery Drive y certificated Repair Station Appleton, WI 54915 manwactunw QK2R112L O. I certify that the repair and/or alteration made to the un t(s) identified in item 4above and described on the reverse or attachments hereto have been made In accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein Is true and correct to the best of my knowledge. Date Signature of Authorized Individual DEC 0 9 1996 7. App a for Return To Service Pursuant to the authority given persons specified below, the unit Identified in item 4 was inspected In the manner prescribed by the Administrator of the Federal Aviation Administration and is ikAPPROVED O REJECTED FAA Flt. Standards Other (Specify) Inspector Manufacturer Inspection Authorization BY FAA Designee x Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection Certificate or Signature of Authorized Ind idual Designation No. DEC 18 1996 QK2R112L C stsre. d . FAA Form 337 112•0 SDNY_GM_02754100 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241022 EFTA01326615 NOTICE Weight and balance or operating limitation changes shall be entered in the approprlate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (lf more space is required, attach additional sheets. identity with aircraft nationality and registration mark and date work completed.) Reworked existing left vestibule entertainment cabinet at F.S. 144 as follows: Removed the following equipment: 1) Stereo cassette deck, Sony P/N: TC-WR808M 2) Stereo amp, Sony P/N: TA-808M 3) AM/FM tuner, Sony P/N: ST-707RM 4) CD player, Sony P/N: CDP-5107 5) Video switch, ASINC P/N: 912001 6) VCR, Panasonic P/N: F85A30987 7) Video monitor, Sony P/N: PVM-2030 8) Video distribution amp, United P/N: PD-6 9) Removed upper shelf and compartment doors retaining forward and aft bulkheads. 10) Relocated existing data loader P/N: DL-800 from upper cabinet to right vestibule upper crew cabinet. Fabricated and installed new replacement compartment cabinet to accommodate new ententainment equipment and provide miscellaneous storage. Compartment cabinet peripheral is conitructed.,from,ML610-10111-V5 Aluminum honeycomb panel assembled together in accOrdance-withi0C Aviation PrdbUOPecification 116. Overall dimensions of cabinet are 34.5" high, la".5" wide and 24.125" deep. Cabinet contains two compartments, an upper removable entertainment cabinet fabricated similarly to compartment cabinet using NL610-10111-250 aluminum honeycomb panel. Cabinet dimension are 17.25" high, 18.5" wide and 14.5" deep and contains mounting provisions for the following new equipment: 1) CD magazine or tape storage 3) AM/FM cassette player, Alpine P/N: TDA7552 3) CD changer, Sony P/N: CDX-91 4) CD controller, Sony P/N: RM-X59RF 5) VCR, Panasonic P/N: PV4662 Lower compartment dimensions are 16.0" high. 18.0" wide and 24.125" deep and is used for miscellaneous storage. The overall compartment cabinet is retained to the existing lower compartment structure and bulkheads using MS hardware and threaded inserts installed per K-C Aviation Process Specification 105. Entertainment and miscellaneous storage compartment are closed out with a hinged doors ancActron positive type latches. Fabricated and installed a new tapes and CD storage drawer in lower compartment. Overall dimensions are 5.0" high, 18.5" wide and 23.0" deep. Door is hinged with Brusso L23 knife hinges and retained in the closed position using an Actron positive type latch P/N: A23060-9. Entertainment cabinet compartments maximum placarded weights are as follows: 1) Upper CD magazine and tape storage compartment - 5.0 Lbs. 2) Miscellaneous storage compartment - 25.0 Lbs. 3) Fitted tapes/disc storage drawer - 25.0 Lbs. Electrical aspects covered separately. All metal fabrication practices per K-C Aviation Process Specification 106. All threaded fastener installations per K-C Aviation Process Specification 105. Fabrication of bulkheads, cabinets, drawers and doors per K-C Aviation Process Specification 116. Cabin interior compartment placards description detailed in K-C Aviation drawing GIV-25-01-218 and layout per drawing GIV-25.04-218. Fasteners torqued using AC43.13-1A chapter 5 as a guide. Corrosion protection accomplished using AC 43.13-1A chapter 6 as a guide. Weight and balance accomplished using AC43.13-1A chapter 13 and the aircraft manufacturer's weight and balance manual as a guide. Materials used meet the requirements of FAR 25.853. The aircraft weight and balance manual and equipment list revised. END 0 Additional sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: 1912-769-0I2/601S7 SDNY_GM_02754101 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241023 EFTA01326616 Form Approved OMB No. 2120-0020 I MAJOR REPAIR AND ALTERATION For FAA Use Only uS — 6 Pgirtramd, Powerplant, Propeller, or Appliance) , Office Identific2o22; 'Ihalt• ' Onkel*, _INSTRUCTIONS: Print or type all ntries. See FAR 43.9. FAR 43 Appendix B.and AC 43.9-1 (or subsequent revision thereof) for Instructions and disposition of thirferTrii. port is required by law 09 U.S.C. 1421). Failure to report can result in a civil penalty net to exceed 51.000 for each such violation (Section 901 Federal Aviation Act of 1958). Make model GULFSTREAM AEROSPACE GIV 1. Al ft Serial No. Nationality and Registration Mark 1085 N88GA Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner COCA-COLA ENTERPRISES INC 2500 WINDY RIDGE PARKWAY ATLANTA, GA 30338 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6. Conformity SlatomeM A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Certificated Mechanic K-C AVIATION INC. Foreign Certificawd mechanic 301 DISCOVERY DR. X1 Cenificated Revak Station QK2R112L APPLET0N, WI 54915 . manufacturer 0. I Certify that the repair andior alteration made tothe un fts) identified in item4 above and described on the reverse or attashmentshereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized Individual DEC 16 1996 1.50-nitle,-te 4., 7. Approval for Return To Service Pursuant to the authority given persons specified below, the unit Identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is (1) APPROVED 0 REJECTED FAA Fit. Standards I Other (Sandy) Manufacturer Inspection Authorization i Inspector BY XX Repair Station Person Approved by Transport FAA Designee Canada Airworthiness Group Date of Approval or Remotion Certificate or Signature of Authorized Individual Designation No. DEC 18 1996 OK2R112L ( loin. tlLZ2 FAA Form 337 .12 or SDNYGtvl02754102 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241024 EFTA01326617 NOTICE Weight and balance oroperating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished pl more space is required, attach additional sheets. Identity with aircraft nationality and registration mark and date work completed.) Installed a GTE/Magnavox C-2000 Digital Airborne Telephone System consisting of: 1 Ea. Air Radio Telecommunications Unit (ARTU), P/N 724855-801 1 Ea. ARTU Rack, P/N 724868-802 1 Ea. Duplexer, P/N 620317-1 3 Ea. Cabin Data Bus Repeater (CDBR-1), P/N 724864-801 '1 Ea. Cabin Data Bus Repeater (CDBR-2),'P/N 902205-803 1 Ea. CAS Unit, P/N 725256-801 1 Ea. Analog Interface Unit (AIU), P/N 724986-801 4 Ea. Phone Assembly, P/N 724866-801WH, -805PL, & -807PL 1 Ea. Antenna, P/N 902131-2 Two Global Wulfsberg Flitefone VI Radio Telephone Systems were removed to facilitate this installation. Removed components consist of: 2 Ea. GWS RT-18D Transceivers, P/N 400-0125-000 2 Ea. GWS WH-I0 Flitefone VI Handsets The newly installed antenna is located on the underside fuselage at FS 100 as per KCA Structural Drawing: Radio Telephone Antenna Installation, 1159-23-01-301, sht. 1, of which the structural aspects are DER approved by M. Lieblich, FAA DER SW-811. The C-2000 system wiring accomplished as per K-C Aviation Drawing: Radio Telephone, GIV-31085-23-98, of which the electrical/electronic aspects are DER approved by N. Kopesky, CHI-262. Existing wiring diagrams affected by the above referenced systems are revised to reflect changes in system design or interface to the newly installed or modified systems as appropriate. All new single conductor wire meets MIL 22759/16 and all new multi-conduc- tor shielded wire meets MIL 27500. All work done IAW AC43.13-2A Chapters 1, 2 & 3 and manufacturers installation data. Aircraft equipment list and weight & balance manual revised. END ❑ Additional Sheets Are Attached GU.5. GOVERNMENT PRINTING OPPICC: It02-769-0I2/60I37 SDNY_GM_02754103 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241025 EFTA01326618 ir g /415-7 ! • • ' ' . , • Form Approved OMB No. 2120-0020 ! I MA,JOR REPAIR AND ALTERATION For FAA Use Only 1 6 I;TAiriniOi , Powerplant, Propeller, or Appliance) Office Identification. R ./.1 INSTRUCTIONS:Print or type:ties. Se•FAR 43.9. FAR 40 Appendix B. and AC43.9-1 (or subsequent revision thereof) for instructions —enddisposition of thisiormitt rt is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty nol to exceed $1.000 tor each suc violation (Section 901 Federal Aviation Act of 1958). Make Model GULFSTREAM AEROSPACE GIV 1. Aircraft Nationality and Registration Mark Serial No. 1085 N88GA Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner COCA-COLA ENTERPRISES INC 2500 WINDY RIDGE PARKWAY ATLANTA, GA 30338 3. For FAA Use Only 4. Unit Identification 5. Tyr). Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item I above) X POWERFLANT PROPELLER Type APPLIANCE Manufacturer & Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.& Certificated Mechanic K-C AVIATION INC. Foreign Certificated Mechanic 301 DISCOVERY DR. XX Certificated Repair Station QK2R112L APPLETON, WI 54915 manufacturer D. I certify that therepair and/Or alteration made to the un Its) identified in item 4 above and described on the reverse or attachmentshereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information - furnished herein is true and correct to the best 01 my nowledge. Date Signature of Authorized Individual DEC I 6 1966 CFP6424, A t t , Z,e r 7. Approval for Return To Service Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the mariner prescribed by the Administrator of the Federal Aviation Administration and is 01 APPROVED 0 REJECTED FAA Flt. Standards Other (Specify) I Inspector Manufacturer Inspection Authorization BY I FAA Designee XX Repair Station Person Approved by Transport 111 Canada Airworthiness Group Date of Approval or Rejection Certificate or Signature of Authorized Individual Designation No. DEC 181998 QK2R1I2L C14,-. , ' *- ,_ FAA Form 337 .12 MP) SDNYGivl_02754104 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241026 EFTA01326619 NOTICE Weight andbalance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (II more space Is required. attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Installed an Allied Signal Satellite Data Communications System (SDCS), interfaced to the existing Airborne Flight Information System (AFIS). The AFIS system is integrated with the GAC installed Honeywell Flight Management Systems providing complete flight plan and weather information through self-contained VHF COMM data link with the Global Data Center. The SDCS is interfaced to the AFIS and provides additional cabin/cockpit communication capabilities. Installed SDCS system components include: 1 Ea. Satellite Comm Unit (SCU), P/N 153-017311-01 1 Ea. SCU Antenna, P/N 121-017537-01 (Sensor P/N S65-8282-101) 1 Ea. HPA/LNA, P/N 153-017310-01 The SCU Antenna is installed as FS 265 in accordance with KCA Dallas structural drawings; 447-5338, of which the structural are DER approved by M. Lieblich, SW-811. The SCU is located in the R/H radio rack extension and the HPA/LNA is located in the R/H cabin sidewall at FS 250 on existing structure. Refer to KCA Drawing: AFIS/SDCS, GIV-31085-34-63, of which the electrical/electronic aspects are DER approved by N. Kopesky, CHI-262. Existing wiring diagrams affected by the above referenced systems are revised to reflect changes in system design or interface to the newly installed or modified systems as appropriate. All new single conductor wire meets MIL 22759/16 and all new multi-conduc- tor shielded wire meets MIL 27500. All work done IAW AC43.13-2A Chapters 1, 2 & 3 and manufacturers installation data. Aircraft equipment list and weight & balance manual revised. END 0 Additional Sheets Aro Attached *U.S. 00VCIIHMENT PRINTINCt OIPICI 1192-70-012/10157 SDNY_GM_02754105 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241027 EFTA01326620 rirc.-7,77 . Form Approved O., . 3M - 6(Akira or i 1.997M , won REPAIR AND ALTERATION • of owerplant, Propeller, or Appliance) OMB No. 2120-0020 For FAA Use Only Office Identificaip2 i i onmsan INSTRUCTIONS:Print or typea en les. See FAR 43.9. FAR 43 Appendix B. and AC43.9-1 (or subsequ nt revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed 51.000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model GULFSTREAM AEROSPACE G-IV 1. Aircraft Serial No. Nationality and Registration Mark 1085 N88GA Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner COCA-COLA ENTERPRISES INC. 2500 WINDY RIDGE PARKWAY ATLANTA GA. 30338 3. For FAA Use Only ',The dna Identif fed herein compiles with the applicable airworthiness requirements oral I. approved for the above described aircraft subject to conformity inspectin by a parsers authorized in FAR 43, Section 43.7". Date DEC 1 0 ME IAA Inspecte 61.13 4. Unit Identification 8. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described In horn 1above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer 8 Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. US. ceniHeated Mechanic K-C Aviation, Inc. Foreign Cenificated mechanic 301 Discovery Drive X Cenificated Repair Station Appleton, WI 54915 Manufacturer QK2R112L D. !certify that the repair and/or alteration made to the un t(s) identified in item 4 above and described on t e reverse orattachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized Individual DEC 1 0 1996 47-ser/V er,IZZ---• 7. Approval for Return To Service Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is XX APPROVED CI REJECTED FAA Fit Standards Other (Specify) Inspector Manufacturer Inspection Authorization BY FAA Designee Person Approved by Transport x Repair Station Canada Airworthiness Group Date of Approval or Rejection Certificate or Signature of Authorized Incrvidual Designation No. DEC 18 1996 QK2R112L cap.,- • FAA Form 337 ono SDNYGlvl_02754106 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241028 EFTA01326621 NOTICE Weight and balance or operating limitation changes shall be enteredin the appropriate aircraft record. An alteration must be conipatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required. attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Modified the previously installed Galley and Cabin electrical system by removing previously installed equipment and wiring and installing new equipment and associated wiring. Installed the following equipment: lea Nordskog HI Temp Oven P/N: 50231L. lea Microswitch Leaf Actuator P/N: JV-26. lea Rotron Fan P/N: FS24H3. lea Tappan Microwave Oven P/N: TMS083E1S0. lea Krups Coffee Maker P/N: Pro-Cafe. 2ea Grimes Light Assembly P/N: 34170-1. lea Audio Int. High Current Control P/N: MSM285. lea Audio Int. Aft Lav Switch Panel P/N: SPS-4-1-1759. lea Audio Int. Aft VIP Switch Panel P/N: SPS-5-3-1761. lea Audio Int. FWD VIP Switch Panel P/N: SPS-5-3-1753. lea Audio Int. Divan Switch Panel P/N: SPS-4-1-1762. lea Audio Int. Divan Switch Panel (Master) P/N: SPS-4-1-1758. lea Audio Int. R/H Galley Switch Panel P/N: SPS-6-2-1754. 2ea Audio Int. Credenza PSU Switch Panel P/N: SPS-3-1-1757. 4ea Audio Int. Passenger Service Unit Switch Panel (PSU) P/N: SPS-4-1-1756. 4ea Audio Int. PSU Switch Panel (Master) P/N: SPS-4-1-1755. lea Audio Int. Vestibule Switch Panel P/N: SPS-6-1-1760. Wiring for the newly modified / installed Galley and Cabin electrical systems is per K-C Aviation,Inc electrical drawings: Electrical Power Distribution (Galley Power), GIV-24-1085-100 (Sheets 1 & 2); Galley and Cabin Electrical Interface, GIV-24-1085- 110 (Sheets 1 thru 3); Water Drain System, Water/Drain Heaters (Digital Switching), GIV-38-1085-112 (Sheets 1 & 2) and Electrical Switching and Control GIV39-1085-126 (Sheets 1 thru 9). Structural aspects of the newly installed/modified Galley and Cabin electrical systems are approved separately. Existing aircraft wiring diagrams affected by the above installation/modification are revised to reflect changes in system design or their interface to newly installed or modified systems as appropriate. All new single conductor wire meets MIL 22759/16 and all new multiconductor shielded wire meets MIL 27500. All work done IAW AC43.13-2A chapters 1 & 2 and manufacturers installation data. Aircraft equipment list and Electrical Load Analysis revised. Aircraft reweighed. END ❑ Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: 1112-761-012/G0IST SDNY_GM_02754107 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241029 EFTA01326622 6 ) f li r , , t& Oewoment t ' MAJOR REPAIR AND ALTERATION .i Form Approved OMB No. 2120-0020 For FAA Use Only ' twai.1 — 6 (Airframe); Powerplant, Propeller, or Appliance) Office identigption OF ttl~ ..• I 4STRUCTIONS: Print or type all envies. See FAR 43.9. FAR 43 Appendix B. and AC 43.9-1 (or subsequ nt reviSiOn then:eel) for instructions matklispositionof.thisloanahimapart is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not toexceed51.000 for each such violation (Section 901 Federal Aviation Act of 1958). make Model GULFSTRENI AEROSPACE G-IY 1. Aircraft Serial No. Nationality and Registration Mark 1085 Ni38GA Name (As shown on registration certificate) Address (As shown on registration certificate) 2. owner COCA-COLA ENTERPRISES INC. 2500 WINDY RIDGE PARKWAY ATLANTA GA. 30338 3. For FAA Use Only oThe dateallIIIIIIIIIIIrldentif led herein =plies with the applicable •Irworthinesa requirements and Is approved for the tows disarmed aircraft subject to cceiformi ty inspection by a person authorized in FAR 43, antigen 43.70. Date DEC 1 0 1996 FM Inspector CUM 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6 Conformity Statement A. Agencys Name and Addres B. Kind of Agency C. Certificate No. U.S. Certificated Mechanic K-C Aviation, Inc. Foreign Cenificsted Meenanie 301 Discovery Drive I Cen Manufacturer D. I certify that therepair and/or alteration made to theun t(s) identified in item 4aboveand described on the reverse or attachments hereto have been made in accordance with the requirements of P rt 43 of the U.S. Federal Aviation Regulations and that the information furnished herein Is true and correct to the best of my nowledge. Date Signature of Authorized Individual DEC 10 1996 e f ewa4/A°' / 0- 7..:, 7. Approval for Return To SeMce Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is XX APPROVED 0 REJECTED FAA Eli Standards Other (Specify) Manufacturer inspection Authorization inspector BY FAA Designee x Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection Certificate or Signature of Authorized Indivdual Designation No. DEC 18 1996 0K2R1121. Catfrp.., c FAA Form 337 meat SDNY_Giv1_02754108 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241030 EFTA01326623 NOTICE • Weight andbalance or operating limitation changes shall be enteredin the appropriate aircraft record. An alteration must be corripatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required. attach additional sheets. Identity with aircraft nationality and registration mark and date work completed.) Removed the previously installed cabin and lavatory lighting system and installed a new cabin and lavatory lighting system with Ordinance Signs consisting of the following equipment: 3ea Aerospace Lighting Corp, Lighting Inverter P/N: AL-0581. , 18ea ALC Lighting Power Supply P/N: AL-5112. 2ea ALC Lighting Power Supply P/N: AL-2000. lea Grimes Light Assembly P/N: B3550. 2ea Grimes Light Assembly P/N: 34170-1. lea Luminator Light Assembly P/N: L16256-1. 21ea Wemac Light Assembly P/N: 2520-3. lea Bruce Industries Ordinance Sign P/N: BR9206-907. 4ea Wemac Ordinance Sign P/N: 3585. Wiring for the newly installed cabin and lavatory lighting systems are per K-C Aviation,Inc electrical drawings: Feature Panel Lighting (Digital Switching), GIV- 33-1085-111; Overhead Cabin Lighting (Digital Switching), GIV-33-1085-122; Vestibule Dome & Boarding Light, GIV-33-1085-114; Reading and Table Lights (Digital Switching), GIV-33-1085-115; Ordinance Lights, GIV-33-1085-125; Lav Lighting, GIV- 33-1085-106; Cabin Aisle Lights, GIV-33-1085-102 and Cabin Terminal Junctions, GIV- 39-1085-128. Structural aspects of the newly installed cabin and lav lighting systems are approved separately. Existing aircraft wiring diagrams affected by the above installations are revised to reflect changes in system design or their interface to newly installed or modified systems as appropriate. All new single conductor wire meets NIL 22759/16 and all new multiconductor shielded wire meets MIL 27500. All work done IAN AC43.13-2A chapter 1 & 2 and manufacturers installation data. Aircraft equipment list revised. Aircraft reweighed. END 0 Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: Illt2-769-012/60157 SDNY_GM_02754109 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241031 EFTA01326624 11.5 (q;1 , • I.: V; i *; I . • • • Form Approved OMB No. 2120-0020 NII9OR REPAIR AND ALTERATION US Identillcati7Use For FAA Only - 6 gmrtnint Powerplant, Propeller, or Appliance) Office 1.." ICISTRUCTIONS.Print or type all e nes. See FAR 43.9, FAR 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for Instructions .loadisposition attlaisforro,Thittegort is required by law (4(1U.S.C.1421). Failure to report can result Inacivil penalty not to exceed $1.000 for each such violation (Section 901federal Aviation Act of 1968). Make Model GULFSTREAN AEROSPACE G-IV 1. Aircraft Serial No. Nationality and Registration Mark 1085 N88GA Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner COCA-COLA ENTERPRISES INC. 2500 WINDY RIDGE PARKWAY ATLANTA GA. 30338 3. For FAA Use Only *The data /a identified herein carpi fee with the applicable airworthiness requirements and is approved for the above sneer ibad aircraft stasJect to conformity inspection by a person authorized in FAR 43, Section 43.74. Date DEC 1 0 100$ FM Inspectorr ie r 0u3 4. Unit identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6 Conformity Statement A. ngeneys Name and Address B. Kind of Agency C. Certificate No. . U.S. Certificated MeChenie K-C Aviation, Inc. Foreign Coniticaled Mechanic 301 Discovery Drive X Certificated Repair Malian Appleton, WI 54915 manufacturer QK2R112L D. Icertify that the repair and/or alteration madeto the un t(s) identified in item 4 above and described on the reverseor attachmentshereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized Individual DEC 10 1996 101.04 /1,r,..11*.Z.:4 7. Approval for Return To Service Pursuant to the authority given persons specified below, the unit Identified In item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is =APPROVED 0 REJECTED FAA Flt. Standards Other (Specify) Inspector Manufacturer Inspection Authorization BY FAA Designee Repair Station Person Approved by Transport X Canada Airworthiness Group Date of Approval or Rejection Certificate or Signature of Authoriz Individual Designation No. DEC 18 1996 QK2R112L (14..40 s, - FAA Form 337 (12461 SDNY_GM_02754110 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241032 EFTA01326625 NOTICE Wert and balance or operating limitation changes shallbe entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. • 8. Description ofWorkAccomplIshod Olmom spacers required. attach additional sheets. with aircraft nationalityandlegistralionmade and date work completed.) Removed the previously installed cabin audio and entertainment systems in their entirety and installed a new cabin audio and entertainment system consisting of the following equipment: 10ea Audio International Headphone Control Panel P/N: HSP-037-1. 10ea Baker Speakers P/N: HF93. 2ea Quam Speakers P/N: 4C5Z8. 4ea Baker Subwoofer Speakers P/N: LF91. lea BBE Sonic Maximizer P/N: SM-4012. lea Collins ATR Rack P/N: 622-1196-001. lea Stereo/PA Amplifier P/N: M3070M. lea Archer Amplified Coupler P/N: 151116. lea Audio Int. Video Switcher P/N: VSSO4. lea Audio Int. Video Switcher P/N: VSS04T. lea Audio Int. Audio Switching Controller P/N: MSM2804. 4ea Baker Audio PreAmp/Power Supply P/N: M1084PS. 2ea Audio Int. Infrared Receiver/Transmitter P/N: IFR9A-A-38. lea Alpine FM/AM Cassette P/N: TDA7552. 2ea Baker 14" LCD Monitor P/N: 990-4110-002. 2ea Panasonic VHS Hi-Fi VCR P/N: PV-4662. lea Sony CD Changer P/N: CDX91. lea Sony CO Controller P/N: RMX59RF. lea Airshow Genesys DCU P/N: 920060. lea Airshow Short Mount P/N: 914026. lea Asinc TTD Controller P/N: 911010-2. lea Audio Int. Mouse Switch Panel P/N: SP-450-1. lea Rosen 6.4" LCD Monitor P/N: RLCD64-1-1ACB. lea Rosen Power Converter P/N: RISR-28-12-6. Wiring for the new cabin audio and entertainment systems is per K-C Aviation,Inc electrical drawings: Cabin Audio, GIV-31085-23-61 (Sheets 1 thru 4); Cabin Entertainment, GIV-31085-23-62 (Sheets 1 thru 9) and Airshow, GIV-31085-31-52 (Sheets 1 & 2). Structural aspects of the newly installed cabin audio and entertainment systems are approved separately. Existing aircraft wiring diagrams affected by the above modification/installation are revised to reflect changes in system design or their interface to newly installed or modified systems as appropriate. All new single conductor wire meets MIL 22759/16 and all new multiconductor shielded wire meets MIL 27500. All work done IAN AC43.13-2A chapter 1 & 2 and manufacturers installation data. Aircraft equipment list revised. Aircraft reweighed. END ❑ Additional Sheets Are Attached *us GOVERNMENT PRINTING OFFICE: I992-769-011/60137 SDNY_GNL02754111 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241033 EFTA01326626 • Form Approved OMB No. 2120-0020 . -=--.- 1'f• AJOR REPAIR AND ALTERATION Ilmn mere vs For FAA Use Only II s a 6 I-Cir:,.(A fri t es Powerplant, Propeller, or Appliance) Office Identilicfroni3 I I INSTRUCTIONS.Print or ry alI entries. See FAR 43.9, FAR 43 Appendix El B. and AC43.9-1 (or subsequent revision thereof) for instructions --anddispositionPi form. This eport is required by taw (49 U.S.C. 1421). F Ilure to report can result in a civil penalty not to exceed S1,000 for each such violation ( 110n 01 Federal Aviation Act of 1958). Make Model GULFSTREAN AEROSPACE G-IV 1. Aircraft Serial No. Nationality and Registration Mark 1085 . N88GA Name (As shown on registration certificate) AddreSS (As shown on registration certificate) 2. Owner COCA-COLA ENTERPRISES INC. 2500 WINDY RIDGE PARKWAY ATLANTA GA. 30338 3. For FAA Us* Only •The data/FS identified herein complies with the applicable airworthiness requirements and is approved for the above discribed aircraft abject to conformity inspection by a person authorized in FAR 43, Section 43.70. Date DEC10 1996 FAA Inspect . GL13 4. Unit Identification S. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As deserted in item I above) X • POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6 Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Certificated mechanic K-C Aviation, Inc. Foreign Certificated Methanic 301 Discovery Drive y certificated Revak Station Appleton, WI 54915 amubOwer 0K2R112L D. I certify that therepairand/oralteration made to the un t(f) identified in item4 above and described on thereverse orattachmentshereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized Individual DEC 1 0 1896 odoe. 4Y/ent-- T. Approval for Return To Service Pursuant to the authority given persons specified below, the unit Identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and Is )(It APPROVED 0 REJECTED FAA Fit. $IBMard9 Other (Specify) Inspector Manufacturer Inspection Authorization BY FAA Designee Repair Station Person Approved by Transport X Canada Airworthiness Group Dateof Approval or Rejection Certificate or Signature of Authorized Individual Designation No. DEC 18 1886 RK,R119L C20w-wr c 16.-: FAA Form 337 0240 SDNYGIvl02754112 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241034 EFTA01326627 NOTICE Weight and balance or operating limitation changes shallbe enteredin the appropriate aircralt record. An alteration must be coMpatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. identify with aircraft nationality and registration mark and date work completed.) Modified the previously installed 115 VAC 60Hz Conveiter system by installing new outpu wiring to the existing galley circuit breaker panel and adding (6ea) new 115VAC outlets per K-C Aviation, Inc. electrical drawing: 115VAC 60Hz Converter, GIV-24-1085-147 and Utility Outlets, GIV-24-1085-146. Structural aspects of the newly modified 115VAC converter system are considered minor. Existing aircraft wiring diagrams are revised to reflect changes in system design or their interface to newly installed or modified systems as appropriate. All new single conductor wire meets MIL 22759/16 and all new multiconductor shielded wire meets MIL 27500. All work done IAW AC43.13-2A chapters 1 & 2 and manufacturers installation data. Aircraft equipment list and weight & balance revised. END ❑ Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: 1992-769-M/60157 SDNY_GM_02754113 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024I035 EFTA01326628 i)N(e-'71 • PI o J.:40 — 6 -,- l'.;::,t i MA OR REPAIR AND ALTERATION (Airfr# , Powerplant, Propeller, or Appliance) Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification A. tidnumtromm - -4//_.; —4 • INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B. and AC 43.9.1 (or subsequent revision thereof) for instructions and disposition el this form. This report is required by law (49 U.S.C. 1421). Failure to report can result ina civil penalty not to exceed 51.000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model GULFSTREAM AEROSPACE G-IV 1. Aircraft Serial No. Nationality and Registration Mark 1085 N88GA Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner COCA-COLA ENTERPRISES INC. 2500 WINDY RIDGE PARKWAY ATLANTA GA. 30338 3. For FAA Use Only •The data, identified herein complies vi h the applicable airworthiness readrements rd is reproved for the above discribed aircraft subject to conformity irapection by a person authorized in FAR 43, Section 43.7a. Date DEC 1 0 1996 FM Inspector • C- - - 61.13 4. Unit Identification S. Type Unit Make Model Serial No. Repair Alteration AIRFRAME . . (As described in Item 1above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6 Conformity Statement A. Agency's Name and Address 8. Kind of Agency C. Certificate No. U.S. Certificated mechanic K-C Aviation, Inc. Foreign Caelificated mechanic 301 Discovery Drive x oolitic's«, rt.pattsumto,, Appleton, WI 54915 Manufacturer QK2R1I2L O. I Certify that the repair andlor alteration made to the un t(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Pan 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized Individual DEC 1 0 1996 c 6,..3„.47,e,"Z:e-.... 7. Approval for Return To Service Pu suant to the authority given persons specified below, the unit identified in Item 4 was Inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is XXAPPROVED Cl REJECTED FAA Fit. Standards Other (Specify) Inspector Manufacturer Inspection AuthOdzation BY FAA Designee Repair Station Person Approved by Transport A Canada Airworthiness Group Date of Approval or Rejection Certificate or Signature of Authorized Individual Designation No. DEC 18 1996 OK2R112L 570,--- t d —IL FAA Form 337 112481 SDNYGIvl02754114 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241036 EFTA01326629 NOTICE Weight and balance or operating limitation changes shallbe entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (It more space is required. attach additional sheets. Identity with aircraft nationality and registration mark and date work completed.) Modified the existing electric toilet system by installing a new Lav Switch Panel P/N: SPS-4-1-1759 per K-C Aviation,Inc electrical drawing: Electric Toilet, GIV-38- 1085-101. Structural aspects of the modified electric toilet are considered minor. Modified the previously installed electric window shade system by installing new wiring and new passenger Service Unit Switch Panels per K-C Aviation,Inc electrical drawing: Electric Window Shades, GIV-25-1085-127. Structural aspects of the newly modified electric window shades are considered minor. Installed wiring for (2ea) new electrical adjusting passenger seats per K-C Aviation, Inc electrical drawing: Electric Chairs, GIV-24-1085-129. Structural aspects of the new electrical adjusting seats are approved separately. Existing aircraft wiring diagrams affected by the above modifications or installations are revised to reflect changes in system design or their interface to newly installed or modified systems as appropriate. All new single conductor wire meets MIL 22759/16 and all new multiconductor shielded wire meets MIL 27500. All work done IAW AC43.13-2A chapter 1 & 2 and manufacturers installation data. Aircraft equipment list and weight & balance revised. END ❑ Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: 166x-766-01L6016T SDNY_GNL02754115 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241037 EFTA01326630 • - Form Approved I ; i \ .. f . C l :. illiVOR REPAIR AND ALTERATION OMB No. 2120-0020 uS4in:crimen ? 6 r,cyxAirt e, Powerplant, Propeller, or Appliance) For FAA Use Only Office IdentifiesIon in Airnirisnotion I) 6".Z.1-, J INSTRUCTIONS: Print or type a I entries. See FAR 43.9, FAR 43 Appendix B. and AC43.9-1 (or subsequent revision thereof) for Instructions - anddisposition of thiSform...112dreport is required by law (49 U.S.C. 1421). Failure to report can result in &civil penaitynot to exceed 51.000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model GULFSTREAM AEROSPACE G-IV 1. Aircraft Nationality and Registration Mark Serial No. 1085 N88GA Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner COCA-COLA ENTERPRISES INC. 2500 WINDY RIDGE PARKWAY ATLANTA GA. 30338 3. For FAA Use Only "The data. (dentif fed herein cowlles with the applicable airworthiness requirements ard is approved for the above described aircraft subject to conformity inspection by a person authorized in FAR 43, Section 43.7s. Date nFe 1 n 1005 FM I nspectr,, i - SI.13 4. Unit Identification 5- Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item I above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer S. Conformity Statement A. Agency's Name and Address 8. Kind of Agency C. Certificate No. . US. Certificated Medtanic K-C Aviation, Inc. Foreign Certificated Mechanic 301 Discovery Drive Certilkated Midair Station X QK2R112L Appleton, WI 54915 Manufacturer 0. I certify that the repair and/or alteration made to the un t(s) identified In item 4 above and described on the reverse or attachments hereto have been made In accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is trUltand correct to the best of my knowledge. Date . Signature of Authorized Individual DEC 1 0 1996 d.sesmi.A° 7 7“. 7. Approval for Return To Service Pursuant to the authority given persons specified haw, the unit identified in item 4 was Inspected in the manner prescribed by the • Administrator of the Federal Aviation Administration and is X APPROVED 0 REJECTED FAA Fit. Standards Other (Specify) Inspector Manufacturer Inspection Authorization BY FAA Designee x Repair Station Person CanadaApproved by Transport Airworthiness Group Dale of Approval orRejection Certificate or Signature of Authorized Individual Designation No. DEC 1 8 1996 QK2R112L 'gen,. FAA Form 337 id.ed SDNYGIv1_02754116 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024I038 EFTA01326631 NOTICE Weight and balance oroperating limitation changes shall be enteredin the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is ICQUired, attach additional sheets. Identity with aircraft nationality and registration mark and date work completed.) Modified the previously installed Cabin Call System per K-C Aviation,Inc. electrical drawing: Call System, GIV-33-1085-124. Structural aspects of the modified Cabin Call System are considered minor. All work done TAW AC43.13-2A chapter 1 & 2. Aircraft equipment list, Electrical Wiring Manual revised. Aircraft reweighed. END O Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: t992-769-012/60157 SDNY_GM_02754117 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241039 EFTA01326632 L. . \--. . Form Approved OMB No. 2120.0020 MAJOR REPAIR AND ALTERATION nw • msm 3 0 'Airframe, .I..:> Powerplant, Propeller, or Appliance) For FM Usa Only Office IdentifiZ fowMm j n 1.. fri INSTRUCTIO • ' tries. See FAR 43.9.FAR 43 Appendix B, arr AC43.9-1 (or subsequent revision thereof) for instructions t of this form. This report is required by law (49 U.s. .1421). Failure to report can result in a civil penalty not to exceed$1,000 for each such violation (Section 901 Federal Aviation Act of 1858). Model WdrFSTREAM AEROSPACE G-IV 1. Aircraft Serial No. Nationality and Registration mark 1085 N88GA Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner MELLON FINANCIAL SERVICES CORP #3 4444 ONE MELLON BANK CENTER PITTSBURGH, PA 15258 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Certificated mechanic K-C Aviation, Inc. Foreign Canificated mechanic 301 Discovery Drive X Certificated Repair Station Appleton. WI 54915 Manulacturer QK2R112L D. I certify that the repair and/or alteration made to the un t(s) dentifled In item 4 above and described on the reverse or attachments hereto have been made In accordance with the requirements of Pan 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Data Signature of Autho zed WU 'dual SEP 2 4 1996 7. Approval for Return To Service Pu suant to the authority given persons specified belOve, the unit identified in item 4 w peeled In the manner prescribed by the Administrator of the Federal Aviation Administration and s ,R. APPROVED 0 REJECTED FM Flt. Standards Manufacturer Inspection Authorization Other (Specify) Inspeet.or Inspect BY FAA Designee Person Approved by Transport x Repair Station Canada Airworthiness Group Date of Approvalor Rejection Certificate or Signature of Auth ed Individual Designation No. SEP 2 4 1996 QK2R112L (C421 C 1-- FAA Form 337 oar SDNY_GM_0275aile SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00241040 EFTA01326633 NOTICE Weight and balance or operating limitation changes shallbe entered in the appropriate aircraft record4seh.prati ust be compatible with all previous alterations fo assure continued conformity with the applicable ainvorfh I-- tits. 8. Description of Work Accomplished Of more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Repaired left (02 from outboard) and right outboard flap drive rods and ground existing structure that rod goes through in accordance with Gulfstream Aerospace Standard Repair Drawing 5E05807901. Removed left and right main gear forward trunnion bearings, removed corrosion in trunnion support and plated in accordance with Gulfstream Aerospace Standard Repair - Spherical Bearing - Main Landing Gear - Sponson Rib - Trunnion repair drawing 5E45732901. No weight and balance change. END 0 •Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: 1992-769-012/60IST SDNY_GM_02754119 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241041 EFTA01326634 017M41143•1 co wg?Inosircei..."'"".“nosmasherroArse "" • STANDARD AIRWORSHNSSS CERTIFICATE istfacM10•••••••00124 k RA --. att., --Is- -.0 NORGA cocrarReam / vxv LOSS ASSORT s-- .1 Yw °"`ARYCOSNEN% 12/14/88 CL atis— TAY (WO VMS CII•t0Call M CMPAII) •• 1 14 WIWI' w ACCOOISCII WPM AMON. Raft FAA Fain 11103-2 ww SONY GM 02754120 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15 EFTA 0024I042 EFTA01326635 SDNY_GM_02754121 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 00241043 EFTA01326636 Fee Armed 020 Na 21200720 MAJOR REPAIR AND ALTERATION For FAA Use Only 0 US Deponent of toreceubo• (Airframe, Powerplant, Propeller, or Appliance) office identification Fekel Medea elsothenneee ii 9—O7 INSTRUCTIONS- Print or typo all entries. See FAR 43.9. FAR 43 Appendix B. and AC 43.9.1 (or subsequent evision thereof) for instructions and eitsposillon of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model I. Aircraft Gulfstream Aerospace G -I V Serial No. Nationality and Registration Mark 1085 N88GA Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner MELLON FINANCIAL SERVICES CORP #3 4444 ONE MELLON BANK CENTER PITTSBURGH, PA 15258 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make I Model I Serial No. Repair Alteration Airframe (As described in Item I above X Powerplant Propeller - Type Appliance Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. LANCE A. MATTESON X U.S. Certificated Mechanic 8560 E. SAN FELIPE DRIVE Foreign Certificated Mechanic AP 1864049 SCOTTSDALE, AZ 85258 Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unfits) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements ofPan 43 of the U.S. Federal Aviation R lations and that the information furnished herein is true and correct to the best of my knowledge. Date 7....70 S • • • -ft r 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit id ntified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is 121 APPROVED O REJECTED FAA Rt. Standards Manufacturer Inspection Authorization Other (Specily) Inspector X BY FAA Designee Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection Certificate or Signature of Auth • In dual Designation No. 7 -A9 -fAr 526705494 IA Ls GL Michael Donnelly FAA Form 337 (07-96) This is a computer ed form created by Michael Donnelly. SDNY_GM_02754122 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_OO241O44 EFTA01326637 NOTICE Weighrand balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) In order toprovide continuity duringfitture inspections, maintenance or alterations a true dopy ofthis FAA form 337 and all listed Wiring Diagrams must be kept with the aircraft's records as long as the alteration remains in effect. July 10,1996. Gulfstream Aerospace Corporation {GAC} Model G-IV, Serial Number 1085, N88GA, FAA Aircraft Type Certificate Data Sheet A I2EA. Aircraft in-service data: 2241.9 hours & 932 landings. Refer to the following FAA Approved Data: GAC Aircraft Service Change {ASC} 143 (ATA 24) Alternator Field Current Overcurrent Monitor, dated: October 7, 1994; and FAA Form 81 I 0-3, dated: 7-10-96, Identifying: Drawing No. ASC 143-062096, Titled: TOP DRAWING ASC 143 (ATA 241 Alternator Field Overcurrent Monitor Original Issue (no revisions), dated: 7-9-96, — the following Wiring Diagrams are listed on the TOP DRAWING: • Wiring Diagram No. 06209601, Titled: }.EFT SIDE DEVIATIONS dated: JUL 09/96 and • Wiring Diagram No. 06209602, Titled: RIGHT SIDE DEVIATIONS, dated: JUL 09/96, as approved data, signed by: John R. Chambless, NM-567, Systems and Equipment (Electrical). The purpose of this alteration is provide an indication that maintenance personnel can use to determine that an overload condition has occurred in a main engine alternator field circuit. This alteration adds a current sensor assembly and fault latch indicator to the left and right converter shelves and modifies the aft equipment compartment wiring. The above referred to Wiring Diagrams show deviations that were made to ASC 143 in order to provide a way to disconnect a DC Current Sensor or Alternator Overcurrent indicator display without cutting wires. These deviations also add a shield braid for each existing alternator (+) field wire and bond both DC Current Sensors, eliminating the need to run new wires to the left and right engine disconnect plugs. Performed all of the modification instructions of ASC 143, except as provided for on the above listed Wiring Diagrams. All parts were purchased from Gulfstream Aerospace Corporation — Savannah, GA and were new at the time of installation. Successfully performed — ASC 143 Operational Test in accordance with Paragraph E. of the ASC's instructions and noted no abnormal conditions or unusual operation. Recorded compliance with this FAA form 337 in the aircraft's maintenance records and returned the aircraft to flight status. No Airplane Flight Manual revisions were required or installed as a result of this alteration. Incorporation of this alteration adds 0.2 amps to the Essential 28 VDC bus. The effect of this alteration on the aircraft's basic weight and balance was negligible and no changes were made to the aircraft's basic weight and balance report. This is • computer generated fan created by: Michael Donnelly ASC14388.DOC WORD 7.0 07/10961239 PM NO ADDMONAL SHEETS ARE ATTACHED. •END' ❑ Additional Sheets Are Attached SDNYGIvl_02754123 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241045 EFTA01326638 -Pi JR . U.S. DEPARTMENT OF TRANSPORTATION DATE , • FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS 7-10-96 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio, Koko:Net, NAME OF APPLICANT ei GULESTFEAM -IV etc.) il ,„ G AIRPLANE THE DIAL CORPORATION AEROSPACE / UST OF DATA IDENTIFICATION TITLE DRAWING NO. ' REV DATE #SHTS DRAWING TITLE ASC-143-062096 N/C 7-9-96 1 TOP DRAWING ASC 143 (ATA-24) ALIEFtNATOR FIELD OVER CURRENT MONITOR °THE ABOVE DATA N REVI WED BY DER CANDIDATE NAME: ..a .7 DATE 7-9-96 Michael natty PURPOSE OF DATA TO SHCE4 OCMPLIAI4CE WITH FEDERAL AIRWORTHINESS REGULATIONS, ON AIRCRAFT MODIFICATION WIRING DIAGRAM CN ANY GULFSTREAM G-IV HAVING ASC-143 APPUCABLE REQUIREMENTS (List spades sections) 25.1301(a,b,c,d); 25.1309(bl); 25.1353(a,b); 25.1357(a,c); 25.1431(c) CERTIFICATION — Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered - NONE - have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. 0 Recommend approval of these data I (We) Therefore F3 Approve these data SIGNATUREtS) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) I DESIGNATION NUMBER(B) CLASSIFICATONIE) Systems &Equipment dr ... 4 or ..7 /.2ser....a.,,,..4 6 John R. Chambless NM-567 (EleCtrical) FAA Form 6110-3 (11-70) SUPERSEDES PREVIOUS EDITION This a a cernpuhr geneated lam anted (0995) by: hada& Dannelly 7.00 Qj 011 YNN0P 9t92 6St Z0L 0C:60 96/0T/L0 SDNYGM_02754124 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241046 EFTA01326639 SDNY_GM_027.125 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024I047 EFTA01326640 ASC 143 (ATA 24) Alternator Field Overcurrent Monitor LEFT SIDE DEVIATION The Dial Corp Aviation Department WIRING DIAGRAM No. 06209601 Original Issue JUL 09/96 , ASC 143 (ATA 24) Alternator Field Overcurrent Monitor RIGHT SIDE DEVIATION The Dial Corp Aviation Department WIRING DIAGRAM No. 06209602 Original Issue JUL 09/96 Gulfstream Aerospace Model G-IV The Dial Corp effective all S/N aircraft having Aviation Department ASC 143 (ATA 24) Alternator Field 2505 E. Airlane Blvd. Overcurrent Monitor Phoenix, AZ 85034 TOP DRAWING No. ASC143-062096 602-207-5363 voice 602-207-5353 fax Original Issue JUL 09/96 SDNY_GNI_02754126 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241048 EFTA01326641 SDNYGM02754127 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241049 EFTA01326642 TV10,114 oq LEFT »WM OttCON/ICCT S010 ret CONN PC" W AHCOWIII •Ltat Akatft dorae• GI.0 11• td.143. »We» «Met»el lEIAPRO 1~ Pent NTA 341 AM.natas field Ovensmem10MMA .1~1~ Tids Waco Nap ~a» an Adana lb ACC NC DIAL CORP MU) WO Immeonel »A en »acme« monn« b. occombø ~ILO Y De ~mar ~en» Ton ..Mn aeon 5.1.• V1013A20— › »ANC NACAMA •••41.11.8 tat 1•110.0.8 S1 . 1År 000141A1C Iq won •••••••••••.» to i» WI.M,011 vermorme bød WM. imbo »OD« irgapommicammelmaimids• MGM SIDE DEVIATION' ~Ns Mtn ~Ka lababre• TMtl rianae. ono» ~WM» NM MAID 143 InM.rb Moan • Way W distant • OG GoribM Sal« M AgrnnM Ostonat ~My dibia.1~ maim •••• 02.1•1Mgt CT.» WA TIN ~Sea MO ~Me •OCA ~lie ~mar 1./.4.11 Cata V.013020 • bonds M. DC Gam» tam" emnaads. No MIN Ma bisatt ~el let ~NA »4 MN taiatit‘i40~1...• VINIX20 .25 MPG Imo» edd til~Milit VIMILANUI Rob» tattilitt »Am» ea Mad wools 1141.0210/18me Pmet•Imetw »see et» Mom Nina am.b• »mum» d+å HI GA@ 44.43 On M lamed .0~ 18 DOG metro M/ »men ammo GAG Wig» tam SI dap» nova IN» at At Ow» • ~0 TO Gødø1 ~S. —• IJCItt *PI •••••• a •••••• •••••• Cain tut (NO ALT» Otleantl4.1Namur MUD mar ~ma CtMAINT we Nunn.. 2040.1 ~et LEFT µNA Ms 10•41—.~...1~ arg OVORGURROKT »a m» NOCAT011 • mapieSTR. oie 1•01.7.021 LEFT CONVERTER SHELF es Der. Hy nit tic saw Mr» Male » outmost St amommmer Ma— »re« • paltatitneett. — ~It att ...es ~Myth" Ailen.mbie lanai 13-1V The Dial Corp effliam ø• AM »emit 55.1.» Mtalniittitlemeta noroam» Alt 10 1ATA LI Anortelor PAM 23,3 Z. AMY* OW& ~moon --a Oremmn». »MI« non» At 11414 otthanam• LOOT SIM pre101014 60201141ere 00000 In =it% WIRMO DIMULUI No DHOW» Orameed Ina AA 0.At • SDNY_GM1,1_02754128 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241050 EFTA01326643 - SDNY_GM_02754129 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024105 I EFTA01326644 wan nit PONT CONVERTER a MCI M - WISP'S TVS'S.% nino.• • ARLO DUD SE add Poen gnome PECOPINECT PP ID SIAM E AUX rootWAY SOX • SPAIN, M OCT 744 33333 sot SEE DM OUR co*I 11•01 SOC SAP PRESTO TOMER waimi ..._ ÷ PO UPOO *MAMIE MAIO lat•LACC E TRECTIR In. Aarpott *tyke agape NAPA S P EREPall t µ 042Mal AEC IP araCOSLICV•gl ra Ihanaltall CA • PI Airanippr INN Ovonai WO rmil LEPT Ma DEVIATIONS masons= ChSW. 100•14111 an b•ONabot NMW1MW INILI IIMO pinolinal Oat an aborarrrent CMIONEa Ns PAPP la ••• 0•1110.47 • perealr OHO areal TIP pearl PPP VP lA.2 POE • wanM Wa0 t 111•0•00/N .M 401 COVV•110/ IIOLOC• slat Saha al modes me an elpairesi toopasnat RONA mm SLOW am Runup O P Spin Pop driNplona Salvers ASAP AEC 143 laaa N Walla • al 10 Ilalatel • DC Comae Sapp or *Rammer Oprearrani PEONS Sap vitheal OAP. Pp. UL IMO Ana Tit -* Iµ440 EIEE PLOP PO Ealip ellepelerl•I Gana00, POI PP n o µ 21 VDC Seal bonds DC Comet Sanwa. .404040E 0a PRI * no Amman4o Op NN PA OSP AR" "al". OS SCP REVCO INN* µ %WHAM 0.4 Illa••••••••• Rant OYU •4•IJSIN.• Ho C••••• lame, EARN PP'S. MI µ.4.t* N ikAVARRIONS•ix VS 11M011 Cal la CAC A.C.43 CAM Opiralon alb may be liebtalbuid. eras. µ Dia 111016"20 REVCO RASE Pt PPS APP. SAC 111,18.1041$04• µ so econocap RP POPO Mn Pad by Po fly. a• Eno CT•02 Apia so•Einem R ENO ALTAR c...•... gab Mayas, ouftinipi ism REED aa••••••• is as realm, OPP CURRENT ••I Maas* ao• SENSOR fa. at RIGHT AETN µ OVERCURRENT NOVATO* spoon- Odd RIGHT CONVERTER SNEER US32.7/014 Mop APRS POW )m• cal• WI MD - -RP laa -Mal. site. inol. ••••••••• atlas Yr Waal Dar e tall 0.01*••• Panora. RAM 04V The Dial Corp ••• Iwo al Wad •I awn. 4040-* al Sal it Gra Paso ARAMs Coorrpro ASO PS IAEA SO Altornirtor Okla >14I E. Plop PAL p•nanµ M1 rod•-lII PROW rbarak.AE 111.14 MOM net OCVLAIIONE 142.7874311) rwa PROP INAGRAII Na.PRAM 1141.38NS //I to Coos! lawn ENLOE/PI • • N • SDNY_Givi_02754130 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241052 EFTA01326645 SDNY_GM_02754131 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024I053 EFTA01326646 .- ha° AIW0nd MIX*. 21204020 Only rb isio MAJOR REPAIR AND ALTERATION For FAA Use a .r (Airframe, Powerplant, Propeller, or Appliance) Office Identification Mr ItISTRUCTIONS' Print or type all entries. See FAR 43.9, FAR 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of (hi /can. This report is required by ism (49 U.S,C. 1421). Failure to report can result In a civil penalty not to exceed 51.000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model I. Aircraft Gulfstream Aerospace G-IV Serial No. Nationality and Registration Mark 108 5 N88GA Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner MELLON FINANCIAL SERVICES CORP #3 4444 ONE MELLON BANK CENTER PITTSBURGH, PA 15258 3. For FAA Use Only 4. Unit Identification S. Type Unit Make I Model I Serial No. Repair Alteration Airframe (As described in Item I above) X Powerplant Propeller Type Appliance Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. LANCE A. MATTESON X U.S. Certificated Mechanic 8560 E. SAN FELIPE DRIVE Foreign Certificated Mechanic A P 18 6 4 0 4 9 SCOTTSDALE, AZ 85258 Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made o the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements ofPart 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best ofmy Imowledge. Date Si o o ed Individual ""717` - p( t 7. Approval for Return to Service e Pursuant to the authority given persons pccified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is al APPROVED 0 REJECTED FAA Flt Standards Manufacturer InspectionAuthorization Other (Specify) Inspector X BY FAA Designee Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection Cenifieste or Signature of Au e 71 d Designation No. 4-- /8-94 , 526705494 IA Michael Donnelly FAA Form 337(114s) This is a cater generated form created by Michael Donnelly. SDNY_GM_02754132 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_0024 (054 EFTA01326647 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) 06/17/96 Gulfstream Aerospace Corporation {GAC} Model G-IV, Serial Number 1085, N88GA, FAA Aircraft Type Certificate Data Sheet Al 2EA. Aircraft time in service: 2234.1 hours and 929 landings. FAA Approved Data: FAA Form 8110-3 Statement of Compliance with the Federal Aviation Regulations dated 11/01/94 for Gulfstream Model GIVAirplane, listing GAC Drawing No. SE45807901 - REV. A - 10/31/94, effective for S/N 1000-1195, title: STD REPAIR — BREATHER WING T.E. BOX - F.S.498.00 (MAJOR), signed by Structures DER John G. Wilder, Designation Number SO-483. The purpose of this repair is to remove the existing GAC P/N 1159W40226-17/-18 (aluminum) breathers that are cracked beyond limits from the aft side of the trailing edge (T.E.) box beam and replace them with new P/N SE45807902-11/-12 (stainless steel) breather on the forward side of the beam as shown on the above referred to drawing. Removed the existing breathers from the aft side of the left and right wing trailing edge boxes by drilling out the attaching fasteners. Trinuned the perimeter of the new SE45807902-11/-12 breathers to fit the installation and match drilled 0.164-0.167 inch diameter holes in the breathers to existing aircraft rivet hole locations. Finished fay surface of SE45807902-11/-12 breathers with two (2) coats of #2012 Epoxy Primer and one (1) coat of 2013 epoxy top coat paint. Attached the prepared left and right breathers to the forward side of their respective beams using new Hilok fasteners P/N HL 10V5-2 Hi-Lok and P/N HL, 70-5 collar at each of the 10 inboard attach points; and new P/N HE., 30-5-3 (-4 at the top position only) Hi-Lok and Bl, 70-5 collar at each of the 6 outboard attach points. Note: All fasteners were installed wet with pro-seal 870 (or equivalent product per MIL-S-81733). Changes to the aircraft's weight and balance were negligible. This computer generated form was prepared by: Michael Donnelly. NO ADDMONAL SHEETS ARE ATI-ACHED. oalD• O Additional Sheets Arc Attached SDNYGIvl_02754133 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241055 EFTA01326648 CIS MI 0 c';_,:y‘F.IVED FAA (../ Form Approved 4 .1)' MAJOR REPAIR AND ALTERATIOW B 121°96 OMB No. 2120-0020 usoeconnwar For FAA Use Only cliemponmen (Airframe, Powerplant, Propeller, or A PPIIMYSSDO office Identification Weed Aviation Administration VWite —6PD INSTRUCTIONS: Print or type all entries. See FAR 43.9. FAR 43Appendix B. and AC 43.9-1 (or subsequent revision thereof) tor instructions and disposition of this form. This report is required bylaw (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model Gulfstream Aerospace Corporation G-IV 1. Aircraft Serial No. Nationality and Registration Mark 1085 N88GA Nam.kiels shown on registration certificate) Address (As shown on registration certificate) Mellon Financial Corp. Ni 4444 One Mellon Bank Center 2. Owner Pittsburgh, PA 15258 3. For FAA Use Only • .0. Unit Identification S. Type Unit Make Model Serial No. Repair Anatol,: AIRFRAME .. (As described in Item 1 above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6 Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. CFC Aviation Company,LI-C u.s. Cenificateo Mechanic C9FI1844.1 Airframe 3,4 dibta The Jet Center Foreign Co:Ideated Mechanic Ptilid10 112 & 3 16300 Daily Drive X eormieatee Repair Station Limited Powerplant, Van Nuys, CA 914064283 manuractwer instrument & Accessory D. I certify that the repair and/or alteration mode l° the un't(s) identified In item 0 above and described on the reverse or attachments hereto . have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of AuthOr Individual FEB. 9 1,38 • '. 7. Approval for Return To Service Pursuant to the authority given persons specified below, the unit identified In item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is 0 - APPROVED 0 REJECTED FAA Flt. Standards Other (Specify) Inspector Manufacturer Inspection Authorization BY FAA Designee X Repair Station Person Approved by Transport Canada AirworthineSS Group Date of Approval Or Rejection Ceniticale or Signature of Authorized lndi • al Designation No. FEB' 9 1996 C9FR844J ..a.-4.-c-t 2 ...--4,...t...4" FAA Form 337 SDNY_GM_02754134 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024I056 EFTA01326649 NOTICE Weight and balance or operating limitation changesshall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations fO assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished- (If more space Is required, attach additional sheets. identity with aircraft nationality and registration mark and date work completed.) 02/09/96 GULFSTREAM AEROSPACE G-IV, SN: 1085, N88GA This is to amend FAA Form 337 dated 01/26/96 regarding the provisional installation of a Honeywell NZ-2000 FMS Computer modified to software version 4.1 which functions as an independent third navigation system and as a warm spare to replace either FMS-1 or FMS-2 including its aircraft systems interface. An upgrade to previously installed dual Honeywell GPS sensors from PN: HG-2021-AB02 to HG-2021-GD-02 was also incorporated in conjunction with the third FMS. These modifications were incorporated in accordance with the applicable technical data contained in configurations 13, 15,16 and 17 of The Jet Center Configuration Control Document 08006005 Rev. D dated 01/20/96, FAA approved 02/02/ as a later revision to plemental Type Certificate No. SA3774NM. Airplane Flight Manual Suplement Document Nos. 08015090 Rev. N/C, 08015091 Rev. N/C, 08015009 Rev. A, and 08015011 Rev. B, all of which were FAA approved on 02/02/96, have been provided to the operator. Minor deviations to the STC with regard to the electrical installation were accomplished in accordance the following Jet Center wiring diagrams which are FAA approved by Sarkis A Karaguzian, FAA Systems and Equipment DER NM-2128 on FAA Form 8110-3 dated 02/09/96: 08069100 Rev. A dated 01/20/96 - No. 3 FMS 08069324 Rev. A dated 01/20/96 - No. 1 & No. 2 Global Position The 3rd FMS computer may be installed in the mount provided. The circuit breakers controlling power to the two GPS sensors can be closed. The placard stating "FMS-3 AND GPS INOP PENDING FAA APPROVAL" placed on the instrument panel can be removed. The effect of these modifications upon the aircraft empty weight was reflected in a revision made to the most current weight and balance report. A supplement to the aircraft equipment list and copies of the wiring diagrams listed above have been added to the aircraft records. The work described has been found to be in conformity with the above mentioned approved data and the aircraft continues to meet the airworthiness criteria under which it was originally certificated. Work Order 9042, on file at this agency, covers the above described work. END O Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: I992-769-012/60157 SDNY_GM_02754135 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241057 EFTA01326650 'at—!o ff . Form Approved 0 • OMB No. 2120-0020 MAJOR REPAIR AND ALTERATION USCepeetrrent For FAA Use Only or soNsoonsson (Airframe, Powerplant, Propeller, or Appliance) Office Identlficatlpp hwassiatioilai Adrewstration Illig -P 512O INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix Et and AC43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report Is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1400 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model GWfstream Aerospace Corporation G-IV I. Aircraft Serial No. Nationality and Registration Mark 1085 N811GA Name (As shown on registration certificate) Address (As shown on registration certificate) Mellen Financial Services Corp. ft3 4444 One Mellon Bank Center 2. owner Fittsburgh,PA 15258 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer 8. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certi Nate No. CFC Aviation Company, L.LC. U.S. Certificated Mechanic C9FR844.1I Airframe 3,4 d/b/a The Jet Center Foreign Certificated Mechanic Radio 1,2 & 3 16300 Daily Drive X Cenificaled Repair Station ..irnited Powerplant, Van Nuys, CA 91406-1283 Manufacturer .ost rument & Accessory D. I certify that therepair and/or alteration made to the un t(s)Identifled in item 4 above and described on the reverse or attachments hereto have been made In accordance with the requirements of Pan 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my nowledge. Date Signature of Authorf Individual JAN 2 6 1996 7. Approval or Return To Service Pursuant to the authority given persons specified below, the unitidentified In Item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is er -APPROVED 0 REJECTED FAA FP Standards (Specify) other(Specify) Manufacturer Inspection Authorization Inspector BY FAA Designee X Repair Station j Person Approved by TrariSPOrt Canada AinvonhIness Group Date of Approval or Rejection Certificate or Signatur Authorized Individual Designation No. ;JAN 2 6 1996 C98148443 -4-4-6-4- - C FAA Form 337 meal SDNYGl.l02754136 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241058 EFTA01326651 NOTICE Weight andbalance oroperating limitation changes shall be entered in the appropriate sacraI t record. An alteration most be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished' (It more space Is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) GULFSTREAM AEROSPACE G-IV, SN: 1085, N88GA, 2,092.0 HOURS, 878 LANDINGS . Removed an existing Honeywell NZ-920 acting as the third Flight Management System Computer with its mount, and the dual Honeywell HG-2021-AB-02 Global Navigation Satellite Sensor Units previously installed per STC #SA3774NM. Flight Manual Supplement Numbers 08015014 and 08015015 "Original" Revisions dated 07/18/91 for FMS-3 and Dual Honeywell Global Positioning Sensor System were removed from the Airplane Flight Manual. Installed provisions for a third Honeywell NZ-2000 Flight Management System (FMS) computer modified to software version 4.1C a ong with mounting provision and a configuration module to function as an independent third navigation system and as a warm spare to replace either FMS- 1 or FMS-2 including its aircraft systems interface. Electrical provision were also made for dual Honeywell HG-2021-GD-02 Global Navigation Satellite Sensor Units that are installed in conjunction with the third FMS. Parts 1 and 2 of the Type Inspection Authorization for FAA Project No. SA4222LA-T have been satisfactorily completed and issuance of the revision to STC SA3774NM is pending FAA approval. Electrical provisions were installed in accordance with the following Jet Center Wiring Diagrams which are FAA approved by Sarkis A. Karaguzian, FAA Systems and Equipment DER NM-2128 on FAA Form 8110-3 dated 01/26/96: 08069100 Rev. A dated 01/20/96 - No. 3 FMS 08069324 Rev. A dated 01/20/96 - No. 1 & No. 2 Global Position The #3 Navigation Computer was installed on an existing avionics shelf located in the right hand avionics bay at Fuselage Station 162.0 (Horizontal Arm 102.0). Both GPS Sensor Units are installed in the existing mount structure used for the removed sensor units beneath floor 15. These installation meet the static load requirements of AC 43.13-2A Chapter 1. The 3rd FMS computer is not installed in the mount provided. The circuit breakers controlling power to the two GPS sensors are locked open pending FM approval. A placard stating "FMS- 3 AND GPS INOP PENDING FAA APPROVAL" is placed on the instrument panel. The effect of these modifications upon the aircraft empty weight is reflected in a revision made to the most current weight and balance report. A supplement to the aircraft equipment list and copies of the wiring diagrams listed above have been added to the aircraft records. The work described has been found to be in conformity with the above mentioned approved data and the aircraft continues to meet the airworthiness criteria under which it was originally certificated. Work Order 9042, on file at this agency, covers the above described work. END El'Additional Sheets Are Attached *U.S. GOVERNMENT PRINTING OFFICE: 1992-769-0I2/601S7 SDNY_GM_02754137 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241059 EFTA01326652 t/414,4,0 Tx"- ? /, Form Aeon:wed OP uSeaslOttfred creonspcneton MAJOR REPAIR AND ALTERATION (Airframe, Powerplant, Propeller, or Appliance) OMB No. 2120-0020 For FAA Use Only Office Identification Wirer *Melon Aaminumnion I/WV —FWO INSTRUCTIONS: Print or type all entries. See FAR 43-9. FAR 43 Appendix B.and AC43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C.1421). Failure to report can result in a civil penalty not to exceed $1000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model Gulfstream Aerospace Corporation G-IV 1. Aircraft 1085 Serial No. NSSGA Nationality and Registration Mark 2. Owner Name (As shown on registration certificate) Mellon Financial Services Corp. 83 4444 PA 15258 Address (As shown on registration certificate) One Mellon Bank Center Pittsburgh, 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME _ (As described in Item 1above) X POWERMANT PROPELLER .SCEIVED FAA Type APPLIANCE JAN 2 9 1996 Manufacturer ' NV FSDC% 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency CFC dlb/a LLC. Aviation Company, us gene:cats Mechanic C. Certificate No. FR844J dlo1,2 &3 Airframe 3,4 16300Nuys, 914041283 Van The Jet Center Daily Drive CA X Foreign Certificated Mechanic Certificated Repair Station Manulacturer ted Powerplant, strument & Accessory 0. I certify that the repair and/or alteration made to the un t(s) IdentifiedIn item 4 above and described on the reverse or attachments hereto have been made In accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the Information furnished herein is true and correct to the best of my nowledge. Date Signature of Aut I ed Individual .IAN 2 6 1996 SA0017 . -e 7. Approval for Return To Service . --ne---4-1----- - Pu suanl to the authority given persons Seedbed below, the unit identified In item 4 was inspected in the manner prescribed by the Administrator of the Federal AviatiOll Administration and is rr APPROVED ID REJECTED FAA Fit. Standards Other (Specify) Inspector Manufacturer Inspection Authorization BY FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rekection Certificate or Signatur of Authorized Inclivp cit! ) JAN 2 61996 Designation No. C9F118441 ..A....e...a..a. FAA Form 337 rizen SDNY_Glvl_02754138 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241060 EFTA01326653 NOTICE e• Weight andbalance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) GULFSTREAM AEROSPACE G-IV, SN: 1085, N88GA, 2,092.0 HOURS, 878 LANDINGS The following major Gulfstream Aerospace Aircraft Service Change is incorporated into this aircraft: ASC No. 349 with Amendment 1 - Navigation (ATA 34) Nav System Upgrade to NZ-2000 The amendment upgrades navigational computers 1 & 2 to software version 4.1. Gulfstream Aerospace Airplane Flight Manual Supplement No. GIV-95-04, FM approved on Nov. 3, 1995, required with this change, has been inserted into the Airplane Flight Manual. The effect of these modifications upon the aircraft empty weight is reflected in a revision made to the most current weight and balance report. A supplement to the aircraft equipment list has been added to the aircraft records. The work described has been found to be in conformity with the above mentioned FM approved ASCs. The aircraft continues to meet the airworthiness criteria under which it was originally certificated. Work order 9042, on file with this agency, covers the above described work. END ❑ Additional Sheets Are Attached OU.S. GOVERNMENT PRINTING OFFICE: 1092-769-012/60167 SDNY_GM_02754139 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241061 EFTA01326654 Form Approved OMB NO. 2120-0020 0 i MAJOR REPAIR AND ALTERATION USOmerunere For FAA Use Only eflecepCeleaa. (Airframe, Powerplant, Propeller, or Appliance) Office Identification Feelefol fretleflon Adminhaemen nt" -590 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43Appendix Mend AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of thisformThis report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed 51,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make model Gulfstream Aerospace Corporation G-W 1. Aircraft Serial No. Nationality and Registration Mark 1085 NSSGA Name (As shown on registration certificate) Address (As shown on registration certificate) Mellon Financial Services Corp. #3 4444 One Mellon Bank Center 2. Owner Pittsburgh,PA 15258 3. For FAA Use Only 4. Unit identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1abo 0) X POWERPLANT PROPELLER Type APPLIANCE Manulacturer S. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. CFC Aviation Company, LLC. us. certificated Mechanic C9F11844J Airframe 3,4 dibla The Jet Center Foreign Cenificated Mechanic Radio 1, 2 & 3 16300 Daily Drive X 0min:sled Repair Station Limited Powerplant, Van Nuys, CA 91406-1283 Manufacturer Instrument & Accessory 0. I certify that the repair and/or alteration made to the un t(s) Wenn!ied in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized Individual JAN 2 6 1696 7. Approval for Return To Service Pu suant to the authority given persons specified below, the unit-identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is 2 -APPROVED 0 REJECTED FAA Fit. Standards Other (Specify) Inspector Manufacturer Inspection Authorization BY X Repair Station Person Approved by Transport FAA Designee Canada AinvorthineSs OreeP Date of Approval Or Rejection Certificate or Signature of Authorized Individual Des na JAN 2 6 1996 C9 tionNo a4/-4 C. Ccja-e-tra.-4 1 FAA Form 337 na-ae/ SDNY_GIvl_02754140 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241062 EFTA01326655 NOTICE • 41" Weight and balance oroperating limitation changes shall be enteredin the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished' (II more space is required, attach additional sheers. Identity with aircraft nationality and registration mark and date work completed.) 01/26/96 GULFSTREAM AEROSPACE G-IV, SN: 1085, N88GA, 2,092.0 HOURS, 878 LANDINGS Removed existing Sundstrand Mk. V Ground Proximity Warning Computer PN: 965-0676-006 from this aircraft. Flight Manual Supplement Number 41 349607-04 dated 10/14/87 for Sundstrand Digital Ground Proximity Warning System was removed from the Airplane Flight Manual. This unit was replaced with Allied Signal Mk. V Ground Proximity Warning Computer PN: 965- 0676-010. The new computer was installed in accordance with data contained in Gulfstream Aerospace Index List No. SC41-349836 Rev. C dated Feb. 20, 1095 reference on Supplemental Type Certificate No. ST00714AT issued on March 15, 1995. FM approved Airplane Flight Manual Supplement SC41 349M36, Rev. "Original" dated March 15, 1995, which is a required part of this STC, has been placed in the Airplane Flight Manual. Minor deviations regarding the electrical installation of this modification where accomplished using data contained in The Jet Center Wiring Diagram No. 08069434 Rev. N/C dated 10/09/95, "Ground Proximity & VVindshear" which is FAA approved by John R. Chambless, FM Systems and Equipment DER NM-567 on FAA Form 8110-3 dated 01/26/96. A forward pressure bulkhead feed through at Fuselage Station 85.5 was added to provide wiring &togs for stall warning computers. This was accomplished using data contained in Engineering Change Order EO043 applied to The Jet Center Drawing No. 08088188 Rev. N/C dated 01/17/96. This drawing is FAA approved by Joseph R. Holton, Jr., Structures DER SW-862 - on FM Form 8110-3 dated 01/26/96. The effect of these modifications upon the aircraft empty weight is reflected in a revision made to the most current weight and balance report. A supplement to the aircraft equipment list and copies of the wiring diagram listed above have been added to the aircraft records. The work described has been found to be in conformity with the above mentioned approved data and the aircraft continues to meet the airworthiness criteria under which it was originally certificated. Work Order 9042, on file at this agency, covers the above described work. END O Additional Sheets Are Attached CU.S. GOVERNMENT PRINTING OFFICE: 1992-769-012/60167 SDNY_GM_02754141 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241063 EFTA01326656 fer • CO MAJOR REPAIR AND ALTERATION Ftelb ArtC0•44 OMID Na 31204030 For FAA Use Only net ar rouenntim (Airframe, Powerplant, Propeller, or Appliance) Office Identification • Dews memo Ader**Lesilei INSTRUCTION& Print or type as envies. See FAR 43.9. FAR 43 Appendix B, and AC 43.9-1 (or subsequent r aef7 Ion thereof) for instructions and disposition of INS lent. This report Is required by law (49 U.S.C. 1421). Failure to report can taunt In a OA penalty not to exceed $1,000 for each such violation (Sedan 901 Federal Aviation Act of 1958). Make Model I. Aircraft Gulfstream Aerospace G-IV Serial No. Nationality and Registration Mark 1085 N88GA Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner MELLON FINANCIAL SERVICES CORP #3 4444 ONE MELLON BANK CENTER PITTSBURGH, PA 15258 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make I Model I Serial No. Repair Alteration Airframe (As described in Item 1 above X Powerplant Propeller Type Appliance Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. LANCE A. MATTESON X U.S. Certificated Mechanic 8560 E. SAN FELIPE DRIVE Foreign Certificated Mechanic AP 1864049 SCOTTSDALE, AZ 85258 _ Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unk(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirem nts of Part 43 of the U.S. Federal Aviation Regu ations and that the information furnished herein Is true and correct to the best of my knowledge. Date Signature of Audio ' ivi /ci t " re — Ce 7. Approval for Return to Service Pursuant to he authority given persons pecified below, the u it identified in item 4 was inspected in the manner prescribed by the Admin'strator of the Federal Aviation Administration and is C33 APPROVED Cl REJECTED FAA Flt. Standards Inspector Manufacturer X Inspection Authorization Other (Specify) BY FAA Designee Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection Certificate or Signature of Authorized In ual Designation No. 526705494 IA Michael Donnelly / - 9 - - 94 FAA Form 337(l1.95) This is a computer gyyriyedfonn created by Michael Donnelly. SDNYGM02754142 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241064 EFTA01326657 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) In order to provide continuity duringfuture inspections, maintenance, or alterations a true copy of this FAA form 337 must be kept with the aircraft's records as long as the alteration remains in effect. January 05, 1996. Gulfstream Aerospace Corporation {GAC} Model G-IV, Serial Number 1085, N88GA, FAA Aircraft Type Certificate Data Sheet Al2EA. Aircraft in-service data = 2090.8 hours & 877 landings. Refer to the following FAA Approved Data: FAA Form 8110-3 dated November 17, 1995 identifying Aircraft Alteration Report No. 23-100895 AFIS PRINTER Original Issue no revisions dated October 8, 1995 Pages 1 through 15 as approved data, signed by John R. Chambless NM-567 Systems and Equipment (Electrical). Refer to the following FAA Acceptable Data: ACCULEX DPP-210/410 THERMAL PRINTERS User's Manual for operator instructions, maintenance, and other information. The purpose of this alteration is to install a miniature thermal printer that will print Airborne Flight Information System (AFIS) received messages. This alteration installs a modified ACCULEX model DPP-410 thermal printer in the co-pilot's side console, associated wiring to the existing AFIS Data Management Unit (DMU), and a I amp circuit breaker on the co-pilot's circuit breaker panel. The installation requires approximately 24 man-hours to incorporate. Performed all of modification instructions listed in the above referenced Aircraft Alteration Report. Printer was modified to -503 status by and purchased from Gulfstream Aerospace Corp. Long Beach, CA. Successfully performed an AFIS message — Operational Test in accordance with the instructions contained in the above referenced Aircraft Alteration Report. The aircraft may be dispatched with the AFIS PRINTER in-operative provided the AFIS PRINTER circuit breaker is pulled and an IN-OP placard is placed on the printer. Recorded compliance with this FAA form 337 in the aircraft's maintenance records and returned the aircraft to flight status. Operation is automatic and straight forward and no Airplane Flight Manual revisions were required or installed as a rcsult of this alteration. The effect of this alteration on the aircraft's electrical load analysis was negligible and no changes were made to the aircraft's electrical load analysis report. The effect of this alteration on the aircraft's basic weight and balance was negligible and no changes were made to the aircraft's basic weight and balance report. this is a computer generaced loon created by: Michael Donnelly PRINTER.DOC WORD 6.0a: 01!05#96 7:43 PM NO ADDMONAL SHEETS ARE ATTACHED. •END' O Additional Sheets Are Attached SDNY_GM_02754143 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241065 EFTA01326658 yt` 0 MAJOR REPAIR AND ALTERATION RIM APMW. am NO 21200020 For FAA Use Only US. Dtparimett N Tenticanitica (Airframe, Powerplant, Propeller, or Appliance) Office Identification ntral A•loan A 4thilsinttlan a t -/C54 6 INSTRUCTIONS: Print Cf typo as entries. See FAR 43.9. FAR 43 Append% B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report Is required by law (49 U.S.C. 1421). Failure to report can result In a civil penalty not to exceed $1,000 for each such viotati n (Section 901 Federal Aviation Act of 1958). Make Model I. Aircraft Gulfstream Aerospace G-IV Serial No. Nationality and Registration Mark 1085 N88GA Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner MELLON FINANCIAL SERVICES CORP #3 4444 ONE MELLON BANK CENTER PITTSBURGH, PA 15258 3. For FAA Use Only 4. Unit Identification • 5. Type Unit Make I Model I Serial No. Repair Alteration Airframe (As described in Item I above ******************* X Powcrplant Propeller TYPc Appliance Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. LANCE A. MATTESON X U.S. Certificated Mechanic 8560 E. SAN FELIPE DRIVE Foreign Certificated Mechanic AI' 1864049 SCOTTSDALE, AZ 85258 Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regu ations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of zed Ingidu /— g - n ./.:ct 7. Approval for Return to Service Pursuant to the authority given persons pecified below, the unit identified in Item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is Ell APPROVED O REJECTED FAA Flt. Standards Authorization Inspector Manufacturer X Inspection Other (Specify) BY FAA Designee Repair Station Person Approved by Transport Canada Airworthiness Group Date o Approval or Rejection Certificate or Signature of Authorize Indivi I Designation o. 526705494 IA /Ale‘ reAe r Michael Donnelly This se a ter generated form creased by Michael Donnelly. FAA Form 337 (11-95) SONY_GM_02754144 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241066 EFTA01326659 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) January 08, 1996. Gulfstream Aerospace Corporation {GAC} Model G-IV, Serial Number 1085, N88GA, FAA Aircraft Type Certificate Data Sheet Al2EA. Aircraft in-service data = 2090.8 hours & 877 landings. Refer to the following FAA Approved Data: Gulfstream Aerospace Corporation Aircraft Service Change 364. subject: DOORS (ATA 52) 12th STAGE AIR SOURCE - DOOR SEAL SYSTEM PRESSURE, dated September 26, 1995. The purpose of this alteration is to reduce the potential for door seal deflation by ensuring a constant high pressure and maximum flow output from the door seal regulator. This Service Change installs additional pressure supply lines, one from each engine, routed from a port located in the pylon upstream of the 12th stage H.P. valve to the existing door seal regulator pressure supply lines located in the tail compartment. The existing pressure supply lines are re-routed to separate the water system pressure tap and the total air temperature probe pressure supply form the door seal pressure supply lines. A separate air supply manifold now supplies this circuit. This Service Change modifies door seal plumbing in the tail compartment and in both nacelles. The installation requires approximately 90 man-hours to incorporate. Performed all of modification instructions listed in the above referenced Aircraft Service Change. All parts installed were provided in kit form by Gulfstream Aerospace Corp. Savannah, GA. Successfully performed a Bleed Air System — Operational Test in accordance with the instructions contained in the above referenced Aircraft Service Change. Recorded compliance with this FAA form 337 in the aircraft's maintenance records and returned the aircraft to flight status. No Airplane Flight Manual revisions were required or installed as a result of this alteration. Entered a change of + 8.0 pounds at horizontal arm 627.7 (ES. 609.7) to the aircraft's basic weight and balance report. this is a computer generated form created by: Michael Donnelly ASC364.0OC WORD 6.0a: 0U08/967:13 PM • NO ADDITIONAL SHEETS ARE ATTACHED. •END• 0 Additional Sheets Are Attached SDNY_GM_02754145 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241067 EFTA01326660 . , Rs Aro.41 OMB Na 21204020 For FAA Use Only 0 u.S. Drys:moil MAJOR REPAIR AND ALTERATION Offee Identification (Airframe, Powerplant, Propeller, or Appliance) TochnlAvIstlea "r"°""°` Mallalstra4.• 554 -- Flea INSTRUCTIONS Print or type all entries. See FAR 43.9. FAR 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for Instruellons and dIsposIdon of thl form. This repents required bylaw (49 U.S.C. 1421). Failure to report can result Ina civil snaky not to exceed S1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model I. Aircraft Gulfstream Aerospace G-IV Serial No. Nationality and Registration Mark 1085 NS8GA Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner MELLON FINANCIAL SERVICES CORP #3 4444 ONE MELLON BANK CENTER PITTSBURGH, PA 15258 3. For FAA Use Only 4. Unit Identification S. Type Unit Make I Model I Serial No. Repair Alteration Airframe (As described in Item 1 above 71 Powerplant Propeller Type Appliance Manufacturer 6. Conformity Stat went A. Agency's N me and Address B. Kind of Agency C. Certificate No. LANCE A. MATTESON X U.S. Certificated Mechanic 13560 E. SAN FELIPE DRIVE Foreign Certificated Mechanic AP 1864049 SCOTTSDALE, AZ 8S258 Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of on Indiv au. liC 6-fr- I 7. Approval for Return to Service Pursuant to the authority given persons pecified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is El APPROVED CI REJECTED FAA Flt. Standards Manufacturer x Inspection Authorization Other (Specify) BY Inspector FAA Designee Repair Station Person Approved by Ithaspon Canada Airworthiness Group Date of Approval or Rejection certificate or gnatu of Autho' d Designation No. 526705494 IA ide /e5 r- Michael Donnelly This is a co efgenerated form totaled by Michael Donnelly. FAA Form 37 (II-95) SDNY_GM_02754146 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241068 EFTA01326661 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required. attach additional sheets. Identify with airman nationality and registration mark and date work completed.) In order to provide continuity duringfuture inspections, maintenance, or alterations a true copy of this FAA form 337 must be kept with the aircraft's records as long as the alteration remains in effect. November 05, 1995. Gulfstream Aerospace Corporation {GAC} Model G-IV, Serial Number 1085, N88GA, FAA Aircraft Type Certificate Data Sheet Al2EA. Aircraft in-service data = 2073.2 hours & 869 landings. Refer to the following FAA Approved Data: FAA form 8110-3, dated September 14, 1995 for Gulfstream Aerospace Model O-111 airplane, Identifying: The Dial Corp Aircraft Alteration Report No. ST4502LA-T; Titled: APU HOUR METER MONITOR Original Issue, dated September 08, 1995 — No Revisions — Pages: 1 through 14. The purpose of this alteration is to provide current limiting protection for the Auxiliary Power Unit's {APU} Electronic Control Unit {ECU} that will prevent a short circuit in the hour meter or associated wiring from affecting the normal operation of the APU. This alteration also provides a visual cue that maintenance personnel can use to monitor the operation of the APU Hour Meter. Past experience has shown that if the APU Hour Meter or associated wiring short circuits while the APU is running an unwanted APU shut down will occur and normal starting will not be possible. It has also been demonstrated that the ECU can be damaged if repeated start attempts are made with a shorted APU Hour Meter or associated circuitry. Performed all of instructions listed in the above referenced Aircraft Alteration Report. Successfully performed an APU operational test using the FAA Approved G-IV Airplane Flight Manual and while the APU was running above 95% APU RPM (+ 4 seconds time delay) verified that the APU HOUR METER MONITOR indicator was ON (dim) and pulsed (bright) approximately once every 3 seconds. Shut down the APU and verified that the APU HOUR METER MONITOR indicator was OFF. Recorded compliance with this FAA form 337 in the aircraft's maintenance records and returned the aircraft to flight status. No Airplane Flight Manual revisions were required or installed as a result of this alteration. The effect of this alteration on the aircraft's electrical load analysis was negligible and no changes were made to the aircraft's electrical load analysis report. The effect of this alteration on the aircraft's basic weight and balance was negligible and no changes were made to the aircraft's basic weight and balance report. HR_MTR.DOC WORD 6.0x IIMPIS II:26 AM NO ADDMONAL SHEETS ARE ATTACHED. *MD* Cl Additional Sheets Me Attached SDNY_GM_02754147 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241069 EFTA01326662 • U.S. DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS September 14, 1995 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE MIS RS Holkoptor. NAME OF APPLICANT so) Gulfstream Aerospace G-IV Airplane The Dial Corp LIST OF DATA IDENTIFICATION TITLE AIRCRAFT APU HOUR METER MONITOR ALTERATION REPORT ( ).,8, 5I _ ORIGINAL ISSUE — dated: September 08, 1995 .c. Report No. ST4592LA-T No Revisions ei r Pages: 1 through 14 ‘& tA° THE ABOVE DATA B EVI D BY DER CANDIDATE NAME: DATE: September 19. 1995 Michael Donne PURPOSE OF DATA In support of Supplement Type Certificate (STC) for the Installation of Current Limiting Protection and Monitoring of the Auxiliary Power Unit's Hour Meter in the Gulfstream Aerospace G-IV Aircraft. APPLICABLE REQUIREMENTS (List specific sections) 25.1301 (a) (b) (c) (d); 25.1309 (b) 1; 25.1353 (a) (b); 25.1357 (a); and 25.1431 (c) CERTIFICATION — Under authority vested by direction of the Administrator and In accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered NONE have been examined In accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. N Recommend approval of these data I (tse)Therefore M Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVES) DESIGNATION NUMBERM CLASSIFICATION(S) . ai Syistems tquipment / 44 7 efi7 6 Z-apf John R. Chamblass NM-567 (E =trio FAA Form 8110-3 (11.70) SUPERSEDES PREVIOUS EDITION nes Ise =craft genecated form anled OM by: (.9:oot Donnelly T006j GET VNN0D 9695 696 Z0L 3Y3 LS:ST 28/SO/TT SDNY_GM_02754148 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241070 EFTA01326663 SDNY_GM_02754149 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241071 EFTA01326664 SDNY_GM_02754150 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241072 EFTA01326665 a REGISTRY IAA AIRCRAFT CATIERA NO. a DATE: 5- lem Apo.. ' .- • means® For FAA We Oa MAJOR REPAIR-AND ALTERATION ligiel. — -' • - ' (Airframe, Powerplant, Proper, Or AppRinee) Offse leant-two .. • .57:x -t e) a iNTIRUCKINS: Print or roe all aunts. See FM 43.9, FM II Appendix B. and AC 43.9-1 (or subsequent ration thereat) for ingthotions and disposidon of dos form. This Noon Is moat by law (49 U.S.0 1421). snore to report can !teak In a ad penalty not to acted $1,000 for each such *anon (Section 901 Federal Avladon Acid 199). Make Model I. Aircraft Gulfstream Aerospace G-P/ Serial No. Nationality and Registration Mark • . 1085 N8RGA" Name (As shown on registration certificate) Address (As shown on registration as ficate) 2. COM16F . , ; ; Mellon Financial Services Corp /13 4444 On Mellon Bank Center .. . . : Pittsburgh, PA 15258 • 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make j Model Serial No. Repair Murton Airframe (As described in Item I above) X Powerplant • Propeller -• -1,Tc Appliance Mandan 6. Caforathey &maw • - . A. Agency, Name and Address B. Kind of Agency C Certificate Ne. LANCE A. MATTESON X U.S. Certificated Mechanic 6560 E. SAN FELTPE DRIVE Foreign Certificated Mechanic AP 10.64049 SCOTTSDALE, AZ 0.5250." Certificated Repair Sudan Manta: am D. (certify the the 'w aneVor amen= made to the wills) identified in item 4 above and demnbcd on the '<verse a seachments berm have then ma to scostace with the requirements (Part 43 of the U.S. Federal Aviation Reganon, IS th.c the infosintion finished Inns is eye and area co the beatof my knowthige. • Date &pane of • ind z.. 2.5-0i4+-cal. itter....- • d 'l • 7. Approval for Raton to Sawn Puma= to thc =betty give paces specified below, the unit tanned en etam 4 was inapsted in a manna *thothed by the Administrator of the Fulani Aviation Administration and is la APPROVED El REJECTED - FAA Rt. Scents Manufacturer x Ramon Authorise* Otha (fiPendY) BY Seems .i FAA Deep= aeprir Sluice :- ?CM= Approved by Transport - Canada Aiswordaess Orem Caen ApprOVal or Cavan or Signsten of Authorized DetisoadonNo. 526705494 IA r Michael Donnelly /Sc -- /P- FAA Fero ) • • 4 — - SDNY GM 02754151 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, -15, and 17 EFTA_00241073 EFTA01326666 GA IAA AIRCRAFT RED IS TTER? .7_ 7.. . Fs CAnES RD* • Weight and baler or operating limitation airy, shall be entered in the appropriate aircraft record. An alteration tympani* with all previous alterations to must he conatinued conformity with the applicable Unworthi ness requiranents. t Description of Work Accomplished - (If more space is required mach idelinond them. Identify with secret =keenly sod rcipstrenon mart =4 Eats work oxonktedi In order to provide continuity during future inspections, maintenance and alterations a Form 337 is required to be kept on board the aircraft true copy of this FAA as long as the alteration remains in effect. March 24, 1995. GulfstreaniAerospace Corpora FAA Aircraft Type Certificate Data Sheet Al2EA tion (GAC} Model G-IV, Serial Number 1085, N8801‘ . Aircraft in-service data = 1896.4 hours ft 784 landings, Refer to the following FAA Approved Data: Gulfstre am Aerospace Corp. Model G-IV (GAC) Service Change (ASC) 234 SUBJECT: ELECT Aircraft RICAL POWER (ATA 24) ESSENTIAL BUS REROUTE dated December 16, 1993. FEEDERS — . _ Refer to the following 26, dated September 30,FAA Ac: ptable Data: Gullet:ream IV Computerized 1994; <IIIIIIONN> denotes applicable wok code. Maintenance Program (CMP) Revision The purpose of this alteration is to separate electric al feeder cables and remove unnecessary wire connections. bliagfiacithe Left Cockoitlunction NW (30 Removed and discarded the following woes from comecto SAD as fol km; 2 (see figwe of the above listed ASC) rs 305A112 and 30:MI112: 1X560016A, I X561121 1X562D16C. 6B. and Removed the following wires from connector 305A1P2 :1X560E16A. DC561E168. and 1X562E IOC. Removed the following wires from connector 305A1P12: I X560A16A: IX561A168, and I X562A16C. Using a GAC P/N GASSOSM blue splice committed the following piths together rim the 305A I bosom plug 1X560516A & 1X560Al6A; 1 X.561E16B & I X561;416B; connectors: and DC562E16C & I X562A16C. Modified the Right Cockpit Junction Panel (10AA1 we follows. (see fig= I of the above listed ASC) Removed and discarded the following wires from aninecto n 306AIM and 305A1113: 2X56013I 6A. 2X5611316B, 2X5621:06C. - .. . . and Removed the following wires from connector 306A IN: 2X5MEMA,230611I68, and 2X562E16C. Removed the following wires from connector 305A1P13: 2X560A16A, 2X561A16B, and 2X562A16C. Using a GAC P/N GASSO5A4 blue splice connected the following pairs tOgether near the 306A 1 — hottattplagesearactx 2X560E16A & 2X560A16A; 2X561E168 & 2X561A16B; and 2X562EI6C & 2X562A16C. )lgglifiggign aircraft wiring as follow, (refer to the above listed acceptable data) Removed and installed Power Distniation Box in accordan ce with C4505@. Removed and installed lbansfor ill accordance with C43025>. Separated (from each other) mer Ftectifler Unit the craning pilot's electrical feeder cables Item the exist electrical feeder cables that nth from the Pow= Distribut ing copilot's ion Box (05A2) to the pilot's (315A1) and to the copilot's break= panels. After reviewing the existing approved configura (314A1) chair tions it was determined the: dorm limited wirt-ron space possible interference with =rating avionics and electrical and installations it wu act practical to comply with the ASC's separating the left, right, and essential bets feeders (from purpoae of each other). Performed AC Power (26 Voh) System - Operatio 4244045> and AC / DC Power Distribution - Function nal Ter; Tat 045051>. Recorded compliance with this FAA form 337 in the Masts maintena nce records and =reed the stash to Mat . Same. . No changes to the south's tier:M=1.10nd analysis Suited hem this Cation The effect of this change on the airendrs Weight and liaise= Ins OtieigthIC and no tinges were made to the weight and balance report Maras sash Buseaccepra generstai farm card by: eras Desalt WORDia 01249511M MI NO ADDRIONAL SI TS ARE ATTACHED. *END' O Additiceal Sheets Are Attached C • C al'aga SDNY_GM_02754 1 52 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241074 EFTA01326667 Rt.Ma-a Oa as :tamp MAJOR REPAIR AND ALTERATION For FAA Um Ord1 0 VIOtswena (Alrlesine, Powerpl anI, Propeller, or Appliahce) . Offtee Marairmatiaa sibuqns• . Fiat...oar aria s a C • hOP INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B. and AC 43.9-I (or subsequent :canon thereof) for Instructions and disposition of this form. This report is required by law (49 U.S C 1421). Failure to report can result In a chit penalty not to teed 51,000 for each such violation (Section 901 Federal Aviation Act-of 1958). Make - . ' Model 1. Aircraft Ca/Usti-mum Aerospace. G-IV Serial No. Nationality and Registration Mark 1085 N118GA Name (As shown on regrowth.* certigrtee) - Address (As shoat on registration certificate) T. Owe Mellon Financial Services Corp 03 4444 One Mellon Earth Center Pittsburgh,. PA 15258 3. For FAA Use Oaly . 4. Dalt identification 5. Ten Uoit I • Model I Serial No. Repair Akeradon . , Airframe ••••••••••"••••••• (As descratird in Item.I ton) X . Powerplant Propeller .1)F i SPOSts-t. " Mahan ' • 6. CoMormith Statement ' A. Agra Name and Address ' B.- KIS of AiOnc, C. Cerlifmata N. •. LANCE A. MATTESON •• , X US. Certificated Mechanic ' 8560 E. SAN FELIPE DRIVE Foreign Certificthed Mechanic AP 1864649 • SCOTTSDALE, AZ 85258 Certificated Repair Slalom Manufacturer D. 1earn the the repair ardoraltaalloa nude to the math) identified in item 4 above sad described co the reverse or atiactimerth hereto have tommak in eat with the requirements of Pan 43 of the US. Federal AnsonRegalia= end thee the information tieraithed herein 4 Se ad CPTIX310 the ben of my knowledge. Daft Signature 7 dua . Ai-aid/acne /per . _ •• ... - . . . Zt .7. Appeoral for Return to Sank, Pornisa to the aaboriry given persons podded below, the St identified in item 4 was Imparted leathern/met preserazd by the Adrokasterne of the Federal Aviation Adatthistration and a OE APPROVED CI REJECTED . FAA Ft Sande* Mande:pm _x rasp:arm Authonzadoe . . Other (Speedy) BY awn PAA Doha" Repair Radon • Person A4Vorned by Toreson Canada Mniortainesa Grow Dale of Appomere Rejection ' Sarsthma or Signature a( A thaintien No. r 3/2.5115 - - 526705494 t u Michael Donnelly 1 - cailaPerec - „ cajole? SCINT GM_02754 153 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241075 EFTA01326668 REGISTRY ^ FAA AIRCRAFT CAKERA ro Diaz t NOTICE Weight and balance or operating limitation changes shall be enured in the appropriate aircraft record. An alteration must be compatible with all previous alterations so assure continued conformi ty with the applicable airwonhiness requirements. 8. Description of Work Accomplished elf rote spec is required. 11111.6 OddlUalla steers. Iskatify with aircraft =noway a a:Otani:in matt and date work completed) March 24, 1993. Gulfsircani Aetolpace Corporation (GAC) Model G-1V, Serial Number 1085, NS8GA, FAA Aircraft Type Catifintitopsta Sheet APEA. Aircraft in-servi ce data • 1896.4 hours & 784 landings. .. Refer to the following FAA Approved Data: FAA Form 8110-3 dated 11.22.93 for Gulfstream Model (3-IV identifying GAC drawing oust I1590D1.40140 REV C (dated 11-17.93), AXLE FI777NG ASSY MAINLANDING GEAR • (five sheets), as FAA Approval data signed by John G. Wilder Structures DER 50-483. Refer to the following FAA Acceptable Data: Gulfstream IV Computerized Maintenance Program (CMP) 26. dated September 30..1994; d 0 0 018> denotes applicable work Revision code. The purpose of this alteration is to install bushings into the boles for both main landing gear (MLG) axle fitting locking pins. In accordance with the above lined acceptable data: lacked the aircraft: <323001>. Removed four MEG wheel assemblies: <324011> 024012> <324013> <324014>. Removed four MIA brake assemblies: <324104> <724105> <324106> <324107>. Removed (car MIA wheel speed season: <324187> <324188 > <324189> <324)541>. Removed the left and right GAC P/N i 159U:440140-II MEG axle fining assemblies. In accordance with the above listed approved data: Modified both MLG axle fitting locking pin holes. Cadmiu plating was done by: Able Metallic Services - FAA m repair station UMBR 624K - lob* 13253. Fabricated 2 and -13 bushings (see Table I) and installed a -11 each -II and a -13 bushing into each MLG axle fitting assembly. painted, and installed both MLG axle fitting assemblies; Prepared, Left S/N CPT 5102 HSM and Right S/N CPT 5221 Changed identification of both MLG axle fittings by lining HSM. an existing GAC P/N 11591-M40140-II and adding identifying mark I I590DLK114434. Note: Installed a new GAC P/N 1159L1420151-II Ma gear axle fining pi (no S/N) and a new GAC PIN I15912440148-13 main locking gear axle fining attach pin: Left SIN CPT 6121110 Righi S/N CPT 6152 10M, into each MLG assembly. . . M and Restored the following equipment to original configuration is meordanee with the above lined acceptable din;,Installed MLG wheel speed so:mom <324187> <324188> <324189 <124490 four > >. lassalled four MLG brake assanblits; <324104> <324105> 024106> 024107>. Inspected and packed all MU) wheel beesiaga <324051> <32.4.032>024053P <324054 Installed four MW wheel assemblies; <324011> <324012>-.02A0I3><32 ;. 4014>. Performed Left. Right. and Emergency Brake Bleed mid Sakti; 424185≥ Anti-Skid System Funnion Tests <324I0I> <324I03>.• 012.4124n <3241i7>. PerforrnedkVbeel Brake Norm'AmF-SkJ4 System Pmelion Test Stodes landing gear and extension. Checked Left and Right NuteraCioi Saila retraction and AdfMameanti26021> <326/32$: Removed auvah <333001>. . fromjacks: An aprimpriately need pilot performed in aircraft Si %animal test and determined that ground handling braking operations were satisfactory.. Recorded complia and nce with this FAA form 337 in the aircraft's maintenance records and returned the aircraft to flight item. , . , . • The effect of this change on the iireraft's weight and balance wattneglignsfie and no changes west made aircraft's basic weight and babnit import. logic - • • : - No AIMMONaMall, ATTAMIM IND° - ' 0. Additional Slats AreMated • SIDNY_GM_02754154 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFFA_00241076 EFTA01326669 REGISTRY TAA AIRCRAFT DATE: CAKERA NO •OZ - Ø1O-19% 14:ff2 FI1 GLLFSTREFTI IECH4ICAL CPS TO 916122075353 P.01 I .t, • estnnescs.• et rotate,,,,, ,.. Rie.C.10 stintiAk AinAlsOm AOMINI OAT{:. STATEMENT OF COMPL/ ION ANCE ?NTH THE FEDERA AVIATIO L N REGULATIONS I / fj: 1. F-- qi AIRCRAFT OR AIRCRAFT COMPON *ARC ENT onNintIcAnom 1100V.11k, • I TYI e (szr. • Reel, It...fit...re" m as< O • AP" tcno. GULFS7RE.A.M • AIRPLANE . GULFSTREAM AEROSPACE CORP. LIST Oit DA TN. «Mil ICATIOW . Tint • Øl40 `.4å ‘‘LE thr -q00 ' F1777 io-6. A siv MAK)LANDI AJ61 6iEA L.. RENÅ C . • • i . I ' ...Ina " " "" Is t Dap 12E- 0%u ‘ QC bytear-r S go cr— tvre1 /4.) cazum PotvGAJT • .• a•PLICAlllt PIC,IliestilTI ItI« .,.. _ ~SD. immts• FS4Z ZS. 3(33--301 CERTIFICATION • V•nle valiant. vianad4 ay 'Waal*, .1 tan Adaniavai «I la al app•iament asiar Pan 113 *Ion iteawiaact 'rid naillaira na a, laatia• Nil& Aviation' alraltlaws, ilia nits.. Jan ad a attacked •Lreis;* ieni --.— kne bln isietsti ia"ataiediaci.filititiaaiik iagatnnega *I tie Silent Aiiataaa Iligaiati ei ratrikeis aid Iowa 60 c.apir ril aialiiiW al: i '' • I <1;pli thra (eta n 'lacteal..d liarnal •I zbesidaaa .. 1 .. taLAnnin dais diem YOM ', MI OF D'Vens V PtHennialMG atnitairtaTNEs Ins3g.da Tic», miadaiainil ClaSUFICatiOmi - • ' . ØN 1" F:IL1 et!..CA1 s-wirr •-•rc I Caa • Piety. /US Ctstetat 4 04~ fl — SDNY_GM Oii54155 - SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 10,15-, and 17 8, 9, EFTA 00241077 EFTA01326670 - - SDNY GM 02754158 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241078 EFTA01326671 •-serAtait. FAA AIRCRAFT REGISTRY CAREW* NO. 3 DATE: r//Y,A .-o•'t="-':--aR'SPe=n•• >?C— nam•I0'''"''•...-. hinelnag OM Ms ittint MAJOR REPAIR AND ALTE Pena Ma Os RATION 0 en ewillIM (Airframe, ?ennoble!, Propeller, or Apatite mese Mazda ame= :1i) MOINISNISR lasliteCTIONL rem or cove ail amen . See 5h. -hoo invitation. ad dispositlen of this form. ThFAR 43.9. FAR 43 Appendix a. and AC 4341 (of subsequent :evasion thereof) lot Penalty not to exceed S 1000 for each sua is moon Is required by law (49 US.0 I421). Failure to report can malt In a civil. violation (Section %l Federal Aviation Act or Mike feel. I. Aireteft Model GWfstream Aerospace Said No. Cr-IV Nalienably end Regientlion Mart INS . • - NSSGA Nemo(Al Soon on tesiarnion 2. Owner outs) lokkess (As town celegiettelion wither) Mellon Financial Service Corp 83 4444 One Motion Rank Cater Pittsburgh, PA 15253 i For FAA Use Only 4. Vett Idoedibef Una Make 5. Tnie I Motlel I Sabi No. Rea Atarieloa4 Airframe (As deeratd inDem I above) ......ae• . X Pontplant i--"; ?rood= . inal Appliance beembainer C Cirefemaley Statement A. Amalie Name red A4clom . B. Kant of Many C. Canilkma No. LANCE A. MATTESON • X U.S. Certificated Meetenie 1660 E. SAN FELIPE DRIVE Foreign Caen/one Mechanic K0175DALE, AZ 15251 - AP 1161041 Catificerted Repair Steffen - • .Manufac turer D. I catty that the repair mit« aternion made - to tha times) identified fahm 4 thaw ee4 deeded ham ban been made In sxordeete yeah the reernme on the tte ofPert 0 oft U.S. Pedal! Arians Regalaaa reverie or etadoneral feembod hetet= ead cornet Co the beg o my cs ma that the infommice knowledge. .. Due Signature • of . bdivickel /2 / 2. ,A......4 //Per ' • .4- 2 .----- • .7. Awed Me Remora se Sarin Plasma to the =dairy even p0 specified below the int identified is item 4 __ impendle the asimisuarit ofMisses:el *visite Attennetr roam poarlst byes anon and is DE APPROVED 0 REJECTED FAA fk Swedente Smalls hienufec tove . X taspacrion Anon:Lan By Ole (394.14) FAA Dnepr, - Ripe Maim I Pesos Approve! by Tramped Nadir Airwoehin!drop Date ottipixovel a Rejection cetese swipe 6•--.69-526705* 4 IA • --7- /A ......_ .— -.. „erg/Pr die! _.../ . micbmb onneny • • -se! • is " 44 • :_ SDNY_GM_02754157 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241079 EFTA01326672 FAA AIRCRAFT REGISTRY CAM RA NO. j DATE: VAY/ 79 . 7.11101- NOTICE Wel* and balance or operating ilmatslion danger skid be entered in Me appropriate aircraft moon!. An Manton campanile mils al previous alientions to assure continued confoemity wish the applicable must to sizworthiness requiem:Is. cs S Desciipike rdWork Accomplished Minors sews ti required. meth salmi Ma ism* Mai Sad eatheadity sedregitralan mak and dam wart camplited.) February 8, 1995. Gulfstream Aerospace Corporation (CAC) Model G-IV, Saul Number 1085, N88GA, FAA Aircraft. Type Certificate Data Sheet Al2EA. Aircraft in-service data -- 1881.0 hours & 775 landings. Refer to the following FAA Approved Data: FAA Form 8110-3 date 02-01-95 for Gulfstream Model G-IV identifying Gulfstream Aerospace Corporation drawing numbei 1159SB20470 REV .71 REWORK VERT FIN COVERS - ACCESS - ATTACH FTGS (five ‘. Sheets), as FAA Approved data signed by John G. Wilder Structures DER SO 483; and' Gulfstream Aerospace Corp. {GAC) Aircraft Service Change (ASC) 230 SUBJECT: STABILJZERS (ATA 55) PER77CAL STABILIZER ACCESS COVERS - INSTALL4 77ON OF prototype copy dated January 20, 1994 <CM? CODE 972300> The purpose of this alteration is to install remc\ able access panels on the vertical stabilizer to improve the accessibility for corrosion inspection of the vertical stabilizer/fuselage fitting and attaching hardware (interior of stabilizer). It also provides a means for inspection of the hardware that attaches the tie strap to vertical stabilizer/fu lag. attach fittings (three bolts per side). Modified the aircraft in accordance with the instructions and data contained on the above referred to drawing. Installed parts were furnished in kit form by GAC product support Savannah, GA Recorded compliance with this FAA form 339 in the aircraffs maintenance'records and returned the aircraft to flight status. The effect of this change on the aircraft's weight andisalsfise was igibk. Sind no changes were made to the aircraft's basic weight and balance nsfigitt. • • -,• .S; • • Zig Jig sans sand tea inopindlir MSS Malty. IMOD - eatil3 Tani NO AIECyCKALIIIIIIIIISAliAITACIIID MOP ' O Addidonil MeAttaebed. •- SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA _0(1241080 EFTA01326673 oak. no nn 0 MAJOR REPAIR AND ALTERATION (Airframe,Powerphint, Propeller, or Appliance) r Or FeeIAA aflame Ur OS *IAr um.. ...saga 0CSTRUCTONS: Rees bps el slat Sr FM U.I. FAR 43 kart B. as AZ 434-1 a Sawa nab se a 130) enserson or this lam. llis mon b many byla (a U.S.C. ea nobta (Saba so FessfslAanak 14213 Fan to mart enrat kt • as way aarnerneems as to nand $11000 ke each a of 1030). Make Model I. Aircra8 C.uffstream AercoPaw G-nr Sena] No. Nations* and Registration Matt 1085 NSSGA Name (As shown on minion ccrolaa) Address (As shoal on regamon aniffais) 7_ Owner Mellon Financial Service, Corp ff3 4444 One Mak. Bank Caner Pittsburgh, PA 15291 3. Tea FAA Do cna, 4. li ra Ideatfleadsia S. Trod Unit Make I Model Serial No. Rem Alaska Airframe (As desalcd in Item l above) , - I Powerplant N RopeBa 4. Cathnolty Staleopt A. Amnon Nan ad Alarm B. Bind of Apnoy. C. Osaka No. LANCE A. MATTESON X U.S. Cannoned Machado Ufa E. SAN FELRE DRIVE Fagg, Catifwated Mechanic ' AP Mad SCCITTSDALE.AZ SEMI Cgtifated Rana StaliCa Manitheturer D. I cat* tha tha agar andier anti= made to la Inn) lamina Mama then ad dedaslad on the rent. or attsekmanta Mao have bat tank id axonlanee with the requirentoa east 43 dais U.S.Pea* Astion Ragoaketa ad rat the ictfomtaia Maned area ins ad aerie, to the bee my knovadp. Date . sigor{ " 6al /2- ar-ty ate A - -- 7. Approval kr fan larded Natal tots rho* Sv pans upecillid below. is ma tanifisd in an 4 fa band la do ream Bred by tho Adariadwaarof as Pedal Make tartan •MA ft ante at is m APPROVED C/ REJECTED Manufacturer s lag:action Andtaision Ode (Spot) BY loa , FAA Donlan Papa Swim . Pao Approved by Tmepai Cana Manta Croup Pat ofApprovalpi-Rejection Clear* or Dassios ta a l - firer IA Aficba DonneBy SDNY_GM_02754159 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024108I EFTA01326674 REGTSTIT VAR AIRCRAFT 1 CAMERA NO. D ATE* - 2. - fPnit .ta. 4'11 - e• egit i NOTICE Weight and balance or ORcoltnil limilatlen changes shall be entered in the appropriate lime word. An aeration must be compatible with all previous alterations to assize continued conformity with the andiable sicraroithiness requirements 8. Description of Work Accomplished or more spree is sash atittanal theta Wean? with iticral tutonality andointealeis nark ed dew wad complatad) in order to provide contnutly during future inspections, tramenance. and aneratorts a caw of Iris FM Fan 337 Ltaicr. Repair and Alteraton is required to be kept on board the aircraft as long as the alteration remains in coact December 27. 1994. Gulfstrutm Aerospace Corporation (GAC) Model G-IV, Serial Nwnba 1085, N88GA, FAA Musa Type Certificate Data Sheet Al2EA. Aircraft in-service data vi 1856.3 hours & 763 lantings. Refer to the following FAA Approved Data: Grulfetream Aerospace (ASC} 239 SUBJECT: ICEANDflAN PROTECTION (ATA .30) RINDMIELD IWAT -DUAL CONTROL SWITCHES dated Asyut 25, 1994. s:CMP CODE 972390>; and Gulftrcam Aerospace GIV Airplane Flight Manual Section 5 - SYSTEMS, pne 5- 40 WINDSHIELD HEAT FAA APPROVE) 4 February 1994. The purpose of this alteration is to provide independent windshield heat control for the Id front-right side and right front-left side windows. This service change adds a switch and modifies the windshield heat system wiring. Performed all of ASC-239's modification instructions effective for aircraft SIN 1085 riccit for the folowing minor deviations: (see - figure 2. Page 9) • Wire 2H537A20N was changed to 2H537A22N in ceder to fit into ground block 54 position "S*; •. Was 2.11538A20N was changed to 211538A22N in orda to fit into ground block E2 position 'flr; • Wire 211110822 was Sated into 318A1P10 position -II" because position small "IC was not available; and • Wire 2.13 /4 64A22 was inserted inns 3113A11)10 position1st because position small It was not available. 7. Installed parts are listed on page 4 of ASC 239 and were furnished in kit form by GAC product support Savannah, GA. Successfully performed Windshield Heat —Operational Test in accordance with paragraph C. page 3 of ASC- 239's instructions. Recorded compliance with this FAA form 337 in the airerafts maintenance recort and rammed the aircraft to !tight status. Information on the dual switch system will be contained in Section 5 - SYSTEMS of the GPI Airplane Flight Manual, revision dated 12 July 1991 or later issue. • The effect of this change on the aircraft's electrical loading is negligible and no changes uric made to the arcraft's electrical load analysis report. The effect of this change on the aircraft's basic weight and balance was negligible and no changes were made to the airaaft's basic weight and balance report. This a • ecitiptan Reoamod form inspired by Mead Deafly. WORD 6.th 0LO2/95 3A9 Pal NO ADDMONAL SHEETS ARE ATTACHED. *DM* a Additional Sheets Are Attached •a 4 ..• • a a. • s SDNY:Gbl_02754160 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241082 EFTA01326675 IIEG/STRT FAA AIRCRAFT CAMERA WO. DATER 2 - 24 - cM . • .e...+ . q.14 er aser resat Oat OS 0 MAJOR REPAIR AND ALTERATION (Airframe, Powerplant, Propel ler, or Appliance) abet thateltatise .. ......= .... I'alkni i 54-Th.--nonsprs....,..... ota= 5»! -elk 5.. FAR Ca FAA 43 Irarials S. arid AC 4314 (a when*, man ainaf) for taborecta as rispostica crthb fern 111a non le required by Inv (40 U.S.C. 1421). Fenn to next ma resat radii only eat to eared 71.000 for each at. station (karat 001 Friers arta M*410541. Make Model L Aarraft , Galan= Aerospace G-n, Serial No. Nancentity and Registration Mark 1085 • N88GA Name (As shown on natation cenifiate) Address (As noon on narration cerrilleas) 2. Owner Mellon Financial Services Corp #3 4444 One Mellon Rank Center Ptttsburgh PA 15253 3. Far FAA Ust Only 4. US Idestillaitke S. Tree Unit Make I Model 1 Sall No. Ink Maim Airframe eon (As detailed in herniae* .' X Powerplat _ Propeller —,t 1,... TYR* Appliance Meaforass 4. CachnedlyStiluemeS A. Aany• Nom ad Aaiun B. Kind or Anna C. Curdles No. LANCE A. MATTESON X U.S. Certificated Mecharde MAL SAN FELIPE DRIVE Foreign Certificated Mechanic AP PUMP SCOTTSDALE. AZ NISI Certificated Remit Station Manufacturer D. lea* dim the mit. =Gs aeration roods IP the wSO) antigen a Wu 4 above and cliecabed on tha mat or thichraente line bass beat malt in secartbace with the naparemnea Mart 43 oF the U.S. Paden% Avarice Regabsfunis aid the the inform= renteted hint Is tree ad coma to the De my knowledge. Des -4 /--- 2 1 -- eV • r t Amoral for Rerun to Service Panama to the sabotity Oven pesos opocifrid below. Ike and identifier S Se 4 WY Mara baths mass pnecaboiby dm Ad:Manna of tba Faded Avalon Administer and ie CO APPROVED 0 REJECTED F43 Fla Iltmerh Mamaciuter x lassos Arabothrelon CemI Preedfin brew BY FAA Drips Resit Slides. Paso Approver by Trump's% Cada'Airerombrame amp Date of Approval or Rejection Coaxes.' Sigottose of Autkeizedn / - it_re 5---- ! 526705494 IA , re---e P r Mithael Darnel& FAA Tes (01-14) SDNY_GM_02754161 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241083 EFTA01326676 REGISTRY . FAA AIRCRAFT -2- - CAMERA N0, DATE: NOTICE spiropriate aircraft record. An alnico artist be Weght and balance ar operatam bralterion changes shall be entered in the the applicable earworthiness xerroxraomti. compliable with all prwitixtt litterOMO S to esame cormone d conform ity with S. Description d Work Accomplistatel 'evasion enszt sad data wort caresteied.) (If mane mice is repay& ma= =Skald =two Woody with =matt emmohly rot Model G-IV, Serial Number 1085, N88GA, December 28, 1994. Gutfetrcam Aerospace Corporation (GAC) Aircraft in-servi ce data = 1856.3 hours At 763 landing.- FAA Aircraft Type Cakficate Data Shea AI2EA. Aerospace Corp. {GAC) Aircraft Service Change 'Refer to the following FAA Approved Data: Gulfaresm , (ABC) 263 SUBJECT: PLIGHT CONTROLS (An 27) FIRVATOR BALLAST WEIGHT COVER - h; GAC ASC-263AM1 SUBJECT: PLIGHT 'it: REYOVAL dated May 11, 1994 clalP CODE 97239t BALLA ST WRIGH T COVES - REVOYAL dated July 15, 1994 <CMP CONTROLS (ATA 27)21,11VATOR T COIVTROLS (4M 27) ELEVAPOR CODE 972391)1 aid GAC ASC-263AM2 SUBJECT: PLIGH <CMP CODE 9779yz>. Note: ASC263 August 26, 1994 BALLAST WEIGHT COVER - REVOVAL dated Abe cancels and suPenedea ASC-263 AM1. weight covers from the left and right elevators and The purpose of this Aircraft Service Change(s) is to remove ballast Remova l of these Coven will provide easier access to the ballast weights for rework the existing ballast weights. corrosio n in the Mire chance of impaction purposes• thereby helping to detect and prevail the the GAC Computaized Maintenance Program Removed left and right elevators from the aircraft in accordance with (CMPI work codes 273007 and 273008. respectively. I.E.FT ELEVATOR RI El EVATOR 11-88 11.88 DATE CODE 1159C820002-S9 1159CS10001-SIO old PART No. 1159SB40518-1 11595B40518-2 new PART No. 1086 1086 SERIAL No. BALANCE DATA 0.01N/LBS NOSE HEAVY 0.0 INXISS NOSE HEAVY BEFORE ASC-243 14.6 BULBS NOSE HEAVY AFTER ASC-263 17.6 INIBSNOSE HEAVY for secret S/N 1085. Installed parts are listed in ASC Performed all of ASC-203's modification instruction effective support Savannah GA Performed required inaPection 263 pages 8 and 9 for Kit 1 end were furnished by GAC product both clews:es in scardance with instruction i Checke d and balanced of both elevators end did ma fmd any contelo Gpry Maintenance Manual Chapter 27. codes 273007 and 273008to tbeir proper positions Installed the left and right elevators in accordance with GAC CMP in accordan ce with GAC CM? code 273005 and performed on the aircraft Performed elevator control rigging check 277015. gust lock system function ter in accordance with GAC Cliff code ance records and maenad the aircraft to flight Recorded compliance with this FAA form 337 in the sixtraffs mainten status. • A weight change of + 10.0 pounds st horizont al arm 939 was made to the aircraft's Iconic weight and balance repot. Deadly =MD La% (WOW= 3S0 PM 1= bats preyed fin "wind by: a NO ADDITON AL MN= all ATTACHE D. MOW 0 Additional Sheets Axe Attache] ‘4011116; t, • - SON Y_Gi.1_02754162 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241084 EFTA01326677 REGISTRY lAA AIRCRAFT CAMERA NO. DATE, -2 - 3— gas a. iiBaia T. /mule oat, 0 MAJOR REPAIR AND ALTERATION APPIlloce) otrat mts. d ins (Airrinilei Powerplast. Pc0PcileT, Of na...u.... 5 -1 .... -If) 6.2 aearem. for norm= era baSTRUCTIONS: Pitacetypa al mod. SA* FAR 43.9. FM 43Mose B. ind AC 43 SI de ditampara naiads bad) b men dmoseto of die toed Ills roxet is WS by law (49 U.S.C. 1421). Fein to report on road Medd PIMPLY net to 077. 01/I.000 add doted. (Soden 90i Federal Malian Ad of NMI Make Modal I. Airasfr Gul(stream Aerospace G-IV Saul No. Nabonabty and Reparation Mark INS NSSGA ' Name (Pd i/OWII on reparrabon batiks'.) Address (As shown on nigkitnnon terofinee) 2. Owns Mann Financial Services Corp 03 4444 Om Menem Bank Ceiter Pbaaborgb. PA 15258 3. For FAA ties Only 4. US Idacolecalko 5. Tote Unit Make I Mudd I . Soial No. •.... RADS I allege Aidruld (As deaczthed in Item I above) na nn•• • •••""n" X PowaVant Propeller TS,* APPMeco abotaatarer • -' 6. Cahn* MatemaP - A. Allays Mars ad Sao B. KIM ofMay I C. Cobb:m14o. LANCE A. MATTESON X U.S. Certificated Mechanic 8560 E. SAN FELIPE DRIVE Foreign Certificated Malunie AP 1864049 SCOTTSDALE. AZ ansr- Catficesed Repair Station Maitufichner and daienbod m Wa maw a madam= D. Reify dal dta cm* wird Merton mods to Oa SION idadiRad lb item 4 toys MasanRaplaixo ad datOretefomsodon Sao in teas mai la accordmea with We againeams ofPut 43 ofiba U.3. Folded Rostatod halm is trot and mom to the be of kacodatip. Dale ' • /i - Ze fiv o, 7. AMOS ke Ran to Santos by Pam tots dadad dy zWa. yam.' apocifiedMaw. S a lanai:din in 4 Will ibly4dAd alIh• =MIN pluccibid the Adaddausor °fed hard At Aelnsieldnom and is ID APPROVED C REJECTED FAA Ma Rimini. Alddllbalset z IM*4646 ARIlltpliba ober(5pACY) BY - later ' YAADalipab Rapt Dem Pawn Approvad bj 'troupe . CS Airoottbssa Orme Date otApprovd a Itcitebon cetera, *t ' Spume of ' " seemboNo i - if- fr 526105894 IA - ' ' Malmel DalndllY . FAA In /37 (03.94) 9 1 111/14‘ A.:.. - i1/4,44S,,,ak" .19 learela2kack- s,%.. : SDNY_GM_02754183 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241085 EFTA01326678 FAA AIRCRAFT RICERS'S CAMERA NO. DATES G-IV, Serial Number 1085, N88GA, December 28, 1994. Gu&tram Aerospace Corporation {GAC} Model ce data 1856.3 hours & 763 bindle. FAA Aircraft Type Certificate Data Sheet Al2EA. Aircraft in-servi date 12-3-93 for Gulfstream Refer to the following FAA Approved Data: FAA Form 8110-3 drawin g number SE25201105 Model G-1V identifying Gulfstream Aerospace Corporation dated 12/2/93, as FAA REPAIR, BLUED F5793.75Rff (MAJOR) including E.O. Al -483. Approved data signed by John G. Wilder Structures DER SO 793.75 bulkhead that The purpose of this project is to repair damage to the Fuselage Station system . was caused by improper engagement of the GUST LOCK above listed drawing. Repaired the "-901 BLKHEAD" FS 793.75 to conform with the Line 110) using MS20470AD5 Replaced GAC 1159C20509-26 bracket (located at Water rivets and optional HL18-5 hylock fasteners as required. GAC CMP code 277015. Performed gust lock system function test in accordance with fs maintenance records and Recorded compliance with this FAA form 337 in the aircraf returned the aircraft to flight status. e is negligible and no changes The effect of this change on the aircraft's weight and balanc were made to aircraft's basic weight and balance report 01/02/95134 PM This is • compute mauled foon prepend by. Michael Donn*. . WORD 6.04; NO ADDITIONAL SHEETS ARE ATTACHED. gams D. Additional Sb:eis Are Attached • „ -airs ‘1.,;SNiertpkz., SDNY GA4 8, 9, 10, 15,_0 an SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, d4 17 275416 EFTA_002410116 EFTA01326679 a.... a 4. onacid I* FAA ow Owls MAJOR REPAIR AND ALTERATION el Ma Ilearthasiot 0 ii Dgaris• (Airframe, PowerpLant, Propeller, or Appliance) d Triniermim riSd 'slim 5)4. eCS 0 Adam/40•••• rind arid AC 43 9.1 (or Man aka tot) for drat INSTRUCTIONS Frts wtat* ad 4,117109 5MFAR 43.9. FM 43 APlakt 8. dsposliced of ahem. Ilia report 4 oanid by WA (49 ll S.C. 1421). Faa to ran as an 4 SF MIMS nal to mad SEWS Rs wa ad. at, (Sadon 901 Federal At Ad of 1958) Make Modal I. Aircraft Gultstream Aerospace C -IV Sand No. Nationality and Registration Mark 1085 MEGA Name (As shown on reargion =drama) Address (As shown on registration mite) 4444 One Mellon Bask Calder 2. Owner Mellon Financial Services Corp lO Mahwah. PA 15258 3. For FAA Use On) • R I DS Ideadaikation S. Too Scrod No. Reps Sage Unit Make . Model Airfhme (As descobed in Imo I above) X Powerplant • PropeDer . The Apphanee Materszr 8. Cadernall7 Mallernme • ad Mare . B. Sled of Agency C. Coles No. A. Agiall It LANCE A. MATTESON X U.S Certificated Median° FONIAP Certificated Mechanic AP 1864049 150 L SAN FELIPE DRIVE SCOTTSDALE, Al. MSS Certificated Repair Station Mandamus ad dmatted tette more or arm= D. I comfy Rs the reps atm shams made to the °nth) toned ea seen 4 above At Regahaims mid din We inf=oncm bum We tom made in empress SA the sequireinexes of Pat 43 of the US Faded _ fornislutl hennas trot ad cooed radiate of_m, knowledge. Dent Snymuie g -' •2 54- tY Ce 7. Approval for %Moro to Bona seer isiqoaad laths ems proositod by dis Pursuant's, WKS Om person specified bdow, the nail Sated is km 4 A na albs Pedant Arledge Athrdsdansion ode T APPROVED O REJECTED MARL DES* Minufactuter inapiciice Anaolizstkei COS (Spa) , Rymer BY FAA Doormat Reps Swim pan Approved by fl agon Clear Mrworthlas 0roop . . . Date of Approval a Rejection Coolies et Aril= Or . ClagmlitS146. - ..... .....--.. 52670504 IA Weasel balmily I .7k . it NI* .:+a 40 111S 110 1.%t-t.s. EDIritaM_0275416 A SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241087 EFTA01326680 REGISTRY FAA AIRCRAFT CAMERA NO. 3111 DATES - 2-9 (145 NOTICE Wright and balance or operating honttoon charms shall be entered in the appropriate eirmenrecord. An skeleton roust be compatible with all previous alterations to assure conimued conformity with the applicable Swarthiness requirements Dnatptko of Work Accomplished Ofmon sax is required. tech addctional glues Identify wish &mart ratiorckty red mom= mat end Si work completed.) November 30, 1994 Goats= Aerospace Corporation ic.Aci Model G-IV. Serial Number l06S, I.O3BGA, FAA Aircraft Type Cediticate Data Sheet AI2EA. Aircraft in-service des - 1856.3 hours and 763 landings. Refer to the following FAA Approved Data. FAA Form 8110-3 date 12-22-93 for Gulfstreant Model G-IV identifying Gulfstream Aerospace Corp drawing number SE05813101 CORROSIONREPAIR BALANCE WEIGHT INSTL AILERONas FAA Appruvcd data signed by John G. Wilder, Structures DER SO-483. The purpose of this project is to inspect and (if necessary) repair all balance weights and holding straps of the LH and RH ailerons. This inspection/repair involves: A. The removal of the left and right aileron from the aircraft B. Removing and identifying the straps and ballast weights to gain access to the balance beam assembly; C. Inspecting the weights, straps, balance beam, and attaching hardware for corrosion; D. If corrosion is found, the removal, preparation and/or treatment of the affected areas; and E. The proper.re- assembly, balancing, and attachment of the aileron control surfaces to the aircraft. In accordance with the GAC Computerized Maintenance Program (CMP} coda 271013 and 271014 removed left and right ailerons from the aircraft Removed the 1159=0602 straps and balance weights from both Maus. Identified all taps and ballast weights for proper re-assembly and inspected balance bans assemblies. Paformal inspection of both aileron assemblies and attaching parts in accordance with the above referral to GAC Repair Dwg The inspection revealed: balance weight straps had no corrosion and Wand weights had corrosion. Performed REPAIR PROCEDURES of above relayed GAC Repair Ds% step 4. for BALANCE WEIGHTS, including um:ructions contained at Engineering Order Al for the drawing SE05813101, dated 11/21/94. Using the original I I59CS20602 straps. installed the treated aileron ballast weights to their original position with new attaching hardware. In accordance with the GAC Maintenance Manual Chapter 27-0, Flight Control Symms, check the balance of both ailerons; LH aileron 20.05 inAbs. NOSE HEAVY and RH aileron 21.89 in-Abs. NOSE HEAVY (tolawice 0-32 in/lbs ) In accordance with GAC CMP codes 271013 and 271014 re-installed the left and right ailerons to their tipper positions on the aircraft. Patterned aileron control rigging check in accordance with GAC CMP code 271005, Performed aileron manual and power system operational tests in accordance with GAC CMP coda 271001 and 271002 respectively. and performed gist lock system (erosion test in woad:ma with GAC O3.(P cede 277015. The aircraft was tan Down by two appropriately rated pilots and it was determined that the repair did not change the flight charadaistics or substantially affect the flight operation of the aircraft Recorded compliance with this FM form 337 in the aircraft's enaidenance records and =mudd the aircraft to flight status. No changes to the aintraffs weight and balance resulted from this repair. fen wpm.] by flits I Daselly. Mord t Oc OVUM 31/ fie This I • mews. sad NO ADDITICROL StIEETS AM ATTACHED. IND. Adektional Sheets Are Amidst .v?..Crtai. • SDN Y_GM_02754 166 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241088 EFTA01326681 1‘ 1431 bar --3 r AA AIRC CAMERA NO. DATn 12-7-94 WIN. 2115013) 0 MA.JORREPAIR ADO AlinRATION Twat Use Ody us tn... OSC• 1416thalit* 4 ....... - (Airframe,Pan-plant Propeller, or Appliance) 7444 A4... Mialens.• - . . 9c -e:. il 1 inSTRuCT0NS Print or type all entries. See FAR 43.9. FAR 43 Append:A O. and AC 43.9-1 or subsequent IVYS len thereof) for illitIlaCti011S and dispootion of this form. This report is required by law (49 U.S C. 1421). Fain to report can result Ina civil penalty not to used $1000 lot each such violation (Section 901 federal Aviation Act of 19583 Make Model' I. Airmail Gull-stream Aerospace -GIV SciaLNo. Nationality and Registration Mark VMS PIMA Name (As shown on remotion caufiate) . Address (As shown on zegimmian certalost0 2. Owner MELLON FINANCIAL SERVICES CORI' 1O 4444 ONE MELLON BANK CENTER PITTSBURQL PA 157.31 3. For FAA U se (My A DonIdeonfkaaloo 5. Type Unit Make .1 Model I Serial No. Repair I Minion Airframe (As demated inItem I above) X . z. . .. .- Powerplard PropcDer • Type. Apphance - bbnatenner - IA Geothermal, Statement - _ .. A. AnneysI4aee i mad Addnea B. Kind of Agency C. Cenifecets No. LANCE A. MATTFSON X U.S. Certificated Mechanic - 1560 F. SAN FELIPE DRIVE Fenian Catenated Mechanic AP 1164049 SCOTTSDALE, AZ 8.5291 Coat:mated Repair Station . - - *Mainifactitta i D. I certify that the repast Sot Samoa made to the atri(a) identified in hem a above eat chanalied on the reverse or anectnnetas henna have been made in err:edam" with the rocrairesomus ofPin 43 of the US. Federal Aiitin Ripsistions and dim the biformoon forrisbed herein is mu and correct to the bat ofisiknowlecbtA Dust Signana c}sjit i utbonzed 06 2 7- fly ' T. Approval toRem te Servke Parsee* the amhority given pants specified ban. the well idsmified in item 4 ow nmpenedM the manna presmbed by the .1dmithansits of the Federal Ablation Adenainion god is LEI APPROVED O REJECTED - FAA 111- S:Ndsd, 'manufacturer r ile/peon= Ainhonation . I Other (Spsify) bspeaer BY FAA Dengue Rept Station Palos Approved by Tramport Cards Airwatlainam Orono Dale of Amcor' or Rejection centhno• • . . Slipmtne ofAuthorized • ' . "IPS". -. IrCrIs i MiamiDino* FAA PermIII (9144) --- ".4 •442C4k }RFC"-rilrat lane SDNY GM_02754167 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241089 EFTA01326682 61opiaafte„. 2,1: sells743144Wfisan6 eszro- NOTICE alteration must be ide aircraft record An utt on cha nge s tha n be entered in the appnap ble airw orth ine ss rem onements. _ rating !m hca Wright and balance or ope to ass ure con tinu ed callow* with the app vious Litt:canons compatible with all pre completed) ion mark en4 etas work ork Accomplished raft =Monate,' ad resisins I. Desertptlen °M an& mach eictitiocim slaws Wen* coat airc s (If mat spere is rem ons a true copy of thi ule ins pe cti on ;, ma intenance. and alterati n remain in effect. continuity during &R g as the alteratio In older fp provide ard the Smart as Son il 33 7 is fe cu nd to be kept on bo er 1085, NM& FA A - FM Em Mo del Cr-IV, Serial Numb e Corpo rat ion 'CA C} Gulfstreare Aerospac & 736 landinp. AUGUST 26, 1994. data - 17116.6 hours • ica te Da ta Sh eet Al 2EA Aircraft ill-Set Aircraft (Type Certif 4, MA KE Cru lfst rearn, ta: - FA A Fo nn 81 10-3 DATE 7-1R-9 ion , LIS T OF FAA Approved Da Aerospace Corporat Refer to the Mowing ME OF AP PL IC ANT Cruftgream E EN HA NC EM ENTS, PE Airplane, NA der Al), TALE BR AK MODEL GIV TY 96 (En gin eer ing Or Pa rt 12 Drawing ATION 115%8412 Seniee Change 296, DATA IDENTIFIC ST EM S & EQ UI P, and GAO Aircraft 0 Bn kc Bu ng ee. - SO761, SY ing 1159SB4056 DER- R. IPESSON ctor and PartM Draw BO 63 Ground Spoiler Reani eration by installing 115 914 300 36 ove `brake-by-wire ' op The purpose of th is alteration is to impr pressure ports to alleviate wi th th e gr ou nd spoiler actuator input reased tension. restrictors in se rie s yin g th e br ak e pe da l bungee's to obtain inc modif hydraulic demand mid AP 977960>. AD pas were instaBed new s for Par t 11 and Per t Dl orGIV ASC 296 <O cation istmuction . - Performed an of modifi t Support, Savannah, GA :cam Mosinee Produc actuators and obtained from Gullet the two ground spode( from the pre ss= inp ut ports (PI and P2) of 1-0 6le t acc otd anc e wit ato 001 ove d fou r eac h Pa l MS21916164 union &t ctor &Pap with new "0" ring pickings, 115902 Rem R.estri PM MHX031590013A and installed four each GA C Drawing /1550430036. s con tain ed on ance with the the instruction x confagurabon in accord Bra ke Ped al Bu tte 's to P/N 11595B40560- OU T &K NE E FO RCE Reworked d each GAC P/N 1139CA0040-x 405 03, 0W 8R AC EP ETtea, BlthiGEEBIUKE CACThawing 11398B as follows: insbuctions contained on & 3 34•3. Installed the Bake Pedal Bonne's 1, 2, coog Pia MINE ccer .AD JUS TM EN T She ets - .WMALMNSIOti 43 S LB S: 324171 poonort • • P/N 0211 241 LBS. 324172 1159%40360-1 43.6 LBS. Pilot's Left C03 9 . 24.2 LBS. 3 LB & 324173 1/39SB40360- 2 43 Pilot's Right 931 340 560 1 03197: ,..- 244 LBS. 43.4 LBS. 324174 Co-pilot's Le l 115 243 LB S. 9SB 403 60- 2 0337 113 Co-plot's Right Whed Brake Systais- det Si tte t Op era tiag:fort enentiot> aound Spo GAC <CMP 276001>'C Successfully performed 324103> AntiSkid System-Fonction Test. • . st and <CA W • e response at Panaion Te ts: The pilo ts tested for ptoper blu app rop iate ly tide d pilo e wh eal ste ainq. No ted by two s, and nos A Cammd Taxi operati onal test was conduc ns wh ile opa arin g win g flaps, goad spotles plot and copilot positio =Ma taxi speeds from • cF en witcti digit status ainVI620 409 60 0t” d retuned the aircraft to 337 in the aire ratt s trtailnalat/Ct to:aidsen h this FA A form Recorded compliance wit a “ad's base Merges were made to the bas ic we igh t end bal ance wait neftlagTh-ble end no on the ant:ars The ef&et of this dense ort. 'stied end baba= rep 01024,1;43 tai_ watt) ass. nam ed kiw i sene wirs by. Wood bcaially. - Ns hese/Poe L AITAOIED. NO ADDITIONAL MIMSAiL Atiebat ' -O -Additional Shall Ne --7a•IrTvik SONY G G502754168 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA ornai non EFTA01326683 toured OIOD ... oda C ler FAA Theo oyes MAJOR REPAIR AND ALTERATION (Althaver, Powerplant, Propeller, or Appliance) Oen 14eadmiee ,............ . .0 C- r - 510 .... evSTRUCTIONT Print Or type all entries. See FM 43.9, FM 43 Appendix 9. and AC 41.9.1 (or subsequent revision thereof) for instructiOrn and disposition of this form. This report is required by Imo (49 USG 1421). Failure t0 report can result In a cUll Penalty not to need 51.000 for each such violation (Section 90l federal Aviation Act of 1954). Make ,Model I. Aircraft Colrain:P.M Aerospace G-IV SailNo. Nationality and Registration Mark 1085 NSSGA Name (As aberion on repatrwion arrtificata) Address (As thorn on reamine,n cen.Lime) 2. Owna MELLON FINANCIAL SERVICES CORP BD 4444 ONE MELLON BANK CENTER PITTSBURGH. PA 15153 3 For FAA Vieth* .4. Uole Ideal/Ratko - - Line Unt Make I Model I SallNo. • Repair Ann Airframe (Ai described in Item I above) X . • Powaplant , \ ... Propeller TYPe Anoltance Mmttfattarer - a. Cadermay Matemeor A. Matey, Sc. end Addreas A.KW of Niamey .. • . C. Octilkela No. LANCE A. MATTESON X U.S. Catifaceled Weber& 8548 E. SAN FELIPE DRIVE port Lea ca4theatal Mechanic AP 1864149 SCOTTSDALE, AZ ISM Catfitated Rata &Mae I Martufaataa D. I ratify t the repair mar Mention node to the onn(s) identified m non 4 stow and &Shed oa the muse or gtschwints hem have two made in r.conLince wilt the napineemm of Pan 43 of ths US. Faded ArketooltecoMions me that the incantation furnished hem" is true nod coned to thebera 0 my lascrwiedge Owe friPernrefirralrifrldrE . g 7- ft( -----.7e .C„ C, 7. Approval for Reran le awake Ps MIS wrap &V pemommacifiM below. the unit HSU! la item 4 was torplaae ha the mew prescolve by the . Ahead. Attie Petted Avilioe Adoiron and S 0 APPROVED 0 REJECTED FAA Pk Or WS Mandictura x lxvictica AildiCS31% .0her(Srpeci(y) BY taps . I: FAA Dmipm Rise; .48691. .. . Pawn Approved by Tnospxt . CisinAtecedirsettittop Dale plApprova or Rejection °AIM. IF " , gpaRpm Of DeOritialt.- .8 — Z9' -s V SISM5491 Lt Michael Donnefry • I M-4.D.O/I0/4..",.. • •••• • ••••• SONY GM_02754169 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, -15, and 17 EFTA_00241091 EFTA01326684 FM AIRCRAFT ISIKY • CAMTRA NO. DATE: 12 -9- 74 NOTICE Weight and balance or operating thretabon changes shall be entered in the appropriate airerae reconi An alteration must be cons pa olge with all previous alterations to ass= continued cantos:miry with the applicable airworthiness 11881801:Mall3. 8. Dvscriptlec of Work Accomplished of more spice is remand. each adduiciutl them. thmtity with that mdonally and mist mark and dee work completed.) in order to provide cordhurty during future inspections, maintenance, and alterations a true copy of this FAA Form 337 is required to be kept on board the aircraft as long as the alteration remain in effect AUGUST:26. 1994. Gulhtream Aerospace Corporation (GAC) Model G-IV. Said Number 1085, N880A, FAA Aircraft Type Certificate Data Sheet Al2EA. Aircraft in-savice data ••• 1786.6 hours. & 736 landings. Refs to the following FAA Approved Dalt GAC Aircraft Service Change (MC} 232, SUBJECT: ICE AND RAIN PROTECTION (ATA 30) WING TEMPERAWRE LOW MESSAGE — PROVISIONS, dated December 17, 1993. The purpose of this alteration is to activate the "WING TEMP LOW" message (Amber) on the Engine Instruments Crew Alerting System (EICAS) and mask alert if the wing has not reached 100 &tors Fahrenheit after two minutes from being selected ON. Performed all of ASC 232's modification instructions effective fOr A/C 1085 except for the following minor dm.iations: • Coacplt Overhead Panel: Existing wires1H151D20, IFINA20, 2H151C20, and 2E126A20 were replaced with new NSW. 22759116-17 to ft GA0335)4L22DS contacts provided with new wing anti-ice:wit. Avioniat Shelf Assemblies: Al added wire connections to the Fault Warning Computer(s) and Data Acquisition Diggs) 'Mt made directly to the rack <on:tenons) Stead or through the shelf disconnects. Main Junction and Relay Panel: Wets IH152F22 and I.H152X22 was remove from T113M positions If and G respectively and spliced together. Win 2H152.1G2 and 2H152F22 way rand from T720 position G and K respectively and spliced Wither. Wire H9076B22 was spike to wire 1H1S2Y22 near Data Acquisition US MI, 95A4PIB pia, 17. Wire H9071322 was spliced to wire 211i 32T22 near Dan Acquisition Und 12, 95A5FIB pin 17. Wen /49078A22 and H9078AA22 were spliced bribe( with wire I HI87D22 nor connector NAINC pin 89. Wires k19079A22 and 119079AA22 were spliced togetha with wire 2H1I37Dn near connector Nmptc pin 91. . AU of the deviations that wire made to the apprerred design %Senecessary to provide for compatibility with existing approved configurations: It has been determined that the deviation made did no after the intent or operation of the approved eiraeft savice change, • • -- -•• All parts were provided in kit fotro and obtained from Gulf:strain Arrospece Produh Ruppert, Savannah, GA Sucossfully performed ASC 732's operational lest. Recorded compliance with this FAA loon 337 in the aircraft's rneintenan ce records and reigned the aircraft to fl ight . . _ The effort of thirchange at the aircraft's basic weight and balance was negligible and no changes sect rna..te to the aircraft's hthic weight and balance mon. lli.as =war romiud fonaprrmul br. aOdsI Omani,' WOAD 6 Oa 01/2691Strt PY NO ADDMONAL stores AtEMTACIIED •E`te 0 Additional Sheets Are Atractu:d • • ST-, - .• • ....atejalate-, ••• ' -1;4 • • • • J . • 4 . .klietialHAPP4 1 7:7- -.7 SDNY GM_02754170 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241092 EFTA01326685 P =nth • CA1CRA SO. I DATE: I 2 _7_ 94 ram Cow :If On I2 MAJOR REPAIR AND ALTERATION Fiera manse us tarown en ' -- - (Airframe, Powerplatot, Plojoeller, Or Appliance) Me 2e kleatifisetian ..... sr...seer INSTRUCTIONS: (,-ics4 O Mot of type an entries. See FAR 41% FAA 43 Appendix U. and AC 43.91 (or subsequent insqintions and disposition of this form. This report Is required by Una (49 US C. 1421K Failure revision !Steen for t report Can result Is a civil mobil, not to exceed S1,000 for each such violation (Section 901 Federal Aviation Act of 1950). Mats Model ' 1. Aircraft Gulfstream Aerospace- G-IV SaidNo. Nae003MY DM Rogistsation Matt 1085 NSSGA Name (As Amen on Illtalle01/ califlone) ' Address (As shown on DOS:Sion Patina.) 2. Owner MELLON FINANCIAL SERVICES CORP ICI 4444 ONE MELLON BANK CENTER PITTSBURGH. PA 15253 3—For FAA Uwe Ott A Unit Mead:Sena= 5. Tne Unit Make •' . I Model I Sail No. papa Minion Airttame *r n :•• • •••••••"'• (As desenled in Item:above) X Pow*** Propeller TYPe hernefieraree 6. ConterenttY Swetweseed A. AP:00 9 Tleme and Address B. Rind of Amoy C. Cctk*s No. LANCE A. MATTESON X US. Certificated Mechanic. A - 856$ E. SAN FELIPE DRIVE FeeWen Catifioded Mechmic ' AP 1364049 SCOTTSDALE, AZ 332.58 Certificated Rosa SUM* Manufacturer : D. I certify that the rep* endior ekeraion male to the noi(e) identified in item 4 tow end detailed on the &vav or enachmenu lino have tem male hi leatednoce with the :Neiman= *Pr 43 of the U.S. Fedenl Avisean Replaeom and via the infixivenon fornithed her* earn wad coma to the bed ofmy Dunned* 9 -,77 rr G. 7.' Apart:9M for Return to Savke Patio the ember*given moons specified Mk* the ant identified in son 4 win hopeaed in the wanner tresedbed by the AflisizelorattheFail Avid= Admlainice and IF OD APPROVED 0 REJECTED FAA De an* BY Menu:Setae* X **Mon Awhothation Other (speedy) FAA Nips Rep& Station I Paton Approved by Troop* CUBIC" MIWOOkillall. Cecesp Date ofApperef or RMection comma., Brit= of • - Deeps* we . 9 — a9-- IY 526705494 IA' • Michael Dcamay SDNY GM 02754171 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241093 EFTA01326686 -=.;,17.17...-4.-fttrftralle„wPnenaNCeinwinvan'7"-'7, IM Allts.RAnlatTgr - - CAHEPA NO. DATE: 1 2_ 7_ 94 NOTICE • Wright and balance or operating limitation changes shall be entered in the amperage aircraft record. An alteration tut be compatible with all previous aluranons to assure continued conformity with the applicable airworthiness re:pit-tents. I. Desaiptien el Work Accomplished (if more span b required, attach addeacual sheet identify wida entry and regnewrion mark rid der a work compleuct.) In order to provide continuity during future inspections, maintenance, and alterations a true copy of this FAA Fame 3371$ required to be kept on boird the aircraft as king as the alteration remain in effect. AUGUST 26, 1990. Gulfstream Aerospace Corporation (GAC} Model O-1V. Serial Number 1085, N886A, FAA Aircraft Type Certificate Data Sheet Al2EA. Aircraft in-service data = 1786.6 hours & 736 landings. Refer to the following FAA Approved Data GAC Aircraft Sent Change (5C) 255,.SUIEUECT: INSTRUMENTS (ATA 31) SNAPSHOT SWITCH INSTALLATION, dated May 5, 1994. - The purpose of this alteration is to provide thc crew with a switch that recants engine parameten in both Fault Warning Computer's (FWC) non VI)Litilc memory. Paformcd all of ASC 255's modification instmcdons effective for A/C 1085 except for the following minor deviations: • • Cockpit Overhead Panel: Installed - SNAPSHOT- switch ASC255DSI on overhead panel in the spare vacant position adjacent to APU fire test switch. Comucted ASC2.55XDSI switch tin wiring as follows: Pint...are FD9030A22N to ground block E2 pin W; in 2 wire FD90213A22 to 318A1P7 pin small U; no why Jumper 22 to Pin IT, all wire FD9030B12 to ground block E2 pint Pins 5 79 All no connections: MA wire W5281.022 to172N Pin D: punB wcc FD9029A22 to ocancrior 31ILAIP7 pin small V; and pin 1p wire FD9031A22 to commenter 318A1P7* small W. • Avionics Shelf Assemblies: Connected wins from 318A1P7J1 ai follows: pin small U wire F09028B22 to Annannator tights Dim and Test Box- 29AIP2C pat 11; pin small V wise Fusvats/2 spliced to wires FD9029C22 and FC9029D22connected to FWC I I •95A IPIA pin 81 and FWC a 2 95A2P1A pin 81, respectively, and pm tan W wire FD9031B22 to Annunciator Dan and Test Box-29AIP2C pin 64. All added wire connections to the Fault Warning Computer(s) and Annunciator Lights Dim ted Test Box were made directly to the rack conneenx(s) instead of through the shelf diatom:Cs. All of the deviations that were made to the appnived design Were necessary to provide for compatibility with aiding approved eccfignaticra and allow both pilots access to the - SNAPSHOT" switch. It has been determined that the deviations made did not alter the intent or operation of the appoval aircraft service change. . • .. • - All parts were ptirdiased from GulfstrearnAaraiiiiiiProdurit finning. Sawing, GA. Successfully_perfamed ASC 255'S nperational test Recorded compliance witlithis FAA form 337 in the aircraft matte reteds and retuned the aircraft to flight stains. •• The effect of ibis their 'dotal load =WW2's %alibi =abaft. Fair fair t eNAFSHOr swath indieaas, is from the o'HEAD LTS PWR 02 aieuit breaker -8HAPRHOr Sint lamp mane &ow (When snapshot switch is prayed or during wanting fights tesOkssthan 02 ats in tnighit10.05 till in .. . The effect of this change on the aircraft's basic weight aid balance w® negligible wid charges were made to the ainitaft's basic weight and balance report • - . NO ADDMONAL man, An AlTACRED •19-496 a Pidmonal MO= Are Attached z..s. - •yrv.ne!-I;+wfrr- ti ' I • -en h •-J-h 4i l % SDNY_GM_02754172 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241094 EFTA01326687 Fe .... csa X. norm 0 MAJOR REPAIR AND ALTERATION r 1r nAth•oute (Airframe,Powerplant, Propeller, or Appliance) des,, siScarica terns tilat••••• iRSTRuCTIONS: Print or type all entries. See FAR 43.9: FAR 43 Appendix El. and AC 43.91 4 ts c ,. / .0 " instructions an disposition of this lone. This report ts required by Ire (49 US C. I421). (or subsequehe revision thereat for Falun penalty not to exceed 51,000 for each s Leh 'violation (Section 901 Federal Artaterin Act of 1950). to report can result loaded Make Model I. Aircraft CulTstream Aerospace G-IV Said No. Natisnably aid Reettalion Mack 1085 MISGA Name (A. shown on repartee enflame) Address (As town orimgetricion eatiame) 2. Owner MELLON FINANCIAL SERVICES CORE' SS 4441 ONE MELLON BANK CENTER ' PITTSBURGH, PA 15253 1 For FAA Us• °ray 4. Unk Ideonacetke 5. Tmee LIM Mt I Model I SailNo. Repro APCIelon Mfrs (As dosentedisIt •••••••••• ... . X Pomp= Proper -.. , TYPe Appellate Mamba= 6. CaMormity Staley= - ... - A. Aspera Nine and Addis B. Kind of Apnc C COMPlitlo: ' LANCE A. MATTESON X U.S. Caicos Mecksinic , 1360 E. SAN FELIPE DRIVE. Foram Catifteatesi Med= AP ISSN= SCOTTSDALE, AZ ISISS Catificated Repair Stagm —Manufsetura D. I catty Mt the rep & and/or aced= rude to the asps) idatitud ict item 4 above ad deaMed on the mime or metements hereto bevy been made m read= wilt the repherrenta of Pert 43 of the U.S. Pedant Let Replalems end dm the informar forentiest hicas is troe and cord to the Mom knowledge. , Date V /eV ------- r r 7. Approval for Remo to Sas Pmassatw the =MeV given ponces specified below the MI Acidified to dome me impeded SS razor preembest by dm Methstamor calm Federal Awallcm Adrolestralice ands 02 APPROVED O REJECTED FAA SR palm& Nasseactunr x thapciSionAtabodation c ater(Spedy) BY ars , FAADeepene Peprix &Rion Pawn Approved by Trietsgoet . t Casts Airouthiosse cheap Dine ofApprove( or Rejection Ccormft.w .' Signature of Assatotized ' Desiengtee N - 8 —/s--- 5° se .526" M S IA • r SDNY_CM_027541T3 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241095 EFTA01326688 NOTICE Weals and balance or operating limitation changes shall be entered in the appropiate aircraft record. An alteration must be • compatible with all previous alterations to asnre continued conformity with the applicable airworthiness requirements. & Dentriptlea of Work Accompllthed - at more epee is required. each deuced Mesta dairy web secret ciacualny and minion mat and die work peefeiseet.) In order to provide continuity during future inspections, maintenance. and alterationfsv anlioopy of this FM Finn 337 is required to be kept on board the aircraft as long as the alteration ' in effect. AUGUST 14. 1994. Galant:am Aerospace Corporation (CAC) Model O.1V, Serial Number 1085, N88GA, FAA Aircraft Type Certificate Data Sheet AI2EA. Aircraft in-snee data = 1786.6 hours & 736 landioid.' Refer to the following FAA Approved Data: Gulfstrcam Aerospace Corporation Aircraft Service Change (ASC} 295 SUBJECT: AIR CONDIT7010110 (ATA 21) CABINPRESSURE*MANUAL CONTROL DVS7'ALLA77ON dated JULY 22, 1994. <CM? CODE 972950> The purpose of this alteration is to allow the cabin'air pressure control to revert to snuff operation in the event 115 VAC power to the pressurization system is lost. Presently, if 115 VAC power is lost, the air pressure transducer and the outflow valve will fat - 32.5AIKI0 MODIFICATION: Price to preforming ASC-295's modification instantiate modified the eating mita Ray & lunction pond to provide for expansion Removed 8, discarded Sating May 315A1K10, Deutsch P/N E4104 385; Exacted all of the wires from socket 315AI XXI°, and Removed te discarded relay socket 315A1XKIO, Damsels P/N 65009004.513. Installed a new Deutsch P/N 65009001.513 relay soda at eft position 32.5AIXKI0 & connected existing wires as follows: WI33D22 • A1; W132F22 - A2; H9014A20 - B1; H9015A2ON - 82; H9013A20 - B3; 09056A20 XI; & G52A2ON - XL ASC 295 DEVIATIONS: Instant:dancer Deutsch P/N 65039-008-513 relay socket adjacent to nil position 325A DOC 10 (see above) and identified as ASC295XKI instead of the relay, socket and bit listed in ASC 295. Perforated all ofthe wising changes shown on Figure 4 of ASC 295's irectructiont amp wires DU/113B20V and DIOICC2OV wee asserted into 326A I P200 and 326A112.00 (espectively) potation P instead ofera T. After completing edam and ring out. installed a new Leach P/N 1A-W4F-005 (aka GA11335590 unto socket ASC295XX1. All of the entailed pasts were purchased from GAC Product Support Savannah, GA. Successfully pained the installation checkout listed in Paragraph B pages 4, 5. and 6 of ASC 295 instructions. Recanted =Same with the FAA font 337th thitherafrs maintenance records and returned the aircraft to flight sums. It has been detennined that the intarebaimehip between this dungy and any previously approved cooftpration will not introduce any adverse effect upon the arworthinionfthe aircraft This deemxinalion includes, but is not boded to. My modifications or deviations made did not atter Pa EMI ofthe approved ancralt service change; Mum performing its maided functions the operation is augment; No %at manual smedameras are require& and the installation is compatible at all previous therations assuring continuous conformity with the appleable ithWOOthilleSS requiremmts. The effect of this change on the airgartelicititial lee4ingtwill be 0.03 amps added to the CABIN PRESS 115V thieuit breaker, essential 115 VACIstes:j...s, _ • ... She act of this change on the airtisfei basic weight and bitten — negligible and no changes were made to the aircraft's busk weight and balancereport • - .. • . . aercaor paredEnnal by. Itdst'Decal WOIUM ON - tandem SAMS - NO ADDMONAL!MEM All Ansium tat 0 Additional Sheets Art Attached • "fr,,'. _ st: .e'• -a • . .t • -44, :•••• . • . _art....c-s,--?entifilsaselleSill*Pere7 SDNY_GM_02754 1 74 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241096 EFTA01326689 ,.....",4 MOM tine= /ItIAA Ono Oily 0 MAJOR REPAIR AND ALTERATION fno ea (Airframe, Powerplant, Propeller, or Appliance) Oilkelocoirsaise . ,..SAME 'Simla 4-ec - t's % MIR Print or type an entries. See FAR 43.9. FAR 43 Appendix It and AC 43.9.1 (or subse trent revision thew!) for insminions and disposition of thks form. This report is required by law (49 uS.C. 1421). failure to report no result Ina clod penalty not to weed 51,000 foe taco such violation (Section 901 federal Aviation Act of 19S 0). Mae Model I. Antraft Gulfstream Aerospace G-IV No. Nationalny and Registration Matt 1085 NSSGA Name (As thorn on niftstraticat arena) Addams (AS IbOVIa 011ttOttri011OlitiliCOW) 2. Owned MELLON FINANCIAL SERVICES CORPUS 4444 ONE MELLON BANK CENTER ' PITTSBURGH, PA 152.58 3..For FAA Use Thdl 4. US IdeollIcanon S. Type Unit Mae 1. Repair Aturadon Akers (At damiadinItmn I Mon) "'in n " ********** X Powaplant Practise .. Ng Msarthamer • . — fa Coneamily Surat A. Aisayb Nine and Addreee IS KIMMir C. Caeca No. LANCE A. MATTESON X US. Certificated Mechanic $560 E. SAN FELIPE DRIVE Patio Catificared Mechanic AP MOMS SCOTTSDALE, AZ 11525$ Cation& Pamir Station Minobetatex D. I naryIS me rapt and/or anion made to the imiaNdaithed inEno 4 Mon and deeedbed on the myna or inedanento beneo have boa wade in sem= nth the requiems= ofPut 43 of the U.S-Fedeni MIS=Rem and that the informetioo fandsbad tonin is tree =ad =tett° the bac my lamededid Dan )—ts,-5, y SiPar 418 d 7. Anomalies Rearm to Scoriae Parent to the ..homy given perms specified barer. W nonModified an in 4 misspend Isi dome=preamlied by the Azteanmeor ate Facet minion Adman:aim =dal Ila APPROVED 0 REJECTED .. AAAFt Semd•d• Memitactunar I Inspechou Ambocintion 9!1, 1(3$410 boon BY Empalme* Rent Mann Person wawa by Daemon • • • Camila Anwortkbas Oran Data ofApproval ar Rejection mama. or - Sipoovre of RearefiaaM . ST6703494 IA _... 7.-otti ,„,," MichaelDonndly efrr/95 1 tareen511(0.494) • • • teces_1-•• ...-.:Atalusa.: • SIJNY ' brA 0175417r SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241097 EFTA01326690 •- • Icis,vksoi.:,:;1 AttarrAfgYegir,it M AIRC CAKERA NO. i • 12-7-94 -• • Nana Weight and balance or °Mating Limitation changes dun be altered in the appropriate atrcraR compatible with all previous alterations to assure continued reo,rd. An alteration must be conformity with the applicable throcorthiness ro:ryercmcnts. S. tamertyttea of Week Accomplished (If more apaar a main& math %attired thects. Itlesity with siren& nsionatity and "misuse= an and claw wed cors[plaied.) in older to provide continuity during Mute inspect ions, maintenance, and altmations a true copy FAA ram 337 is requited to be kept on baud of this the aircraft as bog as the alteration tetnain in effect . AUGUST 14, 1994. Gulf:ream Aerospace Cbrpora tion (GAC) Model G-1V, Serial Number 1085, P/88GA Aircraft Type Certificate Data Sheet Al 2EA Artraft , FAA in-service data - 1786.6 hours & 736 hmdings. Refer to the following FAA Appired Data: Gulfstrcam Aerospace Corporation Aircraft Service fASC) 313 SUBJECT: P Change 4TICS (4E4 3e9 OWN PRESSURIZ477QMSTABIL DECEMBER 17, 1994. ••• IZaj77ON dged aCODE 973130> - 7 The purpose of this alteration is to reduce the cabin pressure rate changes that cocoa dicing rapid power reductions at high altitude. This alteration provides lever an electrical circuit to reset bleed air pressure regulatio 18 PSIG to 30 PSIG when the power levers are n from retarded below pedestal quadrant angle In • retarded descent. without ANTI-ICE oft manifold pressure power lever is maintained above 20 FS1G. This circuit is routed 2500 FT AGL horn mute relay, disabling the circuit through the when this relay is activated Selection of any AN1T-IC function also disables this circuit. E ASC 313 INSTALLATION AND DEVIATIONS: Installed • new Death P/N 65009-001.513 relay socket into a vacant position near 32.3AIXKS8 and identified the socket as ASC313 tad 50: I instead of the relay, socket end thicket hued m ASC Performed all of the wiring changes shown on Figures 3 and 6 313. of ASC 31Ts ismachons. wept for the following deviation Wires D0002820 and 09002A20 were insetted into s: 326AI P200 and 326A11200 (respectively) positions instead Warm D9004A20 and D9004B20 were inserted of maga; into 326AIP2OP and 326A11200 (respectively) position It instead Vises D9004820.139004C20. and H428C20 was inserted of small/ into 326AIT/16 M positions K. L, & AI Despettively)-, Wire D9007A22N was emoted into ground block El position /AMOS of El 1 positio' n lit After completing weirs and installed a new leach P/N .1-W4N005 relay (aka. rigout, OAR833NRI) Ito socket ASC313XK1. AD of the installed pars parbased from GAC Prod= Support Swainish. GA. were SurionsfullY Performed the instatheion checkout hated mEaragnph Service Basin Numbs 3399022-36-1646 has ban previousl E pee 3 of ASC 313's instructiess. Note-Athed Signal • y comPled wild Valves 541.1 and Sala we accessible removing UPPER pylon panel 2 on the impactive side. by Recorded compliance with this FAA form 337 in the Scat's roShmance records and returned the aircraft to flight status. It has been determined that the intentiarionslths between this change rd any pthiously approved /misdate any adverse effect upon the airworthiness of configuration , fla not the aircraft This determination indudes, but is not limited modifications or deviations made did not aka the intimt of the to: My fime5orts the operation a automatic No flight manual approved aircraft service Mange, What performing Its intended supplement! are required; and the instillation is previous durations assuring continuous cont.:achy with compotthle with al • the applicabk airworthiness requarements. The effect of this change en the airmars dectried le:dinge d] be 1.7 crops added to the etseraid de bid SPEED BRAKEFLAP ALARM and 0225 to CB 262 (0.1t7•5 apgsb CB 242 SINGLE PACK). " The effect of this change on the aimata basic Weigth and botanic was regfigilde and no changes were made basic wthda and balance repth. to aiseraft's nit •sthow wens twos w4nNel .. woometiiiitareniAsAgraiatcr'laar 0 Addi6ortal Meets 4r6 Matited 1 • SDNY_GM_02754176 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00741098 EFTA01326691 MIMMIUME CAA A J. *WRAF I ELGISIR ' • • _ SSW Cif -LI__ • - - I......... 010 Wm IFeC 410 MAJOR REPAIR AND ALTERATION Yet IAA CM OM .17nme•••• (Alston., Prewarplant, Propeller, at Appliance) con anasnaaos n....... =IONS: .5-k -elio Mat at type as autos. St• FAA 43.9. FAA 43 APMMix F. and AC 43.9.1 lot subsequitot inunations and disposition of tint fn. This report's swim! by Lt.(49 U. C. nation thentoh for 14214 Nan penalty me 10 o(4• 4 SI.000 N4 atell such Sanaa Manion SO I NOM' Avi9 Ion Act of 195t. to report tan rank initial. Mac Model I. Mud • GalWean Aerospace GEV Saul No. ?humbly and Registration Nick IOU NRSGA ;we on nentenatai cenifcia) Address (Ai shorn on nista= catalog') 2. Ouns MIANCIAL SERVICES CORP CI 4444 ONE MELLON RANK CENTER PITTSBURGH, PA Ina 1 VAR rm Use 0.1, i Ts US . Nib Met ( Sod No Ramat Alan -...• Airtnans ii hem I 'bow) ••••••••••••••"*" I Amanita • • Propsila • Aglow / - Paseasst ik• clear hA. mows to el Mira 1 a Kad of Any C. Lea A. MA11111074 I U.S Catiticated Metric • BMA E. RAN MAT Darn Foreign Cated Modal* 3COTTSDALE. AZ MSS Cataloged Raw Stet MCGLaktita D. I amity Os ma ncnr Sas alma en ion. tint(s) tataitt iiile 4 eon mod dtecolect asactinata bona bap on ends a .ccida• Ina the rapzirentan of Pot 43 of as Us Feint Nat dr adeassecc Monad bac A Cup isl carat to ths falconry teowk4Alt Drs sis ottaiis . . e- 1 7- f y r7 2 4"1C.S. 7. Afarenitse Rani liana Mfluml IF 41* 4411A4sY lima A MASS Sow. tap ana itathid ia Ilmi 4 Me arapiard a is !me Aiwa pandasa ages of tht Fadden Avalon Asa•tatfon ad in IS APPROVED 0 REJECTED . " IA A. goon c bon ltscan z talon Acarsige . sir . BY I FAA Dagen taps Oro- PO= Ascend by halm dadamworttrnan Oro. Du of Approni a Rejection O..§...- sone of Alameda osem...N. I . - ? ta -sr OWNS M -:- • 41;iC: II 01 edictal Donnelly Sigiczaldifida;a ss SDNY_GPA_02754 177 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241099 EFTA01326692 -,›-."- 1• • 1~ ""4- .iii;!~~1h‘4 - ir> NOTICE Weght and balance or opetalang I/sic:ion chars& shell be as in the approrrale sacral mooed M alteration must be 0'i:imperilla wØ al previous iheriaoniiii aware ~cod conformity mA the applicable erwarchiness requirements. . IL Deeertentia at week AconaplIdad (If mon spice ie required. such Slams Mesta Idera4 tab meal ~ay tad ~es mat wad ear wort complated3 In ceder to provide conanurty during Mure Inspections. manteranoe. and Wistaria:a FM Form 337 is requited to In kept on board a true copy of this the aircraft as king as the alteration remain in effect. AUGUST 26, I Amapa Corporation (CAC) Model G-IV. Aircraft Type Serial Number 1085. N88GA, FAA Sheet Al 2EA. Aircraft ia-testcc der. - 1786.6 bows & 736 landings. Refer to the f Approved Da FAA Fin 8110-3 DATE 7-18-94, MAICE MODEL GIV, Gudaream. NAME OF APPLICANT Glace= Aerospa DATA IDE ce Corporal" LIST OF N 11595B41296 (Er#coring Order Al), TITLE BRAKE ENHANCEMENTS, DER- R. 1 761, SYSTEMS & EQUIP; and GAC Aireraft Service Change 296, part II Drawing 11391130036 EO Spoiler Restrica and PalIII Drawing 1159SH 40560 Brake Beppu The purpose of this alteration t ss ve 'brake-by-wire' operation by inctalli ng i • restrictors in series with the actuator input pressure ports to alkriate hydraulic demand and mod e pedal bungec's to obtain increased tension. Removed fox each P/N 14521916164 union the prom= and ~led four tech P/N 1111X0515900BA Pernieto r anew with new the inetructims oanlainal on GAC Draw" 1159H30 036 Rorocked 4 each GAC PJN 1159C40040-x Bake PØ Bunsee's to P/N in:new-tiros contal on GAC Gnaws- 11395134 0503 GIV BRAKE P ADJUSTMENT Shea 1,2, d 3 of 3 installed the large Pedal Sungois POQITION PM Noes Left 11395B405c0-1 Plot's RIP! 1159584)540-2 Co-plot's Led 115958405681 Co-pkit's Pistil 115958405682 Soccaufully performed GAC <CUP 226001> Gromid Spot System Operaliaral-TaL <CUP 3241 ~ton Tat w CUP 324103> Araararl Syslan-Fonetion Test A Ground Ttn operator* ten toes conducted by two mar* need pion. The pion tested normal tam speeds from pilot and copilot par rap:sued vitae apaazo wars 6W, ground galas, and nom wheel mama No Randal omsprnrice with am FAA km 337 oM acerbailiess ~is allleallhe Smart to tit& tar: The effect of eta Sir ante cafes be ale ett ben sup ~sit and es Saw we :irk b the as at, taus weight and laince report main emsear mews as orned by MSS De* rap 911 182 ArlaaeaL fl An ardzsan • O Adderana Shaft An Attached SDNY GM_027541 78 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241100 EFTA01326693 r........d PO. 1.zsara 0 MAJOR REPAIR AND ALTERATION for 'AA UM 0ST of trmiore (Alsfrome, Power',lant, Propeller, or Appliance) once stem. odes sort= ••••••• - • • .OC -Tc9o. INSTRUCTIONS Rant Of (We ap his ries. Sae FAR 43.9, FM 43 rsIMehdit I, and AC 43.9.1 for subsequent revision instructions and dhposirion of t thereof) for tons. This repott Is rrpoinKI in law 09 U.S.C. 14213 Fare t report can nook in a ONINNY nor to xreed 51,04:* for sigh sigh violation (Section al lederld knal_Kin MI Or 195 M. civil Stake Mudd I. Airettit • Gulfstresin Aerospace G -IV &coal No Netionthrysnd Repstntion Dar 1085 NM IGA V( ern on mama astfaa Address (As am on tearoom merwast 2. Owner FINANCIAL SERVICES CORPID 4444 ONE MELLON BANE CENTER ' PITIIISURGM PA 15153 • ..,.... 3. re FAA Us Or ..... --e—r tin. Unr bake E. ' z Model i Sala No. Roar ARM 3.z. Aillinne r in Ilan I MOM) .""nnann....4) X Power*/ Pads TYP4 Appian. leadmin • -.. - . 46 Carlear ii A. Adencys ram ad Addams ' B. lad of Apia C W. e• LANCE A. RIATTEXPI X C 5. Calthairod - ass L SAN nun DRIVE Foam Cat&ad Manic . sco th at's.. AZ suss Cantina Rani St . Monufocturcr - D. I cettifytho the repel Sot nemoott may to 1b ads) identad Sao 4 toe. .4 a: Ma andsnato tonso lim Oa easy is exordia ea a mamas of Put 41010o U.S. Total Aviata the leforrace fined ems a vois a coma to IS aro amass. . ig- 7T PV -........ - , • Pm - t the to tat =dairy pat pima spaled tolom the Ens to ocaerete tarifa bar 4 am lacral Idea m presinal by Oa Ariziammos ads Federal Mince Abollstrean rod I le APPROVED CI REJECTED • ... rna no nem . I gessax r z moon Ammo I DanOran BY bent . FAA D*We , Ferep in .• Peen Aparmay Tampa Can oinnerdos thump 1 DSc of Amaral or ROMS . • Dolblia' Spaof . copsol• .--- . 8 - it -1 ef . • 130". to -laicbod Dandy 4 4.1MV:4-. - " COS4Ir SDNY GM 02754179. SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 00241101 EFTA01326694 S. Discerns el Week AoremplIsbal Of more smog is rent& cab elation& ass. Mandy anni vane neanaley and memo .ant sad ids work complseed.) In order to provide continuity during future inspec ans, maintenance, and Mashers a true copy of FAA Form 337 is isduesd to be kept an board thri. the ant at long es the effetattan remain rn effect. AUGUST 26, 1994. dulfstraan Aerospace Corpora tion (GACI Mole 0-IV. Sant Number 1085, NIOIGA Aircraft Type Catifi , FAA Al2EA. Aircraft iirt,irdas - 1786.6 hours 736 ender Refer to the Ze.t b L/ GAC Aircraft Service One {ASO S. SUBJECT': ICE AND RAIN 1/49EltATURE LOW MESSACiE - PAW/MONS. dead Dextriba 17, 1993. Thu pnapose of this n to activate the "WING TEMP LOW" message (Amber) on the &tax (EICAS) and await ahartinse W4 ha net Fahrcmhrit of er two ".:,: from bean selected reached 100 degree' ON. Main Junction and Relay Punt Wires I/415222 2 and 1H1525C2 was and spliced together. Wires 2/4151202 and 2/115292 2 wee removed from together Wee 49076W vas salsa trifle IH152Y2 2 near Data Accpsisibm 1, 95MPIB pm 17. Rive 1{907- E 22 wr spaced to win 211I321'22 rear Data acepaintion Unit al, 95A5PIEI pia 17. VT together yeah win 1HIIDDI2 rear connseur Z9A!PIC pa 29. The MN 2H127021 near armada 29A1P1C pa 91. All of the devatiorn tint were mode to the approve d design were prinide for append configundiens hint been dreamt:bad tic rotting the dentin neck did not alts the approved strain service dew of the All parts were prodded in kit form ad obtained from Galina Aerospace Predict Support. Staessfolly performed ASC 232's operatieral test • Reorded compliance with thin FAA Co® 337 m the Irate essantermai meads aid maned Altus to night The etTect of this chaise on the wen& a basic weir sod beamed we saaphigaiie sod no dames were made surcrafra name weight and balm report to the .• sew. gene eine pnind kbanalDeal, WOW it Sam12iMI ACIDECENALSts a MLLE* Vla, • . - ..••••••=0,C-- - - • - .42 : - cre,triLl - . - igui.ake'S MbNyfiM_02764180 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241102 EFTA01326695 • .Nragitr Agt5,O3c-stki-: •PJAU• giCa • • .•I rrnAr ican ft.. - O MAJOR REPAIR AND ALTERATION tart* Ms Ody strnmoorma (Aldine. Powerplant. Propeller, or Applian caw ension karat ce) SIIIISSIL INSTRUCTIONS: Print or type all entries. See FM 43 43. fah 43 Appendix " <SC-IC:SO a irstructiom and disposition of this form. Thin report B. and AC 43.94 lot subsequent revision thereon for is required be a (49 U S C. 1421) Failure renal' not to ... tfted $1,000 for each such violation (Section 901 reclitral Arial lon Act o119$8), to report can result inst.& Make . . I. Arad Mood Sol No. Gullatreasa Aerospace - . &Iv • Nerionelity mid Registration Meek • i f I i.: . -- NIIIIGA N •• . ; 2%9. (WPM awakes) ?....,.. Address (Astor' on regltrIDOTI rands.) 2. Owner ME r • N . - ANCIAL SERVICES CORP Ni 4444 ONE MELLON BANK CENTER - PITTSBURGH, PA 13251 IA Li!, 3. Fee IAA Use OWE •.• . id. . 4. 4 Mee . '3. Eno Make I . I - MOMNo. • Riper Monies . Airbag • ..................•... • kem I above) ""•• •••44'.•••5••• • I ' Parepleat 4? -'' Panels • rAlle Afars - e Wein. ne soil , • A. Cava A lean Ned Adana , . B. KIM essay - C. Cedar LANCE A. nunnot4 . L U.S. CerOficated Meekest - IMO E. SAN FILM DRIVE Foreits Catibrated Mecheltie iCOTTSOA&S, AZ CUSS AP .... Caticated Repast &Mx° D.' I ready OM the rep* gator Swami sea to Os •• ' moo) itateed is lea 4 Move al dessolool as Ike • Lain hew bee =do is ecconlosse wee Oa loam of Pen 43 of dr U.3. Feast Avalon Repletion fniskett haat Simi ad eat MS toe ofem keesderce i i~ • Owe 8-27 Tr' • - 7. Antwel lar Rents MUM Pecom la Ms MilmaY Pva PKocia vides Wow. die me ideemilotbea rt e= Admeriersor of do Peeing Minion Adiseserneas ode 4 sweat S a pemobel by the IC APPIIOVED CI REJECTED .. FAA Pril lo Meoutectusu BY lawn x tropecocei Aatkorabos COM (MediY) .•: FAA Cram e. Repot Meioa Puma Approved by Ira,* . a . Clesdeknortkixo. arose- .• f. Due olApprorel Or Rqsdion ' is--- .• . BiOriYe of. , claienencle , .0-/P: ety ,: UMW li .. a Milton Domani), e ••••••C A 401 aunt _ /14 ,1V12/4 r a ./ i SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241103 EFTA01326696 ran.OncirlIV•Cilttlil"Mr Or S. Eleserlptha of Aoosatellead Of more spa is walks& wrack alatione then karata Mm acre carnally wet regent= ®t ins dee wort completed.) In order to provide continuity dung future inspections mainteranCe. and atterabons a true copy of MIA FAA Form 337 m requited to be kept on board the aircraft as long as the alteration remain 07 effect. AUGUST 26, 1994. Gulfs-bozo Aerospace Corporation (GAC) Mryfrl G.W. Serial Number 1085. N88GA. FAA Aircraft Type Sheet A12EA Allyn* in-urn= deta - 1786.6 holm 4 736 Landings • GAC Aetna Sense Chace IAJC1 255. SUBJECT. INSIROMENTSCATASI). SNAPSHOT TION, dead May 5, 1924 The putpae of a to provide the an wattles/rich that meta engine parameters in both Fait Wunmg C) tita What memory • swath ASC2.55DSI on overhead penal in the spot Watt position 1 nvitch socket wince se fakers: bid want FD9030AZ/N to groutal small U; an,2 wee Jumper 72 totall bp..! wire P090)0822 to bred SII521041022 toDv Pn Dpia wire FD9029A22 to CODDSCIDI 31/A1111 On ail W. Avkaske Shelf Asa/sales: Connected • 31/A1P7.11 Who Dim and Tee Box - VA1F2C pit 11; pa small V win FD90298 to F9/C a 1 -95A1FIA pm 81 tad riVC 12 - 95A2F1A pin SI, rospece Dim sod Tat Scot - 29A1P2C pit 64. AD added wee oomeetara to th and Toe Box were trade deo* to the rack con:to(s) instead ofthn All of the &viatica, die was made to the spermod Jess was approved ocinftgurations aid allow both pilots soca, to the deviations mode did is alter the intent or %cram of the The effect of this chapati& brash'. decd load imelya,ml be cesais. Poser it the 01- switch macaw! b from the O'HEAD LTS MR 12 an totter. - SNAPSHOT* Slaw Sop ONUS doe (when snaphot math a pressed or dorms amnia haws tea) a kas than 0.1 amps in hoe/ wid 9.05 amp 4 dia. The e ffeet of this Mange on the turaaft's basic triadrat Saes wee timalaiat Sat orb Ohara were made to the ureraft's belie weight and balance report. Tao Ammar swired Da 'mond Y. ISSN Dear. VOIDGAD -- -araftavarvit. - " SDNY_GM_02754182 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241 164 EFTA01326697 -"finfar. 4"0 /147,MLFTM :440;; .• t pilsesal MO ii• 'MO 0 • MAJOR REPAIR AND ALTERATION """Oi°" album...N. (Metros, Poweeplawf, Propeller, et Appilmmt) oats iiaf taa . I ol l Sulam Ps C. cit) -' IMSTaut.lama Print or type a atria. Sera FAA 43.9. ma 43 imtnakon nbc and disposition of tiro fora. This report b hofaCilY I. and C. 0 .04 (Co 7 revision thereof) for Cro a (49 US C. 1421). Foam to mart can result Mocha Mar to flied $ 1 000 for each such Vaal (Socha a I Fedora Avalon Act of Phi A. Mahe Modd I. Aland • Cantinas AerospaCe C-IV Seril No lalicaity tad Regiongan Mach IOW MEGA Name (A• than on raposica calicia) Address (As Sm on ropengeo cseakos) 2. Ow= FINANCIAL SERVICES CORPID 4444 ONZ MELLON BANK ONTER ' PITTSBURGH. PA IS= K Fe FAA Moamar 3. T • Use MIS MOOd i TO No. Ems Aberaton Aflame ii lam I above) • X Powniot Nopio TIPP Appleton ear & Calliallif A hag, as al Adam B. Cad of Aorta C Oaks Na. LANCE A. MATTLIOPI I U.S. Colligated ISM L SAN MAIMDRIVE Fonda Catificaled ' SCOTTSDALE. AZ na Certificated Rept Swim Mamba= D. I catty Oa the ea* aka dna ads to ra sa(4) trassad in tan4 tow a chicasd tea ay Ear aide is oxonlatat ask a taantats of PEI 43 of the U.S. Falai Arta atachtsas toad area a free ad coma to a toot ofley ardatap a Cam Dia Seam of g/i 574V - r 7. Manna he Rao an Serb Palacio a sakarysia pa= sada bast ink madled nes 4 es saidaiia r as pada by is AtIsmanta arch' Fad At Adamant:a ad a NI APPROVED 0 REJECTED arta aria Maatiams i havato• Athcastaa Car (acity) BY ~ oar FAA lawn Emir San Pm Amara by Tim - A•liall= Croup Dub MN:rani or Rooftop (Noises Sessen of Aabooad toosumato <9 —/s---tre SWOON IA .ti LadDcrttny SDNY_GM_027S4183 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241105 EFTA01326698 • ••••••laellWat 0-AL--tzww f L Osseripliso tifWarkAcomplishwl (r moo specs is ropiest. WI adorned raw teisaelip sin secret swot wit rssinormo mR wet de week completed) In ader to provide contmudy during Uwe inspections, maintenance. and alterations a bus copy a this FM Fare 337 is' raptured tote kept on bored the acre as en; as the alteration remain m effect. AUGUST 14, 1994. Gukstrean Aerospace Corporation (GACI Model G-N, Serial Number 1085, NSSGA, FAA Ain:raft Type Grams. Dm Sheet AMA. Attest in-ten-ice dots 1716.6 Ian 736 Labs", & Rr1aW the f• Approved Data: Gulfs:ram Aerospace Corporation Aircraft Service Change (MC) ECT: AIR CONDITIONING (4 TA 21) CABIN PRESSURE MANUAL 27ON dated JULY 22, 1994. <CKI3 CODE 972930> is to agow the cabin a prams control 10 mat to manual operation in the the Pronorialace sYllao s lot Pow*, d l l s VAC power is lost, the prance trordocu'' the outflow 1. fast Gre -295's modification irstractesas aiodified the existing 325AI Relay & Skins relay 3.25AIK10, Datoch P/N E4161383; Waded .1 relay socket 325A 'XXI°, Dana& P/N 65009-004513, nil position 325AI X1(10 a connected miens wires es folows ON - ft2, HS0BA20 83; GPOSSA20 - XI; tG52A2ON - JCL A3C 795 DEVIATIONS: binged& new tort 500O421.513 Sty socket .4—S to tad position 325A DO(IO (see Wee) and identical as ASC295)3C I instead , socket sod chops shown on Papa 4 of ASC 295's outruceons, orator wets DI01 306AI P200 Grid 326A11200 (vispectrody) pontoon P 'mead of ma/ Leecii P/N )A-W4P-005 fake GASSUSV I) Sao wicket ASC295XILL Proctoo Support Saverrsh. Safully performed the installation cluck= lined in It has been determined that the intentimonship between this Mere and my previa.* approved introduce my adverse effect upon the sinvotainess of Ur sacral Thu dconeznation includes, tea modifications or damsons made did not aka tee ouent of a e approved acrid Sat comae, finis the operation n cal-WC; No .y..anal Illadat. y an Ian. al a instslistion mynas thereon wwiame comnisous conframsy with the applicable lindens requittrena The effect of this change on the turcists electrical leading sill be 0.03 ads .dried to the circuit breaker. mental 115 VAC bus, - SDNY GM_02754184 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241106 EFTA01326699 CAPTLl AVE CIE* t I I ti t'ArWli ISseeecimi Per >Maw - 0 MAJOR REPAIR AND ALTERATION fa /AA CS 0.7 dit...p.om, QUrfreeee, Poweeplant, Propeller, or si... sea Appliance) Ma Swedes eassem rPISTRUCT1ONS: Print a type all *Win See FAR • 3.9. Oc - r'5 N: 1miructions and disposition or this tom. Tile FM 43 Appendix 8. and AC 43.91 (or subsequent revision report a required by La (49 U.S C. 1421). Failure Immo for penally nor to ineetlyi)00 for each wan violation (Section 901 federal Aviation Art of 19$03 to tenon can Mule In a dull Mat! . I. Ararat Model GUItlatItOl Aerostat G-IV Said No. Neicasfaty ad Repose= Me& INS NESGA • Name (As eon on reqiernlion ainifiese) 2 On, Address (Moot oe spite CM/OW FINANCIAL SERVICES CORP 83 4444 ONE MELLON BANK CEYTtE ' PITTSBURGH, PA ln,5$ 3. Per FAA Da OAF ...... L 1441180:alleei lat IM .1,4. Model Sin. I Sal No Ian Alan Aida inIC I non •4• 4••••••••••••••• X Pollan Ropier Awing tr A. las th Ceedweein Hafaa ad Ada B. InSof Ma LANCE A. MATIII3ON C Cant No. X U.S. Cancan M la L. SAN PXLI72 DRIVE Fora Carnicated oda SCDITSDALL AZ I52 Coat:aged Recta Stilton D. I catty Os LS Mai laSS Ca Meaufectura =an COISant a is 4 non ad Cad Into a Co ton ta nora wit In sac intonate ofPut 43 of the U.S. Feta Annia rand balsa ad correa to tbr On of dry dr ietosaina Inntolda. De sr?" 7. Anent Ihir Roan 14 Sinn ,n r Panto S. aciry wee roan speccese Wort dat at an and ma 4 we spa Athreirrair of the Foal Avan Ack•irrairs al as clad by dit sad if TH APPROVED 0 REJECTED PA* Ft Vine ales Ineadlacera x Cocoon tontonan BY C84 (39 442) FAADonate Rata Ca Pa Apron by Tact Coda AnOrda Group IC of Awron or Ration Catama a' f - - eW s Dia eln-A7 SWAM% IA ad.." Mai Dan! SDNY_GM_02754 185 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241107 EFTA01326700 cmam knout? itionike - 7st NOTICE • Weight and balance or operating Enutation change shall be eared • in to appropriate aircraft mead An ateranon must be compete with all previous alterations to assure continued confons ity with the triable Sworthiness reqtarments. & Dratelpelir fl ak Asearlabed at mole Nee a Molted and elationst tees Ids* wan at Mosley ad mite= eark ed des wart scallt&) In order to provide continuity dunng future inspect ions. marrtenenoe, and alterations a true copy of FAA Form 337 is' required to be kept on board the Ss amnia as by as the alteration remain in t. AUGUST 14, 1594. Chaste= Aerospace Corporation (CAC) Model G-1V, Serial Number 1085, N8SGA Aims& Type Certificate Dsta Sheet Al2EA. Auctift , FAA meertia Si - 3736.6 hors & 736 landuigs. Rder to the f Approved Data: Whitman Aaospace Corpora tion Aircraft Service Change (ASC) 313 S NEUM,477CS (ATA 36) CABIN PRESSU RIZ427ONSTABIILZa71ON dated DECEMBER 1 <-CMP CODE 973130> The ptirpose of on is to reduce the cabin prelate rite changes thud occur during maid power lever reductions at high This situation provides/selected came to reset 18 PSIG to 30 PSI bleed air pressure regulation from the power leen at retard below pedestal guide= descent, without angle. Ina retarded power Ice ont manifold is saintsical above 20 PSIG. This cured is tuned 2.500 FT Ala ban mute relay, through the nen this relay is sciarded. Selection of any Awn-ICE function also disables this camas. ASC 313 PLSTALLATICAN AND • new Deulach PIN 65009-001-513 relay socket ins a scant portion near 315AIRKSB and idattified veil 13XK1 indeed of the relay, scar and basket listed in Performed all of the wiring changes shown ASC 313. 6 ofASC 313's insertions, except fir the following devirien Wan D9002B20 and D9002A30 iltre - a P200 sod 326A11203 (rospectivdy) potion S Used ofd: Wee D9004A20 ad D9004820 were I F200 and 326A (reepectiwely) position R hued ofnag Woes D9004820, D9061C20. ad H4D3C20 we anted into 326A1T/1 R. L. & ht (respectivdy); Ws D9007A22N was Seated Son Wound 1110& E2 Parton M insad a new Leh P/N 1-W4N-005 relay (aka GAR835Sued of El a Ala completer war and erg a NRI) into 13XK1. Al of the staled pats wee µnehued from GAC Pet Dawn Savannah, GA Suocessfuly performed the szatim checkout toted Pesegar etlt in kEp ASC 311's weruchons Note- Athed Signal Service Bolen Number 3395012-36-1646 hie been ;mks* complied Veins 54/1 and 5412 ire accesuble by remota UPPER pylon pod I on be reapers stele Recorded complasoce at. this FAA loan 137 n the masts so elmave rant end tamed the status. It has been daermerad that the ersernelstionstup beta= this damps and say previolaty appeared introduce any 'draw act upon the *wartime* dee Sat 7Ls debaxeration artudes, but incekfrations or ember reide did not aka the thank athe Any approval swath service change, its intended fimetems the opcestion es automata; No Oar m.mdagWbmn o are nescirot, and the instance at an prrnous allenziors estanng tie ceakanity Mt tie sppwatietimatticest rearm s. -. • The act °Ishii chore on the saszar's SAMS bar lotd..will be 1.75sssd as the sate S imps to CB 2C SPEED BRAKETLAP ALA1Ud ad 0275 kiCB 20 44.014Pa . . The as of els charge on the raarabatMasi ✓tetalSSekgR selidre are was ode to the .Stmt's bre wage and Slam apart . Ths • •aria 'sealin needale INSI9TiS TARDY% ,.a. .imismiscrion. -• ocAddikvo.k. kens As!. raintsgtiatoaarief irarstirrz --zi _nj* • 2:40vjz;,: .c.,.2 • Geo:4_027541R SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241 I 08 EFTA01326701 lntar ' eV' FAA AIRCRAFT REGISTRY nien,,, CAMERA NO. / DATE: 5' - /7 ".......... - own. Ila4a MAJOR REPAIR AND ALTEEATION - . ....AA visor, • O Cracow= (Airframe, Powerplant, Propeller, or trace) OM. Mereneeriaa - - .......... re..... .. ra4,,, 0L - 63° INSIRuODONS: Prat or type el flies. See FM .3.9. FM 43 Appease 8. sed AC 43 9-I (aassns! MannMt banlanns ad trnensmen a this lam 1S read is rebind by lav (MI U.S.C. t421! Fates to typal as real Ins di pasty not to eragied SLOW breath Bah seam (Seem. 901 Federal Melton Ns of MM. • Mike Modd I. Aircraft Collette= Aertasptce - C-IV Serial No. Nalionsbly and Reese:Woo Mark 1085 NMIGA Name (As show a reparation an -am) Adam (As sawn on remake certacas) 2. Ovals ACFIUM LEASING CORP FOUR EMBARCADERO CTR SAN FRANCISCO, CA 94111 3. For FAA Fry Only 4. Volt Ithogaleadoe 5. Type Ural Ma I Modd I &dal No. Repair Mat= Airframe • 4•••••••••••••••• (As dosed:4d in 11 I above) see...... X Powaplant Propeller - 1 '. Appiamca Alsobtrans • A Cakemilly Stien=8/1 • 'A Stilt and Address B. Kind of Away C Cantata No. LANCE A MATEESON • X U.S. Caticated Me trans .,-• . 9560 E. SAN FELIPE DRIVE F044881Cartthesleil Medmmic AP.1164049 SCOMDALE, AZ MSS CatSated Emma Station liamaimturer D. Inesty Math/mak wellor Mormon waft so the eat(s) identified mama above and 6nenladm the rasa a ancesawn kneto an lam mens in acerdiace Caul nquiteemas orPat 43 ofMa at Fare ' Itagalskaw aid tha the informs:on forawhorl baron is mu ad coma lo the beet o my lambda& Date . .1-ff-ty .&gitatal ri f f - 7. Anneal for Rearm *Arles Persosot to the antharty given peon specified below. Me onit idatiEsdin be 4 vs Spa mare Ana pass wad by the Mitnineracer of the Federal Ariake talon and is XI APPROVED C EMCEED FAA Ft ausbrei Mandato= ' x laspecOmMahceimicas sons (Spicily) BY twat . FAA Dadposa Rep* Station Pam Approve! by Tr dada Afrwarthinea Oroap Den Approval or Ftewtoon eat Dmielam am --- - WO. V 3267950% IA MbNYCM 027541g7 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFI'A_00241109 EFTA01326702 "ra- t eflitigf rY FAA AIRCRAFT REGISTRY a y 4 CAMERA NO. / DATE: NOTICE WM& and bolus a °Paging limilabon dears ant be :raced in the sisnipsu liralf LIMOS. An austionroust be compeale with a0 previous altastiont to assure continued conformity with the applicable airwortbineas remoraocnts. & Desoiptke of Work Aromapllabed (rm= apace b oppoired. cad: eddtionet aka Ida* with &adrsiterty act ranmaion mart ad de wort _.plead.) March 18, 1994. Gotham-am Aerospace Corporation {GAC} Model G-IV, Saul Number 1085, NUGA, FAA Aircraft Type Catificate Data Sherd AMA.. Aircraft ea-service data = 1629.9 hours & 669 landinp. Refer to the following FAA Approved Data: Oulfstream Aerospace Corporation Aircraft Service Change {ASC} 298 SUBJECT: PNEUMATICS (ATA 36) BLEED AIR ISOLATION VALVE RELAY- POWER SOURCE MODIFICATION dated February 16, 1994. <CMP CODE 972980> • The purpose of this alters\ on is to separate the power source fete bleed air isolation valve control relay from the bleed air isolation valve relay. Presently, both relays are powered from the same 28 VDC circuit breaker. This ASC installs an 'AC' control relay for the valve control relay which will eliminate the possibility of a single fault causing a false cockpit indication. Performed all of ASC-298's modification instructions effective for aircraft Say: 1085. Installed parts are listed in ASC 225 page 8 and were furnished in kit form by GAC product support Savannah, GA- Successfully performed GAC CMP code 361064 Bleed Air Isolation Shut Off Valve operational tests. Using the FAA Approved G-IV Aircraft Flight Manual operated the Auxiliary Power Unit and started both main engines and verified that the APU AIR. LOAD, ENGINE START or CRANK, and the ISOLATION. VALVE cockpit switches performed their intended &actions. Recorded compliance with this FAA form 337 in the aircraft's maintenance records and returned the aircraft to flight status. The effect of this change on the aircraft's electrical loading is negligible and no changes were made to the aircraft's electrical load analySis report The effect of this change on the aircraft's basic weight and balance was negligible and no changes were made to the aircraft's basic weight and balance report as a caupgar anered Amnand W wadedDNS* WOW It - mliS%roll AM. NO AOCIELMAL =EU ARS ATIACHIZI *DM' O Atationd Sheet Are Attached SDNY_GM_02754188 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241110 EFTA01326703 ITMlEartj .,. `‘N FAA AIRCRAFT REGISTRY CAMERA NO. /A/ DATE : 7. 7y spas PO to alga ® 011 Nall MAJOR REPAIR AND ALTERATION larAA On CI* (Airframe, Powerplant, Propeller, or Appliance) MNIdadfuriee esommomi rainJae rain tat - SOL "Frf 04 7 nismucTIONS: Pont or type all entries. See FM 43.9. FAR 43 Appendix II and AC 43.9-1 (or subsequent revision Menial for instructions and diiposition of this form. This report is required by law (49 US C. 1421). Failure t report on result In a civil _penalty not to exceed 51.000 for each such violation (Season 901 Federal Aviation Act of 19SM. Maki Model I. Mace{ -/ Gurnee-earn Aerospace t G-IV . Said No. Natiornfity and Registration Mark __ _ 1085 N88GA Name (As shown on registration itertillette) • Adam (As Omni on rewaration cannons) 2. Owner ACEIUNI LEASING CORP FOUR EMBARCADERO CTR SAN FRANCISCO, CA %III 3. For FAA Dee Only 4. Unit liken/Ronan S. Taft unit . Make i Model I Saial No. Repair ( Murton Airframe (As described in Item I above) X Powerplent Propelkr 1Wo .... Appliance Mcderesar 4 6. Carkirozety Steteroad A. Mean Nome and Masai B. Kind of Agony. C. Certaczne No. LANCE A. MATTESON X U.S. Catiksted Mechanic IMO E. SAN FELIPE DRIVE Foreign Catilicated Mechanic AP Ilan SCOTTSDALE, AZ 35253 Catifacated Repair Station Manufacturer D. leanly that the repo mace ammo =de to due mai) Identified in bane above sod described o the reverse armaments hereto have been made in accord= with the To:Orem/nu of Pone) of the U.S FLOM Mama Regithikas aid tha the inkemetion famished bate is ow sad Ceelitt lo the ben ofmy knowledge. . . . Dale signor s2: _.......4 15/ i• 7. Approval for Ran to Pnn to the orthodry given groom spooned below. the toth'clemithed in Om 4 era inspected ia the re= pracrOxd by the Achennirwar of du Federal Mission Attraninion sada CII APPROVED 0 REJECTED FAA FILM..Mt Mamtfacturer x basevaion Azahodation Other (ePedY) BY Sinew FAA Designee - Repair Station Pews Approved by Tampon Cola Mit Group Cote of Approve/ or Rejection Ovens or Signals{ of Mahatma Yydividtrajf onisstise. . - -4 - 1 Ct' -- , y 52670504 IA a<a Pr Michael Donnelly 47-Ca5V4ilinrmt44 44emt :4 "1" Biarrinerre gi lW4 9WY,4.79"'"'"" - ).. SDNY_CM:027541EIS SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFIA_00241111 EFTA01326704 "2"."-": TE'443E-A"r FAA AIRCRAFT REGISTRY • CAMERA NO. A DATE: V: Z 5.4 79 NOTICE Weight and balance or operating limitation changes null be attend in the appropriate aircraft teoxd An alteration must be with the embattle airwoethiness poluiremalb. compatible with all previous alterations to assure continued conftxmity a. DesaiptIon of Work Accomplished atmaayaadrapsomlon mark and drat wort completed) (If mom space is reqvized meat adtmenal abeam Wan* with eiremft (GAC) Model -G1V, Serial Number 1085, N88GA, February 42, 1994 Gulfstrearn Aerospace Corporation in-service data • 1611.7 hours & 6611andings. FAA Aircraft Type Certificate Data Sheet AI2EA. Aircraft I- -- Aircraft Service Change {ASC} 225 Rettig° the following FAA Approved Data: SUBJECT: LIGHTS mu 33) NOSE GEAR TAXI LIGHTS MODIFICATION dated November 1, 1993. CMP CODE 972250> light mounting bmck,etry to The purpose of this alteration is to modify the nose gear taxi taxi light from a spot light to a flood provide optimum visibility. It also changes-the center s an existing circuit also replace light which will eliminate shadows. This service change breaker and taxi light housing assemblies. parts are ation instructions effective for aircraft SiN -1085. Installed Performed all of ASC-225's modific GAC product.support Savannah GA. listed in ASC 225 page 4 and were furnished in kit form by nose landing gear retraction to ensure clearance of Performed Al of die steps listed hi paragraph "C. Perform the GAC P/N 1159EL20064 Wire Bundle Support taxi lights" and noted an interference problem between 2 View A-A and the Nose 1. ceding Gear fruition assembly. Corrected Bracket, refer to Page 6 Figure provide properclearance and noted no other problem by trimming the leading edge of the bracket to abnormal or unusual conditions. ph "D. Perform operational test as follows:" and Successfully; performed all of the steps listed in paragra taxi light operation individually and collectively noted no abnormal or unusual results. In addition, checked and Checke d the operation of the Nose Wheel Stearog System to verify proper circuit breaker configuration; unusual results. with taxi lights ON and OFF and noted no abnormal or s marntenance records and returned the aircraft Recorded compliance with this FAA fora 337 in the aircraft' to night status. loading is -150 VA (watts) added to the Right Main AC The effect of this change on the aircraft's electrical Taxi light operatio n is inhibited if the landing gear is not down and BUS during tan light operation. Note: POSMVE CONTROL for details. rocked; See ASC 131 <CMP cede 971310> TAXI LT balance was negligible and no changes were made The effect of this change on the aircraft's basic weight and to the aircraft's basic weight and balance report. 01/12/94 AM This u “ 0900 gonad In cosmos er blictrel Dawn". wow) re NO ADDITICNAI MEM% AU AlTACHID •@C. O Adcbtanal Shona Are Attached -et, r ----t 4.•- •”:—n-el: t la;visatiarlerlpreltroSta • ?••‘•• aeArremi 10, 15,_0 an SUBJECT TO PROTECTIVE ORDER PARAGRAPH S 7, 8, 9, SDNY_GM d0 17 275419 EFTA_00241112 EFTA01326705 FAA AIRCRAFT REGISTRY CAMERA NO. DATE: 3.3'_ 94 ..••••••• . . 44.. , ars liii imam a MAJOR REPAIR AND ALTERATION PerFAA 136.047 US Down (Airframe, Powerplant, Propeller, or Appliance) MeeIdesidoeics arraspras s IMMO Minn ...A... 5 6t -Fl; e INSTRUCTIONS: Print or type all entries. See FAR 43.9. FAR 43 Appendix B. and AC 43.94 (or subsequent tuition thereof) for Instructions and disposition of this form. This report is readied by LtIV (49 USG 14211. Failure to report an result In a civil penalty not to aceecl S1.000 for each such violation ISection 901 Federal Aviation ACt of 19581. . . Make Modd I. Aircraft . Gulfstrearn Aerospace G-IV Serial No. Nationality end Registration Mark 1095 , N8SGA Name (As shown on resimsion cattate) Address (As 'bon on on cache) 2. Owner BA Leasing & Capital Corp. Two Embareadero Center San Fraoelsco, Ca 94111 3. For FAA Use Only 4. Unit laden/Ranee S. Two Unit Mike I Model I Serial No. Repair Abrasion Ai sine (As desinbed in Ilan F above) X Powerplant • Propeller TYPe. AppiAnce Manufacturer 6. Cordonsity Statemeat 2,6trays Nano end &Mpg. B Kind of Agency I C. Candle= No. - LANCE A. MATTESON X I U.S. Certificated Mechanic SSW E. SAN PXLIPE DPJFE Foten Catificated Mechanic •I AP 1964049 SCoTTSDALEAZ 957.59 I Certificated Repair Stition I . /donut:wrote: • D. I Cc* that the repair ounce akeration made to the ak(e)Mantled in done above mid demntied on the name or smechmada hut° have been made in accordance ..t the requiratoma of Pun 43 of the U.S. Federal Aviation Revelations and that the infcmtation ft:mashed herein is trot and coma to the beat a my knowledge Date e° Signaltne dged hl&i2 `s.3 7, /94- , C .. 5 / 7. ApproerJ for Return to Service Pornau to the anthoray peen persons spoofed below. the tmi Waged la kern 4 was maponed in the =OM poncaled by the Adminssiraa ofihe Federal Aviation Administration and is On APPROVED 0 REJECTED FAA Flt. Seaderds I manuturwer x ineptennn Andwason Ma (Specify) BY learn FAADesignee Repair Sudan Poison Approved by Tampon Coale Atribeti1 Oro Date of Approval of Rejection rostrums re • l . :, . of A ' 'air Dettgataa. No. 5,5-7 4-- 7./9 193 S2670S494 IA Illiire-../ -- - ' ...--P Michmi Doll:WHY -riAliewarliaek4.1169(Gtogniper-aas • SDNY_GM_02754191. SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFI'A_002411l3 EFTA01326706 FAA AIRCRAFT REGISTRY CAMERA NO. 3 tun: 3- 3- 94- NOTICE Weight and balance or operating limitabon changes shall be entered in the appropriate aircraft motel. An attention rough< compatible with z0 previous alterations to assize continued conics:miry with du applicable einenntencas requirements. S. Desorption of Work Accompllsbed (If more space a recpung oh additional theets. Way* with trawl nitionalny and regstrzion mart and data work completed.) September 7, 1993, Gulfstream Aerospace Corporation {GAC} Model G-IV S/N 1085, N88GA, FAA Type Certificate Data Sheet AI2EA, Revision 18. Airmail total time in service 1493.6 hourt and 608 landings. Refer to: FAA Approved GAC Aircraft Service Change (ASC) No. 176 Subject: LANDING GEAR (ATA 32) NOSE WHEEL STEERING FAILURE - ANNUNCIATION dated February 23, 1993. Effective for Aircraft serial numbers 1000-1214. The purpose of this alteration is to add a pressure switch and circuitry to alert the crew of a problem in the nose wheel steering system prior to takeoff and/or landing. The pressure switch and additional circuitry allow additional parameters to be monitored. The amber STEER BY WIRE FAIL message will be displayed on the Engine Instrument Crew Alerting System when one of the following conditions exist: (a) Nose wheel nutcracker switch snack in the ground mode; (b) Nose wheel steering shutoff valve(s) stuck in the open position; (c) Nose wheel steering system inoperative due to loss of power, (d) Improperly installed steer-by-wire ECU or ECU connectors. Using the instructions and parts provided with the GAC ASC 176 Kit, performed all of the instructions applicable for aircraft S/N 1085, except (see Figure 5, Page 13) installed a GAC P/N 1159SB20223-11 BRACKET in place of the GAC P/N 1159F41094-39 BRACKET furnished with the kit This minor deviation allows the Relay Bracket to be removed for maintenance without having to drill attaching rivets. Successfully performed ASC 176 installation checkout (Paragraph H. Pages 6 and 7) and noted no abnormal or unusual conditions. Returned the aircraft to flight status and recorded compliance with this FAA Form 337.in the aircraft's ' maintenance records. F It has been determined that the interrelationship between this change and any previously approved • • configuration will not introduce any adverse effect upon the airworthiness of the aircraft. This determination includes, but is not limited to: There are no changes to the operational limitations; The existing aircraft flight manual provides Migration for dealing with the STEER BY WIRE FAIL EICAS message; and the change is compatible with all previous configurations assuring continuous conformity with the applicable airworthiness requirements. The effect of this change on the aircraft's electrical load analysis and weight and balance data is negligible. This Saco:vow generator form Bled ea ASCIT6DOC: SPS4 Chambers. prepared by Michael Donnelly NO ADDITIONAL SHEETS ARE ATTACHED. *END' O Additional Shxts Are Amen:6 SDNY GeS4_02/5410 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241114 EFTA01326707 FAA AIRCRAFT REGISTRY CAMERA NO. DATE: 3.S me... ,,PET c•c", " ,,a ,s ® 1 ./L2POR REPAIR AND ALTERATION Fa FAA Thie Only hi.i. poem.. (Ak'ri amp, Powmplant, Propeller, or Appliance) swarms ,samosa c 0 L- INSTRUCTIONS: cam or type all entries. See FAR 43.9. FAR 41 Amanda S. and AC 441 (or tutdehoeitt revision thereof) for r 5 .9 - ' • Instructions end disposition of this Form. This report b required by law (49 US C. 1421). 'Mims to report can result in a civd penalty not to exceed $1,000 for each such violation (Sefton 901 Federal Aviation Ad 0(1954 Make Mold I. Mardi ' Golfstream Aerospace G-IV Sala! No. . Nationality and FtsaMennice Mark 1085 Nitl3GA Name (As stows co registration certificate) Addnsta (M shown cm regionalism eatiforate) 2. Owner B A Leasing & Capital Corp. Two Enobarcielero Center San Francais Ca 94111 . 4.. .s ....- isaatJaier SA042151wanly::seta :le oe Ova Riverihman infrewarts id b amrovrO ea a z 'Erma cooterrny irspetho dmerbrd =Fa ailmt to a Nefas ..).0 -43 _.:t -e -91114--v v- OAR 4. Usk Identification 5. Type Ufa . Milks I Model 1 Said No. Repair Altendico ?Whom (As daubed in Item I above) **********••••46499 X 1 Powerplent proi can. t Two AiVisTice t simorasamw . . • 6. Cesiminity Slonement • 21...pparta NO and Address B. IOW of Astaicv C. Catlin No. LANCE A. MATTESON . X U.S. Certifiated Metairie . 65600 E. SAN FELIPE DRIVE Fortino Certificated Methane AP 1664049 SC01173DALE, AZ MO Certificated Repair Station • '. , Mat= .r DAD:eery that the repaa Nadler iiieralice made I o On mit) idedirs1in von 4 above mai casented on the mom er madam_- hems bavc been male ist atientarce with the tespinemet ofPart 43 of tte U.S. Foleral Aviation Regoltioni ad the de informant° fiatiated bran is owed coma do the born dray 171O.thit- 7 Date Signature 0M/thorned je:S......... • tt -ft —cr.) ‘ec 7. Approval for Return to Service Pirate tolb: =hairy given panes sprified bdow, demil identified in item 4 ern laspected is dm 'rarer preeenled by de Athninistrztor oars Fatal Avidice Admin.:rice as OD APPROVE) 0 REJECTED FAAFt 3adertis AID x Insmenos Authorization Odicr(SMOM Impar \ BY FAA Daiiiime - Repair Stance Pastei Appened by Trasport 1 Canada Ainarthiness Gram Date of Approval or Rajemion adtholin Emanate of Audio . DmipsamiRis -il.ilry . 5267054,14 IA Nfichaei Dcrrneth. • . . . • • ..___ -- . SONY CM_62754193 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241115 EFTA01326708 FAA AIRCRAFT REGISTRY . CAMERA NO. 3 DATE: 3_3 -_94 Weight and tehmce or operating hesitation changes Ad beNOTIC E emend in the appropriate aircraft record M thermion mist compatible with N previous Antrim to assure continued conformi be ty with the appraarek airworthiness requirements. Daalpriom of Week Accomplished 123/1 space l? required, meth *Mean stmts. Irks* swath sinzica snorer* ad reguntime mat Nal tie win aopleigri) August 11, 1993, Gulfstream Aerospace Corporation (CAC} Model G-IV, SIN 1085, HUG& FAA Type Certificate Data Sheet Al2F_A This change requires FAA Field Approval The ptapose of this change is to update this aircraft's fuel booretptpitp vent hose system to the current production standard. This modification-will elimina te the need for4W-erdiffenitit'pert number hoses in spare stock and provide for a neater sadiste logical initaffati6C; Modified the LEFT and RIGHT Main ea Afftgl ittflentEntister-fsnapVint System by. Removing and discarding the existing four each vent hoses that connect each fuel booster pump to a wing tank; Removing and discarding the number 6 AN Fitting and Os ring packing Stalled in each of the four booster pump vent ports; Installing a new MS295I 2-06 Ce ring packing on four each new AN8I5-61) Union Finings and installing one fitting ('O' ring packing side toward the booster. pump vent port) into of the four booster pump vent ports; and Installing a each new Gulfstrum Aerospace Pan Number 115H40200- 143 Vent Hose between each new booster pump vent port and the closest existing wing tank port Secured all newly installed ports and hose fittings by torquin g to the current maintenance manual torque value and identified with torque stripe. All parts were new when Stalled and purchased from GAC Product Support Savannah, GA 31402. Performed a leak chock visual inspection of all four fuel booster pumps and attaching hoses while doing FUEL CONTROL SYSTEM FUNCTION TEST in accordance with CMP maintenance code 280005 (card 28-01) and noted no leakage or abnormal operatio n. Returned the aircraft to flight status and recorded compliance with this FAA Form 337 inthWilloriffs - maintenance records. It has been determined that the interrelationship between thischange and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. This determination includes, bin is not limited to: When performing it's intended functions the operation is automatic; There are no changes to the operatio nal limitations; No flight manual end the thosnation is compatible with suPPlements arc required; current production standards and all previou s alterations assuring continuous conformity with the applicable airworthiness requirements. The effect of this change on the aircraft's weight and balance data is negligible. This areptaer mentor torte filed a VeiniOSEdot; 5, 99 CbgeWas. PrcPand by. Kahn Deo* NO ADDITIONAL SHEETS ARE ATTACHED. 'END' Q Addend Shea. Are Anached sbAiTeii:briD41§V SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241 I 16 EFTA01326709 FAA AIRCRAFT REGISTRY CAMERA NO. DATE: 3_ - 94 lai Mem' . A 01014 727)40/ MAJOR REPAIR AND ALTERATION hellall•Coly il) vi dun= Officeidadliesemos a -as.pat (Airframe, Powerplant, Propeller, or Applies's(*) /slal MISR mean. t5-BC -a? INSTRUCI1ONS: Print or type all ewes. See FAR 43.9. FAR 43 Appendix B. and AC 43.94 (or subsequent revision thereof) for Instructions and disposition of this form. nib repon is requited by law 149 USG 14214 Failure to repon can mutt in a civil penalty not to xceed $1.000 for each such violation (Section 901 Federal Aviation An of 19501. . Mahe - Model I. Arad Gtillatream Aerospace . G-1V ' Serial No. Nationality and Registration Madc 1085 N8SGA Name (As shown on mist:raw anificets) Address (As shown on rerasmitoo catifonte) 2. Owner B A Leasing & Capital Corp. Two Embarcadero Cram. .' • San Francisco. Ca 94111 • 3. For FAA Uwe Cady • • 4. Unit Identification . 5. Type Unit Mein I Model i Setae No. Repair Merton .... (As des gibed in Item 1 above) - Airframe ' X • Powell:plant . . PropeRer a T* Appliance Manure:nun A. Ceitereelly Statement A. Agenryel Nana and Address R. Mod of Agway . C. Cara:eta No. • LANCE A. MATTESON X , U.S. Catificated Mt:claret 8560 F- SAN FELIPE DRIVE Foreign Certificated Mechanic AP 1864449 . SCOTTSDALE, AZ 85258 Catificatcd Repair Stance ' , Manufacturer IN I am*dot dm weir nadior Manisa made to the mike) idereffied in item 4 Move aed deathbed on the reverse or aratenems hens here been made In axcedeom with ra :mei:amens of Pat 43 of the U.S. Federal Avalon Ragelations and that the information feeedded herein is tree nreleoraia to damat eiT my ImoMedea Pale „9 ,7 7 :irri • 7. Approval for Retro te Service Pumcmi to tbe milbeety given pions specified below. the and illersined in Mesa was inspected ha We maw prsaMed by the Adrnisescrace Maw Federal Anxion Admousalcion ands IK1 APPROVED 0 REJECTED PMdik Sewiatea Mane/masa i I baPeciwn Arthwawann Other (Speedy) BY Spence FAA Designee' Repair Mama I PetiOn Approved by Tampon I Canada Airwatbinin Group Date of Approval or Rejection Certifiers ar• - Signs of A ideal Owieries No. 526705494 IA Michael DonneRy 547 f 72. SDNY_CM:02754195 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFI'A_00241117 EFTA01326710 FAA AIRCRAFT REGISTRY CAMERA NO. 3 DATE: 3_ 3- 94 • NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alb:radon must be compatibk with all previous alterations to assure continued conformity willa the applicable airworthiness requirentogs. • S. Daseripdon a Work Accomplished (Snore space is reqviroi mach additional sheen. Identify with aircraft natio:lay and reginnuon sit and else work completed) September 7, 1993, Gulfstream Aerospace Corporation (GAC) Model G-IV, SIN 1085, N88GA, FAA Type Certificate Data Sheet Al2EA, Revision 18. Aircraft total time in service 1493.6 hours and 608 landings. Refer to: FAA Approved GAC c-ry Aircraft Service Change {ASC} No. 3 Amendment 2 Subject ICE AND RAIN PROTECTION (ATA 30) WINDSHIELD HEAT - • TEMPERATURE SENSOR TEST SWITCH - INSTALLATION dated February 26, 1993. Effective for Aircraft serial numbers 1000.1155 having ASC 3. . The purpose of this alteration is to modify the wiring to the windskiiikheat to) perature sensor test circuits installed by GAC ASC 3 so that both temperature nsors o each cockpit window can be tested. Using the instructions and parts provided with the GAC ASC 3 Amendment 2 Kit, performed all of the instructions applicable for aircraft SIN 1085. Successfully performed ASC 3 Amendment 2 operation test (Paragraph C. Page 3) and noted no abnormal or unusual conditions. Returned the aircraft to flight status and recorded compliance with this FAA Form 337 in the aircraft's maintenance records. It has been determined that the interrelationship between this change end any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. This determination includes, but is not limited to?There are no changes to the operational limitations; No changes to the aircraft flight man\qal are required; and the change is compatible with all previous configurations assuring continuous conformity with the applicable airworthiness requirements. • The effect of this change on the aircraft's electrical load analysis and weight and balance data is negligible.. This Sacco:pan generator them Ned as AScsAvn rm a n aen. prep .4 by bads Da,„,b,ur NO ADDITIONAL SHEETS ARE ATIISCHED. 'END* CI Addidonal Sheets Are Attached • . • . SDNY_GM_027Sti SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241118 EFTA01326711 .... Pa Asa.. an Ma. 7.17PMX , Toe IAA the Only • MAJOR REPAIR AND ALTUtATION - as= •kmarathe ® us this ' (Airframe, PowerpIat, Pittprlier, mr APPIalla) er.......,.. Polinl Aar ...-- .5-.? c • ,--<sz 2 43.9-I (or subsequent mislon thereof) for INSTRUCTIONS: Print or type all entries. Se* FAR 43.9. fAil 43 Appendix B. ad AC result in a civil Instruction; an on of this form. This report Is required by lea (49 US C 1421). Fealty* to report can penalty not to exceed S 1,0001= tad such ylolathM (Section %I Federal Aviation Add 1958). Mac ' Medd I. Airalf) Golfstream Aerospace G-IV Nationality 0 Registrstioo Mule Stria No. loss N88GA Name (Al dries on regime:ion oaths) Address (As on on repontice catficee) Two Reabanadero Cm1Cr 2. O B A Leasing & Capital Corp. Saa Francisco, CS 94111 3. For FAA Ese Orly 4. Unit Ida -dilation 5. Type' Said No. Repair Al= licit Mat I Model I Airframe (As detertlxd in Item 1 above) X Powaplent Propeller Type Appliance Manidatarer 6. Casformity Statemart - B. Kat of Agoicy C Catificate No. A. µstye Nese al Addis LANCE A. MATITSON X I U S. Cerakaed Mectamic 1560 E. SAN FELIFE DRIVE j Fen* Certificated Medmic AP 1644049 SCOTTSDALE AZ 65256 TCatificated Remit Station I Maaufacturer 6=nbed cede creme a etuchaeces ham his D. lertly diathermia mint elms= nude/oft tee=(.) identified in des 4 above cd fimieled tent S tem made in accerderice 0 the rotaramits of Pm 110(5 y.s. R&M Attie Reptant dim the iefernotis int aid arta to de tea dory towledet Dam Sigmlur loift2a Y---N-F i 7. Approval for Retro to Service I me capeeted in the name preceded by de Athatisocar Passed to the asloity givenpima tprified blow. the me ideaihed in eat REJECTED of dm Fetal Anton Ackrionaba ma is Cgl APPROVED 0 FAA Ft Sumba Mtalfaconer i baps= Axidatatesi Other (Brady) bass BY FAA Designee Repos Stabs Pence Append by Titspert Canada Mn dtea. Cisco Date of Approve/ or Ridection Gots or Signature of Authorized Deilotre No 81/4 2 193 526705494 IA r ?ached Dannelly •.“ r=7;' . V .tr. • • zr . ”5 in hi: 't lt . na • SDNY_GM_02754197 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFI'A_00241119 EFTA01326712 NOTICE An sheralion meat be shall be emend in the awroprime aitcrillrecord. Weight and balsam or operating liaimtioa changes ty with the applicabl e Unworthiness requireameas assure continued conformi compatible with all previous alterations to /I Description of Work Accomplished each antral ruescoltry ad rcgaraa mak ad due work ccepleteM ) Of mere spar is required. math odd:kcal deem. loss* Model G-1V, SIN 1085, MAGA, FM Type August II, 1993, Gulfstream Aerospace Corporation (GAC) time in service 1481.6 hours and 600 landings. Certificate Data Sheet A12EA, Revision 18. Aircraft total •- r SE05201903 REV. A, STAND ARD Refer to: FAA DER Approved GAC Repair Drawing Numbe ICAL BEARI NG, N.LG. , FS 119., BL 0.0 Sheets 1 and 2 of 2, dated 5.5-92, REPAIR - SPHER res DER SO-483. Wilder, FAA Structu Effective for this aircraft and signed by John G. of the Nose Landing Gear Brace Assembly The purpose of this repair is to prevent torsional movement Landing GearDr ag Brace Assembly (GAC P/N 1159LM40588- (GAC P/N 1159L40801-5) and the Nose GB146-10) in the Drag Brace Fitting at fuselage I I) that causes the loosening of the existing bearing (P/N station 119.0. Performed removal of existing bearing PIN Removed the Nose landing Gear Assembly from the aircraft. Brace Fitting, PIN 159B10053 per GAC Drawing GB14G-10. Inspected and reworked existing Drag d new K210-3 Bearing Assembly and torqued to Number SE05201903-901, Standard Installation. Installe 110 in. lbs. Assemblies per GAC Gulfstream IV Maintenance Installed Nose Landing Gear, Drag Brace and Dovmlock Manual, Chapter 32-2-0, page 204; pant 3. in accordance with GAC Gulfstream IV Successfully performed landing Gear Normal Function Test Nose Wheel Steering Function Check in • Maintenance Manual, Chapter 32-0, page 201, pan 2 and r 32.500. page 201;para I. accordance with GAC Gulfstream IV Maintenance Manual. Chapte aer.t with this FAA Form 337 in the aircraft's Returned the aircraft to flight status and recorded oaeopli maintenance records. ;emir and any previously approved It has been determined that the interrelationship between this effect upon the airwort hiness of the aircraft This configuration will not introduce any adverse changes to the operational limitations; No flight determination includes, but is not limited to: There arc no manual supplements are required; and the repair is compat ible with all preyious configurations assuring the applica ble airwort hiness requirem ents. continuous conformity with data is negligible. The effect of this change on the aircraft's night and balance prepasd by 16:;tral DbeooJy This nacos:pester manta form filed as N0SEGEARD0C: 5769 Ono= NO ADD MONAL SHEETS ARE ATTACHED.. !END*. ^ SDNV_GM_02754198 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241120 EFTA01326713 *ra ~Vink" Lts-nrts - rkower•--..00mus *wan miNTOrwarninT~ . TRA Alanten RECISTRT CAMERA AD. DATE: 6- -(13 Pon, Rporoml OMB fia 2120~ e • MAJOR REPAIR AND ALTERATION Por PAA Ure Ody ufatarnon or Appliarice) cd anmemarn (Alrframe, Powerplant, Propeller, name een War (5 e - 4 41 se tinCe Menseno nlreamonowometer Manntions PAR43~mM e.and AC Ci-I falitague orstaucnOtis,Prim or tYPII Ill•eltihs.Sa FAFT43.9. ~Ome inlaw OnUSCAKMhPanda nalfannat Manin ltdd MOUW mtalwand KOM doonallo n d tha We:Mom men b and Ad d len). Mor mok mach vadatim (34rnhon Int Naleal ~Me wam Mike G-IV GULFSTREAM AEROSPACE uee repya ' 1. arend Nimonarny anlirgr ~d Na 1085 01/PEVaD Aanleg Ms Oom Onrontratko~Ko" Name fernsMwn On~4~ TVO EMBARCADERO CENTER Z Crnmer BA LEASING 8 CAPITAL CORP. SAN FRANCISCO, CA 94111 3. Per PAA Uwe Satd4. ,...........27„, ayi aaya aa 4.,,,,aa a aan eg n Mr •::.•• Sv' "ffs ITTIKORI3 M race~ br • or•rt descrod Ihn Sa ~Irae la NOrilán Ka. Y- -F25 InTE S. Type a. om Itle.ntilletbod &NO No. kawa Mbmmm Mere owm UNI mornemm....mo ram,e a Wo n 1 nor') X ~RAKE POWERPLANT PROPELLER Type MOUANCE Manuladuret ...., 4 C. COrdendel naland C Canna* No. A. Agencyk Name and Jans e. Kind of Agency x u9 Caturcatee Naam LANCE A. MATTESON Nmon Catereed nweema 8560 EAST SAN FELIPE DRIVE ~zo Roomt Sims• AP 1864049 SCOTTSDALE. Al 85258 wo.s.a, homo 4 More and drocroDed en me oreme of anmNmem 140,04"TO/0~~1"de WIKT un ROmomwed in Omm innam %quines, * and t the Informat•on 0 . 10e~~ Itecorhhh he milt th* thChlitentl eaS of Pan C dl die V.S. F fan Man node we ben Of my nowledge. , lum~il neem re na and Canal to Me -...."" Dr' loomOmi OM. • APRIL 20. 1993 . L ---,—, 4 ...c c..... x.mprows Re Rdne Te imisib. ~AAM unit Woed« In dam a Ht immarn,n me nameet Prnsfand By K» rammelt to tam imum eIly Olm pemems speolied and is »PPROVED Cl REJECTED Adaruniftwor of Ina Pedro Athibon ANnimstration MIrnarSma•al FAA PrilMimes.% Urnunclumr I inspeaor BV . PemoNmenONTantadat PA* ~gnoe Now Stalen Canada ammarnas Group kommen *a Repelen ~ma m Signalur. of Autroved lno Da* 0 • DwrOMOOn Na r - 6 2 0 0 rttri7fr 191C.744 1 1)Pentredir WASA3 SOI•iY dá4j27 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15,0 an d 17 g41ór EFTA_00241121 EFTA01326714 • • '`r.-77,7,74.1litanOW7Cr#14,,lit ...a. I TAR AIRCItATT REGISTRY ... Illes„ CAMERA NO. S I DATE: VP---9--- -sit NOTICE Anther:monmust be Waters: and balance or operatingImitation [banessnailbe enteralin the appropriate aircraft record. compatible with all previous altelations to assure continued conformity with the applicable airworthiness requirements. a. Oesenaten of weft acteepane III more spec, me required mach additional mesa. identity min aircraft nano/urn and registration mart and data work completed.) 0420193 Guffstrewn Aerospace Corporation {CAC) Model G-IV. Stria/ Nunn es 1085. NDIGA, FAA Anaaft Type Cando:ate Data Shea AI2EA, Revidor IS. FAA Append Data: FAA Form 8I10-3 Statement of Compllaret with the Federal Aviation lb:gala:ions dated 2/3/92 for Gulfs= Model GV. 1159. d 1159A; listing GACRtpair Dwg 11595BM 189 REV. C title CORROSION REPAIRTBALLAST COME. SURF. ELEVATOR sniped by Struction DER John G. Wilt ex, Designation Number SO 683. FAA Acceptable Data: GAC Productioe Dwg 11590520002 REV. E, duets I and 2, inhading through Engineering Orda (EO) RI; dated 1113/92. these drawinp append forprod•wwiew by FM form 8110-3 dated 1118/92 for Gulfureatn Cr4V Anna by FranIt Salmon! SG-7034 Strunna DER GAC C-IV Meicaterme Masai (MM) -Interim Revision 16-1, dated 30 Mardi 1992; OACCeIVMINIYel, I. REVISION 16 dated 6 DECEMBEt 1991; GAC Pe:chain Dwg. 159CS20434, titled SIGN INS7L CODRROt..47YRE-FIEV-STA 1100 a 168.78 LE. MI& 2 rf 2, REV 0 dated 1240-91; and GAC Production Doug- 1159CS20443, titled BALEPTSVS7/. CONTROL SURFACE - ELEYAMR, Ail& 2 of 2 REV F dated 10/28/84. ThentrpeseefilepeieirtetreolaceeitiaMinedinboard nifing edge assembly on the left devisor.. This repair involves: A. The removal the left deviator from the istertee, B. The removal of • inboard trailing edge riveted assembly; C The installation of a new inboard outing edge riveted assembly; D. The removal of a Medan of tbt leading edge riveted skin to pin soon to the balm trim weight attach pond E. Assembly. painting balancing end attachment of the elevator control surface to the aircraft. In accordance with the GAC Conatterized Munn= Program ICBM code 2736.07 anvil the left deviator, GAC P/N 1159CS20022-59, S/N IOW dated I 1 /88. from the anent Flemmed the toned riming edge assembly, GAC EN I 159051120400, S114 1113. date/ Aug 23, 1988. from the left elevator by dribs( ow the attaching rivets Installed a new inboard trailing edge assembly. GAC PIN I59CSM20400-89/F-2/01, SRN 1400, dun holt 1993, onto the demo( by riveting in achtMAPCO with the applicable instructions contained on GAC drawing 11590520002. Rimmed leafing age skin a the balance at wight enact points by drilling ramn rivets to gain meets to the balance trim weight and: pone sad added I each GAC PIN I IS9CS20443.5I (0.5 pound) weighs and -53 doubler in accordance with data cormiood on GAC Dwg. I I 59CS20443. REV F. snouts:id 2, dated 10/11/68. BALLAST ITVEIGH7717,571. CONTROL IRFACE-ELEVAIDR. In accordance with the above referred to GAC Product:cmDee& detailing SKIN NM mstalkd original elevator leading edge to by Mang. Trated, sealed, primed sal painted tetrarch all bare meal. In accordance with the GAC NMI ATA 27-0 Flight Cootrol Systems decked balanced elevator; final balance data after paintin LH elevator 0.0 in.Abt NOSE HEAVY. In accotsbnee with GAC CMP codes 273007 installed be maned left elevator. GAC PIN 1I 59C520002-59, SRN 1086, dated I1/88, to the proper position on the aircraft The mad was not tat flown because it vets disenimd that the tate dal was dote would not change the flight cliamatristies or 0mo/tonally aft xt the Bight operation of the ant This determination inchaded, bin was not lintel to, anderation that the repaired elevator tamale balance, shape. mega and original type =fame design was cot changed. Recorded compliant with this FAA form 337 in de sinnit's maintenaam records and =mod the aircraft to flight tame. Aarall Total Tent: 1362.6 heat Aarah Cycles 547 landings. Changes to the artralTs weight and balance was negSgible Ttm morear ecorraird 6:0 prepond by Mathool Pau idly teen a PcMat/50. Midas CLUAY112073ELD3C.,1555 Calm • ADVTIONAL SHEETS ARE AITACHErt na.ar Addazontit ShWrIt Ai. AitaErtycl r . • • • •'-•!.2.17 15 f. agt., :1 & Fit . 41,/4 a kiwistit.- • ' •: •1 • SDNY GM 02754200 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241122 EFTA01326715 FAA AIRCRAFT REGISTRY , CAMERA IRO. DATE: 40 - 13 a tr" r Sgi Nisi ' 0.1*.119402. ® MAJOR REPAIR AND ALTERATION Far/AA US. Oa, uac....cus (Airframe, Powtrplant, Propther, or Appliance) OtEse Idemdcown erspoils Aillall Z) 1 t tr i/. 2) INSTRUCTIONS: Print or type all entries. See FAA 419, FAR 43 Appendix R. and AC 43.9-1 (or subsequent reviCon ifsenc4) for instructions wvi disposition of this forrn. This moon is required by law (49 US.0 1411). Failure to ninon can result m • civil Peray to to acted 11.000 for each such viotulon (SecOon 901 Rola Act of 195/1 Make Model I. Aircrati ' Galfstream Aerospace G-IV • Serial No. • Noionably ad Registration Mark TOES MICA - Name (As shown co toptinunn ciro.5mtc) Address (As doom cm *strata outdate) 2. Owner B A Leasing & Capital Corp. Two Embaraidao Caner San Francisco. Ca 94111 3. For FAA Use Only 4. Unit Identification S. Type US Make I Model I Saul No. Reps Altermam Airframe (As desaThed in Item I above) I • PowapLarit - Propekr Type Appbsecc ' Madam= C Conformity Statemaa A Agemis Name al Address B Kird or Agiscv C. Cates. No. LANCE A. MATTESON X USCertiScated Meths* /560 E SAN FELIPE DRIVE Foreign Calibrated Mothasic . AP 1861049 SCOTTSDALE, AZ MSS Certificated Repair Stab= Mazufactura a I catty that the mut andke abernice made to do =Ms) idadifiod in mei 4 dote mddesailed ce the Mint Ot °tea berm bin beCti mat to oxcart= with de nstprenamts or Part 43 ciT dic US Federal Mimi= Repack:4w al dads infamatica fonistoTtenia is me and correct beta tot at my Roma/age Date Signatia t Ci : 2 / '' ?..., 7. Approval for Retry to Service Pinson dm mitbrily pm persons spec:del Sow. the ma ideetifee in dm 4 arto impsold in the r natal by the Adminanore °fan Federal An Adman:sire and is CM APPROVED 0 REJECTED FAA D. Stmlurdi R ingo= Askant= bcost. • Manufictister Otter (SpolgY) BY FAA Drama Rcpt Stake Pc Amoral by Traimert Comae AirocatioasCiosp Due clApprovg or Reamial cot rs &pat of Malrituni Onipasims Nu —-- Ili ZIP , -- — — 324705494 LA - Nfrined Dome& L pilan7f44474C:re .. . SONY GM 02754201 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241123 EFTA01326716 • r' ""2"...S0a- 57- .9 . Yei; ' -Ds FAA AIRCRAFT REGISTRY . a _ en 1. I . CANERA NO. aDATE: 10 — 1 13 NOTICE Weight td balance or operates talon change shall be eared in the appropriate termed record An aluraboo 0142 be consparibk with all previous alterations to assure cominued =fort* with the appfrable airworthiness reqtaemems It Description of Wort Accomplished (If more space a naming nue eat ood them Wady with tome • , and avant= mirk ad die Wert omPlotet April 20, 1993, Oulfstream Aerospace Corporation {CAC) Model O-IV, S/7.4 1085, NSSGA FAA Type Certificate Data Shea A 12E/1. Revision 18. • • FAA Approved Data: FAA Airworthiness Directive AD 93-04.02 Rockwell Icrtertatioaal/Collins /niece Division TDR.94D • Mode S Traisparlere FAA DER approved form 8110-3, dot Aped 16. 1993, Ideatificsnoe of Drawing Numbei(s) 08069197 ad 0806919111. edited 09/01,94 ResisiotA, Wag Diagram' No. I and No. 2 Teepee (MOD). John R. Chamdess NM-476 Systems 4: Equipments DER. and Western Coentionder Incorporated FAA STC No. SASO44NM, as approved February 6, 1991. The purpose ofilitictenge is to =Key this aircralls wiring to correct wiring discrepancies team the TCAS and the Mode S transverses syuans Woing disrepute were discovered she both TDR-94D Mode S transponders were modified to Cola; PeN 62:4210-003 a required by the above fisted AD. Prior to complying with the AD this Mend was equipped with Collis PfN 622-9210-002 assn transponders insetted in accordance with the above listed SIC and utilized discrete wiring to the TCAS word hod from each tampon/a, The -003 modifiemire sans transiteders utifim A1UNC 42r data and require removing the discrete wiring for 'STET', - ra - r, 'ALT PORT 7 OUT. and 'REMOTE [DENTIN'. ModSed this aircraft's wiring to conform to the above listed drawings %floor deaden to the approved data with regard to the 'REvIOTE inarr ad 'TEST' was done,, follows: (a) Wire 1SX22822 was removed from al transponder Rff P2-55 ad inserted into #1 transponder Rif PI-16, (h) Wire 2S3C21B22 was removed from e2 transponder WY P2-55 and boated into er2 transpooder RR P1-16; (c) Wire 1SX21A22 sod Wee IS702A22 was spliced iogetter ear TCAS control pad P1; (d) Wire 2SX21A22 and Were 2SX7seso were spliced together new TCAS control pad P2; (e) Wee ISX23A22 had be pmiously removed horn muisponda count pad Palo E and rapped and stowed. and (4 Wire 2SX23A22 had hem previously removed from 52 transponder cord panel Pia E and capped and stowed. Dusan Avant (FAA CRS 'DVS I54F) performed m enegrati sysems tin pa FAR 91.411 and both transpooda systems were toed to amply with Part 43 Appendix E (c) Work Order No 22.37R, Mud 4/I 5/93. Ramp to reeled that the memo co-ax come ton were reversed between the I I and 12 system a the TDR-941)r1163; comae co-ax conreatons to conform with the above feed drawings. Now Trans--der ramp teeing was doe ming LER L-band antenna •HAr steads go ' prim false alerts is arbons TCAS equipped Maid - • Returned the dread to Eight seats ad recorded corgiarace with this FAA Form 337 in the aircraft maircessax records. Ainneft Total Time: 1382.6 been; Aircraft Cycler 547 lags It has bee &rased the the intardetioeship between this change and toy previously approved coaster/M.9n will not introduce( any adverse effect upon the airworthiness of the aircraft This determination incluiten Ss is not limited to: The minor deeigices (a) through (d) above accompashed the intent of the approved data; No changes to the eitoraffs electrical led analysis data were nude; Them are no changes to the operational limitations; No digit manual supplements are reqsjed; and the installsion is compatible with SI previous alunetions assuring CO0SLIOU.S conformity with the applicable IliTY•OnSICSS requirareets. The dim of this change on the wash's weight and balance dais isles:jolt / This mom= gacrord form wet der uses MABC4W33; WORD 2 O0, AD9a 7216 Chas pep. by Mat Dcally. NO ADDMONAL SHEETS ARE ATTACHED. 'END' 0 Additions/ Sleets Are Melded r:. • .7 • ks RFJ 1 v.,4 • vr.21•• a fil=i cwito:liXits - SONY OM_02754202 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241124 EFTA01326717 I ro AIRCRAFT REGISTRY !I l,"CAMERA ND. wi DARE: 4 _2_93 ',IS AliSli — Owe. nNaatt MAJOR FtEPAIR AND ALTERATION Facia Us Owl. ® . nano 0;mans.. (Airframe, Powerplant, Propeller, or Appliance) War Idanoticaaat r........sq ' 55 t --f f:Sb ) xammweq INSTRUCTIONS Print or type all entries. See FAR 43.9. FAR 43 Appendix L and AC 43.94 (or subsequent revision thereof) for instriblons and disposition of this form This report is required by law (49 USG 1421). Failure to report can result in • (MI penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of IOU:. — ?stake I'. Aircm8 Guifstream Aerospace . „Cl atIV Serial No. " and Registration Mak ..... 1085 . NSSCA -Name (As shown co regutrabort catifiudc) Address (As do= cm regisizaion eertitale) 'Two Embareadere Caner 2. Owt B A leasing & Capital Corp. San Francisco, Ca 94111 S For FAA Use Only . 'I A . • es. ' 4. Unit kleatifkation 5. Type Ucit • Make I Model I Said No. Repair Mama Airframe (As descrised in It , I abort) 1 • . • Powerplant 7 ....-.5 * Propeila Tqst, -. AppEaree Misaufrower • ").. e 6. Conformity Statement A Aoscx's Name and Address It Kind of Aricccv C. Catificaa No. LANCE A. MATTESON X U.S. Cat on:al Mechanic 8560 E. SAN FELIPE DRIVE Foreign Certifie43 Meekank AP 1864049 SCOTTSDALE, AZ 15258 Certificated Repair Station Manufactiser a I certify than the repair altar gum= rare to the ma(s) idenriScd is run 4 abase and detailed m the rause or anactwocnn her= have hem corde in aceordacce with triecq=stocou of Ent 43 of the US. Fecloul Asia= Rept.= =I thalete iskniusie fionisbal borcos is true and mica to = tat of we knoakdat Date Sifotaure red leant . -20-n 4':c 7. Approval for Mora to Service . Parma lode mita* Men persons specified bra, the adidentified in it= 4 assmoose! in the ma= prurenied by the Aaninisvaire (IS Third Avila= Atimaisimica India 11) APPROVED 0 REJECTED FAA Ft Sada Nuessfactung x lasaectim Aurtateginn Otter (Sreafy) BY Spier FAA Designs Repair StaSm Passe Approval by Treason Canada Mealtime Comp Date of Approval or Rekcoon canoes a Sipatum Of ' • 1341000=Na. 2— 7.4o-99 '526705494 IA 0.0"" ' Wald Donnelly ••••••• 00. ' zkan itsuasreketInbaSads . ' sir44 ',write-- .1 SDNY GM 02754203 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241125 EFTA01326718 FAA AI RCRA REGISTR Y rl I w DATE:11. CAMERA NO, FT ..2,_9(3 I III • NOTICE aircraft record An ahenuion nuns be Weight sad balance or operating limitation changes shall be enured in the appropriate assure continued conformity with the applicabk airworthiness I equiremcau obestible with all pinions altentioth to L Ikstription of Work Accomplished aid agrarian mark and dare mark Or eve spare ithereired, mach midi:ken dens. SOF/ •th =nett nationality G-IV, SIN 1085. N880A. FAA Type February 20. 1993. Gast= AtiroIAngx Corporation (GAC) Model Certificate Data Shea A I2EA, SUBJECT: ELECTRICAL POWER Refer to: GAC FAA Approved Aircraft Service Change (ASO Nattier 231. MODIFICATIO N: dated JULY 31, 1992 and GAC FAA DER (ATA 24) "E" BUS ALTERNATE POWER - 02-05-93. Approved Wiring Diagram LEO 46603241 rev none. ASC 231 Deviation. date of ASC 231. This alteration stores The purpose of this change is to replace four wins that wan removed during the installation °prefiguration the FWD end AFT Emergenry Battery 'CHARGE INHIBIT circuits to the original production Nftinneci.tlth s fl ail" err PNL 131 25.4.1] z f:Hot.= a free sad, airy installed • Dew Sump /SSW a new Isfil-W-21759116-20 wire 21M111031420. stripped the Sedation from socket contact onto the wire, Sated the wile assembly into GIS - B. Rooted the free aid along coning Deutsch C7S-20/20 leogth stripped the insulation from the free end, crimp Stalled a new Desch CTS- wire rims toward THE, at [hetes to 20/20 socket coma onto the wire, inserted the wire assembly into TI1E - IC Modified ,he R CKPT JCT ENE (306AIJ as follows: insulation from • free end, crimp installed a new Stamp klatSed a DOM Md-W-22759116-20 wire IPU1103620, stripped the onto the wire. Sated the wire =co* into 712M - C. Routed the free end along aiming Deutsch CTS-20120 socket cornett snipped the insulin= from the free and. crimp installed a new Deutsch CTS- wire tuns toward TJ4A. oat the wire to length. areas disturbed during thermion. 2020 socket contact onto the wire, inserted the wire assembly into INA - F. Secured all follows: Modified the FWD EMERGENCY BATTERY WIRING [68A1) as grated Removed the end cap from eating wire Removed wire IPLI9010A2ON coasted between MIAIPIA- land Sae GA0135MMOS socket contact onto the were, I PUI I12B20, stripped the insulation from the free end, crimp installed new thermion. inserted the wire assembly into 68A1P1A to Secured all areas dirket:sod during follows: Modified the AFT EMERGENCY BATTERY WIRING [68A21 as Removed the end cap from existing wire Removed wire 2PU9010A2ON connected between 6$A2PIA - 1 and simraft ground. GACIISAMOS socket comas onto the wire. 22U1112.A.20, snipped the insulation from the free end crimp installed • new inserted the wire assembly into 63A721A - I. Soared all ants disturbed during thenuloo. L4 sot no floors: cpsrice Fathoms masts athekout m aceoräan©e MtnASC 23 i ail pats of paieraph 7 337 in the aircraft's nuirdeconce records. Remind the fact to flight status and recorded compliance with cis FAA Form approved configuration will It has beat determined that the interrelationship between this change and any previously ads:Serf= upon the airworthiness of the aircraft This determination includes. but is not limited not introduce any load analysis data is performing its intended functions the to: The change to the aircraft's electrical negligible; When flight manual supplants are operation is automatic: There are no changes to the operational limitations; No continuous conformity with the squired; and the installation is compatible with all prmious alterations assuring applicable airworthiness requirements. The effect of this change on the aintralts weight and balance dm is negligible. This coasthr seems farm was dole on ACAF3S6/20. Sag WORD 10. fried a CIASC23102ds PSIS by Schad DereellY. NO ADDITIONAL SHEETS ARE ATTACHED. *END* O Addidoral Sheets AM MI MS 1 ••••rreir--1 - SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, -15, and 17 • .4. • SbNY GM_02754204 EFTA_00241126 EFTA01326719 FAA AIRCRAFT REGISTRY CAMERA NO. 2 DATE: 3--)S-- 93 -- ow • taws ® MAJOR REPAIR AND ALTERATION Pre WAS l • iOS W.Il m. . en•mu••• (Airframe, Powerpiast, Propeffer, or Applinet) OAS Llanbabos %dad NISI= 5 - 0i Ada/MIS 'A ); • iNSTRUCTIONS: Print or ran all eels. See FAA 43.9. MA 43 Appestat I. and AC 45.9.1 (or mbar:wont revision thereon foe irennactions sad disposition of this form. This report b rewind by law (49 UAC. 14211. Failure to report can meta • • CAN penalty not to emceed $1SO0 for each such violation (Section 901 Federal Aviation Aa a 1931). Nuke Maki I. Airmaft Gallant:am Aerospace C.-W Serial No. 144417aliaY red Regatta Mark 11025 NEC A, Nom (As town as registraext oroficeie) Addis (As town al roparsoco tati5cate) 2. One B A Leasing & Capital Corp. Two Embarcadena Center So Frwart Ca 114111 3. For FAA Use Ovey t Unit Ittentifkatiaa 5. TM* Urtit Stake I Model I Serial No. Up= Abash Airframe (As clesaised io Mani Love) I PowpLant Propeller Type Appesoce Mau= ii. Conformity Swasett A. Amica-s's Name red Adam R Kid 0f Araw C Cate No. LANCE A. MATTESON X • U.S. Certifgemd Mechanic S.560 E. SAN FUME DRIVE Foreign Certificated Mechanic Ar *M441$ SCOTTSDALE, AZ LAM Certificated Rimer Swam Manufacturer D I orgy Mat dm repot as/or Menke sew lode eras) identeed al Con 4 Mom red damned ca the mane a sand -a rent, here beat made in axerdsoce with the requiem= of Pen 43 of de US. Federal At Reipaa ad gm de iefensaias (aided brain is ins rod area to de boa dray krairedge Data / / cf. , 7. Amami far Ran a Service Paws= to de seferity given mom cecina! Wow, do ma idessthod i it 4 ins imported it the cat presaged by tlz Aftwastreter dale Federal Miriam Adecitannaien ad is an APPROVED 0 REJECTED FAA Ft asedmils bianufahatr 1 bap:aim Auelmizarice Oder (Spa:dr) knot BY FAA Dewiese Rep* Sums Pence Appored by Dation Coda Aiwartlimme Grasp Da of Apron]a/R*2i= cabals Cr Sigma= of Deeproce Ho. 52470504 IA .T24 2, 1993 -r;a: :- Wichsed Dormeily • • SDNY GM 02754205 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241127 EFTA01326720 _ 'H9211Wayea rra FAA AIRCRAFT REGISTRY CAMERA NO. a DATE: 3-is---13 NOTICE Weigle and tern or oparing Futon charges ran be awed in the approprire agate record_ An ettererioe must be compsuble rib el previous altendious to esure comieued cocforSy with the eppEcede einvortlioness requirentetts Derriptioa of Work Arremplithed (If ern epee is reenrett redo ackfitictr emu reedy web wart istraddy es: repstnoon ark and date viva competedO January 31, 1993, Gulfstream Aerospace Corporation (GAC) Model G-IV, SIN 1085, N88GA, FAA Type Certificate Data Sheet Al2EA. Rem to: GAC FAA Approved Aircraft Service Cange (ASC) Number 207, SUBJECT' Auxiliary Power Unit (APU) Electronic. Control Unit (ECU) FAULT SIGNAL - IMPROPEMENT: dated: JUNE I, 1992. Related FAA Approved document GAC ASC 8A AnTillny Power (ATA 49) APU FIRE TEST - IMPROVEMENT; dated: Match 30, 1989. The purpose of this change is to prevent the Data Acquisition Unit (DAU) "nuscornpare message from being displayed on the Engine Instrument Crew Alerting System (EICAS) when the APU overspend shutdown is selected With the preient design it is possible to receive a false DAU MLSCOMPARE EICAS message because of an out of tolerance signal generated by the APU ECU. Performed all of ASC 207s MODIFICATION INSTRUCTIONS fisted as effective for all Gulfstrearn IV aircraft Note: The effoctivitiy of the service change should be Aircraft 1031, 1006 through 1155; not all Cruffsmaun IV aircraft Aircraft Service Change 231 von purchased in kit form from GAC Product Support Savannah, Ga. 31402. Performed installation checkout in accordance with ASC procedures paragraph C all parts and noted no abnormal operation. Returned the aircraft to flight slams and recorded compliance with this FAA Form 337 in the aircraft's iosmance records. It has been determined that the interrelationship between this change and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. This determination includes, but is not limited to: The change to the aircrafts electrical load analysis data (0.02 amps added to the APU control C8236 during fault condition test] does not cause any exceieclann. in the normal or emergency power sources: When performing ifs intended functions the operation is automatic; There are no changes to the operational limitations; No flight manual supplements are required; and the installation is compatible with all previous alterations assuring continuous conformity with the applicable airworthiness requirements. The effect of this change on the aircraft's weight and balance data is negligible. msompileriptergcr ram en ha ce GIPITAreiSCk are WORD 2.O. riled r C1ASC2O76:c; ewer by trchad Etraity NO ADDITIONAL SHEETS ARE ATTACHED. 'END* 0 Ada:loot Slims An Merkel • SDNY_GM_02754206 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241128 EFTA01326721 LAXAIRCRAPI N0.EEC V. CARERS I ' STET DATES 2-4 - 9 3 'ID MAJOR REPAIR AND ALTERATION kin A•1." Oka Wo• 21.1.00) ... Far FAA Meat, es Deree other kluged:Soo e . .oasse (Airframe., Powaplase, Propeller. or A Pr011occ) ..........- ...s.ererem 5- 6 t - t P •,) INSTRUCTIONS: Print or type all emnes. Ste FAR 43.9. FAR 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 14213 Faint to report can result in a chli pen.dry not to exceed 11.000 tor each such violsoon (Season 901 Fetal *ratan An at 1954). Make Modd I. Airaafl Cultures= Aerospace G-W Said No. NatioeigAy and Registration Mark IOES • NESGA Neat (As demi co regimen= coafica) Adams (As shown oo *Salim oath:ale) 2. OVAMIr B A Leasing & Capital Corp. Two Eabanadero Crater . Sul Promisee, Ca 91111 3. For FAA Use Slaty 4. Unit Idetaitlestioe S. TIT* US Make Modd I Saial No. Regan Mama Airframe (As cicsaased in Item I above) I Po...erotica Propeller Tyr ARIA/act Mat= & Cowforaft Slarapent A. Agr's Nome al Aetna R XIS of Apace C. Cate No. LANCE A. MATTESON ' X U.S. Certificated MCCIISC SSW E. SAN FILM DRIVE Foreign Catificatol Mer.lanie AP 1861019 SCOTTSDALE, AZ *32U Care-aced Rare San= Manuficarer D. I certify that the repair aralke ant= nude Loth' mi(e) idereified in roma above awl lambed on de mane anadaeas hove have km made in aeciadaesx web de requiem= ofFart 43 of the U.S. Federal Mistiest Rtadatims arid that tlx reformaan furnished tam is Ins sad Dana so the ben dray knowledge. Dare Slgnaoae ImoW cda.,-, zi /?PS / 6 , 7. Aaron' for Rerun Lo Service Penman tole aahaity Seen passe geedial baser; the air electrified in item 4 wa ®patted in de roar rooted by dm Admixing. had is NO APPROVED I:1 REJECTED ants Fakral Avimiao Admitisindat FAA FY Staler* Manufacturer x hapreso Aothorizoim Odor (WA) BY Space - . FAA ThaPa• Rica Station Pan Append byTriesart Cade Airworthionts Dace of Approval of Rea:ciao Casa of DraipsteoNo. .7 -#.74.12 .., i f pi 51670504 IA Michael Deemer& AA Fern • b• • 002754207 -- SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, -15, and 17 EFTA_00241129 EFTA01326722 FAA AIRCRAFT REGISTRY CAMERA NO. 2 DATE: 2- ct- 9 3 NOTICE An onion sun be and or oteming klub= chews shall be entered S the appeoprisse zinzatl reset Weight ban= wed confonni ty wilt the appbcabk sirword ioso squirms= cotsnable with el scrims then/Soto to assure co & Deaiption of Work Accomplidied web sacra cusenals oil mg/stream mark and to wok conspbend) (Vox= sax u nosed such aldisicest daft. Identify Certificate tion {CAC) Model CblV, SIN 1085. N8SGA, FAA Type January 2, 1993. Gedfirream Aerospste Corpora Data Shmt Al2EA. (ASC) Number 231, SUBJECT: ELECTRICAL POWER Refer to: GAC FAA Approved Aircraft Service Change ICATIO N: dated JULY 31, 1992. (ATA 24) "E"BlISALTERNATE POWER - MODIF the source of power to prevent the loss of critical systems in The purpose of this change is to provide an shanate has many systems powered only by operatio n. The present design crag an E-Bantry (E-Batt) fails during normal be lost. n all of the systems powered by that batty would an E-Batt Should an E-Batt fail dining normal operatio taracanically as an alternate power source l (MS) dc btu power that will save This service clusage provides Essentia operation to the F.-Bases should an &Bait fail dwiiss uorinal 11. CTIONS listed es effective for skald 1001, 1060-12 Parfait:Mid all of ASC 231's MODIFICATION INSTRU and 22U900 5A14 were not installed; Figure 4) Wire Number 1PU900 5A14 except for the following deviations: (see 1PU9005A10 and 2PU9001A10 god commted as follows: ensued two new 10 gauge wires were sump ideotified was connecte d between the Line side of CB2311 tad the line side of ASC231CBI; wire wise IPU9005A10 to (Figure 4) u place of 2PU9005Al4. Raychem solder spikes were used 2PU900$A10 wan conneved ass shown installati on were fitted to the proper size that required crimp mate all three way connections. All instalkd wires d required to maintain ccaformity with previously approve contact or teronival. Now: The listed deviations were 231. intended function of the approve d ASC configurations and did not alter the . Om Figure 3 foe CB idesoenion): ASCDICBI should Note. Figure It'Sezedified Schnook Diagram* is no coma an d ASC23IC B2 stotdd be Wiled A E-BAT el ESS 2IVDC BUS; be labeled F. E-BAT ALT PWR and cosseted to PILOTS ALT Psofk am connected to PILOTS *2 ESS 23VDC BUS. t. Ga. 31402. ASC 231 Kit wee purchased from GAC Product Support Savan l ASC procedures paragraph P d pots and noted no abnorma Performed install/airs checkout in accordance with operation. not e with this FAA Form 337 in the aircraft's msnitera Returned the aircraft to flight status and recorded complianc records. this change sod no prniubsty approved configuration will It has bits daermined that the interrelationship between iness of the ant This determination includes. bust is not limited not introduce any adverse effect icon the airworth l load analysis data is negligible; When perfonning its intended functions the to: The change to the ainnes electrica nal limitatio ns. No 'light manual supplants/ me operation is reno.matic; There arc no cbangei to the operatio continuous conformity with the pinions alterations assuring required: and the installation is compatible witha all ents, V applicable airworthiness requirem balance jail is negligible. The effect of this change on the aircraft's weight and WORD 2.O, filed as CAA= I eke; reepered by. Mida Cosectly. This ones= oasts fun so dace on GIM40.6/30, wog ARE ATTACHED. *END* NO ADDITIO NAL SHEETS O Additional Sans Are Anacted GSA 7 542 08 10, SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, SONY 15,02and 17 EFTA_0024/130 EFTA01326723 A& An RA ca , Wan Roe a DAUB. 1;-30-a1 m..... -..._, Oa.. DICSIZI --. ® MAJOR REPAIR AND ALTERATION Far AAA the OS vs wa nt nanny (Airframe, Powerplant, Propeller, or Appliance) news Anew se. INSTRUCTIONS. Print or type all entries. See FM 43.9. FAR 43 Appendix R. and AC 43.9.1 Tors instructions and disposition of this fonn. This report is required by a(49 U.S.0 14211. misloinfaZ Penalty not to 'Need S1,000 for each such violation (Section 90I Feelers Aviation Act of Failure 19591. to report can result Ina chid Maim Model I. Aircraft GuiRare= Aerospace C-IV Said No. Nationality and Resignation Mari 10125 MICA Name (As sans on regisizan centlate) . Malls (Aa Mown on *maim note) 2. Owner B A Leasing & Capital Corp. Two Embareadero Carter San Francisco, Ca 94111 3. For FAA US. Only 4. Uset Identification 5. Type Unit Make I — Model I Serial No. Repair Attention Airframe (As desented in Item I above) X • PM/anise Propeller TYE,' Appliance Manbconee 6. Conformity Straeswi A. Amoco Nes and Addams B. Rind of Agency C. Catifraw No. LANCE A. MATTESON X U.S. Certificated Modsnie UM E. SAN FELIPE DRIVE - &gaga Ortafreated Mataric ' AP 11144049 SCOTTSDALE. AtIka193 Cedeeted Repta Safi= Martufmnaer a testify eta the mar anda Anion ma to ate maks idonalle4 mlam 4 stove and dieenbed on the reverse or _____ haw have beat made it oxotemee with the tershemeati.of Pan 43 of the U.S. Real Mision katted bade is no and COMOL to the barium knowledge. Replanom me Um the infonnision Date ifiai A-s, /tn._ s@wne r 4:bdiv7 11. 2,--Ca 7. Appromd for Return to Sava - Perna to the setaity Riven ram spaified below. the ea Sada in ha 4 a impered in the rant poseraxd by the ' Adminiontor of the Fedad minion Adanaimaion;nib l APPROVED 0 REJECTED FAA Flt swab Manufactures i lospechoa Artaboringion - . Caber (Specify) BY .....^• FAADrips Reply &Mon Pawn Approved by Tneeport 7. Cameo Almaden=Mom Gate ofApproval or Rejection Or Signature of rierismaicao. /1- 2-r-9 2- 526705494 IA ter t Michael Dortray • • • --- sb4rd-o.4 b27S4269 • _ SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241131 EFTA01326724 FAA AlIC AFX incistn I wan E. ?k Inn 12-3( - 92 • NOTICE • Weight and balance or operating limitatiov,:hangcs shall compstbk mit an previous alunaiors to assure continued in the appropriate tart record. An alteration must be fo ity with the applicable airwortbinas reqirements. Desalp Um or Work Aaoaiphsbed armors geese u squired mach skimped des Identify ISM Some itineareity and remorse= mat nd du wag completed) November 23, 1992, Gulfstream Aerospace Corporation (GAC) Model Sas( 1085, N88GA, FAA Type Catificate Data Sheet Al2EA. Refer to: AEROSPACE UGHTING CORPORATIO N {ALC) FAA Approved Information Bulletin 92-001, tided UPGRADING SERIES "66"FZ No. .UORESSITLIGH77NG SYS7ENS WITHAL -"I.2" SERIES LAMPS original release dated October 15, -1 992. The impose of this change is to upgrade this aircraft 's Cabin Fluorescent lighting System by =totin existing ALC Series "66" fluorescent Lamps and g the Connectors and installing the ALC Series "12" Fluores Lamps and Connectors. The installation upgrade cent to the AL -12" Series Fluorescent Lamps on this eliminates the requirement of having to comply with aircraft Airworthiness Directive 90-14-06. Rammed the existing 14 each ALC P/N 6635.12 20-25 cabin fluorescent lamps and 28 each ALC PIN 31.85.1A lamp end connectors and installed (in the existing motmittg clips) 14 each new ALC P/N AL- 1235-1220 lamps and 28 each new ALC P/N AL-511 3 lamp end connectors in accordance with the applicable INSTRUCTIONS in the above referred to ALC Information Bullet 'Al installed parts are FAA/PMA approved and were purchased new from Aerospace Lighting Corporation; 101-8 Cohn Drive-, Holbrook, N.Y. 11741; telephone . 516-563-6400 and 516.563.8781 fax Berfonaxl System INS*CITON and CHECKOUT in accordance with paragraph 5.0 of the above to ALC Information Buie& and noted no abnorm referred al operation of any of the cabin Fluorescent Lamps. ReturneA the aircraft to flight status and recorded compliance with this FAA Form 337 in the aircraft' mairlieTnce records. s It has been determined that the intareli5orship between this change and any previously approve confvhcation wgl not hlreCitlett any adverse effect d upon the airworthiness of the aircraft. This includes, but is not limited to, consideration that the determination FAA New York.Aircrall Certification Office has reviewed the information and procedures contain ed in the D3 92-001 and considers the AL "1r Series Lamps and AL-5113 Lamp Connectors to be accepta ble; and Mavis= FAA approved Power Protected Unit installed at each Fluorescent Lamp circuit that will automatically &connect power should a malfunc tion The effect of this change on the aircraft's electrica l load analysis data is negligible. The effect of this change on the aircraft's weight and balancedata is negligible. Thu comma= wart= form war dour on a mgr. Amos WORD Z0; Med a CSAI.CLTS doc Paharl DctromnY. NO ADDMONAL wen ARE ATTACHED. *END' CI Additional Sheets Are Altschul SDNY GA4_02754210 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 I 132 EFTA01326725 FAA AIRCRAFT CAMERA NO. REGISTRY DATE: 19-9ą" prunes .0- .• oopana ; @ *MAJORREPAIRAND ALTERATION • "'- • .ftirathe anty moire Office lireeneden • Pilenia Ihrietpl!st, rrpralt• cF.SPYinet) . . Indian msw.. a9C ad INSTRIKISOM Print or type all entries. See FAX 43.9. FM 43 Appendix B. and AC e 3.9-I (or sunnom revision therm/ for Instnxtions and disposition of this form- Thh report is required by law (49 US C 14 2 11. Failure to report an result In a cMI Penalty not to need $1.000 for nkwd‚ violation (Senn 901 Federal Aviation An of 19$s), Modd 1. Aircraft ,...Caltstream Aerospace C-IV ł Soria. $0. . Nationality and RegistraSon Mark • • ' ille5 NSSGA Neste (Al dwom onegistratim cerdfiarM - - . Address (Aa dawn co registration catiflade) Z Cimsa B A Leila* & Capital Corp. Two Embartadero Certa . San Prawico, Ca 94111 3. For FAA UK Only • . t Urn Ideaderatbae ' S Typ Udt Make I Modd I Serial No. Rew Agamiom Airtime . (As dercnbed in Rem I aboM) X .. - .. • ..,• Proper TOP • Aperture Maftraincr A. Mats Name aratt Min . B IDS afAmdcy C. Catificus No LANCE A. MATTESON X U.S. Catificated Mechanic /1560 L SAN FELIPE DRIVE . Foreign Catifacated Mechanic AP 1864049 . scorrsoms_ AZ asz.ks C.atiEcered Repair Stanco Manufacturer D. lamny dat the repair ardor skeanmalm to St) idepalkd S On 4 Mm and downbed en dw reverse a menuems lwem have bam ads hi accordance "nth nie reni= °Pm 43 ate U.B. R&M MMus &inn and tai the informed= Aniist.wd herein is true and own to the bon of my knowledge. . .--, Date . . *Signature of • Cr M.ial • ł/7. . 22 / y e Z- • - - .) Amoral for Haan to Service t kurant to ttr arbom pre pans imaged berm. te out Mmdxl ir, ime 4 oma irpaciatt ia te ram= preacrixd by the Admirientor oft. Fakes/ Aviatai Antenatko aM d O APPROVED O REJECTED e FAA Ft Sean ihilinuSicturer = lawin am Ditiar ) Ignite BY FAA Deligai• Rfn Statim Palm Awned by Tremom - •• Cann Antos Date of Approve/ or Rdedion Signature of Dann Cwanallo. ' 8/3/A Ł-- 5267/5494 IA Michael Donotfly •- ....i . • _: I . j .:i SDNY GM 02754211 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFM_00241133 EFTA01326726 • .7. REG} 0 ort - FAA AIRCRAFT AIL CAMERA NO. . .• N.* • NOTICE Weight end balance or operating limitation changes stall beentered in theMpopriste aircraft record. An alteration mug be compatible with all rots alterations to mane continued conforzeity with the applicable airaorthioas tequitemects & Deaniptlem fl out Accomplished (If more space a required. mad Coed Meat. Mat with Jinni nanceality ad regbaatire ark ard date workcm0lfrd) August 31, 1992. Cruz/seem Aeromwe Corp. MedeIG-IV, SIN 1085, NSSGA. FAA Type Certificate Data Sheet MINA- FAA APPROVED DATA:1 FAA form 337 dated August 2, 1991 for this aircraft; FAA form 8110-3, . Statement of Compliance with the Federal Aviation Regulations, dated 4-6-90, for Gulfstream G-IV Airplane, GAC, List of Data - Identification - drawing 11595B41039 REV A dated 4-6-90, effective for aircraft 1000-1130, titled APU SILENCER GARRETT GTCP36-100G PEP 39 (G-IV) TOP DRAWING; and FAA from 337 dated December 27, 1989 for this aircraft detailing STC No. SA1 I INE, dated November 24, 1982, covering the installation of PATS P/N 43206-9 FAA/PMA louver assembly. The purpose of this change is to remove the Gulfstream Aerospace Corporation modification to the Auxiliary Power Unit's (APU] Accessory Cooling System installed by PEP 39 and re-install the previously approved configuration that uses the PATS, Inc. APU Accessory Cooling LOWCI. Removed the GAC P/N 1159B21419-93 panel (APU inboard enclosure wall) and re-installed this aircraft's original GAC production P/N 1159621419-79, Rev. MI (date code 0887) panel. Re-installed the PATS, Inc. FAA/PMA approved PiN 43206-9 Accessory Cooling Louver and attaching hardware onto the 1159B21419-79 panel. Attachment of the Accessory Cooling Louver is detailed in the above referenced STC SA 1 1INE and was accomplished with 5 each NAS1103-3 bolts; 5 each AN960CI0L washers; 5 each MS21059.13 nuiplates that were attached to the panel with 10 each MS20427M3-3 rivets. Performed operational check of the Auxiliary Power Unit, including electrical and pneumatic loading, using applicable procedures contained in the Gulfstream Aerospace G-IV FAA Approved Aircraft Flight Manual and noted no abnormal or unusual operation before, during or after the operational check Recorded compliance with this FAA form 337 in the aircraft's maintenance records. and returned the aircraft to flight status. No flight manual revisions or supplements were required or installed as a result of this alteration. No changes to the aircraft's continuedAirworthiness inspection schedule resulted from this alteration. It has been determined that the interrelationilip between this change and any previously approved configuration will introduce no adverse effect upon the Airworthiness of the aircraft This determination includes, but is not limited to, consideration that: there will be no cockpit procedural changes; the modification is not related to any safety or Airworthiness condition; the design of the APU compartment and accestory cooling arrangement wall:tot allow fire migration to other areas of theaircraft; and this alteration was previously installed on this aircraft (and other similar model aircraft) with satisfactory performance. N changes to the aircraft's electrical Iliad analysis or aircraft's weight and balance report were required as a result of this modification. Mu morn reented ism ;awed* Wad Darellyag s'/UN/1o.ALElied sr evottaaeallOA0131MODCC. ' NO ADDRIONAL SHEETS MIAOW •E".1" O Additional Sheets An .Attached SDNY GIN 027542 2 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 I I 34 EFTA01326727 is glattilOttf 22:11-ItT .8Iiii_2_ ! • . -.- • • ---- 1• I ® • . MAJOR REPAIR AND ALTERATION °VS. tire:a Fos FAA Um Out c uloon.m. aka Wotan • Yeafreae, Powerplant, Propeller, or Appliance) Pa•flem MISISIa • cat-r:io d Icentocnotcs flint or type all truism See FAA 43.9. CAR 43 Appanclix 8. and AC 43.9-1 W SubFAKAnnt revision thIll*On for Instructions and dispoiltkannf this font This c4GOrt Is required by law (49 U.S.C. 14211. Failure to ', Put an rnuft In &del Penalty not to exceed SI 000 for each such violation (Section 901 Federal Aviation la of 1958t Make Mot I. Aircraft Gullictream Aerospace C-IV Sall No: Nalianakty and Rcatittation Mart • INS MCA Name (A. flown on ntuntoo crate) Address Qs mown ea recierefiee cerolleas) 2. Own= B A Leasing & Capital Corp. The Embareadere CS Sas Freaclacs, Ca 94111 I Far FAA Ube Oaly • 4. Usk lilltes 5. Tyre Una Maim I Model I SwigHa poplar as Airframe (As described in ltan I alms) •••••••••••"•••••• X . , Rowerplani Proptier IYIse Applience Maullocemor it. Comforsity ware A. Meemb Nee eat Addles B. ICS of Agpacy C Dans No. IAMB A. MAITESON X U.S. Certificated Medanie 1560 E. SAN FELIPE DRIVE Fortran Certi6mtet1Matta AP 1964•49 . SCOTTSDALE, AZ a ISI Catficated Renee Stencil hunufecturer D. tautly cha the near and/or ammo= aide CO the Se) ant m E 4 ton sal delabed an the warn or asahmeta of Pat Odds U.S. FetedMt balm taw beat meat is =orders with the reciremeas dar. Regatta= el Rase b ass , facriehal herein at= eitt awed tots be ofay browle Sapience oraliatlas ' . 7-3•TZ.--- 7. Appreval fec Raw te Sank* Panel to the tabor*Pan paums Readied below. the lack deeded la ism 4w leipeCted1 the se= pessibed by the Ancohnimior of the Freed Mt Ailmicuarsion and is CO APPROVED 0 REJECTED yli - FAAFIL ii=Yril Mambas= x bspeenne Areharsom to (3pea4y) • • .• BY •FAADeilpes Rape Swam Paws Apprecald byIlaapas • OW& KIEWIONWIS criccp Dan Approval or Rejection OwcifieW or of Docipnfolth. - 7 7s- fe 4 SUMS IA /12 4;nt . namely (84-82) SONY GM_02754213 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241135 EFTA01326728 Li-fittilli"off at:Ilinsiiiin . NOTICE Weight Wbalance a operating Sitation chimps shallhe altered in the oppropiate Mash mead. An alterstion amt be complete with all previews abatis to assure continued conformity with the-rehab& ainvonhinen romirements. t Dem*San 'Mark Ateemp tithed (Ifma spa a required nI isidawne ,he . Idwity web Mae rationality aid region= mak and data wart canerad.) 07/0492 Gulfstmom Aensspace Corporation rag Model G-IV, Sale Numbei1085, NINCIA, FAA Airco& Type Cattalo Da Sheet Al2EA. Aircaft in-wince data wl116.5 home and 449 landings • Refer to the following FAA Approved Da FAA Free 8110-3 Statemerd of Compliance with the Federal AViAli011 Regulations dared 2392 for Gulfstream Model OW, 1159, & 1159A; listing GAC Repel Deg 1159SB30189 REV. C tine CORR0SIO,YREPAIR/BALLAST net., CONT. SUR', ELEVATOR signed by S ts DER John G. Wilda, Desigraten Nimiba : Refer to the following FAA Acceptable Data: FAR 43 Appendix AiFAR 91417 (bk GAC G-IV Mainteninie Memel {hung tataim Revision 16-1. dated 30 March 1992; GAC G-IV M/M Vol. 1;REVISION 16 dated 6 DECEMBER 1591; GAC Production Dwg. I 159r-S20434, titled SP:NOME CONTROL SURF-ELEVSTA 1100 to 165t78LE e l & 2 of 2, REV 0 deed 12-10-91; and akc Production Dwg I 1-59CS20443, tided BA/7-ATINS72. CONTROL SURFACE- HZVATOR. eh I &2 of 2 REV F dated 10/21418. The petit of this repair is to inspect the and remove any onaoson that has pruned on this airmails elevator control surface in the inn where the den=ballast weights me attached. This inspectenheair involves: A. The removal of the le and right devators from the *Safe B. The removal of the leading edge riveted alit to pin access to the ballet weight assembbes and idiots Mutant; G Idatifying the beast mania removing the What weights andinspecting *weights end enacting hardware for comnion; D. Inspecting the balance beam assemblies for OXIDTIOEL E. If cat is found, the removal. peponten and/or treatment of the affected areas; and F. The proper re-staanbly, balancing, sad seemed of the elevator control surfaces to the aircraft . • In =ado= with the GAC Comp sued Mentenmce Program (CND" cedes 273007 and 273008 removed left and tight eievators from the Matt Removed the leading edge skins of both elevaion. Identified all ballast wages fa popes reasaanbly, removed the ballast wages, and pined areas to the balance beam assaults. Perform= ramectice oftodi elevator assemblies and attaching parrs in *accedence with the above referred to GAC Repair Dwg The inspection reveled centre., aim and cad olotint wet not intact on both elevators • Perforned CORROSION REPAIR PROCEDURES FOR LEFF AND RKBIT ELEVATOR LFADLNG EDGE ASSEMBLIES it accordance with the above referred to GAC Repair Drs. Note: NO interim rework was pestered. Re-assembled the Sad elaator ballast weights in their anginal paell' using new hardware purcbased fuze GAC in accordance with above mimed to GAC Production Dwg. detailing BALLOT (WEIGH?) MIL CONTROL SUREACEBLEVATCR. In accordance with the above referred to GAC Production Dwg. detailing SIGNMTh ends original =dile edge skin (which ms within let) after popes preparation and tearment Treated, seabed.Primed andPanced to match ell ewe metal In scieadance widiebeGAC MINT ATA 27.0 Right Control Systems balanced both dentin (LH elevator 0.0 inea. NOSE HEAVY and RH elevator 0.0 in/lbs. NOSE HEAVY) In accrete= with GAC OAP codes 273007 and 273008 re-installed the let and right devotees to they proper positions on the Aiwa Perfomsed den= credrel tenet check in accordeice with GAC CLIP code 273005 and palmed gust lock system function test in accattmee with GAC Cie code 277015. The Mere was not test flown became it was determined that the repair this we dale did not chorine the gee chenconistics or substantially aired the thght operation of the anent This detention included, but was not firmed to, conederation that the elevator atemblYs weight. balance, shape, strength a engine type =Sat deep was not charged Recorded compliance with this FAA form 337 in the eradts maintmance meads and reamed the tart flight status. No threes to the Suits wage 'rebalance reseed from this repair. TA.€0•PoIAI TAAAAAA b. Prnrod by swiss Deny tag gppwn.nk OM NA cirattLONSIOA0790110-DOC NO ADDITIONAL SEMI AS! ATTACHED "MA 0 Additions/ 9seet Are Anschon1 SDNY GM_02754214 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241136 EFTA01326729 I RIEVATcri 'MI78117/92. ![.. cm, •• unarm • MAJOR REPAIR AND ALTERATION For FAA Vag)* oz. Denim ' (Airframe, Powerplant, Propeller, or Appliance) OIS•4 Iseediteacs doweiemo t •••• 6714 - Erie asid•• w sawwwi INSTRUCTORS. Print oc type m entries. See FM 43.9. FM 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for irdstrual005 and disposition of this form. This upon is required by law (49 U.S.C. 14211. Failure to report can musk in a dull MANN not to exceed 51.000 for each such volition (Section 901 Federal Aviation Act of 19591. Make Model ' I nog Gulfstalas Aerospace ei-W Said No. Naafis/Sy and Registration Mat . 1085 MICA NI= (As down on revere= waffle) Address (As shown on reyestrytion ontinars) .2_ Owner B A Leasing &Capital Corp. • Two Etabareasitro Center Sea Presidio; Ca 74111 3. Far FAA Use Duly • • 4.:US Ideallieseke - I TIP, Urea Make Model I Sail No. . Rya Altimeion . t •• Airframe (As dumbed in Solids:we) ••••••••"•••• **** X ToNerptint ' Propellor ' TYRF Applierce Menabansw • ,_ C. Comfanoltr S- A. Afgatiline and Addran B. Kind of Agway C. Ceetlicets No. LANCE A:MATTESON X U.S. Certificated Mechanic . /56OE. SAN FELIPE DRIVE . • Fon,* Certificated Mamie AP lart4049 . SCOTTSDALE, AZ SS= Cathode! Repair Sega= Menthe= - D. I eatify tha the rep ir auVor Mentixt made to the wa(e) identified in ilia 4 lave and 6ineribed on its inert or Mschinsall halo have bom Male ta exordsoce with the require:0am of Pot 43 of the US. F Atm end this the informsion famished hetein is erne and comet to the bear. my knowledge. Dale Signal= o t Asoroval kw Retro (*Swam Parma to die Mb:City Own pawns speeded below. the exec identified in item 4 wet imposed in the larAtlf prteoSsel by dm . Adminatneor of the Federel Aviaioo Adnunierrawn end is I APPROVED CI REJECTED FAA Ft fwd.* MantIfiCtuter x blipedn Althodaliati Odes (Specify) ' ' BY Isq•cras • FAA Dawn Repair Stake Fano Approved by Tempo Gouda Airercohinea Group ' • Date' f Approval or Reaction coats.iv Signinue of D•dpidc•N• 2 -9--9 SIMIAN IA Michael Death /AA FernISTIOS-931 • • • SDNY GM 02754275 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241137 EFTA01326730 }c" rA E NC IoP. AFT V .E DC A]; T F.I 17 1, 2.. . j r: - . . • ___ NOTICE Weigh and ISilanee or operating turatabon theists shall be enterod Si the appropriate aircraft record. An skerabon net be comp:Wilk with ad pmious she:Mons to assum continued °andante/5r with the applicable airworthiness requirements. t Daserlptlee el Work Atebenplisbed (If mom ry s s molted. mach additional ahem. Identity welt mend rwionassy and rouration mark and Wu work completed.) lime 23, 1992, Guffstream Aerospace Corporation PAC) Model C-IV, SIN 1085, /488GA, FAA Type Certificate Data Sheet Al2EA- R.cfcr to: GAC FAA Approved Aircraft Service Change MSC) Number 175 A, SUBJECT: POWER PLANT (AM 71) ADDITION Of FIRE ;Nap PO ACCESS DOOR HINGES, dated: .kPRIL 10, 1993 The pinyon of this service change is to improve the Sr resistance of the engine component access doors . located on the engine cowling, "Ibis alteration replaces one aluminum hinge assembly, attaching engine component access doors to engine cowling. with a stainless steel assembly. This change in conjunction with \ the two existing fireproof latches, wit provide a sturdy three point support for the engine component access doors should the remaining aluminum hinge bum through. The purpose for this revision to ASC 175 is to update the hardware Cams( on Figure 1 and change the location of the 1159P41270-25 and -26 hinge halves on Figures I and 2. It also updates the ton on Pages 2 through 4. Performed all of the MODIFICATION INSTRUCTONS listed in the ASC 175A for aircraft 1000-1137. All Stalled parts were purchased in Kit Form from GAC Product Support Savannah, Ga. 31401 Returned the acraft to flight status and recorded compliance with this FAA Form 337 in the aircraft's maintenance records. Filled out the ASC 175 A complinc card and returned it to Gulfstream Aerospace Corporation. There was no change to the electrical load analysis data. The effect of this change on the aim-rafts weight and balance data is wait ma commuter $ennaor form w does on OPINalleit. bath; WORD ZR Mod lb CflASC1/51..doc pawed by Modal Downy. NO ADDITIONAL SHEETS ARE ATTACHED. °ENV - O Additional Sheets Ate Attached I IllbodelPnisseovan- - :••-•T w`-'1W:71-trit,1*, SONY GM_02754216 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241138 EFTA01326731 ILi• FAA AlPgtA. Tr AELI T T. : 2 /91 8117j i on", nhao Ng . • MAJOR REPAIR AND ALTERATION if IAA Or Oily € en. Oran:ant du (Airframe, Powerplant. Prophet, or Appliance) snanine.. Ci llt - DO INSTRUCT/OHS: print or type all entries. Sae FM 43.9. FM 43 Appendix 9. and AC 43.94 (or subsequent revision thereof/kr instructions and disposition of fhb form. This report Is required by law (49 U.S.0 1421). Failure to report ran result in a chit penalty not to need 54000 for each such violation Genoa 901 Federal Aviation Act of 19S0. • Make . . . Model I. Aircraft OW&main Aerospace G-IV Soil No. Nationality end Registration Mark DOSS.: i . N8SGA Name (As shown on repentionatIllfinta) AMP=(As duns sw. repaired= webs) 2. Owner B A Leasing &Capital Corp. Two Embircadero Cater -' Sao Francisco, Ca 94111 1 For FAA Use Ooh • • 4. thdlIdinstMeallan t TYPO Unit Make J Model I - Se:1Mo. %ma AMISS Airframe (As desenbed in Ran I shovel 77-7"nr•••••••••• a ., . Powerplant n — _ . I Propelier .. I ITN .. •• . Aptatianoc .. . A Ormferadtv Stamm & Althen Naas md Addles LANCE A. MATTESON ' - OM E. SAN FELIPE DRIVE SCOTTSDALE, AZ 152.51 - B. Kind of Mery • X U.S. Cannata Mechanic Foreign Conflated Mechanic Certificated Repair Stanon I Manufienzer C. Cordes No. AP 1144049 . ' 1 a I catty that the repel nutty Litton made Co the muds) idantdied u nem 4 above and described on the mans or such:nes hereto have beat made m accordance with is rommeaems ofPan 4) ofMe ti.S. Fettle* minim 4ultw ad tha the intonation furniahad henan a woe and cornett/add ben ci, my imowle Dare Signature of L-45- rz__ 1 T. Antos/ fee Res* to Sevin Mosowa to the audio* given poem specified below. the us Weeded in itan 4 was impend in the at pmcdtelby the Adminintnix °film Federal AVILOIT Admirtionnon and is T APPRONTD El REJECTED . FAA Ill Sam* Manufacturer • ! i : Manton Andiontaion 01. 440 1POMYY • BY lawn' ! . FAA Despeo I Reps Banal I Person Approved by Transport : Canakb Aineonitineas Dote ofApproval or Rejection I cenliamw pawn wo. 7 -7 -92- i s:67.5494u Miebad Dorm* eityYeeplinteeteseA71:=0.A4aPA"•;eat 2Mortedatili tlhTe.;i SONY GM 02754217 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241139 EFTA01326732 IFF7997:7:17:71, -7•••• rte.- - — t Description of Work Accomplished Of MM. s. la required. wtach. Wino:Cud ghee. Wealdy with wash ruccrishry mid regtanon mast sod dat week comps]) lime 23, 1992, Gulfstream Aerospace Corporation (GACI Model G-IV, SIN 1085, NSSGA, FAA Type. Certificate Data Sheet Al2EA: - • Refer to: GAC FAA Appftved Aircraft Service Change (ASC} Number 175, SUZUECT: POWER PLANT (4TA 71) ADDITION OF FIRE SHIELD TO ACCESS DOOR HINGES, dated NOVEMBER 151 1991. The purpose of this change is to ®paw the fire resistmee of the engine component mass doors located on the engine cowlingg. This change replaces one aluminum hinge assembly, attaching engine component access doors to engine cowling with a stainless dal assembly. This change, in conjunction with the two existing fireproof latches, will provide a sturdy three point support for the engine component access doors should the remaining aluminum hinge burn through. Prepared the aircraft for safe maintenance and pertained all of the MODIFICATION INSTRUCTIONS fisted in the ASC 175 on the above listed aircraft All installed parts were purchased in Kit Form from GAC Product Support Savninah. Ga. 31402. • - „ ---• —• •••— — SDNY_GM_02754218 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241140 EFTA01326733 • o REGISTRY CAMERA NO. j DATE: 7.-43^9a Amer.: amm ZID=5 "Brix* UN ORO - . MAJOR REPAIR AND ALTERATION el- slew to Appliance) sloes (Airframe, Powcrpbat, Propeller, or "- se rataI a.sem i1/41•10110•• 43.9. FAR 43 Appendix 8. and AC 1 211(fr cb( '- ' ":5°P° subsequent revision Llano° for INSTRUCTIONS: Mot of Tyra all entries. See FARreport repels can naSuk In a civil is required try las (49 U C 14 1 allon to Inatnfolora and diSpraicIon of thks fomi. This viola/Jon /Section 901 Federal Aviation Art of 19581 A00 for each such Wan not co exceed 11 Mat Mike -GIV I. Aireaft Gtestr eatii Anne , Netionnlity end Registration Mick r SailNo. NSSGA I885 n oblate ) Address (As tan on repstretica eaftillcale) Name (As ibmemoa resimmtio Two Ensenada. Cater 2. Owner B A Leasing &Capital Corp. Sem Entedeco, a 91111 3. Per FAA 1. se Only 1 S. TM. 4. Unit lamellate Notion Unit Make I Model 1 Seel No. Rot •• I (As desated in[enlace) ••••••• Anframe Powerplant Proyelter TYPI Appliance .— _ i 4. Owtherstie Smatte r C Cease Na ' B. KM orMete A- Mori time al Mem U.S. Cali oted Mabee LANCE A. MATTESON X I 7 c AP 1$6•4049 WO E. SAN FY-LIPE DP3In FatinCathode Niceherti Canie' Rpm Stetson sCOMDALE, AZ U2 Manufactura dente on the tome or mactentota to the nee) knife inkese e Mee od D. 1 cal* Na Oa I WS See ention meek of Peet 0 cite U.S.F kisiionRepletion. arsi Ms the intent= the requireme nts hereto have bookmade in meordetese Ma 44 1 . o my knowtedm farnisle heel is tem te aana to the bet Signettre f De S h; 1e- 7. Amwerral ter Rein O. Sonia ' OMmamer presaileed by the Wow. the unit identifiedin item I eaheed Pursuit to the cabocity siren parsons specified APPROV ED 0 REJECT ED Adenine= and in CM Athena of the Federal At hopecion Mehrehation . Other (Spacity) PAMIR Image /*antam= i Iwomet . BY Peon *Wee by TattOxi FAA•Dmisme Rape Oise --51 Omani Airmathinim Group engem or Signature of/gyp/gyp nddvi Demo Amoral or Rejection .10esipsdaaNt 5247•304 IA ' . Maw/ Donnelly 51 i i if z__ IAA lwt 137(0s-el) . - • - . . •• • . • . SONY GM 02754219 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024/ 141 EFTA01326734 FAA A1RCRAFT REGISTRY CAMERA E0.31.4 DATE: 7 -a3-qa NOTICE Waght and balance or °pawing limitation changes shall be entered in the appropriate thrash record An aeration must or romped* with all previous &cations to rinse contirmed conformity with the applicable airworthiness requiremaus. Description of WoricAccomplbbed Ornate trace u mired, mach addmorwl Meow Mem* was matt reoccubly and registrar= rust rd das work completed) May 28, 1992, Gulfstrcain Aerospace Corporation {GAC) Model GdV, SIN 1085, NSSGA, FAA Type Certificate Data Sheet Al2EA. Refer to: GAC FAA Approved Aircraft Service Change (ASC) Number 187, SUBJECT: ICE AND RAIN (ATA 30) P1TOT HEAT ADICATION - 31ODIFICA77ON., dated AUGUST 3, 1991. The purpose of this change is to provide annunciation for the pilot heat system which will better reflect when power is applied to the haunt. Presently, it is possible to ept at OFF light in the picot heat system when one of the heaters is not working and one is working. This ASC wig eliminate the misleading indication. This change reroutes wiring in the relay and junction paned (326A1) and will require approximately 15 man-hours to complete on the above listed aircraft. Performed all of the MODIFICATION INSTRUCTIONS listed in the ASC 187 for aircraft 1001, 1006- 1143. Note: removed the 326A1 panel from thuairaaft to do the modification. Noted the following errors in ASC 187: Wire Number F217A20 should be removed from De stsch Ground Terminal Block ¶24-B* and discarded and Page 7, Figure 3, Triangle 2 should read "ACFT G-IV S/N 1001, 1006.1143' instead of 'ACFT G-IV S/N 1001, 1006-1043'. Note: it was not necasary to use the wire number F214A20 or the OAS805A3 Splice to extend the existing wire. • All Stalled pas were purchased in Kit Form from GAC Product Support Savannah, Ga. 31402. Performed Operational Test in accordance with ASC test procedures paragraph F all pans and noted no abnormal operation. Returned the aircraft to flight status and recorded compliance with this FAA Form 337 in the aircraft's maintenance records. The effect of this change on the aircraft's electrical load analysis data is negligible. The effect of this change on the aircsafrs weight and balance data is I:eery/Mc. This computer gsnenaor to win dons on gPfb08016: miss WOW lac EMS m CAASCIttdon prspad by htszhael DormeBy. NO ADDITIONAL SHEETS ARE ATTACHED. *DID* C Additional Sheets Are Attacked • I • • • - ••I SDNY GM 02754220 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241142 EFTA01326735 FAA AIRCIAPT. RECTSPRT CARRRA 20 An' 7-as-9 FOrm Approvtd -- • OW No. 2120-0320 MAJOR REPAIR AND ALTERATION For CAA Use Only utoccreft. a Vensosnmen (Airframe, POMONTIlarlt, Propeller, Or Appliance) ' arepicatlog.. aigliniimmo. - -s- ,>-) 4- I A- Arbemerso . . ..... B.IndAC43.9:1 fOreolsemittent reTfefenihere*BN4 Inetnlebone INSTRUCTIONS: Print ortype all entree SeeFARCEI.FAR 43APPendlz (401.1.S.C.1421).F ellunobareplet CanMull in &ChM penalty none weed St.003 and Opposition of Pus form. This repents fequIred by taw Act of 19663 for eachasiCh violetiOn ISection 901 Fedor& Amgen • Make GULFSTREAM AEROSPACE MOW G-IV I. Afrereft 4 Nahonakty waren Mark Renal No. loss Addiees (As shown on regdfrafhan 40bl'asfe) Name fAS shown on sestisirstkon ceMbeeffl • BA LEASING & CAPITAL CORP TWO EMBARCADERO CENTER 2. Owner $AN FRANCISCO, CA 94111 . 1. Fee FAA Use Only • 4. Unit Identatcatfon E- Type Una Mane i model I 5.1,51 NO Reim" Allefabon /As Pe <va t labs I Y XX AIRFRAME POWERPLANT PROPELLER Type APPLIANCE Manufalswer • ' S. Cenionelty gleeestiont tv • 6 Kind oe Agency C. CertItIcalle NO. A *genera Name end Address U.S. CNINCSOUOCINnoi LANCE A. MATTISON . formptCortscatal mammas , - .1411 1864049 8560 EAST SAN FELIPE DRIVE Conan:me ReerStahon SCOTTSDALE. AZ 85258 . Inool.if hoot ' a above and drartbed anthem...armor Attachments Wee D I certify oral the repair endAralteratton made to Me un HQ. earned Molten federal AviSSOA Regulations end that the information hare been made in ageOrciance wen me requirements of PIO 43 of the U.S. furnished he 4 trot and correct its the Deal of my nootedge. Signature of Au heft Inchvalc a_ . Date 3 .4 4 —re...._ —/C4 • • ' . Approval log Return To &NUM . • persons speed*, Dam. Merit q•nbffed in dem A wet oUPOCIO0 Ifithe mina, prescribed by Ibe Pursuant 10 me authority given ACInonottfll0f of the Federal Aviation AOTiroMfIlliOn and it e APPROVED 0 REJECTED Other CS:Meer) BY l FAA Al. Slandards InspKior Itifanulacturer . •X Impeehon Authorization OVIOO OOPIOVNI by Transport • i FAA Designee I Roper Smoon . , Canada Antennae= Gr o I CANUICalto Of Stratum of Ind I , DIII•01AppflowidOnlyeCtOn • Designation No 5267054941A MICHAEL DONNELLY i 5 /14 4 f e- FAA Form 037...... VIZAWFV2aivettags;il; SONY GM - 02754221 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241143 EFTA01326736 PAA AIRCRAFT REGISTRY CAMERA NO. -Si DATE: 7 -a3 -ega NOTICE Weight endbalance or operating limitalionthanges shad beenleredIn the aPPrOPriale aircraft record. An alterttion risat be compatible with all previous alterations to assure continued conformity with the, applicable airworthiness requirements. Deees.pUeo a Mat A.ccOingiahed ' at mom , P, C11 is required. MICA eristitionei sheets. Identify with small nalionanty and registration mot and date rent cOMMIS.1 . May II,1991. Gulfstrtarn Aerospace Corp. Model G•IV. SIN 1085. MUG& FAA Type Cad:Scats Data Sheet Al2EA. Refer to: Gulfstream Aeritspacc Corporation FAA Approved Aircraft Sat Change Number 157 SUBJECT: FIRE PROTECTION (ATA 26) SMOKE EVACUATION VALVE INSTALLATION - • BAGGAGE COMPARTMENT, dated March 27, 1992; Gulfstream Aerospace Corporation FAA Approved Aircraft Flight Manual Supplement 89-03 Rev B 16 January 1991; and FAR 25.857 (b). The purpose of ibis change is to install a system designed to assist in smoke and fume evacuation from the , baggage compartment aft lavatory and aft galley areas. The system allows the baggage door seal to be deflated and allows cabin pressure to evacuate smoke overboard past the seaL A two position manual selector valve is Stalled above the cabin entrance to the baggage compartment. The valve positions are • labeled EVAC SMOKE (deflates the door seal) and NORMAL OPS (normal control of door seal) An access panel will need to be designed on installation to match cabin interior. This panel should be' designed so it cannot be closed when valve is not in the NORMAL OPS position . , Performed all of the applicable effecfrvity installation instructions detailed in the above referred to ASC 94 installation instructions. Fabricated SMOKE EVACUATION VALVE access panel cover to match existing interior scheme and so that it cannot be installed when the valve is not in the NORMAL OPS position. Performed installation check out by complying with ASC 357, paragraph C, Perform installation check- out as follows: all steps. Verified that the aircraft's flight manual has the above referred to flight manual supplement Stalled that details specific EMERGENCY PROCEDURES dealing with SMOKE AND FUMES EVACUATION and SMOKE IN BAGGAGE COMPARTMENT, AFT GALLEY OR LAVATORY. Recorded compliance with this FAA fonn 337 in the aircraft's maintenance records, antretumed the aircraft to flight status with SMOLT EVACUATION VALVF. in the NORMAL OPS position and the access cover installed. ft has been determined that the interrelationship between this change and any previously approved modification will introduce no adverse effect upon the airworthiness of the aircraft. This determination includes, but is not limited to, consideration that the cockpit procedural changes arc included in Inc - aircraft's FAA approved aircraft flight manual. No changes to the aircraft's electrical load analysis or aimraft's weight and balance report were required as a result of this modification. pfisIZA/SCe WORD ell CIASCI b7.dac. prepind by: 311ctel Doetily. NO ADDITIONAL Slare ARE ATTACHED. '72,1r O indilparial Sneels Are Attached •U see 1Del-C.44.1%11 •-• ..... • - SDNY GM 02754222 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0(1241144 EFTA01326737 callmiCem-wpworar FortetApprovod _": "' OMB No4124020 t- 0 MAJOR REPAIR AND ALTERATION Deounee Poe FPA Ueet tirdy us crewman:nu (Airframe, Powerplant, Propeller, or Appliance) resew Dwane, 0ariltentircatkut 1 az. -}st)o INSTRUCTIONS:PAMor typfaii entnes.See FAR43.9.FAR 43 ADO•nditt B. and AC 43.9-1fOttubsecluatra feeniOnl‘feOR inf insinfain sad dispotation clot form.TNaseport is requited bylaw (49U.S.C.1421). Failure to Japan can redone Advil wally nOI tendedEl.000 tor each such violation fSecti t Federal Aviation Act of Ma). AEROSPACE tac4/4 -GIV . Mak, GULFS 1. Alactift _.... Seri& •No. Nationality and Registration Mart 1085 1, A • , N88GA NOW (As shOwn On feetstraMt Centaca40) Adana= (AS shown on repisoolion coadielOW 2. oilleet . &Ain& & CAPITAL CORP. ` TWO EMEAFtCADERO CENTER -- SAN FRANCISCO, CA 94111 - '. N. • •• ‘ - a: For FAA Use OW/ - / i r A • - 4. Unit Identiricabon E. Type Unit • Mate MOCIel . Serial No. Regale Attomoon AIRFRAME i 0 towel XX POWERPLANT PROPELLER Type APPLANCE leanufaCtunof I . I . IL Conformity Stateroom' -. A. Agency's Hama and Address 8 Kind ad Agency " I C. Certificate No. U S °initiated Medstme LANCE A. MATTESON Soften (.'olaCatea mamma 8560 EAST SAN FELIPE DRIVE ! I Condeams Rene Simon AP 1864049 • RflITTST)Al IF A7 tic7 AR I I manutenutee • . 0. i heath" IPPON wad anOtor auenthon made To the wets) 'annul:HI in nom 4 atroveand °ascribed on tfie revene of attatnin•Alahatel0 have been made in accoreance with the movements or Pen13 of me Y.S. Federal Aviation Regulation, and that DM information .. furnished herein is live and carted to t tend 01my ancsiodge. Date i Stratus/ ot Aum indm,S • .. I • ..e r-e•e'f . 7--.. F. Approve. toe Iheiton TO Sanaa - Pu suam to tne authority give persons specified below. thejel identified in item 4 was inspected et me manner presctibsd by Me Aorrosostrator of Ine •Federat Aviation AdmomstraliOn and is A APPROVED CI REJECTED ' ' FAA Fie Standar:IS Other iSooe•Pn — Manufacturer' . X InSpeCtiOn AWN:tea:4n InSPector . BY • FAA Designee Repko Station r i Person Approved by TransoOn I Canada Aneonhautes Geo Date of Approval ot &Poulton Censticalece.. ' -•.• ' - Signatuted1Se Designation No. -47;57fr ia 5267•54941A _MICHAEL DONNELLY FAA Foam 337 to aft ar:fesinar-Z - -4014a4. SONY GM_02754223 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241 145 EFTA01326738 TIMA AIRCRAFT I STRY cAr. so. I Ai Mtn: 6* -OO-sAti NOTICE Weight and balance or operieng limitation changes shall be enteredin toe appropriate aircraft record. Analterationmuffed Compatible with all previous alterations to assure continued conformity with the applicable aliwOnhiness requirements. De•Cripti0n el Wort Accompliahed (if trent space if retorted. altaell eddittOnat aneete identity with *meta nationality and registration mei, and deft wore contoarecH May 14. (Mfg:ream Aerospace Corp. Model G-IV, 544 1085 8188GA. FAA Type Certificate Data Shed Al Va. Refer to: Gulfstream Aerospace Corporation FAA Approved Aircraft Service. Change Number 94 SUBJECT: FLIGHT CONTROLS (ATA 27) GROUND SPOILER FAULT DETECTION FUNCTION TEST - MODIFICATION, dated July 31, 1991. The purpose of this change is to eliminate removing the interior to gain access to the relay and junction boxes in order to perform the required tests during the 18 month inspection. This is accomplished by relocating the Ground Spoiler test plugs from the relay and junction box to the left hand avionics shelf. Added jumper connectors will simulate relay removal required dining Fault Detection tests. Performed all of the applicable effectiviri instal/anon instructions detailed in the above referred to ASC 94 installation instructions. This change adds 4 test plugs on the top left hand avionics shelf and modifies associated wiring. The installation required approximately 69 man hours to complete. Replaced connectors 07L2P1 and 07L2P2 with new .Acro Electric P/N AE559L10SL3S-B connectors. Noted the following errors in the installation instructions: Step E, Page 5. ASC94K901B and ASC94K902B should read ASC94P90113 and ASC94P902B; Step E. Page 6, ASC94K903B should read ASC94P903B: Parts Required. Page 6. item GAC800PT18-32PN Plug CHECK delete the word CHECK: item GAC800PT18-32SN is not required; Figure 5, Page 12, Wire O165O20 wasiis connected between TJIT-D: Figure 7, Page 14. Wire G173A20 vtavis connected to 1121J-F nein though effectivity is listed for 1096-subq., Wife WI43G20 connects to TJ4U-K even though effectivity is listed for 1096- subq., Wire G I 88C22. wavis G 188C20. • Performed installation check out by complying with Gulfstrerin Aerospace GIV Computerized Code Maintenance Program Code 276004. Ground Spoiler Fault Detection System - Ftfilictional Test and 276001 Ground Spoiler System - Functional Test and noted no abnormal operation. Note: Disconnecting ASC94P901B is the same as removing NUTCRACKER RELAY It: Disconnecting ASC94P902B is the same as removing NUTCRACKER RELAY 46; Disconnecting ASC94P903B is the as same as removing POWER LEVER IDLE RELAY #7.; and ASC94.160B has the same jumper points 325A1J60. Recorded compliance with this FAA form 337 in the aircraft's mairiumance records. and returned the aircraft to flight status with ASC94P901B. ASC94P902B. and ASC94P903B connectors installed. It has been determined that the interrelationship between this change and any previously approved modification will introduce no adverse effect upon the airworthiness of the aircraft This determination includes, but is not liMited to. consideration that there wit be no cockpit procedural changes and the modification is not related to any safety or aisworthiniss condition. No changes to the aircraft's electrical load analysis or aircraft's. weight and balance report were requited as a result of this modification. ATTACHED. t%O• pS iwse. W0Ill) in CSASC94 dot papered brIdatielDaly. IC ADDITIONAL SHEETS AM a Adla'anal Sheets Aol ATIKNO nlsesa) n, C: .4 SDNY_GM_02754224 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241 146 EFTA01326739 FAA AIRCRAFT REGISTRY CAMERA NO. 3 DATE: 3 - 20 - 12. i 1/2 /01€41P' 0 20-0020 Mearnenen cslomooren MAJOR REPAIR AND ALTERATION ""."-I (Airframe, Porverplant, Propellei,eir Appliance; 0 e.c.12 JAN 3v."' I rwiftn°1113APP473 21 For FAA Use Orta/ ' aimItTAWorn • - --• — .. - - - • ' - • ' •-• Office Identificatice • / VNY FSDO 11-O -0 ' INSTRUCTIONS:Print or type all tedriesSee FAR 439.FARCIAOpendix Band AC 43.9-1 (or subsechsent revisionthereof) for inslifictIon$ and dittaMitiOn Of MIS bon. WM MOOR Mier:wired by law fitilU.S.C. 1421). Farldreto repartees result i acne conaltynot tattooed SISOO for each such violation (Section WI federal Aviation Act of ISSIO Make Goirstream . Model Mmpr et • Crlir I. Alma Sena! No. adendlity and Rearadon ark LOSS . MEGA Name (43 shown on norstrorion corriAcirl) -. raficlrele (As strewn on registration aridirata) 2. Owner BA Laskin ad CROW Corp ' : TooEsibenalsro Cabe as lbsodue, CA MILL ...r.c . 3:Fee FAA the Oak ... - 4. Unit karma:Won S. Type Unit Make Model Serial No. Repair 'Alleration .--..-. AIRFRAME awr.rwiwerre~wwwweat dintweedMO•nr) abort/ x .• POWERFLANT PROPELLER . I Type m APPLIANCE li Manufacturer ' rir • • ILICanteivelly Saran A. Agency's N Me and Address i b. bind ol A$14aCY . C. Cerra-cam No. :Western Commaarkf, la lit w? sal Lidos.* . • RA311801LAbtrae 3,4 1000 Dally_Drive Faeign ta.rals muse R•49 1, 2 & 3 Van Num CA 9140f e r m,t, ' . X Cortir,unto RePalir Slaw . Instrument & Menducwrot D. I certify that me repair and/or anerationjnade to rap in Iii) identified Marne above and described on the reverse or anachmenu hereto have been made In sccordancerth the requirements of PIS 43 of its U.S. Federal Aviation Reputations and that me inforinction tumished herein is true and correct Wine best of my ItnowMge. Dee Signature MAuthorized Indivirloal Jitabsiy 27, 1992 .../....e,...-".41 ' Amen& ler bewn.7. &woo, Pompano the authority sea persons specified below. TM um titled in item 4 was Inspected In the rmnmr prIP0100.1 by pre. ACIMillilltalOf of the Federal Aviation Adsninistration IllIbri : APPROVED 0 REJECTED FAA Fit Stewards Olher(SPNWY) • i leepeetor klamtleauter Riga:ration Authorlution 10 • - Ftson Approved by Transport r '. 0•119.164 X Repair Station. CartadaproortlWeal Group Date of Approve) orRejection 'JAN 2 7 I99/ - FAA Penn 332 male onottutioa yr...°.4Hiosth=€(.........4 Cerfificele or SONY_GM_02754225 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0O241147 EFTA01326740 I FAA AIRCRAFT REGISTRY CAMERA NO. 3 DATE: 3-20-42 NOTICE alterationmust be Weight and balance or opirating limitation changes shell beintonedin Me apprOprialiabate record. An airworthiness requirements. compatible with all ruinous alterations to assure continued conlormity with the applicable DmicripliOn el Wort Accomplished registration male and date work completed.) (It mote space is required. attach additional shags. Identify with Winn nationality snit Honeywell Traffic Men and Collision Avoidance System (TCAS II), as previously ' installed with minor deviations to Gulfstream Aerospace provisional Supplemental Type Certificate #5A30335O issued December 6, 1991, has been FAA Approved for placement into service by authority of Gulfstream Aerospace Corporation Sit 0SA3033S0, emended on January 17, 1991 Reference FAA Form 337 dated December 12, 1991, covering the provisional installations. • The TCAS Receiver/Transmitter unit has been installed into its mounting rack, the circuit breaker previously pulled and locked out has been activated and the placard installed adjacent to the TCAS control stating: 'TCAS INOP PENDING STC APPROVAL- has been removed. va Gylfstream Aerospace Ground Test Plan/ReponittSC41 129602 for Honeywell (TCAS) Systems has been accomplished to verily the installation and operation of tee systems as installed in this aircraft; test results have been recorded and are on file with this facility. FAA Approved Airplane Flight Manual Supplement, GAC Document ftSC41 129M0Z dated January 14, 1992 and FAA Approved on January 17, 1992, is required for this alteration and has been provided. The effects to the aircraft's basic weight and balance has been calculated to reflect the above mentioned alterations. The aircraft equipment list has been amended to reflect the new or modified equipment installed. The installation as described, 'tuts been found to be in conformity with the above mentioned approved data and continues to meet the airworthiness criteria under which it was originally certificated. G Mallon' Sheen itie Attached a gerfirgr ia % SDNY G0.4_02754n6 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 11 48 EFTA01326741 FAA AIRCRAFT REGISTRY t .11 CAMERA 13 Oa/ • R .DATE: 1 - 24 - 92 . • Fain Approves I 0 OMB N027200030 ' MAJOR REPAIR AND ALTERATION FOEFAA Use 0* us ceormart elaaarerce . (Airframe, Powetplartl, Propeller, or Appliance) OfficeAdondfloation Aidnimesten ildemiseem • .1A7(4)0 0 - -1 INSTRUCTIONS: Print or type ill.I etudes. See FAR43.9. FAR 43 ApoentaA B. and AC 4S9.1iorsuesememmespenalty iontlamit08 torIntuitions not to exceed $1.000 and dispositionphis torn. Trim tenonis rernared bylaw Ng %M.O. 1421). Fs lure lo reponcen result In • civil for each such notation (Section 901 Federal Aviation Mt of a63). Make • • IMMO Galfstrem, Amnion ' G-TV I. Allaret Nationality inc Regissazion lash INS NMIGA -• Address (AS shown on regatretiOnartilicaln 1.42". S4 shown on neiartirlon certiticner Mlewin sod Capital Ceres Toro Embercedmo Cater 2, Owner Sea Francisco, CA 94111 . 3. F.r IAA Doe One/ • 4. Un4I lOwaltIcalkm4 - I Type • Model SerldNo. Repair Alteration Unit Usk* • AlAFAAME • (As Oncelb40 In lam f4above) X .-- . ... V *. pov.-F.apuor .1 • - . .'! - PROPELLER Type • minus._ - • . . •... MrelJARCE A. Annoys N ma and Address ii.f CattfornWly Slalegawd 8. 10M 0 Agency , i C. Cerr:ficste No. . Western Caamancler, Inc. - t us c.,14,:aue wer..4 ' RA3R8MILAistreele 3,4 16300 Nib Drift Cotton Gnaws,Mechanic Sadao r 2 & 3 914% - II— Melted Peerractefleti • Van MOIR CA Cethicate n.,44 Via • Insinuerat & Manutectie• reverse or ameninentspereto D. I certify that die repair and/or eiwauonmade t6 the uo t(f) IdentifiedInitemI above and described On Me WO that the IntormetiOn neat been matte in accordance with the ilollieftenents of Pert M oi tn. U.S. Fan: Aviation Regulations iuMiltiect herein 4 Inn end cane/Ito the test of my nonleclge. ' • Date Signature of Authentic; I I December 12, 1.991 ." A - -7. eamemi lee To lweesta to the authority Inn pentons specified below. tm ani died Nitem 4 will infpnled in the manner prescribed bY the AdlniniltililOt 01 the Primal Aviation Administration and Is APPROVED ID REJECTED . ate (Smarty) FAA Rt. Sier4wds manufainer Inspection Aurnoraman ' Inspector BY FAA (*Knee DatewApp,...,...... XIReoair Stelion Dniotoitiesz ales .. Sep Person Morey*: by TratiOCel Canada Ainimminess GM* Authorized ....e—e.../..., Ir , cO4./._______E, . DEC 1 2 -1991 - • FAA Form 3314ta.set SONY GM_02754227 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241149 EFTA01326742 FAA AIRCRAFT REC,ISTRT CAMERA M0.1 N DATE: - 24 - 92 rylq it y • NOTICE Weight andbalance or operatingIlmita • compatible withIll previous altera tiOn changes Shallbe enteredin the appro • tions to assure continuer/ conformity with priate aircraft record. AnalterationMust be the applicable alnvOrthIness rebuke/hell :S. • I. Description of Work ACcomplished (IImore Viten rebutted. Mats additio nal sheet:rides:11y we/takers!: netionehry ens registration mare and thee work completed.) t. This supersedes that portion of installation . of ap auxiliary radio FAA Form 337 dated September 7, 1989 regarding Systems, Inc. Engineering Report rack in this aircraft per Elsinore Aerospace #1,23. Elsinore Aerospace Systems Report covering:: this installation does #1-23 ieferenceA on the original FAA Form 337 that is installed in this aircraft. not represent the nature of the . actual rack . The auxiliary RAI forward radio the configuration of that found in rack as installed: in this aircraft conforms to Report 1-52 dated 1/18/89, entitled Elsinore Aerospace Systems, Inc. This report has been FAA appr "SUBSTANTIATiON - RH FWD AVIO Engineering NICS RACK". //NM-494, with FAA Forth 8110 oved. by Robert E. Poteet, FAA Structures DER -3 dated 12/05/91. The effects to he aircraft's basic result of this correction to weight and balance has installation in this aircraft. The the records pertaining the no! changed as a above referenced to be in conformity with the abov installation as described, has been found meet the airworthiness criteria e ment ioned approved data and continues to under which it was originally certif icated. END 0 Additional Shot. An MUCHA • 9/1:2Wt-fitittk4rf P:;9k,IP.-L1:. r --t— soNiietvi:02754228 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 I 150 EFTA01326743 • • FAA AIRCRAFT REGISTRY 1 CANTU. N0.1 N DATE: 1 - 24 - 9? 0 in ceornwen MAJOR REPAIR AND ALTERATION Form Approved OAS No. 2120-0030 -. • For FAA Use Only onoscorceo, (Airframe, Powerplant, Propeller, or Appliance) Win Assn ONico Idea,legion OP --r$O4O — / INSTRUCTIONS:Print of type allentnes. See FAR 43.9. FAR 43 Appenclie B. end Aq 43.9-I for subsequent revision thereof) lorlintruclIons and elnipOsition of this tom This report is required by law N9U.&C.14213 Fanureto upon an resultin a civil pepeltynottonceed$1.000 for each such violation (Section 901 Federal AvistIon.Act Of N.M. . Iteke Modal . GuIrstreem Aerospace G-W I. Aircraft Serial NQ. Nationalny and Registration Ma* • DM -PaliCA • Name (Al entown an registration omit/can) Address (As shown on toolstralion cortiticaril) 2. Owner BA Lamle:sad Capital Com. Two Embercedero Crater - Sao Francisco, CA 94111 3. For FAA Us* Only .• 4. Deft IderitIllealon ... S. Type Unit Make Model - BMW No Raper Allsratoon , . . AIRFRAME ' (As daserityrdIn item I 400.) X 0 • P0VAIRLANT' PROPELLER ' • • Type APFINACE ' ' . • te., ManullidluterN • a , t • & Cailorinily Statement - A_ Agency's Name and Address B. Kindof Agency " C. Cenlecate tat.. Wawa temiamoder, Inc. US cemnbased mechanic, ' .. RAIRAPIL Airframe 3,1 11.30D Dab Drive rotor Corlafrated lichank Rae, 1,2 &3 Van Nom reA 91406 • x Cerielkuee Rini, Station umbid P NM, Woulacium •. I Instnuntit & sort • D. I certify that disrepair anatoraiteration made to the woofs) identified in item 4 aboveand described onMe riveral or anachmenu hereto Mill.0111.1 mad in accordance with the requirements of Pan 43 of the U.S. Federal Aviation fliligyiSSOOS Sad that the inlonnation • . e. lumished herein islrue and correct to the pat of my nowledge. ' Date Signature of Authodued Ind I , December I.I. 1991 9 0 .e . • 4 ...C.-. : N 7 Appeal lee To Service Pursuant to the montrity given persons specified below. the uniyidentified in item 4 ins impacted in the 'memf prilted by me Administrator of the Federal Aviation Administration and la e' PROVED 0 REJECTED FAA Fit Standards Other (Specify) IrepaCter Manulactures inspected,' AutnOritatien BY -• FAADemme. X Reedit Station Pawn APOnned by Transport Canada Airworthiness Group °Meer Aeon:welter Repoction Certificate Siguy AuthOsited ty DotignM No. DEC 12 1991 orRRML ..."--e--/-e- Ca' r-"0-4---"-t ll i FAA Fpm 937 Mier 0411: I v*C111Thitridaltan t - ::)_. _..-tlecauc-nt Aft . SDNY GM 02754229 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, -15, and 17 EFFA_00241151 EFTA01326744 FAA AIRCRAFT REGISTRY CAMERA NCI./ Al DATE: ; - - NOTICE Weight andbalance or operating limitation changes shall be 'Metedkith& apptopriamdrerelt neon'. An aeration must be Compatible wills all previous &ifnations to enure continued conformity with the alnanable eirlsOsthinese requirements. S. Description or Wort Accomplished Ili more spies is nausea attach elthoonal swim Identity with aircraft nationality and twastration mum one data work compiesea.) The following structural modification has been incorporated into this aircraft in accordance with data approved by Schwartz EnWreermg Company • 1. 14per L-Band Phone Antenna Installation - WCI Drawing #08068088 Rev. IR, dated 11/15/91. This drawing has been, FAA approved for installation on this aircraft only by Peter A. Schwartz, FAA Structures DER itSW-586, with FAA Form 8110.3 dated 12/11/91. • The aircraft's basic weight and balance has been revised to reflect thcabove listed modification. The work described, has been found to be in conformity with the above mentioned approved data, and continues to meet the airworthiness criteria under which it was originally certificated. Work order 6719, on file at this agency, coven the above described work. END lr • - 0 Additional &loon Ara Attached .1 • SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241152 EFTA01326745 1, !AA AMUSE RECESSES • CAREW 10a N DATE: I - 24 - 92 • • • • RUM No. OMB No. 21204020 • 0 MAJOR REPAIR AND ALTERATION . utoicamarm Fee FAA the Only eamayem, (Airframe, Powerplant, Propeller, or Appliance) meal Idenahcedon Nam amen • • g —eit-eal n -ileiniertakei INSTRUCTIONSPrintor type all trade. Se•FAR43.9. FAR CAppendix Rend ACW3.9-1(orewbse cruent revislonthersoBtor instructions reSult In•chil penalty not tomcod 51.000 and dittIOSItiOn at thiSIOnn. This report Is Noulred byIt. (49 U.S.C.1421). Fa lure so reportcan for each such violation (Section 931 federal Marion Act 611950). • .• Model Make • • ColEstntam Aestepeee - _Swore' 1. Alone Semi NO NetiOneliry and Registration Marl; tring Ka ri tillThe (As shown on argot/40°n conilican) Ad0nms (As shown on togisootion c•rtincals) 2. Owner BA Leasing and Capital Cap.. Two Fdatensdero Cala' To Prendsco, CA 94121 & For FAA Use Only , • • . 4. Unit kamUlicemon . S. Type Model . SOS raj Repair Anitansn Unit Mike . . AIRFRAME wwwhiwmwwwrwwwwwrww.(As dew bed in gent I shove) X - i FlOviERPLANT •• PROPOSER a • . Type h..) APPLIANCE ManuleCturer r" • • :Zs • I Conleetray Stemmed 1r - C. Ceti mate Na A. Agency* Name and Wren a Kind of Aden I U s. geminate, Mae RA3RBOBL Airframe A 4 a lac 16300 Daily Drhe Farago CandtesistiMeniaree Radio I 2 & 3 Van Noy& CA PIS . 1 OrtilimielReps Vaasa Use/Std Instnasent i.4ory • umuracturei hereto 6. i canny Mat therepaireml/oraberation made to led unapt) identified initem 4 above and d•Saibed On the reverse orshachments hive been made in aCCOrdanCe with the requirement& Of Part al of the US. Federal Aviation Regulations and that the Inlonnation furnished herein Is true and correct to the best et my knowledge. Dale Signature of Authonted ineav thkearer 1.2, OK T. Apparel for 7 r..4 TO Sefeloe , fa dun 4 urn inspected in the minces prescribed ay the Pursuant to the evthority given persons specified below. Pie unit IdentIfied In Administrator of the swan Aviation AOrnentratalion end le. 0-SPPROYED 0 REJECTED Other (SpeCdr) FAA Ft Stand*" asnuyacuter . Inspection Aulhodzation Inspector BY Person Approved by Transport FAA Designee - X Repair Mewl Canada Airworthiness Gasp MIN of Approvalor Rejection AS Certinar te Or Signa AuthOrliedr. 04eIgnatiOn NO. ..O--e--<4__ 1 63 ✓4 '‘C.www.-47 DEC 1 2 1991 BRSOBL FAA roan 337 uteri • SDNY GM 0275;3231 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, -15, and 17 EFTA_00241153 EFTA01326746 LI FAA AIRCRAFT REGISTRY CAMERA 140.1 A' DATE: 7 24 9 NOTICE Weight and balanceor operating limitationChangesShall be enteredin theapproprlate aircraft record. An aharationmust be compatible with all wet*: alterations to assure continued conformity with the applicable alnvorthiness requirements. Descriplion of Work Accomplished (II mere spot* is reooked. erten additional Skeels. idennly wen tifdin nellonaUty and registration mark and date work completed.) The following major Gulfstream Aerospace Aircraft Service Change has been incorporated: . ASC #178 - Instruments (ATA 31) Electronic Checklist - Installation NOTE: An airplane change that makes the electronic check-list incompatible with the required crew procedure in a manner that could be hazardously misleading will require the corresponding change to be made to the checklist or the display to be disabled entirely. This determination is to be made by the operator at the time that such changes are incorporated. e Flight Manual Supplement Number GIV-89-03 Revision C has been inserted int6 the current copy of the Airplane Flight Manual to reflect this change. The effects of this change to the aircraft's basic weight and balance and the aircraft's electrical loading is negligible." Work order 6764, on file at this agency, covers the above described work. END CI Adddponal Sheets Are Attached •- SUBJECT TOPROTECTIVE ORDERPARAGRAPHS 7, 8, 9,10,15,and17 SONY GM_02754 . 232 EFTA_00241154 EFTA01326747 FAA AIRCRAFT\FICISTILT $9 .\DATE: / - 24 - 92 CAMERA "Or/ Form App/oved • 0 OMS No. 2120.0020 MAJOR REPAIR AND ALTERATION • InCeormari For FAA Um Only eitimainacn (Airframe, Powerplant, Propeller, or Appliance) Anieressmosim Office MentifieetIen seinsiesmen • i•Cd-CF1 r INSTRUCTIONS:Print Of type ell ems es See FAR 41g. FAR 43 Appendix LAM AC 42.0-1(Or stresraidenlaraSiOninent00 [Or instruction/ anddisposition of this form. This report is required by leve (49 U.S.C. 1471). Faun) tOMport can result in • civil penalty not to 'acne $1.000 for each such violation (Section 1)01 Federal Aviation Act of 1956). Make Meal Gatrelnam Aerospace G-IV 1. Meath Serial No. Natkrnaety and Regret/aeon Marx Name (As shown on mgairation ceetitt.atil) Address (At mown On legestsation ~Wale) ' 2. Owner BA Leasing and Capital Corp. Two Embroider* Gutter Sao Francisco, CA 94111 3. For FAA Use Only , 4 - 4. Uall lantihcaticia 5. TYPe Unit Make • I PAWN I Set Na Repair Ntetation AIRFRAME (Ant ;reel' fl It also i t X POWERPLANT PROPELLER • Tyra APPLIANCE Manufacturer • • a Coalonolly Slaternme A. Agency" N me and Address B. it ol Agency i C. unmade aci. - Western Commander. Ina U.S Cerin.attos aNc...nc RA3118091Airframe 3,4 16300 DeilyDrhe Feregn Coellece3r< iercPunc Radio I, 2 & 3 Van Noya,CA 91406 A Can:tared Read Sisbon limited Permaxticatisfy • Nenutacinn• Instrument & 0. I me-Myrna; tonrepair and/oralterationmede toNeuritis) identified initem 4 an me cierientsw on the r•Wri•Or in•Chments hereto Ave been made In +can:Lena wen the requirements of P n 43 Of Me U.S. Federal redeem Regulations and mat the InformatIon furnish:0d herein it IIIMIIICI torrid to the ben of my nowledgo. / Data • Sigraturo of Authorized Individual December 12,1991 ....e---- I Mena for To Sen4oe ~yam to the authority give person specified below. the ern{ riddled In item 4 was Infp•CtId in the manner aresalos try cm Aernwtsueior or ins Federal adman Administration and a APPROVED 0 REJECTED By •I FAA FIt StanclaRIS Inspector / /AlOuNiCtufte InepeCliOn AtrtNartnbon Person Approved by Transport OINN (StaarTY) [FAA Designee X Reeler Station Canada Aiwartninela Group Cafe I Approval or Rejection Genii-ate a Sigtuthorized eI y1( 0 .......z ta...........4 Onignation No. .-45•14-,de..— DEC 1 2 1991 RA3RIIMIL FAA Fonn 337 • • . .* • SDNY GM 02754233 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241155 EFTA01326748 FAA AIRCRAFT REGISTRY CkNEtA 110.1 N DATE: 1 - 24 - 92 ■ NOTICE • An latOtatiOn MOSt be shoot.* enteredin the appropriateaircralt record. Weight andbalance or operating limitation changes conform ity with the applicable airworthiness requirem ents. altaratiOn S to assure continue d compatible with allprevious DescOomm of WA Mmm,ftlAiW retistation mate and ante work completed.) l shalt Identify wan sacra nationality and (II More SDK* le required. attach ackfig(ns Traffic Alert and Collision Installation of provisions for a Honeywell in accordance with Gulfstream Avoidance Seiron (TCAS II) has been accomplished 3SO issued on Aerospace ration Supplemental Type Certificate NumberSA303 991 per Gulfstr eam Index List. SC 41 129802 . Revision C, dated December 6, December 4, 1991. referenced STC have been Minor electrical wiring deviations to the above s listed on FAA Form 8110-3, dated accomplished in accordance with those diagram DER NM-476, Systems and 12/11/91 as approved by John R. Ciambless, FAA Equipment Engineer.. „ d in accordance with Western The TCAS antenna provisions have been installe 090 Rev. IR, dated 11-21.91 (Upper Commander, Inc. Installa tion Drawin gs #08068 #08068 079 Rev. IR, dated 8-28-91 (Lower TCAS TCAS Antenna Installation), dated 7/30/91 (TCAS. Antenna Antenna Installation), and #07068179 Rev. IR, s have been FAA approved for Curvature Adapter [Honeywell]. These drawing tz, FAA Structures DER installation on this aircraft only. by Peter A. Schwar #SW-586, with FAA Form 8110-3 dated 12/11/9 1. Software modifications to the following components are reflected by part number has been accomp lished by Honeywell - Avionics changes as listed below and STC: Division as approved under the above referen ced 0-903 to -904), 3 each SG-884 Spibol Generator. (from P/N 700857 700754 0-932 to -942), 2 each DC -884 Display Contro ller (from P/N Fault Warnin g Compu ter (from P/N 700748 4-904 to -905). 2 each FC-880 eam Aerospace-oCag SC41 As instructed on Engineering Order Cl of Gultstr d from its mounting rack nd the 129002-01, the TCAS computer has been remove breake r has been pulled and locked out. A placard, installed alljacent circuit NG STC APPROVAL". IIII • to the TCAS control states: 'TCAS INO1) PENDI revised to reflect the above The aircraft's basic weight and balance has been been found to be in conformity listed modifications. The work describ ed, has ed data, and continu es to meet the airworthiness with the above mentioned approv Work order 6719, on file criteria under which it was originally certificated. at this agency, covers the above described work. END a Add rt,onsl ShettliAnt A ...waddeadStetask.sk-...'..; "4.4 ' -- SDNY GA4 2754234 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15,_0 and 17 EFTA_00241 I 56 EFTA01326749 FAA AIRCRAFT REGISTRY __ I - 2.: _ 2 CAMERA SC.; T DATE: [ e 4 • tna-i RECEIVED FAi. r : Form Approved DEC 1 6 199 was No. 2120-0020 0 MAJOR REPAIR AND ALTERATION For FAA Uee Onk °ma idenc.oc ri= in twoomew ortoecenmea (Airframe, POwerplard, Propeller, or Applian — FSDO ii,14 Y Asimpensew if -el Of sanneerawn Apbenoia B. and AC432-1 (or suberopte ntrevisiow tnereoft kw inelmetione FAR4.3 INETRUCTIONS:PrIM or quell entries.See FAR 43.9. Ina civil penalty nO1toexceed $1.000 y taw pleu.S.C.I42”. F lore to reportcan result end dispobtion of INS form. TM; report is retwiredb Act ol1968). foe each such violation (Section 901 Worn AviatiOn Mode Mate G-IV 1. - Gaeta*. Amapa I. Aircreft Natenatity ma Registration Mark Saul • No. NMICA INS Address (As Mown on espialawn canines:a) Name (As Sheen on regIstraloncerldioalt) The Embarcadero Comer 2. Owner BA Leashes and Capital Corp. Sao Francisco, CA %III 3. Val FAA Use Only • 4. wet Mentlaration 6. TYPO Serlal No. Repair Afteratkin Maim Model Unit • X CAS diacAtopeIn !Hai i arroyo AIRFRAME . . POWERPLANT PROPELLER ,. TYPe APPUANCE- Manufacturer . •• G. Confomeryitemment • C. Corarketa NO. B. Kum of Agency A Aiency4 Name and Address Ma Gnats:aim immarm . RARRISMIL Airframe A 4 Western Commander, loc. I Radio I, 2 & 3 14.100 Daily Drive Forum Cemiates Neck em I Limited Fowerplant, Yen Nuys, CA 91406 A Cenotrawd Paper Stoma 1 Instrument dr Aa- wl sammoum oratticluents hereto tog» unMeMa ntrlied initem 4 above andoescalbed ono reverse D. I Certify MN the repair and/of Nitration mar* of Pan 4301 Me U.S. Federal /Malice Regulations and that the Information accordan ce with the requirement, hove bean mar* in knowledge. furnished non is true and carted to the but of my SMnatomid AutheritedAdividuel Dale / December 12.199E . T. Apprenil To Service d by the specified below. me nft...Identi fleo in item 4 was liespecied In the manner prescribe Pu scant to VW IllAhCalty given persons ation and is rAPPROVED 13 REJECTED Administr ator of the Federal Aviation Administr derraperayi FMIII.Stendards manuteesaw la•Penion Mathlti011 Inspector . BY FWDOnAppeOvapd try Tranaparl FAA Designee X Repair Stake " Canada AI/wordage Warp AutitorlzedCa c laa..... L ...,47 Mal or Rejection Certificate Of 77 Detect A Deeigne noD_ o. -e- . -1---1-1- DEC 1 1991 ItAntS08L FAA Pena 331to-r •r • -' SDNY_ d 1/64nr• SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241157 EFTA01326750 FAA AIRCRAFT REGISTRY CAMERA NO./ 'DATE: I - 24 - 92 NOTICE Weight and balance or operating limitation changes shell be enteredin the appropriate aincraltrecord An alterationmust be compatible with all previous alterations to assure Continued Conformity with the applicable altwOcthilaa3S requirements. Description cot Wont Accomplished rThOIO 3POC4 is require& attach addifetnal sheets. Identify wetly aircraft natranahty aria reqqtraffon nark and dale work completed) This supersedes that portion of FAA Form 337 dated September 7, 1989 regarding installation of a third Honeywell Flight Management System, a third Honeywell Inertial Reference System (IRS) and a Single Honeywell VLF/OMEGA Sensor as previously installed per Western Commander, Inc. (WCI) Supplemental Type Certificate SA3T74NM. Previous installations approved under WCI STC NM3774NM have been modified or upgraded in the following manner: Installation of a third Honeywell Flight Management System has been updated by incorporation of a third FMS computer (modified to Part Number 7004402-976), a Single Honeywell VLF/OMEGA Sensor System has been removed and a Dual Global Positioning System (blended) utilizing Honeywell receiver processors (Part Number HG-2021-AB-02) has been installed. These systems have been installed in accordance with option 6 of WCI sealed Top Drawing 08000004 Revision F dated 5/08/91, as approved on 7/18/91. This installation conforms to pages 7 and 12 of Western Commander, Inc. Configuration Control Document 08006005 Revision B dated 5/03/91 and FAA approved on 7/18/91 under WCI STC SA3774NM. The Airplane Flight Manual SuppleMents that were previously provided for the above listed systems, have been removed and replaced with the following Airplane Flight Manual Supplement Documents (dated July 18, 1991): 08015011 Rev. A (AFIS), and 08015014 Rev. NJC (FMS 3) and 08015015 Rev. N/C (GPS). Minor deviations to the above referenced approved data with regards to the installation of both Global Positioning System-antennas has been accomplished in accordance with Western Commander, Inc. Drawing #08068080 Rev. IR dated 8/27/91. This drawing has been FAA approved by Peter A Schwartz, FAA Structures DER #SW-586, with FAA Form 8110-3 dated 12/11/91. The effects to the aircraft's basic weight and balance has been calculated to reflect the above mentioned alterations. The installation as described, has been found to be in conformity with the above mentioned approved data and continues to meet the airworthiness criteria under which it was originally certificated. Work order 6719, on file at this agency, coven the above described work. END Additional Sheen Are Attached _ - ----- *---- ipico0:4-tro542a6— SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA (10241158 EFTA01326751 FAA AIRCRAFT REGISTRY CAMERA NO.! DATE: 7 - 24 - 92 • • Fri, Approved , 0ol nwo'-a, MAJOR REPAIR AND ALTERATION OtAS No. 2120.0020 Fes FAA Use Only in,,,„, (Airframe, Powerplant, Propeller, or Appliance) maw swam orrice Wenlincadon Aerrenonnr q•- 0 'On INSTRUCTIONS: Panto.hale all Melee Sat FARalle.FAR43Apperdix Band AC 43.0-1 (Or Sutdefluant renSiOnMantel lor instructions and dispositionMinis loan. This report is required by law (49 U.S.C. Ica Failure to repeal can result In 'aftpenaltynot to tamed 91.000 for each such violation (Section 901 Federal Aviation Act of 1956). Mate Model GeffOrSem Aenswece GIST it. Aireasit Social No. Nationality and Registration Mark IOU NISGA Name (As flown on nonrralon candid.fill Adams/As shown on ragastrarioncondidala) 2. Owner BA lasing and Capitol Corp Two Esobercadere Cates San Fracristo, CA 94III A Rir FAA Use Only 4. Unit ldwitineadon , S. Tyre .. Unit Slake Serial No. Paper Alteration I • . AIRFRAME (A d bad' If 1500 1 X . • r MIOPIEUER • Type .. APPUINCE Manufacturer - S Cmdcwaili Suilowee r A. NSW* Name and Address B. Kind 01Aganey C. CartifiCalll No. Western Commandeer Int USCancan. Want J RA3RSOSI. A/drawn A4 16300 Mtly Delve neer dendeated Wealaine • I Radio . 2 er3 Vs. 749S V1406 . A Unclosed Rage Mama I limited Poeferplamta . ( InStrument & Aceasesy D. I candy Mal thermion end/or aerationmade to the Wig$) ideMIfied in item 4 above and demand on the fawn Or attachants hereto have Wen made In imainninCe with lira requirements of Pan 43 of dm U.S Federal Aviation Regulations and that the iniormation hatnished herein is true and COMO to the but of my nowledge. Date Signatur f Authortzed Ina Deosenber IX 1991 • . m - k • 7 Arionwei ler P To Seam Pursuant to the authority give persons speeiliffd Delow, the a ' tined In nem a was inspectad in pm manner preaddeed by the Administniter ol the Federal Aviation AdmMistratiog and Is APPROVED 0 REJECTED - T FAA Fit Standards rInspacaor Manufacturer. ' - acacia Audwritation. Other (SPOT) • BY FAA Derby** X hpair Sistias • Parson Award by Trowels, Canada Ameenniness Group Ws olApployal orRelection Certificate or SignrAuthorized ,Ogisel ci , DEC 1 2'1991 ' 411tillast. - • --ers—e-a— CA! FAA Form 331irt.ma r• • - : CM)2754-237 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241159 EFTA01326752 1./ . FAA AIRCRAFT REGISTRY 1 CAMERA NO.; Y DATE: 1 - 24 - ;'-' . NOTICE alteration must be shall be entered in the appropriate aircraft record. An requirements. Weig hi and balance or opera ling limitation changes iness ble with all previous alteratio ns to enure continued conformity with me applicable airworth compati a. DesaWden or Work AcCerhrilithod frank and date work arnpieted.j (II more Span is reclulfiCC art•ch additiona l 'Meta Identity with annul natantiCy and ItylVrtriCn Systeni and Stalled Collins Removed existing Collins TDR-90 Mode C Transponder nce with FAA approved Western TDR-94D/Mode S Transp onder System in accorda DraWn g 080060 06 revision A dated January 18, 1991, Commander Installation Top 44NM as approved on February as listed on Supplemental Type Certificate #SA50 6, 1991. data with re to antenna Minor deviations to the above referenced a with Wester n Comm ander, Inc. mounting has been accomp lished in a N/C, dated 11/20/9 1 (Top ATC #1 antenn a), 08068087 Drawings 08068091 revision a), and 08068092 revision N/C, revision N/C, dated 11/15/91 (Top ATC #2 antenn s have been FAA approved dated 12/02/91 (Bottom ATC #2 antenna). These drawing vnth FAA Form 81104 dated by Robert E. Poteet, FAA Structures DER #NM-494, 12/95/91. FAR Part 91.411 (a)(b) were Transponder system ground test requirements of 1, in accordance with Appendix accomplished with IFR Ramp Test Set Model ATC-60 ed in FAA Notice N8300.99 F of FAR Part 43; Mode-S testing requirements address A - Octal Code 53016023) were including verification of ICAO address code (N8SG ments of FAR Part 91217 (b), were satisfied. Altitude reporting test require ed in A.C. 43-6A, Para. 8, to accomplished in accordance with procedures containments per FAR Part 91.411 45,000 feet. Pitot static re-connect check require Tester Model 181111 162, in (a)(1) were accomplished with Barfield PitouStatic(a) and was found to be within a accordance with Appendix E of FAR Part 43, Part operation was found to be tolerances•established by FAR Part 25.1325. System satisfactory for return to service. . has been calculated to The effects to the aircraft's basic weight and balance installa tion as described, has reflect the above mentio ned alterati ons. The in conform ity with the above mentio ned approved data and been found to be under which it was originally continues to meet the airwort hiness criteria on file at this agency , covers the above certificated, Work order 6719, described work. • END O AdditiOnal ShOets Are Attached Ilk 'ewe •. . e • .. ....wwwaaillbw. rsafeew+trewellibleetha r • ar ..w•rat • • SDNY_GM_02754238 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 I 160 EFTA01326753 FAA AIRCRAFT REGISTRY CAMERA NO. I DATE: 1i — — US 00•4411444 Of TRANSPORTATION '• • FEDERAL MIATIOtteADAWESMATION rene Appered Elettett Reap. Ne.14-660.I MAJOR REPAIR AND,M.TERATION FOR PIA WE ONLY (Airframe, Powerplant, Propeller, teeth IDENTITICADON of INSTRUCTIONS; prim or ope ell mariee Zair - et.41)r.., / • for knouniono sod dispoopion of this form. See /ALUM 1%R 44 Append... 11,ed./ itc4).Tot Co. oubekomo of•idooMeTeeo0 0.1.40 I MODEL • GulEst ream Aerospace • • I . MUM GIV ...• SOUL NO. ' 5 ]NATIONALITY AND 403403411014 MARX 1085 . ..0" . USA W886A-- • NAME (Ai Mon on fopiskertiss evelifp*Al • •I ADDRESS fAi Jan so ontendon ceneteste ) 7. °WM BA Leasing and Capital . o Corp. • ISan. Francisco, CA Center 94111 . 3. Ied MA USE ONLY , .--'''. t 7--- 1000. CFA A O, S.- / ... c •Pj. 0 ebe, 4. WI I nuncio - vv. ... ..... "Obit scfril • I Mat. NO. MM. Am Amp. AIRFRAME . M. *woof/ as he; I Mom) POW/IIPLM0 • PROntta ee NH APRIANCI mmourecroome .• • • • E. ullfawn STOW: A. sowers NANO AND ADDRESS I. RIND Or AGENCY C Ca MCAT NO. Western Commander, Inc. trd tiltinCATIO edoutmee RA3R808L • 16300 Daily Drive POSISt Wils•Cittf• .6101•ssc f 3, 4 'Van'Nuys, CA 91406 x Clinine.ATIO Mail ST410•4 Airframe 2, 4 3 aturyPACWOU 11mi ted Powerpla 1 • Instr. 4 acceSs. D. I Only due the wale end/or al ttttt oeuthatoti Immo ben been made la iota nude to ai valets] identified ho hem 4 above tad described sccepdatm oa the imam oa' mid tbs. ibe leformetio• hnliatsfil lop* e ith ,be requiemoonto of Pan 43 of the-US as Mt • el count to Me hen of my knorlpdpe. ; Metal A ti ttion Reeeladoet . • DATE • SIGNATURE Of AUTHOR .. AUG 2 1 1991 • C__ 1NDMDUAL . 7. AMNIA'. TM MINN TO SEIM Ammo. is Ilw embodier give ike Adminiontor of the Peden proem spetified below as unit Se ded io hem 4 no Atiedoo *dna&tttttkm lad is Ey APPROV iri ted Jo the mane peneribed by ED REJECTED NA AT. ItmeaerN sweippeepte . cannel omeeCtiemancouanor4 MEN flmostl sr Ma 011.0141 x ItMili MOON .. alOtaui. NSW OP MieteCill BOOKTOt OM Or APPROVAL 04 CO siOCull IRTICICATE 04 SIG OP AUTNORIZED INONIDUAL REACTION INSIGN4TION NO 8/21/91 g438808L ....4-4C-1.-t 0 at/e-t-tn.--( ... - -..- . own in V-6 rt. ' . • _ SDNY_GM 027542§r SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241161 EFTA01326754 . . NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. required, attach additional sheets. 8. DESCRIPTION OF WORK ACCOMPLISHED (If more space is identify with aircraftbationalfty and registration mark and date work completed.) with Gulfstream Aerospace • The items listed were installed in accordance 14; 1988 and the Report 11159C-GER-023, Revision 12, dated•November Engineers, •Inc. following- reports as listed in Consulting Aerospate and DER NH-1362. and Arora Associates roports approved by DER NM-442 and The following major components installed per the reports specifications as listed: . 1. Service Ladder -Installation CAE AIN-GIV-10 2. Service Tow Bar. Installation AA 103-8 ent List Aircrieit Weight and Balance corrections computated and_Equipm revised. Zhapter 2, All workmanship accomplished according to A.C. 43-13-1A., Section 3. C) ADDITIONAL' SHEETS ARC ATTPCICO •V.; OOVCPN,ILNT paisTiricoeneCTINIGN.WIWZO SDNY_GM_02754240 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241162 EFTA01326755 [ I A RTFli REGISTRY i I C!E: 1 DATEL/) - f .- (7/ • . DATE ioc. AAAAA ENT ma. AAAAAA Contemn . c- SFDESAL AVIATION ADWINVID•TION - Dec. 12, 1989 • STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR-AIRCRAFT COMPONENT IDENTIFICATION . MAKE NODE% HO. TYPE cbirpione. Rae.. lielleitlet. ilAaint Di APPLICANT a el.4 Gulfstream G — IV Airp.lane REX , INTERIORS, INC. LIST OF DATA - itittlITAICATIOti TITLE Report: AIN - GIV "Structural Substantiation Of Various Cabin (Section 1 thru Interior Modifications That Are Applicable 15 covered by To All G -IV Aircraft' Rev. K) STRUCTURAL APPROVAL ONLY 1. . This approval requires that Aero Interior verify ' • that the footman (Item - 2 Section 3.0 and 5.0) is a forged or machined part. 2: Approval -is -subject to Aero Interiors inspection of installation and components fabrication per ( sketches in report AIN - G - IV. I .. ". 3. This. approval is applicable to only the data contained in report AIN - GIV. The installation of all items requires the approval of an FAA inspector. .." PURPOSE Of DATA substantiate installatign of To structurally 2 ' components in a Gulfstream G - IV. • APPLICALL IL REQUIREMENT/ (LIP opeetateeeneno • st FAR 25 Subparts C a D • -CERTIFICATION - Unlace authority by direction el the Adisisist AAAAA mad la accerdaece with cent 'oar ad limitation # or appointment under Peet IBS al the Federal bristles Repletion. dais listed above and ea attached • tuts namberd NONE • I. v ban numbed Is &teatime with established procedures ad land a coply with applicable requirements el the Federal artistica Reguleticss. \ • I (K) Therefore 0 11de/weal amoral al am Amen these data SICHATUR (SI OF DESIGNATED tiCII/EE IIIG REry45ENTATNTOT data DESIGNATION NUUBERNE) CLASSISICATIONITT DER NM 442 Structures >9_-- .--ua A-- --..--. Michael Kappa n FAA hum 8 110.3 II km SUPERSEDES PREVIOUS EDITION ..•. SDNY GM_02754241 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241163 EFTA01326756 FAA AIRCRAFT REGISTRY CAMERA NO. DATE: \ OATC mitlION UA rTARATIJET 0cIPLUISTI .. µ N 16 AUGUST 1991 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS • AIRCRAFT OR AIRCRAFT COMPONENT IDENT:FICATION NAAR YODEL NO. Tyra (floptalt. III.I.. 14•Ittopen, MARC Or APPLICANT \ • pus STREAM Adam AFRO INTERIORS - N. .../ 'AMERICAN ' GIY LIST OF DATA' COEN TIFICATION • nit( AA REPORT N0.103 TOW BAR INSTALLATION SECT. 8.0 r • \ - ' • . . ‘ • I •-••••••A• • ,... . • . • ABOVE MENTICNED INSTALLATION MD ITS PURPOSE Or DATA THE TO STRUCTURALLY SUBSTANTIATE SUPPORT STRUCTORE APPLICARL E. SICOUI U. stmts. nat.') . . 4 .601 • r FAR 25.301 .307 • • .303 .333 • - .305 ' .561 :605 .607 AND .609 accaldauct wish coadhieits sod limO•lioas CERTIFICATION • UnDa nitwit; vested by tirtailea •I she Male loins., sod In Ansa a•mbra —. al apialaaaeot oh, Pea III of Ai TeIled A•Istlaa Replallna, Ism Woe.' above sad as •N•chtI opplitable N/A._ i's• 6 al. d In cc I • wish I III had penedarea Oa' land to dearly midi mutts...we • die Edepal Awimian Ilrillalloaa. Racemes.' oppyanl el slim dale . . ldi U» Theca lei Appian thile 4••• DESIGNATION NUMBERSIII ELASSIFICATIONI0 UCHATURIWOi DErby4TEDENGuiEtaINO DEPRESOITAINEM • • jad-1362 STRUCTURES k Cies ATISH K ARCIRA • • Fv•cattets PRLVIOUS EDITION FAA Form 1110• 3 °net SDNY GM 02754242 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241164 EFTA01326757 I FAA AIRCRAFT REGISTRY CAMERA NO. I DATE: I i — 4- - 91 i FOrm POINOved • OMB No. 2120-(KQO 0 ' MAJOR REPAIR AND ALTERATION For MR Use 0* S ascot.* a Isnanown (Airframe, Powerplant, Propeller, or Appliance) Office Ideinilleadon - it an Anamen minivenusko 4.1/'-00 INSTRUCTIONS: PrIM or type all Oman. See FAA 419. FAR43 Apperna 8.and AC4314-1(or sunachoem revision then.° foF intruedOne and disposition of this forrn.This report is required by law (49U.S.C. 1421). Failure to report can multi idyll wally not to exceed 51.900 tor each such violation (Section 901 Faders! Aviation Act of 1965). Make Model GULFSTREAM AEROSPACE CORP. G —IV t . Nationality and ROgisIrM0.1Mark - Serial No. 1085 ' NEISGA Name (As shOwn on regIatinorminifleale) Acldeen (Az shown on regmfration mintICAM) 2. Dame BA LEASING & CAPITAL CORP TWO EMBARCADERO CENTER SAN FRANCISCO, CA. 94111 3. For FAA Use Only- i 4. UM Menem e. Type Unit Make Model • EMS No. Ann Minion I • . MIFRAME (Al CleICAOH A Rem I Mom/ JOC PO ERPLANT • PROPELLER Type APPLIANCE Melnulanrnra, 6. Conlonnay Staten* A. Agency's Nan* and Address 8. Kind of Agency C. Genie* No. K I us. gefbecated Mathew LANCE. A. MATTESON Foracon Canicataci Macrae 8560 E. -SAN FELIPE DRIVE CeniricaMe Palma SO n AP. 1864049 . SCOTTSDALE, AZ. 85258 Menpranger 0. 'witty IP.MI the repair and/Or alteration made 10 theynol(S)identiled in item 4 above rd deecnbadOnlhe mein ornaeMnents hereto have been macto in accordance wan the requirements of Pan 43 of me U.S. Federal Aviation RegulatiOne and that the inkirmetion ' hanistmo herein is true and Correa le the nal of my novriodge. Date Sign ao ed In* 41 --- r - S : 7( • 6- 7. Approval nor Ratan TO &less Supt. of Maintenance Pursuant to the authority given persons specifier: Mow. the unit identified in item 4 was inspected in the manner prescribed by the moninistretor DI the Federal Ay 'von Aornaustration and es v li APPROVED 0 REJECTED Other ISM*/ If AA Ft "annuls I manufacturer )D(iinwcionminonya iee - • nspacter ay • • Person ApprOwIdts TrinatiOn FA,. Designee Repair Slat* Canada Aint011eindaS OfOuP Oate of Approval or Reinhart Genital, or Signature of 'un Ind, Dessmairon No. su .t 5 - 6 - 1/ 526705494 „.... FAA F0fIll 337 .+7 B/5/91 7:33 PM 1085FACE.WPS Michael Donnelly_ _ _ • " - • SONY 0M32754243 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241165 EFTA01326758 FAA AIRCRAFT REGISTRY ••• CAMERA NO. DATE: — NOTICE ‘" auarationmust De sted in the appropriat e aircraft record. An s mower:wed cha nge s sha ll be twi app lica ble airw orth ines oroperasinp limitation assure continued conformity with the • hewn andbsiance alterations to compatible with all previous date work comord edj /POWS:ion meth 500 n Anco ffel igne a ati nothanality liner Wo S. °meow)ofe is Winne. attach atkIttIOnal Meets Iden tity ATM ithw l No. 1085, NBBGA, (I' more epe e Co rp. (GA G) Model 0-IV, Seria stream Ae ros pac 8/5/91 7:24 PM ilUlf rtificate Data Sh eet Al2EA. Aircraft Type Ce bject: FUEL ange (AEC) 134, Su Rec om men ded Ai r.:raft Service Ch ril 28. 1991; and CAC ASC 134 GAC ed Ap FAA APPROVED DATA:ST PUMP CONTROL-MODIFICATION, dat (ATA 28) FUEL BOO ed Jun e 199 1. relay mendaent 1, dat 500 millisecond tim turn on time delay(2 n lst to add a e del ay rel ays The purpose of Wa this alteratio pump control circuits. The Landing Gear Wheel g fuel boost box (Right Main to each of the in the fiel pump control junction occur, during electrical bus each), located vent boost pump failures that can Well), will pre interruptions). in' transfers (power tructions contained 4 kit in acc ord ance with the ins of usi ng a CAS 805A4 ts of ASC -13 tea d Installed the par ent 1, except, ins2) installed a new Deutsch p/n to ASC and Amendm 3, Page 8, triang le A1K1 and the above referred cti ons Fig ure ) for ward of relay 354 l at splices (see ins tru c rai l Ter min al Junction (354A1TJ1 min al Jun cti on block* in the rai ly ter DI-el-IA-02, plasti h new Deutsch p/n CTJ120E018 es for installation into the new installed two eac . Prepared the fol lowing wir n from the wirpar e, crimp position "K" & "L" ly by str ipi ng the insulatioh properly pre wir ed wire with.a 354 A1T .11 ass emb tac t ont o eac e/contact installed h CTS 520 /20 con ins ert ing eac h installing a new Deu tsc l and M22 520 /7-,12 Xisliione r and abo ve ref err ed to ASC for details) coo the L-C: 1090005)20 to M22520/7-0i basic s: (sire Figure 000 J, age fs ofL-1 assembly as follow 209 820 to TJ1 3: 059H2O to TJ1 to TJ1L-A: . Wire No. 209000A20to TJIK-8: and 06'H2O to Ij1K-C 131K-A; 109000820 . Installed a p/n 1N4006 diodes 354 A1 CM , CR2 , CR3, and CR4;suppressor in place of the diodes ng transient spike K3, & K4). Torqued and torque Removed the existi 1NO/84A iransorb K2, h new Motorola p/n d across each relay (354A1K1,nds and all 6/32 stud nuts to 8 inc that were remove inch stud nuts to 25 inch pou striped all 144 meet the pounds. s installation and ipm ent wer e pur chased new for thi (2)(3)or(41- equ (b) (1) All added parts and applicable parts of FAR 21.303 requirements of the structions and out of the ASC-134's :.n al test. per for med the operational check Boo st Pum p Aut o-change operation 32 amps Successfully Pro gra m's Fue l s run nin g) tc be Maintenance any engine t switch the toaputerlmed st lumps current draw ((without pect to tte cockpi Measured each boo the cor rec t pum p operated with res that 2 amps. Verified st pump circuit breaker function. ctrical selection and bOo manual, inspectio n schedule. ele s cra ft' s fli ght a res ult of thi No changes wereor made to the air worhtiness inspection program as continued air load analysis,, • alteration. ce records. craft's maintenan e wit h thi s FAA fora 337 in the air Recorded complianc between this cha nge and.any d tha t the interrelationship—uce any adv erse effect upoite n the erm ine It has been detroved configuration will not int rod d to, y App ina tio n inc lud es, but is not lim e to previousl cra ft. .Th is det erm tem s wil l be abl 'airworthiness of the air ial, and back-up sys s that might all normal. essent que installation consideration that e int end ed and there wore no uni ion s, to thi s ASC that change the function as they wer require deviat s notification or• . interface with thi of the FM APP ROVED design change were priginel intent weight and balance ft' s .el ect ric al load analysis andresult of this alteration. aircra as 3 -7he effect upon the to either report changes were made negligible and no ARE ATTACHED NO.ADDITIONAL SHEETS END OF THIS SHEET nelly 3..W.S Michael Don 6,5/91 7:24 N'ASC1 O Additoonel Sheen Ate AllaCeed 7i sySOP0s .0443, • • SEMGA402754244 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA ()0241166 EFTA01326759 FAA AIRCRAFT CAMERA NO. 3 V DATE: 9 - 20 - 91 • 4 5. . 1.. . Form Approved t uil/ • OMR No. 2120-0020 • MAJOR REPAIR AND ALTERATION • •— For-FAA Use 0.ly a icrapbow, z. (Aireranii, Powerplant; Propillet, or Appliance) • . .. .. . . , . . .... .. Oita Identification " mmeassem „COL _ laso a .INSTRUCTION& Pant or typeolantries.SaFAR 41.9, FAR 43Appendia EL isMAC 4.31-1(or subsemrentrension thereof) forinstnalons ' and disposal:in Of this town. Tile MOW II nejtared bylaw (49U.S.C.1421).Faibure tO report can mein a mei penany not to mood S1,000 for each such notation (Section %l Federal muerte Act ol IOW. Mein ' model 1. Alma GOLPSTREAM AEROSPACE CORP. C' IV Serial No. Naumann, end Regisusnon Mark 1085 NSBGA Nom (As shown on minion CanACalle) ' • Address (AS 'hewn On rinaistnainn Candidata') - BA LEASING & CAPITAL CORP. TWO EMBARCADERO CENTER SAN FRANCISCO CA. 94111 , t Foe FAA Use Only • 4. Unit Idesnacellos S. Type . - ' . Um Make . Sinai N. ROOM AhMatiOn AMFIIAYE . (AS ADSCIfenl' nem 1&bra) XX POWMANT -• PROPELLER ; ! , Type APPLIANCE Nana/Mum S. Conaway Statement A. Amnty's Nemo and MOM . B. Tind Of AgeinCy C. Castilian No. X ',flatmate Wawa< LANCE A. MATTESON Fonogn Gantt-nee nonninc 8560 E. SAN FELIPE DR. cereutadeecor stow. AP 1864049 SCOTTSDALE, AZ. 85258 istmanum D. I anginal 'nemesis and/or alteration made tO the on t(s) identified in dent a above end described on me felts* or lalaChmentS lieral0 have been made in accordance with the recarements of Pon 43 of the U.S. MOWN Aviation Regulations anti UM Mil iniOrmation Unread herein is um me COMM to the bet of my nowledge. Date siffrata al In026.3zz. . 2 — 7 6-- , 7 acenival tor Mtn To Senna SUDE.' or Maintenance Pursuant to Me *Linen'," given Parma specified below. ON unit identified in item I was inspected In the manner prescribed by the AdminilleMOT o4 In. Fnecal Aviation Administratam and a CS APPROVED 0 REJECTED FAA FA Stamens °the (soon Manulanuist Inspection AtahoniatiM steno. X BY . MA Designee Repau Steen Person Approved Of transport — Canada AMmeedenel$ Gawp Daniel Approval or Rejaclen Connate or Simmons of Au • • • MOM • C., .SIg?"1541. 11 .."' ' . An• . joaet . 9 -2-1r 526/05494 . FAA Form SS7 nral • MlChaa - sbNy--_-Gm:.27.2,3 — SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241167 EFTA01326760 NOCE approphate ihrcratt record. An alteration musibe Weight and balance0r Oiniaring!imitation chamy«Wal be antereilin thewith the apphCabl• ainvolthinm requaaments. cOrnpatiblai willi alt prOvious atterallOna lotno," cOnhnued conlOhnity DInialpOon ol Wodz Accomplighed mrAalus dwa inwit [On‚5444.) more ‚pace h ‚nawal altach «Wadiami anta lewady wrn Wiwat national« and nwittrat(on G-TV, wh 11:05, Ainatt Pipa OecHfimt6 ties TaMat 2, 1931. Gulfstteaa rearscre Cap. gr) ttch1 Swat 4121i4- Peter to: FMKM 8110-3, Etaet af Caspharte vith 7tviatirn Itsulatzlens, dated 4-6-93, fcr ~sen G-13 A1cpUper C7C, vat i lata - lattificearn - dravirg 11933013039 MIA:1~ 4-6-93, 213 effittuthe far sima 10M - tatlal AIG SilitcER mær arcm-ion rinna-rn •BP MØG. ~sina Sa Gr HP3312 catat'al an ta fonen; ~nis: SE33-145 Rw G. thiffler ~0752-4 ED TA Malet Tastallatan - 1~011-15 Itv B E. Cl arieIlte • 119rZ1419-119 lem s N2 Tateastrr Coaling tstallaticn ~-1 NU papuge af tids alteraticn is to 1r:stall de @C Pmart Mamaer Rwym (lom) Altecretcr maling Maidficatirn. ad tle CC phi Proed t7e edstirg FRTS EM/fric Mi 432C6-9 laver AsartLy, attaChing terSare, 11.3*21419-73, Par. NI (date aie r) pni, D= S NU stase. h:stalle:d a rew Gle Wn 1159321419-93 de ~e rareacd grel (MO altan !Sid sial) uslrg M320315-449 ~5-414 ri:~ as datailed m tu inarp fcr altainatcr (talrig TrataLlatiat • ta fa= tie Sali Us edsting NU tall pips, atachin7 hadere, ard tle AFU 5x;e Valve ~Uting aircraft. Irstalled a rew GIC pin 1~1633-147 ER7 tai pipa silens cr raffler), attaching huds= ad gz tria, as «afled cn s aloe ~d to darli:prr far Mina M:~ Inataliaacn, ard Saw 31.te. tle phi Ractired Ue irstalaticn af tle edsting 3307 9ainless 9:æ1 (.010) lulaldrg platgi ?samar fa- 3703313-101 Zlme amator (we FM Ram 337 far thi: aircast cts(ad 12-77-133). 411 parts det rate iretaLlecl as a result cf chrwcp ~ nar at de the cd hatallatirn ad fu:nist:Ed bi ae with tre 13993-1 Flt. 9icsacd tle ART carertaent ad radaral a =Se cpaaticrel test of tle MC uting treirccaltrcs inni in ltds aizaaft's EM MITOM Airccalt niria Maral ad roed tresl gratla befale, dring, cr atter tie tast. - Fa:turne tle aiccraft to fligt status, recackd omplIate wab tids EM faza 337 ani FIEP33-1 in tle ahcatft s maintererce rads. It tes real te rap tiet tre intecrelaticrehip brun tids Saft ad arylxavicus~Ad anfigraticn ell not inizoduce av aha= affat uan de aincrthiare cf de ~saft. %his chteaciratirn irclaried, tut es na lanital to, cassiddratia: tret da dage to de essigt re tle AK3 omar aut ad axEscray cmlirg arargreact visl nut alitu iks igatticn anto Wla arms cf tle ahcraft; ad all installed arberiaLs ad parts tave ban na TER aigocual far iratallatiat m Ss aitait. lt4t rhr9cs leve ban mad in tle aircaft's lada ad Wam krat. •••••••••••••im rims stEttmnntIO =S REATLICEED".******103-02-9142aPnen****i~ C Additenal Shoels ATS SDNY_CM_02754246 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241168 EFTA01326761 FAA AI R)3. 17. REGISTRY CA2TR. A e ? ... mow mien • DATE: Ofttoonert dcoy:nom Mete .. .7 9 - 20 - ‘,1 ; MAJOR REPAIR AND ALTERATION (Airframe, Poweiplarn, Propeller, or Appliance) INSTRUCTIONS: Prim or type all traria See FAR and disposition of ens lOnli. This report it required by der (49 u.S.C. 1421). Failure io wagon for oWt such violation (Section 901 Federal Aviation .GOLFSTREAM AEROSPACE CORP. 1 , Ir CS. FAR ALTAppendix El.andACC-9d (or Act of 1358). Mcelili Office Montauban . 14/P subeeetsent revision thereof) fOr InStrUCtiO can sun i acerb perialtynol10 Meese G-IV Fix", Aeferfred OMB No. 212O-0020 ne $1.000 For FAA Use Only', ject - r ? 1 1. must Nationably and flagistralica Mark stew Na N88GA • 1085 Address (At shown On toystratiOn COnsfiCON) Nett* (As shown on reottronion conitic41O TWO EMBARCADERO CENTER • BA LEASING & CAPITAL CORP. 2. Owner / SAN FRANCISCO CA. 94111 • ___ . . 3. For FAA Use Only 6. Type - a. Us liarntibrellon Sera No. Repair Alteration Make Model Unit I AIRFRAME bas dncriWd in nem i aeon/ xx I POWEAPLANT . I -• PROPELLER Type APPLIANCE MandlEtuter I . [Cantonal" Slelemild C. Certificate No. . ie. Rind of Agency A agency:5 Name and Address 4 I u 9 Greece** Moctone LANCE A. MATTESON Foredo Cendfc.""Mtnanc . AP 1864049 8650 E. SAN FELIPE DR. Combats PleM40 &Mai SCOTTSDALE, AZ. 85258' lainninCliotel nts hereto in!tern 4 aeon end descnbed on Me reverse or attachme made Wine un t(s)identified 0. I certify Mel the teplet and/Ot enetavon U of IR, US. FINPRN kneten R•OullIbOns and MN the intOttniliOn . roads m accordan ce with me requidea nts of Pen hive been WM Cil My nowlegge. hammed hereon it true anti correct to the Signature ea Incline Data 04/20/91 . T Cr r . tAmmwsimmoumuswAm upt. of matntenance in ROT 4 44ss inspected in me manner Ormented by the SINCelled below. Ineynat identified Pureuent to vie Nononty invert atfICIIS 41 APPROVED 0 REJECTED alaon son If Administrator of the Fedeal Motion Admaitstr • Ogler (Spot) FAA Ft r Standards illanvIedurar Inspectein'Authonzetion IlitSpectc . BY I Person Approved en Transport . IFAA0mignint Rap.' Stston Canada AnorTnicreas Group Certificate Or - Signature CI Aul I Partneri Oale of Annecy.' or DescneltOn No. q— 2 1 ''. 9/. . 26705494 -.. M c ae o ell" FAA Fem. 337.•. """!/.. .141,tt'e llraeldsit irlI ff eeWmr.•••_-nerearinalk;Sfew..- _ SDNY G0.4_027S4247 • SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0(1241169 EFTA01326762 AA AIRDFAE7 IvIS • FCA1n7-4 AO. ; DATE: 9 - 0 - 9I NOTICE Weight and balanceOr operating limitationchanges shallbe enteredin the appropriate aircraft record. An compatible with all previous alterations to enure continued contestant,. with the aPpirtable airworthinessalteratiOn must be requirements. e. DirspiptiOn 01 Wen ACCIMINIOSSII tit mote space Is requited. Vlach additiOtIO sheets. Weedy with aircraft nationality and reartUationnsart end dale wore cciartiertiaI April 20, 1991. Gulfstream Aerospace Corp. Model G-IV, s/n 1085, Aircraft Type Certificate Data Sheet Al2EA. N88GA, Refer to: PAA APPROVED Gulfatrean Aerospace Corp. (GAO) MANDATORY Aircraft Service Change (ASC) No. 186 subject: COMMUNICATIONS (ATA 23) COCKPIT VOICE RECORDER/AUDIO - IMPROVEMENTS, dated January 17, 1991. This alteration modifies the cockpit voice recorder system to comply with the requirements -of PAR 91.609 (d)(e) and PAR 25.1457. This installation adds an underwater locating beacon, provides required audio recording of the cockpit flight crew and ensures that the system is powered from the most reliable electrical bus. The change also revises the audible tone generator and audio control panels to the latest production configuration. Complied with Part One and Part Tvo of ASC 186 referred to above. The Fairchfld Model 93-A100-10 Cockpit Voice Recorder, sin 53674, DOM 8/88 vas modified to a Model 93-A100-30 (underwater locating beacon and reflective tape) by The Jet Center Van Nuys, Ca. 91406; the Baker Electronics, Inc. Model M1045-F284-RGH3 (Pilot's) Audio Control System, sin 8608104, vas modified to a Model M1045-F330 -HG83, Mod 11 by Baker Electronics, Sarasota, Fl 34234; the Baker Electronic s, Inc. Model M1045-F284-HGH3 (Co-Pilot's) Audio Control System, c/n 881067, vas modified to a Model M1045-F330-MGH3, Mod 11 Status, by Baker Electronics, Sarasota, Fl 34234. All parts that were installed as a result of this change were new at the time of installation and furnished with the ASC 186 kit. Successfully performed the ASC's operational test. Returned the aircraft to flight statue, recorded compliance with this FAA form 337 and ASC in the aircraft's maintenance records, returned completed compliance card to GAC. It has been determined that the interrelationship between this change and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. This determination included, but vas not limited to, consideration that the changes to the aircraft's electrical system (Electrical Load Analysis) would not jeopardize service to essential or emergency loads. The effect upon the electrical load analysis vas a decrease of 20VA to the ESSENTIAL 115 VAC PHASE C electrical bus and a increase of 20VA'to the ESSENTIAL 115 VAC PHASE A electrical bud. The effect of this change on.the.aircraft's basic weight and balance report vas negligible. END C AddtliOntal Shirts Aie Altached 1 SDNY_GM_02754248 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241170 EFTA01326763 FAA AIRCRAFT REGISTRY _rAMERA DATE: 7.- 24- 92_ _ _ SDNYCM3275;i2;19 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241171 EFTA01326764 a FAX AIRCRAFT REGISTRY CAMERA NO. j DATE: 6- 9/ Form Approved 01.40 No.2120-0320 0 MAJOR REPAIR AND ALTERATION For FAA Ufa OS vs Ceceeen a Parcomen (Akira, Powerplant, Propeller, or Appliance) Enke Mentilicebdo wan ins n P 0 swiss SD/— tension thereonlot instruction* - INSTRUCTIONS:Primo/ type all entriee.See FAR 4391FAITIDAPtentlia B.and AC 4.1.94 (ot subsequent on "Wait M a lifal lidnallY not tonce.211"° yd disposition of Ws lorm.This Mean is reavired bY lee M9D.D.C. TIDD•FailudelOMPri Tor each we 'Anibal (Silakin 901 Foetal Amnon Ara O11161). Mak* Model I. sa GOLFSTREAM AEROSPACE CORP. G —IV ma MMionality and ReWaration wart Sent No. 1085 NBBGA HUMP /At shown On rearttrittgli cartillcata1 Adtrass (As Mown OA nigisfranon clittifiattal - BA LEASING E. CAPITAL CORP • TWO EMBARCADERO CENTER 2. Ownor SAN FRANCISCO CA. 94111 1 For FAA Use Oat, ' • ..-rt 4. thelldentdlaillon . IL T. Model Sertal No. Repair Memnon Unit Make I . I , AIRFRAME :Assn pep i 0000•1 XX • — POWERPLANT I PROPELLER I I 4 Type I APPMANCE 1 Mantdattwes - IL CoMensilly Stnemeed B. Kind el Agency I C. Candidata No. A MARCO Mama and Address . H = I Vs Certaninee mecitanc • LANCE A.• MATTESON se.•444erb, cmeassecron4 - AP 1864049 8650 E. SAN FELIPE DR. I Gambes saw Simon SCOTTSDALE, AZ. 85258 . m,m,,,,,, _..• caddy mat Inc mow anclhar weapon maw toter ;initial idient.l.ed in ill/MdlibOweaft4OffaMMI on me reverse or ausenmonu mitt° 0 I Federal Amnon Reputation, and mat tne mtormatan nave wen rninW in accordance won ter requirements of Past 43 of ter US. hon.:Ned Perron d We and anent to me best 0 my knowing* Dale . 6 Sigma 9/ I . 4.4-",.E /-.• i - 7. Antonl PM Return re Samoa SUDS.. OE Heinienance . was emporia' In per manner PreMnbed by dl' govin: molt* awnonly Enna persons specified below me ond CV% no m rum 4 A041%mentMOI 01 the Federal Aviation Aornmrstration Ina es p APPROVED C REJECTED 1 I Other (Speedy? • I I rnAA FitioSflanoatos I I Manutsclune Inmecben Aumontalitin ' • X By 6 I I Person APProveo by Tranwort I (FAA Elsugnee . JCanadafteeonieness Good I IRE.' Slit." Oars on Approval or Repecoon Cang i pos on naltie ilca orNI. . 6"amide of Autnbrtati In ideal Li — n - 1/ .526705494 Michel onnel y FAA Form 317 •-• • r SON YIGN1_027 54255 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241172 EFTA01326765 FAA AIRCRAFT REGISTRY - CAMERA NO I DATE: 6 - - 9/ NOTICE • Weightand balance d operating/om • compatible with all previous altera italrOn chang es shall be enfOr echn the aPPt0Pliste tions to assure Cant:hued conformity reSorchAn slinatiOn must be with the applicable airwor thiness requiternetnft a. Oncripbon of Were Meese/dashed (It more niece l meowed. attecnadOWsOnal'Pinta Idenuly wen secret narwnuuy and registration slant and late wet* cOMPOWWS1 April 21, 1991. Gulfstre am Aerospace Corp. Model Aircraft Type Certificate G-IV , s/n 1085, N88GA, Data Sheet Al2EA. Refer to: FAA APPROVED Gulfstream Aerospace Corp Aircraft Service Change . (OAC) RECOMMENDED (ASC) No. 198 subject: AIR ACM (AIR CYCLE MACHINE) CONDITIONING (ATA 21) BYPASS SHUTOFF VALVE - November 19, 1990. ACTIVATION, dated This alteration modifies the air conditioning syst °COOLING TURBINE HOT' mess em to prevent the age on the °FICAS (Engine Alerting System) from annu Instruments and Crew nciating when the aircraft feet and wing or covl anti is below 42,000 -ice is selected.- - Addi added to ensure the air tional circuitry is cycl the aircraft is below 42,0 e machine bypass shutoff valve opens when 00 feet and wing or cowl anti-ice is selected. Complied with installation instruction of ASC 198 In addition, provided posi refe tive locking to the 8 scre rred to above. to attach the relay rail ws that are required to the tail junction box (see figure 1). All parts that_xere inst alled as a result of.this time of insta—lation and change were new at the furnished with the ASC purchased frOm. Gulfstre 198 kit that vas am Aerospace Corp. or comp (b)(2)(4). ly with FAR 21.303' • • Successfully performed the ASC's installation checkout test. Returned the aircraft to flight status, recorded FAA form 337 and ASC 198 comp in the aircraft's maintena liance with this completed compliance card nce records, returned to GAC. It has been determined that the interrelationshi and any previously appr p between this change oved configuration wilt effect upon the.airvorth not introduce any adverse iness of the aircraft. included, but vas not This determination limited to, consideration done in a manner that that the alteration vas will not.intecfere with or safe operation of the adverstly affect the aircraft. - • The effect upon the elec trical load analysis was- nebligible. The effect of this chan ge on tBeaireraft's basi report was negligible. c weight and balance • • END_ • ts- st-114Fgaa"?. ite•Z:2?-444;a1" 17 SDNY_Gm_o27t42t1 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF-EA_00241173 EFTA01326766 oteistc'- ‘" 4•Rer! ' 7 7 - •-• :len"?' - Br • IAA, AIRCRAFT REGISTRY tAmm O. RAM 3t.7-'9/ REGEIVE6 FAA rn . . O MAJOR REPAIR AND ALTERATION FEBFED0 5 • En , t 0148 NO. 312C4020 Aere.v" w--- Cot FAA Um Onte • Ohara , cif irneerewn ' (Airframe, Priererplanl. Propeller, or AppliarVny F-• at,no Office Idenuedation Nemeerwee• -- li P.C.,. .-1 assammin 3 1 :PrInt or Typeset/mimeEa FAR 4.3.9. FARO Appendix S. and AC 43.1-1 tersigmeguent revision owreel) ferinstructIons WaTuLY-7.:41 tOrnortoannsult in a cMI penany eaglet:led $1.003 and heteptien Muir law Thl tan Is required by law (49U.S.C.1121). F aura • :or each such vielilien (Salton 901 Federal Aviation Act e119519 . \--- IMMO • Maim GULFSTREAAIAEROSPACE ' ' • 4.-IV • .N L Aircraft . Serial No. RO,OceMY and ROOM/Mien Mark togs USA RUDA • • Name (As sawn en reoutration combos(*) Adores; (Oa shown on tooltfrallbn cortigabl). BA Leasing and Capital o Corp. . Tea Emberodeto Canter San Frandsen, CA 94111 • 2. Orme . , , . . . t Mena Use Only •- 4. unit Meettikatien B. Type • MetalNa. Repair • Month= Unit Make Mob! AIRPAME (AidosOtits1 Mho! l bow) • X POWSIFLANT I . PROPELLER a Type ApruAria Manufacturer ' 4. CeelenelteStreeteeM. • 16. Kind Of hemem • i C. °protium Ho. A. bitbools Hama and Mona utctemeinas IAMPAIM , Western Commander, Inc. RA3R8081Airframe 3, 4. 16.3110 Day Drive Radio 1 2 & 3 X Certerer Rear Shaw ,11zolted Powerplent, Van NuTst CA 91406 'Instrument &Areressorr .. • • teerutecom hereto 0. I cora, that the repatriate( Maeda made to the oafMideadflad a Muni &tern VS daunted enure merit ex armaments relent Ariake Rnutaains and tnat toe informodon new been mare in ar..efOince with ihe repuiremenho of Part 43 el the US. . furnished herein ii Lea and oorreh to me best of my nowkolg. • Oats Signature at AuLlenne Marldual Maury 41991 . • X 12A-----•' 7. amen la To SeSce Purrant to the atdnerhy given persona specified below. the unOleenaml In earn a was fashathed In 5W manner twelabed by ma Ada:tetra:et of the Federal Avietiun AddinistratIon she la WAPPROVED D REJECTED Cam (Spree/ Inure Sterdarea I Imani so n ; Instal= Autnorizahan tkIsitctor ‘ SY Person raormai Tampon I CANNIAiiheifthitieli Group na Desiree' Ix lane, sums, On ef Arrant erfleMetten Creacata or 4""'" zed-, • . 2 / 0 1 / la -• .RA3118081 I. . • SON Y_GliCO2754252 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241174 EFTA01326767 FAA AIRCRAFT REGISTRY CAMERA NO. / • DATE: 3- 7- 9/ NOTICE vicga• and balance oronaret ngtimnarlonchangesshanb.entered in throppropein!airerattrecord. Ariattaraiion must be cc:moil:eV with en meow aerations to assure continued conformity with the a0PaCare airworthiness OoserttOon Of Wort AccamplltNW • (Irma SPACP is Mown. coach additionat shoay kfeithly wW eiterfli riciionany and sligistrit;Oti mart and ate work COolOANOO) • • Installed Sensor Systems, Inc. L.-Band Antenna, PN: S65.5366-24 Serial No. 5712, at Horizontal Arm 151.0, in accordance Installation Drawing 1653-04 (-513 antenna installation) as substantiated by applicable portions of Elsinore Aerospace Systems Inc. engineering report 1.175, dated 12-11-90, approved by Robert E. Poteet, FAA Structures DER #494. • All workmanship has been accomplished in accordance with applicable pardons of Advisory Circulars 43.13-1A, Chapter 2, and 43.13-2A, Chapter 3 and 13. The Aircraft Weight and BalanCe Report and Equipment List has been revised to reflect this installation. The work described has been found to be in conformity with the above data, and continues tomeet the airworthiness critena under which it was originally certificated. END SDNY_GM_02754253 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241175 EFTA01326768 -jets, • FAA AIRCRAFT REGISTRY • CAv.EkA VD. / DATE: • , • ' , It leLick-Li r alsimowevau Otte NO. 21204:020 : • MAJOR REPAIR AND ALTERATION EB 5 'buil • 0 otMonnors Far FAA Use alit a.*:nkno.. (Airframe, Powerpiank Propeller, or Appliance • '''' anal iesettification FollSe"man Alsoreirat — "' . VNY FSC0 Q -O-G! INSTRUCTIONS.Printor two all orariek.SolFAR41.9.FAA a3AcpaniSiaL and AC 43.9-1(OraoSatiothInwiaion MInangratioatniniona and eisaosinon of this lonn. This *MIS IMAM O./ Ara f4OU.S,C,Ian. Failure to re9Ortean rano:tin 4 chli penalty flax to =tad SI.= by ur-n such violaban (Section sot Federal Aviation Allot IASI). Mak s , Wool - GULFSTRF.AMAEROSEACE• G-IV 1. Airtran NaUonality ana Raer strhica mot SON No. 1085 USA NNIGA Name/At Mown on rogAsuatiOn Amnon:4y Aeven (At mown on mn.owition conaktre. RA Lasing and Capital Corp. ,--• , Two EmbascaderoCenter i Ovine, San Francisco, CA 94111 .• I Fot FAA the Only 4. UM Idannlicabon S. Type . - - Una Mahe Mudd Serial NO. ROOS A.Iternon . . . . AIRFRAME IAs dolorlbOd AA hoe I chow,) •- X ICAYEAPIANT inOPILLER I 71,4) APPLIANCI Marataconar • - - I. Caolonnity Ilateinoin A. Aptrimys NV,, and Manna I B. Kind S AgAncy I C. Granule No. • I uS.Careacitao woman< Western Commander, Inc. ANAL Airframe 3, 4 16300 DallyThin Iteceqn Cerilteeted lArc.anc. "o 1. 2 SU Von Noys, CA 91406 . .. X crenate. /lona Ss on IllmItal Powaylazt, n Idinufliaitet IInsUomtnl & Aulasory - 0 leutny um, too rifle and/or altmodon rnanato CoI unit(s) lanbtodInitem I AbArro sod On.r.beden.nerrAteltOrarttAnmenCnvoto titre Nen nude es lieenreinCe wit. the requitenientl or Pan 4.3 of en US. Flat Aviation RagnIStioaa and that tie kiiarmation hardened herein le tale int correct le the Wu of my linowiedga. Dam • ' 1 Signature, of Aulhodiiiis inateldual . Unary I; 1-991 • I 7 . /ei.:•-•;-.. • T. Amnia tarn re Sonia ' • PurtY4/11 to Ma aultionly Ceded;nate ...weird -*low. The ;:n9Orleor*3 In item 1 wag bora' in ma "Wass TIMIREbmIl bY Si. c4mulatratos el the Federal Aviation AtItninisInnon cede a -APPROVED 0 ASJICTED I CIon:PIIIOU I " Int $" " lifea I luanitaton ' I inna-bon Autnodunion I "Ir / Inn ila01 I / _Y II 1 I AA N yco" Ix ' Ammer sada, . !Pima Appeared by Tranuor: I Canada Ainionhnins Coto* I :IamnfAcolosatorgenic0en (CAMS= or i5iOnficl Autriony/o4/9.7,xiGat ...? ICelionaoon No. .4.,-1-e :Alf zit; /9/ 'I RMRSOBIL,• I A - .. ' FAA Farm 337 .1.10 ipitOMIfirsr7"7 — . SON1716N1_07542E.:1 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241176 EFTA01326769 NOTICE Wednt end bitence or operating limitation change:shell tt: entered In IN en;w0Orlate eleven record. An attemtion must be competiWe with all previous alterations to assure continued cont‘trni, ♦:Y. int applicettisetretotchtness teduuenients. 1. Incorporated G•IV Phase II Product Enhancement Modification per Gulfstream Aerospace Document it11S9SB42116, Revision A. Revision to the Aircraft Weight & Balance Report has been provided. Flight Manual Supplement 89-03 has been provided for incorporation mto the Aircraft Flight Manual. 2. The following major Gulfstream Aerospace Aircraft Service Changes have been incorporated: . . SDINFCG0.4_0/7§12er SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241177 EFTA01326770 r43LikaTlg::.: • it tekk AlitrIARE RECUT*? cmaita"no.. 0 2 -verni ve: ; "row • tiara: ay.- /.3 1- 97. ll . -2 Fond Apprdrred 01AB NO. 2I23-0320 0 MAJOR REPAIR AND ALTERATION for FAA un May vs move« Appilanee) encresmare (Airframe, PoserplanL Propeller, or ~Mew Mom Anshe issmasseet Dt.-Pa AO .9-i (or suteepue nt ralsionth meW lorInebotents FAR 439. FAR 43 Appeals A enclAC43 I Gee sernly not CO none II.0O3 INSTRUCTIONS-. Note BMW entree Sea by law (49 U.S.O.1421). f ehrreto report can result end damortiOn ogee form This repon a rectered Amnon Act (II 1955) ' to, each stge resew (swoon 901Feat Wen • GITLESTREAM AEROSPACE CORP. G-IV t. AlrcMl Netionaely onO Rejetralin nut Sown No.. N88GA 1085 eettlIkeW Addrcos (At shown On ~bon Iteree (As Mee on redorradoneortMean) TWO EMBARCADERO CENTER BA'LEASING & CAPITAL2.CORP. \ SAN FRANCISCO CA. 94111 2. Caner - ‘. 3.•f-er FM Use OW, a. Tree 4. Unit idenonesuon Serial NO. ' Asper manse UM • . MeMermited on Men I Wore) AYNMYE , . rerT MUPILLEA `., ,.. APPLIANCE . I ACAMOrnIvineMel C Centime No B. Kindle Von A, *Genera Hens len0 Areal S I US. Mehered lecterse LANCE A. MATTESON ror.yne.eaarnarumm AP 1864049 3015 NORTH HAXDEN ROAD eseitereeset ease SCOTTSDALE. AZ. 85251 mewed I*nth< news of attacremenis hereto an~enedelOtiveu nemsen atteatneemeseee too eau/its: mnformaten 0 ;centre tessentease SeveretbMe the sesteementi °ten 43 or thre U.S. Feder', Mitten Anulatens and that ow no* been made et accordan ce non*, ts true and coma to IM Opt el ray!nowhere. banished Llete • osi 9/pta r K-id 7 A-Adroed Ow Rene To WrMee Supt. Of 2421i Pit AAA ILCA fine lama« in teem I was Mowed in ne manner preocrind by de mime se Paean to the Dulaney given weans weasel end is Li APPROVED 0 REJECTED Mffinetretor of the Feline Aviation ~tress Can (WOW MA fief...incline - InstecemAnhonntea Inspactor . A BY Pelenenneed try lemon MA Oterree Stann Canna Amoneeen Group or Sign!~ of Autorren Dam cl Moron or Reectoon o No. One Cateen 1/7 y-1 o 44i7.05424 FM Form SW “r rev Michael Donnel 1"10.4k000.5,4lbot. IL • * SbI _02754256 10, SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, n 1 5, and 17 EFTA_00241178 EFTA01326771 FAA AIRCRAFT FECISTIT CAhTAA DATE; /.. /j5-57 r64.64.mayes6sr. - " Jesm--?t;2_ • NOTICE • We4pht and balanceof operetinp limitation changesshall be enteredln thatapprOptlate aircraft mord An attention must be compatible with all previous alterations to azure continued abalone?* at the apptiCable einvonhinius requirement. censtamoiwesseasscasvo proonsyse•arrentemessauvorsithonsournmarrasenalved aM 6666mm,marldowsvoe°4666.4J November 9, 1990. Gulfstream Aerospac6 Corp." Model G-IV, s/n 1085, 088GA, Aircraft Type Certificate Data Sheet Al2EA. Refer to: FAA APPROVED Gulfstream, Aerospace Corp. (GAC) Aircraft Service Change (ASC) No. 166 subject: optional EXHAUST REVERSER SECONDARY LOCK AND WHEEL SPIN UP-- MODIFICATI (ATA-78), THRUST ON dated August 17, 1990; GAC G-IV Wiring Diagram Manual drawing L159AV40137, Landing Gear Indicator System (sheet 1 of - 1) 32-6-1, Page ), dated January 19/90; GAC G-IV Wiring Diagram Manual drawing 1159AV4010 8, Thrust Reverser System (Sheet 2 of 2), page 3 dated August 31/87; and GAC G-IV Maintenance Manual 24-0-1 Page 5, dated August 8/86 para 10 Bolted Electrical Connections - Torque values. This ASC adds circuitry which ensures prompt thrust reverser deployment with wheel spin up. In addition, it adds a time delay relay to each thrust reverser's secondary lock solenoid circuit to prevent burning out solenoids due to exceeding the duty cycle. Complied with all of the applicable instructions contained in the ASC,. All installed parts were installed new and comply with the appropriate parts of FAR 21.303 (b)(1)(2)(4). Successfully performed the ASC's operational test: Returned the aircraft to flight status, recorded compliance with this FAA form 337 and ASC in the aircraft's maintenance Secords, returned completed compliance card - to GAC. It has been determined that the interrelationship between this change and any previously approved configuration . will not introduce any adverse effect upon the airworthiness of the aircraft. Thik,determination included, but was not limited to; consideration that the workmanship that vas done, the materials-that-yore-J.18°d, and the condition of the aircraft after this alteration were equal to-or_bett er than original Certified condition. The effect upon the electrical load analysis vas an-increase of 0.3 AMPS added to the ESSENTIAL DC BUS (during Thrust Reverser Deployment). The effect of this change on the aircraft's basic weight and balance report was negligible. END SDPIY G-0.4:017.542E7 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241179 EFTA01326772 YAA AIRCRAFT REGISTRY e'l • CAMERA NO..2 DATE: /3 - ft RECEIVED FAA Di MAWTSONTCOIRMOOREATITI • . ODT . 2.3 t$114^nAlt=f FEDERAL AVIATION ACATINFSTRAERte4 ' • ateks VA 04-406a.t MAJOR REPAIR AND ALTERATION FOE FAA USE OWLY VNY FSDO OFFICE OBOVCATION (Airframe, PrverpTara, Propeller, or Appliance) INSTRUCTIONS: PSI or type ell entries. get FAR 43.9. FeR 41 Apptedit R. and for sennections sad &galantine d nib fora AC 41•9-1 Cot uttsweeeet revision theme° • . • imams GULESTREAN AEROSPACE . A. G -1V I /NOME SERIAL NO. e ' INATIONALTTY AND RENSTRATION AMIE 1085 ' U.S.A. N88GA NAME (A. skein re reentref I.4001IISS (As thew. en nperroticet ontigane) onsitgeerei X MEI BA Leasing and Capital .Corp.] . . Two Embarcadero Center San Francisco, CA 94111 3. FOGA* us* an . 4. EISIT IDEMMAIN)N S ME own Nail . ones sena to>. ante- serait MION • AEVEAME (Ai &weal ma Aim I ahem) X FOWIPPEANT POOPEGIA not APPLIAna • . • .- • •6. 0)/0041AIT STATUE/I A. AGENCY 5 NAME AND AbOltESS I. KIND OF AGENCY C. CERTIFICATE NO. Westarn Commander, Inc. at ClefoliCatte ace... 16300 Daily Drive - . 101.101.1 CIITIIIttlle 04CM...0 Repair Station No. Repa Yan Nuys, CA 91406 X Cleetwerre WM. HAMM RA3R80.8b 0•10410401,0till A3 Seri lti,42f, & 3 D. I certify tbet•ibe. weak. sed/or Jambs made te the onitli) ideeti6ed is iron taschnewts hence Iwo brae made is accoadeace ends the requireeento of 4 above sad described cos the etyma or and chat the Wormedw haelsbed twat Is trite and comet to Pan 43 or die U.S. Fetna Aviation Itegolanicep the beet cd ray knowledge. .. ' DATE SIGNATURE OF AUTNOW2D INDEVIDUAL October 24, 1990' (17 - t AMEMO4 NU SU Pyrites to the sethedry_gewee reins specified below the van identified in New 4 was ies&teratd a the unseen prewriteed by the Adsieleauto at the Fedeesl Aviation Adesantstruiese sad is Em APPROVED irpz TD ra. ea AT. Moan tea d/W•fathIlel . ame• 0....,, II . fauvism Warabie . sea 00.01411.-- - X'. &MA stArtOn co nasty nset otrICTOR CO MONT ' — • .- DAR of AffEIOVAL pa COMRCATI Oa DISIONATION NO. October 24, 1990 SS4 7 1: r irte UArt:e . . CRS NRA3R808I. ... SDNY_60.4 02754258 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241I80 EFTA01326773 'FAA AIRCRAYI RIGISIIT CAVIERA PIO. gp DAIL: -- / /433 - 9/. •- NOTICE Weight and balance or operating limitation changesshab bonterediri the ePtarogiate aircraft record. An alteration must' be compatible with all'prpwOOS.alteratIOnslo assunr continued conformity with the applicable ainyorthiness requirements. • 8. DESCRIPTION OF, WORK ACCOMPUSHED (If mare-space is required' attach .additional_sheets. Identity with aircraft nationalityand registration rnailtand date mark completed) • . • •-• • - Install ed Remote Heading/Courie'Conifols -on pilotand oc pilot control wheels in accordance witg.puPP1eliental Type. Certificate ISA5001NM, dated Aygust 1990.— Flight Manual. Supplement 008015004 NTO.- 'dated' August . 30;- 1990r Was, been •provtded: t" " • The effect of this iiicialtatib -p- citairciiaft—basic weight and . _ balance is wegtigible. Thls_kircraft continues -t o mesa all „ • . . — airworthiness—ff.:jut . rementsi- cifvo,r.1Tina. 1--certifieation. _ FAA AC 114904 Cu t. Govrtmurmt S`PJPIltur. Cr rcc.- 1144-€T .b H it tie pr. Iliin SDNY GM_02754259 ---- SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241 IR! EFTA01326774 ISIMMIIERUIRP ,Lt .17M 1141STRI T CAMERA RD. 7, DATE4.02 /G4" 4/3I ,G- 1 cfMtlete O* neentgrATON fin - MEW AvIATiON ADJAIKSTIATION 1.,, _a ...n Batt .4.. r t NA ot-R060.i ‘‘' MAJOR REPAIR AND ALTERATION 0 FOR MA UM ONLY TAPfroma, sowarplant, Propellor, or APP1h4F 5 -0 .a 3. ONCE ofrancanoti . INSIRUCTIONS. Print al type ell ristlici. Stil FAR CS, PAR 43 ApPidna 8. foe lostrealos sad dliposIdoo of this feat sod AC 4351 les Abatement adios dash . MAXI MOOR •I. ROAR GIII.FSTREAR AEROSPACE G1V SOW NO. NADONALM AND atcaStitanom NARK 108S , U.S.A. 888GA Waif& aftwornmenthetotico terlilleoN) ADDRESS Os rod on dyistrodo cesA0.0) 2. OMER 8A Leasing and Capital Corporation Two Embarcadero Center San Francisco CA 94111 --., 3. FOR MA WE OW .. . ,, 4. UNIT IDERTIFIGTION $ TIN UNIT mast AMON AIRFRAME •,- /4 do cased le Dem I eon) ' X PM/RANT tin ANUANCI IIAMPALIVIIIII • • • . E. 1NIFOIIIP11 STUMM A *can we AND ADDRESS I. RIND OP AOENCf ' C. CIADACATE NO. WEStEAN COMMANDER, INC. as aninuiva Aff00.4/41C 'Repair Station No. 16300 Daily Drive mato« CtIMO•CMID iiitaeli , I1A3A8081 - Van Nuys, CA 91406 K CICIIKARD Walt STATION A3 A 4, Al, 2, 8 3 IsutUFaCIIMIt Ll , A .1 P D. I cotify that the npals end/or ahead°. somas to the waifs) identified east otats bent* be bees made Is ettoolsoce with the ageless' ofisPart beta 4 above sod desalt.' es the tame ot Nod that the haforthatioa fandthed herds is true ad canto to the ben of my 43 of the U.S. Metal Addeo R.gviedo. honk:dot DATE PC/NATURE Of ALMIOALUE7400ADUAL August 24, 1990 ' 7. APPROVAL FOR AETUI soma-. Panda to the sotharisy_fibm dada eddied below tho die Needled La item 4 the Adataban of the Mad Analog. Adalebetedos Midis (3 APPROVED ratted ia the odder prescribed by IM sit Pe4.0404 mas tAssan OMR DANA, IMPICTIMINTIOCCArOl IT CAPObt011 PIAXIMIM 1.0. Men X WAR RATON 0 9141.201B tWCOI DATE OF APPROVAL OR ONITINCATI OR 310 Uld Of AUER/NUM PCMDUAL REJECTION NO august 24, 1990 DISIGNA")" RS RRA3R808C • . Z .....4..c.o.c. 67 O.2%tes , ‘ f. • t tYib,-,NtOtters' 3 SDNY_GM_02754280 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFIA_00241182 EFTA01326775 t • • ASS rOLA Li/WELTS itIGISTIRI Clint* FO. 02, rant -: 13 - Weight and balance or oar ating limitatio NOTICE An alteration mint be compatibie with n changes shall be entered in the appropr oft previous alterations to octane continu iate aircraft •ecord. applicable airworthiness requirements. ed conformity with the L DFX(MPTION OF WORX ACOMPLIWIFO (If more croft ncdionality and registration mark space is required. attach additional sheets. Identify with bi- and date work completed.) The following major Gulfstream Aerospace Aircraft•Service Change s have been incorporated: . . . ASC.#135 = ECS .PaCk Sequetielog',G uringlEngine Start - ASC #137 G-111 HMI Dedicated hydraulic Filter - Installation The effect of these changes on the aircraft's_ basic weight and balanc e are negligible. WhiY_GiAji3275#2031 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241183 EFTA01326776 FAA AIRCRAFT /dC1STIT CAMERA PO. a? DAM - /3 - 57/11 • DIA01107 OF TWISIVIDAWNI eO at Fa. -• • Fillasi AVIATION AOMPIISTUIDON- 49 9 2 o . 44 . e./j.. MO; 04- R060.1 'FOR PAA USE ONLY MAJOR REPAIR AND ALTERA1113i9V),,,, ." 0 047 OFTKE. IDROFICATION • (Airframe, Powerplant, Propeller, or ApplioneaVaa v 'Y -C.' "C;_. INSTRUCTIONS, Pain of type all aught' See FAR 45.9, FAR 4) Appnadia 8, sad AC 43.9-I for nbsentene it Vilna diete00 fur en.ereaieei and dispo34104 of ibis form. .-1 • MAKE MODEL Gultstrean Aerospace Corp. 0-Ill ( r‘ -j I. MtUAR SERIAL NO. NADI:MAW( AND REGISTRATION A9 9/RR 1085 ..- . OS& N880A MANE (As 'Lawn en snistersPop affilicetel . ADM-SS (A. .bon au Nipidtalicia cuntmotel 7. °WWI BA Leasing and Capital Two Emhargadero Center Corporation San Francisco, CA 94111 - 3. FON FAA ME OM 4. UNIT IIIINTIFKATIMI s im Mitt 1 MAO . Ø 'is,. NO. ilt/sill WO. ' JØ A2MAla ••••••••••• (A ~lied il Ova I Sore) POwTOLI•HT PII01111ER 'YU Cockpit Voice Recorder MOO 53674 x APPLIANCE SW4WArnitall , - Fairchild , V F. CONFORMITY SIATEMDIT ' . A. AGENCY'S NAME AND ADDRESS a. KIND OF AGENCY C. CERTIFICATE NO tit. Cletif CAM KIChanK Western Canaander, Inc. •Canis a BletICATIO MIONSC < RAIR808L APR. 3, 4 16900 Daily_Drive ' Radio 1, 2 å 3 . Van Nuys, tit 91406 . E' nitonart RIME li mion Limited Powerplant, mu.VIACIVan Instrument & Ace. D. I «nit( Ow On awls end/o• alwidon ede to the wigs) identified in hem I non sad desnind on the titer.. oe anarbennes hereto lave bien node In nowinace with he feqoineenta of Pan 43 ad Jr V.S. adinl Aviation Regobona and dui the inketaatien furalnal barren ia we atill nation act ne bed of an knowledge. DATE . =NATURE OF AUTHORIZC Le l. 5 7"'" t• 8-TO • • N t J. Arno FT FOR UM TO Siena Paaaaa na to Ion anbority In ponninecited bond the oak Egynainal i. Item 4 -a inward n an'tnanet pennant by tbe Annie, o( es. Federal .A.istna A.Wittiacrneo and is al. APPROVED R EJECI RD in Tu. StAtnArs annfl." 1 1 mAndmausta. Onteacea ALITICOLTAMM oMclot SY CAMPY. btrAttady41 c MA 04SanaTA , Wm» Dane• IN tnestOn ~KIM • t o o tpØ " " ' DATE Of APPROVAL OR . CERT111CATE OA SIGNATURE Of AUTHORIZED INDIVIDUAL REJECTION , DESIGNATION NO . , ...i f 9 - 28-90 . . -4eae.- CP CZ.1 / FAA Form 337 then oast do O. moo (83701 • SDNY_GM_02754262 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241184 EFTA01326777 FAA AIRCP.AFI REGISIIT CAMERA 110. _ Malt ea— /Or n, • 14CitiCt • ma y - in the ppisfopriote aircraft recent Weight and balcince or operating limitation aangesAoltbi inroad , (reassure Coatipoed conformity with the An alteration most be compolible‘wills all previous allproliiins --. applkabli critworthiness requirententw ... . - • • . sheets. Identify with air. 8. DESUITT1OR OF WM AttOlAtt1140 (II more secant illeitilred, attach additional croft nationality and registration' mark and date work completed.) . • ; • Cockpit Voice - Added Dndereater GocatinO1Device to Fairchild Model A100 Systems, Fairchild Recorder, Serial ylvieber_53614,. hi' complying with Loral Data Modification 7 hes Aviation Recorders, Field' ServiceiDulietin. Berber cvit•aSee - . • - beau marked oo..the Nedificatiop Plate. "• requirements of, and The Voice Recorder.inakellatiiiii-in this airplitoe Melts the easei1O withIPAC.91:605.. (dl)_: (e); FAR 25.1457 (a1),(a2),(6),(e),(d),(0), • • • tc- • 1 noe4;sto,q4aOfAtir 44‘ t - "N" SDNY G0.4_02754263- SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241I85 EFTA01326778 \NM r,M-,AllteRATT CAI4TILA w0. ap DATE: e2- /3— 9/ . • Keen *moves — OMR No. 120•OZD 0 MAJOR REPAIR AND ALTERATION us moans FOY FAA LINO* a sastateen (Airirame, Powerplant, Propeller, or Apparent) . Oros kleleteketien Podert•••••••• ilerfeeswelke S2) I- — rst> INSTRUCTIONS. Print oe type all entries. See FAR CA FAR 43 Apparel' Et. and AC 4194 (or subsebuent revision thereof) for instructions and catoositionol this loon. This report le illaulflid by taw 09 U.S.C.1411). Future to rayon can resist I solve penalty not to estee211.400 fat each such notation (Section poi Federal Aviation Ad of 1954). . Make Model GOLPSTREAM AEROSPACE CORP. . G-IV 1. Astro Serial No, Naisoremywern Merit . i 085 11 Sens Ms short on topttrigke mellow ' Adder;Ma shown ms repiatratlon Cerlfdeetel BA LEASING A CAPITAL CORP. TWO EMBARCADERO CENTER &Owner ' SAN FRA:NELES1 30 - 09c•-• •-•94111 . I • 1.ForPAAUse00, P. • IF • 4. Unit letantlecaton S. Type Unit Make Model Senal No. Repair i Aittration I._ • AIRFhAME . (As darned' Item I above XX POWERPLANT 1 ' PROPELLER I Type i . ..,- Aetna Maistachne• 6. Contomaty Stliallallee A. Agency's Name end Address ). Kind ci APR*•• • : i•• C. Ceara' No. us cenegasseMicaesic • LANCE A. MATTESON Fame CarelialeiMann • • 3015 NORTH BUDS ROAD AP 1864049 aninetned flaw Samos .i i SCOTTSDALE, AZ. 85251 • .. kraniAaner D. I certify that the repast and/or alteration made to the urn(s)elsotsfsed in AIM 4 above end described on the resat.01,1LlautientaPatti: Mn bola maws in women« wan ins nowemenisca Pan 43 of me DS. Federal Anabon Fleautsbons and that she infaimatem turneshed lino is two arse Cereal to the but of my rowledge. Owe Regnante* of A ividualz . 4,...7, /5, qto•L t'APPreval tor Rant To Sande "5.0—- .-.f SitastLLstient,... . Purloin, to the atahontY yetipens'absented belOw. IMt identified in tleM 4 twn inspeeted in the manna emcee by the ACIII.MalratOf al the Federal Avow Administriban ono is APPROVED - 0 REJECTED FAA Fe. Stittsfaras let Opt (Specify) etsdeCke u•nosautx i wspactianAUlbOriZttiOn BY FAA pewee Rae Station , . . Pawn nopand by Tension osia oi Approval°, asecnon canna* Ot Signature of nelnid neon No. Alt CI 1 Of I 9 ID °511705484: . ''. Michael y FAA Furor 2 7 • -- _ - 1:W4in- . • ••• SONY GM 02754264 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241186 EFTA01326779 • ; IAA AIRCWOMREGISTRI CAMERA RO. Q bATL:4,- NOTICE Weigh! endbalance or operatinglinUfation changesshailbe enteredin thiaapprOpriala airmenrecord. An'arteration muttbe • compatible with allprevious afterabona to &nun continued conformity with the applicable airworrhinen requirstmillt. I. Description et ork AO>teeplbrie0 in mon space le Moroi attach additional enema klerwly withrain naaywwy one regotnicen wad and 0at@ *Ore COntOtelett) Aug. 08, 1990. Gulfstream.Aeroepace Corp. Model G-IV, sin 1085, NO8GA, Aircraft Type Certificate Data Sheet Al2E.A. . Refer to: FAA FORM 337 dated1-1S-90, for the-above referred to aircraft. The purpose of this alteration--is-to-remove the -changes that were incorporated to the Auxiliary-Power Chit (APO) Surge Valve Control circuits, as detailed on the above referred to FAA FORM 337, and return the Surge Valve's circuit to it's original.certificated configuration. In the Aux Power Relay and Junction box (39A1) performed the following wiring changes: Removed vire H70C20 from relay 339A1X1115 position B2, routed the vire along existing vire runs to 339A1TJAN position C, cut the vire to length, stripped the insulation from the free end, crimp installed a new CTS-520/20 contact onto the prepared vire and inserted the wire/contact into TJ1N position C; Removed and discarded wire H77MF22 from 339A1X115 B1 and 339A1TJR position Er Inserted a new CTS-S16/16 contact into 339A1XR15 position B2 and position Bl; Secured all of the wiring, components, and access of the 339A1 Aux Power Relay Junction Box. . All installed parts.vere purchased new and comply with the appropriate parts of FAR 21.503 (b)(1)(2)(4). Tested the alteration by :rising the FAA Approved aircraft flight manual procedures for starting, rift:ping, and stopping the APO'and noted no abnormal operation, indication or performance. ' Returned the aircraft to flight status, recorded compliance with this FAA FORM 337 in the aircraft's maintenance records. It has been determined that the interrelationship between this change and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. The effect upon the electrical load analysis and the weight and balance of this aircraft as a result of this change vas negligible and no changes to either report were made. . END 08/08/90fted/89mf"" 0 Additional Sheets Am Allacttl. • SDNY GM 02754265 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241187 EFTA01326780 FAA AlliCtlar 110187 • CAN1RA N0e7 N Dills ft - 2040 . roan hltreved MAJOR REPAIR AND ALTERATION OW No.2120-0320 0 al alarm. a kneroshof , (Airframe, Powerplant, Propeller, or Appliance) i Por FAA Use Ordy ildliSININSR . 1 116117864ran INSTRUCTIONS: Print or type ell trees. See FAR43.9. and dispowlien of nu form. This reporttsi•Rufreeb FAR 43 Appendet El. endAC43.2-1(oesubeertuent . rerbionthereo0fOrInelructIons for eacn NIA violation (Section 901 federal yisw(49t4S.c.101).Failureto repent= npeelOn 4 CBI penlityno Arinion Aa of 1964). t lo evad$1.000 Mane • Moe* GOLPSTREAm AEROSPACE CORP. 1. *boron G—IY Serial tex taboret*, ono Refrotretion Min 1085 - N880A Name (As shown on mgestrionetakee te) hocIress (As Uptown on nvierwan awakes) BA LEASING 8 CAPITAL CORP. 3 Oar TWO EMBARCADERO CENTER • . SAN FRANCISCO CA. 94111 3. For FAA Use 0 I. UM kliontlikstlan , a Trot tem make mese Sens NO. . fterau Atieralion •• • ,, ' . . • raFPAIAE Ms clasintielIn Rem I Send • XX . j.." PONERPLANT . ,. PROPELLER •Type • I I • , a CorionarlySleleinel A. Agenets learns am A600121 B. Kneel , C. Gramme No. LANCE A. pairssow -- • 3015 NORTH HAYDEN ROAD SCOTTSDALE. AZ. 85251 AP 1864049 . '0.ieermymmummeerammeweneemeaftioew4 here been nudeIn acoyedence fen the tadonIne reverse or &Revenant nereio refenteart44,4 funnels) tete Plea ancl Oyenlo to the ligterons and the, the tnforrimbert best ol flyer Date S .... - r Anis. kw - -pt. of Maintenance Pas* to the Sae* Shen ;Sans specitiett beet Orkplet4dentefee fa de AdTabittlitit of the ',Clem, Mt° 4 hes Women Sine manner prescribed by Ataseustraka and b AD APPOOWIO . 0 REACTED - Me Fizellarniforris r •- - woodmen. OtteISPearr) x bispectanAgoineczeon BY FAA Deephee. Repay Station tBetNAN NIWOOtensmom I lainemeAtroronlass Oats 01443900WIlor Resection cemlate or SWAIM, Daignaaenwo. 6 -.1.8 —RO 126705494 . AA Fora aA fo Michael D an Ily SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241188 EFTA01326781 e. .tAtit,(1):SW- : • I FAA AlICRAFF *Emma CAMERA WE./ DATES 12 NOTICE • Weight and balanceor °panting limitation changes shall beentered in theappropriate aircraft record. An alteration Must O• , compatible with all previous alterations to mute continued conformity with Ma applicable airworthiness requirements. 0. disMpbort of Wmt Aacoi.eSMd in more space is emoted. atoo astrhbansf shifts. Identily Win eltaWInationentyyna registration man and daft work computed.) June 28, 1990. Gulfstream•Aexospace Corp. Model G-IV, s/n 1085, 688GA, Aircraft Type Certificate Data Sheet Al2EA. Refer to: FAA APPROVED Gullstream Aerospace Corp.-(GAC) optional Aircraft Service Change (ABC) No. 131 subject: LIGHTING (ATA-33), TAXI LIGHT POSITIVE CONTROL-MODIFICATEON,.dated February 26, 1990. sheet 1 of 3) 33-1-3, page 3, dated January 23/88. This ASC modifies the taxi light circuitry to ensure the tax( lights go off whenever the landing gear is raised. . • Complied with all of the instructions contained in the 6SC; except as noted herein: (Refer to figure- 2, page 7 of the instructions) instead of the in-line diode module part number 1159SCAV-903 utilized an existing spare rail mount diode assembly Deutsch part number CTJ420E011 and connected the wires as follows: (a) Wire L9001A20 to position A; Wire L9000A20 to position B; Wire G66AA20 to position F; and vire L9000B20 to position G. Note the existing rail mounted diode assembly has identical ratings as the in-line diode furnished with the ASC and, in addition, offers a more secure mount, spare parts commonalty, and a neater installation, (b) Figure 2 shows 326A1J4 and 324A1P4 incorrectlY,'Vire number L9000D20 is connected.to 326A1P4 position small Fend vire number L9000C20 is connected to 326A1J4 position small P. Note 326A1 is part of MAIN JCT'AND RELAY PANEL i2. - -- (c) Wire L540A20N vas removed from 823 position H, the drawing and text - list HIS/position - - All-Initalled parts were purchased from GAC and comply with the appropiiate parts of PAR 21.303 (b)(1)(2)(4). 'Successfully performed the ASC's operational check after replacing the defective left taxi- light with a new GE 4587 lamp, returned the aircraft to flight itatus,:recorded cempliance with this ASC in the aircraft's maintenance records, and returned the completed ASC compliance card to GAC. - • It has been determined that the interrelationship between this change -and any previously approved configuration vill'sot introduce any adverse effect upon the airvorthiriess of the aircraft. This determination included, but vas not limited to, consideration that any deviations to the original. ASC- would - not change the intent, operation, or test procedures. • _ _ The effect upon the electrical'load analysis and the weight and balance of this aiccraft'as a'result of this change vas -negligible -and no changes to either report vere made. - . END ❑ Additional SIMMSAn .AttiChld • SDNY GM_02754267 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241189 EFTA01326782 1434rDt ,fl :•:3.4 FAA AIRCF.AfT itEczrat CAXLP.L PD.i N DATES 72 . . Fonn AOINOvild owe No. 91200020 0 MAJOR REPAIR AND ALTERATION uSononeen tForuF IdentificAAatioUnm** Asaeoneen (Airframe, PowmplarA Piapolier, Of Appliance) - °Moe ii............ _ HarassHarassHarass , PO 7 - INSTRUCTIONS: hrint Cirtype all *nue.. Sear/ACE FARMIAppendia El.m0044394 (or sitteepirant Mahan that/1100 Mr inshudinnt and disooNtion of anslorret.PMraper is required bylaw/(49U-S.C. 1121). Failure le tepottean mannIn a chid penally not to exceed 91.000 for each such violation (Section 901 Federal Aviation Act Cit INS).. - . . Make PAWS GULFSTREAM AEROSPACE CORP. G -IV 1. Aka* Wel No. r NFIFFISFY and Fleantration Mark 1085 - N88GA Nemo (As shown on icestranon onstPCO) Midas, (AS Ahern OnIlpiglatiOn Candlelit*, BA LEASING 8 CAPITAL CORP.. TWO EMBARCADERO CENTER tower SAN FRANCISCO CA. - 94111 :. •3; ferFAAlls•Oida .... a. Unit identdAmion S. Typo Unit /Asks Mode Seal No. Repaa' Alteration MRCAAME (A. ONO NO It show,' XX ,T :.• POWERFIAM , b a AMPULLA Type APRJNCE Manuiscaens • - a. Conlennily Satan A. Agency* Men' end Addams Ca Kind of ArienCy - C. Corolicat• No. u.S. Genera. illaCtsVC . LANCE A.,MATTESON - ' . . 'wain Glin4001,10.4•OUSC 3015 NORTH -HAYDEN ROAD • conarammasesimen AP 1864049 'SCOTTSDALE,—A2. 85251 . Minutattair -0. I Wrote that tharepaa antIANaltaraitomnade loth,Lineal tdonulied in demo ahoy* and agameed on the mangy:gamy-Anent, hemp have been nada in atelNelanel with me requirements ol Pan a3 elm* U.S. Federal Aviation Regulators and that ma ntormation luenished herein C Ma and Canna to MeatN of my knowl•d9ll- .,. . Yip ' Ora 4.,C "1:2-7 If Pe • 1 ' c L....-. C , 1 Apron'I itre Reba r 0 tormiceStiot . of Maintenance . purr a) We autheety pen omen SPeCifted 0810w. ‘011roil kit040•0 in item a was irameeteil In he mwr plasaited by the Adminlalrator of Me Feint Milton Admintatrabon 'and is . , X3 APPROVED .13 REJECTED FAA FR. Stanclattb /- OlharISPOW . InWector t Insincton Mithentarion BY i - " FAA NW*. • 'Room SUNNI Pinion Arnroved hY TranSOOn Canada Mr.cordnesa is 1ii Dataeapproval as RapICIPOn ' 'Gotham de Sionanot ea -- 4, '03 —cp . • liDestora,on No. ' t26765494 - • FAA Fenn DV arm. • Michael Doz. ! Ily SONY GM_02754268 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241190 EFTA01326783 •7 tion must oa rd. Anal:ora NOTICE 0 Pr la ti !Urfelfler thMen requiroomon- M the eillX e aipl.cable einvor Nr be 'Mead ish th g lim itatio n cftargeaahittlnued curtormity w e or O pe ra tin as su re co balanc ons to Waive and with all previous alterato *04 oaTem ez/ compatible riS tra ti3n en list and tin , llOrlibYr and nf /n 1085 , N88GA pl ish es ; a w or dy with 'IWO na - I V , s n of Wal t Accom ach adOilional fl e Model G a. Deatplio Muiresl, an e Corp. Of MOO sons, a m A erospac Al2EA. Gulfst r e a Sheet nded , 1990. ertificate Dat recomme u n e 2 8 C o r p . (GAC) T A - 2 4), J t,Type C rospace RICAL (A Dog Aircraf G u l f s t ream Ae subject: ELECT tioner (Watch g P R O V E D . 1 3 0 l C o n d i V W i r i n AP No na -I o: FAA e (ASC) ment Sig 1990, G cator Refer t Service Chang Engine Instru d January_30, strument Indi t e n g Aircraf ns for Standby tallation, dat andby Engine I nd G-IV Wirin o s t a Provisi st Citcuit-In 1159AV40192, S nuary 19/90; dim a n d t est Te raving a dated J nciator Lights Timer) Manual -d Page -2, nu • Diagram of 1) 77-3-1. 159AV40129 An nuary 23/88. 1 1 Ja (sheet Manual drawing age 3, -dated - tandby engine p r D i a g r a m o f 3 ) 3 3- 1 - 3 , c u i t f or . the s al conditione its r n (sheet 1 f o r a test ci S C F 4 1 2 -17 sig complished in NS 159 ac t a ROVISIO ioner. The 1 his ASC may be be replaced a C adds P it n: " T r may This AS t signal. cond t r i t i o cond i t i o n e en h at instrum eplaced throug 412-17.signal r viii be and the 1159S CP t as , excep entiret te. y e d i n the ASC ns) utilized a contain e instructio later d uctions th tandby o f t h e instr 2, page 7 of ction to the S . Note i t h a l l f i g u r e e c o n n e t i o n 5 3 d w fer to for th I posi ilized Complie e in: (Re 101205 contact onnector 92A1P s contact; ut 20 and d h e r note G A C8 35 9 2 A 1 ) c f o r t h i W 8 8 8 A sting ner -( ber ires the exi gnal Conditio rrect part num onnection of w sition A vas e S i n c o e c p o figure Engin ts an i d of. A forth 5A1P51 because listed on the e 5 lis ct triangl ition V instea 5A1J51 and 32 t i v i t y c o r r e a r e p o s t o rs 3 2 o t e t h e effec 06-1054). The f the G-IV' sp e c N 10 o at conn .vice.. t (a/c note 2 W888620 by an existing 1 is incorrec d in triangle u p i e d a t P 5 l i s t e o v e . occ ion ).as ab connect 06-1095 rred to for the ty -is (a/c 10 59AV40192 refe h the t i v i l 1 1 ply wit effec D i a g r am Manu a m G A C and com Wiring f r o chased )(2)(4) . ere pur raft a l l e d parts w R 21'.303 (b)(1 he airc urned t ONER Part i l i n s t s o f F A a t , r e t I A rt ity te CONDIT iate pa continu SIGNAL appropr he ASC's INE INSTRUMENT rack 92A1, rec and orded o r m e d - t G , y ' p e r f D B Y E N l e d i n e c o r d s full N with STA 05891020 insta s maintenance l r Success status n t ' l i g h t 1 3 s / c r a f to f 412- e air GAC. 1159SCF C in th card to nge No. GAC e with this-AS C -compliance his cha "compli a n t m p l e t e d A S h i p b e tween t any n57ersn s d the co elation not introduce tion returne e interr . a m i n e d that th iguration will This - determin tions to n d e t e r e d c o n f c r a f t . d e v i a e v y It has be ly appro the air that an st a n y p revious rworthineis.of consideration ration, or te and t h e a i e d t o , e n t , o p e upon imit -int effect , but vas - riot l oi change the d include nal ASC-would:r i balance ht and the ori rei. gi t he weig .: s a n d nd o n procedu l o a d analysi as negligible a trical ange w thrplec this ch e e f f e c t upon at a'result.oi . Th t e aircraf ere mad of this report w g e s t o either chan ,„, SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 104,7;,°754715-17 EFTA01326784 ta, 0 lel Orconin . MAJOR REPA al ereAla•A leasv ea (Aid tame, IR Powerplant, Pr AND ALTERATION Ada APProved leh ebasils. . OMR No. 2120-00 s opeller, or A 22 . pplianinl) ' fa FAA Use On INSTRUCTIONS Office Identfike ly :Print or type MI :. tion end Peptone entries. Se ley nee we s, of "tea. ll viol:bon las mond nae EN241.2. FAR a Apperax41 0 P (97 ' (Section 90I hoes Av iad bytadatitU .arl AC atkt (or - SC.142u. Fala iation AO of 19 i° report caea sed ant Raton ther -' - Make 58). nnon in•arilye eoftfor naity not battaataxans I. Alava GULPSTREAM AERO . al DISCO Sad No. SPACE CORP. 1085 • '. G-IV New (At Se - 0770afiy ad Regle 2. Caw em coref BA LEASINitlGrat&ilineCA etlileate) NBEIGA ardion teat PITAL • .CO . . . RP. Adam OF Mown On reg .. TWO 'EM ist len Irl BARCratAD iel ERO lelCENTER I. feria Use Only - Unit & Una tranducati on ' areal 5. Type Saud No. Amid AtterA.zn AS de 4 000 born POWERPI.AKT XX eaeOeFtLf9I .. Type APSUNCIE IlIaleiSaetwer I A Arca , * Mane an d Mitten S. LANCE - MATTESO 9. Rind of 3015 NOA.RT Mara H N A VS.C.reseed44 0 Ceara Na HA YD SCOTTSDALE, AZ. ROADEN lea .41:Aarae • reeGelikele04 140IY 85251. _ Oirtecaleci ANY Slaw A4 0. I ands mat the Met been suet ropes estypor SRrneonmath AP I664049 in accede to the tin to) lueraill IS OM is dee en nce we me adAreeriera at Pastenetrntho epee mote and One d coned to IN, best at My rt 43 at ihel.A .S. Federal Av described on the ritae14090. aeran Regu ~soot lation an ho MUChenents Motto d t the elletena Led Jrreerer I 7./ "f eta - ' • ' • FC' Ant ant to me . 7 Aprotalke antinistrator ot eulhOries Whin pistons Rave TO Spree . us the fan Ag specified bar. WF no laia atraistra the ea Iodated IF1t4mo rl,- v FAA fit Dattala . , nen add " 0, in elan 4 an APPROVED inepeeted in the Tanner Inspector 0 REJE-C11912. preicritted by the BY ' . - • -. Ote4MISD FAA Di OOFF1 leers. Pepin Seabe Oen of Ap e Pasonleiwor proval Or Mart el by TeSelipo ian Gera Airea rdenen Grove n . 6 -,z7- 9)O Certhate or OlOgnatton No. . • at 526705494 /4? .e. fel -rr' s- VOA c•aissa;4 027542--r SUBJECT TO P 8, 9, 10, 15, and 17 ROTECTIVE OR DER PARAGRA PHS 7, EFTA 00241 EFTA01326785 1 1'7 FAA AlwCTAYI XTGIHIAY CAmERA NO.!.N DATZI 12 - .r NOTICE' weight and balance or operatinglimita compatible with all previous alteqationstion changes shallbe enteredin the appropilate ahcrak record lonstnecOntinuedcoaformitywith theapplicableastw . An alleration AAnmat be orthenessrequiroments. L DoserLitlowel Welt ACconSed (II mere space at resold. much • SWIMS :Sniffy *Oh strati netionafity and agitelyttion rivek she June 27, 1990. Gulfstre and date work completed.) am Aerospace Corp. Model G-IV, Aircraft Type Certificate Data s/n 1065, NEIAGA, Sheet Al2EA. Refer to: FAA APPROVED Gulf stream. Aerospace Corp. (GAC) Aircraft Service Change (AS recommended C) No.. 170 sub: AIR-CONDITIO Cockpit/Cabin Temperature sens NING (ATA-21), or power source-rebus, dated 1990;. GAC G-IV Wiring Diag March 30, ram -Manual drawing 1159AV40103, DISTRIBUTION, (sheet_1-ot- DC 2) 2475-1, Page 3.,_dated annuary19 POWER^ Military Standard MS35336; /20k_ and MS51957: This ASC moves the power sour ce ofcabin and cockpit temp system from the right main 28'V erature control olt DC Bus to the essentia hue. • . l 2U'Volt DC . . Complied with all of the inst ructions contained in the ASC, noted herein: Wire P615AB14 except as was removed from the aircraft discarded, a new vire was and stamped and identified P602 between CH212 and 08292 AF10 and connected and a MS51957-43 acre:, vas inst connecting the vire, bus bar alled at CH292 P603AD10 vas removed from and circuit breaker together prop the aircraft and discarded, erly; Wire stamped and identified P600AG10 a new wire vas and a MS51967-43 screw and conn ecte d between CB214 and CH256 vas installed at CB256 connecti bar.and circuit breaker ng the vire, bus together. properly; Wire P615 P615214 were not removed fro AA12 and Wire m the aircraft. These devi original ASC were done to ations from the conform to production chan incorporated in aircraft s/n ges that have been 1120 and subsequent and prov wire/circuit breaker matching ide for•proper ; see:.FAA AC 43.13-1A para • 429*, b., c. All installed parts were inst . alled - new and comply with parts of FAR 21.303 (b)(1)(2 the appropriate )(4). Succeisfullyperformed the ASC'a operational test, retu to flight statue, recorded rned the aircraft CoMpliance'vith this ASC in maintenance recordi, retu the 4ircraft's rned coMpleted compliance card to CAC. It has been. determined thatille Interrelationship and any previousli, appr between this change ovedTedefigOration vill.not effect upon the aitiforibine introduce any adverse ei 'of thw:aircraft. This included, but was -dot determination limi to the original ASC woul ted to; (a) consideration that any deviations d not chinge.the intent, oper procedures, (b) Aircraft qual ation; or test for the current reqUirem ity vire vas-used that vas elitd,-operating temperatures the correct size conditions, and (c) the , -and environmental installed equipment will that will not interfere'vi function in a manner tfi OthiadVersely effec't the aircraft. . the safe operation of The effect upon the electriCal.l of this aircraft-as a oad analysis and the weig result of-this change vas ht and balance changes to either repo negligible and no rt vere'made. ArialionailloitaAni AttaCted • . , 2 : • a t 41,— :an ts . SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241193 EFTA01326786 FAA AIRCRAFT REGISTRY. CAHERA NC. 3 N DATE: 70-23-90 • roan Approved-- 0 MAJOR REPAIR AND ALTERATION - oue No. 21204320 • • rroarocooNo (Airframe, Powerplonl, Propeller, or Appliance) For FAA LW OS! federensist Mop loomilication MINSIanaie. L—Pra"DOg.--D INSTRUCTIONS:POW ortypfli entries.Se•PAR43.9.FAR43 AppenomB. and AC432-1 (orsubsaquarand slon thereof} forinstructionS and disPosition Ofthis form. This nowt 4 rewired try law (49 U.S.C. 1421). Failure to wort owl WW1 Macivil penally wit to Mad 91.003 lot each such violation (Erion 901 Federal AvWion Act of 196$). MSe Modal ' GULFSTREAM AEROSPACE CORP. G —I V 1 Alectill SSW HO. 1°85 Nationality and Jr N88G Mart • - .—i "awitlitatfirg2IrtCatch CORP. Ana. (Al a wn EhtDrEtergE aR t it aNIT ER 2. Owner - SAN FRANCISCO CA. 94111 3. For FAA Use Only • • • 4. Unit Idenbfeation . 11 Type Unit Mite Model Serial No. ENS Allegation ' AIMS/4 MS ti• NW wove) XX POWER/I-Oa PROPELLER .. Type . APPUANCE • I. Canfonnity St.te'wca A. Aroney'e HAM and AWNS ft Kind of genet C. Canifiewa No. \ - Z ertecated Wenn.< 11.1.C— • • LANCE -A. MATTESON . ' Fan. Canaan° Lot-n.4 ' 2407 EAST SHEA BLVD. . Congesiad Remo Simon AP 1864049 PHOENIX, ARIZONA 85028 Menotarkeee . D. I comfy thattWi101it andimaltanton maw to me °win ciontareo in non • now: ono oltalloa .../ on too . ererseoraltacomeus onto Pave been made in scoivtlarca with the tileenceineKAS a Pert Cot the U.S. Federal Aviation Finulations and that mile inlormation . • furnished herein it trims and cornea to the beat of my Way/ledge. - Dee — Eismatontol 12/27/89 --- t........— i . . 7. AppenW fee Pan. roterviceSupt . of Maintenance PurSuant tO Ole atietentr Peen Pimae specified below the unit Melded In Ilan 4 erne inspected in the manner orescnbrel by Aeounistrwor or the Foam ANolke Arinistrabon sore X c APPROVED the 0 REJECTED FAA FILSiondatds Other (SPOT/ Instlede44 Manutoceat . InedeCbco AuthOnZabOn eV : 2 Ic FAA awn* . spur Station Anon Approval byTningerl Canada AirmOrthinala Group Date of Approve or Ropcoon ConNoote or Dosignatal No. / 2-27.4? 526705494 FAA Form 33) At. Michael Donnell • SDNY_GM 027641272 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFIA_00241194 EFTA01326787 FAA AIRCRAFT'REGISTRY CAMERA MO. I N DATE : 10-23-90 rea.giu and lan compatage ba CtOf ore.sang amaa 'NOTICE with au preveric a atm 'ie.onshon chendee quillbe angledmin • Ao attute continu ed conformity e appmpitata wan Ina ap fulcra:t record. An afternoonm p4e4ble Stewart I 046600100 of hin•SS 100010 111 ust:* HI win space 06 0 t1tC4106100110 As mewed 011/. inethetilettionet sn ails ;Sway with ancsa la hation>lity end reptsfrab0n mark DECEMBER 27 anctOent croft , completed) 1085 N88GA, 19 89 . cpizsiltAx Aircraft Ty AEROSPACE pe Certific CORP. (GAG ate Data ) MO REFER TO: FAA APPROV Sheet Al2E DEL G-IV. s/n Maintenanc ED STC No A. e . SA111NE, INSTALLATI Manual ATA Chapter dated Nove ON HANDBOOK 49; mber 24 31-0251A Se cond Edit AIRBORNE AU Garrett Turbine Engi , 1982; GAC. ion. XILIARY PO ne Compan WER UNITS, y, The purpos TURBINES e of this cooling ai ?I r inlet th teration is to prov thus prec at is enti ide a sepa -... luding the re ra interactio possibilit ly separate from th te sourc - n between y of cool e co mpresse cooling ai ing system °>33 inlet, rflow and st Inatalled compressor arvation and, any, A new PATS ai rflow. APU's inbo FAA PNA p/ ard enclos NAS1103-3 ure wall. n 430206-9 LOUVER as bolts: 5 Attachment sembly on that.vere each AN96 was acco tcpthe attached 0C with 10 ea 10L washers; 5 each mplished with S each ch Ms2042 MS 21 05 9- L3 nutpla Fabricated 7M3-3 rive tes a blanking ts. thick that plate usin vi ll cover the g 4304 Stainl • Installed existing p/ ess source us the blanki ng plate n 3708913- Steel 0.040 inches ing existi to cover th 101 ' ng har4va re. e original flame arrester. Secured AP co mp ar tm en U compartm t inlet ent.. Performed op procedures erational test of Au Manual an contained in the ai xiliary Pgwer Unit d rcraft's FA after the noted no abnormal using the operationa or unusual A approved Aircraft l test. operation Flight Returned th before, du ring or e aircraft su?plement to flight s were re status. No guired -Or - flight ma . thAtaIied nual re It has been as a reIb de te rmined that lt of thin visions or anC any pr the altaratior ev - adverse ef iously approVed co interrelationship fect upon nfigUratio be tw een this ch determinat the airwor n will' not ange ion includ thiness of introduce design of es the APU co , but is not limi the aircraft. This any not allow mp te fire migrat artment and access d to, consideratio of a fire n that the proof chec ion into other ar ory cooling arrang satisfacto k eas emen rily since valve and an identi of the aircraft th t will GI159A V5GF .2982 one ca ru aircraft. G1159 airc l louver has operat the use raft and si ed The effect nc e 1984 on on the airc a raft's weig ht and ba END OP TAIS lance repo - SHEET"" rt is neglig no additi ible. onal shee ts are atta ched ❑ Add,tA503/ Str eets Are Arlalled SONY _can 02754273 SUBJECT TO P andE1m7s'* RO TECTIVE ORDE R PARAGRAPH S 7, 8, 9, 10, 1 5, 0024 EFTA01326788 Yak AIRCRAFT REGISTRY . CAMERA NO. 3"41 DATE: /0.;23-',0 • . . • 0/413 .21200CCO . 0 MAJOR REPAIR *100 ALTERATION For FAA Use Only of Oecomen Oterecorine (Airframe, Powerplant, Propeller, or Appliance) Mai Identleateht Padteh•Sa elebinette Atee 59- F5D0 - 1.1 tneeeehons Appeams EL enp A. -13.9.1 wa teeetwent revision thereof) tot INSTRUCTIONS:Print or typo ell emnes.See FAR 43.9. FAR4i I'allure la reoretcan Mutt In annopenany nOt toexceedS1.000 . and ditposniOn Of MIS Item'. This tenon is mquirad tnitlw MAU S.C. 1421I. 'or etch yeti% wciatiOn 'Wean SO, Federal *moon Arlo! ,jaj. •—..— . L Mold Nee GIV • • ' GOLFSTREAM. AEROSPACE CORPORATION I. Akeratt . r Nationaltyandflegisuation HUM Sena' Na .. • N449GA 1085 Namnr=i1118"ffigint CORPORATION "- • cSAN itettaintigteriltili n FRANCISCO CA 94111 _ 7_ Owner .1 For FAA Use Only r OVe • 4. Unit IdendlleatIon • Roper Metals:a Nadel '• • CAI deketted in nem I aporey l AMERADA -- Th PCNIERPLAIif rl PR9PELLER JAN 04 990 Type E. • APPLIANCE - tAID-SOUT i F:S00 laansdacturr, ATLANTApA. • A cennnety swam* B. Kind of Arley C. C;rbeAllItio. A. Agoney's Nears and MIMS • US. Centeetea lehawee GULFSTREAM AEROSPACE ?CORPORATION • . !nen CerutcalldIalquali GR4R216M P.O. BOX 2206 - TRAVIS FIELD Cenorsteo Aeon Storm . SAVANNAH r GA i1402-2206 WalolettUre, itlentele0 In item 4 neon smadescntred on the revealor atiaehrnents hereto CA! seemlythat'll, repair andior alteration made to Dion hal and mat the information teelterentents al Part 43 of to DS. Feoend Aviation Regulations ben at" made in accordance will the ' turnoned herein n. true and coma to ter beet 07 tort hlehafee0h. . hate 41. SOIWtire iel AuthOrhe 3 Irelledual ' • . . •PATRICK J. LYNCH Ger...g • .......a... 12/01/89 ... 7. Approval ter Return Ye Enke in Men a wee laseletteel Si the manner pr•SCebett by OW Puritan. to ine bt/Mority given persons speafied below. IM unn identified ['REJECTED Administrator of dm Feders1 Aviation Administration and is X3 APPREV.0 lOther (SPIelly) . I i FAA Alt Standards insmiction Aumonzation • • laaniAaelwer I iltoaCtei BY I StibOn Pete AVOrched bY ThlettOtel I. • Repot Senjoiiterwettlerellt cite.* I F" Deign". Certilleate or httAittire ol Atith0,40 labVidal (Mehl APPrOvill or thejeCtiOn • . ...--e.-4.. ' 12/01/89* De4ignabon No. GR4R216M •• PATRICK J. LYNCH Pa. FAA Pena 337 neap ....II, • • EZt •(:410 SONY CM_02T54274 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241196 EFTA01326789 FAA AIRCRAFT FEGISTRY CAMERA NO. 3 A' DATE: 1072i -PO NOTIC E f. sshalI be entered in the alitirOpP ale airCraii recurs!. An alleratiOn must limitatio nchanse requirementa Weight and balance r operatin g d conform ity with the applicable airworthiness ns tO assure continue compatible with all previous alteratio d.) I. OesalOCM of Wort ACMTIVIWVW • t* mar' *AO Cate walk complete aerial', nationality and reps:rei addosonal Sh•es. identity with ill more space IS flptteol. 'Mach • ACTT: 153 HOURS ACTL: 93 LANDINGS WORK ORDER NO. C04-108&2089-4486. REFERENCE: GULFSTREAN AEROSPACE CORPORATION ATION AIRCRAFT SERVICE CHANGES 1. • INCORPORATED GULFSTREAM AEROSPACE CORPOR LISTED. (RECOMMENDED) 1000-1059 NOSE GEAR DOWNLOCK SWITCH BRACKET 1000-1109 EXCEPT 1039 GROUND SPOILER HYDRAULIC, PLUMBING MODI INST1N A/C - WATER SEPARA TOR DISCHA RGE - TUBE EWORK/REMOVAL (PT 1 - 6) 1 LG/NLG & WHEEL WELL COMPONENTS-R TO 5150-5, UNIT PER DOYITY ROTOL MODIFIED NGS FEED BACK MANIFOLD, 5150-3 AND D2 PER MOO., ALSO MODIFIED NOSE DI BP 05100 AND GAC DWG 0 1159L40400, 50 1159SCL200-43. WHEEL STEERING UNIT, 1159SCL200-41 TO • -END- SDNY_GM/12T5 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15,and 17 EFT/1_00241197 EFTA01326790 FAA AIRCRAFT REGISTRY CAMERA NO. ? A DATE: 1J-23.90 . _ DEPARTLen OF 11WISPO 57 at 0 , 41.10601 IRATION—FEDS:/12 . AVIATION ACYJN ISTRAIION • STANDARD AIRWORTHINE INATOWITY SS CERTIFICATE 2 wayeACTIAWRA, 111.04,114 4.4.1.41.5 OOODO. 4001AOT 1 4 ZAMICA. Seal mom-arvomonmasico asuma • 2085 Inseam Unto. • secrat ur...-Oe....c no *Nal O.-rano tw roar AWO.A.a.091514AuriO Leen au. orAg cowman ras ag toe.. toIwo inirtoo to to. Li Po rot or.A:06. awl>sane onOo....on Tl ••••••• Dr....ma ••• Cr...' re +=role. to la • .O rolitron...7.42144•1.‘toon•dor Lavin A.:zoo. MKS n moo owe. ato.teOn•noS••• GRs no COO Una.,vuWam.yFY **an PI 7.P.W.r. OM • ••••• arrow as agai ve ann.% •••••• • • 0O4riIt Sault[! • • iry. ThoOur.• ft.o.win.P a• •• • •••Z• ,0 7.16W• 11.03.:44et W 00 ; • O.r. ooet•a•WA....... OOP.Ore• iltly••• • i OA i s iaii v•Onost•••Onn4 • r•O'A•2 r toity. vs DISIGYA WOW ..7 t• ...,Aigt;".4.40L......e r MP AR- .( 444— I ao ,..a Y tea O.* CIRFOICAlf musl tm may WU...OW In etalgibio•CAaO c. VOW intro Aviacir ottootaroCea FAA Fawn 8100-2 mmh cnitOo oommnizo at '.1 ANCAAIT OA AOODOO :40 op.. .N.,.......;•.••••••03 • AM,O Oen. . 0000M; MEAN Gam tn.' 04 vr- SDNY 027S4278 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241198 EFTA01326791 ' FAA AIRCRAFT REDISTRT CAMERA no:3 N DATE. t0 -2J -F0 • SbilY 6402754277 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241199 EFTA01326792 WADTAMN MiSlike-a • DEPARTMENT°, TRY.SMATATION —FEDUIAL AVIATICOIADMINISTWips1 • STANDARD AIRWORTHINESS-CERTIF(DATEI , WALOCTUPOI0.0140EL 30000IOW I • CaG.:av 13 MP stWirm apd . •P‘Pat I N4A86A 'CULFSTREA11 / G1V. 1 1085 (TRANSPORT !.1 A911.0;01, AK 1 MK. 'O *SWAGE •• • Th........wousenicapts...•espwramer•••semeanoosicief tt recs - 4•10, 13.1•011W (41•440.1.,.• ..we 0.030 t-W2 sateen npsoreane 110003* M ton tellam Vette. Is b• 031401IP uw awnett /Atha te.0•0•••10 VWMpareaWat eta =WWI wwwww• aM wars •nornang c, trevas• J ra NONE • Tema kaccacenons M.W. POW ialana laWWW11 OPOOC PI 10.3.300 fa it 01010•0 fp AWWWW. fa PWILIAN4 OP00/* eigIne Wow Pe nanny. ilweflaf cianunano. w.•!MOWN WICAPIO CCOWNIPIWPW•31 0 arcOnttinawil Cytaaseareatcr.n•fournente.....tec Vain DATE 0 , SalolfaCC Of-9424.004.0villa 16 DEC 88 VI F.. L VA • JR. bMIR ACE 1052 I AP! 0.03 owfaCtal In elmiceentawnarttnanearay•WInnfillieen3S 1101cogrowcw-nm.menCf0 r•••• CfstiFiCalt WT Mt INSPvivra IN 704 har-A0/ n. sCCOADAPett nit. arta! riCan 33300.03tefe-ATIOPS - FAA Form 8100-2 042. • ••• - , .• • . • SDNY 0.4:027§12i8 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241200 EFTA01326793 FLA AIRCRAFT REGISItt. • CAMERA NO. 3 N DATE: 70-23-90 • ',Z.\ • !'s • SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241201 EFTA01326794 PAA AZACILAPT REGISTRY CAMERA NC. 3 # DATE: — 23 90 . Form APPremr4 • ..• •. O. - u1Dirsons MAJOR REPAIR AND ALTERATION OMB • No. 2120-0120 ter FAA too olaiv orerresonain (HInnume,POiterplant, Propeller, or Appliance) OtSop lesteNtatIon Asisseaes. *arms. " 5.01— PS00 INSTRUCTIONS: Pant *MP'S,' entries. See FAR pg. FAR 43 Appendix tang AC 43.9-1(ortoesseemeArreilier. tenon ter leSeuilhoesT a chll penalty nem* execs:MA/0 anemspolillon el ells forre4Thiareport is frawhed by nra tag U.S.O.1421). Failure to Ripon an mutt In ' foe each such dolalion (SecnOn Sal federal Menke Mt of 1966). . MMus Node GULPS/REAM AEROSPACE CORP. G-IV t. Alma ., Flefinnelitt and Flegetradco SW' 1085 : . NBEIGA . • ' Mane (As Mean on ANN0NANA coliNGINN Addnes (As shown on regisaarion cieretteffe) BA LEASING A CAPITAL CORP. TWO EMBARCADERO CENTER LDS SAN FRANCISCO CA. 94111 A.• No FAA we 00/ • S. Typo Model renal No. Reiner Anersiken Ural Mae AnIFRAME ' (Ai Orsonbod in nom 1 abOvel XX S I ' PR0PD.LER • Menutacearer . • • I—..— S. Confortetty Stalarosat B. Kind of Agency : C. Grooms No. A. NooncriNorno and Aldan* • X US. ColofraistI ilbref*Mc . LANCE A. MATTESON . • Pomp on:nig:4 iihicianic AP 1864049 2407 EAST SHEA BLVD. Ownliciten nest Siouan PHOENIX, ARIZONA 85028 WantUttar collie D. I cirelylhat the reedit androt anion made totne un IN) klentified in item 4 'bon and deecribedArians or atteehineets hereto nen of Part 43 of the U.S. the information hare been made In eccordanca wren ht ine Waned heroin in and correct to bed ol mytugowledgo. DO, f .- Z(V0-117 • 'Supt of Maintainer.. . T. App.:miter Plan To Sena In IP44i 4 wn4 Inslineled in the manner plegaited he me Pursuing biltiiiiittnOntf *An 0041441* 0 444144I tenni in/iBrin klignnrinil Aderanletrator of the Federal Ariadon Adirefelatrehan end es net APPROVED 1:1 REJECTED ., lothenSprory/ 4 FAA nt.Siondures Manufactufer leil Inspactan Authorization IINC4CW . Br Person /Wend SY , . FM Designee Reedit Sulam Tra l3c/n Ainsoninnen ....sr Canine EssoolApprovaleratelectiOn Certificate or : , Signature of AellhOnted Designation No. 526705494 r 11- 1 0 751 ici c-Nortgazir-- --- SUBJECT TO PROTECTIVE ORDER PARAGR APHS 7, 8, 9, 10, -15, and 17 EFTA_00241202 EFTA01326795 `Cyan FAA AIRCEAFT REGISTRY CAMERA WO. 3 N DATE: 10-23-90 'd NOTICE t be Weigh:andbaMnceoroptttllfl'g tamsiation ctianpea sMllbe entered in the appropriate aircraft record.Anelleralionmus conformity with Ma applicable airwOrthintss requirements. compatible. with all previous alteationS to man comintilM IL Descriptor% el Work Accompisind nationality and nogistraton mark and date work completed.) More space is required. Nisch addelional slyest Identify with aircraft NBBGA, TC Al2EA. GULFSTREAM AEROSPACE CORP. MODEL G-IV, s/n 1085, APPROVED, Optional refer to: Gulfstream Aerospace Corp. [CAC], FAA AIR-CONDITIONIN2 Aircraft Service Change [ASC] Number 87, subject: n-, dated Octolird 5, (ATA 21) Cockpit Display Unit [CDU] - Modificatio 1989; GAC G-IV Wiring Diagram Manual, Drawing number 1159/140,71- COWL 3, titled ENOIHE effective for A/C 1060 & Subsequent, 30-2-1 Page installer. ANTI ICE SYSTEM; note: this aircraft has GAC ASC 49 Display Unit: [DU] fan The purpose of this alteration is to modify the to disable the fans when the pilot's, co-pilot'S, and Engine circuitry Instiument/Crew Alerting System [EICAS] display master stitches are This change also modifies the ?ewer all in the off position. will not come circuitry for the display controllers [DC] so that th4y ol. This on when the above switches are all in the off.positi DU fans and modification's design is only capable of disengaging the off the display controller s during ground 7peration. When shutting locked out and the fans the aircraft is airborne ASC 87's circuitry is and display controllers perform their intended fwActions. spliced to vire No. Removed vire No. 2H31A22 from 318A1P10 n which is X. 2028E22 and then removed vire No. 2H28E22 from 318A1P4 vire No. 1H31A22 from 318A1P9 GG which is spliced to vire No. Removed H. 1H28E22 and then removed wire No. 1H28E22 from 318A1P3 2H28D20 from Removed vire No. 2H31B22 from 318A1J10 n and vire No. butt splice. 318A1J4 X and connected them together with a crimp No. 1H28D20 from "Removed vire No. 1H31B22 from 318A1J9 GG And vire splice. 318A1J3 H and connected them together with a crimp butt changes to the engine tool anti-ice circuits were The above wiring from the done to remove unnecessary vire, connections and spices connection overhead console electrical assembly and free up electrical for ASC 8.7. ns contained in Performed all of the applicable modification instructio referred to ASC, steps A thru E and tested the ASC in the above thru P20. accordance with the instructions Contained in steps Fl with Returned the aircraft to flight Status by recording compliance computerized this FAA form 337 in the aircraft's maintenance records, GAC. ' • maintenance program and retorting the ASC compliance card to All parts that were were new and purchased from GAC Product Support. ion There will be no cockpiw procedural changes due to the incorporat electrical of this alteration. ?Etre are -no changes to the aircraft's load analysis. balance The effect of this efiange on the aircraft's basic weight and is negligible. ***end of this greet noCielhez sheets are attached *** 11/10/89 med*** \LI AtIdalOnd Steels MAaaclwd • k •ez:v - • ! sbNyG-040os2er SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241203 EFTA01326796 .r- FAA AIRCRAFT REGISTRY CAMERA NO. 3 A' DATE: ;0-23-70 - ' ;ll? v. /441-44%, U S COMMENT Of TRINSIVRTATION From 4 t o.., 2a4m.r4g:::fpD. PI-!060.1 FEDERALAVIATION ADMINISTRATICN CS I :'' - - -. • FOR FAA CM ONLY MAJOR REPAIR AND ALTERATION OFFICE CANTFICATION Appliane. r r .LA.. (Airframe, PoweeMent, Propeller, et WP-FSD0-I all murky Sn VAR 0.9. FAR 43 AppeoMit O. and AC n).9-1 lot tabromem envision Mena) . INSTRUCTIONS: Print or type for insumemins and or this form. . .. NORE . . . ICat • . -• I 0. v 1. SJK1AR I. Lone - rear tar e ap ar. . - - MMTIONAMM AND REGISTRATION MARA mm . . 1 Wit I vitCa ' ! M0INM SS (At Amin 9, molortrhon nnsignon) 'NAAR (Al 04mn 4W NgioNslion dwORRI6) I The Bmbarcadere 0tr, 10th Floor BA Leasing and Capital Corp. l 1 n I CA 94111 . 3. IN NA USE OiI.13" Pi.. "‘""• 4. BIM lownionox a S. ME SINu4 b. AttINI- , wow I ' IMAM Men Atha snow AIRFRAME N Am Apoied a iss. I ,bon) X . POSVIIIPIANT PROMS nol ANRUO43 03•NINIMMIN 6. pommuun STOWE, ' L MNO Of AGENCY C. MINICAR NO. A. AOSNCV.1 NAME AND ADOUSS uA. COMPKete aiNmwmE • 104110.. UNIIICATO ithOW4IC ROAD STATION RCM Western Commander, Inc. Drive - afroxANO IIIMI NOON A.3 S4IA,M. 3 LLAit '16301/Daily ' is A elounlfaCTIPUIR Van Wuys, Cl. 91406 - man or la ideotiMMI in ices 4 Awry sad desnibed on theResubdoes D. I catnip, throe the repel. sod/or Otermion made' to the lanknnpairemems of Put 43 of the U.S. hilinst Avian.. MthetthilM3 Mono Lim beet made in accordance with the din bog of m knowledge. . ad that the WkweestIon (*unshed Moneta Is tree Ind corm, to . PAM m DATE , September 8, 1989- - 7. AMC At KM REIM 10 SaViCE by . optui6ed below, the unit :Manned is item 4 ruktsgted W she mum, pmeribed room" to the eelbeelffirmtel. PunDee APPROVED RFJRCiFn the AdtaInieautor d dm Mail ANatio* Administration sod is 0101pee*, the "M UMMA* ... .;;Jithyilyeth beiPICTONYAIS/A11011 Pala ST Coltat. Manisa rnt Mice a OM POOR 0 1Weilthrt PIVECItht cattocut a -• RE or AOTMOMZE0 INGIVIOUAL Don OP artoteL OR Marriott DESIGNATION NO: • e . ....Y 9-8-1989 114 21 FAA Farm 337 tt-en o_ 71;ori, ' Walt. • ;p t.• • SONY CM 02754282 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241204 EFTA01326797 • FaA AIRCRAFT REGISTRT: • . "CANERA.NO. 3 M DATE: 70-2J-90 shall be entered in the appropriate aircraft record. An Weight and balance or operating limitation changes tions to - assure continued conformity with the ous altera alteration- must be compatible with all previ applicable airworthiness requirements. attach additional sheets. SHED (It more ';Paco is required. 6. DESCRIPTION OF WORK ACCOMPLI n mark and date work comp leted .) hientify with aircraft nationality and registratio Aerospace . in accordance with Gulfstream Custom interior installed ision 12 dated November 14, 1988 and the Report t1159C-GER-023, Rev in Consulting Aerospace Engineers, Inc. d ;following reports as listeINN-442 and Aero Interiors, Inc., Drawing reports approved by DER 198 9. IAI-G-1085 dated August 28, rts and nts installed per the repo The following major compone specifications as listed: CAE AIN-52-2 1. L/H Bar Installation CAE AIN-52-3 2. R/H Galley Installation CAE AIN-18-3 3. R/H Fed Crew Galley tion CAB AIN-38-8 talla 4. T.V. Entertainment Ins tion CAE AIN-41-4 5. Vanity Cabinet Installa net Inst alla tion CAE AIN-41-8 age Cabi 6. L/H 6 R/Ii Stereo/ Stor CAB AIN-33-26 7. Bulkhead Installation ement 6 Net Inst . CAE AIN-GIV-1 8. 539.75 Bulkhead Reinforc l Installation CAB AIN-GIY-2 9. Aft Toilet Service Pane CAE AIN-GIV-4 10. Floorboard Replacem ent CAE AIN-GIV-6 stal Installation 11. Water containers 6 Pedi Net Installation CAB AIN-GIV-8 and 12. Aft Baggage Shelves tion CAE AT!-GIV-9. 13. Drain Mast Installa CAE AIN-GIV-10 ion 14. Service Ladder lastalat CAE AIN-GIV-12 15. Aft Toilet Installation tion CAE AIN-GIV-13 16. Service Tool Box Installa CAE AIN:01V-le ,; 17. Seat Track Installation of FAR rials meet the requirements ed in Insullation and covering mate (a) thro ugh (d) as stat graph 25.853 Appendix P part 1 para ember 7, 1989 rt IAI-1085-FR-45 dated Sept Aero Interiors, Inc Repo DER- INN- 682. Cale*, Inc. FAA and substantiated by John upon completion of outfitting. Aircraft aligned on js-Les and balance reports revised. Equipment list and weight Chapters 5, according to A.C. 43-13-1A All workmanship accomplished pters 9, 12 6 13. 3-2A Cha t• 6 7 end A.C. 43-1 END f *vs dowimplesnnnnnsia or nem 1.44.411-121 /AM° TIV E OR DE R PA RA GR AP HS 7, 8, , SONT_GM -2154283 9, 10 -- SUBJECT TO PROT EC 15,_O and 17 EF-EA_00241/05 EFTA01326798 EFTA01326799 - FAA AIRCRAFT FECISTRT CAK6' ' • ,4 NC. 3 A' CAls: Weight and balan alteration mus ce or OP00564 limitation chan NOTICE t be compatible ges shall be en applicable air worthiness req with all previou tered in the appro s alterations to priate • uirements. assure continued aircraft record. An conformity with the B. DESCRIPT ION Of WORK identity with AMOMPUSHED (If aircraft nationa more space is lity andregistratio n mark and date wo required attach additional shee rk completed.) ts. Installed Ca bin Entertii N/C dated 8- nment System 20-88, -'appr located at oved by DER 0N according to WCI Dwg. Horiz. Arm 74-476. Vide $080 cabinet at Horiz. Arm 142.0; othe r system comp o Monitor un 69137 onents inst it 172.0. alled in System inst with FAR allation an d Operation 25.1309 Pa meet requir Para. (a), re. (b), (d ements of an (b), (c), and ), and (g), d complies (a). . Far 25.1431, FAR 25.1309 Radio freq uenc causes no in y interference check accomplished equipment. terference with aircra . System op ft communicat eration ion or navi gation Television picture tube meets requir emegts of U. Aircraft We L. Report 01 ight and Ba 410. lance Report and Equipmen All workmans t Lists amen hip accompli ded. 13, and 15 and A.C. 43 shed according to A.C. .13-2A Chap 43 .13-1A Chap ters 1 and ter 2. END v.1. covensweier Ion a rots of nCe isn -419.1:1/491.0 * ef t SUBJECT TO PRO 9, 10, 15, and 17 TECTIVE ORDER PARAGRAPHS 7, 00'4) 8, errs EFTA01326800 se**Iti611 I- IAA AIRCRAFT FEGISTRY LEAMEFA NO: i X DATE: ;6-23-90 ir • RE mm FEDERAL AVIATION ADMINITTRATICM SERV:4190S • ' August 17, • 1989 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION a...DAV Nat MODEL NO% TTADData. Asa. MADDIATA • DANZ 3 a., G-fr Airplane ' Nesternam mandep, Inc Gulfstream • Lin OF DATA . IDENTIFICATION • WW1 Drawing. Number 408069137 NC' •. Dated 8-20-88 .Wiring Diagram - Cabin Entertainment System. -.- . . . - kt. • . `-... r. . . . ' • • 'Vaal OF DATA • on in Gulfstream To substantiate Cabin Entertainment System Installati Aerospace G-IV. S/N 1085. ' maLicaLt Rauffitsaivs (La watt Rasa • FAR 25.1301, 25.2309, •25.2353,..25.1357, 25.1359, 25.1431 . with coodIclete ad linhatleso CERTIFICATION - Uglier sethoelty veld by &take al the Admisienter sad is ',conduce elite sad cc attached theme osethonAl --- Al °mamas sat Pin ISA of the retinal AvistIes ?kakis's,. dote Void to comply with oppIkalle ium bees omaltted In accordion with wetabIlsiod preeedimeo and lend requInothons of the Faint AwtotIett Repletion. II Foosonond Were! el these data I Nom Theroforo PI Amen them a. DEPONATiOlt Hula MU CLASITFICATIOND SIONATuRECSIOFTAMONATEDIENGINEERINO REPReartAlTESTO •'NM-476 Systems 4 Equipment /r Raigta 7 John R.• Chambless ---._._• • _ • • . - • SESM_02754288 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241208 EFTA01326801 LFAA AIRCRAFT REGISTRY CAMERA NO. 3 N DATE: 16-23-90 --L.,...z. SDNY GM 02754287 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241209 EFTA01326802 `AA A.'3C ::---- AF7 REGESTRV L4 :1. ASERA NO. 3 N DATE: ha. A ”.....je • . it_ ‘.• •-i 0.1 US DEPAMMOR & DIAIDR :MADCA Pante WeeMe No 0.-S06 •. ISTRATION 47 / FEDERAL AVIATION ADMIN FOR FAA USE ONLY • / ' ION 'OFFICE ODENTIOICAT MAJOR REPAIR AND MSERANON erple nt Prop ellor, at Appliance),_, - ..._, g —L19 -O1 (Althorns, Pew valmeeptent teeision thereon S. sad AC 43.9 I 'tot he FAR 45.9. 44R 41 Appeadis type all • INSTRUCTIONS: Print ornion diepoi of mit (cent. ' he iniubmions aml oot "" Gulfstream Aerospace ;M I G-IV iNATIONAUTV AND itects wAso • n ?AMC . I. NICAMT SEW/ NO. NSSCA 1 1085 an isegetfroNon aveihree) Ifrstess (At 0~ r NAME fee Aeon on e•444.0144 coliAtoft) Embarcadero Ctr, 10th Floo VAD Corp. o, CA 94111 2., "I" BA Leasing and Capital ' an Fran cisc . FAA Dar • - $ nn A. OM/ IDNIMCIA0S VIM I Haw u0. ten."' .non Aaal LAM X (4 domeetnef ' - I atmml AIRIIIAME I POWERPLANT floras Me APPLIANCE anwPAC711.• 6. HAIM DATUM C. CERVOICAN NO. _, I. KIND Of AGENCY SS A. AGENCY'S NAME MO ADOIL 41..... 04110C4IIP rI(WOIC NC REPAIR STATION :4121 MIMS CIIIII10.1.0 mICOLI Western Commander, Inc. I. CiensicanO tttttt moth. A.344.t.-1,2.4.3 • LI, A &I 16300 Daily Drive sAinleatryatit Van Nuys, CA 91406 and hicribed on the reverse or lea merle to the unit's ) identified is Item 4 shoveU.S. NUM Aviation Repletion) D. I way that the '<AAA and/or al accord ance with he requirements of Pen 4) of elst is AsoAlt4Se. casehmence berme Ian hen mode • 4 conga to the ben of eny mad that the futaisbc4 -herein 1, inn DUAL SIGNAT 1 OF AUT/4O1IGLO INDIVI DAR Z i : ..--, September 7, 1989 7. APPROVAL F WOO TO CUE ibed by ed in item 4 was ins ed in the matinee prescr asebot iry pen paean s specifi ed below the unit 'derail APPR OVED O REJ ss Stuniam so tee GI *antic° Ad/shimmies sad is the Aeltnieshemot of eh Perked COMO flowan 1•444AtON t . NA RI ID•044145 ~MOO awA44 01.44A •41014 404•14 Rusanno. otembeEnt lif x Strom SINUICHv 0 MAIWOIT 8•1•10011 Al MA ODided et of i. .. ..„ yd:.... SIGMA OF AUDlowe,,, ,y.,.. CUTIFKATI OR VAR OP APPROVAL OR DESIGNATION NO ..e , RVICDON D goicnham, Chief Inspector ny C. ...... ...r 9-7-89 .._ 64221 - GRAP HS 7, 8, 9, 10, .542er SUBJECT TO PROTECTIVE ORDER PARA -S0N-CGS1-0-27 15, and 17— EFlik_00241/I0 EFTA01326803 FAA AIRCRAFT cct,/,STRY. (..IMERA No, 3 A DATE: 10-13-90 • NOTICE in the appropriate aircraft reco rd. An nce or ope ratin g limi tatio n changes shall be entered tinu ed con fom ity with the Weight andbala ns to assure con ble with all previous alteratio alteration must be compati irements. • applicable airmorthinass requ al sheets. , attach addition K ACC OMP LISH ED Of more space is required plet ed) 8. DESCRIPTION OF WOR k and date sack com and registration mar Alen* with aircraft nationality gs listed on installed per drawin ic and Ele ctri cal modifications N/C dat ed 8-8 -88 and approved Avion Drawing 108000012 n Com man der Top Wester by DER 1NM-476. data Warning System per dst ran d Ma rk V Ground Proximity d per We ster n Installed Sun iations performe SA218880. Minor dev 2-8118 approved by DER 0114-476. approved by STC ed 108069091 N/C dat Commander drawing ordance sor System in acc wing Ho ney wel l L5Z -850 Lightning Sen n Com raad ner Dra Installed 50 and. Wester ed by STC SA2388 1814-476. with data approv 11- 14 - 88, approved by DER dat ed No. 08069157 N/C SA4749SW a approved by STC o Lights per dat Installed De Yore Log 8. Rev. *3 dated 1-21-8 (IRS), a third well Inertial Reference System puters (3), a thir d Ho ney vig atio n Com Installed Ma nag eme nt System, NZ910 Na anc e wit h data Honeywell Pli ght Sensor in acc ord neywell VLF/OMEGA and a Single Ho 774NM. approved by STC SA3 t revised. and Equipment Lis Ma nua l sup plements provided ise d. Flight rev balance report Aircraft weight and END Cier PM* TIM° Of nct• 1>IS.W.121/02.0 • (LC GOVCOINI4 --§bN 15-k,bfil SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10,Y:o an 42d 17 11- EFTA_0024I/II EFTA01326804 FAA AIRCRAFT REGISTRY: CAMERA NO. 3 N DATE: iv- 2,.;p RFCE1VED FAA May : '- FEDERAL AVIATION ADMINISTRATION ' August -17, 1989 STATEMENT OF COMPLIANCE win' THE FEDERAL AVIATION REAULATJotti AIRCRAFT OR AIRCRAFT COMPON INT JOEKTIFICAT101. MARC NODEL NO. Ty re (uma....n.a..H.riamorn, NANA Or APPLICANT N.: N G-IV Airplane Western Commander, Inc Gulfstream LIST OF DATA . - TITLE IDENTEDEATION entwing Number 408000012 NC , Dated 8-8-88 Top Drawing G-IV Sill 1085 • • - N • PURPOSE OF DATA - To substantiate electrical and avionics modification in G-IV Aircraft, S/N- 1085 only. APPLICABLE MEOW (Lie. Anne antAm.) 25.1431 FAR 25.1301, 25.1309, 25.1353, 25.1357, 25.1359, • cad Is acenduce with condition-sad limealloae CERTIFICATION • U.S.. Jodie teotid by /Erection el de Adstiyiairytot att. end ea numbed obest• elieberod of appolytwyonsider Pan 113 of be Fetal AChaloo Ragslathey, data listed tooth .1th applicably ban byes cashed h steatite. with ostabIlyhed plocetres sad head to Fill roopleysysta *I the Festetill Avalon Rogoletleae. I Oat news. Reopened approval el than deet Amen these dais • DEROSATIOW PILIYIBERSIT) CLASSIFICATIONIR 'TOMATO/1th/ OF DISIONATE0 MINI UAW) REPRO:ROAM= . _ - .NM-476 ' 'Systems 6 Equipment i....erip,z,.......7..i.s.t i /- John R. Chambless FAA Form 8110-3 till-101 31.IPERSCONS PREVIOUS COITION. rzt, SDNY_G0.4_02754290 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241212 EFTA01326805 FAA A IRGRAYT REGISTRY CAMELS -No. 3 k DATE: ii:-23-Co -- SDNY_GM_02754291 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241213 EFTA01326806 !AA AIRCRAFT REGISTRY, CAMERA NO.3 le .DATE'. 70-23-90 • ••••MS.. . • • 710er, • • . y e ' US DINATIVAMT Of. RISKSPOUSIICot FEDERAL AVIATIC41 ft sANISIRATON ' — Est A W.04-1000.1 • MAJOR REPAIR AND ALTERATION Vnif FSL70 FOR FAA USE ONLY G CENTIFICA • (Aldrome. Poweadant, Propeller, or Appliance) OO TION *., IA —O1O INSTRUCTIONS. Plias os 9.pe ail ;win. See FAR 43.9. TIRO Appcndix Sad AC43.9 I Ica tobantwat m be iestrunions sod dispern of this fora, um Smog) • MA Aerospace I mODN. G-IV I. WOMB • S AL NO. !NATIONALITY AND PROISTRATION NARK . 1085 I MEGA NA.ol IM shwa on tesonnntan mAifsecA0 ‘ LODRESS (AS itomm w• roptiennke ontiAtole) 2. "IS BA Leasing and Capital Corp. two Embarcadero Car, 10th Floor . /San Francisco, CA 94111 3. COI FAA USE. OKI 4. NIS IONTIFILAIION S IIII VIM mail .. m0Olt NOY MO. 4 1 0. a -AM non •••— r - mytuit (Al allesdnet n item I wen) POWIIIPIANI • •. • ' PROPRILIN • TM ANUANCI MAMO/MOVel 4 LOSMIsITESTATIABIT A. A0414CrS NAME AND MOMS I. MHO Of AWACS C. CERTIFICAD NO. U.S. Corinscans .1Oissiele Western Coisznandel, Inc. IOUS. OMMICATI0 a/PSC 16300 Daily Drite ROAM STATION #472I A cern/Kane tent nano« Van Nuys, CA 9.1406 An A 1 '0,13 IA. A & P •••enecniur D. I candy Mat dm mole antUot dictation made to dm ileitis) Noodled is item 4 above and ataibtd as the nevem or tastharatou Innis betebets made its stasedanoe tennimmenas of Pan 43 of the U.S. fedora sibthe Avinies RaSulation: sod that Or kforamalie ("NAAS hamin is ran DAM. .. and conga to the ben of my knosoledge. AUTHORILLO INDIVIDUAL . ., . :September T el 1989 „„-- e. _, .1 7. *MOM MUM IS SttinCE POI Eris to des AschoAry p•bb persons speasetbdo: the oak AcessiSed ' item 4 wee Uspaad I•the envier presaihed do AdosiolaneSt of the Ideal MatitH Admibintstima by sad is pi APPRAD (^ RS) TID . . faa a ifiveaS One Owe*) .F1. .40yobowlyy : IHMKTOMMMOOMZAMOM . • • CAMSOmM Oftakbobet to.COINTROR - , x NNW States. • ot rturIPOIT IMI•KbOt Of CAN AMORAL OS CERTIFICATE CS ' VONA RE Of AUTMOV(O...."2 IN . a I .....) ✓ . • eaSKINAriON NO 9-7-439 • #4221, • --- _ f_ n C. 1- Dafaa-1 =ham, Chief Inspector A t C. W320) •..% • - BDNY_GM 02754292 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241214 EFTA01326807 LFAe AIRCRAFT REGISTRY '74MERA NO; 1.4TE: 10-23-90 NOTICE Weight and balance dr operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatib:e with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. DESCRIPTION OF WORK ACCOMPLISHED 7f more space is requh'ect attach additional sheets. Identily with aircraft nationality and registration mark and date work completed.) The following modifications were performed in accordance with Elsinore Aerospace Systems, Inc., engineering reports as listed below: 1. Skyphone Antenna Installations Report 41-24 dated 10-26-87 2. 43 Comm Antenna Installation Report 41-19 dated 07-28-87 3. Pressure Bulkhead Feed-through Doubler Installation - P.S. 85.5 and P.S. 596..0 Report 41-22 dated 09-16-87 4. Auxiliary Radio Rack Installation Report 41-23 dated 09-09-87 5. Ice Detector Mounting Installation Report 41-14 dated 02-07-87 Above reports approved by FAA DER 4N/47492 and #NM-494. Weight and Balance Report revised after completion of modification. END O •COTIOtml. SICE1S PAZ ATTSCHLD C • FAA AC/141•4 GOVCIPOICNT PromTING or ma In, -eiss tritaozoo • SDNY_GM 02754293 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241215 EFTA01326808 FAA AIRCRAFT REGISTRY CAMERA NO. 3 4' DATE: 10-21-9° I :sit RFtn\f - O FAA FEDIALAvisro==1; STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS 19 JULY 1989 AIRCRAFT OR AIRCRAFT .. Slow/A. IDENTIFICATION KA'S - moan... G-IV ( r""400W r----.:7-.--'-r--- AIRPLANE i COMMANDER, INC. - vaVLAIHAM • LW OF DATA OVITICI.TATIO. TITLE •ELSINORZ pOCUMENTS: ON .DOC. 1-14 • STRESS ANALYSIS OF ICE PROBE MOUNTING INSTALLATI REV. A DOC. 1-22 SUBSTANTIATION - PRESSURE BULKHEAD DOUBLER INSTL REV. NC 08068007 - 08068008 DOC. 1-36 SUBSTANTIATION - NO. 3 VHF ANTENNA INSTALLATION REV. NC • DOC. 1-66 SUBSTANTIATION - PEDESTAL MODIFICATION INSTALLATION REV. NC .... • (DETAIL DESIGN AND STRUCTURAL APPROVAL ONLY) .""mEDF w"A TO SUBSTANTIATE INSTALLATIONS IN LISTED DOCUMENTS FOR G-IV AIRCRAFT S/N 1085 LopLicsoLe mmv. an, NNW. on.....? FAR 25.3,03,25.305, 25.301, 25.561, 25.603, 25.607, 25.609, 25.615, 25.769 with sodium and ianteurwe CERTIFICATION • Cedar meant, vaned 17 discus al Se Arisistswarm sad a magmas sad eci surmised Sens moire ed --- el eppaisaast Wits Part Mot Se Foie& Aviska Raptures'. Is. Goad Oise whb applicable kis ben embed S steteedeaco MA asaalOsieed ponders ad lend ter semi., ngeimemsto el dm Featal Ailaidee RepUtims. I Opt Thenkm M Reasoned approval tithes data =Approve ase Su IDISMetATMA mASEAstMl CLASIFICAIMMO ROmMtuRMMOF DESIONATIDINFANEESMO RSIONNUTWIM e . Fealc4, 1 I I NM-494 I, STRUCTURES ROBERT E. POTEET . I I PREVIOUS CaTION FAA Folm 8110-3 I I l•ft" • SUPZItlEOLS • . . • ' SDNY_GM_02754294 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024J2I6 EFTA01326809 EAA AIRCRAFT CAMERA NO. i ARECISTit. DATE:- 10-23-90 SDNY OO2764295 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241217 EFTA01326810 Cal:17/1 FAA AIRCRAFT 220%N :it CAMERA NO. 3 f? DATE: •:0-23-90 R7-C: Ftir:r, . US. DEPAIRMIle 0/ TRANIPOTTATION • Fa Aper, mod FEDERAL AVIATION ADMINISTRATION 78.4., Eats. Ns. 011.4060.5 MAJOR RIMS AND ALTERATION yet, , ,..:,‘ ,L,,, FOR FAA USE ONLY Dina oepaincAnoN (Airframe, Powerplant. Propeller. et Applian?) WnSOCT*2 INSTRUCTIONS, Prim et IOM eII retries. See FAR 435P.FaR 43 Appendit a. mid Ar.45.9-I lot memo:hang resibicsa lot kernsaions sad dismission a des form thereon mm,Gulfstream Aerospace ImCos. I G-IV I. /MGR Sam NO. .OrTATFINALITT AND REGISTRATION MARK • 1085 i N88GA NAM (4 Arms en fodffMs. 4• 491NITAI !AODIESS Mother r mgetrenon ceetifer00 7. 048 BA Leasing and Capital Corp. • trim Embarcadero Ctr, 10th Floor ;San Francisco, CA 94111 I. BM FAA DIE ONLY - I. INITMOMOTION S nn wen -a Mott I lam no. ',SAM "".. Atio. AIRFRAME Me *tease wo neen I Aso) X POWER/LAIN PROMO APPLIANCE SIIMI/PACTI/Ol• ' • A. NITMINX: A. *Cerra I NAME AND. ADDRESS I Epee Of AGENCY C. CERTIFICATE NO. MS artisans meanie %. Western Commander, Inc. rowan cen ICA 11. 0404 c 16300 Daily Drive WAIR STATION E4Ol a Ct mane rum. neater. AI & 4, R.I,2, 13 L-.I. A II i Van Nuys. CA 91406 immumation D. Len t* rho the repair aadior serration made to the lodes) identified in item : actschisme -Memo Ism been made in accordance mid% he requitemeno of Pan 45I of444 and described on the re-Nme cm sad that dm inreetamies foritialied beteg bt US. Meal Al.iiiI i0O RitzyLaic,' . is we s 4 maven to the best a my knee ledge. DATE . . SIGN At OF AUTHORIZED INDIVIDUAL . September 7, 1989 ...c ./.124-rart-r3 7. ANIONµ 04 tElleaSEIVICI . hillWhet to the incleney pna peneas specifies' haler the sem Identified is imis-4 eu inp.naa is the WAdmisirauot of the Peden' Minim. AdsaMiseseers and 4 p ribed by mass.resc pi, AP PROVED la REJ ones isaew -adt• itornACIven Partner ALMOMILITIOM St IAA CIIMINIt Camemse Melfalta x w mu, PSI a W.01300.1 INIPICTeo DAIE•Or Mesa Ot CeirOSCAre OA SKI se or sursOet,..72 0.0. I ni IH DESIGNATION NO . #4221 ' Da ny C. arnham; Chief Inspector. II320) s:try SDNY_GM_02754296 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241218 EFTA01326811 fFLA altitid.F.T .RECI.STiY. 1 CAMERA NO. 1 N DATE: • NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. DESCRIPTION OF WORK ACCOMPLISHED Of more space is .required, attach additional sheets. - Identify with aircraft nationality and registration mw* and date horn completed) Repositioned Emergency Park Brake Control and Flight Control Power Shut off Valve Control in pedestal. General location remains the same, (forward, left hand side). All of the GAC Park Brake Installation remains the same, with the ex- ception of the cable being pouted in a different manner at the pedestal The GAC Flight Control -Power Shut off Valve installation remains the sage, with the exception of: 1. Factory handle (PN11591240386-1) replaced with a modified handle made of stainless steel materiel. 2. Connecting Rod Assy (handle to lowei control arm) P/N 1159F20780-11 replaced with modified rod made of stainless steel. Both handle and rod replace original parts made of aluminum, and have been modified to allow handle to be pulled up and aft instead of up and. forward. ' • Soth Emergency Brake and Flight Control Shut off systems function and operation remains the same. Rifting and system functional checks performed in accordance with Gulfstream Maintenance Manual, Chapters 27-0-2 and 32-4-1. N • All workmanship performed in accordance with AC 63.13-1A Chapter section 1 s 2, Chapter 5 & 7.Section 1. .. This modification has no effect on weight' nd balance. END ..-....o.s."Ge.vcotrokuty_•"temila w nee ne. 45. 1211.° 24° - - - . - . SDNY GM_02754297 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241219 EFTA01326812 max: ILA 4/ AIRCRAY: iEGISTRY i I' DATE: ;0-23-'3 0 sc. •:••• US ocookluens or titeithWATIOr • r For. APP•rid rCOERAL AVIATION NRAINISTRATI0N ', &Agee Dana No or-Ro6o.i MAJOR REPAIR AND ALTERATION FOR AAA USE ONLY ' (Airfromo, Poworplanb Prop - 0/1KI IDINTWICATION ellor, or Apeliancie)• ' ANSTIWCylONS• Print or type an twin-- Sn EAR 43.9. FAR WPPSD04: for an te...Tien. and disposition 43 Appendix B. ad AC 43.9 I of this tarns . for tubsequens revialoo thereon - iateXf Gulfstream Aerospace I INCLIST -..,, Mint NO. . . L'Cv Ar a uota:rGrr-IL I 8 ' 1085 moIsmAerv, MAR[ I N88GA ?Oaf (Ai she...,. eol reeparolies cortidta I ADCOKS$ (As Ana LOWE, IBA Leasing and esrogithogion antAtele) Capital Corp . ITwo Embarcadero Ctr, 10th Floor I San Francisco. CA 9411 I Wecli MEOW 1 • 4. Uhf IDEFMAIIINI u.i r.Y1 S ITN shoot I mouno. tent. oval amp AJVIAA.1 . ' (A. doeastird sons labors) - • X -. • POWUPIAM isoreurA • IWO AMINO sieurVOACTUOUI A. -ACiffeal NAAR NC I. ry AMBIT /ZOOM B. RotO OF AGENC t 5 .-- Y , 1 C. CERTIFICATE Western Commander, Inc. U.S. O147.1C4Ite maCKANC . 16300 Daily Drive Porto. cinecore ...awn Van Nuys, CA 91406 X artirsCARD Walt nohow tour. STATION 44221 A.3 & 4,R.I.E.83 L.EA & P D. I certify Oat du repair oamowenr• . endsot detrain rook to the .......5 - intscheares beano have bog made ) starlit.. to aces 4• stave and In secord aiore described on nod that the inform ation furahibed herein is ton sad the tequiteibent of Pan 43 of Ihe V.S. Federal Aviatiothe bids reverse or roam so the ben of any n Regulatinai 1; 600 44 4. OAR. . SIGMA E Cr ALITM040&i.. WINVI OUAL September 7, 1989 7. MEOW FOE IIIIIII I 'WOKE Purses co des eueborierioven do Adsoltileageoe of the prow aprairs1 Sky cbt unit 'W Federal Anode. Adaiio uunion sad is go APPR io item 4 naizigted ia the maim prescabod by OVED OMt P" Kr' naWP A" WaNACTUMS *MOOR ,.../ eareerceeAlfireeS;1O.4 011•4I l_4J ET MA MOM! Onsaus DIPArlan SWAM SWOON X 01. 11.0010.1 04...004. OAT! OP APII.0XAL OR 04 CERTACATE OR REACTION ,r DIDONATION NO - OF ALITMOSIZIDIJAItte t„.... j . 9 - 7729 ' C.:-. :4221 ban C. M rnham Chief Inspector Paull A] v-0m . . • -- • . • 02754298 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF-EA_00241220 EFTA01326813 FAA .IRCRAA., . 7Z011,511a CAMLEi NO. 3 p 'DATE: lr.- ) 3.-90 Weight aidbalance or opera ting NOTICE alteration must be compatible limitation changes shall be enterer/in the appropriate widi all previous 'Herat:cos to aircraft tabard An applicable airworthiness assure continued confo requirements. . rmity with the 8. DESCRIPTION OF WOR K ACCOMPLI ldentifywAhaircraftnationalityandreg SHED (ff more spice is required, attach additional sheets. igtradonmarksiddate workcomp leterf) Complimiiiith the followin g Gulfstream Aerospace Customer Bulletins: Alert CB 44 - AOA Sta ll Warn Computer P/N 96S-00,4 Alert CB 45 - Engine Fire 1-03.4. Extinguisher Systems Alert CB 46 - N/L/G Forw /Check. ard Truss Brace Assy. A/N Custoter Bulletin 46 - 1159I.M40802-1 Brake by Wire F.Bal P/N Customer Bulletin 48A1 - FOB Terminal Lug 6004903-2. Customer Bulletin 410-- Inspection. Inspect Outfitter Flouresc ent Lighting Incorporated the followin g Gulfstream Aerospace Changes: Aircraft Service - ASC 43 Windshield Heat - Temp ' 48A Aux Power - APO Fs.ry Sensor Test Switch - Inst all Test - Improvement 413 APU Starter Drop -tut Light #49 Cockpit Display & Nose Compartment Fans - Rep 497 Air Cond. - Cockpit lace Temp. Sensor Replace/Rel 4110 Elect. Display Con oca troller fl & 42 Wiring Mod te €119 APU Shut-down Mod ification ification 4122 Take off Range Warning 4132 E Battery Wiring Ind. Swit ches - Adjust Modification rnsmalled Phase 2 Wiring per GAC Dwg. 41159SE4203 8 Rev. A dated 4-10-89. END ❑ ADOMONAL SHEETS ARE AnACHED C IAA AC /14•1114 nve.covemmewrommilwaArnct.OS-M-1 21/4020, SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241221 EFTA01326814 FAA J.:SEE:at FECISTRY CAMERA NO, F I DATE: 1E-23-90 VS CEPARTeetert CA TRAASPORT --"ThASI- ----_; —Miorrem••• FECCRAI. AVIATION ADMINKMAUON • t r. v • - ' : -. Eider &am S.. 044060.1 • MAJOR REPAIR AND ALTERATION FOR FAA USE ONLY .. DANCE IDESIVICATION (Abframo, Powerplant, Propellor, or Appliance) — • l7P-F5D0.1. INSTRUCTIONS: Print or type 'II mine, MR 0.9. f ta 43 Appetit& R. aid AC 4).9 I Cat taanoiatftt for inateaspano and diaptamoori of the nem. •See revision ihmon 1 mk"Gulfstream Aerospace imam G-IV I. MONT I • SERIAL NO. INATPONNITY AND REGISTRATION NAM( , 1085 i N88GA NAME In New nu regietration arlifeade) !ADDRESS (At Amm en rosiseratitei corMomN) 7. OWED BA Leasing and Capital Corp. ?Frio Embarcadero Ctr, 10th Floor $an Francisco, CA 94111 3. FOE FEE USE OIST • 4. UNIT IDEIMIKAtt01 S TOE we, We moon Num ma. mret. ware area AIR/MME • (Au Ancand a An I than) X POWIXPIANI • PIA2481111 nn APPUANC1 •SMVICIVI99 4. DEPLOY STAT017311 A. AGENCY'S MANX AND ADDRESS S. (ND Of AGENCY . C. CERTIFICATE NO. V.I. ClIng1CAnD anKaNte Western Commander, InC. raglian Cfna.C.An0. .4CM•riC LIME STATION #42.2I 16300 Daily Drive r Van Nuys, CA 91406 a oni..c.ne Mail ..... Om ie3S 4.3 -1. 7r 43 !rd•A 1 sui....1.0Vent D. I fortify &at the repair tad/ot Alttttt ios umebannta betno be.. bent We in &swim&tomidi made the %man &nand io utgli 4 above and &scribed on the evert as the requireamots of Pan 4) of O. U.S. Total Minion Reftvletion3 tad dial the isformatia• furnarbed herein is rive sad Rouen to the Nn of my knot Mast DAR • SIGMA Of AUMORIZ20 INDIVIDUAL September 7, 1989 e ..,, a-----/ „ANIMAL PiANIIN4 to, dm motheariey meta persitto sPerift4d below the mit der Admialemot of the Paine Aviation Admiaiatenion Mt MUER TO ME iprosifird is imm 4 was ins ad ia the manner prescribed by tad it cE APPROVED REJ . f PAIL se itmebatty OrKIR 509,0 ....:1 pappartit e& arancncee•OTFONIATIOM trOPIC701 IT • PIA MOM CANAbtan prneogan x Wu. sumps • pruarep00 SWIM@ 0, DAIS OP APPROVAL 011 CERTIFICATE Oft VONA Of' AUTHOR? INDONJU d a td ‘ zin j LENCIION DESIGNATION NO 9-7-89 24221 D y C. F nham,..tgief Inspector v.n 11320, SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241222 EFTA01326815 FAA AIRCRAFT 1LGI5Tky cAmERA NO.. 3 At -DATE: 1D-23: 0 0 • NOTICE Weight arid balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all. previous alterations to assure coot, rued conformity with the, applicable airworthiness requirements. 8. DESCRIPTION OF WORK ACCOMPLISHED (If more space is required, attach additional sheets. Identity with aircraft nationality and registration mark and date sock completed.) Installed Smith Industries Standby Altimeter/Airspeed Indicator, P/N WLM101AMS-1, TS0 ClOb and C2b. This indicator replaces the factory (GAO) installed Aero Mechanism Standby Altimeter and Airspeed Indicators and is connected to the same standby static source. This installation conforms to Gulfstream 0 -IV Outfitting Interface Specifications, IliV. 2, dated 11-14-88, Section 7 and FAR Part 25 Sections 25.1323 and 15.1325: Aircraft equipment list revised. 0 ADDITIONAL SHEETS WE ATTACIED C ruvt•nwr it OA. 00.100/00.FT .PINNTING Cor sact: tm-its..aiteatte • _ _ . SDNY GM 02754901 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241223 EFTA01326816 FAA. AIRCRAFT REGISTRY CAMERA NO. Y ,v DATE: ;0-ii-90 US OCOMciaMT Of IWISPORTATErs Paw FM/A AVIATIONAONINISTPADON i5 ,:.GAIDTAT:".71 NA IliIal MAJOR REPAIR AND ALTERATION -' FOK FAA 0$! ONLY (Airframe, Powiaploni, propellor, or Appliance) pia ONKt con sKinott • r 3,...i... 111P4SDar ': INSTRUCTIONS: Prins or type all casein. She FAR 43.9. Fill! 45 ON Dative's/is end diseAsition of this font Appall Dad AC 433-1 (iir subeequent revision . Gess!) ' AusgCulfstream Aerospace ' MOOS I. krun I ' D701V . SOUL NO. INttIONALITT AND RECASTRATION MANS • , • . 1085 I NS8GA tardefar Owen an sonesRericee .wades) !ADDRESS (As Jaen in neavosen ortriRcoro 2.00k3 ) BA twilling and Capital Corp. ?Two Embarcadero Ctr, 10th Floor ken Francisco, CA 94111 • • 0II • . 4. Mot INR7IIKATIOR mint S. ME ••••••1 .000 Uiro•tr.O. I awn Ana. ( rieweesf I obees. X POWEIPLANT ' J MMUS APPLIANCE • ansivraell ..- 6. (01006111/ STAIDIERI A. AGINCCS NAME AND App[![[ II. UP. OP AGENCY C. CERTIPICATE NO. • VS. CIIMPICATID aftliatelK . Western Coomandeil Inc. • , pen CIIIIICATIO MOIAMC 16300 Daily Drive. WAN STATION Van Nuys, CA A Gensscanti rinse Hefei A,3 &4.2.-1,2,113 L.I,ASP 91406 . Annettcwne D. I certify au she repair sisdnri jeered** sttsehoserits Mine Uses here ark is aide to Ow uollig) islestifseri is hen 4 shove sad described *Gardena Ala he requires's° of Pan 43 a Si VA. Pah& as the nen or sad that Etta isles...lice Asririased hangs Aviatige Rarektieny Is inn sad cents, to Elbe best of my Issowlerigh DATF PONA RE Of AUDIORIMD INDIVIDUAL Septedber 7, 1989 G. ...." . .• .7. AMOVALFOR IETUIN 0 Malt ft vat to ibe simony ono the Adokriseror of sty Nide& penes* eperified below h, sari id/nailed is i® 4 esamigzied is she =Snail Atheism AdaisArystio sad is (3 APPROV preecribed by ED CLEW1 4e NA 49 ITOCANd cost inacrl . -.sr, NINO, ' shuliP9Citleet - IMPtC1.00.a.M406,2AT04 •. 411.• r Y via MOON x ISIGISISIDes candwe Otrallet7 01 Sala NPICRilt / a DAROP APPROVAL ORNA cannon a - 4 SIGMA 0 s 9-7-89 • DESIG TION NO nt"cirrlia..41,../a..„---) 14221 .. D y C. w rnham, Chief'Inspector- - • .. • SDNY GM_02754302 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241224 EFTA01326817 . so.PCFAFT P.EGISTRY IAnitA NJ. 3 A DnE: '0-23-9O NOTICE Weight and balance oreperating limitation changes • shall be entered in the appropriate aircraft re:c-d. alteration must be compatible with all previous Aa applicable airworthiness requirementx ',iterations to assure continued conformity with the 8. DESCRIPTION Of WORK ACCOMPLISHED (If n-ore space is required, attach additional sheets. Identify with aircraft nationality and registration marX and date not* completed.) Installed Oxygen System in accordance with data approved by STC ESA.4416NM amended 11-13-87. Top Drawing SAI-G-32862:005 Reit 0 dated 11-16-87. Operational Test Performed, Weight 6 Balance and Equipment List amended. Flight Manual Supplement SAI-DIV-1012-02-001, dated 11-13-87, provided. All workmanship accomplished according to A.C. 43.13-1A chapters 2, 5, 6, 7, IT; 13 and A.C. 43.13-2h chapters 1 and 16. . V.5.. co VCMYEMI Pfbn T.C. Of fICt 1166.41S-1:'.'.'v SIDMY GM 02764363 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241225 EFTA01326818 SDNY GM_02754304 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, -15, and 17 EFTA_00241226 EFTA01326819 FAA AIRCRAFT REGISTRY CAMERA NO. / DATE: 3- 2c - 89 (cm Owes! 0 APPLICATION FOR • meSTMAIIONI — Pas to alinellip AIRWORTHINESS a ass.&or {slin Sao wane in Micie atm/hese eat MA g bastatsoFLA awns Nal2040/1 WICM•1117.1 .111•Walmorl kr spiciatillgN ••1••••r as CERTIFICATE Ore vt A ver asmama pentescoapiablagell isstAlik•rod ofla LaillaWl lit•Lerf MA Mom IL 411.01•111•Xti.COVOnraw 4 Ala% I/ , N449GA .0 GLIUSTREAM ' 11 94.... L eficukt ilitabirtioat Maw GIV 7.,mcnicatoosanom 1988 AC, 7O1Ic• • .. 1485 ROLLS ROYCE O. MAMA. CI DolorS • ••••V-til• SOUSE S* Way TAY MK 611-8 Is IrOPeUlamtertnaras S4656 TWO (2) N/A IL 2A02arr OICAIU J•p04•••• AMPUCATCS a aOW N/A I•lcor wt lee .Caramel IMO • • I X ST Nose nosan•muCtal titan owea awn I IowaI ItriLilw I Imocsnclitpumsoctr I • i albs. Jianainfe itSCUMrallOanar••••••••••4 Ian' I f Hu co4 'I IMMO 1 I IllOWISC•al.loaaa, I CUSS 1 - • Clan • I 1 WIC3A.tu‘ Ye MT Carnet Piern•ciIIIr••••• molest./ a I /Ow. PTIIIPA I ALM^ Aorreas • I is ••••t~ • Mal el• 4:I iii.meinslen I 0•100.aka • weave COMM% I CAPAI•OE OF C.MCO I OTIS flaw • OiSitmoi No Drolbullfr • 1 129•110.1•1/•••••••••••••4 I ostoa (RAT • coerce, I *le earl • Patna I atfw tO••••••1 l.a UAW, • • TO tie*CC•••uu•X atm IM I 7VVIV MGM? 0 .0P*AS. at.115WC•4.tiannsi•Cit OA STOUG• V40/4 RCM at" Omani* $ CVADIat Pig, MCA OF NOSCIPC OUP, I 101.••••••11••••••••• van 140.~ INS Y. 0. Am s anansa• 6. Etta Os u•Aawcentrc•710 TAOAct ....curt • Newer .......sal I Cis IMAM ON Liar , i III I P•XvcreOtia•rr lilac • CLISIL•Aft02•10aTIATION INST. C I q IAA CAA samcorrfroas$ Cin eon 10..••••OW "••••••• 0••••••••"••• Snore. Cadet' a ass, A. AfroSTERID Oal4 Men., et ••••14... GI In... w'.••• ,9 ••••* VOWS% Cat= OCIM ACCOLIS I X GULFSTREAN AEROSPACE CORPORATION P O. BOX 2206 SAVANNAH, GA .....*:"Arlaantavoil.4.141Caicliespoorraamegewoomnintanstom 31402 € •a•pari WO. C•704 OK are Saar. Ns . Mt C•201.C.ATI WM Pal MVOMI abliffiarnetlitettrirttrOwo • or °Sams AP a un••••• ow...roma Al2EA REV. 1117 X ••• Ana) • 88-24-16 PAOU:111•11•4 rat CiDtt. an C.••••ainn I X N/A s VC •••••••• • C. PACM.P1 OPIT•104 no masatram N/A lA WWI= <mat 0 Waft el TOT AL 455 0%.1Wan MOWS g X uaMin min 5:03 o ngaidertm ,I ,...., seven. Oar He ton lir. s..• •••• ••••• • N/A &a:IRS:Ana - i hoer wiry ••• I a •• mgerime este in• mg • •• soma ~Ye Nem ••• ••• a • ese••••••••• Oa' Anton nay •••••• a.m. •••••••••••••••• Ian./ ••••••••• an c• Amscalnst NAPA NC TPA ir•••• .an POIGCLOI• 16 DEC 88 JAMES 0 WEST • he •POWT OCianD JAW( my AGENT .a.---eta. 0- C410th KM awn:C7a nap KumnamoirrsT I IC,sCaival• SO 0~ f 27 $001 SI 2 22.2517,22 inpt IV OPthicAn rate res. 1_2 1 02m0CA22 22...20. TurtcmpaeKen 1 1 1f ffs 2rwattbowia, trAnCso taw Links. • anon loms•Cilaeolls• ft .. i • 00.4 ' i I 6 4 WI ITT< SiOSIUNC ••••••1a dads*, am • 4 A.••1 4 .1 Ire Our •• ••••••••••••0 x Tit CAMICATIIMOASTED a SVEN. Iv tat ••••••••••••••• 4 •••:semen• Ca SOC•ne.an g I a. •••••••• I> • AVOW let le••• •••• Seam • ,.- e =nasal IPA •iirECION j .›. Or Onkel •OvollilistaiGt•nnt I g‘t MANX •Tz li IItont 'WILT Oent• Oa LOCIER. Wes I II!•AUI.Wousi I Fo.• us " itAk, ../ .4 IAA 30.14•CTCSISKIMATIA L I' 16 DEC 88 SAV-MISO-CE42 • 12 vi F. VAN , JR.. . DMIR ACE 1052 — SDNY GM_02754305 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241227 EFTA01326820 S NY GM 02754306 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241228 EFTA01326821 TM RY AIRCRAFT CAMERA SO. I REGIST DATE: 3-25_ 89 enrcenutstarmapc. • DEPARTMENT a 1RANSPORTATiON-41:01RAL AVV.TION A0IMNISTRATOI STANDARD AIRWORTHINESS CERTIFICATE re;ww.c z l••••••Crtoolli oaaril WI" • CATICOS %WM. N4496A I system% sty • Arror01•Tv "AO PSG FO• SSW= two onorron••••••••• sue matron. 1•11mmIlesdpierscorrhislarermlakiroo.malltarlOraair• on re nor mod re ire. .- in Iowa to rar•••flo ar ••• ramie goo*. Y win *PAW" rem bmn ore.. ro cooloon • sob •• Ina •4••loplea•••100••••••••••• GNAW ii••••••• rioloro gores my .sr. Coreormor a. isorroarod Gonadial.nal CROWS OrlMIMI rest NONE a olir•o3 APO 0000, 06 We wove ••••••••1 0.1•••••• sari et a Wenn. am • Paso •••••••• My Pa hirramiralr. . km VS .•••••••c• orrorrord a r•••••••••••••••Ot .1.1sear Pell At Siam OOPOOrawamarto••••••=marrotrlYat W I O. 6Suorol rum POMP ,16 DEC sa 1• • a• • ono inorotcooncoerha corilicsomoo.roarrobriloo ille•••••••••••••IMO Or mei or Da ISIS CMSCatsMST SC MOW= lOr ~en on ri•••••••VO mroolPmriCcroLOOPOO TM( ISOM" •IXOVJAMCI writ. •PRICaliLt =OW.. FM Fonn 8100-2 re 600 too .••• 4 4 - SDNY_GM_02754307 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241229 EFTA01326822 SDNY Gf...4_027 1308 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241230 EFTA01326823