EFTA01331032

OMB tee memo ElecircricTrecknehatet EV: W31/20.4 fll 0 BY MAJOR REPAIR AND ALTERATION or FAA Usi Only us Osean- ent or Tremont/fen (Airframe, Powerplant, Propeller, or Appliance) Newel Mitten AdenInlotretien INSTRUCTIONS: Print or type ail entries. See Title 14 CFR §43.9, Part 43 Appendix B, and AC 419.1 (or subsequent revision thereof) for instructions and disposition c4 this form. This won Is rethireid by Law (49 U.S.C. §44701). Failure to repot can ankh in a civil penalty for each such violation. (49 U.S.C. §48301(a)) Nationality and Registration Mark Senaf No. N908JE 20115 1. Aircraft Make ode eves BOEING 727-31 Name (As shown on registration certificate) Address (As shown on registration certificate) Arklent )02 FOULS HO ST E 202 2. Owrer JEGE INC Cry VetAfiNGTON Stew OE ip 11003.3742 Ceu try SA 3. For FAA Use Only 4. Type 5. Unit Identification Repair Alteration Unit Make Model Serial No. lil AIRFRAME (As described in Item I above) O O POWERPLANT 0 O O PROPELLER Two O APPLIANCE Manufacturer S ConfomiltyStetement A. Agencys Name and Address B. Kind Of Agency tams Bergen Ak ServkeASok•OMplen U. S. densidned wawa I Manufacturer Ads.“ SS OrI ma vein Foreman Commend mechanic C. Certificate No. Cry ft isethedels ore' FL x Cortietled Seater Stow SD4R514M Po 'POO Corr/ USA CSISCeleeMeireenteCeorperrat0IN D. I certify that the repair ancVor alteration made to the unit(s) identified in Om 5 above and described on the reverse or attachments hereto have been made In accordance vMh the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information famished herein is true and correct to the best 01 my knowledge. blended range fuel SDate of Authorized Incividual ow 14 CFR Part 43 O . APP. 0 4 :// David K. Crosby 15 JAN 2016 /.....• ../ ov I for m to Service Pursuant to the authority g yen persons specified below, the u ' retied in rem 5 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration end is XIApproved I—Rejected FAA Fri Standards Pawns Approved by Canadian Manufacturer Maintenance Organization Depannuthr or Transport Inspector BY 0010r (Speedy) FM Designee X Repair Station Inspection Authorization Minato or 7 4-iitu ate of Authorized Individual Designation No. SD4R514M i / 92 a 1. David K. Crosby 15 JAN 2016 FAA Form 337 (10/06) SDNY_GM_02759647 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246569 EFTA01331032 NOTICE Weight and balance or operating hmitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible AIM all previous alterations to assure continued conformity with the applicable airworthiness requirements. II Description of Work Accomplished fa more space is muffed. attach &rational sheets. Identity with aircraft nationaAty 811:1reptstration mark end date work competed) N908JE 15 JAN 2016 The following work was accomplished on Work Order 82484. Nationality and Registalion Mark Date INSTALLED: Aviation Communication & Surveillance Systems (ACSS) STC Number ST02406LA, entitled 'Installation of TCAS version 7.1 In accordance with FAA approved AML No. ST02406LA. dated February 06, 2012, or later FAA approved revision.' The following Aviation Communication & Surveillance Systems (ACSS) Traffic Collision Avoidance System (TCAS II) equipment andlor components were removed for modification: 1. RT-910 TCAS II Computer Unit (Change 7.0) PIN 4066010-913 The following Aviation Communication & Surveillance Systems (ACSS) Traffic Collision Avoidance System (TCAS II) equipment and/or components were installed after factory modification: 1. RT-910 TCAS II Computer Unit (Change 7.1) P/N 4066010.914 The above modified equipment and/or components was installed in accordance with ACSS TCAS II/2000 Change 7.1 AML STC Master Data List, Document No. 8900067-002 Revision E dated August 07, 2013 (FAA accepted on September 9, 2013 Los Angeles ACO) or later FAA approved revision, as listed on the FAA Approved Model List (AML), Document No. ST02406LA, dated September 25. 2013 or later approved revisions, and the ACSS Traffic Alert and Collision Avoidance System, System Description and Installation Manual, Pub. No. C15-3841.005, (ATA No. 34-43-00). Revision 004 dated 15 Oct 2013, Including Temporary Revision No. 8 dated 15 Jun 2011 or later appropriate revisions. The required FAA approved Airplane Flight Manual Supplement (AFMS), Spec. No.: 8008565-001. Rev. IR dated August 9, 2012 or later FAA approved revision has been inserted into the Airplane Flight Manual. The aircraft Weight & Balance change negligible and Equipment List amended. The electrical load was computed and found not to exceed 80% of the system output. Log book entry made. INSTRUCTIONS FOR CONTINUED AIRWORTHINESS (ICA) 14 CFR 425.1529 The Instructions for Continued Airworthiness are contained within the ACSS TCAS II/2000 Change 7.1 AML STC Instructions for Continued Airworthiness, Document Number 8008572-001 Revision B dated 18 April 2013 or later FAA accepted revision. END A00it cred Sheets Ate Atteehial FAA Form 337(10/06) SDNY_GM_02759848 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246570 EFTA01331033 -r BANYAN Federal Aviation Administration Date: January 15, 2016 Aircraft Registration Branch AFS-750 PO Box 25504 Oklahoma City, OK 73125 Ann: Record Keeping Subject: ,ubmIttal of FAA Form 337 for N311AG Boelna 727-31. SM 20115 for the installation of the AC S TCAS II Chance 7.1 IAW ACSS STC ST02460LA Enclosures: 1. Original FAA Form 337 for the Installation of ACSS STC No. ST02406LA. dated 15 JAN 2016. The above listed enclosures are being submitted as per 14 CFR 43, Appendix B paragraph (a)(3). Please contact myself with any questions or concerns. Banyan Air Service Fort Lauderdale Executive Airport • 5360 NW 20" Terrace • Ft. Lauderdale FL 33309 www.banyanair.com SDNY_GM_02759649 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024657I EFTA01331034 . . . • SDNY_GM_02759650 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246572 EFTA01331035 OMO 1.1 21M 0,20 Douro* Troclong tivatw En: &'3t11014 l 0 MAJOR REPAIR AND ALTERATION 0 saw OW LIS Dopeerent . al!romantic., (Airframe, Poworplant, Propeller, or Appliance) Foilsniknoesa AAISSetteeen INSTRUCTIONS: Pita or type at entries. See Title 14 CFR §43.9. Pad 43 Appen B. and AC 43.9-1 (or subsequent revision thereof) for insvuctions and disposition of this form. This report is required by law (49 U.S.C. $44701). Rause to report can result in a civil penalty for each such violation. (49 U.S.C. §46301(a)) Nationality and Registration Mark Serial No. N908JE 20115 1. Aircraft Make Model Series BOEING 727-31 Name (As shown on registration coreficete) Address (As shown on registration certificate) maw iC0 Mout ROAD SUITE 202 2. Owner JEGE INC CO, WILIMeTION 5.01• CE Zro 1010S.3712 Cava, U.ASTED STATES .. .. _ 3. For FAA Use Only 4. Type 5. Unit Identification Repair Alteraton Lint Make Model Senal No. El 0 AIRFRAME (As described in gem 1 above) In POWERPLANT El El O PROPELLER Twee O D APPLIANCE renureckcer 6. Conformity Statement AL Agency's Name and Address B. Kind ol Agency Nam BOCA AJRCRAFT PANNTENANCE LLC x U S. carlificaled Mechem I Mandecluter km.. sesAmicaT Yew.* I Foreign Cenfteled PiethenC C. Certificate No. Cer BOCA PATON Wee Ft Cenficated Rope., Saloon, re 31131 cc..„, wart° SMITS CertiScated Maintenance Orearrieben A&P 2884154 D. I certify triat the repair and/or alteration made to the unite idenblied in item 5 above and descnbeS 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 ItnoMedge. Extended range fuel SignalureiDate honied Ike ma per 14 CFR Part 43 O APP. 8 r / "/d) 7. Approval for Return to Service Pursuant to the wAhonly even persons specirted below, the unit identified In nem 5 was Inspected in the manner prescnbed by' the **nenestratorol the Federal Aviator, Administration arid Is nApproved illiejected FAA Fk. Standards Per Aneovel by Caneden Manufacturer Meinlonance Organization Deparenerd el Transport Inspector BY Other (Sneer)) FAA Designee Repair Station X Inspecaon Authorization Celli cote Or win iAx.d incWidual Designation No. A&P/IA 3434119 1/9/20/5- FAA Form 337 (10/06) Page I SDNY_Givl_02759651 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246573 EFTA01331036 NOTICE Weight and balance or operating limitation changes shell be entered in the appropriate sirens!? record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. S. Description of Week Accomplished of more space is required. attach additional shoots (dent h secret nationaiW and registration math and date ewe completed.) • Milt2015 Nationality and Regolnition &lark Date REMOVED AVIATION COMMUNICATION AND SURVEILLANCE SYSTEMS (ACSS) TCAS SYSTEM PROCESSOR P/N 4066010-910 (S/N 91050384) AND ROUTED TO MANUFACTURER FOR INCORPORATION OF SERVICE BULLETIN 8008230-001, REVISION 02 (ATA SB 4066010-34-6036). REINSTALLED REPAIREDI MODIFIED TCAS PROCESSOR P/N 4066010.913 (SIN 91050384) AFTER INCORPORATION OF ACSS ATA SB 4066010-34-6036. PERFORMED OPERATIONAL TESTS WTTH NO NOTED DISCREPANCIES PER ACSS TCAS II SYSTEM DESCRIPTION AND INSTALLATION MANUAL (SDIM), ACSS PUB 0 CIS-3841-005 (ATA NO. 34-43-00). NO CREW OPERATIONAL PROCEDURES HAVE BEEN AFFECTED BY THIS SOFTWARE UPGRADE. MODIFICATION IS WITH REGARD TO PROCESSOR SOFTWARE ONLY AND THEREFORE: WEIGHT AND BALANCE IS NOT AFFECTED. ELECTRICAL LOAD IS NOT AFFECTED. CONTINUED AIWORTHINESS REQUIREMENTS ARE NOT AFFECTED. ALL WORK WAS PERFORMED AS PER FAA AD 2012.02-08. CAddltaUtiSh4)013 Are Attached FAA Form 337 (10/06) Page 2 SDNY_GM_02759652 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246574 EFTA01331037 Mobile Repair Team Boca0Aircraft • NAAINTENJANJCE CRS# 380R5358 3300 Airport Road Hangar 2 Suite 121 Boca Raton. Florida. 33431 MOO . baKia43 ft /WWI** lirral tiber a - 3?CA &SC\ O ?Tc±- - 20i:C— werehistio o asks to oe PFIiirlifeil (--,D (ICs Ik-tcw I C- 7 C ,t,Cci\Air NE \ ete,, Pe7Strirre Ars`rito ( VeTirilerff&) pi ee \I\ CA- N3 -N.... Cc, • erso sj A therized t rf c2 erO Tr, to S7 e Ira ^spectionsand Appr ved or Reit f • 10 Service e 6rnp oyee ©26117@italitcDr OCTIMillein J. C,S2 0rilik A •ri vi.‘ 0,,,.4 24 ,v•,T., -z y S Le r) 5- V Authorization efrUtist Kousmg Adequate a imps and Equipment a Parts and Materials Available Technical Data Available Et' RSIA/OO.1 Copy AviaLabla Et- Destination: F.J6 Notes: • Manager's / Lead's Signature Authorizing MRT Date. Form MRT 4/1/2011 SDNY_GM_02759653 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246575 EFTA01331038 • • • SDNYGM02759654 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246576 EFTA01331039 romtApporWl Enoric Treckna finest OIM we z‘200:00 0 tirJOrSOF VS Deow's.sei MAJOR REPAIR AND ALTERATION **flare 0* of Ttetspalien (Airframe, Powerplant, Propeller, or Appliance) codonlAvisdea AdeSiatrulen INSTRUCTIONS: Print or type as entries. See Title 14 CFR §43.9, Put 43 Amer* B. and AC 43.9.1 (or subsequent revision Owed) for inanabons and disposition of thi$ form This report is required by law (49 U.S.C. §44701). FaNure lo report can result in a civil penalty for each SuCh ViOlitiO . (49 U. S.C. 546301(e)) Nationality and Registration Mark Serial NO. N908JE 20115 1. Aircraft make Model Setts BOEING 727 31 Name (As ShOWII on togivronon °Miyake) AddreSS (As Shown on legtsinstiai cortMOAAM JEGE INC. wow. 103 FOULK ROAD SUITE 202 2. Owner stew 0 tar WILMINGTON to 19803-3742 Coat/ UNITEDSTATES 3. For FAA Use Only 4. Type S. Unit Identification Renew ARMWon Unil Make Model Serial No. O AIRFRAME (As dexROue on Item I above) Z El POWERPLANT O O O PROPELLER rya O APPLIANCE O Minufacturte 6. Conformity Statement A. Agency's Name and Address B. Kra al Agency woe FLIGHTSTAR AIRCRAFT SERVICES. 110. 06. coneested Necinent I Manutacturer Mises 8021FLIGHTLINE RD BLDG. 615 Fotiolati Girtkaki MOChark C. Certircate No. on JACKSONALE s FL i CertliCato0 nervier SIMON zy 32221 cater UNITED STATES FOTR986N CentkomaiminsenmotOrosnaMon 0. I certify trial the repair andfor alteration made to the WAS) klenflflOO in item 5 above and deserted an the reverse or altativntelit here*, have been made in accordance with the requirements of Part 43 al the U.S. Federal Alston Regulations and that the inforrnetlen fuenished herein is 'rut and cared to the best of my knowledge. Extended range fvel Sigr)ie Of Aulh5rnatO Individual per 14 CFR Part 43 App. B O ,e.,t..., Act/. - / PETER JACKSON 91482 MARCH 01, 2012 T. Approval for Return to Service Pursuant to Ow authority given persons specified beiow, the unit identified in item 5 was inspected in the manner pronatted by tie A0MiriSedlOf of Me Federal AvIEIPOO Administration and is gl Approved O Rejected FAA FR. 9landards Pence. APProved try Caliklen Manufacturer Maintenance Organization Mamba DepOrlfrent of Minivan BY Other (Speofy) FM Designee x Repair Station Inspection Authorization Onto:ale or Si u ,tiol dAu honied Individual Oesignation No. PETER JACKSON 91482 MARCH 01. 2012 FOTR986N osa.4920 " FAA Fun 337 uses) SDNY_GM_02759855 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246577 EFTA01331040 NOTICE Weight and balance or operating limitabon changes shah be entered in the appropriate aircraft record. An alteration must be compatible with at previous alterations to assure continued confomety with the applicable airworthiness requirements. S. Description of Work Accomplished (amore space is required. attach oddoonal sheets. Identify with aircraft national:I], and registration mark and date work comPieredl N908JE MARCH 01, 2012 Stationary and Registration Mark Date W/O 21219 1. WR 25306: REPLACED RIGHT WING FRONT SPAR VERTICAL STIFFENER AT APPROX. W.S. 200 WITH PIN 65-16200-3M IAW BOEING 727 SRM 51-30-2 REV. 103. 2. N/R 25522: REPAIRED RIGHT HORIZONTAL STABILIZER REAR SPAR LOWER CHORD BETWEEN STAB. STA 56 TO 113, IAW COTNEY AEROSPACE DRAWING AL81.55.101 REV. IR. FAA FORM 8110-3 DATED FEBRUARY 03, 2012 ISSUED. MATERIAL USED: ANGLE; PM54-2304 7075-T6511, DIM. 4" X 55.75% ANGLE; AND10137-3001 7075-76511, DIM. 16.375" X 3.75', RADIUS BLOCK; 7075-T6, 0.125', DIM. 12.5' X 2'. 3. N/R 25523: REPLACED RIGHT HORIZONTAL STABILIZER VERTICAL STIFFENER ON AFT SPAR AT ELEV. STA 53.91 IAW BOEING DRAWING 65-16876. MATERIAL USED: EXTRUSION; BAC 1505-29222 707576511. 12.5' LONG. END ❑ &Mb,* Meets Na Awned FAA Form 737 noes) SDNY_GM_02759656 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA (X1246578 EFTA01331041 Farm Approwel 11 wt Paden; Mats OW No 21204020 0 US Ogionmel MAJOR REPAIR AND ALTERATION 1.2•20is oda. Us O.* at Three:ono, (Airframe, Powerplant, Propeller, or Appliance) net.ii Media Aciaanithatiee INSTRUCTIONS: Print or type all entries. See Trde 14 CFR 643.9, Part 43 Appendix 13, and AC 43 9-1 (or subsequent revision thereof) for instructions and disposition of this but This report is required by law (49 U.S.C. §44701). Faire to report can result in a ovil penalty for each such violation. (49 U.S.C. 448301(1)) Natiortady and Registration Man( Serial No. USA N9C8JE 20115 1. Aircraft loam model Series Boeing 727 31 Name (As shown on regisuahon contain) Address (As sham on nesistration conical.) Amens 101FOUI K an STF 2112 2. Owner cry VVILhliNGTON sue DE_ JEGE INC 7. 19803-3742 coney ‘USA 3. Fa FAA Use Onty 4. Type S. Unit Identification Repair wierason Unit Make Model Sate No. (As clescdbedM Rem/wow) • if AIRFRAME O • POWERPLANT • • PROPELLER tyre O APPUANCE O lasnutaClurer it Conformity Statement A. Agency; Name aid Address El. Kind of Agency rem TIMM) u. S. Conf.:ow MeChenic I Manubicluart New 102 SE Academic Ave. Foreign Ceircaled meowno C. Certificate No. oil I eke City see Florida . / Cortriesise Reps, Station rr 32025 Owe, USA coneeter Mainianarek0Mtnawn DU4R141M Class IV D. Icor* Smith. repair anclior alteration made to the snit( ) identified in item S above and denoted 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 idonnation finished herein is true and correct to the best of my tnoweitge. Extended range fat Signs ate of A m671 par 14 CFR Pan 43 • APP. 8 A Gregory A. Christman - 28 FEB 09 7. Approval for Return to Service Pursuant to the authorey given persons below, the uNt Identified n dem 5 was inspected in the manner prescand by the Administrator of the Federal Adak., Administration and is 2 Approved O Rejected FM Fe Standards Manufacturer Maintenance Organization eenons Append by Deneefien Inspector Cepailement of Teensy:A BY Omer (SPIT*/ FM Designee I Repair Inspection ArAlloriZatiOn CerlifiCale Of Sign I Designation No DU4R141M Class n/ Anthony V. Baroni - 28 FEB 09 FAA Form 337 nom> SDNY_GM_02759857 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246579 EFTA01331042 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft retold. An alteration must be compatible with all previous excretions to assure continued conformity with the applicable airworthiness requirements. 8. Descdpdon of Work ACC0Mplish0d (If mote space is required, reface addtional sheets Wen* with atone nationatty and registration mak and date work completed) USA N908JE February 28, 2009 Nationally and Registration Mark Dale The following major modification was accomplished: 1. N/R #31809 Accomplished Deactivation of Rogerson Auxiliary Fuel System installed under STC #SA2734VVE in accordance with Quiet Wing Technologies Inc. Modification instructions No. M727-3-2008 Revision NC dated 19 NOV 08. approved per FAA Form 8110-3 by DER Mark Ostendorf #DERT-605421-NM dated 12/23/08. Minor deviations accomplished per Modification Instructions JEGE 8727-100 dated.2-26-09. SUMMARY 1. All work accomplished IAW STC fiSA2734WE and Quiet Wing Technologies Mod M727-3-2008. 2. Records of all work accomplished is on file at this repair station under Service Order #185008. 3. All Repairs are permanent unless otherwise stated. end Additional Sheets Ate Attached FAA Form 337000N SDNY_GM_02759858 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246580 EFTA01331043 Foe. Aocromi4 Becoa,t Lapp Mover ow en. zizo-coth ffri orthezoc MAJOR REPAIR AND ALTERATION ret MAUviiithe LiS owwwww of TSAI:WIN/0+ (Airframe, Powerplant, Propeller, or Appliance) Iodeni ANsfion Adminiontion INSTRUCTIONS: Print or type all entries. See Title 14 CFR §43.9, Part 43 Appendix a and AC 43.9-1 the subsequent revision memo° 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 sad. such violation. (49 U.S.C. §46301(e)) Nationality and Registration Mark Serial No N908JE 20115 1. Aircraft Maly Model Series Boeing 727 -31 Name (As shown on tegistathon condicate) Address (As shown on togishation certificate) JEGE Inc mufti. 103 Foul( Rd Sle 202 2. Owner Gib WiminatOn sew DE at 19003,3742 coon USA 3. For FAA Us. Only 4. Type 5. Unit Identification Repair Alteration Unit make Model Sonar No. (As desated in Item 1 80010) 0 (Z AIRFRAME o O POWERPLANT E 0 PROPELLER APPLIANCE 0 0 Manulack4s, 9. Conformity Statement A. AgencYs MIMS and Address B Kind of Agency rithe FLIGHTSTAR AIRCRAFT SERVICES. INC. u. S. Certhcated Mechanic I manuthcesw sass BLDG. 815,6025 FLIGHTLINE RD. 44441;n Certificsiod medwic C. Certificate No. ok, JACKSONVILLE es., Fl., / Catecated Raper Sheen be 32221 c....„, USA FOTR986N Ceonciders meinuensnce Organization D. I certify that the repair oridlor alteration made to the unli(+) identified in Mon 5 above end described on the reverse or attachments hereto have been made in accordance well the requirements of Pari 43 of the U.S. Federal Aviation Regulations and that the information i Mnlshed heroin is Duo and correct to the best or my knowledge. Extended range fuel Signature/Dale of Author! ad Individual per 14 CFR Part 43 0 CHRIS ADAMS 30 JULY 2008 APP. B It 7. Approval for Return to Service Pursuant to the authority given persons specified below, the MN Identified in item 5 was nspected in the manner prescribed by the Administrator of the Federal Aviation Administration and Is IZ Approved Rejected L FAA FN. Standards Persona approved bye:moan Manufacturer Maintenance Organization Desarvneri or Transport InspectOr BY Other (Spotty) FM Designee x Repair Station Inspection Authorization Corti math or Signature/Ciato of Authorized Individual Designation No. CHRIS ADAMS 30 JULY 2008 FOTR986N l id Cej , FAA Form 337 tooth SDNY_GM_02759659 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024658 I EFTA01331044 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft reCOnl. An alteration must be Compatible with all proWous alterations to assure contoured conformity with the applicable eiwnxthiness requirements. S. Oaticrlption of Work Accomplished (Ilmore space Is required, stla0 additional shoats. Identify mei aircraft nahenegity and repotratlon mark and dote work comaltfed) N908JE Nationality ON Registration Mn L 0 JULY 2008 Oats WIO 8181 1. COMPLIED WITH DFDR 11 CHANNEL UPGRADE IAW MODIFICATION ORDER EMTEO 2.80158.801 REV. B. DATED 07-30-2008 . FAA FORM 8110-3 DATED 07.30.2008 ISSUED. ENO ❑ Additional Shoots Ara Attached FAA Form 337 threat SDNY_GM102799660 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246582 EFTA01331045 0 MAJOR REPAIR AND ALTERATION Form Approved OMB No. 2120-0020 U.S. Departmtel of (Airframe, Powerplant, Propeller, or Appliance) For FAA Use Only Transportation Federal Aviation Office Identification Admabin tin INSTRUCTIONS: Print or all aeries. See FAR 43.9, FAR 43 Appendix B and AC 43.9.1 @shy:gas revision Chaco( for instructions and disposition of this form. This report is roquira q law (49 U.S.C. 1421). Ware to report can result ma cull penalty not to exceed $1,000 for cad. such vxdatan (Section 901 Federal Aviation Act of 1916). Make MODEL BOEING 727-31 Serial No. Nationality and Registraioo Mark 20115 USA N908JE I. Aircraft Name (As shoal on regisnatiOn eatificalc) Address (as shown on registration certificate) WOE INC 103 FOULK RD STE 202 2. Owner WILMINGTON, DELAWARE 19803.3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make I Model I Serial No. Repair Alteration AIRFRAME (As descriked in item I above) )O( POWERPLANT PROM 1ER Type APPLIANCE Mumfaeturer 6. Caaferalty Statuses • A. Agency's Name and Addreu B Kind of Agency C. Certificate No. U.S. Certificated Mechanic DU4R141M TIMCO Foreign Cenificated Mechanic 102 SE Academic Ave. X Certificated Repair Station CLASS IV Lake City, FL 32025 Manufacturer D. I certify that the repair sad/or alteration made to the units identified in km 4 above end described on the reverse or attachment% Mato have been made in accordance with Migliternatt3 of Part 43 of the U.S. Fedend Aviation Regulations and that the information furnished herein is true and correct to the bat of my knowkdge. Sisputure of Authorixed Individual Date April 28, 2008 Owen H. Pritchard t Approval for Return To Service Pursuant to the authority given persons specified below, the unit identified in itan 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is 121 APPROVED 0 REJECTED FAA F1L Standards Manufacturer Inspection /unhorizstion Other (%4c169 Inspolor FAA Designee X Repair Station Person Approved by Transport Canada BY Ainuatinen Group Date olApproasi or Rejection Certificate or Designation No. Signature of 'vides! April 28 2008 DU4R141M Antb yV 7 WrE :;1. CLASS IV FAA Form 337 (12-88) Us. 00VEINMENT MINTING orna 1992.76-012.0157 SDNY_GM_02759661 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246583 EFTA01331046 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.) Boeing Model 727-31 S/N 20115 Reg. No. N908JE Page 1 April 28, 2008 The following major repair was accomplished: 1. OPS #24157 Repaired frozen bolt at I/B elevator hinge of RJH horizontal stabilizer by removing .023" corrosion, HFEC, no cracks noted. Fabricated and installed I ea. bushing IAW TIMCO REO-L01064 Rev. IR dated 04/14/08 approved by FAA Form 8110-3 by Richard C. Saltivan #DERT-40157-CE dated Apr. 17, 2008. SUMMARY 1. All work accomplished JAW TIMCO REO and FAA Form 8110-3. 2. Records of all work accomplished is on file at this repair station under service order 185006. 3. Aircraft was weighed and Weight and Balance updated accordingly. 4. All repairs are permanent unless otherwise stated. -end-- CI Additional Sheets Are Attached * us GOWN*41DIT PIUN114O OPICE ISMI4S-0IMI SDNY_GM_02759662 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246584 EFTA01331047 Form Approved 0 OMB No. 2120.0020 For FAA Use Only US Oepanntert MAJOR REPAIR AND ALTERATION Office IderlaheatiOn Or Transportation Fount (Airframe, Powerplant, Propeller, or Appliance) aviation ...... So- rs vo- i INSTRUCTIONS: Print or type a entries. See FAR 43.9. FAR 43 Append& B. and AC43.9-1 (or subsequent revision thereof) for Instructions 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 such violation (Section 901 Federal Aviation Act of 1958). Make Model 1. Aircraft Boeing 727-100 Serial No. Nationally and Registration Mark 20115 USA N908.1E 2. Owner Name (As shown on registration minket.) Address (as shown on registration certificate) J.E.G.E, Inc. 103 Far* Road STE 202 Wkniegton, DE. 19803-3742 3. For FAA Use Only S.L.'. • in de Idevaieti bthe snow . :"'::: -.... • c....... arwortors itzwirentwes airersit r diddr. e serrred 43-7 spew sa_f 5V 0- 1-7 OCT Dim el ite= 4. Unit Identificat 5. Type Serial No. Alteration Unit Make Model Repair AIRFRAME '""'"'"""*"•(As described in Item 1 above) POWERPLANT PROPELLER Type APPLIANCE Manufacturer 8. Conformity Statement A Agency's Name and Address 8. Kind of Agency C. Certificate No. BANYAN AIR SERVICE u.s. Certificated Mechanic AVIONICS DIVISION Foreign Certificated Mechanic Radio SD4R514Mlass C 1.2.3 1635 NW 51st Place 0 Certificated Repair Station Limited Airframe Ft. Lauderdale, FL 33309 Manufacturer D. I certify that the repair and/or alteration made to the unit(s) 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 arid that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized Inch ( O ofg OCT-4912 0 1004 Steve Ouellette 7. Approval for Return to Service Pursuant to the authority given personsSpecified below; the unit identified In Item 4 was inspected n the manner prescribed by the Administrator of the Federal Aviation Adrrinistration and Is Si APPROVED O REJECTED FAA Fit. Standards Manufacturer inspection Authorization Other (Specify) BY Inspect( FM Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Refection Certificate or Signatur thodzed I . Designalion No. Oeneoc.;:goa4 . SD411.514M -oZ -- • Steve Ouellette FAA Form 337 (12436) SDNYGA402759663 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00246585 EFTA01331048 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 edationat sheets Identify with aircraft nationality andregistration mark and date work completed) The purpose of this 337 is for the work performe,on 119087E under Banyan Air Service; Avionics Division work order #71301 completed on A 023/ 46 A. Installed an AirCell Iridium ST-3100 P/N 400-10680-001 and removed a previously installed AirCell AGT.01 P/N 900001-2. Minor wiring changes were made at the mating connector IAW installation manual P/N 800-10680 Rev. B dated June 2005. B. The above installation was performed in accordance with AC43.13-IB, Chapter 7, sections 1-5, AC43.13-1B Chapter.11;sections 3-17, AC43.13-2A Chapter 1, AC43.13-2A Chapter 2, paragraphs 24 & 25 and the aircraft's maintenance manual. : A functional test of the aboVedquipment has been performed FAR25.B09 and FAR25 .1431 for proper operation and did not adversely affect any other aircraft systems. An electrical load analysis was conducted and it was confirmed that this installation would not exceed 80% of the generator output. D. A log book entry and equipment list was generated to reflect the above installation. The weight change is negligible. the equipment list was updated to reflect this change. E. Instructions for continued airworthiness is attached.. END O Additional Sheets are Attached SDNY_GM_02759664 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246586 EFTA01331049 Instruction for Continued Airworthiness for AirCell ST 3100 Aircraft Subscriber Equipment System Installed on Boeing 727-100 N908JE S/N 20115 Revision O. Dated: 9/17/2006 SDNY_GM_02759665 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246587 EFTA01331050 SDNY_GM_02759666 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246588 EFTA01331051 • APPLICATION REVISIONS DESC. NEXT ASSY USED ON REV DESCRIPTION DATE APPROVED ST 3100 ASE SYSTEM BARON 95-BSS A BASELINE RELEASE 2002-10-16 K. FRANTZ B SEE OEN 00579 2002.10-25 K. FRANTZ irniet ALL SHEETS CARRY THE SAME REVISION LETTER UNLESS OTHERWISE SPECIFED • DIMENSIONING & TOLERANCINt LAW IN ASAE Y14.5M-1994 lir C 11 AirCell, Inc. DIMENS/ONS ARE II STANDARD TOLERANCES. ir e 1172 Century Drive Suite 280, Building B .% t ±. .1 X< = 1.02 YYJC = ± .010 Louisville, CO 80027 APPROVED DATE PREPARED BY YEAR-MO-DA K FRANTZ 2002-10-16 MECH DESIGN YEAR-MO-DA INSTRUCTIONS FOR CONTINUED Z HOH 2002-10-16 AIRWORTHINESS ELEC DESIGN YEAR-MO-DA B. SOUKUP 2002-10-16 TECH SUPPORT B. NIELSON YEAR-MO-DA ST 3100 ASE SYSTEM 2002-10-16 SYSTEMS YEAR-MO-DA K FRANTZ 2002-10-16 ENGINEER,* YEAR-MO-DA SI2E CAGE CODE DRAINING NUMBER REV J. POISON 2002-10-16 A 1NO67 . 820-10680-001 B FILE FORMAT: Microsoft Word 2000 SCALE: NONE WEIGHT: NA SH 1 of 8 FILENAME: 820.10680-001-B.doe 65010377, A.St71SPEC TEMPLATE DOC SDNY_GM_02759667 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246589 EFTA01331052 SDNY_GM_02759668 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246590 EFTA01331053 ge e e TABLE OF CONTENTS 1 GENERAL INFORMATION 3 1.1 SCOPE Cc THIS DCCUP•ENT 3 1.2 TECI-MAL SLFPCRT CONTACT WORMATION 3 1.3 GENERAL NOTES 3 1.4 Acmsomes 4 p 2 SYSTEM DESCRIPTION 2.1 TCPLEVEL SYSTEM COVIGURATICN 2.2 OPERA1O4OF1HE SYSTEM 9 6 3 OPERATIONAL TIME LIMITS AND SCHEDULED MAINTENANCE ft 7 4 UNSCHEDULED MAINTENANCE ft 7 4.1 TRnan Fs-DOINGPRO:IMRE ft 7 5 AIRWORTHINESS LIMITATIONS ft 7 ft ft FIGURES AND TABLES Table 2.1-1 System Component Definition ft 6 Figure 2.1-1 Block Diagram of ST 3100 ASE System 6 ft ) ) ) ) AirCell, Inc. AltrCelf 1172 Century Drive Suite 280, Building B SIZE A CAGE CODE 1NQ67 FILE FORMAT: Microsoft Word 2000 DRAWNG NUMBER 820-10680-001 REV B Louisville, CO 80027 I SH 2 of 8 FILE NAME: 820.10680-00143.doc ST EOM ASCE SPEC TEMPLATE DOC SDNY_GM_02759669 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024659I EFTA01331054 SDNY GM 02759670 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246592 EFTA01331055 1 GENERAL INFORMATION f 1.1 SCOPE OF THIS DOCUMENT This manual defines the instruction s for continued airworthiness (ICAW) Subscriber Equipment (ASE) system. for an AirCelI 3000 Series Aircraft The manual is written to dem and 25.1529. Specifically, this onstrate compliance with FARs 23.1 manual defines the Instructions for 529 System (ST 3100). the Model 3100 Satellite Telephon e This manual is subdivided into secti 4 ons to support the general oper ST 3100 system. Section 1 defines gene ation, Inspection and maintenance I ral information for the maintena of the system. Section 2 provides general nce and airworthiness of the ASE Information on the configuration Section 3 presents a discussion of and operation of AirCell ASE systems. the scheduled maintenance and Section 4 and Appendix A provide operational time limits for the syste I instructions for system operation m. maintenance and component repla al checks, troubleshooting, unschedu cement. Section 5 provides a brief led limitations for the ST 3100 system. statement addressing airworthiness $ t 1.2 TECHNICAL SUPPORT CONTACT INFORMAT ION Technical support for AirCell products is available from 08:00 to 17:00 Zone GMT —7 hours) Monday through United States Mountain Time (Tim Friday. The contact information for e follows: AirCell Technical Support is as G Q G From a landline: Phone (in the US): Phone (outside the US): 1.888.286.9876 (toll free) 001.303.379.0278 (toll call) i From an AirCell phone: From an Air Mode/AMPS phone Q (in the US): 611 From a SAT Mode (Iridium) phone (toll free) (worldwide): 2471 (toll free) Email: customerservice@aircell.com Note: The toll free numbers for AirCe Q ll phones will only work for AirCell provided phones and services. 1.3 GENERAL NOTES V • All pages in this document carry the same revision level. Revision statu on each page of this manual. s is indicated by a letter printed • The material in this manual is subje ct to change. Before planning or maintenance operation, check with has the latest revision. AirCell Technical Support to verify that performing any installation or this manual is complete and ert • AirCell, Inc. welcomes your comm ents, suggestions, and corrections V include in your correspondence the publication number, equipment part concerning this manual. Please number, page or figure number, et and a brief description of any problem or consideration you noted. Plea se send your comments to: a AirCell, Inc. Corporate Publication Coordinator 1172 Century Drive Suite 280, Build ing B • Louisville, Colorado 80027 cpc@aircell.com a t kirrCelf AirCell, Inc. SIZE CAGE CODE DRAWING NUMBER 1172 Century Drive Suite 280, Building B A 1NQ67 820-10680-001 REV B ot FILE FORMAT: Micro oft Word 2000 Louisville, CO 80027 I SH 3 of 8 FILE NAME: 820-10680-001-B.doc Se csioon kSZE SPEC TEURATE.DOC SDNY_GM 02759671 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246593 EFTA01331056 SDNY GM 02759672 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246594 EFTA01331057 *) 1.4 ADVISORIES • WARNING • Statements in this section contain critical safety inform • carefully before installing this unit. ation. Read these statements • WARNING • Observe standard safety precautions and wear safety glasses to prevent personal injury while performing maintenance on this unit in the aircraft . 0, WARNING Shut off power before connecting or disconn ecting the ST 3100 system, as voltage b transients may damage the unit or the interface wiring. WARNING Components or subassemblies found in this unit may contain materials such as beryllium oxide, acids, lithium, radioactive material, mercury, etc. that can be hazardous to your health. If the component enclosure mat is broken ► , precautions must be taken against personal contact or inhalation in accordance with OSHA requirements 29CFR 1910.1000 or superseding documents. AirCell strongly discourages the opening or disassembly of sealed components. WARRANTY AND CERTIFICATIONS Any alteration of this product voids the FAA or FCC certification and the AirCell warranty. 2 SYSTEM DESCRIPTION The ST 3100 ASE system provides access to a range of two way communication options from an aircraft, including voice and data applications. With the ST 3100 system these services are available when the aircraft is in the air or on the ground. The AirCell satellite mode communications link Is provided using the 1600 MHz Iridium LEO (Low Earth Orbit-485 miles altitude ) satellite network, which provides coverage from the ground up over the entire surface of the earth. 2.1 TOP LEVEL SYSTEM CONFIGURATION The ST 3100 system consists of a number of primary system components. The heart of the system is the ST 3100 ASE Transceiver, which includes internal electro nics to support operation in the Iridium satellite network. Other system components include the externally mounted antenna, a low loss coaxial cable, and various user interfaces including multiple ASE handse ts (up to 9), an RS-232 data port, and an audio panel interface. AirCell, Inc. AirCelf 1172 Century Drive Suite 280, Building B SIZE A CAGE CODE 1NQ67 FILE FORMAT: Micro oft Word 2000 DRAWNG NUMBER 820-10680-001 REV B Louisville, CO 80027 I SH 4 of 8 FILENAME: 820-10680-001•Eldoc CGS XOTT. A.SIZE SPEC TONI-Alt1:QC SDNY_GM_02759673 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246595 EFTA01331058 SDNY_GM_02759674 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246596 EFTA01331059 The primary components of an ASE system include Line Replaceable Units (LRUs) and AirCell specified assemblies (such as coaxial cables or wiring harnesses) that are manufactured or purchased by the system installer. A list of the LRUs and specified assemblies is provided in Table 2.1.1, and a representative block diagram is provided In Figure 2.1-1 to demonstrate the interconnection of a typical ST 3100 system. For detailed information on the system components, please refer to ST 3100 ASE System installation manual (AirCell document 800-10680). or contact AirCell Technical Support for assistance. t Table 2.1.1 System Component Definition System Designatlo Description AirCell PH. Approved AirCall PH Component n Alternate(s) of Alternate System tRU ST 3100 • Transceiver _ASE Transceiver 400-10680-001 none • *4_,,,..Transceivet LRU 3/8 ATR Wen 3000 Seder : Mounting Tray Mounting Tray 800007.1 Mounting Rails 151.10689.001 System Wiring Specified 26 wire System NA Harness Assembly Harness ASE Handset LRU Flush Mount Standard ASE (4 400-10001.10x' Handset 400-10035-001C ASE Handset Podable Colic:ad ASE Handset 400-10015-00r Custom Retracted° ASE Handset 400-10019-COr Satellite LRU 1600 MHz Satelte 1600 MHz Satellite 015-10683-601 ASE Antenna _ ASE Antenna, Patch Style 015-10306-001 ASS Antenna. Blade Styx ee Satellite Channel Specified Low Loss Coaxial NA Coaxial Cable Assembly Cable (vendor item)" (4 4! • 'X' designates the color of the ASE handsets. 9 The system coaxial cable Is a required item that is not provided by AirCell. The system Installer will need to purchase this Item from an approved vendor as defined later in this document. • ar ai a ai 4Airrce il •e AirCell, Inc. SIZE CAGE CODE DRAWING NUMBER REV 1172 Century Drive A 1NQ67 820-10680-001 B Suite 280, Building B FILE FORMAT: Microsoft Word 2000 SH 5 of 8 Louisville, CO 80027 FILE NAME: 820-10680-001-B.doc Mixon.xsai SPEC TDAPLATE SDNY_GM_02759675 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246597 EFTA01331060 SONY GM 02759676 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246598 EFTA01331061 ME SATEUJ1E 6 \-I AHIDMA 0 AM SYS HS CNCIR ASE 'wow CHANNEL 0 FUSELAGE 0 ASE SYS HS Oat CI MED ASE HANDSET CANNEL 0 ME SYSITU %OR ASE SYS HS CN 0 ] AN HANDSET CHANNEL SAT AN1D1NA CD TO AUDIO PANEL MIX ENGIRD NO COWECTION ASE SYS RS232 OCT, O TO 1.5.23.2 DATA TERMNAL SYS DIOR TO NRCRAFt PMER (28 We) AtrotArr FUSELAGE Figure 2.1-1 Block Diagram of ST 3100 ASE System p Note: Each 'Handset Channel' listed above is capable of supporting up to 3 ASE handsets, making it I possible to integrate up to 9 handsets in the ST 3100 system. I 2.2 OPERATION OF THE SYSTEM p The user interface and operation of the ST 3100 system is designed to be very similar to the operation of a p terrestrial cellular or PCS phone. Some key features of the ST 3100 system are as follows: • The system will power up when the avionics master switch for the aircraft Is powered on. The p AirCell system Is always on when the avionics master Is powered on. I • ' The Satellite mode network provides coverage anywhere on (or above) the surface of the earth with a I clear view of the sky in all directions. • To place a call from the system handset, the user must verify that the system is 'in service'. SAT mode calls are typically dialed as international long distance calls (00 + country code + phone I number). After dialing, the user must press the " SND key on the handset, and the phone call will proceed as a typical cellular or PCS call. At the completion of a call, the user may press the " END p key to terminate the call. If • The user may receive Incoming (ground to air) phone calls depending on the in service condition. The user can answer these calls by pressing the ' SND ' key on the handset. • Data calls can be made from Air to Ground over the ST system by connecting a Data Terminal I Equipment device (such as a PC) to the RS-232 port of the system. The ST system has a built in modem function, so some user setup of the DTE will be required. p More detailed operating Instructions are provided for this system in the ST 3100 User's manual (AirCell document 810-10680). p I AirCell, Inc. SIZE CAGE CODE DRAWING NUMBER REV cifinCell. 1172 Century Drive Suite 280, Building B A 1NQ67 FILE FORMAT: Micro oft Word 2000 820-10680-001 B SH 6 of 8 Louisville, CO 80027 FLE NAME: 820-10880.00143.doc OPYKOn A.SLZE5PFC lEMPLATEDOC SDNY_GM_02759677 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246599 EFTA01331062 SDNY_GM_02759678 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 002466((1 EFTA01331063 3 OPERATIONAL TIME LIMITS AND SCHEDULED MAINTENANCE result of The ST 3100 system is designed and manufactured to be maintenance free after installation. Asa operational time limits or periodic maintenance checks or procedures that must be this design, there are no performed for the system. Inspections and/or system verification checks are only required In the event of a system failure (On Condition), as defined in Section 4 of this document. As an option, the system operator may perform a visual inspection of the various system components at the aircraft annual inspection, or other periodic maintenance Interval as defined by the aircraft manufacturer. 4 UNSCHEDULED MAINTENANCE The ST 3100 system is designed for "On Condition" maintenance only. In the event of a system failure, the system user/aircraft operator is advised to follow the troubleshooting procedure defined in Appendix A of this manual. After performing the basic procedure, the user will either have returned the system to normal operation, or should contact AirCell technical support for additional guidance. Note that, in the process of performing the troubleshooting procedure, authorized field service personnel are (with prior permitted to perform repairs to wiring harnesses, RF cable assemblies, mounting interfaces, or approval from AirCell Technical Support) to remove and replace any of the primary system Line Replaceable level Units (LRUs). AirCell does not, under any circumstances, authorize field repair or subassembly Sealed LRUs should always be returned to the AirCell FAA Repair Station for maintenance on any LRU. evaluation and repair. 4.1 TROUBLESHOODNG RROCEDLRE Appendix A provides a guide to identify simple problems that may be identified and/or resolved with simple field inspection and test processes. It is advised that the procedure in this appendix should be performed before contacting AirCell Technical Support for additional instruction. No specialized tools or equipment are required to perform this procedure. the In the event that a step in this procedure is not dear, or the results of a procedure are not conclusive, test operator should feel free to contact Technical Support for assistance., 5 AIRWORTHINESS LIMITATIONS The AirCell ST 3100 ASE system is a non-critical communications system. In accordance with FAR 23.1529 (with Pan 23 Appendix G) and FAR 25.1529 (with Part 25 Appendix H) this system has no Airworthiness Limitations for either Part 23 or Part 25 aircraft. The airworthiness limitations section is FAA approved and specifies maintenance required under Sections 43.16 and 91.403 of the Federal Aviation Regulations unless an alternative program has been approved. AIrCell, Inc. SIZE CAGE WOE DRAWING NUMBER REV AirCell 1172 Century Drive Suite 280, Building B A 1NQ67 FILE FORMAT: Micro oft Word 2000 820-10680-001 B SN 7 of 8 Louisville, CO 80027 FILE NAME: 820.10680-0014.doc WMCOTT. A.SZE WIC TEMPIATEOCC SDNY_GM_02759679 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246601 EFTA01331064 SDNY_GM_02759680 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246602 EFTA01331065 4./ 0 • • I p • 9 Appendix A b p ST 3100 ASE System Troubleshooting Procedure p ) ) ) ) ) ) ) ) ) ) iv. AirCell, Inc. SIZE CAGE CODE DRAWING MJ!,16ER REV ) ) AirC ell 1172 Century Drive Suite 280, Building B A 1NQ67 820-10680-001 B ) Louisville, CO 80027 FILE FORMAT: Microsoft Word 2000 I SH 8 of 8 ) ter1.1077). SZE SPEC TENRATE DOC FILE NAME: 820.10680401-B.doc ) SDNY_GM_02759681 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246603 EFTA01331066 SDNY GM 02759682 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246604 EFTA01331067 EFTA01331068 8I AirCell -o c (0 Possible Caine Discussion Verification Step(s) Symptom The handset display should always CI Verify that the aircraft power system (master avionics switch) is on. Symptom I Power is not available to ASE be illuminated when power is O Verify that the ASE system circuit breaker is closed. C9I a-1 System Handset Display is applied to the ASE transceiver. O Visually inspect the displays of all installed handsets in the system. If all handsets not illuminated Because the failure of a handset are off, proceed to the next bullet in this list. If most handsets arc illuminated, but display is unlikely, a 'dead' display one is not, then proceed to Symptom 2. (One or more suggests that there is a problem with O Wall handset displays are dead, the problem is likely in the power system wiring handsets integrated in the input power to the ASE system. before the ASE transceiver. Visually check the system connections and the wiring , aC system, no handset In the event that the one or more harness leads between the transceiver and the aircraft power system. Repair or displays are handset display(s) are not reconnect any obvious problems. 06. illuminated) illuminated, the user/operator should O If needed, ring out the power lints per the system wiring diagram. Repair any verify that aircraft power is on and broken wires or rework to match the system wiring diagram. available to the ASE transceiver. O If this procedure does not resolve the problem, contact AirCell Technical Support tr) for additional guidance. O Some ASE systems integrate multiple handsets. If more than one handset is • Bad connection or faulty wiring In a system with multiple handsets, Symptom 2 installed on the system, check the display on all handsets. If only one of multiple between handset and if some handsets are operating and Handset Display is handsets is not illuminated, then the problem is either a bad handset or in the handset not illuminated transceiver• some arc not, then it is likely that connection! wiring harness between that handset cradle and the transceiver. cc either the handset is bad or the wiring between the handset and the O Perform a visual inspection to verify that all connections arc made in accordance (ASS System has or transceiver is faulty. with the system wiring diagram. Correct any obvious problems. multiple handsets, O If all system connections arc correct, then switch the 'dead' handset with a known Bad handset good handset and retest the system. lithe handset is still dead in the new location, and the displays of most handsets are on, then the handset is bad. Contact AirCell Technical Support for repair/replacement a. instmetions. but one handset is not O If the known good handset is now dead, then the problem is in the system cc illuminated.) wiring/connections between the handset and the transceiver. Ring out the lines per the system wiring diagram. Specifically check for 9V power and ground leads on 0 the HS power line from the transceiver system connector. Repair any broken wires c4 or rework the system wiring hamar to match the wiring diagram. 0 0 If this procedure does not resolve the problem, contact AirCell Technical Support for additional guidance. 0 o_ 0 A-1 ST 3100 ASE System Troubleshooting Procedure );.•*. •• ;a, 820-10680-001, Rev B • 3 c7 i • tit hn-ftteittilt. SDNY_GM_02759684 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246606 EFTA01331069 EFTA01331070 viiv vs sew wwwwwww ur sir er var vs se is se it IP ler vb 1St IP eV nil WI le1 k irCe1F Symptom Possible Cause Discussion VerificationStep(*) Symptom 1 Possible Cause 3A The ST 3100 transceiver operates in Verification Test 3A O Verify that the system SAT antenna has a clear LOS to the sky in all directions. A Handset Display is System antenna does not have Satellite (SAT) mode. When in illuminated and Line of Sight (LOS) view to coverage the ST system should clear LOS is defined to exist when there are no obstructions (such as buildings, display indicates no satellite. detect and register for SAT mode trees, vehicles etc) that are higher than 30 degrees above aircraft horizon in any signal for Satellite service. direction. This should never be a problem in flight. (SAT) mode. O Use the handset to enter the SAT lock mode (FCN, 3, 3) keys on the handset. The Ql If the system does not register, then it is likely that either the antenna handset will display the word "IRIDIUM" when the SAT mode is locked. does not have a LOS to a satellite O Once the LOS has been established the system should register on the SAT network within 60 seconds. The system is registered when the "NO SVC" indicator is not OO (3A), or there is a problem with the visible on the handset display. RF channel in the aircraft (38). In this condition, it is unlikely that O If the "NO SVC" indicator extinguishes, then the SAT mode is engaged, and the v) there is a problem with the system problem is resolved. The user may choose to make a test call and verify the transceiver, operation the system. O If the - NO SVC" indicator stays illuminated, then the system cannot register, and it is likely that there is an installation or equipment problem. Either contact AirCell Technical Support for additional guidance, or proceed to Verification Test 38. cc No Satellite mode Possible Cause 3D Verification Test 3D w signal There is a problem with the O While the aircraft is on the ground, perform a visual inspection orate ASE system Satellite RF channel. satellite antenna. Verify that the antenna is installed to the aircraft fuselage in accordance with the system antenna installation drawings. Verify the mechanical < integrity of the antenna, and that the antenna is reasonably free of dirt, oil, ice and other undesired coatings. a_ O Visually inspect the RF satellite channel, including the coaxial connections to the cc antenna and the system transceiver. Inspect the coaxial connectors to verify that Lu they are connected in accordance with the system wiring diagram, and that they arc C not damaged. Look for breaks, kinks or other damage to the coaxial cable. 0 The user is authorized to correct installation errors (such as cabling errors), or to repair minor damage (such as broken coaxial connections, damaged coaxial cables, etc). The user is not authorized to open or modify sealed LRUs. Lu O If these steps do not resolve the problem, contact AirCell Technical Support for additional guidance. Other conditions For all other conditions, contact AirCell Technical Support for guidance. U Lu 0 O I- A-2 I- U ST 3100 ASE System Lu Troubleshooting Procedure 820-10680-001, Rev B cTo' D SDNYGM_02759686 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246608 EFTA01331071 Forrn Approved 0 OMB No. 2120-0020 For FM Use Only aosarenant nmortation MAJOR REPAIR AND ALTERATION Office klentificalion Powerplant, Propeller, or Appliance) For Fs So- Ask., AdISIMMIOn DO- iq INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC43.9-1 (or subsequent revision theme° for inalnadtkaa and diseosltion 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 breach such violation (Section 901 Federal Aviation Act of 1958). Make Model 1. Aircraft Boeing 727-100 Serial No. Nationally and Registration Mark 20115 USA N908JE 2. Owner Name (As shown on registmeon certificate) Address (as shown on registration certificate) J.E.G.E, Inc. 103 Foot Ftoad STE 202 INihnington, DE. 198033742 3. For FM Use Only .., 4. Unit identification S. Type Repair Alteration Unit Make Model Serial No. AIRFRAME (As described in Hem 1 War ►all POWERPLANT PROPELLER Type APPLIANCE Manures:haw 6. Conformity Statement A. AgenCits Name and Address B. Kind of Agency C. Certificate No. BANYAN AIR SERVICE U.S. Certificated Mechanic SDIR514M AVIONICS DIVISION Foreign Certificated Mechanic Radio Class1.2,3 1635 NW 51st Place 0 Certificated Repair Station Limited Airframe Ft Lauderdale, FL 33309 Manufacturer D. I certify that the repair and/or alteration made to the unk(s) Identified ki kern 4 above and described on the reverse or attachments hereto have been made in accordance wan the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein S true and coned to the best of my knowledge. Date Signature of Authorked c_Inr2a2,__ October 10. 2006 Steve Ouellette 7. Approval for Return to Service Pursuant to the authority given pensoressecified below, the unk identified in kern 4 was inspected in the mater coescralial by the Administrator of the Federal Aviation Administration and SO APPROVED O REJECTED FM Ft. Standards Manufacturer Inspection Authorization Other (Specify) BY Inspector FM Designee X Repair Station Person Approved by Transport Carlin AIWOrthilltin Grow Dab c4Approval or Rejection Certificate or sian2re:TrIzed I I 0esienston No. October 10, 2006 SD4R5I4M - e--- Steve Ouellette FAA Fam 337 (1248) SONY_GM_02 759687 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246609 EFTA01331072 • NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An Operation must be compatible with eh pmvious alterations to assure continued conformity with the applicable ainvorthlness requirements. 8. Description of Work Accomplished (// mole space is required. Witch edthtionsi sheets Identify Sin aircraft natiOnelity and registradan mark and date work completed) The purpose of this 337 is for the work performed on N908Th under Banyan Air Service; Avionics Division work order #71301 completed on October 4, 2006. A. Installed an AirCell Iridium Antenna P/N S67-1575-109 in accordance with DER Services drawing number 2006-173-1 approved per FAA form 8130-3 signed by Robert Belgau DERT designation number DERT-510024-CE. B. The above installation was performed in accordance with AC43.13-1B, Chapter 7, sections 1-5, AC43.13-1B Chapter 11, sections 3-17, AC43.13-2A Chapter 1, AC43.13-2A Chapter 3, paragraphs 43 & 44 and the aircraft's maintenance manual. A log book entry and equipment list was generated to reflect the above installation. The weight change is negligible. the equipment list was updated to reflect this change. D. Instructions for Continued Airworthiness is "on condition only." Additional Shies are Attached SDNY_GM_02759688 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246610 EFTA01331073 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTATION DATE STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS October 07,2006 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE TYPE mil e"* A•sw macww al NAME OF APPLICANT Boeing 172731E Airplane Banyan Air Service LIST OF DATA IDENTIFICATION TITLE DER Services Effectivity: Drawing: S/N: 20115, T/N: N908JE 2006-173-1 Iridium Antenna Installation STA 515 - BTWN S-2R & S-3R . Rev. UR tr.:. Dtd. 27-Sep-06 END ____ END END END END END END END END END END END Note: This aircraft is effected by AD 98-11-03 RI. Certification to FAR 25.571, Damage - tolerance and fatigue evaluation of structure may be required. Per Advisory Circular 25.1529-I Instructions for Continued Airworthiness of Structural Repairs on Transport Category Airplanes, the damage tolerance and fatigue evaluation of the structure must be performed before 4/11/2003. Notes: 1) 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 approval. (Ref. 8110.45 8/30/02 for more info) 2) This approval is valid for the aircraft model and aerial amber listed below 3) This approval is based on FAA Approved structural analysis on file at DER Services Office in Ft. Lauderdale, FL. or DER Services, Inc. office in Birmingham AL. Model No. 727-31 Serial No. 20115 PURPOSE Approve data for low profile antenna installation (structural aspects only, Stalls Analysis) OF DATA APPLICABLE REQUIREMENTS (LIST SPECIFIC SECTIONS) CAR 46.200, 46.201, 4b.202, 4b.260, 4b301, 46.302,46.303, 4L106 CERTIFICATION - trader antbotity vested by dirt-thee of the Administrator ad is accadaace with coadidos sod limitation of sppolatrant oder Part IS) of the Federal Mimics Repletion, data listed been tanated In accordance wltb established proudest sad toad to comply with applicable regainmeas of the Fatal Aviation Repletion I (We) Therefore O Reamstend approval of these data ril i Approve these data SIGNATVRUS) Or DESIGNATED ENGINEERING REPRESENTWEW) DESIGNATION MAIDENS) CLASSIFICATIONS) Robert J. Belgau DEBT-510024-CF. Structures esen---(•••-•- -rid, IAA FORM II 14.311i.n)strrascou PittViOUS tOrrilXv DER SERVICES PROJECT NO. F2066-173 SDNY_GM_02759689 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246611 EFTA01331074 SDNY_GM_02759690 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002466 I 2 EFTA01331075 EFTA01331076 en •er Cg N 8 7 6 5 4 3 I 2 at C in I. GENERAL NOTES: DESCRIPTION DATE APPROVED VR INITIAL RELEASE 09-27-200T{(4,42az 1. FABRICATE PART(s) AS SHOWN. Lri O ri 2. BEFORE INSTALLATION OF DOUBLER. ROLL TO STA 515.00 FASTENER CODES z vi D MATCH AIRCRAFT MOLD UNE RADIUS. ITEM DESCRIPTION saananstrel•Wa D •O ri 3. BREAK AU. SHARP EDGES .020/.030 R. telASANOONAIPUN cri 4. TREAT ALL REWORKED AREAS USING ALODINE 1201S (PER MIL-C-5541. CLASS 1A) AND TWO (2) COATS OF 0 EPDXY POLYAMIDE PRIMER (PER MIL-P-233377, TYPE I). 5. FINISH ALUMINUM PARTS USING ALODINE S - 2R EXISTING FUSELAGE SKIN R 120IS AND TWO (2) COATS OF EPDXY PRIMER. (REF) S - 3R --- 6. MAINTAIN MINIMUM 2D • 1/16' EDGE DISTANCE C FOR AU. FASTENERS ON DETAILS; MINIMUM 2D EDGE DISTANCE ON ASSEMBLY. STA 510 .--- STA 520 C re 7. ALL FASTENERS ARE TO BE INSTALLED IN <9 TRANSITION-FIT HOLES. HOLE TOLERANCE PER RAVINE cc EXISTING BONDED 8. ALL FASTENER LENGTHS ARE TO BE VERIFIED STRAPS 4- FOR TOLERANCE PRIOR TO INSTALLATION. (REF) cc 9. INSTALL ALL PARTS AND THREADED FASTENERS WET USING PRIAM TYPE III SEALANT ON ALL 0 FAYING SURFACES. EL 8 8 10. RESTORE ORIGINAL FINISH PER 9727 M.M. 51-21. 50 COUNTERSUNK RIVET NAS I 097AD4 -2 OP L 0 8 RIVET - NUTPLATE ITS20426A03- 2 OPL 11. PROTECT REWORKED AREA AGAINST 4 4 SCREW MS24694C55 OPL CORROSION PER 8727 SRM, CHAPTER 5140-2. .3 4 NUTPLATE NAS1473A3 OPL 2 1 DOUBLER - INTERNAL 0.050" 2024-T3 00-A-25015 OPL 12. REFERENCE 8727 S.R.M. CHAPTER 51.30 FOR LI CPS-IRIDIUM ANTENNA 567-1575-109 OPL FASTENER REMOVAL AND INSTALLATION PROCEDURES. ITEM Ott NAME PART NUMBER MATERIAL MIL -SPEC VENDOR 13. REINSTALL ALL ADJACENT STRUCTURE Ports List O A REMOVED TO FACILITATE ANTENNA INSTALLATION. liitss scat NA BANYAN AIR SERVICE Mit orICHA LIT a DER OW ~SERVICESI la tin 100 A cc o_ 14. BEAD SEAL ANTENNA WITH PRC 1422 SEALENT. SAMOA MANI 802bra OCCJIDA OM Ns MOP/SAY02 SAAAAAN Al- ORAIVIC• /anew an , WAYS —ft gs'atiNINSEP 09-27 2006 IRIDIUM ANTENNA INSTALLATION STA 515 SINN S-2R 8 S.3R 0 •••001......s • Ca losm•army @SSA UNSPEEISIED TOLERANCE W.D.OUVERI Ait NT. BOEING av 15. REVISE AIRCRAFT RECORDS TO REFLECT INSTALLATION. A.600a. as WI S•••• .. a we •PO —AV I•al. NAAA/AAO Atari seorvic• FOLIOS NCLES IECDIALS A Si MAW m sacs IPA R.J.BELGAU stt w.. 727-3f r 2006-173-1 !TR ••• OA••• Fmoun ••••• Poo era AA amithSr. SY re ...CMS_ !I/32 t 43 miss to W.D.OUVERI us. w N902KIE 0. 3J g 2006-173 nt NA. Tu. t AI ammo rn R.J.BELGAU stRAL IA .20115 STRL INSTL no fir 3- 8 7 5 4 1 3 2 1 V) SDNY_GM_02759692 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246614 EFTA01331077 EFTA01331078 8i r-r E,4C 7 6 5 4 3 2 at tn 8 (13 IRIDIUM ANTENNA INSTALLATION STA 515 01.00 © STA 515.00 - BTWN S-2R 8 S-3R ri STA 510 CONNECTOR CUTOUT IN SKIN STA 520 A D c EXISTING BONDED EXISTING STRAPS FUSELAGE SKIN (REF) EXISTING BONDED (REF) cri STRAPS (REF) 00 - S - 2R r-: (n 0 0 • 0 0 0 0 C 0 0 • •••• • o • C cc • • C9 ea f • cc 4 •r • ° a • LBL 12 4- • • • .. • CL LLI • it 0_1_ • • • • 0 a • • • 0 0 0 0 a 0 - S - 3R U w EXISTING BONDED H STRAPS (REF) cc EXISTING A -I 4 a_ A FUSELAGE SKIN x4 SECTION A-A A 0 (REF) VIEW LOOKING UP Tins roe... an AN OMR •CoW001.6.NOMPAIMICDOCCOMPThano. • 01111.... As.es se glea. Ow 6.. ..•••• DER SERVICES ir 2006-173-1 H • Ca *tan as, lie% saminitaarretwa frea. emeid Op talon on am man OM Wows Sauey MIA rt lailiatia FL la wan ream.. is. gab ninimio•00.6,420 B W.D.OUVERI OR SOME STRUCTURE REMOVED FOR CLARITY an WRAY no Om off miner% fa. manors shale...a/ •••••••• ONINSWHINO U de. •••••••••••3 IMMWA swot or 20115 KA13•4 I, wit 2 If 3 8 I 7 5 4 3 I 2 1 tn SDNY_GM_027596. SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002466 I 6 EFTA01331079 a O a a 0.00 0.38 0.75 0, O, 1.13 1.50 1.88 2.25 2.83 O 3.00 3.38 ---O 3.75 ! MINI 4- 4.13 i i iiiqi i 4.50 O .. il ii i i i 4.88 O I 5.25 O O O O it " I I tot Oft tit. I 5.83 .._ O O O I. O I iiti i 6.00 I j.! .0, q, lit' 1 i ri 1 ,:' ,.., z 0 Jo)Ei 0 OK% XV °WM (7 ill va O O SDNY_GM_02759695 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246617 EFTA01331080 , SDNY_GM_02759696 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 002466 I8 EFTA01331081 ._ Form Approved 0 OMB No. 2120-0020 For FAA Use Only us Depactran MAJOR REPAIR AND ALTERATION Office Identification or Trainecetarthe (Airframe, Powerplant, Propeller, or Appliance) So- re) Do - /7 Faders Awoke, MminIstnalon INSTRUCTIONS: Print or type all enures. See FAR 43.9. FAR 43 Appendix B. and AC43.9-1 (or subsequent revision thereof) for instructions and C0SP0SIt0rl of this them. This report is required by law (49 U.S.C. 1421). Faure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act o(1958). Make Model 1. Aircraft Boeing 727-100 Serial No. Nationafity and Regisbabort Mark 20155 USA N908JE 2. Owner Name (As shown on registratlan cerfAkate) Address (as shown on rogistrstion certificate) J.E.G.E. Inc. 103 Pout Road. Ste 202 • Wimington, DE. 19803-3742 3. For FAA Use Only 4. Unit Identification s. Type Unit Make Model Serial No. Repair Alteration AIRFRAME """""•"'s(At deserted Mir 1 above 0. POWERPLANT PROPELLER Type APPLIANCE Manufacturer IL Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. BANYAN AIR SERVICE U.S. Certificated Mechanic SD4R514M AVIONICS DIVISION Foreign Certificated Mechanic Radio Class 1,2,3 1635 NW 51st Place 0 Certifkated Repair Station Limited Airframe Ft. Lauderdale, FL 33309 Manufacturer D.1certify that the repair andkit alteration made to the unit(s) lammed in Kern 4 above and described on the reverse or attachments hereto have been made in accordance %Nth the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is We and coned to the best of my knowledge. Date • Signature of Autheria2.3.1 . 4 _,./2 : x i / et_ 8 November 2004 Zoe/ Steve Ouellette 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 prescnbed by the Administrator of the Federal Aviation Administration and is APPROVED O REJECTED FAA Fit. Standards Manufacturer inspection Amthorlzabon Other (Specify) BY inspector FAA Designee Repair Station Person Approved by Transport Canada Atheorthiness Group X Date of App oval or Rejection Certificate or Signature of Authorized Individual Designation No. ........ ) d2l egit u 19 November 2004 9D4R314M t_ Steve Ouellette FAA Form 337 02-88) SOFIY_GM_02759897 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246619 EFTA01331082 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. Description of Work Accomplished (IImore space is required, attach additional sheets Identify with aircraft nationality end registration mark and date work completed) The purpose of this 337 is for the FAA approval of the new flight manual supplement on N908JE under Banyan Air Servive, Avionics Division work order #68062. A. Removed existing TDR-94 transponders P/N 622-9210-003 and routed to the manufacture for upgrade to P/N 6252-9210-007 to provide flight ID. System ground and flight checked good. B. The weight & balance is not affected and equipment list was updated. C. Instructions for continued airworthiness are "on condition only". END O Additional Sheets are Attached SDNY_GM_02759698 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246620 EFTA01331083 Form Approved OMB No. 2120-0020 - - 0 For FAA Use Only US Deponmem MAJOR REPAIR AND ALTERATION Office Identification f a Federal (Airframe, Powerplant, Propeller, or Appliance) 1 A,&gon 50 •3 /4 1451)6P-47 ! AdmiNstraban INSTRUCTIONS: Print or type all obits. See FAR 43,9, FAR 43 Appendix B. and AC43.9-1 (or subsequent revision thereof) for Instructions a 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 I. Aircraft Boeing 727-100 Senal No. Natlonaity and Registration Mark 20115 USA N908JE 2. Owner Name (As shown on registration certificate) Address (as shown on registrallon certificate) J.E.G.E, Inc. 103 Folk Road STE 202 • Wilmingten, DE. 19803-3742 -- 3. For FAA Use Only 4. Unit Identification 5. Type Repair il terabon • Unit Make Model Serial No. AIRFRAME •m1-----"(AS described in Item 1 abover--- --- el POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6. Confomilty Statement A Agency's Name and Address B. Kind Of Agency C. Certificate No. BANYAN AIR SERVICE u.S. Certificated Mechanic SD4R514M AVIONICS DIVISION Foreign Certificated Mechanic Radio Class 1.2,3 1635 NW 51st Place I81 Certificated Repair Station Limited Airframe Ft. Lauderdale, FL 33309 Manufacturer 0. I certify that the repair ancllor 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 Author iduaadail. ar A‘l/eifrilge? a Steve Ouellette . '°‘71 7. Approval for Return to Servile 1 Pursuant to the authority given persons cified below, the 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 Ft Standards Manufacturer inspection Authorization Other (Specify) BY Inspector FMDesignee Dale of Approval or Refection /9 ferewisel_ace , X Repair Station Certificate or Designation No. SD4R514M win Pilsen Approved by Transport Canada Ainvorthiness Group Signature II /* '''''' Steve Ouellette FM Form 337 (12-83) SONY_GM_02759699 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246621 EFTA01331084 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. O. Dinalotion of Work Accomplished (It more space is required, attach wititional sheets. Identity with aircraft flattened), andregistration mark and date week completed.) The purpose of this 337 is for the work performed on N908JE under Banyan Air Service, Avionics Division work order #68062. A. Installed a Universal Avionics Systems Corp. Terrain Avoidance and Warning System in accordance with SIP Technical Services, Inc. data list 7280-DL-001-501, Rev. H dated December 5,2002 or later. (STC# ST09951SC) B. The above installation was performed in accordance with AC43.13-1B, Chapter 7, sections 1-5, AC43.13-1B Chapter 11, sections 3-17, AC43.13-2A Chapter 1, AC43.13-2A Chapter 2, paragraphs 24, 25, and 28, AC25-23 and the aircraft's maintenance manual. C. A functional test of the above equipment has been performed FAR25.1309 and FAR25 1431 for proper operation and did not adversely affect any other aircraft systems. An electrical load analysis was conducted and it was confirmed that this installation would not exceed 80% of the generator output. D. A log book entry and equipment list was generated to reflect the above installation. A weight & balance was calculated. An FAA approved flight manual supplement provided with the above STC, Document No. 7280-FM-001, dated December 13, 2002 or later E. Instructions for continued airworthiness provided by SIP Technical Services Report No. 7280-ICA-001 Rev. F dated June 6, 2002. END O Addilional Sheets are Attached SDNY_GM_02759700 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246622 EFTA01331085 !tuna ,tate• Of eetencriut ptpartment of Zaransparintion - gehrrnl cikbizition jktiministralion Supplemental Egpr aertifirate ST09951SC &-iftesah• award/0 SIP Technical Services, lac. 10107 McAllister Freeway San Antonio, TX 78216 era 4u ea or., b. a yr , .4.9.A. GMerowasis, sear assi sznetena4 ZZONA•aJ 44000S01 07,0r4 46 sabsbablefibeiki yerabiwaseisti ivegiwit 4b 1/c& Civil Air Sacjiaral.r. ektouregkv&e., .Fif/se KelOoszie ./Ifiest4e: A3wE ada.4.. Boeing - 0 -4•441 : 727-100 Series giosootavb ("rem atogw, War Installation of a Universal Avionics Systems Corporation Terrain Awareness and Warning System in accordance with SIP Technical Services, Data List 7280-DL-001-501, Revision H, dated December 5, 2002, or later FAA approved revision. FAA approved Airplane Flight Manual Supplement Document Number 7280-FM-001, dated December 13, 2002, or later FAA approved revision is required. Siouratavw resireassia4nS. Compatibility of this design change with previously approved modifications must be determined by the installer. If the bolder 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. 82.3 Kra // that" andh& JOISWee41, data rairket t ‘t iftweVa.b syrbata-osvas:b 6. viren.a Jae...staved Ja4neneed nrchetaia, a knasinalien W.4 I cawrae intateW4. 44 aiiauh,:serato, 044 .3i.t4e,ae l../Sevialeys ../erkstoeVeciZievs. Sate cideesivs4Pbalebvs August 02, 2001 eee:i.kteae.- Sale oeisia4.44r :December 13, 2002 gek amended.. (ml.) Mr ai ion of this certificate is p bisbthla by s 1455 or not racemi,y Q. 000, or opt rower, 29 I fl air, or both. PM Son 1110.3(10-4•I Paha l a s certificate soy he traiarare0 to scnrdsacs with OA 22.57. SDNY_GM_02759701 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246623 EFTA01331086 SDNY_OM_02759702 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246624 EFTA01331087 Banyan Air Service Avionics Division 1635 NW 51st Place Ft. Lauderdale, FL 33309 FAA APPROVED • AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR BOEING 727-100 WITH UNIVERSAL AVIONICS SYSTEMS CORPORATION DUAL MULTISENSOR UNS-ID+ FLIGHT MANAGEMENT SYSTEMS • REG IL N908TE SERIAL #. 20115 This supplement must be attached to the FM Approved Airplane Flight Manual when the Universal Avionics System Corporation UNS-1D+ Flight Manitgement System (FMS) is „installed in accordance with field approved 337 dated eV:: /la/ (21O(-)le . The information contained herein supplements or supersedes the basic manual only in those areas listed herein. For limitations, procedures, and performance information not contained in this supplement; consult the basic Airplane Flight Manual. FAA APPROVED Gary Justice Principal Avionics Inspector Federal Aviation Administration Flight Standards District Office #17 Ft. Lauderdale, FL 33315 Date: NOV 8 2004 Rev. 0 VFilige 1 of 9 SDNY_GM_02759703 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 002436625 EFTA01331088 4 Banyan Air Service Flight Manual Supplement Avionics Division UNS-1D+ FMS 1635 NW 51st Place N908JE BOEING 20115 Ft. Lauderdale, FL 33309 Table of Content' SECTION PAGE GENERAL 3 LIMITATIONS 3 EMERGENCY PROCEDURES 3 NORMAL PROCEDURES 3 PERFORMANCE 8 RECORD OF REVISIONS Revision Pages Description Approved 0 Ail Initlal Release . NOV 8 2001 Date: NOY 8 2004 Rev. 0 *Et: O. Page 2 of 9 SDNY GM_02759704 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246626 EFTA01331089 Banyan Air Service Flight Manual Supplement Avionics Division UNS-1D. FMS 1635 NW 51st Place N908JE BOEING 20115 Ft. Lauderdale, FL 33309 SECTION I - GENERAL 1. INSTALLATION DESCRIPTION. The Universal Avionics Systems Corporation dual FMS's use inputs from their integral GPS Receivers, Navigation Receivers and DME Transceivers to provide a blended position for navigation. Each FMS contains an Internal TSO C129a GPS sensor (GNSS 2400), which is cross-wired to the other FMS such that both systems have GPS 1 and GPS 2 data as inputs. The EMS's receive air data parameters from an Air Data Computer. A Data Transfer Unit (DTU100) is used to load periodic navigation data base updates via zip disks. The systems provide navigation and steering data to the flight director/autopilot system. Refer to the appropriate Operators Manuals as applicable. The FMS's contain software SCN 8021902 which provides capability for point-to-point navigation, as well as SIDs, STARs, holding patterns and GPS approaches. These SCN's comply with requirements of TSOs C115b and C129a Class Al when interfaced to the internal GPS sensors which are TSO C129a Class Al/B1/C1 certified The UNS- 1D+ FMS may contain either a GLONASS sensor or a GPS sensor, depending on hardware configuration. Lateral and Vertical deviations are provided for En Route, Terminal Area and Approach operations, including GPS overlay approaches. Approaches may be FCS coupled both laterally and vertically. Multi-Mission search patterns are available with SCN 902. 2. LATERAL NAVIGATION APPROVALS. Provided the FMS multi-sensor navigation system is receiving usable signals, it has been demonstrated capable of and has been shown to meet the accuracy specifications of: VER/IFR En Route domestic, Terminal and Instrument Approach (LOC, BC, GPS and GPS-overlay NDB, VOR, VOR-DME and RNAV) operations within the U.S.National Airspace System using the WGS-84 coordinate reference datum in accordance with the criteria of Advisory Circular AC 20-130A and AC 25-15. Satellite navigation data is based upon use of only the Global Positioning System (GPS) operated by the United States. Additionally, Russian GLONASS satellites provide increased accuracy but are not used for integrity or Receiver Autonomous Integrity Monitoring (RAIM) calculations or predictions. The dual FMS installation with dual internal GPS sensors, as installed, complies with the requirements of FM Notice 8110.60 for GPS primary means of Class II navigation in oceanic and remote airspace (including NAT MNPS in accordance with AC 120-33 and 91-49), when used in conjunction with the Universal Flight Planning Program, PN 10751 with SCN 24.0 or later FM approved version. This does not constitute an operational approval. Date: NOV 8 2004 Rev. 0 Page 3 of 9 SDNY_GM_02759705 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246627 EFTA01331090 Banyan Air Service Flight Manual Supplement Avionics Division UNS-1D+ FMS 1635 NW 51st Place N908JE BOEING 20115 Ft. Lauderdale, FL 33309 SECTION I — GENERAL (cont.) RNP- Approvals The dual multi-sentor FMS installation integrates dual GPS sensors and complies with equipage and accuracy requirements of FAA Order 8400.12A paragraph 12b(4), for operations in RNP-10 airspace. This does not constitute en operational approval. This installation also complies with equipage and accuracy requirements of AC 90- 96 paragraph 7b(1), 7d(3)(a) 2, 7d(3)(e) for BRNAV (RNP-5) when operating in Class I airspace, without time limits. The table details time limitations placed on RNP-10 and BRNAV operations with minimum sensors in NAV mode. Sensors RNP-10 Limitations RPN-5 (BRNAV) Limitations Available minimum dual FMS's required) (minimum single FMS required No time limitation when used in 1 GPS only N/A Conjunction with UFP VOR/DME only N/A No time limitation DME/DME only N/A No time limitation 3. VERTICAL NAVIGATION APPROVAL The dual Flight Management Systems, as installed, meet the requirements for VFR/IFR En Route, Terminal Area and Approach VNAV operations in accordance with the criteria of AC 20-129 and AC 90-97, paragraph 7.a (2). SECTION II — LIMITATIONS 1. The FMS Operator's Manual, Report Nos. 2423sv802/902 Dated 9/16/03 (or later revision) must be available to the flight crew whenever navigation is predicated upon the use of the Universal Avionics Flight Management System. 2. The system must utilize software version SCN 802/902.X, where X represents FAA approved minor changes. 4. IFR En Route and Terminal navigation are prohibited unless the pilot verifies the currency of the database or verifies each selected Waypoint for accuracy by reference to current approved data. Date: NOV 8 2004 Rev. 0 • Page 4 of 9 SDNY_GM_02759706 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246628 EFTA01331091 Banyan Air Service Flight Manual Supplement Avionics Division UNS-1D+ FMS 1635 NW 51st Place N908..IE BOEING 20115 Ft. Lauderdale. FL 33309 SECTION II - LIMITATIONS (cont) 4. Instrument approaches must be accomplished in accordance with approved instrument approach procedures that are retrieved from the FMS database. The FMS database must incorporate the current update cycle. a. Instrument approaches must be conducted in the Approach-mode, and GPS Integrity monitoring (when using GPS for approach guidance) must be available at the Final - Approach Fix, as indicated to the pilot by the 'GPS INTEG' amber annunciator being off. b. When an alternate airport is required by the applicable operating rules, it must be served by an approach based on other than GPS navigation, the aircraft must have.. operational equipment capable of using that navigation aid, and the required navigation aid must be operational. c. GPS can only be used for approach guidance if the reference coordinate datum system for the approach is WGS-84 or NAD 83. d. GPS will remain selected for all GPS approaches and any approach with a 'G" suffix to the approach identifier in the navigation database. GPS will be deselected for any pilot-defined VOR or VOR/DME' RNAV approaches. e. Pilot-defined IFR approaches must be defined using Waypoint coordinates from FMS's navigation data base. f. The FMS's are approved for pilot-defined VFR approaches as a VFR pilot aid only. NOTE: All sensors remain selected for VFR approaches. 5. When operating in other than oceanic and remote regions, the aircraft must have other approved navigation equipment installed and operating appropriate for the route of flight. 6. Displayed FMS navigation parameters are referenced to Magnetic North, and operation of the aircraft is limited to latitudes between N730 and 860o, unless magnetic variation is manually entered by the flight crew. 7. When using VNAV, the Altimeter on each pilot's panel must be used as the altitude reference for all operations. 8. ' Fuel display parameters are advisory only and do not replace primary fuel quantity or fuel flow gauges for fuel load and range planning. SECTION III - EMERGENCY PROCEDURES NO CHANGE TO AFM. 7 4 Date: NC V 8 2004 Rev. 0 Page 5 ors SDNY_GM_02759707 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246629 EFTA01331092 Banyan Alr Service Flight Manual Supplement Avionics Division UNS-1D+ FMS 1635 NW 51st Place N908JE BOEING 20115 Ft. Lauderdale, FL 33309 SECTION IIIA - ABNORMAL PROCEDURES 1. If 'GPS RAIM' becomes unavailable (as indicated by a Message and 'GPS INTEG' (amber annunciation), continue navigating using the GPS equipment or revert to an alternate means of navigation appropriate to the route and phase of flight, as necessary. When continuing to use GPS navigation, position should be verified every fifteen minutes using another IFR-approved navigation system. 2. Should an FMS system component fail, in most cases the CDU will go blank or the 'FMS MSG' light will flash. Depressing the MSG key will display the Message Page, which will indicate the component which has failed. 3. If sensor information is intermittent or lost, utilize remaining operational navigation equipment as required. 3. The FMS and associated components are protected by the following circuit breakers: C/B Name Amos Location Bus FMS No. 1 5 Pilot 28VDC Avionics Bus No. 1 (Triple-Fed) FMS No. 2 5 Copilot 28VDC Avionics Bus No. 2 (L GEN) FMS DTU 1 Pilot 28VDC Avionics Bus No. 1 (Triple-Fed) SECTION IV - NORMAL PROCEDURES 1. OPERATION Normal operating procedures are outlined in the FMS Operator's Manual, Report No. 2423sv802/902. 2. NAVIGATION DATABASE VERIFICATION. After power-on self tests have been completed, the INITIALIZATION page will appear. The term 'NAV DATABASE EXPIRES' followed by a date will be displayed. If the actual date is later than that which is displayed, the FMS will notify the pilot with a 'DATABASE EXPIRED'-message. Refer to the Operator's Manual for navigation database update instructions. 3. SYSTEM ANNUNCIATORS Each FMS has the following annunciations presented on the Universal Electronic Flight Instrument (EFI) displays (refer to the EFI Operator's Manual, as applicable) : MSG Illuminates and flashes in conjunction with the CDU to indicate a message is to be acknowledged on the MESSAGE page. SXTK Illuminates to indicate that selected crosstrack is active. FHDG Illuminates to indicate that the FMS is in Heading sub-mode. APPR Illuminates to indicate that an Approach has been activated. GPS INTEG Illuminates to indicate GPS Integrity is outside of the allowable limit for phase of flight (2.0nm En Route, 1.0 nm Terminal and Approach transition, and 0.3 nm Final Approach segment). Date: NOV 8 2004 Rev. 0 Page 6 of 9 SDNY_GM_02759708 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246630 EFTA01331093 Banyan Air Service Flight Manual Supplement Avionics Division UNS-1D+ FMS 1635 NW 51st Place N908JE BOEING 20115 Ft. Lauderdale, FL 33309 SECTION IV - NORMAL PROCEDURES (cont) 4. AIRCRAFT INTEGRATION a. Universal Avionics EFI display of FMS information 1) FMS information is displayed on the Universal Electronic Flight Instrument (ER) displays. The associated EFI Control Panel provides control of each display. See the appropriate Operator's Manual, as applicable, for each EFI display system. 2) Lateral deviation display scaling meets with requirements of TSO C129a and AC 20-130A (5.0 nm full scale for En Route, 1.0 nm for Terminal operations, and 0.3 nm for Approach operations). 3) b. En Route and Terminal Area Flight Control System Operation 1) With 'FMS'-mode selected by using the EFI Control Panel, the respective FMS information can be presented as Flight Director steering commands by pressing the [NAV] button of the FCP-65 Flight Control Panel. 2) With reasonable navigation data being displayed, the steering information can be Autopilot-coupled, to the pilot's or copilot's Flight Director system, by pressing the 'AP ENGAGE' - button on the APP-65A Autopilot Control Panel. c. Approach Operations NOTE: ILS approaches can be retrieved from the Jeppesen database and linked to the flight plan, but cannot be armed or activated as FMS approaches. The FMS can be used to provide navigation up to the final approach course, at which point the EFI must be changed to display raw ILS data which can be coupled to the Flight Control System (FCS). NOTE: GPS will remain selected for GPS and CPS-overlay approved approaches from the navigation database, as well as pilot-defined VFR approaches. Refer to Operator's Manual, Section V, Approach Procedures. Date: NOV 8 2000 Rev. 0 ):11Y, Page 7 of 9 SDNY GM 02759709 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024663 I EFTA01331094 Banyan Air Service Flight Manual Supplement Avionics Division UNS-1D+ FMS 1635 NW 51st Place N908JE BOEING 20115 Ft. Lauderdale, FL 33309 SECTION IV - NORMAL PROCEDURES (cont) c. Approach Operations (cont.) LOC, I3/C, GPS, NDB, RNAV, VOR, VOR/DME, and VFR approaches may be linked into the flight plan and then laterally and vertically coupled to the FCS as follows: 1) Approach Transition: When an entire approach transition (e.g., procedure turn, DME arc, etc.) is to be flown, first arm the approach on the FMS (ARM APPR). If the FMS is not armed manually it will arm automatically at 30nm from the airport. With the desired DIRECT TO or FROM/TO Waypoints selected, or the desired FMS Heading selected with INTERCEPT ACTIVE, select FCS 'NAY- mode by pressing the [NAV] button of the appropriate FCP-65 Flight Control Panel. When the FMS . has automatically activated the approach, denoted by the 'APPR' annunciator displayed in the associated EFI display, press the [APPR) button of the Flight Control Panel. When the FCS has captured the "APPR" — mode, a white "VNAV" will appear on the PFD and a white VN on the ADI signifying the 'arming' of the VNAV mode. The "VNAV- and 'VN" annunciation will turn to green in color when the FCS has captured the VNAV glideslope. See the EFI operator's manual for specific display annunciations. Continue monitoring both lateral and vertical deviations throughout the duration of the approach. If required, initiate 'Missed Approach Procedures' as described in the Universal Avionics Operator's Manual. 2) Heading Vectors: If given heading vectors by ATC to the final approach course, manually activate the approach on FMS NAV page 1/3. The FMS will enter the 'FHDG" mode, the EFI display will now display final approach course data, and the INTERCEPT prompt on Nav page 1/3 will be active. When cleared to intercept final, press the INTERCEPT line select key to intercept final. Ensure that commanded heading mode is canceled. Select [APPR) on the FCS Flight Control Panel to capture and track the final approachlateral and vertical information. NOTE: Guidance is provided to the runway threshold or missed approach point. It is the pilot's responsibility to level out at MDA if the runway environment is not in sight. Date: NOV 8 2004 Rev. 0 • Page 8 of 9 SDNY_GM_02759710 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246632 EFTA01331095 Banyan Air Service Flight Manual Supplement Avionics Division UNS-1D+ FMS 1635 NW 51st Place N908JE BOEING 20115 Ft. Lauderdale. FL 33309 SECTION IV - NORMAL PROCEDURES (cont) 3) Press the APP-65A Autopilot Control Panel [AP ENG]-button to couple the AP to the selected FD. The Autopilot will track pseudo-Localizer and pseudo-Glidesbpe signals from the FMS. b. Advanced Approach Operations 1) Advanced approaches may be identified in the data base by the prefix "A° to the approach listed in the 'ARRIVAL' page and in the navigation data base They are characterized by course changes on the final approach segment of greater than 6 degrees and/or having multiple flight path angles. To avoid excessive deviations from course and flight path, these approaches may need to be flown in FCS [NAV) mode until on the final leg of the approach. Select FCS (APPR] sequencing the final waypoint to engage vertically. c. Vertical Navigation 1) Vertical Navigation (VNAV) information is displayed on the EFI display and is available for enroute, terminal or approach descents. Pitch steering commands for enroute and terminal VNAV operations are not provided to the Flight Control System. SECTION V - PERFORMANCE DATA NO CHANGE TO AFM. Date: NOV 8 2004 Rev. 0 Rage 9 of 9 SONY_GM_02759711 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246633 EFTA01331096 coos SDNY_GM_02759712 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246634 EFTA01331097 . Form Approved C OMB No. 2120-0020 For FAA Use Only US Department MAJOR REPAIR AND ALTERATION Office Identificabon Ot Transportation Anon (Airframe, Powerplant, Propeller, or Appliance) kelaton AOrrinistration INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B. and AC43.9-1 (or subsequent evision thereof) for instructions and ...a i disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can resutt in a civil penally not to exceed 51.000 for each such. violation (Section 901 Federal Aviation Act of 1958} 1 Make Model - 71 : 11. Alreraft Boeing 727-100 Serial No. Nationality and Registration Mark 20115 USA N908JE i i2. Owner Name (As shown on registration certificate) Address (as Mown on registration certificate) .. J.E.G.E. Inc. 103 Foulk Road STE 202 Wfirringlon, DE. 19803-3742 3. For FAA Use Only Tr, data denoted rsortilints racluirement• desentood real subfoct il.x...24 tz, =Say lt: iM bf • person wrerizea tr. FAR C. al. OCT I 9 7004 ,A, , 5° - Fs Do-17 Os ggMsnFMbUQS I 4. Unit Identify atb 5. Type Alteration 1 Unit Make Model Serial No. Repak . ?, AIRFRAME '"•"--'---(As described in Item 1 above)^•^•^---^rrear *"si POWERPLANT .i ffPROPELLER r Type •• APPLIANCE Manufacturer 8. Conformity Statement A. Agency's Name and Address B. Kind of AgenCY C. Certificate No. BANYAN AIR SERVICE u S Certificated Mechanic SD4R514M AVIONICS DIVISION Foreign Certificatedmechanic Ftadio Class 1,2,3 1635 NW 51st Place ra Certificated Repair Station Limited Airframe Ft. Lauderdale, FL 33309 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 cdnY knoMedge. ' Date ty,) ; a vg . se ,..200 %zr Signature of A=arral 6,2 zado, _ , . frf die .A. 'r-- Steve Gluellette• . 7. Approval for Return to Sera* • 'pursuant to the authority given persorts specified below, the unit identified in item 4 was Inspected in the manner prescribed by the Administrator or to& Federal Aviation Administration and is APPROVED O REJECTED FAA Fit. Standards Manufacturer Inspection Authorization Other (Specify) ..t- :Ety Inspector FAA Designee X Repair Stadal Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection Certificate or Signature of Au UI ' I a ct / • Designation No. /9 AA4,041/1"X. SD4R314M Stave Ousileili FAA Form 337 (124e) SDNY_GM_02759713 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246635 EFTA01331098 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be ...,ompatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. I ra. Description of Work Accomplished idmore space ls required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed) 1 The purpose of this 337 is for the work performed on N908JE undo Banyan Air Service, Avionics • Division work order #68062. A. Installed an Artex ELT406-2Hivl per Artex installation document number 570.5000, Rev. A, dated 12/10/02 mounted in unpressurized aft compartment. The antenna is mounted in the aft tail section. A remote switch is mounted in cockpit in the copilot's insrtument panel. An aural activation monitor is mount within the vacinity of the ELT per the installation document listed above. B. The above installation WaikkiredinIceordancemith AC43.13-1B, Chapter 7, sections 1-5, AC43.13-1B Chapter 11, sections 3-17, AC43.13:2A Chapter 1, AC43.13-2A Chapter 2, paragraphs 24, 25, an—d78;76-C43:T3,-2ATChapter 3;paragraph 38 and the aircraft's maintenance manual. C. A functional test of the above equipment has been performed FAR25.1309 and FAR25 .1431 for proper operation and did not adversely affect any other aircraft systems. An electrical load analysis was conducted and it was confirmed that this installation would not exceed 80% of the generator output. D. A log book entry and equipment list was generated to reflect the above installation. No Weight and balance was generated as the aircraft was weighed. E. Instructions for continued airworthiness is a battery due time change. This due date is reflected on the log book entry. Annual inspection is required per FAR 91-207 (d). END • 0 Additional Sheets am Attached SDNY_GM_02759714 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246636 EFTA01331099 a us Drotirtintira Form Approved OMB No. 2120-0020 For FAA Use Only or Trareportran MAJOR REPAIR AND ALTERATION office Idenb5cabon Fedani (Airframe, Powerplant, Propeller, or Appliance) Artiftil Aterdnisinakm . INSTRUCTIONS: Print or type al entries. See FAR 43.9, FAR 43 Appendix B. and AC43.9-1 (or subsequent °vision thereof) for instructions and ;disposition of this tone. This report S required by law (49 U.S.C. 1421). Failure to report can result Ma civil penalty not to exceed 51.000 for each such. iiridation (Section 901 Federal Aviation Act of 1958). Make Model it. Aircraft Boeing 727-100 Serial No. Nationality and RegStration Mark ii 20155 USA N9081E • 2. Owner Name (As shown on legislation certificate) Address (as shown on ripiStration certificate) • J.E.G.E. Inc. 103 Fouls Road, Ste 202 ' Wilmington. OE. 19803-3742 3. For FAA Use Only Tn-, data elcnbatil canoes the Waage° at mammas is for the Move described Octet corionnity by • elniOn iri FAR 4.1, 43.T NO0uthar2004 -r-svo-f 7 Mee 4. Unit IdentifIcatc 5 Type AllareUdl Unit Make Model Serial No. Rep* .' 'AIRFRAME (As described In Item 1 above CI . . POWERPLANT i PROPELLER Type APPLIANCE Manufacturer t Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. BANYAN AIR SERVICE U.S. Certificated Mechanic SOIR514M AVIONICS DIVISION Foreign Certificated Mechanic Radio Class 1,2.3 1635 NW 51st Place 0 Certificated Repair Station Limited Aidrame Ft. Lauderdale, FL 33309 Manufacturer 0.1certify that the repair and/or alteration made to the unit(s) identified in tern 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 knowtedge. Date Signature of rodi I .44.05.466-4 ,,,,74/09- c..._ Steve Ouellette 7. Approval for Return to Service Pursuant to the authority given persons s below, the unit Identified in Item 4 was inspected in the manner prescribed by the Administrator of the Feder I Aviation Administration and is APPROVED Q REJECTED FAA Flt. Standards Manufacturer Inspection Authorization Other (Specify) BY inspector FAA Designee Repair Station Person Approved by Transport Canada Ainvorthiness Group X Date cf Approval cc Rejection Certificate or Signature of Authorized Indi ' ual Designation No. /9 j (4gs , see e e.- 2 2, / SD4R514M Steve Ouellette FAA Fenn 337 (12-88) SDNY_GM_02759715 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246637 EFTA01331100 NOTICE Weight and balance or operating limitation changes shell be entered in the appropriate aircraft record. An alteration must be compatible with allprevious alterations to assure continued conformity with the applicable airworthiness requirements. 0. Description of Work Accomplished almore space is required, attach additional sheets. ideMily with aircraft nationality and registration mark and dale work completed) The purpose of this 337 is for the FAA approval of the new flight manual supplement on N908JE under Banyan Air Servive, Avionics Division work order #68062. A. Removed existing UNS-1D Flight Management System (FMS) control display/computer units and routed to the manufacture for upgrade to UNS-1D+. Reinstalled UNS-1D+ FMS CDU computers. System ground checked good. B. A flight manual supplement has been generated, approved and incorportated into the existing flight manual. A weight & balance and equipment list update are not required. END PIP .z. vum 44.3 akcpc,A i.S70 O Additional Sheets are Attached I SDNY_GM_02759716 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246638 EFTA01331101 NOV. 8.2004 9:50AM PYKA AEROSPACE NO. 2146 P. 3 Doc. No. 7280-FM-001, Rev A TAWS System Issue 092401 AFM Supplement for S.I.P. Technical Services Inc. Boeing 727-100 10107 McAllister Freeway San Antonio, TX 78216 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT UNIVERSAL AVIONICS TERRAIN AWARENESS WARNING SYSTEM (TAWS) AIRPLANE MAKE: BOEING AIRPLANE MODEL: 727-100 AIRPLANE SERIAL NO.: /1/7013—C REGISTRATION NO.: (-90 //6" This supplement must be attached to the FAA Approved Airplane Flight Manual when the airplane is modified by the installation of a Universal Avionics Terrain Awareness Warning System (TAWS) in accordance with FAA STC number ST09951SC. The information contained herein supplements or supersedes the basic Airplane Flight Manual only in those areas listed herein. For limitations, procedures, and performance information not contained in this document, consult the basic Airplane Flight Manuel APPROVED: 1--f-1,/gern yR S. Frances Cox, Manager Special Certification Office Federal Aviation Administration Ft. Worth, Texas 76193-0190 DATE October 25, 2004 Page 1 of 9 SDNY_GM_02759717 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246639 EFTA01331102 SDNY_GM_02759718 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246640 EFTA01331103 NOV. 14 4 Doc. No. 7280-FM-001, Rev A TAWS System Issue 092401 AFM Supplement for Si.?. Technical Services Inc Boeing 727.100 10107 McAllister Freeway San Antonio, pc 76216 LOG OF REVISIONS REv, DESCRIPTION REVISED PAGES APPRD. By DATE IR New supplement All S. Frances Cox 12-13-2002 Allow use of CDU or MFD A display. Format and editorial All See cover page 10.25.2004 corrections throughout. FAA APPROVED Date: October 25, 2004 Page 2 of 9 SDNY_GM_02759719 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024664I EFTA01331104 SDNY_GM_02759720 i SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246642 EFTA01331105 NOV. 8. t 4 9: 1A/1, 'YKA A A NI. i4 Doc. No. 7280-FM-001, Rev A TAWS System Issue 092401 AFM Supplement for S.I.P. Technical Services Inc. Boeing 727-100 10107 McAllister Freeway San Antonio, TX 78216 TABLE OF CONTENTS SECTION PAGE SECTION I - GENERAL 4 SECTION II - LIMITATIONS 4 SECTION III — NORMAL PROCEDURES 5 1. Operation 2. Cold Temperature Operations 5 3. Systems Test S 4. Pop-Up Terrain Display 6 5. System Anntmciators 7 SECTION IV — EMERGENCY/ABNORMAL PROCEDURES 9 EMERGENCY PROCEDURES 9 ABNORMAL PROCEDURES 9 1. Circuit Breakers 9 2. Use of TERR INHIBIT switch 9 3. Response to TAWS Warnings 9 4. Response to Glideslope Deviation Alerts 9 5. Use of Flap Override Switch 10 SECTION V - PERFORMANCE 10 SECTION VI - WEIGHT AM) BALANCE 10 FAA APPROVED Date: October 25, 2004 Page 3 of 9 SDNY_GM_02759721 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFFA_00246643 EFTA01331106 SDNY_GM_02759722 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246644 EFTA01331107 MK 8.2004 0:514.M PYKA AEROSPACE h0. 2146 6 Doe. No. 7280-FM-001, Rev A TAWS System Issue 092401 AFM Supplement for S.I.P. Technical Services Inc. Boeing 727-100 10107 McAllister Freeway San Antonio, TX 78216 SECTION - GENERAL This Supplement provides general information for the Enhanced Ground Proximity Warning System installation. The aircraft is equipped with a Universal Avionics TAWS system. The system uses inputs from the air data computer No. 1, navigation receiver No. 1, radio altimeter, and the Universal Avionics UNS-1 Flight Management System (FMS) , and an internal terrain database to provide basic GPWS alerts and terrain alerts The TAWS alerts provide the crew with aural and visual indications of possible inadvertent flight into terrain. TAWS alerts are generated if one or a combination of the airplane's: 1) vertical speed, 2) rate of closure to terrain, 3) accumulated altitude loss, 4) airspeed, flap and /or gear configurations or 5) glideslope deviation is unsafe given the airplane's radar altitude and phase of flight. Terrain alerts are generated by comparing aircraft position and altitude to the EGPWS terrain database. This system also provides "Flight Plan Look Ahead" terrain alerts and warnings by comparing the FMS flight plan to the terrain database SECTION II — LIMITATIONS The TAWS display will be used for situational awareness only. Navigation must not be predicated upon the use of the TAWS. The 3-D view provides no amuck information. To avoid giving unwanted terrain alerts, the TAWS terrain alerts must be inhibited by pressing the TERR INHIEI switch when landing at airports that are not included in the airport database or when landing at an airport other than the airport in the FMS flight plan. Deviation from Aix Traffic Control Clearances is authorized to the extent necessary to comply with TAWS warning. The use of terrain awareness warning and terrain display function is prohibited during QFE operations. The current local altimeter setting must be entered in the pilot's altimeter for proper terrain alerting. The TAWS database and alerting algorithms do not account for man made obstructions FAA APPROVED Date: October 25, 2004 Page 4 of 9 SDNY_GM_02759723 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246645 EFTA01331108 SDNY_GM_02759724 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246646 EFTA01331109 NOY. 8.2004 3'514M PYKA AEROSPACE NO. 21 4 6 Doc. No. 7280-FM-001, Rev A TAWS System Issue 092401 AFM Supplement for S.I.P. Technical Services Inc. Boeing 727-100 10107 McAllister Freeway San Antonio, TX 78216 SECTION III — NORMAL PROCEDURES I. Operation All aircraft crew interface is conducted through the Universal Avionics display, either multi- function display (MFD) or FMS control display unit (CD11), end system annunciator switches. TAWS terrain information may be presented on either an MTID or a CDU. The TAWS requires inputs from the following systems, radio altimeter, air data computer, VHF navigation receiver, FMS, gear position and flap position. 2. Cold Temperature Operations TAWS uses baro-corrected altitude as the reference for Fonvansd Looking Terrain Alerts (FLTA). TAWS does NOT compensate the baro altitude input for non-standard temperature lapse rates that may be encountered in extreme cold conditions, causing degraded FLTA operation. Basic ground proximity warning modes (1 through 6), as well as Premature Descent Alen (PDA), are radio altitude based and not affected. In extreme cold conditions, the aircraft will be operating at a lower altitude than indicated, thus resulting in TAWS alerts being delayed or missing. The color -banding on the TAWS display will be offset by the cold temperature altitude error. When operating into and out of airports where cold temperatures exist, the aew should be aware of the difference between the indicated baro altitude and the true altitude and the effect this has on FLTA and the terrain display. To determine the effect on FLTA warnings consult the Airman's information Manual Chapter 7 paragraphs 7.2.3d and 7-2-3e. 3. System Tests BUILT IN TEST TAWS has a Built-In-Test (BIT) function which includes Power-Up Self Tests, Initiated Tests and Continuous Tests. Where there has been degradation in capabilities that result in TAWS being unavailable, BIT annunciates the fact to the flight crew via a GPWS FAR. or TERR MOP Lamp. PRE-FLIGHT TESTS A TAWS Self Test should be conducted prior to each flight. Momentarily press the GPWS TEST annunciator. The following indications confirm proper TAWS operation: PULL-UP Annunciator Illuminated TERR Annunciator ➢luminated BELOW G/S Annunciator ➢luminated G/S INHIBIT Annunciator Illuminated TERR INHIBIT Annunciator Illuminated FAA APPROVED Date: October 25, 2004 Page 5 of 9 SDNY_GM_02759725 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246647 EFTA01331110 SDNY_GM_02759726 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246648 EFTA01331111 • NO.2146 P. 8 PYKA AEROSih.E hil4. 4.2404 TAWS System Doc. No. 7280-1 (it , Rev A AFM Supplement for Issue 092401 Boeing 727-100 S.I.P. Technical Services Inc. 10107 McAllister Freeway San Antonio, TX 78216 S iCcatinuedi SECTION IIT — NORMAL PROCEDURE GPWS FAIL Annunciator illuminated GPWS TFST Annunciator Illuminated TAWS Terrain Display Test Image (Colored Bars) Awe! Amtunciarions "TERRAIN, TERRAIN" "PULL UP, PULL UP" "DON'T SThlE" "SINK RATE" "GUDESLOPE" "TOO LOW TERRAIN" "TOO LOW GEAR" "TOO LOW FLAPS" "ME HUNDRED" TERR ot During this time the Greys FAIL and Once the test is complete, TAWS will rebo gene rated on the MFD a TAWS FAIL message will be INOP annunciators will remain lit and one min) until the system is operational. (approx T annunciator again within five NOTE: As a result of pressing the GPWS TES l and the TAWS computer will seconds of initiating this test, the test will cana continue to operate without rebooting. 4. Pop-Up Terrain Display MFD or the TAWS display will "pop-up" on the In the event of terrain alert, the map view of t to the ay will remove the pop-up and rever CD1J. Pressing any function key on the displ selected display function. a star shaped Terrain Threat Symbol. Both Prospective terrain conflicts are depicted by flashing red with this symbol. Terrain warnings are a Warnings and Cautions are annunciate(' threats along by a flashing yellow symbol. Terrain symbol while Terrain cautions are depicted of conflict e ol and represent the predicted first point the flight plan are depicted by a whit symb between the flight plan and terrain ay indicate a Terrain Alert (30-second wanting). RED threat "stars" on the TAWS displ ing). S ay indicate a Terrain Caution(60-second wan YELLOW threat "stars" on the TAW displ FAA APPROVED Page 6 of 9 Date: October 25, 2004 GRAPHS 7, 8, 91 10 1 SUBJECT TO PROTECTIVE ORDER PARA d 17 an9727 15,0275 SONY_GkL EFTA_00246640 EFTA01331112 sj SDNYGM02759728 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246650 EFTA01331113 NOV. 8.2004 9:52AM PYKA AEROSPACE ti0 2146— P. 9 Doc. No. 7280-FM-001, Rev A TAWS System Issue 092401 AFM Supplement for S.I.P. Technical Services Inc Boeing 727.100 10107 McAllister Freeway San Antonio, TX 78216 sEall)N III - NORMAL PROCEDURES1Coneina edi WHITE advisory alert " stars" on the TAWS display indicate a flight plan terrain conflict. These alerts are annunciated by a "star" on the display shortly after a VNAV altitude is entered into the flight plan or when a procedure (STAR or approach) containing altitudes is linked to the flight plan Flight plan terrain advisories do not require immediate action but indicate that adhering to the flight plan as entered will cause a future terrain alert. Waypoints and altitudes should be checked for accuracy. 5. System Annunciators The following system annunciators are provided for the system; A. PULL UP Red PULL UP annunciators are located on the Captain's and First Officer's instrument panel. This annunciator illuminates whenever TAWS has detected terrain in the aircraft's immediate flight path The annunciator will remain illuminated until the terrain has been cleared. Aural annunciations of "TERRAIN, TERRAIN, PULL UP" or "PULL UP, PULL UP" are also provided whenever the red PULL UP annunciator illuminates. B. BELOW GS Amber BELOW GS annunciators are located on the Captain's and First Officer's instrument panel. This armtmciator illuminates on approach whenever the TAWS has detected that the aircraft is at least 1.3 dots below the glideslope. This annunciator remains illuminated until the aircraft has returned to within less than one dot of the glideslope. Aural warnings of "GLIDESLOPE-GLIDESLOPE-GLIDESLOPE" sound until the aircraft has returned to within less than one dot below the glidepath The aural annunciation may be canceled by pressing the BELOW GS anntraciator/switch. However, the BELOW GS annunciators will remain illuminated. If the aircraft goes below the glideslope after the aural warning and light annunciation has gone out, the light and aural warning will again sound. C. GPWS FAIL Amber GPWS FAIL annunciators are located on the Captain's and First Officer's instrument panel. This annunciator illuminates if the TAWS has failed. FAA APPROVED Date: October 25, 2004 Page 7 of 9 SONY GM_02759729 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFM_00246651 EFTA01331114 SDNY_GM_02759730 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246652 EFTA01331115 NOV. 8.2004 9:53AM PYKA AEROSPACE NO. 2146 P. 10 Doc. No. 7280-FM-001, Rev A TAWS System Issue 092401 AFM Supplement for S.I.P. Technical Services Inc. Boeing 727-100 10107 McAllister Freeway San Antonio, TX 78216 SECTIONH7 - NORMAL PROCEDURESiContinuedi D. GPWS TEST GPWS TEST switches are located on the Captain's and First Officer's instrument panel shared with the GPWS FAIL annunciator. This switch is utilized to perform a self-test of the TAWS system. E. TERR Amber TERR annunciators are located on the Captain's and First Officer's instrument panel. The "TERRAIN, TERRAIN" aural warning paired with a visual alert is indication of reduced terrain clearance. F. TERR INOP Amber TERR LNOP annunciators are located on the Captain's and First Officer's instrument panel. This annunciator illuminates when the terrain function is inhibited by TERR INHIB switch, terrain datah.lte is invalid or failed, terrain alert function is inoperative due to hardware failure or lack of a required input such as position or altitude. G. TERR LNILIB Blue TERR INHIB annunciator/switch is located on the Captain's instrument panel adjacent to the TERR INOP annunicator. This annunciator/switch is illuminated white visible only when the TERR INHIB is active. FAA APPROVED Date: October 25, 2004 Page 8 of 9 SDNY_GM_02759731 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246653 EFTA01331116 SDNY_GM_02759732 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246654 EFTA01331117 NOv. 8.2004 9:530. PYKA AEROSPACE NO. 2146—P. 11 Doc. No. 7280-FM-001, Rev A TAWS System Issue 092401 AFM Supplement for S.1.P. Technical Services Inc. Boeing 727-100 10107 McAllister Freeway San Antonio, TX 78216 SECTION IV -EMERGENCY/ABNORMAL PROCEDURES EMERGENCY PROCEDURES No change to basic Airplane Flight Manual ABNORMAL PROCEDURES 1. Circuit Breakers The TAWS system is protected by the following trip-free circuit breakers: NAME JACATION AMPS BUS GPWS P-18 5 28 VDC Ess. 2. Use of TERR INB1B switch. The Terrain Awareness Display inhibit switch (TERR WHIR) must be placed in the INHIB position in the following conditions: 1-Whenever the FMS in the Dead Reckoning (DR) mode 2-Within 15 nrn of approach or landing at an airport not contained in the TAWS database. NOTE: When an off airport landing is required the FLTA and PDA functions should be inhibited by activation of the TEAR INHIB switch. 3. Response to TAWS Warnings When an aural 'TERRAIN, TERRAIN, PULL UP" or a red PULL UP warning light annunciates, execute a positive pull up maneuver, apply maximum rated thrust, and ascend to at least the best climb angle until the warning ceases. Notify ATC if action requires deviation of ATC cleared flight plan. When an aural "CAUTION TERRAIN", "TOO LOW TERRAIN," "SINICRATE" "DONT SINK," "'TOO LOW FLAPS" or 'TOO LOW GEAR" caution annunciates, initiate corrective action to remove the cause of the warning. 4. Response to Glideslope Deviation Alerts When the BELOW GS annunciator illuminates and an aural "GLIDESLOPE" annunciation alert occurs, initiate corrective action to fly the airplane back to the glideslope centerline. To inhibit the "GLIDESLOPE" annunciation on back course approaches, select the BELOW GS warning light/switch. The glideslope inhibit function is only available below 2000 ft AOL when the BELOW GS annunciator illuminates. FAA APPROVED Date: October 25, 2004 Page 9 of 9 SDNYGPA02759733 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246655 EFTA01331118 SDNY_GM_02759734 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246656 EFTA01331119 NOV. 8. 2004 9:530 FYKA AF.;O5:1 ACi. NC. [ <16 12 Doc. No. 728O-FM-OO1, Rev A TAWS System Issue O924O1 AFM Supplement for S.I.F. Technical Services Inc. 10107 McAllister Freeway Boeing 727-1OO San Antonio, TX 78216 SECTION IV — EMERGENCY/ABNORMAL PROCEDURES (Continued) 5. Use of Flap Override Switch When landing with less than normal flaps, the FLAP OVERRIDE switch should be usesd to prevent the `TOO LOW FLAPS" turn] annunciation. SECTION V - PERFORMANCE No change to basic Airplane Flight Manual. SECTION VT - WEIGHT AND BALANCE Refer to applicable weight and balance document. FAA APPROVED Date: October 25, 2OO4 Page 10 of 9 SDNY_GM_02759735 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246657 EFTA01331120 SDNY GM 02759736 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246658 EFTA01331121 Form Approved 0 MAJOR REPAIR AND ALTERATION OMB No. 2120-0020 al instsatiktn (Airframe, Powerplant, Propeller, or Appliance) For FAA Use Only resew emo Office Identification AtImbilllmtrallOn .51, -r-spc, - /7 INSTRUCTIONS: Rim or type all entries. See FAR 43.9 Appendix B, and AC 419-1 (or subsequent revision thereof) tor' 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 81.000for each such violation (Section 901 Federal Aviation Act of 1958). Make Model BOEING 727.31 1. Aircraft Serial No. Nationality and Registration Mark 20115 U.S.A. N908.1E Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner JEGE INC 103 FOULK RD STE 202 WILMINGTON DE 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type UM Make Model Serial No. Repair Alteration AIRFRAME As described in Item 1 above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6. Conformity Statement A Agency& Name and Address B. Kmd of Agency C. Certificate No. U.S. Certified Mechanic CRS EYKR782D JET AVIATION ASSOCIATES LTD. Foreign Certified Mechanic AIRFRAME 1,3. 1515 PERIMETER RD. T c i Certificated Repair Station RADIO 1,2,3. WEST PALM BEACH. FL 33406 Manufacturer LIMITED A/F &ENG D. I certify that the repair and/or alteration made to the unh( ) idenfilied in item 4 above and on 11! reverse A \attachments hereto have been made in accordance with the requirements of Pan 43 of tine e U.S. Federal Aviation ' and that information furnished herein is (rue and correct to the best of my knotiledge. Date Signature of Authorized Individual 1 6/12/02 Christoptia Hoeseuorth Inspector. , . \ 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit dentilied in item 4 was inst3ected m the bY6 Admini trator of the Federal Aviation Administration and is 0 APPROVED 0 REJECTED Other (Spear) FAA R. Standards Manufacturer Inspection Authorization Inspector BY Person Approved by Transport FAA Designee X Repair Station Canada Airworthiness Group Date of Approval or Refection Certificate or Signature of Authorized Individual 6/12/02 Designation No. EYKR782D John K. Urso. Inspector., -: -;l" k L us` I ' ' 6 FAA Form 337 risen / SDNY_GM_02759737 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246659 EFTA01331122 rr NOTICE Weight andbalance or operating lirritation donor* shall be entered in the appropriate aircraft record. An alteration must be soaped :de with allprevious alterations to assure continued conformity wIth the applicable altwortNness requirements. 8. Description of Work Accomplished (If more space Is required. attach additional sheers, Identify with aircraft nationality and registratim mark and date work accomplished) N9081E. BOEING 727-31, S/N 20115. W.O. 18046 REFERENCE F.A.A. FORM 337 DATED 7/2A)1 INSTALLING A UNIVERSAL AVIONICS CORP. UNS-I 19 FLIGHT MANAGEMENT SYSTEMS (FMS) WITH INTEGRAL GPS SENSORS. RECONFIGURED AIRCRAFT WIRING TO PROVIDE V-NAV DISPLAY INFORMATION ONLY. FROM THE EXISTING a 1 AND it 2 UNS-ID FLIGHT MANAGEMENT SYSTEMS. MS MODIFICATION AS ACCOMPLISHED PER THE FOLLOWING JET AVIATION DRAWINGS. WHICH ARE SUBSTANTIATED BY FAA FROM 8110-3 RESPECTIVELY: WIRING DRAWINGS. • BM-16236-410, REV A. DATEDawe SHEETS I THRU 5. TITLED - NO. I FLIGHT MANAGEMENT SYSTEM. • B727-16236.411. REV A, DATED/1/16/0Z SHEETS I THEW 5.1TfLED - NO. 2 FLIGHT MANAGEMENT SYSTEM. REFERENCE F.A.A. FORM 8110-3 DATED 4/19/02 BY SYSTEMS AND EQUIPMENT DER NO. DERT510087-NM. ACCOMPLISHED OPERATIONAL CHECKS PER UNIVERSAL AVIONICS CORP. RETURN TO SERVICE MAINTENANCE AND CHECKOUT PROCEDURES MANUAL NO. 34-60-21. DATED 19 MARCH 200) writ NO DISCREPANCIES NOTED. AN EMI TEST. REPORT NO.: 8727.16236-080 REV IR. SHEETS I OF 5. DATED 06/19/2001. WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY CANER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.13- I II, CHAPTER 12. SECTION 3, PARAGRAPH 12- 37 AND AC 43.I3-2A. CHAPTER 2 PARAGRAPH 23f. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER FAR. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE REQUIRED F.A.A. APPROVED FLIGHT MANUAL SUPPLEMENT DOC NUMBER B727-16236100, REV A. SHEETS 1 THRU 9. DATED 5/8/02 HAS BEEN INSERTED INTO THE AIRCRAFT FLIGHT MANUAL END ❑ Additional Sheets Are Attached * U.S. G.P.O 1990-761-753 SDNY_GM_02759738 - SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246660 EFTA01331123 Apr -19-02 08:08A N 3 Curran 352 243 1011 P . 02 DEPARTMENT OF 11LAREP0RTAT ION FEDERAL AVIATION ADMDFISTRATI0N DATE STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS Apri119, 2002 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane. Radio. NA:copier. <IC) NAMEOF APPLICANT Jet Aviation Associates Boeing 727-31 Airplane West Palm Beach, FL UST OF DATA IDENTIFICATION TITLE 8727.16236410, Revision A, dated NO. 1 FLIGHT MANAGEMENT SYSTEM April 16, 2002 0727.16236.411, Revision A. dated NO. 2 FLIGHT MANAGEMENT SYSTEM April 16, 2002 PURPOSE OF DATA in support of major alteration to Boeing 727-31. serial number 20115, registration number N9OSJE. APPLICABLE REQUIREMENTS (List specific sections) CFR TITLE 14. CHAPTER 1, SUBCHAPTER C FAR 25.681 (a)(b)(1) FAR 26.1329 (h) FAR 25.1529 FAR 25.869 (a)(4) FAR 25.1351 (a) FAR 25.1581 (a)(b)(d) FAR 25.1301 (a)(b)(c)(d) FAR 25.1367 (a)(c)(d)(e) FAR 25.1309 (a)(b)(c)(d)(e)(g) FAR 26.1381 (a)(b) FAR 26.1322 (b)(c) FAR 25.1431 (aKb)(c) CERTIFICATION - u..........rn ........ st feecciWe dd. A4LE.L.ARRER4 inconte...eD ...s• L no I...RR. RE oflacasto ...D.P." Me( 41. Fete A..... 141.4 .••••• tia WM ant ad co sinthed YIN enacted NOM In. bin ma'am' is monism. Rub alablitbed procedens obiCowed ft amply' nii animal. retektanet day rs., Afloat. KflaaAn 0 Rwomtnegid appnwsl .thew dem I W) Therefore ILI Appnn that data (Spleen & Eq.Ipmat REPK0'. DaliK APPreval thily. Dom NM COMOIDR lesiollAtios Appretsh tiGNAT1nt 'MGM CO EI RIPIRESOCCAlinai OCSIGNATIOM HUMIICINCCI CLASSOICATI0Nis• L. _ie./A__ DERT-510087-NIYI Systems & Equipment No an J. an FAA Form /*P0) sun/LS/DES PRZYIOUSEDmoN GP0001-433FIENAME30 727414CREYADOC SDNY_GM_02759739 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024()661 EFTA01331124 SDNY_GM_02759740 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246662 EFTA01331125 Jet Aviation Associates Ltd. AFM Supplement to Bldg. 1515 Perimeter Rd. The Boeing Company 727-31 Palm Beach Intel Airport Serial No. 20115 West Palm Beach, FL 33406 FAA Form 337 FAA CRS EYKR782D Document No. B727-16236-100 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR BOEING 727-31 REGISTRATION NO.: N9013JB SERIAL NO.: 20115 WITH DUAL UNIVERSAL AVIONICS FLIGHT MANAGEMENT SYSTEMS (UNS1-D) INSTALLED This supplement must be attached to the FM approved Airplane Flight Manual when the airplane is modified by the installation of dual Universal Avionics Systems Corp. (UASC) (UNS-1D) Flight Management Systems (FMS), with Frequency Management via a UASC Radio Tuning Unit (RTU), receiving navigation inputs from Triple Honeywell Inertial Reference Sensors (IRS), dual internal GPS sensors, and VORIDME from the Collins No. 1 and No. 2 VORIDME systems in accordance with manufacture's InstalatIon and Checkout Manual No. 34-60-09, Rev. 2, dated August 15, 1997 or later approved revision and FAA Form 337, dated ,fune 26, 2001. The information contained herein supplements or supersedes the basic manual only in those areas listed herein. For limitations, procedures, and performance information not contained in this supplement, consult the appropriate basic Airplane Flight Manual. FAA Approved: 'Or c7 . ' Cif, Federal Aviation Administration Flight Standard District Office -17 1050 Lee Wegener Blvd. Ft. Lauderdale, Florida 33315 FAA Approved Date: June ;1.2001 Revision A. Dated: 5/3 ,:.n> Page 1 of 9 SDNY_GM_02759741 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246663 EFTA01331126 SDNY_GM_027.742 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246664 EFTA01331127 Form Approved fig, MAJOR REPAIR AND ALTERATION OMB No. 2120-0020 US Orartrnre of Tansp3rwlon . (Airframe, Powerplant, Propeller, or Appliance) For FAA Use Only Federal Aviation Officeldenlifisation, AdenletIstrallon . Eri-k- 1.3U^37 INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B. and AC 43.9-1 (or subseque t revision thereof) for Instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can re ult in a civil penalty not to exceed $1,000 for each such violation (Scotian 901 Federal Aviation Act of 1958). Make Model BOEING 727-31 1. Aircraft Serial No. Nationality and Registration Mark 20115 U.S.A. N908.TE Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner JEGE INC. 103 FOIE-ICRD. STE 2O2 WILMINGTON DE. 19803-3742 3. For FAA Use Only 4. Unit Identification 6. TYPO Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer . 6. Conformity Statement A. Moneys Name and Address B. Kind of Agency C. Certificate No. U.S. Certified Mechanic CRS EVICR782D JET AVIATION ASSOCIATES LTD. Foreign Certified Mechanic AIRFRAME O. 1516 PERIMETER RD. x Certificated Repair Station WEST PALM BEACH. FL 33406 RADIO 1,2,3. Manufacturer i METED D. I certify that the repair and/or alteration made to the wafts) identified in item 4 above and described on the reverse or A/F It ENG 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 COrTett to the best of my knowledge. Date Signature of Authorized Individual 1/14/02 John K. Ursa. Inspector. L44 114.— 7. Approval for Return to Sera Pursuant to the authority given persons specified below, the unit dentilied in item 4 As inspected In the manner prescribed by the Administrator of the Federal Aviation Administration and is ig) APPROVED DI REJECTED FAA Fit. Standards Other (Sadly) Inspector Manufacturer Inspection Authorization BY FM Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection Certificate or Signature of Authorized Individual Designation No. 1/14/02 EVICR782D Ronald K. Bystrom. Manager Quality Assurance. FAA Form 337 (1288) SDNY_GM_02759743 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0O246665 EFTA01331128 NOTICE Weashlandbalance or operating amitalion changes shall be entered in the appropriate aircraft record An alteration must be compatacfir With al:previous alterations to assure continued contumely with the applicable ainvorthiness requirements. 8. Description of Work Accomplished (If more space is requited, attach adirdonal sheets, Identify with aircraft nationality and mgistration MEM and date note accomplished.) BOEING 727-31, S/N 20115. N908.1E: W/O 17454. ACCOMPLISHED AN ALTERATION TO THE CABIN INTERIOR FURNISHING ARRANGEMENT PREVIOUSLY INSTALLED UNDER PAGE AVJET STC SA3137S0, DATED 1/17/92, BY REMOVING THE FOLLOWING INTERIOR FURNISHINGS: DESCRIPTION POSMON P/N S/N F.S. WIT 0/B AFT FACING SEAT. FORWARD SALON 303413-2 4350 401.94 R/H VB AFT FACING SEAT. FORWARD SALON 303413-10 4351 401.94 FORWARD RAI TABLE AND PEDESTAL FORWARD SALON A727-2531-001 NSN 438.50 LH AFT FACING SEAT CENTER LOUNGE 3034131 4354 73200 COFFEE TABLE AND PEDESTAL CENTER LOUNGE 727-2535-003 NSN 772.50 THIS ALTERATION WAS ACCOMPLISHED PER JET AVIATION DRAWING B727-17454-200, REV IR, DATED 1/2102, SHEETS I & 2, TITLED - MINOR DEVIATION TO STC SA3137S0, THE LIMITED 727-100 GENERAL ARRANGEMENT. REFERENCE F.A.A. FORM 8110 DATED 1/6/02 BY STRUCTURES D.E.R. NO. DERT-810028-NE. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS TAW AC43.I3-1B, CHAPTER TO, SECTION 2 AND AC 43.I3-2A, CHAPTER 1 PARAGRAPH 9. THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES REQUIRED FOR THIS ALTERATION. END O Additional Shoots Am AttaOhod * U.S. G.P.O 1990.781.753 SDNY_GM_02759744 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246666 EFTA01331129 Form Approved le MAJOR REPAIR AND ALTERATION OMB No. 2120-0020 US Otp.vtraceni olranoccetabca T (Airframe, Powerplant, Propeller, or Appliance) For FAA Use Only Federal Minion Office IVtifictlion AderisisbaGen 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 Boeing 72731 1. Aircraft Serial No. Nationality and Registration Mark 20115 N908JE Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner JEGE Inc. 103 Foulk RD STE 202 Wilmington, DE 198034742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME As descnbedin Item 1above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer / f I 6! Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. X U.S. Certified Mechanic Gary K Palmer Foreign Certified Mechanic 6 Hyacinth Lane Certificated Repair Station #84544584AP Holbrook, NY 11741 Manufacturer D. I certify Nat 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 Authorized Individual 08/01/01 Gary K Palmer 7. App oval for Return to Service Pursuant to the authority given persons specified below, the unit dentified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is 0 APPROVED ID REJECTED FAA Ft Standards Other (Snooty) Manufacturer X Inspection Authorization Inspector BY Person Approved by Transport FAA Designee Repair Station Canada Airworthiness Group Dale of Approval or Rejection Certificate or of Authorized Individual x , Designation No. 08/01/01 84544584W Gary K Palmer ----Y .-42i ern' 331(12438) SDNY_GM_02759745 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246667 EFTA01331130 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. B. Description of Work Accomplished (Ifmore space is required, attach additional sheets, Identify with aircraft nationality andregistration math and date work accomplished.) Firebtocked and upholstered existing, one (1) cabin single chair (Erda SIN 4359) in Townsend: Leather Lambskin Pads Alligator Embossed/Tipped Gold/Black, leather and two (2) cabin chairs (Erda S/N 4357 and 4358) in Clarence House: 1037901S-37 Velours Mohair, fabric. D.E.R. Identification 62326-01. Fireblocked and upholstered existing, two (2) cabin single chair (Erda SIN 4360 and 4361) in Old World Weavers: Edmond Petit FMPOO 10004 Zoom, fabric. D.E.R. Identification 64318-01. Fireblocked and upholstered existing, one (1) cabin single seat (Erda 5/14 4354) and one (1) three section divan (Dettmers S/N 520, 521, and 522) in Gellman Ind.: Tiburon TWeed, fabric and one (1) divan (Deitmer SIN 516) in Clarence House: 10379MS-37 Velours Mohair, fabric. D.E.R Identification 65624-01. Fireblocked and upholstered existing six (6) single cabin seats (Erda SIN 4350, 4351, 4352, 4353, 4355, 4356), one (1) LH forward sidefacing divan (Dettmers SIN 517), and two (2) 3-place reclining divans (Detainers S/N 518 and 519) in Old Weavers: EA81340013 Alfa Check, fabric and ETS J. Tessin SA.: Mastic #19075, leather. D.E.R. Identification 65059- 01. All materials meet FAR 25.853(a) Appendix F, Part l(aX1)(ifi. Aircraft seat cushions have been fireblocked as per the requirements of FAR 25.853(c) Appendix F, Part II. Amendment 25 - 83. Results of sample bum tests are documented on SAL's Test Plan #7428, #7617, #7722, and #7759 and on attached DER approved 8110-3, Identification 62326-01, 64318-01, 65624-01, and 66059-01. Seat cushions have been tagged as being in comp5ance with the applicable regulatory requirements. Aircraft seatbelts were sent to Aircraft Belts. Inc. Repair Station YB1R632K for rewebbing, work order number 0046395 and reinstalled on the seats and divans. Replaced 19 each P.L. Porter 5102300-28 seat recline Hydrolok and 6 each P.L Porter 5102300-21 divan recline Hydrolok. Hydroloks were replaced using standard interior practices. Installed Erda Hydro Legrest PIN 302617-3 and mechanical control single P/N MC15-36 on two (2) cabin single seats Erda seat SIN 4360 and 4361 in accordance with Erda drawing 302617 Rev B. Attached: FAA approved Townsend: Leather Lambskin Paris Alligator Embossed/ Tipped Gold/Black, leather and Clarence House: 10379015-37 Velours Mohair, fabric. Test Plan #7428, form FM 8110-3 dated 04/16/01, Judy Boggs, DERY-405020-CE. Identification 62326-01. Attached: FAA approved Old World Weavers: Edmond Petit FMPOO 10004 Zoom, fabric. D.E.R. Identification 64318-01. Test Plan #7617, form FM 8110-3 dated 06/20/01, Judy Johnson, DERY-405020-CE. Identification 64318-01. Attached: FM approved Gellman Ind.: Tiburon Tweed, fabric and Clarence House: 10379BIS-37 Velours Mohair, fabric. Test Plan #7722. form FM 8110.3 dated 07/12/01, Donna J. Parrish, DERY-410100-CE. Identification 65624-01. Attached: FAA approved Oki World Weavers: EA81340013 Alfa Check, fabric and ETS J. Tessin SA: Mastic #19075, leather. Test Plan #7759, fowl FM 8110-3 dated 07/24/01, Donna J. Parish, DERY-410100-CE. Identification 66059-01. Attached: Aircraft Belts, Inc.: CertificalloniPaddng List, work order number 0046395 consisting of 11 sheets. Attached: FAA form 8130-3 from P.L. Porter Controls, Inc.: 5102300-21 and 5102300-28 Hydrolocs tracking number 7723, 6751, 7176. 6759, 9495, 7367, 7368, and 9292. Pertinent data on file at International Jet Interiors, Inc. under W.0.#: 01119. Customer to install seats and divans In aircraft. Log entry has been made. EN 0 Additional Sheets Are Attached * U.S. G.P.O 1990461453 SDNY_GM_02759746 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246668 EFTA01331131 ()V 0 - Form Approved 0303 No. 2120-0030 ' MAJOR REPAIR AND ALTERATION Dpartrnalto (Airframe, Powerplant, Propeller, or Appliance) For FAA Use Only U.S on man Federal Aviation Office Idaztillosion Administration d, - tl5o F.5 gel -1 S gi-6 -- ')'sn" form. This= P", +2" 195 5. aerie issirtifi"1, re ( . . y ). a FAR 43 Appendix B, pad* 43.94 (or who:quad.rivision Owedfor instructions and stisposhicp of this ton:port result an civil penalty not to cohan151,000 fix radi MI violation (Scale,. 901 hislaal tion MakeBoeing Medd 727-31 sawNo.20115 Nationality and Rogan:ice Made N908JE 3. Aircraft Marne (As shown as regLaratica ocitificatc) Micas (xs Aomori rogistraticn certifunte) JEGE INC- 103 FOULKRD STE 202 L Owner WILMINGTON DE. 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make I Model 1 Serial No. Repair Alteration AIRFRAME (As domIxd in hats 1 above) XX POWERPLAYT PROPELLER Twc APPLIANCE hbindacturcr 6. Conformity Statement A- Agaicds NarnexadMdrou B. Kind *Maw/ C. Catificate No. U.S.Catificatoitachanic DU4R141M TIMCO Foreign Cati6coodMechanic Lake City Municipal Airport X Catillaitof Repair &Mica Lake City, FL 32025 Manufactura D. I certify that the repair ander alteration mad, to the logs idaulfief in itcnr 4 abonond dam-bida:ft rcruscorattichmonhereto have bon made in accordance vrilltropaircinents ofPartAl ofdoU.S. Wool Aviation Regulditosandihathe ioknaaticaDanishitdhock istrucandoxinctto die test &my blade* Date August 1, 2001 Signature orAuthorized Individual Owen H. Pritchard II ..._ 7. Approvalfor licturriToSers c Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by die Administrator of the Federal Aviabon. Administration and is 12 APPROVED 0 REJECTED FM Fk. Standards hlimufacturcr Inspation Authicizatiai Other (Sptcy54 Inspector FAA Datignix X Repair Station Pasco Approved by Transport Canada BY Ains Group Donor 49(0=1or Rejection Catifiratcor Dosignaticas No. Sigmas a Authiciud Ind' L. Palm August 1, 2001 DU4R141M FAA Form 337 (12-88) SDNY_GM_02759747 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246669 EFTA01331132 NOTICE Weight and-balance or operating limitation changes shall be enteredin the appropriate aircraft record. An alteration must be compatible with allprevious alterations to assure continued cot:fannies with the applicable alnvorenness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration matt and date work completed.) BOEING S/N 20115 REG. NO. N908JE . Page 1 August 1, 5001 The following major repairs were accomplished: NR# 27754 Repaired detaminated R/H Mid Flap Trailing Edge wedge by removing the delaminated section and fabricating and installing a new T/E wedge and strips TAW TIMCO REO-L00464 dated 7/17/01 FAA Form 8110-3 approved by DER. Richard C. Saltivan DER # DERT-405157-CE dated June 19, 2001. MU 27918 Repaired the delaminated and corroded Left Hand Inboard Mid Flap bottom upper Rock-shield panel by removing Rock-shield and corrosion, treated and primed area to be bonded, impregnated fiberglass overlays as required, applied conductive coating and. installed panel IAW B727 SRM 57-50-2, 5140-8, MM 51-20-0 & SB 727-32-247 RI dated June 5, 1981. SUMMARY 1. All work accomplished JAW Boeing SRM, TIMCO REO, FAA Form 8110-3 and ServiceBulletin. 2. Records of all work accomplished is on file at this repair station under work order 185003. 3. Aircraft Weight and Balance updated accordingly. end 0 Additional Sheets Are Attached SOSGOVEIOJQ4T PRINIONIOFFICE IW1.769.0i2,1007 SDNYGNI_02 759748 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246670 EFTA01331133 6 us Departmeel . of TrwepOrtallon MAJOR REPAIR AND ALTERATION (Airframe, Powerplant, Propeller, or Appliance) Form Approved OMB No. 2120-0020 For FAA Use Only Fearslablatica Office Identification Adenlitstrailon 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 SOI Federal Aviation Mt of 1956). Make Model BOEING 727-31 1. Aircraft Serial No. Nationality and Registration Mark 20115 U.S.A. N008JE Name (As shown on regIsfralkx; certificate) Address (As shown on registration certificate) 2. Owner JEGE INC 103 FOULK RD STE 202 WILMINGTON DE 19803-3742 3. For FAA Use Only in-, data idatIttheod %Val liet the appacrot 2:nottniele retirements apperee est the above emenbe:/ acre. when by a perton JOS:161hr 433. So -rs-Da- ir Ch" a re minsondet 4. Unit !dentinal on) 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. Certified Mechanic CRS WEICI4752D JET AVIATION ASSOCIATES LTD. Foreign Codified Mechanic AIRFRAME O. 1516 PERIMETER RD. x Certificated Repair Station RADIO 1,2,3. WEST PALM BEACH. FL 33406 — Manufacturer LIMITFD AIF &FNG 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 V.S. Federal Aviation Regulations and that the information furnished herein Is true and correct to the best of my knowledge. Date Signature of Authorized indivi 'A4/ . lobo K. Urso. Inspector. 4 (Ler — 7. Approval for Return to Servl Pursuant to the authority given persons specified below, the unit derained in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and Is Fs) APPROVED 0 REJECTED Other (Specify) FAA Fit Standards Manufacturer Inspection Authorization Inspector BY Person Approved by Transport FM Designee X Repair Station Canada Alnvorthiness Group Date of Approyal or Rejection Certificate or Signature of Authorized Individual Designation No. 7 4 1- / 0 / EYKR782D Ronald K. Bystrom. Manner Quality Ass FAA Form 337 ti2-as) SONY_GM_02759749 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024667 I EFTA01331134 NOTICE Weight andbalance or operating finiltation changes shall be enteredIn the appropriate aircraft allprevious alterations to assure continued conformity with the applicable &neon/darks record. M afteratkn must be teakettle with requirements. • 8. Description of Work Accomplished (Ifmore space b required, attach arketional sheets, identify with aircraft nationality and registration mark end date wog* accomptshed) AIRCRAFT: BOEING, TYPE: 727-31, S/N 20115, DATE: 06/14/2001. W.O. 16234 PAGE 1 OF 2 INSTALLED A SINGLE EVENTIDE AVIONICS ARGUS 5000/CE MOVING MAP DISPLAY SYSTEM (ISO CI13). THIS MODIFICATION WAS COMPLETED USING JET AVIATION DRAWING NO. B727-16236-270, ARGUS 5000 CIE MOVING MAP DISPLAY, REV. A. DATED 06/19/01. REFERENCE FAA FORM 8110-3. DATED 6/20/01, BY SYSTEMS AND EQUIPMENT DER NO. DERT-510087-NM. THE EXISTING LASERTRAK WIRING WAS RE-BUSSED DUE TO RELOCATION OF LASERTRAJC C.D.I. THIS MODIFICATION WAS COMPLETED USING JET AVIATION DRAWING NO. 34-61-32-1, LAZERTRILIC SYSTEM MODIFICATION, REV IR, DATED 5/24/01. THE STRUCTURAL INSTALLATION OF THE AROUS.540weaimovate Ma.DISPLAY SYSTEM AND THE RELOCATION OF THE LASERTRAK Cal. WAS COMPLETED USING JET AMIUM40„ Iwo. ARGUS 5000/CE MOVING MAP EQUIPMENT INSTALLATION, REV. 112. DATED 0929/0 . MAFORM AlEp 06/03/2031. BY STRUCTURES DER NO. DERT-13100213-NE. ;on. -7- — THE EVENTIDE AVIONICS ARGUS 5000/CE MOVING MAP DISPLAY IS A PICTORIAL NAVIGATION INSTRUMENT, WHICH PROVIDES VISUAL REFERENCE OF AIRCRAFT POSITION RELATIVE TO LANDING FACIL(TIES, NAVIGATIONA L AIDS AND SPECIAL USE AIRSPACE. THE ARGUS 5000/CE RECEIVES GEODETIC POSITION AND OTHER NAVIGATION INFORMATION FROM THE NO. 1 UNS- ID FMS THROUGH AN EVENTIDE AVIONICS ARINC 419/429 ADAPTER UNIT AND THE AIRCRAFT'S NO. 3 HONEYWELL "LASERREF" INERTIAL REFERENCE SENSOR (IRS) DIRECTIONAL HEADING SYSTEM WHICH, PROVIDES MAP GRAPHICS AND BEARING ORIENTATION. THE FOLLOWING SWITCHES ARE LOCATED ON P16 FORWARD CONTROL STAND. BELOW THE ARGUS 5000 CE MOVING MAP DISPLAY: ARGUS INFQ MOMENTARILY DEPRESSING THE ARGUS INFO ILLUMINATED (BLUE) SWITCH BRINGS UP INFORMATION ABOUT MAP OBJECTS ON THE ARGUS 5000/CE MOVING MAP DISPLAY. IF THE ARGUS SWITCH IS PUSHED IN FOR 1 SECOND, THE ARGUS 5000/CE WILL RETURN TO THE MAP DISPLAY IN $ 4F0 THE SAME MODE AND AT THE SAME RANGE SET. WHEN INFO WAS ENTERED. ARGUS MOMENTARILY DEPRESSING THE 612GUS SEL ILLUMINATED (BLUE) SWITCH CYCLES THE ARGUS 5000/CE DISPLAY THROUGH THE VARIOUS MAP OBJECTS. ARGUS TEST MOMENTARILY DEPRESS THE ARGUS TEST SWITCH TO ENABLE DISPLAY SIMULATION TEST. THE ARGUS 5000/CE MOVING MAP DISPLAY IS APPROVED FOR IFR ENROUTE NAVIGATION ONLY WHEN RECEIVING NAVIGATION INFORMATION FROM AN IFR APPROVED CPS, LORAN. OR OTHER LONG-RANGE NAVIGATION SYSTEM. THE ARGUS 5000/CE DATABASE MUST BE CURRENT (NOT EXPIRED). THE ARGUS 5000/CE IS APPROVED FOR USE AS A SUPPLEMENTAL NAVIGATION DISPLAY FOR VFR AND IFR OPERATIONS BUT IS IJMITED TO THE APPROVAL OP THE LORAN C OR GPS NAVIGATION SYSTEM. THE ARGUS 5000/CE MOVING MAP DISPLAY HAS BEEN SHOWN TO MEET THE CRITERIA OF FAA TSO.CI 13, AIRBORNE MULTIPURPOSE ELECTRONIC DISPLAYS. AND HAS BEEN PREVIOUSLY INSTALLED UNDER EVENTIDE INC. FAA APPROVED STC SA0054NY. IN AN AIRCRAFT AND MEETS THE FAA REQUIREMENTS FOR OPERATION IN THE AIRCRAFT DURING INSTRUMENT FLIGHT AND CAN BE USED AS A REQUIRED INSTRUMENT. THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER EVENTIDE AVIONICS INSTALLATION MANUAL NO. 5003. REVISION 03.07. DATED JULY 10, 1995 WITH NO DISCREPANCI ES. AN EMI TEST. REPORT NO.: B727-16236-080 REV IR, SHEETS 5. DATED 06/19/01 WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.13-IB, CHAPTER 12, SECTION 3, PARAGRAPH 12- 37 AND AC 43.13-2A, CHAPTER 2 PARAGRAPH 234 THE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.I3-2A. CHAPTER 1. PARAGRAPH 3 AND WAS FOUND TO MEET THE REQUIREMENTS OF PARAGRAPH 2. MATERIALS AND PRACTICES COMPLY WITH PARAGRAPHS 4 THROUGH 12. THE ELECTRICAL LOAD ANALYSIS UPDATE REPORT NO. B727- I 6236-041, REV IR. SHEETS 1 THRU 21. DATED 06/11/2001 WAS COMPLETED IN ACCORDANCE WITH AC43.13-111. CHAPTER PARAGRAPH 11.37. 11, SECTION 3. 121 Additional Sheets Are Attached * V.S. G.P.O 1990-761-753 SDNY_GM_02759750 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246672 EFTA01331135 NOTICE Wejght and balance or operating knitation changes shag be entered in the appropriate aircraft record An alteration must be conpatible with ail previous alterations to assure continued confonnily with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is requited, attach additional sheets, Identify with aircraft nationality and registration mark and date work acconwashed.) AIRCRAFT: BOEING, TYPE: 727-31, SIN 20115, DATE 06/1412001, W.O. 16236. PAGE 2 0F2 • AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-18, CHAPTER 4. SECTIONS 1, 2.3 AND 4, CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.13-1B, CHAPTER 7, SECTIONS I.5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MD. SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43.13-1B, CHAPTER I I, SECTION 4. EIECTRICAUELECTRONIC WIRING WAS SELECTED AND INSTALLED TAW AC43.13-1B, CHAPTER 1I, SECTIONS 5-8, 13. 15, 17-19 AND AC43.13-2A CHAPTER 2, PARAGRAPHS 21,22 & 27. ROUTING, LACING AND TYING COMPLIES WITH AC43.13.1B, CHAPTER 11, SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-18 SECTION 16. ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURER'S INSTRUCTIONS AND AC43.13.2.A, CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3, PARAGRAPH 44. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS TAW AC43.13.1B, CHAPTER 10. SECTION 2 AND AC 43.13-2A, CHAPTER i PARAGRAPH 9. MAINTENANCE FOR CONTINUED AIRWORTHINESS IS OUTLINED IN EVENTIDE AVIONICS DRAWING NO. 140003, REV. B, DATED JUNB JUNE 0. 1999. AND STATES THAT THE ARGUS 5000/CE MOVING MAP DISPLAY SYSTEM IS "ON CONDMON". THE REQUIRED F.A.A. APPROVED FLIGHT MANUAL SUPPLEMENT DOC NUMBER B727-16236401, REV 112, PAGES I THRU 6 DATED jilrle 2-1 OO1 HAS BEEN INSERTED INTO THE AIRCRAFT FLIGHT MANUAL ,END 0 Additional Sheets Are Attached * U.S. G.P.O 1890-781-753 SDNYGIvl_02759751 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246673 EFTA01331136 SDNY_GM_02759752 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246674 EFTA01331137 Jet Aviation Associates Ltd. AFM Supplement to Bldg. 1515 Perimeter Rd. The Boeing Company 727-31 Palm Beach Intl Airport Serial No. 20115 West Palm Beach, FL 33406 FAA Form 337 FAA CRS EYKR782D Document No. B727-16236.101 I FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR BOEING 727-31 REGISTRATION NO.: N9OBJE SERIAL NO.: 20115 WITH A SINGLE EVENTIDE AVIONICS ARGUS 5000/CE MOVING MAP DISPLAY This supplement must be attached to the FAA approved Airplane Flight Manual when the airplane is modified by the installation of a single Eventide Avionics Argus 5000/CE Moving Map Display receiving navigation inputs from the No. 1 UNS-1D Flight Management System (FMS) in accordance with manufacture's Installation Manual No. sop Revision 03.07, dated July 10, 1995 or later approved revision and FAA Form 337, dated VW/ The information contained herein supplements or supersedes the basic manual only in those areas listed herein. For limitations, procedures, and performance information not contained in this supplement, consult the appropriate basic Airplane Flight Manual. FM Approved: Federal Aviation Administration Flight Standard District Office -17 1050 Lee Wagener Blvd. Ft. Lauderdale, Florida 33315 FAA Approved Date: JUN 2 1 2001 Page 1of6 SDNY_GM_02759753 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246675 EFTA01331138 SDNYGM027597. SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246676 EFTA01331139 attn-2O-O1 O8:53 Jett Aviation P . O2 Jun-20-01 O8:O3A N J Curran 352 243 1O11 P 02 IMPPADIENT Of VIANWOATATION DAM Matt MIA 00s. ADIMOTRADaN STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS 06/20/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAIk MOOD. NO. TYPEUnarm. Rad*, *hoopla. tic) MAME OF APPLICANT Jet Aviation Associates Boeing 727-31 Airplane West Palm Beach, FL MT OF DATA IDENTIFICATION TITLE 8727.16236.270, Revision A, dated ARGUS 6000ICE MOVING MAP DISPLAY 06119/01 PURPOSE OF DATA In support of major alteration Io.Boelng 727-31, serial number 20115. regisUalion number N90BJE. APPLICABLE REQUIREMENTS (Lba specific sections) FAR 26469 (a)(4) FAR 25.1431 (a)(b)(c) FAR 25.1301 (a)(b)(c)(d) FAR 25.1629 FAR 25.1309 (a)(b)(g) FAR 25.1581 (a)(b)(d) FAR 26.1361 (a) FAR 25.1357 (a)(c) CERTIFICATION - t ion ..a..........•6,anah•or a.,......«.m. ads swam.nante••••••••••••••healorpriSsam••••I.n mutat no...«now rwr ia...... a... —01/CE._. ...4.... 1^•••••en "ea Hp.... *masa. 0 lientasead marvel ofSae Oslo I OM.) rbarefore ID Ann...Hem tam (Symms • tqcOnsessi Aspects. Di/sin AprOai thi)..DiaMt Cant:eta bawl:Weft Apprt...• WAAMILCI CO t"C ainnENTAM11O4 OCJIGOATICM. PUMPS% C /AMICK •MINI. DERT-510087-NM Systems & Equipment fee --, o n J. n SDNYGIvl_02759755 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246677 EFTA01331140 SDNYGM02759756 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246678 EFTA01331141 JET AVIATION ASSOCIATES, LTD • ie SET NifffS1701111 1515 PERIMETER ROAD PALM BEACH INT'L AIRPORT ilidin iCH Fliiiiiiii.493 MODIFICATION DRAWING PIONIOOLY tOret la. *roof, esSe "Tsars, wd/ do* tweeted neoelok newts espy ore Idisoike US we we So navy erg .0 OSZOI ASSCOOO. OP %M.o./ ere USW V/ b eedSoot on*Soeedo. bode es Ti oel to •• Sea of goons on wool/edged onoSeta pens 4404.4 the sins weedogrego JO IIMMoil 0130000. km TITLE: LASERTRAK SYSTEM MODIFICATION PAGE: 1 OF 1 DWG NO.: REASON: RE- BUSS LASERTRAK INSTRUMENT LGHTING FROM CENTER PANEL 34 - 61 - 32 - 1 TO CAPTAINS INSTRUMENT PANEL DUE TO RELOCATION OF INSTRUMENT _ A NOlt$: 1. AIRCRAFT WIRING INSTALIATION MW FM AC. 43.13-18, CHAPTER 11, SECTIONS 1, AND 3-20. 2. ALL WIRE PER MIL-W-22759 UNLESS SIOELDEO. 3. ALL SHIELDED WIRE PER IAL-C-2750010. 4. A.U. METE 20 MC UNLESS SPEOF1ED OTHERMSE. S. All. CIRCUIT BREAKERS PER 11536574. 6. ALTERNATE TWISTED WIRE COLORS MAY BE SUE411TUTED: Mat $LS TRIPLE TWISTED RED (R) WIVE (R) SLUE (B) BLUE (El) YELLOW (Y) ORANGE (0) TWISTED PAIR: RED (R) MITE (R) BLUE (6) BLUE (8) 7. LOWER CASE LETTERS ARE SHOWN UNDERUNED. LE. S. 8. THIS MODIFICATION DRIOTINC ONLY CHANGES THE COSTING LASERTRAJC SYSTEM PER THE WRANG SHOWN. FOR ALL OTHER INFORMATION REGARDING THE LASERTRM( SYSTEM REFER TO ORCRIAL PAGE AWET DWG. 34-61-32. THIS MODIFICATION DRAWING SIAU. 8E ATTACHED TO THE ORIGAMM. PAGE AVJET DRAWING FOR REfERNCE ND. i- rim BRCIDIST . D9504 n .. r Fl a i 01-20 II 1Nsirt L.'? t 0 µ I-20 _ .... _0 19_ 20_ _ PAGE CMG. 33-11-11 I dr ' tticZt LO rrisfina FAsERTRAK h COI 1—I 0915 3 Rim LTs II 09315 1 20 I {SC 9I 09315 9-20 LAL`rrift>7 141117 . ,a Ipi tan:t r .-8> 40C GIS .4 MC 040 o SYMBOL MID NORM REFERS TO PARTS LIST REM NUMBER. mute a, sada. AND NUMBER REFERS TO WSTALLATION NOTES. 1 .43> aS)LD Gle -B> .0415515 CND NEW WOE REMOVED WIRS COSTING WIRE O sweet Mt LETTER ren REFERS TO LEE LETTER w SYMBOL ON DWG,. NO. WIRE TOE NOTES: ( ) (• 1G. SCALE: NONE SER. NO.: 20115 PREPARED BY: G.L. KARR APPROVED BY: T. JARDINE A/C MODEL: 727-100 REG. NO.: N9OBJE DATE: 05/24/01 DATE: 05/24/01 SDNY_GIvl_02759757 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246679 EFTA01331142 SDNY_GM_02759758 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246680 EFTA01331143 OEPAFtTMENT OF TRANSPORTATION I-DATE FEDERAL AVIATION ADMINISTRATOR STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS June 3, 2001 AIRCRAFT OR ARCRAFT COMPONENT MENTRCATER MAXE MOM NO. TYPE (Mpent Radio. HokopteLeict NAME OF APPUCANY Boeing 727-31 Airplane Jet Aviation Associates- WPB LIST OF DATA ICSITFICATON TITLE B727-16236-1270 Argus 5000/CE Moving Map Equipment Installation Sht 1-5, Rev IR B727-16236-1331 Aircell Equipment Installation, Sht 1-6, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPUCAME REOUTTIMNS (LAl sped& secetas) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.561 25.601 25.603 25.605(a) 25.609 25.611 25.613 25.789 CERTIFICATION - Wider al/Monty vested by *Gaon of the Administrator aid in accordance vets caulbore and knitallons of eopoktrnant under Past 183 of the Federal Aviation Revise onS.data listed above and on attached sheets numbered 0 have boon exantved in iteowdenee with established procedures and round to eemPlY whil appecatio raquIrements of the Federal Avlatke Nebula One. ,0 hoosonnend *Prover of these data I (.4 thersevo Approve these data SKUMTURE(S) OF INSIGNATE0 010Inax.10 imppisaiNTATNE(S) OESIONATON reuratEMS) GLASSINE-010NR) David E. Haralson ,Poode. iliontio-- DERT-810028-NE Structural orm 8110 3 it t40.SUPERSEDES PREVIOUS ECTOM Ell01207.dc< SDNYGlvl02759759 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024663 I EFTA01331144 SDNYGM02759760 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246682 EFTA01331145 - o Form Approved O MAJOR REPAIR AND ALTERATION OMB No. 2120-0020 OS Depaterera (Airframe, Powerplant, Propeller, or Appliance) For FAA Use Only el Transpoeudon Wend 4Vaeon Office Identification Administration 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 S1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model BOEING 727-31 I. Aircraft Serial No. Nationality and Registration Mark 20115 U.S.A. N908JE Name (As shown on registration certificate) Address (As ahem on registration certificate) 2. Owner -GE INC IF 103 FOULK RD STE 202 WILMINGTON DE 19803-3742 . 3. For FAA Use Only on ests Werneree herein complise S re sad is aresenteres ragawireents r appatedeeerrryyy tre ma above deserted rad. mekxm t4psaseet by • Penal • tAliOrtid In FAR 43. 43.7. aktiaair ' So- spo-t 7 AllIrefh1 -ow olFAA Irmo 4. Un Identification S. Type Unit Make Model 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. U.S. Certified Mechanic CRS EYKR782D JET AVIATION ASSOCIATES LTD. Foreign Certified Mechanic AIRFRAME 1,3. 1515 PERIMETER RD. X Certificated Repair Station RADIO 1,2,3. WEST PALM BEACH. FL 33406 — Manufacturer LIMITED A/F & ENG. 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. Dale Signature of Authorized Individual /1/0) • John K. Ursa Inspector. it- It. --6- 7. Approval for Return to Se ce Pursuant to the authority given persons specified below, the unit dentified in item 4 was inspected In the manner prescribed by the Administrator of the Federal Aviation Administration and is 0 APPROVED O REJECTED Other (Specify) FM Fit. Standards Manufacturer Inspection Authorization Inspector BY X Repair Station Person Approved by Transport FM Designee Canada Airworthiness Group Date of Apprpvalpr Rejection Certificate or Signature of Authorized Individual 4/ / Designation No. 24 7C EYKR782D Ronald K. BretrOn Manager Quality FAA Form 337 024s) SONY_GM_02759761 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246683 EFTA01331146 NOTICE Weight and balance or operating Imitation changes shall be entered in the appropriate aircraft record. An Memnon must be compatible with all previous alterations to assure continued conformity with the applicable einvorthIness requirements. 8. Description of Work Accomplished (if more space is requ)rst% attach additional sheets, identity with Leonia nationality and registration mad( and date kiosk acoomFdshed.) AIRCRAFT: BOEING, TYPE 727-31, SIN 20115, DATE: 06/14/2001, W.O. 16236, PAGE 1 OF 2 REMOVED THE EXISTING NO. 1 AND 2 HONEYWELL NZ.920 EMS SYSTEMS AND 771E DL -900 DATA WADER UNIT. AND INSTALLED DUAL UNIVERSAL AVIONICS CORP. UNS-1D FLIGHT MANAGEMENT SYSTEMS (EMS) WITH INTEGRAL GPS SENSORS, A UNIVERSAL AVIONICS CORP. RADIO TUNING UNIT (RTU), AND A UNIVERSAL AVIONICS CORP. DTU-100 DATA TRANSFER UNIT (DTU). THIS MODIFICATION WAS COMPLETED USING EST AVIATION DRAWING NO. B727-16236-410, NO. 1 FLIGHT MANAGEMENT SYSTEM, REV IR, DATED 04/10/01 AND B727-16236-411, NO.2 FLIGHT MANAGEMENT SYSTEM, REV. IR DATED 04/15/01. THE RTU WAS INSTALLED USING JET AVIATION DRAWING NO. B727-I6Z36-293, FLIGHT MANAGEMENT SYSTEM RADIO TUNING UNIT, REV Et, DATED 04/16/01. REFERENCE FAA FORM 8110-3 DATED 05/292001 BY SYSTEMS AND EQUIPMENT DER NO. DERT-510087-NM. raw. ot atm mares &Wel Pi, It at ' d° Ottnel 'en° "IOWA= If WC Span' arine• • THE STRUCTURAL INSTALLATION OF EACH EMS, THE DTIMEN0tHeitT0 WEFEC2MPLETEA OJET AVIATION DRAWING NO. B727-16236-1410, DUAL MIS W/RTU EQUIPMENT INSTALLATIONS. REV. IR, DATED 05.117/01„. lalE FAA FORM 8110-3, DATED JUNE 1, 2001 BY STRUCTURES DER NO. DEBT-81 S-ANTENNAS AILED • USING JET AVIATION DRAWING NO. B727-16236-1441, GPS ANTENNA INSTALLATI N, REV. A, DATED 05/29/01, REFERENCE FAA FORM 8110- 3. DATED 018/01 BY STRUCTURES DER NO. DERT-510024-CE. THE UNS-1D SYSTEMS RECEIVE BARO-CORRECTED ALTITUDE AND TAS INFORMATION FROM THE NO. 1 AND NO.2 AIR DATA COMPUTERS RESPECTIVELY, VOR/DME BEARING AND DISTANCE INFORMATION FROM THE NO. 1 AND NO.2 COLLINS VIR-432 AND DME-442 SYSTEMS. AND CROSS SIDE GPS INFORMATION AS WELL AS EACH UNITS INDEPENDENT GPS SENSOR DATA, FUEL FLOW DATA FROM THE AIRCRAFT FUEL FLOW SYSTEM AND IRS INFORMATION FROM THE EXISTING NO. I. 2. AND 3 HONEYWELL "IASERREF SYSTEMS. THE UNS-ID FMS HAS BEEN PREVIOUSLY INSTALLED UNDER UNIVERSAL AVIONICS SYSTEMS CORP. FAA APPROVED STC SA5072NM, IN AN AIRCRAFT AND CERTIFIED FOR YEA AND IFR NAVIGATION WHICH QUALIFIES THIS INSTALLATION AS A "FOLLOW ON" INSTALLATION PER AC 20-130A THE UNS-ID EMS SYSTEMS HAVE BEEN SHOWN TO MEET ALL OF THE REQUIREMENTS OF AC-20-130A FOR VFR-IFR NAVIGATION ENROUTE, TERMINAL, OVER WATER AND IN REMOTE AREAS, AND FOR NON-PRECISION APPROACHES. THE NO.1 AND 2 EMS SYSTEMS ARE DIGITALLY INTEGRATED TO THE EXISTING HONEYWELL FIVE-TUBE ELECTRONIC FLIGHT INSTRUMENT SYSTEM (EFTS). THE PILOT AND COPILOTS EFIS SYMBOL GENERATOR'S HAVE HONEYWELL SERVICE BULLETIN A21-2000-028 AND THE MULTI-FUNCTION GENERATOR HAS HONEYWELL SERVICE BULLETIN A21-2000429 TO INCORPORATE NON-PRECISION OPS SCALING VIA GAMA ARM 429 LPN INTERFACE WHICH MEETS REQUIREMENTS OF TSO C129A AND AC 20-130A. THE EMS SYSTEMS ARB CROSS-COUPLED TO EITHER THE PILOT OR COPILOT EELS FOR DISPLAY AND NAVIGATION. THE EFTS CONVERTS THE DIGITAL TO ANALOG OUTPUTS AND PROVIDES ALL LATERAL STEERING TO THE AUTOPILOT AND FLIGHT DIRECTOR SYSTEM. VERTICAL NAVIGATION (VNAV) FROM EITHER EMS SYSTEM IS NOT DISPLAYED OR COUPLED IN THIS INSTALLATION. THE FOLLOWING REQUIRED ANNUNCIATORS FOR THE FMS SYSTEMS ARE DISPLAYED ON THE EFTS DISPLAYS: yMS MSG INDICATES A MESSAGE IS TO BE ACKNOWLEDGED ON THE MSG PAGE. (COWR: AMBER) LOCATED ON EADL SELECTED CROSSTRACK IS ACTIVE (COWR: CYAN) LOCATED ON EHSL ZVSI INDICATES WAYPOINT ALERT TWO MINUTES PRIOR TO WAYPOINT IN EN ROUTE MODE, AND 15 SECONDS PRIOR IN APPROACH MODE. WHEN THIS ANNUNCIATOR FLASHES. IT INDICATES THAT AN UPCOMING VERTICAL FLIGHT PATH ANGLE (EPA) CHANGE IS WIT EN TWO MINUTES. (COWR: AMBER) LOCATED ON EHSL AN APPROACH HAS BEEN ACTIVATED. (COWR: CYAN) LOCATED ON EHSL Additional Sheets Are Attached * U.S. G.P.O 1990.781.753 SDNY_GM_02759762 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246684 EFTA01331147 get NOTICE WAY* andbalance or operating limitation changes shall be enteredin the appropriate akcraft recon1 An alteration must be compatible with allprevious alterations Massone continued conformity with the applicable airworthiness requirements. a Description of Work Accomplished Of more space is required attach additional sheets, Identity with aircraft nationality and registration mark and date work accompashed) AIRCRAFT: BOEING, TYPE: 727-31, S/N 20115. DATE: 06/14/2001. W.O. 16236, PAGE 2 OF 2. THE FOLLOWING REQUIRED ANNUNCIATORS WERE LOCATED ON THE EXISTING PILOT AND COPILOT'S INSTRUMENT PANEL ADJACENT TO THE EADI UN/TS: j'MS UDC THE Ems IS IN HEADING SUB-MODE. (COLOR: BLUE) GPS INTRO GPS INTEGRITY IS OUTSIDE OF THE ALLOWABLE LIMIT FOR A PHASE OFFLIGHT (2.0-NM EN ROUTE, 1.0-NM TERMINAL AND APPROACH TRANSITION. AND 0.3-NM FINAL APPROACH SEGMENT). SEE SECTION III, ABNORMAL PROCEDURES. (COLOR: AMBER). THE ADDED ANNUNCIATORS AREDIMMED AND1m tr.O USING THE EXISTING PI OT AND COPILOT ANNUNCIATOR COUPLERS. THESE UNITS HAVE BEEN MODIFIED USING JET AVIATION MODIFICATION NO. 3349-02-1, CAPT. AND FIO ANNUNCIATOR COUPLER MODIFICATION. DATED 04/12101. REFERENCE FAA FORM 8110-3, DATED 05/29O001 BY SYSTEMS AND EQUIPMENT DER NO. DEBT-510087-NM. THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER UNIVERSAL AVIONICS CORP. RETURN TO SERVICE MAINTENANCE AND CHECKOUT PROCEDURES MANUAL NO. 34-60-21, DATED 19 MARCH 2001 WITH NO DISCREPANCIES NOTED. AN EMI TEST, REPORT NO.: B727-16236-080 REV IR, SHEETS I OF 5. DATED 06/19/2001, WAS CONDUCTED AND THE INSTAL 1PD EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.134B, CHAPTER 12. SECTION 3, PARAGRAPH 12- 37 AND AC 43.13-2A. CHAPTER 2 PARAGRAPH 23f. THE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.13-2& CHAPTER PARAGRAPH 3 AND WAS FOUND TO MEET THE REQUIREMENTS OF PARAGRAPH 2. MATERIALS AND PRACTICES COMPLY WITH PARAGRAPHS 4 THROUGH 12. THE ELECTRICAL LOAD ANALYSIS UPDATE REPORT NO. B72746236.041, REV IR, SHEETS I THRU 21. DATED 06/110001 WAS COMPLETED IN ACCORDANCE WITH AC43.13-LB. CHAPTER II, SECTION 3. PARAGRAPH 11-37. AIRCRAFT METAL WORK-INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-1B, CHAPTER 4, SECTIONS 1, 2, 3 AND 4, CHAPTER 6. SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.13-1B, CHAPTER 7. SECTIONS 1- 5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MIL SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43.13-IB, CHAPTER 11, SECTION 4. ELECTRICALJELECTRONIC WIRING WAS SELECTED AND INSTALLED LAW AC43.13-1B. CHAPTER 11. SECTIONS 54, 13, 15. 17-19 AND AC43.13-2A CHAPTER 2, PARAGRAPHS 21,22 & 27. ROUTING. LACING AND TYING COMPLY WITH AC43.134B, CHAPTER IL SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-IB SECTION 16. ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURER'S INSTRUCTIONS AND AC43.13-2A, CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3. PARAGRAPH 44. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THB AIRCRAFT RECORDS TAW AC43.13-IB, CHAPTER 10, SECTION 2 AND AC 43.13-2A, CHAPTER 1 PARAGRAPH 9. MAINTENANCE FOR CONTINUED AIRWORTHINESS AS REQUIRED BY FAR 25.1529 IS DETAILED IN THE UNIVERSAL AVIONICS CORP. UNS-ID FLIGHT MANAGEMENT SYSTEM TECHNICAL MANUAL NO. 34-60-09, DATED AUG 15/97. STRUCTURAL CONTINUING AIRWORTHINESS INSPECTION REQUIREMENTS ARE CONTAINED IN AT.E. INC. STRUCTURAL REPORT ATE6I12001 DATED 6/12/01. SUBSTANTIATED BY FAA. FORM 8110-3 DATED 6/12/01 BY STRUCTURES DER NO. DERT-510333- CE THE REQUIRED FAA. APPROVED FLIGHT MANUAL SUPPLEMENT DOC NUMBER B72746236-100, REV SHEETS 1THRU 9, DATED sone zi, 2co I HAS BEEN INSERTED INTO THE AIRCRAFT FLIGHT MANUAL. END 0 Additional Sheets Are Attached SDNYGlvl_02759763 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246685 EFTA01331148 SDNYGM02759764 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 002466R6 EFTA01331149 t ta, Jet Aviation Associates Ltd. Bldg. 1515 Perimeter Rd. AFM Supplement to Palm Beach Intl Airport The Boeing Company 727-31 West Palm Beach, FL 33406 Serial No. 20115 FAA CRS EYKR782D FAA Form 337 Document No. B727-16236-100 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR BOEING 72741 REGISTRATION NO.: N908JE SERIAL NO.: 70115 WITH DUAL UNIVERSAL:AVIONICS FLIGHT MANAGEME NT SYSTEMS (UNS1-D) INSTALLED ' - This supplement must be attached to the FM approv ed is modified by the installation of dual Universal Avioni Airplane Flight Manual when the airplane cs Management Systems (FMS), with Frequency Manag Systems Corp. (UASC) (UNS-1D) Flight (RTU), receiving navigation inputs from Triple Honey ement via a UASC Radio Tuning Unit well internal GPS sensors, and VOR/DME from the Collins Inertial Reference Sensors (IRS), dual accordance with manufacture's Installation and Check No. 1 and No. 2 VOR/DME systems in out August 15, 1997 or later approved revision and FAA Form Manual No. Rev. 2. dated 337, dated. 7 a 01 The information contained herein supplements or supersedes the basic manual only in those areas listed herein. For limitations, procedures, and perform supplement, consult the appropriate basic Airplane Flight ance information not contained In this Manual. FM Approved: Federal Aviation Administration Flight Standard District Office -17 1050 Lee Wegener Blvd. Ft. Lauderdale, Florida 33315 FAA Approved Date: JUN 2 1 2001 Page 1 of9 SDNY_GM_02759765 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246687 EFTA01331150 a' SDNY_GM_02759766 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246658 EFTA01331151 May-29-01 01:59P N C 352 243 1011 P . 06 voinameNTOPTRASSIOATATION DAT I MOM ASA110). Ammoniac". STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS 05/29/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Alalant Para Hamra. at) NAME OF APPLICANT Jet Aviation Associates Booing 72741 Airplane West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B727-16236-293, Initial Release, FLIGHT MANAGEMENT SYSTEM RADIO TUNING UNIT dated 04/16/01 8727-16236-41D, Initial Release, NO. 1 FLIGHT MANAGEMENT SYSTEM dated 04110/01 B727-16236-411, Initial Release, NO. 2 FLIGHT MANAGEMENT SYSTEM dated 04/15/01 3349-02-1, Initial Release, dated CAPT AND 1/0 ANNUNCIATOR COUPLER MODIFICATION 04/12/01 PURPOSE OF DATA In support of major alteration to Boeing 727-31. sedal number 20115, registration number N908JE APPLICABLE REQUIREMENTS (List specific sections) FAR 26.581 (a)(b)(1) FAR 26.1329 (h) FAR 25.1529 FAR 25.869 (a)(4) FAR 25.1351 (a) FAR 25.1581(40)(d) FAR 26.1301 (a)(b)(c)(0) FAR 26.1357 (a)(c)(d)(e) FAR 25.1309 (a)(b)(c)(d)(e)(g) FAR 25.1381 (a)(b) FAR 25.1322 (b)(c) FAR 26.1431 (a)(b)(c) CERTIFICATION - v.a,...a,,•17.4 .7 and. a a. ass iitnien,4 Igiatoed•bee.iditattynesol t.a.......r..".+0•ni...I., Owl Meth.(us. ssiiiii Ansis•A W.Lowmsg.... ...as 6,......k..., NONE s....•........d ...fa... win, intAL•Spepnmlurnied lived i• ace,.kntvh,Mt •nimn..... a a• F•4• 0 A.,•••••• *nubbin. 0 Flasemesliapprost el Sac data I (at)Tbertfore 7 SlOGVIV, i 5icons b la g amnatn.antrA Apron that dab (E)Tterat & Equips's( Aspect. Daip Appeal Oa).Das Nee Ontstilin losullsks A pp sus') oraranion NPOrita) DERT-510087-NM OASSIPICATWOCLI Systems & Equipment rt a No an J. n (I I40)5UPERSEDES PRIMUS EDITION OPOSOI4l3 FILENAME SC-721.INISDOC SDNY_GM_02759762 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00246689 EFTA01331152 " SDNYGM02759768 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246690 EFTA01331153 DEPARTMENTOF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS June 1, 2001 AIRCFLAPT OR AIRCRAFT COMPONENT IDENTIFICATION - - PARE N one. Ramo. Hoicopter. et) MMIE (TrARTLTONT Boeing 72731 Airplane Jet Aviation Associates- WPB UST OF DATA IDENTITICATION • TRIO B727-16236-1261 AT-855/RTA680 Antenna Installations, Sht.1-7, Rev A 5727-16236-1410 Dual FMS W/ RTU Equipment Installations, Sht 1-6, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to sen.rice by FM authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 72731, S/N: 20115 APPUCABLE REQUIREMENTS Mist spec* semen,/ FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.601 25.603 25.605(a) 25.609 25.611 25.613 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance vAth conditions and En:nations of appointment under Part 183 of tho Federal Aviation Regulations, data listed above and on attached sheets numbered 0 have been examined In accordance telthestabrished procedures and found to comply with applicable requirement. of be Federal Aviation Regulations. Recommend approvalc/ wise data. I 441 Riergere Moroi, mandate. SIGNA fURE(S) OF DESIGNATED ENRNEERING PIPRESEttfARVE(S) DESIGNATION mastitis/ I CLASSSICATION(S) David E. Haralson DEC. 14,-.4..__ DERT-810028-NE Structural FAA Form 8110-311140) SuPERNOE3PREVCCOS ENRON EA01202.4“ SDNYGIvl_02759769 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024669I EFTA01331154 SDNYGM02759770 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246692 EFTA01331155 U.S. DEPARTMENT OP TRANSPORTATION DATE FEDERAL AVIATION ADMMISTATION June 18,2001 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MARE MODEL TYPE Oilf.l.e.ithlis &Avner. oat.) NAME OF APPLICANT Boeing B727-3I Airplane Jet Aviation LLST OF DATA IDENTIFICATION MLR Jet Aviation GPS Antenna Installation Engineering Drawing Betting B727-31, N908.1E, SIN 20115 No. B727-162364441, END END END END END END END END Dtd. 5/29/2001, Rev. A Note: The certification basis of this aircraft Includes FAR 2.5.571 Damage - tolerance and fatigue evaluation of structure. Per Advisory Circular 25.1529-1 Instructions for Continued Airworthiness of Structural Repairs on Transport Category Airplanes, the damage tolerance and fatigue evaluation of E.ND END the structure must be performed before 6/182002. . . Notes: 1) The structural aspects only of this above listed data are approved herein. 2) This approval is valid for the aircraft model and serial number listed below 3) This approval is based on structural analysis on file at DER Service: corporate office in Ft. Lauderdale, FL. Model No. B727-31 Serial No. 20115 PURPOSE Approve data for antenna Installation (Structures Only) OF DATA APPLICABLE REQUIRMENTS anrspea TIC SECTIOM) 25.301,25.303, 25305, 25.307, 25.601,25.603, 25.605, 25.609, 25.613 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with condition and limitations of appointment under Part 163 of the Federal Aviation Rerulations, data listed above and on an ached sheets numbered have been examined In accordance with establisbed procedures and found to comply nith applicable requirements of the Federal Aviation Regulations. O Recommend approval of these data I (We) Therefore pi Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) Robert J. Belgau DEBT-510024-CE Structures FAA FORM 81103 (11-70) SUPERSEDES PREVIOUS EDMO N DER SERVICES PROJECT NO. 2001-082 SDNY_GIvl _02759771 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246693 EFTA01331156 SDNY_GM_02759772 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246694 EFTA01331157 Form Approved O s MAJOR REPAIR AND ALTERATION OMB No.2120-0020 . usCrow:men (Airframe, Powerplant, Propeller, or Appliance) For FM Use On a TranspartatIon Fhiaia1 /Melon Office Identification Adtallfigtetrn 5O- FcDo- / 7 e g INSTRUCTIONS: Print or typo all entries. See FAR 43.9 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for 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 51.000 for each such violation (Section 901 Federal Aviation Act el 1958). Make Model BOEING 727-31 1. Aircraft Serial Na Nationality end Registration Mark 20115 U.S.A. N9OSJE Name (As shown on registration certificate) Address (As sham on regisuatlon certificate) 2. Owner MOE INC. 103 POUIX RD. STE 202 WILMINGTON DE. 19803-3742 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 POW ERPLANT PROPELLER Typo APPLIANCE Manufacturer %., 6. Conformity Statement A. Agency% Name and Address B. Kind of Agency C. Certificate No. U.S. Certified Mechanic CRS BYKR7S2D JET AVIATION ASSOCIATES LTD. Foreign Certified Mechanic AIRFRAME 1,3. 1515 PERIMETER RD. X Certificated Repair Station RADIO 1,2,3. WEST PALM BEACH. FL. 33406 — Manufacturer LIMITED ME et ENG. 0. 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 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 7/2/01 DX IO. CC v •-•"' John K Urso. inspector. 7. App oval for Return to Service Pursuant to the authority given persons specified below, the unit dentified in Item 4 was inspeoeed in the manner prescribed by the Administrator of the Federal Aviation Administration and is 0APPROVED IC REJECTED FAA FIL Standards Other (Specify) Manufacturer Inspection Authorization inspector BY Person Approved by Transport FM Designee X Repair Station Canada Airworthiness Group Date of Approval or Rejection Certificate or Signature of Authorized Individual S t a pp Designation No. 72/01 EYICR782D Ronald K. Bystrom. Manager Quality Ass FAA Form 337 (1248) SDNY_GM_02759773 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246695 EFTA01331158 NOTICE • II 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 andregistration mark and date work accomplished.) BOEING 727-34 SMI 20115, N9081E, W/O 16236. INSTALLED 2 EA NEW GARMIN GPS ANTENNAS P/N 011-00134-00 CI29A). I EA AT FUSELAGE STATION 2844, BL 0.0. AND 1 EA FUSELAGE STATION 9343 RBL 4.56, PER JET AVIATION DRAWING B727-16236-1413, REV IR. DATED 6/5/01 TITLED-DUAL AUXILIARY GPS ANTENNAS INSTALLATION. REF F.A.A. FORM 8110.3 DATED 6/6/01 BY STRUCTURES D.E.R. NO. DERT-510394- CE. AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-IB, CHAPTER 4, SECTIONS 1, 2, 3 AND 4. CHAPTER 6. SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.13-1B. CHAPTER 7, SECTIONS I- 5 AS APPLICABLE CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE ME. SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43.1340. CHAPTER I I, SECTION 4. ELECTRICAL/ELECTRONIC WIRING WAS SELECTED AND INSTALLED TAW AC43.13-1B, CHAPTER IL SECTIONS 5.8, 13. 15. I7-19 AND AC43.13-2A CHAPTER 2. PARAGRAPHS 21.22 & 27. ROUTING. LACING AND TYING COMPLIES WITH AC.43.13-1B. CHAPTER IL SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-1B SECTION 16. ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURER'S INSTRUCTIONS AND AC43.I3-2A, CHAPTER 2. PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3. PARAGRAPH 44. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTOTHE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS TAW AC43.I3-1B, CHAPTER 10, SECTION 2 AND AC 43.13-2A. CHAPTER 1 PARAGRAPH 9. MAINTENANCE FOR CONTINUED AIRWORTHINESS IS CONTAINED IN ENGINEERING REPORT IMER-836. REV Ut, DATED 6/10101. REFERENCE FAA FORM 8110-3 DATED 6/11/01 BY STRUCTURES DER NO. DERT-510394-CE. THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES DUE TO THIS MODIFICATION. END ❑ Addidonel Sheets Are Attached * U.S. G.P.O 1990.761.753 SDNY_GIvl_02759774 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA (1)246696 EFTA01331159 ASK CUBIYUS 002 -- • 1/2. DEBARTDLENT OP TRANSPORT ATION PEP AL AVIATION ADSTINSTRATION DATE STATEMENT OF COMPIIA NCE WITH THE FEDERAL AVIATION REGULA TIONS Tune 6, I001 AIRCRAFT OR AIRCRAFT MAKE COMPONENT ID&MI7CAT MODEL. NO. IGN TYPE (Alvaro. Radio, Nolkod •ocr. ac.) NAME OP ArnycANT ROPING' FTT77-1I Airplane __ In Ayrto/Iim ~crib LIST OP DATA bed...1 to IDENTIFICATION TITLE B727-162361413 OR DRAWING - Sbeets I - 3 (615101) DUAL AIDOLIARY GPS ANTENNAS INSTALLATION NOTE: Approval for the sat:cm:al aspects relaxed to the above design data will be covered by a separate Form 8110-3 which will be issued for bbd Proof of and will include required inspe SIG/4401e ction item® to «are COni associated with this modification. Meal Airwor1DVIedb END END END PURPOSE OF DATA To provide a record of design appro val of the above data applicable to for manofactaring and conformity 8127-31, SIN 20115, Rog/McGinn No. . See NOTE above. N9081E. APPLICABLE REQ<JDMIL NTS (Lin spxilic atakos) FAR 25.6601 FAR 25.609 FAR 25.603 FAR 25.611 FAR 25.605 FAR 25.613 altT/F7CATION . Under antoriry bested by direction of inc AM...Mira:a brat men =Art port ILO of etc PoSinl Abiado In doconlanco with wodåaoro and Idnion o Ittdob ' oorn. dart figs atom sad on om or ext=6ed hb nordariloth earth *wart/ gran tonehored !~ pc:adorn and found ob tomfly bin!) ‘opikabk reoblretbents of Or )ØAblati WA Wm teen on Redubtims. 1(IX) 7banfoto D Recommend approval of obese dart X Amore them dim (Sac NO113 above) SIONKIW(S) OP DESIGNATED REPRZSENTAIITVEIS) DEDGNA170N NUADLER(S) CLASSIFICATION(S) C2 / 9 2 , $-C.C‘ DERT - 510394 - CE STRUCTURES (10. TILB -11/4-4C4Fnm• Kaman W. Damp= FAA Form 8110.3 (11-70) SLIPE12SEDES PREVIOUS EDITION shed 1 of SDNY_GM_02759775 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246697 EFTA01331160 SDNYGNI02759776 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246698 EFTA01331161 U.S. DEPARTMENT OF TRANSPORTATION DATE ' FEDERALAVIATION ADMINISTRATION , STATEMENT OF COMPLIANCE WITH 171E FEDERAL AVIATION REGULATIONS June 11, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENITEICAT/ON MAKE MODEL NO. TYPE (Ainittne. Radio. Helicopter. etc.) NAME OF APPLICANT PORING 8727-11 AIRPLANE _ JeLAyiltion Assneisted Ltd LIST OF DATA IDENTIFICATION 1TTLE ENER-836 IR ENGINEERING REPORT — Dated 06/10/01 STRUCTURAL SUBSTANTIATION - DUAL AUXILIARY GPS ANTENNA INSTALLATION ON A BOEING B727-31 AIRCRAFT, S/N 20115 NOTE: The operator of B727-3I aircraft S/N 20115 modified by drawing B727-16236-1413 dated 6/5/01 issued at no revision, is required to incorporate in the Airworthiness Limitations Section of the Instructions for Continued Airworthiness applicable to the eriwing MaimVnanrA Program, an inspection item at a frequency not to exceed 3700 flights to detect signs of distress (0.25 inch or smaller crack and/or working rivets) common to the GPS antenna installation as detailed in drawing 8727-16236-1413. Refer to FAR PART 25 Appendix H and Report JMER-836 IR page 4.1 (CONCLUSIONS) for instructions. PURPOSE OF DATA To provide a record of design approval of the above data as applicable to 8727-31 S/N 20115 and to show compliance to the following FAR's: APPLICABLE REQUIREMENTS (List sped& sermons) FAR 25.301 FAR 25.307 FAR 25.605 FAR 25.613 FAR 25.303 FAR 25.571 FAR 25.609 FAR 25.625 FAR 25.305 FAR 25.603 FAR 25.611 CERTIFICATION - Under authority vested by direcdon of the Adminittnuor and in accords= with condidons and limitations of appohmornt under part IS3 of the Faders! Aviation Regulations. dam tined above and on Matched sheds cumbered N/A have been examined in accordance with established procedures and found to comply with applicable reqeirements of the Federal Aviation Regulations. I (k) Therefore O Recommend approval of these data X Approve these am (Structural aspects only) ' SIONATURE(S) OF DESIGNATED REPRESENTATIVE(S) DESIGNATION NUM:KRIS) CLASSIPICATION(S) 9(1 44 ,1fell 10- 0. 1A , 7,4 -/- 44--. DERT - 510394 - CE . STRUCTURES Kenneth W. Thompson .. FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION sheet I of I SDNY_Ghl_027597 7 7 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246699 EFTA01331162 SDNYGNI02759778 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246700 EFTA01331163 Form Approved 0 j MAJOR REPAIR AND ALTERATION OMB No. 2120-0020 tIS Depentrant d Tronsoortatloi (Airframe, Poworplant, Propeller, or Appliance) For FAA Use Only Faint Aviation Office identification MmIntetnitca INSTRUCTIONS: Print or type all entries. Soo FAR 43.9 Appendix B. and AC 43.9-1 (or subseque t revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can re tilt in a civil penalty not to exceed 31.000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model BOEINO 727-31 1. Aircraft Serial No. Nationality arid Registration Mark 20115 U.S.A. N908JE Name (As shown on registration certificate) Address (As shovwn on registration certificate) 2. Owner JEGE INC. 103 FOULK RD. STE 202 WILMINGTON DE. 19803-3742 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. COS:tate No. U.S. Certified Mechanic CRS EYICR782D JET AVIATION ASSOCIATES LTD. Foreign Certified Mechanic AIRFRAME 1,3. 1515 PERIMETER RD. x Certificated Repair Station RADIO 1.2,3. WEST PALM BEACH. FL 33406 — Manufacturer LIMITED A/F & ENG. 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 heroin Is true and correct to the best of my knowledge. Date Signature of Authorized Inane u 7201 John K. Urso. Inspector. ie.•(.4—e-- 7. Approval for Return to Servl Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner proscribed by the Administrator of tho Federal Aviation Administration and is ISI APPROVED 0 REJECTED FM FIL Standards Other (Specly) Inspector Manufacturer Inspection Authorization BY Person Approved by Transport FM Designee X Repair Station Canada Alnyczthiness Group Date of Approval or Rejection Certificate or SignatureBysofAuthorized Individual Designation No. 717/01 EYKR782D Resale K. trom. Managa Quality Asnses FAA Fenn 337 (124el SDNY_GM_02769779 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024670 I EFTA01331164 NOTICE • Weight andbalance or operating lirOalion changes shall be entered in the appropriate aircraft record. An alteration must be compatible with elfpvvious afteratione to assure continued conformfty WM the applicable alnyorthiness requirements. & Description of Work Accomplished Of more space is required, attach additional sheets, Idea* with aircraft nationaltly andregistration mark and date work acconplished) BOEING 727-31. SIN 20115. N908.TE. W/O 16236. INSTALLED A NEW KGS ELECTRONIC MODEL UC-28-14, 28 VDC TO 14 VDC CONVERTER AND THREE POWER OUTLETS IN THE COCKPIT IN ACCORDANCE WITH KGS ELECTRONIC MODEL UC-28-14 INSTALLATION MANUAL AND ADVISORY CIRCULAR 25-10 (INSTALLATION OF MISCELLANEOUS NON REQUIRED ELECTRICAL EQUIPMENT) USING THE FOLLOWING JET AVIATION DRAWINGS SUBSTANTIATED BY F.A.A. FORM 8110-3 RESPECTIVELY WIRING DRAWING: • B727-16236-352, REV IR, DATED 5/25/01, SHEETS I & 2. TITLED - 28-14 VDC CONVERTER WIRING DIAGRAM. REFERENCE F.A.A. FORM 8110-3 DATED 6/7/01 BY SYSTEMS AND EQUIPMENT DER NO. DERT-510087-CE. STRUCTURAL DRAWING: • B727-16236-1352. REV IR, DATED 06/01, SHEETS 1THRU 5, TITLED - 28-14 VDC CONVERTER EQUIPMENT INSTALLATION. REFERENCE F.A.A. FORM 8110-3 DATED 6/10/01 BY STRUCTURES DER NO. DERT-810028-NE. THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER KGS ELECTRONIC MODEL UC-28-14 INSTALLATION MANUAL WITH NO DISCREPANCIES. AN EMI TEST, REPORT NO.: B727-16236-080 REV IR, SHEETS 5. DATED 06/19/01 WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.13-IB. CHAPTER 12. SECTION 3, PARAGRAPH 12- 37 AND AC 43.13-2A, CHAPTER 2 PARAGRAPH 23f. THE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.13-2A, CHAPTER 1. PARAGRAPH 3 AND WAS FOUND TO MEET THE REQUIREMENTS OF PARAGRAPH 2. MATERIALS AND PRACTICES COMPLY WITH PARAGRAPHS 4 THROUGH 12. THE ELECTRICAL LOAD ANALYSIS UPDATE REPORT NO. B727-16236-041. REV BL SHEETS 1 THRU 21, DATED 001112001I WAS COMPLETED IN ACCORDANCE WITH AC43.13-IB. CHAPTER I I, SECTION 3. PARAGRAPH 11-37. AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-IB, CHAPTER 4. SECTIONS 1. 2. 3 AND 4, CHAPTER 65 SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.13-IB, CHAPTER 7, SECTIONS 1.5 AS APPLICABLE. CIRCUIT BREAKERS. SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MIL SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43.13.IB. CHAPTER II. SECTION 0. ELECTRICAL/ELECTRONIC WIRING WAS SELECTED AND INSTALLED TAW AC43.13.IB, CHAPTER II. SECTIONS 5-8. 13. 15. 17.19 AND AC43.13-2A CHAPTER 2, PARAGRAPHS 21,22 & 27. ROUTING, LACING AND TYING COMPLIES WITH AC43.13-1B. CHAPTER II, SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-1B SECTION 16. ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURERS INSTRUCTIONS AND AC43.I3.2A. CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3. PARAGRAPH 44. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS TAW AC43.13-1B. CHAPTER 10, SECTION 2 AND AC 43.13-2A, CHAPTER 1PARAGRAPH 9. THERE IS NO CHANGE TO THE MANUFACTURERS MAINTENANCE FOR CONTINUED AIRWORTHINESS DUE TO THIS MODIFICATION. THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES DUE TO THIS MODIFICATION. END ❑ Additional Sheets Are Attached * V.S. G.P.O 1990-781.753 I SDNY_Gtol_02759780 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246702 EFTA01331165 a DIMItTMENTOF TPANSPOlTATION FEDIDlel. AVIATION ACIaltillSTPATION DATE STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS 06/07/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane. Radio, Reliever. de) NAME OF APPLICANT . Jet Aviation Associates Boeing 727-31 Airplane West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B727-16236-352, Initial Release, 28-14 VDC CONVERTER WIRING DIAGRAM dated 05/25101 B727-16236-580, Initial Release, CABIN NO. 2 60 Hz SYSTEM dated 05/25/01 8727.16236-600, Initial Release, SPARE WIRING (PROVISIONS) dated 05/25/01 PURPOSE OF DATA In support of major alteration to Boeing 727-31, serial number 20115, registration number N908JE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.869 (a)(4) FAR 25.1353 (a)(b) FAR 25.1301 (a)(b)(c)(d) FAR 25.1357 (a)(c) FAR 25.1309 (a)(b)(g) FAR 25.1431 (a)(b)(c) FAR 26. 1322 (b) FAR 25.1529 FAR 25.1351 (a) CERTIFICATION - thid.,....iumy void by dirstdoe a the Adaishirlase unt ha accentuate oh* fl atness and inaniadas Mappaianium wider Pan HU gar Fatal Mist.. Fteentaitoss atata Wet obeys W.. musing 'Neu mowed NON? hen We. maws Is accordance one esuatetstod smears e•O roma inesply eta nvikak Repladoes ...mono trim room Aaiun* ❑ ReC040Mend Approval of these data I (We)fberefore a Approve Mete data (Systems & Edoiproatt Aspects. Desiga Approval Only. Does Not Constitute lostalls doe Approval/ SIGMA tit PORESEXPATIST(S) DESIGNATION NUMMER(S) CLASSIFICATIONS) DERT-510087-NM Systems & Equipment o an J. ran FAA Form 8110-3 I-70)SUPERSEDES PREVIOUS EDMON ORO 901413 F/LIDUMIESD-727•CAD•PWR.DOC SDNY_GM_02759781 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246703 EFTA01331166 SDNY_GM_02759782 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246704 EFTA01331167 OEPARIMENT OF TRANSPORTATION OAR FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS June 10, 2001 AMMAR OR ANICRAFT COMPONENT IDENTIFICATION MANE MODEL NO. TYPE (Neer* Raba. Kelomtmetc.) NAME Cf APPUCANT Boeing 727-31 Airplane Jet Aviation Associates- WPB LIST OF DATA IDENI1FICATION iTILE 8727-16236-1352 28-14 VDC Converter Equipment Installation, Sht 1-5, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval Is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA authorized personnel. C PURPOSE Of DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REQUIREMENTS Wemonde sccdoes) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.601 25.603 25.605(a) 25.609 25.611 25.613 CERTIFICATION - Under authority vested by direction of the AdministnEcc and in accordance With OX4100t19 and Iota lons of appointment under Pal 183 of the Federal Aviation Replationsidata wee above and on attached sheets numbered 0 have been examined In accordance wall established procedures and found lo comply Wei applicable requirements of the Federal Aviation Regulat OM. ❑ Recemmend approval of :nese data. I (X Therefore OLaJI Approve ace date. SIGNATURE(S)OF DESIGNATED EN3INEERING REPRESENTATIVE(S) OES:ONATON NUMBER(S) CIASSWICATIONISI David E. Haralson 1:7O-ecr. N0,01.-- DERT-810028-NE Structural onn 8110-3 (1140) = SIeseK¢ PREWOUS EDITION r • SDNY_GM_02759783 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246705 EFTA01331168 SDNY_GM_02759784 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246706 EFTA01331169 Form Approved 0 MAJOR REPAIR AND ALTERATION OMB No. 2120-0020 us osiiiiviva For FAA Use Only es Trr, (Airframe, Poworplant, Propeller, or Appliance) Office Identification Federal swum annifinninion 50- r5Do-i7 afif INSTRUCTIONS: Print or typo all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequo I revision thereof) for I 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 51,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model BOEING 727-31 1. Aircraft Serial No. Nationality and Registration Mark • 20115 U.S.A. N908JE Name (As $1701471 on registration certificate) Address (As shown on registration certificate) 2. Owner JEGE INC. 103 FOULK RD. STE 202 WILMINGTON DE. 19803-3742 —, 3. For FAA Use Only 4. Unit Identification 5. Typo Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER Typo APPLIANCE Manufacturer ,.. 6. Conformity Statement A. AgencYs Name and Address B. Kind of Agency C. Certificate No. U.S. Certified Mechanic CRS EYKR782D JET AVIATION ASSOCIATES LTD. Foreign Certified Mechanic AIRFRAME 1,3. 1515 PERIMETER RD. X Certificated Repair Station RADIO 1,2,3. WEST PALM BEACH. FL. 33406 Manufacturer LIMITED MP & ENG. 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 Authorized Incavklual 7/2/0I John K. tine. Inspector. N....“...._, 7. Approval for Return to Servl Pursuant to the authority given persons specified below, the unit dentified In item 4 was erected In the manner prescribed by the Administrator of the Federal Aviation Administration and is El APPROVED El REJECTED FAA Flt. Standards Other (SPecifY) Manufacturer Inspection Authorization Inspector BY Person Approved by Transport FAA Designee X Repair Station Canada Airworthiness Group — Date of Approval or Rejection 712/01 Certificate or Designation No. EYKR782D Signature of Authorized Individual Ronald K. Bystrom. Manager Quality ASSWIDC eligig -c -, FAA Form 337 ozem SDNY_Glvl_02759785 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246707 EFTA01331170 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft recant An alteration must be compatible with aft 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 accomplished) BOEING 727-31, S/N 20115, N9081E. W/O 16236. INSTALLED A UNITRON 60 HZ CONVERTER P/N PS-62-66D AND 26 EA CABIN °MUTTS PER UNITRON 60 HZ CONVERTER INSTALL MANUAL NO. PS-62-66D-6. THIS MODIFICATION WAS ACCOMPLISHED PER THE FOLLOWING JET AVIATION DRAWINGS WHICH ARE SUBSTANTIATED BY F.A.A. FORM 8110-3 RESPECTIVELY WIRING DRAWING• • B727-13236-580, REV IR, DATED 5/25/01, SHEETS I THRU 5, ITILED -CABIN NO. 2 60 HZ SYSTEM REFERENCE FAA FORM 8110-3 DATED 6/7/01, BY SYSTEMS & EQUIPMENT DER. NO. DERT-510087-NM. STRUCTURAL DRAWINGS: • B727-16236-1580. REV IR. DATED 911/01, SHEETS 1 THRU 7. TITLED - CABIN NO. 2 60 HZ EQUIPMENT INSTALLATION. REFERENCE F.A.A. FORM 8I10-3, DATED 6/13/01, BY STRUCTURAL D.E.R. NO. DERT-810028-NE AN EMI TEST, REPORT NO.: B727-16236080 REV IR. SHEETS 5, DATED 06119/01 WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.B-1B, CHAPTER 12, SECTION 3, PARAGRAPH 12- 37 AND AC 43.I3-2A, CHAPTER 2 PARAGRAPH 23f. THE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.13-2A, CHAPTER I, PARAGRAPH 3 AND WAS FOUND TO MEET THE REQUIREMENTS OF PARAGRAPH 2 MATERIALS AND PRACTICES COMPLY WITH PARAGRAPHS 4 THROUGH 12. TEE ELECTRICAL LOAD ANALYSIS UPDATE REPORT NO. B727-16236-041, REV IR. SHEETS 1 THRU 21. DATED 06/11/2001 WAS COMPLETED IN ACCORDANCE WITH AC43.13-1B. CHAPTER 11, SECTION 3, PARAGRAPH 11.37. AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-I B. CHAPTER 4, SECTIONS I. 2. 3 AND 4, CHAPTER 6, SECTIONS 3 AND & HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.13-1B, CHAPTER 7, SECTIONS I- 5 AS APPLICABLE CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MIL SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43.13z It CHAPTER II. SECTION 4. ELECTRICAL/ELECTRONIC WIRING WAS SELECTED AND INSTALLED TAW AC43.13-I B, CHAPTER I1. SECTIONS 5-8. 13, 15, 17-19 AND AC.43.13-2A CHAPTER 2, PARAGRAPHS 21, 22 & 27. ROUTING. LACING AND TYING COMPLIES WITH AC43.13-1B, CHAPTER I I, SECTIONS 9.12 WIRE MARKING COMPLIES WITH AC43.13- I B SECTION 18 ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURER'S INSTRUCTIONS AND AC43.I3-2A. CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3. PARAGRAPH 4t A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS TAW AC43.13-1B, CHAPTER 10. SECTION 2 AND AC 43.13-2A, CHAPTER 1 PARAGRAPH 9. THERE IS NO CHANGE TO THE MANUFACTURERS MAINTENANCE FOR CONTINUED AIRWORTHINESS DUE TO THIS MODIFICATION. THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES DUE TO THIS MODIFICATION. END ❑ Additional Sheets Are Attached * U.S. G.P.O 1990-781-763 SDNY_Glvl_02759786 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246708 EFTA01331171 DEParkitIT Of TRANSPORTATION floN DATE STATEMENT OF COMPLIANCE WIATIA THE FEDERAL lw" AVIATION REGULATIONS 06/07/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio. Helicopter, etc) NAME OF APPLICANT Jet Aviation Associates Boeing Airplane 727-31 West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B727-16236-362, Initial Release, 28.14 VDC CONVERTER WIRING DIAGRAM dated 05/25/01 B727-16236-580, Initial Release, CABIN NO. 2 60 Hz SYSTEM dated 05/25/01 8727-16236.600, Initial Release, SPARE WIRING (PROVISIONS) dated 05/25/01. • PURPOSE OF DATA In support of major alteration to Boeing 727-31, serial number 20115. registration number N908JE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.869 (a)(4) FAR 26.1363 (a)(b) FAR 26.1301 (a)(b)(c)(d) FAR 25.1357 (a)(c) FAR 25.1309 (a)(b)(g) FAR 25.1431 (a)(b)(c) FAR 25. 1322 (b) FAR 26.1629 FAR 25.1351 (a) CERTIFICATION - orma.o.lts mud by &yaks of Ot Adalek*In satIlkliftenbeke kith cort4kMes nil Speknikee of app•Satewst nier nn is, ktOt Eaten. AWila. Reg...kink data Estal •bekt and us shucked gnu eakend NONE kin bent *maimed to makrtfrate with klalksberd prikkluils sad bask ki on*, Rekalidea kid. kpplkabk ',eineme of thit Etkeni MOS, O Recommad approval albeit dam I (We) 7Iterefore F2 Appieve these data (Systems & Equipment Aspects, Deign Approval Only. Des Not Constitute hatallatioa Approval) =NATE osnusorrAnYtm orsictunon NUMBEATO CASSIOCATIONIO lne-O--. DERT-510087-NM Systems & Equipment No an J. an AA Form 8110-3 I-70)SUPERSEDES PREVIOUS WTTON GPO 901-613 sun. SC-72LCAB-PWR In SDNYGlvl_02759787 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246709 EFTA01331172 SONY GM 02759788 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246710 EFTA01331173 a DATE DEPARTMENT Cr TRANSPORTAPON FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS June 13, 2001 NRCRAFT OR AIRCRAFT COMPONENT ICENTIPICATON FAKE MODEL NO. TYPE (Airplane. Radio. ireaoretexem) NAME OF APPLICANT Boeing 727-31 Airplane Jet Aviation Associates- WPB LIST OF DATA IDENTIFICATION TITLE B727-16236-1580 Cabin #2 60 Hz Equipment Installation, Sht 1-7, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA authorized personnel. C PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REOUIRFJJENTS Mkt speedo sealsrei FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.601 25.603 25.605(a) 25.609 25.611 25.613 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appoinreere under Past 183 of the Federal Aviation Regulalrentdsita Ested above and on attached sheets numbered 0 have been examined In accordance with testae:I:had procedures and found to comply with eppdcatte reqthements of the Federal AVAtrall Regulations. Gootameed aPPIWal of these data i(X Thereon Altera.* Dm data. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRF-SF-IITATIvE(S) DESIGNATION NUMBER(S) CLASSIFICATIONS) David E. Haralson Pmde. /10,./...- DERT-810028-NE Structural oan 8110-3 iii40)SUPERSE0tty names tornat EJI01210.6ac SDNYGlvl_02759789 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002467 I I EFTA01331174 SDNYG1,102759790 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246712 EFTA01331175 Form Approved ' ID MAJOR REPAIR AND ALTERATION OMB Na 2120-0020 usDepinsta (Airframe, Poworplant, Propeller, or Appliance) For FAA Use 0i)ly 01TrerwolaWn Firdnil *Nam sinumersoon Office Identification c0— /-57jO- INSTRUCTIONS: Print or typo all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for 'nal 17 e- ta ens and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can ro ult In a civil penalty not to xceod 81.000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model BOEING 727-31 1. Aircraft Serial No. Nationality and Registration Mark 20115 US.A. N9O&TE Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner MGR INC. 103 FOULK RD. STE 202 WILMINGTON DE. 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AJRFEAME (As described in Item 1above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer 8. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate Na U.S. Certified Mechanic CRS EYKR782D JET AVIATION ASSOCIATES LTD. Foreign Certified Mechanic AIRFRAME 1,3. 1515 PERIMETER RD. X Certificated Repair Station RADIO 1,2,3. WEST PALM BEACH. FL 33406 Manufacturer LAMED MP & ENG. 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 knovetedge. Dale Signature of Authorized Individual 7/2/01 John K. Urso. Inspector. 7. Approval for Return to Service Pursuant to the authority given persons specified bedew, the unit &sniffled in item 4w inspected in the manner prescribed by the AdrrdnIstrator of the Federal Aviation Administration and is .7J APPROVED O REJECTED Other (Specity) FAA Fit. Standards Manufacturer Inspection Authorization Inspector BY Person Approved by Transport FM Designee X Repair Station Canada Airworthiness Group Date of Approval or Rejection Certificate or Signature of Authorized Individual Designation No. 7/2/0I EYKR782D Ronald K. Bysirom. Manager Quality FAA Form 337 0248> SDNY_GM_02759791 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002467 I 3 EFTA01331176 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be avowable with allprevious alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more spaceIs required attach additional sheets, Identify with aircraft nationality andregistration mark and date work accompffshed) BOEING 727-31, S/N 20115. N9083E. W/O 16236. INSTALLED AN AIRCELL ATG.01 FLIGHT PHONE SYSTEM CONSISTING OF AN ANTENNA PIN CI-5O30, A TRANSCEIVER PIN 900002-2, and AN ANTENNA MATCHING UNIT P/N 83518, 4 EA HANDSETS P/N 440-10035-001 AND 4 EA HANDSET CRADLES P/N 400-10038-001. THESE MODIFICATIONS WERE COMPLETED USING THE FOLLOWING JET AVIATION DRAWINGS, WHICH ARE SUBSTANTIATED BY FAA 8110-3 FORMS RESPECTIVELY: WIRING DRAWING• • B727-13236-330, REV. 111, DATED 4/30/01, SHEETS I THRU 3. TITLED- AIRCELL ATO.01 AIR /GROUND TELEPHONE REFERENCE FAA FORM 8110.3 DATED 5/29/01, BY SYSTEMS & EQUIPMENT D.ER. NO. DERT-510087-NM. STRUCTURAL DRAWINGS AND REPORTS: • B727-16236-I330, REV. A, DATED 529/01, SHEETS 1 THRU 4, TITLED- AIRCELL ATG.01 AIR I GROUND TELEPHONE ANTENNA INSTALLATION REFERENCE FAA FORM 8110-3, DATED 6/18/01, BY STRUCTURAL D.E.R. NO. DERT-510024-CE. • B727-16236-1331, REV. IR, DATED 5/24/01, SHEETS 1THRU 6. -WILED -AIRCELL EQUIPMENT INSTALLATION REFERENCE FAA. FORM 8110-3, DATED 6/3/01, BY STRUCTURAL D.ER. NO. DERT-810028-NE. THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER AIRCELL ATG.01 FLIGHT PHONE SYSTEM INSTALLATION MANUAL REV IL DATED 611I/99 WITH NO DISCREPANCIES. AN EMI TEST, REPORT NO.: B727-16236-080 REV IR, SHEETS 5. DATED 06/19/01 WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.13-1B, CHAPTER 12, SECTION 3, PARAGRAPH 12- 37 AND AC 43.13.2A, CHAPTER 2 PARAGRAPH 23f. THE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.I3-2A, CHAPTER I, PARAGRAPH 3 AND WAS FOUND TO MEET THE REQUIREMENTS OF PARAGRAPH 2. MATERIALS AND PRACTICES COMPLY WITH PARAGRAPHS 4 THROUGH 12. THE ELECTRICAL LOAD ANALYSIS UPDATE REPORT NO. B727-16236-041, REV IR, SHEETS 1'MU 21, DATED 06/11/2001 WAS COMPLETED IN ACCORDANCE WITH AC43.13-18, CHAPTER II, SECTION 3. PARAGRAPH 11.37. . AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-1B, CHAPTER 4, SECTIONS 1, 2, 3 AND 4. CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.I3-1B, CHAPTER 7. SECTIONS I- 5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MIL SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43.13-IB, CHAPTER 11, SECTION 4. ELECTRICAUELECTRONIC WIRING WAS SELECTED AND INSTALLED TAW AC43.13-1B, CHAPTER 11. SECTIONS 5-8, 13. 15. 17-19 AND AC43.13-2A CHAPTER 2, PARAGRAPHS 21.22 & 27. ROUTING, LACING AND TYING COMPLIES WITH AC43.13-1B, CHAPTER 11. SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-1B SECTION 16. ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURERS INSTRUCTIONS AND AC43.13-2A, CHAPTER 2. PARAGRAPHS 21 THROUGH 26 AND CHAFFER 3, PARAGRAPH 44. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS TAW AC43.13-1B, CHAPTER IQ SECTION 2 AND AC 43.13-2A, CHAPTER 1 PARAGRAPH 9. PER THE AIRCELL ATG.01 FLIGHT PHONE SYSTEM MANUAL ALL COMPONENTS ARE CONSIDERED LINE REPLACEABLE UNITS AND DO NOT AFFECT THE MANUFACTURERS INSTRUCTIONS FOR CONTINUING AIRWORTHINESS. STRUCTURAL CONTINUING AIRWORTHINESS INSPECTION REQUIREMENTS ARE CONTAINED IN A.T.E. INC. STRUCTURAL REPORT ATEAI 12001 DATED 6/12/01, SUBSTANTIATED BY F.A.A. FORM 8110-3 DATED 6/12/01 BY STRUCTURES DER NO. DERT-510333-CE THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES REQUIRED FOR THIS INSTALLATION. END ❑ Addtional Sheets Are Attached * U.S. GPO 1990.761.753 SDNY_GM_02759792 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246714 EFTA01331177 a _bgAy-29-01 01:5DP N J Curran 352 243 1011 P.IJ/ DEMMUM a TUNSIORTAT KIN ITDISAL /MAT /COI NatroOSTIATCW. DATE STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIAT ION REGULATIONS 05129/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATIO N MAKE MODEL NO. TYPE IAIIDIOne. Rat*. fkikopIer. ete1 NAME OF APPLICANT Jet Aviation Associates Boeing 727-31 Airplane West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B72746236430, Initial Release. AlRCELL AGT.01 AIR/GROUND TELEPHONE dated 04/30/01 PURPOSE OF DATA In support of major alteration to Boeing 727-31 . serial number 20115. registration number N9OSJE. APPLICABLE REQUIREMENTS (List specific sections ) FAR 26.581 (a)(b)(1) FAR 25.1357 (afle) FAR 25.889 (aX4) FAR 25.1431 (a)(b)(e) FAR 25.1301 (a)(b)(e)(d) FAR 25.1529 FAR 25.1309 (a)(b)(g) FAR 25.1361 (a) CERTIFICATION - Wt. rOn.liy....4 by ilimaIIMgtSt AIS/ISInall ill OtiOalate as aikmen...• dos Wed den Was ataid tinnosbn,4 HONE Ins ton onistd ka Ilaelksitt .4.5 eaaflobef swan..dors.......«.h. la a A.raunsaA.s.;twins., Ilardeds. plotalun mll fond iv —* ebb npbnkk nialnann *Ia. flan, miry. O Rename/DO mpprcnnol orange date I (We)TDenton la Apply/web/se tlics (Spleen & EalfSeat at Aspects Dear Approval Osly, Doe Nit Contilirlt Inlathithe AppaNa0 SICNATVet A) Watt 07frtE517 4,0, ,ttrattll DISIGNATIOniM,Mma) CIASSIOICATONSI DERT41008741M A- Systems & Equipment No n J. C n rA - r-- --- - • ) 901411 FILDIAML SC-7274U RCELLOCC SDNYGIvl_02759793 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246715 EFTA01331178 SDNYGM02759794 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246716 EFTA01331179 U.S. DEPARTMENT OF TRANSPORTATION DATE FEDFItal AVIATION ADMINISTATION Jane 18,2001 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL TYPE ~L.% AS,A tiegaId• 114 NAME OF APPLICANT Boeing B727-3I Airplane Jet Aviation LIST OF DATA ilnallsR.AIRsn limn Jet Aviation Aircell AGT.01 Air/Ground Telephone Antenna Installation Engineering N Drawing Beoing B727-31, N9OSJE,S/N 20115 o. B727-16236-1330, END END END_END END END END END Dtd. 5/29/2001, Rev. A Note: The certification basis of this aircraft includes FAR 25.571 Damage -tolerance and fatigue evaluation of structure. Per Advisory Circular 25.1529-1 Instructions for Continued Airworthiness of Structural Repairs on Transport Category Airplanes, the damage tolerance and fatigue evaluation of _ END END the structure must be performed before 6/18/2002. Notes: 1) The structural aspects only of the above listed data are approved herein. 2) This approval is valid for the aircraft model and serial number listed below 3) This approval is based on structural analysis on file at DER Services corporate office in Ft. Lauderdale, TV. Model No. B727-3I Serial No. 20115 PURPOSE Approve data for antenna installation (Structures Only) OF DATA APPLICABLE REQUIRMENTS (LISr SPECIFICSECTIOMS) 25301, 25303,25.305,25J07, 25.601, 25.603. 25.605.25.609, 25.613 Lexs1EICATION- Under authority mad by direction of Me Administrator and in monism with cOnclitiOn and ti cm of appointment under Part anorak Federal Aviation Regulations, data listedabove sad on *Mak d sheet. eves bare beta emitted Is accordance with established procedures and freed to comply with applicable mainmasts alba ra Ariake Regulation,. I (rye)Therefore O Recommod approval *Mae data Fil Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTIVE(S) DESIGNATION NUMBERS) CLASSIFICATIONS) Robert J. Ilielgau DERT-510024:CE Structures 4,45 4f.------. FAA FORM 81104 (II-70) SUPERSEDES PREVIOUS EDITION DER SERVICES PROJECT NO. 2001-082 SDNYGlvl02759795 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246717 EFTA01331180 SDNY_GM_02759796 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246718 EFTA01331181 DEPADEPARTMENTOF TRANSPORTATON DATE FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS June 3, 2001 AIRCRAFT OR AIRCRAFT COWONENT IDENTIFICATION MAKE MODEL NO. TYPE (Aaeems. Read NOtercterte) NAME OF APPLICANT Boeing 727-31 Airplane Jet Aviation Associates- WPB LIST OF DATA OIRCITICATION TIRE B727-16236-1270 Argus 5000/CE Moving Map Equipment Installation Sht 1-5, Rev IR 8727-16236-1331 Aircell Equipment Installation, Sht 1-6, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval Is based on drawing review and Inspection. 3. After the alteration, the aircraft must be returned to service by FM authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, SIN: 20115 APPLICABLE RE-OUIEFIAPNTS Rid Speak section') FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.561 25.601 25.603 25.605(a) 25.609 25.611 25.613 25.789 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations Cl appoMment under Pm 183 of the Fedora, Av4ition Regulations,data listed above and on attached sheets numbered 0 have been examined In armaidmice with established procedures and found to comply Mrh applicable requirements of Federal Aviation Regu'ations. i Recommend approval of these dais. I ag llurefere APprove coca data. SGNATURE(3) CC DEVGNATED ENGINEERING REPRESENTA1TVEr$1 DESIGNATION tathaftEurgf CLASSUICAMONS) David E. Haralson DEC. Awe.-- DERT-810028-NE Structural orrn (1,-70)SUFVLSEOES MEMOS °MON ER011074(4 SDNYGlvl_02759797 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246719 EFTA01331182 SDNY_GM_02759798 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246720 EFTA01331183 DaAtenittolOFTRAIMOVIAllai . DATE r FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS JUNE 12, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE NO. TYPE t*Avis.itaRedds.v. •IAME OF APPLICANT viv.4 BOEING 7 27-31 AIRPLANE JET AVIATION LIST OF DATA nava/EAU* MU A.T.E. INC. BOEING 727-31 SIN 20115, AERO-M SATCOM ANTENNA INSTL, UPPER B.S. 360.390; STRUCTURAL REPORT OPS ANTENNA INSTL, UPPER B.S. 312-328; AIRCELL AGT.01 ANTENNA INSTL, No. ATE6112001 LOWER B.S. 400-420 DAMAGE TOLERANCE ANALYSIS; SH. 1-31, REV. (IR) PIOTE• REOU(RED INSPECTIONS ATTACHED t THESE DATA APPLY ONLY TO HOED* 727-31 SIN 20115 PURPOSE OF DATA TO APPROVE DATA FOR DAMAGE TOLERANCE ANALYSIS, B-727-3I SIN 20115 APPLICABLE REQUIREMENTS Rai wait xviivei FAR 23311 (STRUCTURAL ASPECTS ONLY) CERTIFICATION - Ueda authority vestal by &mica &the AdealnidesMe sod in matdance with conditiceu and amassnit • of appolevocM caw Pan 1113 ante Fedaal Aviation Replations, data listed above and en attached sheets maned loft haw beta ittatained In azawdatice with atatilithott mantras and found lo comply with appEcable recpiranents or the Federal Aviation lissuladoon Paammmd approval ofthese I (0) re k r Approve data . SO:Ran/REM OF DESIGNATED ENGINEERING DESIGNATION NUMBER(S) CLASSIFICATION(S) DERT-510333-CE STRUCTURAL IiZ— e n/ 0 /Lot . L) FAA Fens 9110-3 wad SIAMIS100 pitman crow. Of0101411 SDNYGlvl02759799 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024672 I EFTA01331184 SDNYGM02759800 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246722 EFTA01331185 Form Approved MAJOR REPAIR AND ALTERATION OMB No. 2120-0020 us Dorris% 0 ol Tramp:aka (Airframe, Powerplant, Propeller, or Appliance) For FAA Use On! fibril Minkel Office Identification AchnintsinUcc SO-F5 Do - i 7 Int11 INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instruct' and disposition 1 this form. This report is required by law (49 U.S.C. 1421). Failure to report can to tat in a civil penalty not to o ed $1.000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model BOEING 727-31 1. Aircraft Serial No. Nationality and Registration Mark 20115 U.S.A. N91:187E Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner JEGE INC. 103 FOULK RD. STE 202 WILMINGTON DE. 19803.3742 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 APPUANCE Manulacturbr 6. Conformity Statement A. Agencys Name end Address B. Kind of Agency C. Certificate No. U.S. Certified Mechanic CRS EYKR782D JET AVIATION ASSOCIATES LTD. Foreign Certified Mechanic AIRFRAME 1,3. 1615 PERIMETER RD. X Certificated Repair Station RADIO 1,2,3. WEST PALM BEACH. FL 33406 — Manufacturer LIMITED A/F & ENG. 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 heroin is true and correct to the best of my knowledge. Date Signature of Authorized Individual 7/2/01 John K. Urso. Inspector. X-11L-r- 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit dentified In Item 4 was spected In the manner prescribed by the Administrator of the Federal Aviation Administration and is El APPROVED Ull REJECTED FM Fit. Standards Other (Specify) Manufacturer Inspection Authorization Inspector BY Person Approved by Transport FAA Designee X Repair Station Canada Ainvonhiness Group Date of Approval or Rejection Certificate or Signature of Authorized Individual Designation No. 7/2/01 EYICR782D Ronald K. Bystrom. Manager Quality Assurance FAA Form 337 0243) SDNY_GM_02759801 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246723 EFTA01331186 NOTICE Weight andbalance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with al1previous alterations to assure continued conformity rah the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach ackNional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) BOEING 727-31, Sal 20115. N9081E. W/O 16236. ACCOMPLISHED AN UP-GRADE TO THE EXISTING HONEYWELL WEATHER RADAR SYSTEM FROM PRIMUS 870 TO PRIMUS 880. REMOVED THEY 1 & 2 WC-870 CONTROLLERS P/N 7008471-803 AND INSTALLED WC-880 CONTROLLERS P/N 7008471.405 (ISO C63c), REMOVED THE WU-870 ANTENNA & RECEIVER / TRANSMITTER UNIT P/N 7012640-902 AND INSTALLED NEW WU- 880 ANTENNA & RECEIVER / TRANSMITTER UNIT P/N 7021450-801 (ISO C63c). INSTALLED A HONEYWELL LSZ-860 LIGHTNING SENSOR SYSTEM CONSISTING OF AN 1.1 -860 PROCESSOR P/N 7011822-904 (ISO C110) AND AN AT-855 ANTENNA P/N 7014062-901 (ISO CI10). THE LIGHTNING SENSOR SYSTEM INTERFACES WITH THE PRIMUS 880 RADAR SYSTEM THRU THE If 1 & 2 WC-880 CONTROL t FRS. RELOCATED EXISTING SECURITY SYSTEM ANTENNA PM DMC57-1 TO THE TOP OF THE RADAR ANTENNA & RECEIVER / TRANSMITTER UNIT. THESE MODIFICATIONS WERE COMPLETED USING THE FOLLOWING JET AVIATION DRAWINGS, WHICH ARE SUBSTANTIATED BY FAA 8110-3 FORMS RESPECTIVELY: WIRING DRAWING: • B727-16236-260. REV. R. DATED 5/29/01, SHEETS 14 2, TITLED - WEATHER RADAR SYSTEM UPGRADE (PRIMUS 880) REFERENCE FAA FORM 8110-3 DATED 6/7/01. BY SYSTEMS & EQUIPMENT D.E.A. NO. DERT-510087-NM. • B727-16236-261, REV. IL DATED 4/10101, SHEETS ITHRU 3, TITLED- HONEYWELL LSZ-860 LIGHTNING SENSOR SYSTEM REFERENCE FAA FORM 8110-3 DATED5/29/01, BY SYSTEMS & EQUIPMENT D.E.R. NO. DERT-510087-NM. STRUCTURAL DRAWINGS AND REPOR]% • B727-16236-1261, REV. A, DATED 5/30/01. SHEETS 1 THRU 7, TITLED- AT-855/RTA-880 ANTENNA INSTALLATIONS REFERENCE FA.A. FORM 8110-3, DATED 6/1/01, BY STRUCTURAL D.E.R. NO. DERT-810028-NE • B727-16236-1242, REV. It. DATED 5/21/01, SHEETS 1 & 2, ITILED - LSZ-860 LIGHTNING SENSOR EQUIPMENT INSTALLATION. REFERENCE F.A.A. FORM 8110-3, DATED5/28/01. BY STRUCTURAL D.E.R. NO. DERT-810028-NE THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER HONEYWELL PRIMUS 880 RADAR SYSTEM INSTALLATION MANUAL NO. 34-42-12, REV 3. DATED 2/15/00 AND THE HONEYWELL LSZ-860 LIGHTNING SENSOR SYSTEM INSTALLATION MANUAL NO. 34-41-50, REV 5. DATED 2/15/01 writ NO DISCREPANCIES. AN EMI TEST, REPORT NO. B727-1'6236-080, REV IR DATED 6/19101 WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. THE STATIC WADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.I3-2A, CHAPTER 1, PARAGRAPH 3 AND WAS FOUND TO MEET THE REQUIREMENTS OF PARAGRAPH 2. MATERIALS AND PRACTICES COMPLY WITH PARAGRAPHS 4 THROUGH 12. THE ELECTRICAL LOAD ANALYSIS UPDATE REPORT B727-16236-041, REV 111, SHEETS 1 THRU 21, DATED 06/11/2001 WAS COMPLETED IN ACCORDANCE WITH 43.13-IB, CHAPTER 11, SECTION 3. PARAGRAPH 11-37. AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.134 B. CHAPTER 4, SECTIONS I, 2, 3 AND 4, CHAPTER 6. SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.13.1B, CHAPTER 7, SECTIONS 1- 5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MIL SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43. I3-1B, CHAPTER 11, SECTION 4. ELECTRICAUELECTRONIC WIRING WAS SELECTED AND INSTALLED TAW AC43.13-18, CHAPTER II, SECTIONS 5-8, 13. 15, 17-19 AND AC43.13-2A CHAPTER 2. PARAGRAPHS 21.22 & 27. ROUTING, LACING AND TYING COMPLIES WITH AC43.13-1B, CHAPTER 1I, SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-1B SECTION 16. ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURER'S INSTRUCTIONS AND AC43.13-2A, CHAPTER 2. PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3, PARAGRAPH 44. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN ME AIRCRAFT RECORDS TAW AC43.13-1B, CHAPTER 10. SECTION 2 AND AC 43.13-2A, CHAPTER 1 PARAGRAPH 9. MAINTENANCE FOR CONTINUED AIRWORTHINESS IS CONTAINED IN HONEYWELL PRIMUS 880 RADAR SYSTEM INSTALLATION MANUAL NO. 34-42-12, REV 3. DATED 2/15/00 AND THE HONEYWELL LSZ-1160 LIGHTNING SENSOR SYSTEM INSTALLATION MANUAL NO. 34-41-50, REV 5. DATED 2/15/01. • THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES DUE TO THIS MODIFICATION 0 Additional Sheets Are Attached * V.S. G.P.O 1990-761.753 SDNY_GM_02759802 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 1x)246724 EFTA01331187 DOARTMDFFOF TIWIStallATICO4 MODAL AVIATION AD/AINISTILA11011 DATE STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS 06/07/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio. Helicopter. etc) NAME OF APPLICANT Jet Aviation Associates Boeing 72741 Airplane West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B727-16236-260, Initial Release, WEATHER RADAR SYSTEM UPGRADE (PRIMUS 880) dated 05/29/01 • !... • PURPOSE OF DATA In support of major alteration to Boeing 727-31, serial number 20115, registration number N980JE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.5131 (a)(b)(1) FAR 25.1351 (a) FAR 25.869 (a)(4) FAR 25.1357 (a)(c) FAR 25.1301 (a)(b)(c)(d) FAR 25.1431 (a)(b)(c) . FAR 25.1309 (a)(b)(g) FAR 26.1629 FAR 25.1316 (b) CERTIFICATION - thocknAtioDy voted by dtrAik.et OA Adnosainoor and La Mardsett with csaditlass mad Itaitadoas or appokause•A sidfr nn lilathe /Wen' Minas PnilaSesh mu rums above mad m awns .Neu steams NONE Nn Wei tunic.' h. attentimott wilb ettailabed pnadern awl fend to comply with Reptant VOW* requimentni the (atm, Aristke O Retommend approval of these data I ere)fbereare al Approve these data (Systems & Equipment As Dales Approval Only. Dom Not Constitut Installation Approval) SIGNATU FD REFILIZENTATIVOS) DESIGNATION MUDIEMS(S) ClASSMCMONT /zap. DERT-510087-NM Systems & Equipment an J. ran FAA Form 8110-3 1-70) SUPERSEDES PREVIOUS EDITION GPO 901413 FlIEHAME SC-7274tDR_DDC SDNYGIvl_02759803 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246725 EFTA01331188 SDNYGM02759804 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246726 EFTA01331189 . DENJUUDIT OF lltANSPORTAIIPN FEMME AVIATION ADMDLISTAATION DATE i STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS 06/07/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Retro, Hdicarier. ac) NAME OF APPI.ICA NT Booing Jet Aviation Associates 72731 Airplane West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B727-16236-260, Initial Release, WEATHER RADAR SYSTEM UPGRADE (PRIMUS 880) dated 05/29/01 PURPOSE OF DATA in support of major alteration to Boeing 72741 , serial number 20115, registration number N980JE. • APPLICABLE REQUIREMENTS (List specific statees ) FAR 25.681 (a)(b)(1) FAR 26.1351 (a) FAR 25.869 (a)(4) FAR 25.1357 (a)(c) . FAR 26.1301 (a)(b)(c)(d) FAR 25.1431 (a)(b)(c) FAR 25.1309 (a)(b)(g) FAR 25.1529 FAR 25.1316 (b) CERTIFICATION - Doter saoierity nand by tettlaa tribe Adnkatrat er nal I. malting ',nib atilt:nu w linianieu tato Sand &boat al ea .rasp &nen enabend otatgaa'ainnel utter n,11u aloha Eiden: Aviation NONE Inn bent eannIsta ia &contact with acsallabed *,cation, Regattap. prontnand And in comply wad appluatit intim:nit of Ma Enka, Minim ❑ RetOMITItIld approval of these dais I evo Terefore tEl Aopove these data (Systems & Equipment Aspects. Dcsltn Approval Only. Dom Not Constitut Installs tloo Approval) SIGNA F DEM C strustransivErn DESIGNATION MOSSO) RASSIFICA110/1(1) DERT-510087-NM Systems & Equipment o an J. FAA Form 81104 ill-anSUNERSEDES PREVIOUS EDMON GPO 901-613 EILESIANt& SC-7274UORDOC SDNY_Glvl_02759805 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246727 EFTA01331190 SDNY_GM_02759808 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246728 EFTA01331191 May-29-O1 O1:58P N J Curran 352 243 Steil OUNUNIFIll Of TRANS/ORTATICet DATE 1100.Q.MIATIONAOMSCISTILOP3N STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS 05/29/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE Misplace. Rothe.ittlieopeet..lc) NAME OF APPLICANT Jet Aviation Associates Boeing 72741 Airplane West Palm Beach, FL LIST OF DATA IDENTIFICATION TIRE B727-16236-261, Initial Release, HONEYWELL LSZ-860 LIGHTNING SENSOR SYSTEM dated 04/10/01 PURPOSE OF DATA In support of major alteration to Boeing 727-31, serial number 20115. registration number N90I3JE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.581 (a)(b)(1) FAR 26.1367 (a)(c) FAR 25.869 (a)(4) FAR 26.1431 (a)(b)(c) FAR 25.1301 (a)(b)(c)(d) FAR 25.1529 FAR 25.1309 (a)(b)(g) " FAR 25.1351 (a) CERTIFICATION - veer.=nem, wadi lry tombs' aro Aeolakintor an ea seensneenu mainsna seinen senoncena nen Pen inane ernsMinimLynne. *to raid O,nad 1d st,......a...• _I;(32INE M Fa moist.Is newts, kb swammate,.- kind ....pi was meats..ass art frees swim,. Iterlanos. O Reonnotod approval cube Oats I Paeyllternote a Approve One data (Spiess At tepennest Aspects. Delp Approval Ooty, Don Not Ccestitate lostallados Approval) SICAAT r lib rfc itnoznacIrrnin(a OtSICNATION MOMS) CULUMCA110.110) l C0gin. 40 _ DERT-510087-NM Systems & Equipment No an urran FAA Form 8110-3 el1.70) SUPODILDES PREVIOUS EDITIONOOS01413 FELENAME.SC.4274.7OSNSILDCC SDNYGIvl_02759807 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246729 EFTA01331192 SDNYGM02759808 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246730 EFTA01331193 DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS June 1, 2001 AIRCRAFT OR MRCRAFT COMPMENT IDErinFICATON MAKE NOMA NO. TYPE (AarIones Redo. Helms:W. oI ) NAME OF APPOCJINT Boeing 727-31 Airplane Jet Aviation Associates- WPB UST OF DATA IDENTIFICATION TITLE 5727-16236-1261 AT-855/RTA-880 Antenna Installations, Sht 1-7, Rev A 6727-16236-1410 Dual FMS W/ RTU Equipment Installations, Sht 1-6, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration. the aircraft must be returned to service by FAA authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, Mt 20115 APPOCASTERECIUREMENTS (Use speoac sedan) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.601 25.603 25.605(a) 25.609 25.611 25.613 CERTIFICATION - Under authority vested by direction of the Administrator and In accordance with conditions and OrnitilliOnS of appointment under Fart 183 of the Federal Aviation Regulations, data fisted above and on attached sheets rermbered In acCordance Ath established procedures and found to Consul), with apigicabre fer:cements 0 have been examined Of the Peden! Aviation Regulations. ReCOSIIRS.VS accesSill 04 thesis two. 1 (IX Therstore *Move these date. SIGNATURE(S)OF DESIGNATED ENGINEERING REPAESENTA TIVErR DESIGNATION MAMER(S) ,• ; . CIASSFICATION(51 David E HaralsOn P...ie. N ir DERT-810028-NE .7,, , Structural . .14. •r: OIm ti sUPEASEDESTALMOOSIMII011 esone2ser SDNY_Glvl_02759809 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024673 I EFTA01331194 SDNYGM02759810 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246732 EFTA01331195 DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS May 28, 2001 AIMCRAFT OR NACRAFT COMPONENT iDENTW1CATICN ALINE MODEL NO. TYPE (AliSant Real, Ifetcomer. etc.) NAME OF APPLICANT Boeing 727-31 Airplane Jet Aviation Associates- WPB LIST OF DATA IDEMTFICAMON TITLE 8727-16236-1262 LSZ-860 Lighting Sensor Equipment Installation, Sht 1-2, Rev IR B727-16236-1342 Aero-M SATCOM Equipment Installation, Sht 1-7, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA authorized personnel. PURPOSE Oh DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPUCABLE REWIRE:MATS Rat speak cocoons) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.561(b)(c) 25.601 25.603 25.605(a) 25.609 25.611 25.613 25.789 CERTIFICATION - Under authority vested by *action of the Admire-.eater and In accordance with conditions and limerdlons of appoinenent under Pan 183 ad the Federal Aviation Regulalieas, data listed above and on attached sheet: numbered In accordance with established procedures and found to comply with applicable requirements of 0 have been examined ME Federal Aviation Regulations. Recommend approval of these dam i 4 0 Theielore Appian these data. SIGNAIL DESIGNATED EENGGINEERiUG REPRESENTATIVE(S) DESIGNATION R( ) CLASS ROMS) David E. Haralson Po-ee. wont_ DERT-810028-NE Structural FAA Form 8110-3 (ii-le) SUPERSEDES PREVIOUS ELMO/4 ER012054“ SDNY_Glvl_0275981 I SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246733 EFTA01331196 SDNYGNI02759812 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246734 EFTA01331197 DATE OEPARIMENtOF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPUANCE WITH THE FEDERAL AVIATION REGULATIONS May 28, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDEMIFICADON MAZE MODEL NO. TYPE (iMolisne. Rado. lixtinemr, et) NAME Of APPUCONT Boeing 727-31 Airplane Jet Aviation Associates- WPB UST OF DATA IDEM1RCATPON THE B727-16236-1262 LSZ-860 Lighting Sensor Equipment Installation, Sht 1-2, Rev IR 8727-16236-1342 Aero-M SATCOM Equipment Installation, Sht 1-7, Rev IR Note: 1. This approval Is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPUCABLE REOUIRPMcNTS NV specifeneirenta FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.561(b)(c) 25.601 25.603 25.605(a) 25.609 25.611 25.613 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 Adadon RepulatlenS. data Wed above end on attached sheets numbered 0 have been examined 2 In accordance with estabilshed procedures and found to comply vah appkablo requirements of the Federal Aviation Regulaliorm. ReCCOVIlet4 approval of those data. I DX 'Therefore Approve IMSOCiati. SIGRATURE(S)OFDESIGNATEDENDerLEANGREPRESENTATNEtS1 DESIGNATIONriumaER(R) CumSIFICADOMSf David E. Haralson ase. th.....e.__ DERT-810028-NE Structural FAA Form 8110-3 ulTre SUPERSEDES PREVOll5 ECOION ER01205 doc SDNY_ GE/1_02759813 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246735 EFTA01331198 SDNYGNI02759814 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246736 EFTA01331199 Form Approved • 0 4 MAJOR REPAIR AND ALTERATION OMB No. 2120-0020 us Dpartenint al Transportilkm NSW Avtattal AdmInIstratIon (Airframe, Powerplant, Propeller, or Appliance) Mt 62,6 For FAA Uso Only °Identification 50-fisbo- t7 INSTRUCTIONS: Print or type all entries. Soo FAR 43.9 Appendix B, and AC 43.9-1 (or subseque t revision thereof) for ins and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can re ult in a civil penalty not to exceed 51,000 for each such violation (Section 901 Federal Aviation Act of 1966). Make Model BOEING 727-31 1. Aircraft Serial No. Nationality and Registration Mark 20115 U.S.A. N9081E Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner MOE INC. 103 FOULK RD. sm 202 WILMINGTON DE. 19803-3742 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. Certified Mechanic CRS EVICR782D JET AVIATION ASSOCIATES LTD. Foreign Certified Mechanic AIRFRAME 1,3. 1515 PERIMETER RD. K Certificated Repair Station RADIO 1,2,3. WEST PALM BEACH. FL 33406 Manufacturer _LIMITED ME & ENG. 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 boon 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 know/edge. Date Signature of Authorized indi ual 7n101 ee John K. Urso. Inspector. it.... K. Ct--c- 7. Approval for Return to Servl Pursuant to the authority given persons specified below, the unit dentified in item 4 w inspected 'n the manner prescribed by the Administrator of the Federal Aviation Administration and is I21 APPROVED CI REJECTED Other (Specify) FAA Flt. Standards Manufacturer Inspection Authorization inspector BY Person Approved by Transport FM Designee X Repair Station Canada Ainvorthiness Group .. Date of Approval or Rejection Certificate or Signature of Authorized Individual Designation No. 7/2/01 EYKR782D Ronald K. flystrom. Manager Quality Assurance. 4 FAA Form 337 (12-04) SONY_CM_02759815 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246737 EFTA01331200 NOTICE Weight and balance or operating limitation changes shall be entered In the appropriate aircraft record An alteration must be compatible with ad previous alterations to assure continued °creamily MV) the applicable airworthiness requirements. 8. DesaiptIon of Work Accomplished (If more space Is required attach; additional sheets, Identify valh aircraft natiimality and registration ma*and date work accomplished.) BOEING 727-31, S/N 20115. N908.113, WIG 16236. ACCOMPLISHED A WAS CHANGE 7 UPGRADE TO THE EXISTING HONEYWELL WAS 11SYSTEM PREVIOUSLY INSTALLED UNDER PAGE AVJET CORPORATION SW SA3094.50 DATED 8/24/93. REFERENCEFAA. FORM 337 DATED 8/25/93. THE WAS PROCESSOR P/N 4066010-904 WAS MODIFIED TO P/N 4066010-910 (CUSTOMERS UPGRADED UNIT) IN ACCORDANCE WITH TIMCO MASTER DRAWING LIST 01T012L001, REV IR, DATED 5/21/01. REFERENCE F.A.A. FORM 8110-3 DATED 5/21/01 BY SYSTEMS AND EQUIPMENT DER NO.DERT-510239-CE. THE TCAS B CHANGE 7 PROCESSOR WAS INSTALLED AND TESTED IN ACCORDANCE WITH TIMCO ENGINEERING ORDER DOCUMENT 0IT012E006, REV IR. DATED 5/21/01 WITH NO DISCREPANCIES. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE AIRCRAFT EQUIPMENT LIST WAS AMENDED AND ENTERED IN THE AIRCRAFT RECORDS. AIRWORTHINESS DIRECTIVE 94-01-04 AMENDMENT 39.8786 IS WA TO THIS INSTALLATION BY PROCESSOR P/N. THERE IS NO CHANGE TO THE AIRCRAFT WEIGHT AND BALANCE THERE IS NO CHANGE TO THE AIRCRAFIS MAINTENANCE FOR CONTINUED AIRWORTHINESS REQUIREMENTS DUE TO THIS INSTALLATION. THE REQUIRED F.A.A. APPROVED HONEYWELL INC. WAS U FLIGHT MANUAL SUPPLEMENT DOCUMENT "ICAS-APPS-0294, REV A, DATED 3/21/00 HAS BEEN INSERTED INTO THE AIRCRAFT FLIGHT MANUAL _END ❑ AddaMnal Sheets Are Attached * U.S. G.P.O 1990-781-753 SDNY_GM_02759816 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246738 EFTA01331201 eornmtmtcations Aviation Communications Si Surveillance Systeme A]0.V»]-Ylce May 16, 2001 TIMCO 623 Radar Road Greensboro, NC 274 Artm: Mr. Gregg Stutes Re: Letter of Authorization to use technical data Dear Mr. Styles, This letter is to authorize TIMCO ("Recipient") to use the following technical data owned by L-3 Communications Corporation —Aviation Communications & Surveillance Systems (L-3) for the limited purpose indicated here below. The technical data subject to this Letter of Authorization ("Data") is the L-3 developed data used to apply for the following FAA certifications: Supplemental Type Certificate STC SA4834NM, as defined by ML4070349, for B727 aircraft. L-3 Authorization to use Data is limited to the following B727 aircraft tail number, namely: • B727 S/N 20115 L-3 Authorization to use Data is granted hereby for the sole purpose to provide the Recipient with technical information for its internal use and engineering review purposes. The Recipient recognizes L-3's proprietary rights in Data and will limit its disclosure to a need-to-know basis for its employees. The Recipient will not use Data for any other purposes than the internal use and engineering review purpose established for this Authorization. The Recipient will not sell, license, rent, market, transfer, assign, distribute, or otherwise disclose to any third party, exploit or permit any other use of Data. L-3 does not provide any warranty whatsoever on Data, whether express, or implied, or implied by law, including but not limited to merchantability and fitness for any particular purpose. SDNY_GAl_02759817 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246739 EFTA01331202 SDNYGNI02758818 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246740 EFTA01331203 In no event shall L-3 be liable for • Any direct, incidental, indirect, special or consequential damages including but not limited to loss of use, revenue or profit, even if L-3 has been advised, knew or should have known of The possibility of such damages; or • Damages caused by the Recipient's failure to perform its obligations and responsibilities; or • Claims, demands or actions against the Recipient by any other party. The term of this Authorization is one (1) calendar year from its date. If during such term L-3 believes that its proprietary rights in Data are being infringed or injured or otherwise are at risk, L-3 reserves the right to terminate Authorization hereunder and, upon notice to Recipient, request the Recipient to discontinue any further use of Data. Upon termination of Authorization hereunder, the Recipient will either destroy or return Data in its possession and notify L-3 that no further use of Data will take place. For any communication concerning this Authorization, please contact F.W. (Bill) Lynch, Certifi Fax Pinter., countersign this Letter of Authorization and return it to us as follows: original by mail (with the original signature of your authorized representative); a copy by fax to the undersigned. Thank you for your interest F.W. (Bill) L ch Agent for L-3 Communications, ACSS SDNY_GM_02759819 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246741 EFTA01331204 SDNY_GM_02759820 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246742 EFTA01331205 %Wad Zinn of arks Btpamnent of transportation —OW ablation administration *pplemental `Egg &vacate SA3094so} ireap...—/As4414a.e..120 Page Avjet Corporation 9809 Tradeport Drive Orlando, Florida 32827 artiead.44,66.70.4.44-40...24r/a.,,,e1h.henaa...datmactmandeoan. ..Itien,fluti.ohe tatesteoruench41-.4‘.euirecordhassirrewmastehrearl 25 i ts Federal Aviation glerlallangt, etraSideci-40. - gertieanah•-: A3WE 405-4: Boeing 727-100 Series SlaP iAn'9491. -Pl r ta r ; Installation of Provisions only for a Honeywell TCZ-910 TCAS II System in accordance with Page Avjet Master Drawing List MDL-91- 41, Initial Release, dated November 19, 1991, or later FAA approved revisions. ...eneiatientwazeage-naedion.1 This approval should not be extended to other airplanes of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. S terlOca4,2,tae.awcplinrcerlepareartt pY dehaaleiysrewalehrilrentaina.Atwra.ma— wetuhretsUafriteheiwoveXectiwobwhettowhinati:wit..eZhir sa edelftecheehleaaed.100 Lie .51triitiwih/m/..h a, : October 21, 1991 Y04. ietahweik -47.iteliesetenew: January 15, 1992 9:4.„ ww4404, hn ligue aismg„, ger, Atlanta Aircraft Certification Office (Tide) Any alteration ofthis certificate it punishable by efine of exceeding $1,000, or imprisonment not exceeding &yews, or both. This arttfate me; be hottftered le etweedonee with FAR 21.17. PAAIets 10-2 (Mal) SDNY_GM_02759821 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246743 EFTA01331206 SDNYGNI02759822 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246744 EFTA01331207 DATE U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION •5 7 24/0/ — ' STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATLON REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MODEL NO. TYPE (MRPLavE. ROC% IfSJCOPIER NAME OF APPUCANT MAKE EICJ 727-100 Airplane TIMCO Boeing UST OF DATA IDENTIFICATION TITLE TIMCO Master Data Honeywell TCAS II Change 7 Software Upgrade for a Boeing 727-100 List, 01T012L001 Rev IR Dated 5/21/01 END OF DATA PURPOSE OF DATA aircrafL STC SA4834NM is To document and approve the installation of a TCAS Change 7 in a Boeing 727-100 the approval basis for this installation. APPLICABLE REQUIREMENTS ommeotreRaw FAR 25.1301 (a), (c) ... • conditions and limitations of CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with of the Federal Aviation Regulations, data listed above and on attached sheets numbered appointment under Part 183 found to comply with applicable have been examined in accordance with established procedures and requirements of the Federal Aviation Regulations I 1( ) Therefore • Recommend approval of these data IE Approve these data ateesie _., DESIGNATION NUMBERS) CLASSIFICATION(S) SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVES) • DERT-510239CE System & Equipment Robert McClellan FAA Form 8110.3 (11-70) SUPERSEDES PREVIOUS EDITION SDNY_Givl_02759823 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246745 EFTA01331208 SDNYGM02759824 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246746 EFTA01331209 Taco EIONEEREO SYSTEMS. be `a ouweve•Sae *raw A MASTER DATA LIST TITLE: HONEYWELL TCAS II CHANGE 7 SOFTWARE UPGRADE MDL NO. 01T012L001 REV/DATE: IR/ 5/21/01 STC / FAA PROJECT NO.: SA4834NM / 650259 AIRCRAFT TYPE: BOEING 727-100 ENGINEER: P. FERGUS APPROVAL: ROBERT MCCLELLAN SHEET 1 OF 1 DOCUMENT REVISION TITLE SHT NUMBER LTR DATE 01T012C002 IR 5/21/01 HONEYWELL TCAS II CHANGE 7 SOFTWARE UPGRADE FOR A BOEING 727-100 1 ISSUED MAY 22 2°1 gloom con-too. l estrtsfedpen ,......,,,,,,,...y...PrZe0.7%0EV= SSyge.A.=:= Oketel•b po r ilfwearanZtrilhrtzrecisluItterie.d Inkn titsgms toIndsm.folt.COEFIVSH.Sr..... a. OW0, 10 2002 nmeo Ehameews snow.. V. 0IT0IX001$ Sod ft :091MM LbL9rZOO- V.L.43 EFTA01331210 SDNY_GM_02759826 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246748 EFTA01331211 to Form tix: OON TACO ENGMEJMEOSYSIF.A8 DAV: 01,01/00 co tic CONFIGURATION DOCUMENT M seam*SuntanMI A • rn TITLE: HONEYWELL TCAS II CHANGE 7 SOFTWARE UPGRADE FOR A BOEING 727-100 ' CFG NO. 01T012C002 H IR/ 5/21/01 H REV/DATE: ENGINEER: P. Fergus APPROVAL: Robert McClellan SHEET I OF 1 0 I. CONFIGURATION DATA A. APPLICABLE MDL: HONEYWELL TCAS II CHANGE 7 SOFTWARE UPGRADE # 01T012L001 B. EFFECTIVITY I SSUED rn 1. BOEING 727-100 SERIAL NO. 20115 KAY 22 AM 0 pooMENT C0NIR0L C. DESCRIPTION O 1. THIS INSTALLATION WILL CONSIST OF USING STC SA4834NM AS THE APPROVAL BASIS TO PERFORM THE TCAS CHANGE 7 MODIFICATION TO THE TCAS COMPUTER UNIT. -a D. DEVIATION FROM PREVIOUSLY APPROVED DATA , 1. NONE -o Items marked with an asterisk (*) are for manufacturing and certification and will not be supplied. If required, the documents will be sent directly to the customers certification authority only after TIMCO receives assurance that their confidentiality will be protected. CO tD DOCUMENT REVISION NUMBER LTR DATE TITLE SHT u, 9 01T012E006 IR 5/21/01 Installation of a Honeywell TCAS II CU with Change 7 in a Boeing 727-100 6 011012R007 IR 5/21/01 Description and Substantiation of a TCAS II Change 7 Installation 2 Y' 1= 1O w NJ 9103 Oar. proptery Cl. inSpic9dObry W. TACO England SWIMS. Me and b rogricled IM VW by desireted pan Ms cc ono-aces C. ton ',anima Mn been (1111Ctid no Use sap lo inlearn TACO Farmed Slain kw- sad O_ so MbII Pandas againsi My Wn sash. by tenet elMt p014antort et Ws Otter. In urauChalted use tad Ougalon Is recette. andII Is poleclet yoke anInPUtathed <WOW COWIght(C) 2000 BumenSeedod syntax Inc N StXlchlr 091100403 LVIT012 Jet Artiflo101T012CC02tdoc EFTA01331212 6PL9tZ00-V.L43 SDNY_GM_02759828 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246750 EFTA01331213 Fenn?.la: EN-0002 TECO ENGINEERED SYsmes. nc Date: (WOWS ettearet tan Creener A ENGINEERING ORDER E.O. TITLE: Installation of a Honeywell TCAS II CU with Change 7 in a Boeing 727-100 E.O. NO.: 01T012E006 AIRCRAFT: Boeing 727-100 REV: IR DATE: 5/21/01 INITIAL RELEASE REVIEWS P. Fergus ISSUED PREPARED73Y.rir::152;24€,AsIgg HAY 222001 David Thornton P0OMENT CONTROL • CNECIOD.BNC-0..VCE'-gizi7Ltij;iza.e.'it.i Richard Cunningham 7:okftelireing eciCIA(Sreg- '4&iitarl, Robert McClellan APPIRWITALaigksfrargAigiti TIMCO ENGINEERED SYSTEMS, INC. 623 Radar Road Greensboro, North Carolina 27410 Telephone: 1Ws Oats Ls the wopeny a. and voyntary to. TIM M Engineered %%lent. Inc. and Is mated for metydcgv4E persons. ems ce carp:esters nsth %nem conIncts have been entered It Usti agreed b IndinneY TIMCO Ern:imam Sygenn I t. and to hoSI II harries DOW any claim arising by reason of the ccasecan dela Cured. ca smut/milted Lae ar4 0.clication b rchaittl. and Ills prattled undcr an unpubazb'ecl copra' Ccppicht (C) 2000 TACO Enreesed Systems. Inc CriT012E0)SS Sloe* no 091 ladled SDNYGlvl02759829 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8,9, 10, 15, and 17 EFTA_0024675 I EFTA01331214 SDNYGM02759830 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246752 EFTA01331215 AFM SUPPLEMENT Honeywell Inc. 21111 North 19th Ave. General TCAS/ACAS Applications Phoenix, AZ 85027 Spec. No. TCAS-APPS-0294 FAA APPROVED WHEN EQUIPPED WITH HONEYWELL TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM ( TCAS II) for aircraft that have been This supplement must be attached to the FAA Approved Airplane Flight Manual of the Honeywell Traffic Alert and Corsion Avoidance System (TCAS II) in modified by installation accordance with a Honeywell STC (see SECTION I). The information contained in this document For limitations, procedures, and supplements and supersedes the basic manual only in those areas listed. Manual. performance information not contained in this supplement, consult the basic Airplane Flight FAA APPROVED Manager, Flight Test Branch, ANM-160L Federal Aviation Administration Los Angeles Aircraft Certification Office Tranwort Airplane Directorate Date teat. Zeirt, SDNY Glv102759831 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246753 EFTA01331216 SDNYGM02759832 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246754 EFTA01331217 Form Approved tp MAJOR REPAIR AND ALTERATION OMB No. 2120-0020 usmow:met (Airframe, Poworplant, Propeller, or Appliance) For FM Usey:i illy as Tiensparlasba Federal AvIallon Office Identification AclergasentIon 50- f5Do- (7 ,-ti INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for inst ons 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 od 51.000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model BOEING 727-31 • 1. Aircraft Serial No. Nationality and Registration Mark 20115 U.S.A. N908.TE Name (As sham en registration certificate) Address (As shown on registration certificate) 2. owner JEOE INC. 103 FOULK RD. STE 202 WILMINGTON DP. 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in ltem 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. Certified Mechanic CRS EYKR782D JET AVIATION ASSOCIATES LTD. Foreign Certified Mechanic AIRFRAME 1,3. 1515 PERIMETER RD. jc Certificated Repair Station RADIO 1,2,3. WEST PALM BEACH. FL 33408 — Manufacturer LIMITED ME & FNG. D. I certify that the repair and/or alteration made to the unit( ) 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 "dual 7/2/01 John K. UrsaInspector. la f(.- U --e- 7. Approval for Return to Servl Pursuant to the authority given persons specified below, the unit dentified in item 4 w inspected "n tho manner prescribed by the Administrator of the Federal Aviation Administration and is El APPROVED 0 REJECTED Other (Specify) FM RI Standards Inspector Manufacturer Inspection Authorization BY person Approved by Transport FM Designee X Repair Station Canada Ainvorthiness Group Date of Approval or Rejection Certificate or Signature of Authorized Individual Designation No. 7/2101 EYICR782D Ronald K. Bystrom. Managa Quality FAA Form 337 (Im) SDNY_GM_02759833 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246755 EFTA01331218 NOTICE Weight andbalance or operatinglimitation changes shallbe enteredin the appropriate akciaft record. An aftamtion must be compatible with WIprevious alterations to assure continued conformity with the appacable airworthiness requirements 8. Description of Work Accomplished (If more space Is required, attach additional sheets, Identify with aircraft nationality andregistration mark and date work accomplished.) BOEING 727-31, S/N 20115, N9081E. W/O 16236. INSTALLED A UNIVERSAL AVIONICS 7T-3000 SERIES AREO-M SATCOM SYSTEM PER UNIVERSAL AVIONICS AIRBORNE SATELLITE TELECOMMUNICATIONS SYSTEM INSTALLATION MANUAL NO. 23-15-02 DATED 317/01. SYSTEM CONSISTS OF 2 EA HANDSETS, 1EA ANTENNA, I EA HIGH POWER / LOW NOISE AMP AND THE SATELLITE DATA UNIT. THESE MODIFICATIONS WERE COMPLETED USING THE FOLLOWING JET AVIATION DRAWINGS, WHICH ARE SUBSTANTIATED BY FAA 8110-3 FORMS RESPECTIVELY: WIRING DRAWING: • B727-13236-340. REV. IR. DATED 4/30/01, SHEETS I THRU 3, TITLED -TT-3000 AERO-M AIRBORNE SATEUITE TELECOMMUNICATIONS SYSTEM. REFERENCE FAA FORM 8110-3 DATED 5/29/01. BY SYSTEMS & EQUIPMENT D.E.R. NO. DERT-510087-NM. STRUCTURAL DRAWINGS AND REPORTS: • B727-16236.1340, REV. A, DATED 5/29/01, SHEETS I THRU 5, TITLED- AERO-M SATCOM ANTENNA INSTALLATION REFERENCE F.A.A. FORM 8110-3, DATED 6/18101, BY STRUCTURAL D.E.A. NO. DERT-510024-CE. • B727-16236-1342, REV. IR, DATED 5/21/01, SHEETS I THRU 7, TITLED- AERO-M SATCOM EQUIPMENT INSTALLATION REFERENCE F.A.A. FORM 8110-3, DATED 5/28/01, BY STRUCTURAL D.E.R. NO. DERT-810028-NE. SYSTEM TESTED PER UNIVERSAL AVIONICS INSTALLATION MANUAL FOR 7T-3000 SERIES AERO-M, DOCUMENT 23-15-02, DATED 3/7/01 WITH NO DEFECTS NOTED. NOTE: UNIVERSAL AVIONICS SERVICE BULLETIN NUMBER 10101.00-23-2669, BLOCKING OF BREATHING HOLES IN SATCOM ANTENNA PIN 10101-00, DATED 7/25/00, WAS INCORPORATED AT ANTENNA INSTALLATION. THIS HAS NO EFFECT OF THE STRUCTURAL OR MECHANICAL INSTALLATION OF THE ANTENNA. AN EMI TEST, REPORT NO. B727-16236.080, REV IR, DATED 6/19/01 WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. THE STATIC WADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.13-2A, CHAPTER I, PARAGRAPH 3 AND WAS FOUND TO MEET THE REQUIREMENTS OF PARAGRAPH 2. MATERIALS AND PRACTICES COMPLY WITH PARAGRAPHS 4 THROUGH 12. THE ELECTRICAL LOAD ANALYSIS UPDATE REPORT B727-16236-041, REV IR, SHEETS 1 THRU 21. DATED 06/11/2001 WAS COMPLETED IN ACCORDANCE WITTI 43.13-1B, CHAPTER II, SECTION 3, PARAGRAPH II -37. AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC 43.13-IB, CHAPTER 4, SECTIONS I, 2, 3 AND 4, CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED THE INSTALLATION CONFORM TO AC 43.13-111, CHAPTER 5. SECTIONS 1 AND 2, CHAPTER 7. SECTIONS 1, 2.4 AND 5 AS APPLICABLE. CIRCUIT BREAKERS. SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURE OR ARE MIL SPEC APPROVED FOR AIRCRAFT USE AND MEET TFIE REQUIREMENTS OF AC 43.13-1B, CHAPTER I I, SECTION 4. ELECTRICAUELECTRONIC WIRING WAS SELECTED AND INSTALLED TAW AC 43.13-1B, CHAPTER I1. SECTIONS 5-11, 13. IS, 17- 19 AND AC 43.13-2A CHAPTER 2. PARAGRAPHS 21, 22 & 27. ROUTING, LACING AND TYING COMPLIES WITH AC 43.13-IB, CHAPTER 11, SECTIONS 9-12. WIRE MARKING COMPLIES WITH SECTION 16. ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURES INSTRUCTIONS AND AC 43.13-2B, CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3, PARAGRAPH 44. A LOGBOOK ENTRY REFLECTING THIS MODIFICATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS TAW AC 43.13-1B, CHAPTER 10. SECTION 2 AND AC 43.I3.2A. CHAPTER 1PARAGRAPH 9. PER THE AERO-M SATCOM INSTALLATION MANUAL ALL COMPONENTS ARE CONSIDERED LINE REPLACEABLE UNITS AND DO NOT AFFECT THE MANUFACTURERS INSTRUCTIONS FOR CONTINUING AIRWORTHINESS. STRUCTURAL CONTINUING AIRWORTHINESS INSPECTION REQUIREMENTS ARE CONTAINED IN A.T.E. INC. STRUCTURAL REPORT ATE6112001 DATED 6/12/01, SUBSTANTIATED BY F.A.A. FORM 8110-3 DATED 6/12/01 BY STRUCTURES DER NO. DEBT-510333-CE. THERE ARE NO COCKPIT PROCEDURAL CHANGES OR FLIGHT MANUAL SUPPLEMENTS REQUIRED FOR THIS INSTALLATION. END ❑ Additional Sheets Are Attached * U.S. O.P.0 1990-781.763 SDNY_GM_02759834 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246756 EFTA01331219 May-29-01 01:5BP N J Curran 352 243 1011 P _ 02 DUARTMENT Of 111AMPORTAIION DATE Maltµ AVIATION AtIMIMSTRATION STATEMENT OFCOMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS 05/29/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Aitplanc. Radio. Helicopta. ttC) NAME Of APPLICANT Jet Aviation Associates Boeing 727-31 Airplane West Palm Beach, FL LIST OF DATA ' IDENTIFICATION TM,E B727-16236-340. Initial Release, TT-3000 SERIES AERO-M AIRBORNE SATELLITE TELECOMMUNICATIONS [fated 04130101 SYSTEM PURPOSE OF DATA In support of major aeration to Boeing 727-31. serial number 20115. registration number N908JE. APPLICABLE REQUIREMENTS (List specific sections) FAR 26.581 (ahhH1) FAR 25.1351 (a) FAR 25.889 (a)(4) FAR 25.1357 (a)(c) FAR 26.1301 (a)(b)(c)(d) FAR 25.1431 (a)(b)(c) FAR 25.1309 (a)(b)(g) FAR 25.1529 FAR 26.1316 (b) CERTIFICATION - Vat. start, we by 'Innis.NN. Arolen. onre ...nee.. dab eladrsamased Sena.. e s.,...e ...dr dar in of .1. nonstAnm••• linema. tunst...."..i............,...d....s . Nciat_ i an beet nroero. ...urea nb nlaibillierlitednMd 4 .' 4 n ...Pi> .'"Wfr at N. rani ...`.. r‘i Ur...a Itivelmies. 0 Recommtod approval of i hose data I (We)Tkrefore El Appian tam data (Swoon At Equipment Astarrets. Dellipi Approval Ooty. Don Not C.:marital Instanal 'co Approval) Slam F MOOG liZPRIMITATTIfircy DOIGMATOMNIAMiuS) cusSIIICArketin Leze.0 __ DERT-510087-NM Systems & Equipment No an urran — - ---- - II40)SUPERSEDE3 PREVIOUS ECCION CP0901-613 PTIXNANCE SC.727-SATC0MDDC SDNY_GM_02759835 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246757 EFTA01331220 SDNY_GM_02759836 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246758 EFTA01331221 U.S. DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTATION June IS. 1001 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL TYPE fahlov.Ra. ffrgetfle. ac) NAME OF APPLICANT Boeing B727-3I Airplane Jet Aviation LIST OF DATA WEN I INCA I ION Illibt Jet Aviation Aero-M Sateen Antenna Installation Engineering Drawing Boeing 727-31 / S/N: 20115/N908,1E No. B727-16236-1340, Dtd. 5/29/2001, Rev. END END END END END END END END A Note: The certification basis of this aircraft Includes FAR 25.571 Damage -tolerance and fatigue evaluation of structure. Per Advisory Circular 25.1529-I Instructions for Continued Airworthiness of _END_END_ Structural Repairs on Transport Category Airplanes, the damage tolerance and fatigue evaluation of the structure must be performed before 6/18/2002. Notes: ll The structural aspects only cf the above listed date are approved herein. 2) This approval Ls valid for the aircraft model and serial number listed below • 3) This approval is based on structural analysis on file at DER Services corporate office in Ft. Lauderdale, FL. Model No. B727-31 Serial No. 20115 PURPOSE Approve data for antenna Installation (Structures Only) OF DATA APPLICABLE REQUTRMENTS (Lt.STSPEC!PICSECTIONS7 25.301, 2.5303, 15.30S, 25307, 25.601, 25.603, 2.5.605, 25409, 15.613 CERTIFICATION- Ueda authority voted by direction of die Administrator and In accordance with condition and 1St of appointment wader Pan In of the Federal Arline,. Regulations, data hued shoe and ea attached sham numbered have been trammed In accordance veldt ateibbed procedure and found to comply with applicable mermen of the Fe Aviation RtsviadOOS. I0 Recommend 'enema of these data I Therefore pi Approve that data SIGNATURE(S) OP DESIGNATED ENGINEERING REPRESENT') E(S)DESIGNATION NI/MIENS) INASSIFICATION(S) Robert J. Begat! DERT-S10024-CE Structures FAA FORM 81103 (11.10) SUPERSEDES PREVIOUS EDITION DER SERVICES PROJECT NO. 2001.0S2 SDNYGlvl02759837 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246759 EFTA01331222 SDNYGM02759838 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246760 EFTA01331223 CCPARTMENT OF TRANSPORTATION DAIS FEOERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS May 28, 2001 AIRCRAFT OR AIRCRAFT COMPCNENT CODIFICATION MALE MODEL NO. TYPE(Mitne. Radio. hlebtoplet. etc) NAME Of APPUCANT Boeing 727-31 Airplane Jet Aviation Associates- WPB LIST OF DATA IDENTIFICATION TITLE B727-16236-1262 LSZ-860 Lighting Sensor Equipment Installation, Sht 1-2. Rev IR B727-16236-1342 Aero-M SATCOM Equipment Installation, Sht 1-7, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FM authorized personnel. r L. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE RECUREMERIZ CUR spacemen:WV FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.601 25.603 25.5810)XO 25.605(a) 25.609 25.611 25.613 25.789 CERTIFICATION - Under authority vested by direction of the AdminastRitOr and in accordance with conditions and EmItaLions of appointment under Faun of the Federal Aviation RegLiatiors, data haled above and on attached sheets numbered 0 have been alias/nod in accordance with established procedure and found to corny with applicable requIremenO of the Federal Aviation Reputations. Recommend append of Rase den. I (t$ Time:eta Approve these nets. • IS) CF DESIGNATED ENGOE (S) Si NATION NUmbut(s) I CLASSMI LOtt(S) David E. Haralson Po-re. 1-4,4-__ DERT-810028-NE Structural h RSECI ER01205.6de SDNY_GIvl_02759839 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024676I EFTA01331224 SDNYGM02759840 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246762 EFTA01331225 DIPAATISITCOTWISPORTATION . DATE FEDERAL AVIATION ADMNGSTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS JUNE 12, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MARL MODEL NO. 4A/AE OF APPLICANT ME Manum. limmum egia BOEING 727-31 AIRPLANE JET AVIATION LIST OF DATA umwrdimAnOw wns A.T.E. INC. BOEING 727-31 S/N 20115, AERO-M SATCOM ANTENNA INSTL, UPPER B.S. 360-300; STRUCTURAL REPORT OPS ANTENNA INSTL, UPPER B.S. 312-328; AIRCELL AOT.01 ANTENNA INSTL, No. ATE6I12001 LOWER BS. 400-420 DAMAGE TOLERANCE ANALYSIS; SH. 1-31, REV. (ER) NOTE- REOUIREUNSPECTIONS ATTACHED THESE DATA APPLY ONLY TO BOEING 727-31 S/t4 20115 PURPOSE OF DATA TO APPROVE • DATA FOR DAMAGE TOLERANCE ANALYSIS, B-727-31 S/1420115 APPLICABIS REQUIREMENTS (lAttswAd sada.) FAR 25-571 (STRUCTURAL ASPECTS ONLY) CERTIFICATION- Under authority wasted by &, on of the Administrator and in accordance will conditions and Senitatiera • of appointment under hri IS) oft Fehr& Aviation Itesolmions. dais :IFS *ova and on asembed dims numbered I of I have boa °unlined In accordaus with ettibfabed procedures and found to comply add' applicabk nmultesnenta i, of ow Federal AVOWS Regulagices. I (0)Tbatfose Rceommcad appronl of Approve data . SIGNATURE(S) OF DESIGNA ENGINEERING DESIGNATION NUMBER(S) CLASSIFICATION(S) 9 DERT-510333-CE STRUCTURAL wAle.mt FAA Form *110-3 OVA) se/rumen memos eomeei CeOf01413 SDNY_Glvl_02759841 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246763 EFTA01331226 SDNYGM02759842 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246764 EFTA01331227 WI= $7.41TSCC MENG DIPIAILDIT 11V403PORIAT0441:004AL "M1104 ACIYOUSTRAllat STANDARD AIRWORTHINESS CERTIFICATE I 10713114.01. 4:0 PS•getrOGRAMIIMOISOOIL • Alialair *Slat 4 OuliKAY istoewarce wow Mlle( N90/JE BOEING 727-31 20115 • TRANSPORT ♦ 14/0111/4.44404kUS Sat WILAUCC. dmilliinitoliailalmo4 past•14144/444•IMINNOM41011Bawl ofilain Etna nil* lima r ha 1•44011 14•4.44•••••••••••44,02444ninillOwlit 411•114••••••••••••••••••• 1•4104•40 41•••••••••••••••emsbutelinik4 almaam• pmid•Whaill•144COvellobaliagesICIMMOS.441141.4 lad leek Calsolls NOT • , OWS Na COMM,/ WY* •••••• ••••••••t .4404.414 • Imikee MS Is Sea aPeOhn bp Fav/s/fra almsp••••••man* ••••••• ••••••••• altallnlin milin4•1 .4•404,44.4111.14 ma NM NI Mae IMMO/ Ir=r 4 04.4101431:014011.11 R May 17 2001 S017 senalarrittilare awl svIa:errs "'l emma It . FM taialC04111.1 wibila Splis4•AmPens SDNY_GM_0275984 3 CT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, E EFTA_00246765 EFTA01331228 SDNY_GM_02759844 CT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, a EFTA_00246766 EFTA01331229 . towymeomo.a. • cowmen or........otnno..-rom...“..w..somanura. STANDARD AIRWORTHINESS CERTIFICATE • . .. .,..=... ..........era . :=7..... • wow SSOSLS DOSING 72741 20115 ?PASSPORT • ...........".................. . ..... ... .... • NOSH ... '0 .7:77-90 "JA S zu)A /-., x.4_1,7,47 ...b.. .............. FAA Fore 01004.... ....... ....... 7 TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00246767 EFTA01331230 SDNY 02/b9866 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 0024676% EFTA01331231 0 Forts, Approved OMB No. 2120.0020 MAJOR REPAIR AND ALTERATION ILE- DtPD4449191. (Airframe, Powerplant, Propeller, or Appliance) For FAA Use Only Transportation • Federal Aviation Office Montifuntion Administration - / 56 ... rt• 49 -10-... •9 / INSTRUCTIONS: Print a all entries. See FAR 43.9, FAR 43 Ardis B, and AC.43.9. I (or subsequent revision thereof for instniaions and deposition *Antis form This report is requ law (49 U.S.C. 142 I), Failure to repo rota in anion penalty not to exceed $1,000 for rucksack violation (Section 901 Federal Aviation At of I9$4 Make Model Boeing 727-31 Serial No. Nationality and Registration Mark 20115 N505LS I. Aircraft Name (As shown on registration certificate) Address (as Amon on registration certificate) NORTHWEST DELAWARE CORP 1105 N. MARKET ST 2. Owner WILMINGTON DE 19899 • 3. For FAA Use Only 4. Unit Identification S. Type Unit Make I Model _I Serial No. . Repair Alteration AIRFRAME --- (As deseribed in ikon I above) ••---•-•----•—••-- XX POWERPLANT PROPELLER 1.4' ' 4 APPLIANCE Manufacturer 6. Conformity Statement A. AgeneYs Name and Address R Kind of Agency C. Catifrcate Na TIMCO . US. Certificated Mechanic Foreign Certificated Mechanic DU4R141M Lake City Municipal Airport X Certificated Repair Station Lake City, FL 32025 Manufacturer D. Irani& that the repair and/or alteration made to the units identified in item 4 above and dmaibed on the raven* or attachments hereto have been made in accordance with requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information Punished herein is true and carat to the beta of my knowledge. Date Signature of Authorized Individual August 23, 1999 Arthur E. Saylor seniadlit4e ce 7. Approval for Return To 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 El APPROVED • REJECTED FAA Flt. Standards Manufactora Inspection Authorization Other (Spann.) Inspector FAA Daiftwe X Repair Station Person *woad by Tampon Canada BY Ainnethintss Group Date of Approval or Rejection Certificate or De:0vation No. Signature of Authorized ividest August 23, 1999 DU4R141M Scott L. Palm FAA Form 337 (12-88) This 337 supersedes 337 dated August 7, 1999 SDNY_GM_02759847 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246769 EFTA01331232 NOTICE j freight andbalance or operating limitation changes shall be enteredin the appropriate aircraft record. An alteration must be compatible with allprevious 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 completed) Boeing 727-31 Reg. No. N505LS S/N 20015 August 23, 1999 Page 1 The following major repairs were accomplished: I. 060N1-0059 Repaired corroded seat track at sta. 662 RBL 56 IAW TIMCO E.O. 99-1190 Rev. PR dated 12 JUL 99 Approved per FAA Form 8110-3 by DER Wayne Fink DER #DERT-510117-CE dated July 12, 1999. 2. 060O1-0066 Repaired corroded and delmainated skin above #2 engine pylon L/H side at stations 1342.4, I371.5 and 1387.85 Joynes DER IAW TIMCO E.O. 99-1191 Rev. lilt dated 23 Jul 99 approved per FAA Form 8110-3 by DER D. #DERY-635317-NM dated 21 July 99. 3. 060H I-0027 Engineering Repair Repaired cracked and disbonded #2 engine upper skin on aft fairing assembly IAW ROHR D. Shutrump DER #DERY-605 526-NM dated August 3, Data Sheet and FAA Form 8110-3 by DER Jeffrey 1999. SUMMARY FAA Form 8110-3's. 1. All work accomplished IAW TIMCO E.O.'s, ROHR Engineering Repair Data Sheet and 060/T-361. 2. Records of all work accomplished is on file at this repair station under work order --end- 0 Additional Sheets Are Attached us.00wormarridonnia onyx ien.resoivout SDNY_GM_02759848 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246770 EFTA01331233 ft) Pam Approved MAJOR REPAIR AND ALTERATION monk. 21204020 US. Depannum of (Airframe, Powerplant, Propeller, or Appliance) Transportation For FAA Use Only Federal Aviation e Office Identification Admbdstradon .4OO'—ear 7/ INSTRUCTIONS: Print r twee all nitrite See FAR 43.9, FAR 43 midix B sad AC.43.9.I (or subsequent revision thtreoffor inskucticas and ffispo form. This repro is requiredby Mae (49 U.S.C. 1421). Endure to rep raion °PM m tan In 4 C1•11 penalty nee to exceed 11,000 for esch such violation(Section 901 Aviation Act of ISIS) Federal Make Model Boeing 727-31 Said No. Nationality and Registration Mask 20115 N505LS I. Aircraft Name (As shown on regittration«rtificato) Address (u shown on registration cobra:ate) NORTHWEST DELAWARE CORP 1105 N. MARKET ST 2. owner WILMINGTON DE 19899 3. For FAA Um Only 4. Unit Identification 5. Type - Unit Make Model I Serial No. Repair Alteration AIRFRAME GU described titan I above) XX POWERPLANT PROPELLER TY,. APPLIANCE Manufacturer 6. Conformity Statement A. Agway's Name and Addams B. Kind of Agency C. Certificate No. TIMCO • US. Certificated Mechanic DU4R141M Foreign Certificated Mechanic Lake City Municipal Airport X Certificated Repair Station Lake City, FL 32025 Manufacturer D. I certify that the repair ancVor alteration made to the units identified in item 4 above and desaibed on the male or attachments hereto have been made in moord.uwe with requirements ofRut 43 ofthe V.S. Federal Aviation Regulations and Out the information famished herein is we and coirect to tiro tent ofmy anossIcdgc. Dale August 7, 1999 Signature otAuthorized Gregory A Christman,/ 7. Approval for Return To Service Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the FTh prescribed by the Administrator of the Federal Aviation Administration and is Z APPROVED O REJECTED FAA Fit Standards Manufacturer . Impaction Anthorization Other (SpeeiM inspector FAA Designee X Repair Station Person Approved by TransprtCuada BY Airworthiness Ciro Dale ofApproval or Rejection Certificate or DaignationNn August 7, 1999 Signature of ottL am DU4R141M FAA Form 337 (12-88) SDNY_Gh4_02759849 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00246771 EFTA01331234 . NOTICE Weight and balance or operating limitation changes shall be enteredin the appropriate aircraft record. An alteration must be compatible with allprevious alterations to assure continued confonnisy with the applicable airworthiness requirements. S. Description of Work Accomplished spaces (If more required, attach additional sheets. Identify with aircraft nationality and registration mask and date work completed.) Boeing 727-31 Reg. No. N505LS S/N 20115 August 7, 1999 Page 1 The following major repairs were accomplished: I. 060N1-0059 Repaired corroded seat track at sta. 662 RBL 45.5 TAW TIMCO E.O. 99-1190 Rev. PR dated 12 JUL 99 approved per FAA Form 8110-3 by DER Wayne Fink DER #DERT-510117-CE dated July 12, 1999. 2. 060O1-0066 Repaired corroded and delaminated skin above #2 engine pylon L/H side at stations 1342.4, 1371.5 and 1387.85 JAW TIMCO E.O. 99-1191 Rev. YR dated 23 Jul 99 approved per FAA form 8110-3 by DER D. Jaynes DER #DRRY-635317-NM dated 21 July 99. 3. 060H1-0027 Repaired cracked and disbanded #2 engine upper skin on aft fairing assembly JAW ROHR Engineering Repair Data Sheetand FAA Form 8110-3 by DER Jeffrey D. Shutrump DER #DERY-605526-NM dated August 3, 1999. SUMMARY 1. All work accomplished TAW TIMCO E.O.'s , ROHA Engineering Repair Data Sheet and FAA Form 8110-3's. 2. Records of all work accomplished are on file at this repair station under work order 060/T361. end El Additional Sheets Are Attached * us.oovaionrirrinterremoenct IM449419,40U7 SDNY_GM_02759850 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246772 EFTA01331235 1u1.21. 1999, 22:06 PDT MegNum': CPZ-LR1C-99-0 0014H Page 2 of 2 67/Z1/99 RED IS :08 FAX 9 @Oat U.S. DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS ZZL. 1 tic; 159C AIRCRAFTOR AIRCRAFTCOMPONENTIDENTIFICATION MAKE MODEL NO. TYPE Glirydone, Radio. Helicone r. err.) NAME OF APPLICANT Boeing 727 • Airplane Boeing Commercial Airplane Group IDENTIFICATION LIST OF DATA TITLE. Subject Center Engine Support Side Panel Corrosi on, Deb/ideation • Requestor: 'HMCO (CP2) for The Limited (LH) Part Number/Serial Number. 65-17556 Model No.: 727-100 SerialNo.: Registry No.: N50014 20115 Basic No.: E22I8 Variable No.: E3704 Line No.: 735 Flight Cycles: 21643 Howl: 31835 Service Bulletin/AD: N/A . . • • • CPZ-LRier89.0204-'112 'HMCO telex with description ofblindant . . Dated-9.1cl 1999 - • deltunination areas at Station* /3711S: 13S7:85 end doubler repairs to corrosion and , and 1342.4. " ' CM-Lk/09-00006H Boeing reply that repairs aiditeuthiall)lideaci Dated- /21u1.1999 • ' ey Withpreiyefions. • : - ' ''•••• -.?.t• c. '. v. .. ...,.., . . • CS...ER(699-0208TR .. :•1Th4C0 telex witlisiaiemehtiliatiep .• • .' Dated 191ul f999 afeliisi ()tea ChiliPleeeei Pei disieltition• ' ' for form. • • • • aisitresjMesi' ' - ' • ; . ' . . . . —. . . • • PURPOSE OF DATA Structural Substantiation of Repair Plan • APPUCABLEREOUIREMENTS (List spec*naiatu) CAR 4b • Subpart C: 46200 through 46.202, 41).270 Subpart D 46.300 through 4b.304( a),46.306(a)44(b) tEFITIRCATION - Hofer authority vested by (Erection of the Atbrdnistralor and In accordance with. of appoimment under Part 183 of the Federal Regulations, data listed above condldoac and limitarions i have been Guunined in accordancewith esmblishand on attached sheets numbered requirements of the Peden° Aviation Regulations. ed procedures and fouod to comply with applicab le I We) Tterefore O Recommend approval of these data . elf Approve these data SIGNATURFIs) OF DESIGNATED ENGIN NG FtEPRESENTATIVE(s) DESIGNATION NUMBER(s) CLASSIFICATION(s) 1). Joyner . DERY-635317-NM Structures FAA Form 81103 1-70) SUPERSEDES PREVIOUS EDITION Page 1 of SDNY_GM_02759551 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246773 EFTA01331236 SDNY_GM_02759852 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246774 EFTA01331237 07/15/89 15:54 FAX TURCO ENGINEERING • LAKE CITY Q002 US. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION DATE STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATION S July 12, 1999 AIRCRAFT OR AIRCRAFT COMPONEN MAKE T IDENTIFICATION MODEL NO. TYPE (S7Fanas Rada HaFxt der. eta) NAME OF AppucANT Boeing . 727 Airplane TIMCO LIST OF DATA TIMCO E.O. 99-1190, B727; SEAT TRACK: STATION Rev. l/R, 662. ROL 56 CORROSION BLENDOUT REPAIR. Dated 12 JUL 99 TIMCO REPORT NO. STRESS ANALYSIS; SEAT TRA S.A. 99-1190. Rev. VR, CK CORROSION REPAIR AT STA 663 RBL 54 Dated 12 JULY 99 END • NOTES: 1. This approval is for Nort hwest Delaware aircraft N505 LS, S/N 20115 only. PURPOSE OF OATH In support of a Major Repair accomplis only and is not Installation approval. hed on aircraft S/N 20115. This approval is for design and static analysis APPLICABLE REQUIREMENTS rya *sae satiorte) FAR 25.301. 25.305, 25.601, 25.60 3, 25.605. 25.609 and 26.613. CERTIFICATION - Under authority vested Part NM of the Federal Won by direction of dm Adrrirlistralce Regul and In at:Cadence with wilt; estabeshed procedures and rendations . data Wad above and an Seed shoals numbered condit ions and Ernitadcos ciapp to comply van applicable requir WA nave been examinedOintrnant inlet ements ofUm Federal Aviation In accordance 0 Recommend approval adie Reputations. u data I pmPlanta* 0 Approve Mese data MOROI/REM OF DESIGNATED EN&M EERING REPRESENTATIVE) • DESIGNATIONsnatasts(al CLASSIFICATION(S) ti -)C3-- DERT-510117-CE Wayne Fink STRUCTURES en A Can.. 1111&L1 /.1.2.110i beaten ELECTRONIC FORMAT (449) SCNT_GM_02759853 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246775 EFTA01331238 SDNY_GM_02759854 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246776 EFTA01331239 a- J-UK 4.00 F$ ;bliedli. Z1 FKUUKAM 2/ U.S. DEPARTMENT OF TRANSPORTATION DATE . FEDERAL AVIATION ADMINISTFtATiON STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS August 3, 1999 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (4apitme. Radio. lielicopeas dm) NAME OF APPLICANT Boeing 727 Airplane Rohr, Inc. _ LIST OF DATA IDENTIFICATION TITLE • (Ref. ERDS C1036) ERDS Cl 036 Engineering Repair Data Sheet, Definition of discrepancy and repair design for P/N dated August 3, 1999 VA545300-1 (AR Skin - Upper Skin Assembly) -. . B.. Cox Skin Disband VA545300-1 Stress Analysis Dated August 3, 1999 • PURPOSE OF DATA To submit substantiating data for a repair. This constitutes approval of the repair design only. APPLICABLE REQUIREMENTS (Ubisstific scams) (1) FAR 25.301 (1) FAR 25.307(a) (1) FAR 25.605(a) (1) FAR 25.619 (1) FAR 25.303 . (1) FAR 25.801(a) (1) FAR 25.609(a) (1) FAR 25.305(a)(b) (1) FAR 25.603 (1) FAR 25.613(a)-(d) .; • CERTIFICATION — Under authority vested by direction of the Administrator and in accordance with conditions and limitations appointment under Part 183 ofMe Pedant Aviation Regulations, data listed above and on attached of sheets numbered NONE have been examinee in accordance with established procedures and found to comply with appreable requirements of the Fedaml Aviation Regulations. I (We) Therefore ❑Recommend approval of these data Approve these data • SIGNATURE(S) OF DESIGNATED ENGINEERING E ENTATNES DESIGNATION NUmeen(3) CLASMFICKnON(S) (1) Jeffrey D.Shutrump DERY-805628-NM Structures FAA onn 8110 11-70) SUPERSEDES PREVIOUS EDITION (rammer Serlostad try Rohr. inc.) SDNY_GM_02759855 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246777 EFTA01331240 SDNY_GM_02759856 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246778 EFTA01331241 cuiss WSW. PEV. PACE ENGINEERING REPAIR Dux* ci036 nIr n RC/IMMO. I ' DATA SHEET (ERDS) enra REV. OF nu n PART NO. tisnagantom Odavict.catirca otIn • me VA545300-1 `.ART SERIAL NO. N/A SCOEL V727RE r liT kPONt FORM 81103 REQUIRED AFT FAIRING -UPPER SKIN ASSY M- al sERVCCE /CURS S UNK WA CUTOMER THE LIMITED 2 co REPAIR: OISCFtEPANCY: (8E SPEOFIC • PRWT CLEARLY) ITEM A. Repar. g ITEM A. The upper skin on the AFT faring assembly, PIN UPPER SKIN REPAIR .MA545300-1, on the #1 Engine position shows a disbonded -a condition on approxknately 50% of the AFT surface, Including 1. Remove discrepant upper skh from any. Care should be two crescent shaged cracks on an existing repair (fiben2lass?). taken not to disband the lower skin of the easy. On this same are'on the lower surface of the panel, an area of 2. Fabricate anew upper skin from .032 gauge 202443 per QQ- material is also missing and fated as above. The lower reps& A-250/5. stops before transitioning to pan down of honeycomb. 3. Remove lower surface Clad (bonding side). Do not thin below See page 2 for sketch of location and description. .029. 4. Make sure all remaining "old" adhesive Is removed from core. MATERIALS: Clean and prep sldn (using PM or Pasa-Jefl 105) and exposed Upper Skin .032 2024-T3 CIO-A-250/5 core (using Pasa-Jell 105) on panel. Clean repair area per 727' Lower Skin .016 2024-0 QQ-A-250/5 SRM 51-40-6, Par. G(2) (SRM 5140-5). Heat treated to —T42 per MIL-H-6088 5. Pane bond side of skin and core with BR-127 adhesive Honeycomb .3103/16-10(5052) MIL-C-7438 primer, per manufacturer specifications. 6. Apply two coats of FM-73 adhesive material, per manufacturer specifications. 7. Bond replacement upper skin to core and tower skin per 727 SRM 51.40-6, paragraphs E, J & K 8. Perform Post Bond inspection by visually Inspection of periphery for evidence of adhesive bead, and tap test the whole panel for voids. ORnitiGailtaiAlannals' Is land Ink IP CW I 'REPASS) SY DATE AIRWORTKNESS APPROVAL CATE Don Adams 8-02-99 sT .7----.._ £ fr,A.r4c .P-_7- ? 7 FORIINO SOW SDNY_GM_02759857 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246779 EFTA01331242 SDNY_GM_02759858 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246780 EFTA01331243 RCS NO. &v. PAGE ENGINEERING REPAIR C1036 R0HR.ING. DATA SHEET 2 OF 1.11) WonWhe (EROS) S.0. NO. oda VW CM* Mir-z» SUPPLEMENT SHEET NIA 2 (DISPOSMON CONIIUNUED) (brscerniver covriferea) LOWER SKIN REPAIR E 1. Remove existing repair (fiberglass) from discrepant area on lower surface. . - 2. Cut filler to size of discrepant area from .016 gauge 202443 per QQ-A-250/5. 3. Fabricate doubler from .020 gauge 2024-0, per DO-A- 250/5 to cove finer. Doubler to overlap filler periphery by 1.50 min. Optional to use 202443, no heat treatment required. 4. Form doubler to match lower skin contour per BAC 5300. Heat treat to -T42 per BAC 5602 or MIL-H-6083. Verify hardness per SRM requirements. 5. Inboard and outboard edges of doubler to be tapered to. .010 min. Care should be taken so the edges of the doubler land mid spaced between existing assembly fasteners. 6. Install doubler using steps 3 through 8 above. 7. Install new panel, filler & doubler using BIP fasteners to complete assembly. Apply sealant to edge of logo fight cut out . and sea all gaps at assembly. 8. Clear Abdine all external clad surfaces per MIL-C-5541, Class 3. ORIGINAL!DMILIET.... When Ibis Steam hatred Ink EOMMI E7913.11 SDNY_GM_02759859 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246781 EFTA01331244 SDNY_GM_02759860 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246782 EFTA01331245 •8-, 3-99 4:55 PM ;SUPRA 27 PROGRAM ; 5/ 8 DOOM BY B. COX DATE 08/02/99 =El PAGE 1 of 4 enK131-5frefgrATE EROS cioss ROHR TITLE Skin Disbond VA545300-1 ROHR, INC. Us or d rc of chi: infonration ts subject to the Tottrietion on the utle.3.0 or on the lint• of This document Super 27 I. Discropancy: Tho outer akin of the upper skin assembly of the aft fairing is disbanded and the aft edge of the outer skin has two cracks. See sketch below from ERDS. II. Proposed Disposition: Remove the outer skin of the upper skin assembly and bond on a new outer skin using FM 73 adhesive and BR 127 adhesive primer. The cracks at the aft odge have been reported to be along a previous repair that was filled with a fiberglass patch repair. The fiberglass patch will be removed and replaced with a metallic patch and doubler. All metallic materials will be the same as BP materials. III. Static Analysis: The aft faking is analyzed in section 10 of Reference 1. In section 10 of Reference the substructure has been analyzed to withstand all the aerodynamic loading without using any of the skin as affective. Therefore, this analysis will only investigate the capability of the adhesive to carry the shear stress to the core conservatively assuming that the skin will carry the aerodynamic loading. Strut Stress Analysis (VA-CR154 Rev. C) SDNY_GM_02759861 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246783 EFTA01331246 SDNY_GM_02759862 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246784 EFTA01331247 8- 3-99 4:55 PM ;SUPER 27 PROGRAM 8/ 8 ❑❑❑1J BY B. COX DATE 08/02/99 ❑❑❑❑ PAGE 2 of 4 CHK13 EROS c1036 DATE ROHR TITLE. Skin Disband VA545300-1 ROHR, INC. the or disclosure of this infant-stain ts subject to the restriction on the htle Age ce- 071 the stint page of this clxument The noted adhesive primer is compatible with the adhesive as shown in the excerpt of MIL-HDDK-337 at the end of this analysis. Conservatively assume all the aerodynamic load is reacted by a 1.0-Inch wide by 30 inches long beam that is simply supported between the fuselage and outboard edge. The core shear stress (L) is expressed by f c = V / hb where V is the vertical load being reacted at the supported end h is the centroid distance of the sandwich panel h = t/2 + to/2 + t b is the beam width From page 10.7 of Reference', the aerodynamic pressure (P) on the aft fairing Is .5 psi limit (.75 psi ult). Therefore the ultimate vertical load at one end of a simply supported beam is V = .75(30)(1.0)/2 = 11.25 lbs (ult). From VA545300, t = .016, to = .032 and t, = .30. h = .016/2 + .032/2 + .30 = .324 in f c = V / hb = 11.25 / .324(1.0) = 34.7 lbs/in2 From the certification sheet shown at the end of this analysis, the allowable lap shear for the FM 73 adhesive is 6.523 psi at 75° F. Since there is nu test data readily available for this adhesive system for core bond, a comparison of this adhesive system will be made to EA9649R (RMS 058). From figure 3.3.2 of Reference 2, aluminum core and face sheet with EA9649R adhesive has an allowable of 220 psi for the BP core configuration. Since the lap shear for the repair adhesive is significantly higher than EA9649R (2,838 psi at 75° F), it is reasonable to assume that 34.7 psi core shear Is acceptable for this adhesive system. The repair at the aft end of the faking is acceptable by inspection since the aerodynamic load is very little to nil at this location. IV_ Fatigue Analysis: Repair is acceptable for fatigue strength by inspection since the ultimate margin is high and there are no additional stress concentrations compared to the type design. Meth anIcal Design Allmables (RI IR 85 -013) SDNY_GM_02759863 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246785 EFTA01331248 SDNY_GM_02759864 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246786 EFTA01331249 8- 3-99 4:55 PM ;SUPER 27 PROGRAM 7/ • DODO BY B. COX DATE 08/02/99 DODO PAGE 3 of 4 cHXD EROS C1036 DATE ROHR Tine Skin DIsbond VA545300-1 ROHR, INC. disckme iefenurtton Ie HAdeci A, Me =Waft OA the thic OeMW on dlefintrast Of lath domanant 812D4058K-337 1 Ammmber 2882 I II lit 1 I i Ji I Si l . , 1 .i .. E . i, 1 11 it 11 ... ill - €4 H i 1g 1g :1is 1-s I 1 1I i 4 A i gx 0 .z g j • li 02 i ai # ; i -,i 1 I- 8 i ri 9. n in k ii LIE , i iss 1 .I i 1 — = .-•-•. ≥ i 1 z • 44 SDNYGivl_02759865 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246787 EFTA01331250 SDNY_GM_02759866 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246788 EFTA01331251 8- 3-99 4:55 PM ;SUPER 27 PROGRAM ; 8/8 DOM av E. COX DATE 08/02/99 PAGE 4 of 4 CHICO ERDS C1036 DATE ROHR TITLE Skin Disbond VA545300-1 ROHR, INC. useQf nisch:num omit InnermatIon s rublect to the rowletIon on the tie.Pluto or on the Bntpax. document of = R am's Willisaws Men S akalg CBRTKrrewom COLD •111400-LARD CITY TO P.O. BOX 1909 LANK Clry YL. 32026 sale TIMC0-1.14102 CITY To =GMAT 90 EAST Zat.,TAZ =Ma 20uTE 19, NOR 1029 OOR ORDER IA= CITY 0023439/001 FL 32026 CUSTOMER DArm SHIpPRD ORDER 690376 06/17/99 pRoDucr BMW* 28CEIPTION . mix 49132 rig 7111 .06 rSV 3 • ASR Flaw MS00101202 5 .00 ET7 RECOOLMENDED GTORA23-- 12 Nouth0 FROM maw OP SWIM AT oR DZZOW BETEMENT 0 negrsoo P --------....... DEA5 BATOR/OBIT MID BATCH// TIT NUMBER DATE NUMB= fratiljTACMXW 2742-037 aVS.13,1000 (=WITT am in 274 300.00 SF 02 TOTAL 1. WATCH OTT - sou.00 k TOTAL-, Ise TOTAL OTT 600.00 4.* ISIS CgRTIP2a4 TES DUITNRIA4 AT tD or 0131/e/0252 001052900; To APPLICABLE: DRNMINGS AND BectIFICATIOU3 MOT= USLOW. SPECIFICATTOBg: • MW-Ar/32 RSV B. TrAW-2 ran I CLASS 2 FORK P CROW 3 6747a 21132BEaVii OR PR2/092 MOTES ALv4EXPTANC72 PBSKIIRM2012 3 AS PART OF a Clic PART XDP2CIVII CYST2m- TUR-1 AE3 cemy TO BR USED WITH TNS mATC22K40 Arcarvt OR PIXTFEMX TD WADI CESTIPICAT/ON. SEE CYTEC FOR Aliti I I? trgg 42928TM:ice.* TEST A A 76 F LAP 9KRAR 40 180 F [iRs.9. stag, 6704. 6622, 6122 Psx 4s3R, 4370, lave. 4260, Rsxs Pai VTBIC:tir .061, .061, .062 Par OA ADTKORI2RD SIgZIA.TORS e1/ 224ljl e /$2r 4r 9 /C : lAng7JVcr LZ )1gdng: Pid fre:C eg-C -g .-40224-Nalflal SONY_GM_02759867 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246789 EFTA01331252 • SDNY_GM_02759868 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246790 EFTA01331253 Work Order 43736. . Fonn Approved i . , 4. . IfIII MAJOR REPAIR AND ALTERATION"' 'a'. • "'"• OMB No. 2120-0020 US Dopitimontol " • ' • • ' • t For FAA Use Only •• T importation (Airframe, Powerplant, Propeller or Appliance) - "" ' ' wwwkoriwa •• • - •• • . .... .. , Office Id ratification U % ot . idailalsin00. T -; I ap'--.. • • ‘.. • INSTRUCTIONS: Print or type al entries. See FAR 43.9, FAR43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for InstrucUons and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penally not to exceed 51.000 for each such violation (Section 901 Federal Aviation Act of 1858). • •. Make Model •• . . / 1 r"'Ir .. •- • ..'.:. .. ,r: I 1. Aircraft Boeing N 727-31 j • 1• 1 • l • ” I Serial No. •4 : Nationality and Registration Mark •. 20115 N505LS Name (As shown on registration certificate) . j i., :4 Address (As shown on registration certificate) .., . . , 2. Owner Northwest Delaware Corporation. 1105 N Market St . • " Wilmington, DE 19899 3. For FAA Use Only -The data identified herein complies with the applicable airworthiness requirements and Is approved only for the above described aircraft, subject to conformity Inspection by a person authorized In FAR 43, s Ion ••. . 43.7 20fr %deaf / GL-CMH FSDO aura of FAA Ins cler fJetsus Zubia - Unit Identification 5. Type Unit Brake '. "a" h' . 1‘ I. • Model . , . Seder NO. Repair Alteration ' . ....... ..................... AIRFRAME . Jetta:dee:We Kem 1above)A.ri ,,,., , , c.o., ,„.....,. ? . . .. . . ... X • •' • - ' ••••. POWERPLANT • • . . •• "..f P! 'n tr ;,. f ' • ". I. .. i i AI An.. • r.•:•' ":" . A' • PROPELLER ' • -ri ntsx,;• ' 'IV • Typo ,. APPLIANCE Manufacturer ' I ' • 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Cedificate No. ElectroSonkS U. S. Certificated Mechanic • • Repair Station AE1R005K. 4391 International Gateway Foreign Certificated Mechanic Radio Class 1.2 8 3: Instrument Port Columbus International Airport X Certificated Repair Station Class 3, Accessory Class 3 Cotentin, OHIO 43219 Manufacturer Limited Altimeter D. I certify that the repair andfix alteration made to the unit(s) Identified in item 4 above and described on the reverse or attachment; hereto have been made In accordance with the requirements of Part 43 of the U. S. Federal Aviation Regulations and that the information furnished heroin Is hue and correct to the best of my knowledge. Dale Signature of Authorized indi April 28, 1999 - • • - - • - • •-- - • • • - 7. Appro al Rot Service l I - ' 4 Pursuant to the authority given persons specified below, unit id n item 4 was I spelled In the manner presented by the Administrator of the Federal Aviation Administration and is ID APPROVED 0 REJECTED i'.: ' I • FAA Fit SLindards InSpectot Manufacturer Inspection Authorization Other (Specify? . . .... - • rtz:: BY FAA Designee X Repair Station Person Approved by Transport 1•.1 ii. . •e •1 I• Canada Airworthiness Group Date of Approval or Rejection 1 .• Certificate or Signature (Authorized Ind hi I Designation No. . , r • q -di -"Ii AE1R005K . — --• - --- ' SDNY_GM_02759869 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024679I EFTA01331254 NOTICE V. 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 shoots. Identify with aircraft nallonakty and registration mark and date work completed.) . • 1. The following equipment was removed from the aircraft: PART NUMBER QTY MAKEJMODEUDE.SCRIPTION STATION 622-7203-101 3 Collins VHF-422b Comm C37c, C38c 450.0 2. The following equipment was Installed In the aircraft. • INSTALLATION PART NUMBER QTY MAIEJMODEUDESCFtIPTIoN TSO STATION DATA • 822-1115-001 3 Collins VHF-422c Comm C37c, C38c 450.0 523-0772719 3. The above work was accomplished IAW FAA Advisory Circular AC 43.13-16, Chapter 11,12 and AC 43.13-2A, Chapters 1, 2. 4. This work has been accomplished under ElectroSonics Work Order 43736. •. 5. Removed existing Collins VHF-422b corn's to accomplish 8.33lan modifications Collins S.8.17. Following modification, reinstalled as VHF-422c and performed a complete operational check. 6. A complete test of the installation of the modified unite has been conducted to confirm that other aircraft systems are free of interference as a result of this Installation. All tests found to be satisfactory. 7. Collins does not specify any new continued airworthiness instructions for the above equipment The owner/operator should consult the Boeing maintenance manuals for general avionics continued airworthiness requirements. 8. The owner/operator must comply with manufacturer's maintenance instructions to ensure continued airworthiness any time the above equipment Is removed and/or repaired and reinstalled. 9. The aircraft Weight and Balance is unchanged and Equipment List has been amended. 10. The aircraft must be loaded JAW the prescribed loading'Information from the manufacturer. END • 0-3 II-1 2 54 3-0 C-1 C.4 £4 ti-Iffil 54 134 I {4 C-2 A4 44 04 *4 . vans, storm A3 . 7 04 0-41 .,Ni — 31999 04 AeR 2 8 1999 1 1A ii.f. . r i; Al , C-3ci,„I,,„„ commas es kieto 04 34 4e SC 0-6 04 0-t ..,..,s. C-9 i C4 I65 COIULI10ON 1A41 11410 A-9 . 1,7 - 1-7 A-/ 04 C-4 C-S 311 A40 A-8 .A.7 All 0 Additional Sheds Are Attached r • U.S. GPO:1991-0-568-012/40035 SDNY_Glvl_02759870 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246792 EFTA01331255 vo• :•16 r.., : Work Order 43736. , Form Appmved . • : r. •Ir • :. 01 MAJOR REPAIR AND ALTERATION''' •• • 1 OMB No. 2120-0020 US Departrnoce el (Airframe, Powerplant, Propeller or Appliance) , For FAA up Only ' Pampa, Ike foams 440444 • • • 4eninfoneen e.' . 27: -. GL07 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43Append& 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 • 1 1.•1 . . : ' t . -4I ' , ''..1 :k i. Boeing ‘11 . . 1. Aircraft 727-31 Serial No. Natronafty and Registration Mark 20115 • • N505LS Name (As shown on registration certificate) ::., Address (As shown on registration credilicale) 2. owner' Northwest Delaware Corporation.. . . . ..1105 N Ilarket St 111/11n4nOpp, DE19899 ' . .. • 7 . :: : c .. 3. For FAA Use orgy • •I"i :7 - The data Idenktred herein complies with the applicable airworthiness requirements and is approved only for tho above described aircraft, ..., .. . ...,, subject to conformity Inspection by a person authorized In FAR 43, section 43.7 / 4 17 4 07 • GL-Clitti FSDO . Dale tura did/ , r Jesus Zubla • • • ' • ;,'• 4; Unit Identification S. WIN . .,,.. ,:., .• .: f. •.,'• • r. ol . 4. :. •.;i:i:.:. Unit Make - Model .StnialNo. Ntecation AIRFRAME . , . .. , • a deSeriberd ill lien, t above). et .17•I7..arr.”, .rr f • • ! , •. ; X POWERPLANT . .,,,gur•r• •••• .4 e 't ".' 1 PROPELLER Type • .' '.• *. • • •• r• - '• Or • APPLIANCE Manufacturer • .. . 6. Conformity Statement A. Agency's Name and Address. : B. Kind of Agency • • •- '' ''• t 1. ' • C. Certificate No. - • EledroSonics U. S. Certificated Mechanic Repair Station AE1R005K . 4391 International Gateway Foreign Certificated Mechanic Radio Class 1,2 & 3: Instrument Port Columbus International Airport X Certificated Repair Station Class 3. Accessory Class 3 Columbus, OHIO 43219 Manufacturer Limited Altimeter D. I candy that the repair *miler alteration made to the nit(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 knondedge. Date Signature of Au orized Ind i ; . r.1 , .. .—• .. April 28, 1999 i N / i ....> i :. *c.-- . 7. Approval or turn o nice : Pursuant to the authority given persons specified below, the un Idea In m4 was inspected in the manner preacnted by the Administrator of the Federal Aviation Administration and is CIAPPROvED FAA Fl Stanclaxis 0 REJECT® ?. i ()poi :.) c leSpectof Manufacturer Inspection Authorization Other (S , BY • ..; FAA Designee X Repair Station Person Approved by Transport Lt- \ ; Canada Airworthiness Group I Date of Approval or Rejection Certificates Signa r of Authorized ' ual Designation No. • Li - 11 - 99 AE1R005K - -- - - --- 'BM SDNY_GM_02759871 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246793 EFTA01331256 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 Conformfty 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.) 1. The following equipment was removed from the aircraft: PART NUMBER CITY MAKEJMODELJDESCRIPTION STATION 622-6520-005 2 Collins CTL-22 200.0 622-6520-005 '1 Collins CTL-22 • 259.5 2. The following equipment was Installed In the aircraft. MAKEJMODEUDESCRIPTID4 INSTALLATION PART NUMBER OTY ill:) .. STATION. DATA 822-1120-005 2 Collins CTL-22c C37c, C38c 200.0 523-0072719 • : 822-1120-005 1 _ Collins CTL-22c . I. i C37c, C38c, 259.5 • The above work was accomplished IAW FAA Advisory Circular AC 43.13-1B, Chapter 11,12 and AC 43.13-2A, Chapters 1, 2. ' ••• ' ' 4. This work has been accomplished under EiectrOSonics Work Order . 43736. 5. Removed existing CTL-22 to accomplish the 8.33KHZ spacing modifications Collins S.B. 31. Following modification, reinstalled units'and performed a complete operational check. 6. A complete test of the installation of the modified unite has been conducted to confirm that other aircraft • systems are free of interference as a result of this installation. All tests found to be satisfactory. 7. Collins does not specify any new continued airworthiness instructions for the above equipment The owner/operator should consult the Boeing maintenance mahuais for general avionics continued airworthiness requirements. 8. The owner/operator must comply with manufacturer's maintenance instructions to ensure continued ; airworthiness any time the above equipment is removed and/or repaired and reinstalled. I . 9. . The aircraft Weight and Balance is unchanged and Equipment List has been amended. _ . • 10. The aircraft must be loaded lAW the prescribed loading information from the manufacturer. END A-1 0-1 41-1 2 S•A S•0 C-1 C-2 A4 2.1.p I 34 1S-0 I C-1I C.4 A-2 0-2 A-2 04 ctcfRI0 - SCW* .A.3 A-3 0-9 61 ' 0. Alit( 28099 A.4 :•iiii ''' 3 0 ) le5 .- •A oJ ..,„ 1500 COLO:ABU 014 ii, GIN SDO• • •FOill. A ,, 4.. , 0) C-3 I C-4 I C411.41 I A.I0 1.-9 A-7 0-7 1 c.-a e-e, C4 A4I -1.-10ii.-9 it' A4 04 i . • . 01 O Additional Sheets Are Attached . U.S. GP0:1991.0-568-012140035 SDNY_GM_02759872 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246794 EFTA01331257 Form Apprrsed OMB No. 2120-0020 r MAJOR REPAIR AND ALTERATION uS OeParencs (Airframe, Powerplant, Propeller, or Appliance) For FM Use Only d Transportaion Oftioe Identification .e44. Federal Aviation AdmInIstreUen Asto-o 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 disco:Won of this foot This form is required by lay (49 U.S.C. 1421). Failure to report can mutt in a civi penalty not to exceed $1,000 for each such volition (Section 901 Federal Aviation Act of 1958). Make Boeing Mom 72741 1. Aircraft Serial No. Nationality and Registration Mark 20115 N505LS Name (As shown on regStra0an certificate) Address (As 5/10W77 on registration cettiatte) 2. Owner Northwest Delaware Corp. 1105 N Pdaltit atrii .. WilmIngin, 98 1. 4 3. For FAA Use Only Alki 1 0 1C93 CM-DALLAS SW05 4. Unit Identification 5. Type Unit Make Mo0el Serial No. Repel( Altera= AIRFRAME (As described in item 1 above) X X POWERPLANT • PROPELLER Type APPLIANCE Manufacturer 6. Conformity Statement A. Agencys Name and Address B. Kind of Agency C. Certificate No. V.S. Castrated methane TX2Ft203L Associated Air Center 8201 Lemmon Avenue Foreign Certificated mechanic Airframe Class 3 & 4 Dallas, Texas 75220 Radio Class 1, 2 & 3 X C,ertifcated Repair Staten Menvfackuer a i certify that the repair an/or alteration made to the unit(s) Identified in hem 4 above and described on the reverse or attachments hereto have been made in accords= with the requirements of Pal 43 of the U.S. Federal Aviation Regulatory% and that the information furnished herein is true and correct to the best <limy knomedge. Date Signature of Authorized IndMdual 8/4/98 ›rionjA 1141 O °— 7. Approval for Return to Service Pursuant to the authoritygiven persons specified bele", the unit Identified in item 4 a inspected m the reamer prescated by the Administrator of the Federal Aviation Administration and is ®APPROVED 0 REJECTED FAA Ft Standards Other (Specify) Manufacturer insponionAuthorizarlon Inspector BY Person Apfund ly Transpal FM Designee x Rent Station Canadian Ainvalhmess Group Date of Aquae' a Rejection Certificate or Signature cfAuthatted IndiAdu.al Designate No. 814/98 TX2R203L 71i,a- 4/ 40 141.4rdler—• orrn 337 (1248) SDNY_GM_02759873 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246795 EFTA01331258 NOTICE Weight and balance oropereting 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. Description of Work Accomplished almore space is require; attach addoxial sheet& meow wen aircraft nationality and leglerallco mark and Ode work completed.) Aircraft: Boeing 727-31 Aircraft Total Time: 31,675.6 Registration #: N505LS Aircraft Total Cycles: 21,567 Serial #: 20115 August 4, 1998 The following alteration was accomplished at Associated Air Center, Dallas, Texas under Work Order 1565. 1) Mode "S" Transponder ICAO Code Strapping Change in accordance with AAC Drawing 1565-001 Rev A dated July 28, 1998, 8110-3 approved by D.E.R. SW-997, David A. ICimbrell July 29, 1998. The following repair was accomplished at Associated Air Center, Dallas, Texas under Work Order 1565. 1) Repair - L/H Horizontal Stabilizer Trailing Edge Beam at Elevator Station 156 in accordance with AAC Repair Drawing 1565-002 dated July --, 1998, 8110-3 approved by D.E.R. SW-810, Robert IV Manashi August 4, 1998. **************************END************************** ❑ Additional Sheets Am Attached U.S. GOVERNMENT PRINTING OFFICE: 1992-769-012/60167 SDNY_GM_02759874 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246796 EFTA01331259 DAK-98-089 OrlArnewr OF TautaPORTATION DATE FEDERAL AVIATioN ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS JULY 29, 1998 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE ( 41Irplano, Radio, Holleoptist, NAME OF APPLICANT BOEING 727-31 eta.) ASSOCIATED AIR CENTER AIRPLANE DALLAS, TEXAS LIST OF DATA IDENTIFICATION 1TTLE 1565-001 MODE S TRANSPONDER ICAO CODE STRAPPING CHANGE REV. A 07/28198 ' I ... : • iikl. NOTES: TC DATA SHEET A3WE. ELECTRICAL DESIGN ASPECTS OF THIS DATA IS APPROVED. THIS APPROVAL APPLICABLE TO B727-31 Sits; 20115 ONLY. THIS 8110-3 FORM IS IN SUPPORT OF FAA FORM 337. PURPOSE OF DATA TO SUPPORT THE AVIONICS/ELECTRICAL MODIFICATIONS. APPLICABLE REQUIREMENTS (List specific sactrons) FAR 25.1301(a)(b)(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 0 have been examined In accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. Recommend approval of these data M I OM Therefore Approve these data SIGNA\URE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE/Si DESIGNATION NUMBER(S) CLASSIFICATION(S) 7 i i DAVID A. KIMBRELL SW-997 AVIONICS/ELECTRICAL SYSTEMS /L.-/e2ezbear ylo 7 -1: 71/../ ... FAA Form 8110-3 0140) s. ‘FTIFS ', Remus Ecmom( COMPUTER GENERATED) GPO 1,01413 SDNY_Gtv1_02 759875 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246797 EFTA01331260 SDNY_GM_02759876 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246798 EFTA01331261 AUG-04-1999 10:39 ASSOC AIR 214 357 2845 214 357 2845 P.01 U.S.OEPARTmENTOFTPANsPoRTATION DATE #98421 GEDERALAVIATIONADMINI8TRATION AtIO03T Oil, 1992 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS _ AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MARE MODEL NO. TYPE (seats. was en) NAME OF APPLICANT 307.1NO 727-31 AIRPLANE A280CIATZI1 Alit (N5001.3) - CENTER LIST OF DATA IDENTIFICATION TITLE ASIOCIATrD ALA Car= DUNI= NO. 1565-002 REPAIR - L/H HatazzoNTAL STAB:LIZ= T/t OPFER SIM - SLEW STA ASV. "IR', 136. DATIO 07-29-1928 (Slat 1, 2 AND 3 or 3). 140725: 1. THE STRUCTURAL A3PiCTS ONLY Or TEE ABOVE LISIID RATA ARP arrimmoo tronasn. suss APPROVAL 28 roil ens ENGIUMMIro DESZON DATA ONLY. 2. THIS APPROVAL 13 VA.= ONLY FOR HOEING MODAL NO. 727-31, AIRCRAFT 2/N 20125 AND Is ism= IN St719PCCRT Or A MAJOR REPAIR Or THY SUBJECT AIRCRAST. PURPOSE OF DATA IN SUPPORT OF A WAJOA AMUR ON HOEING )DOLL NO. 727-31, AERCFATI 3/N 20115. APPLICAELE REQUIREMENTS as %vox sae CAR 41).200 (a) , (b) , 41).201 (11) , (b) , (e) , tb.202, 4b.300, tb.301, 4b. 302, 417.903, 4b.304 (al , (b), 4b.308 (a) , (b), (d) • CERTIFICATION - Under authority vested by &U MW of the AdmIntStrator and in accordance with conditions anti limitations of appointment under Part 183 of Ma Federal Aviation Regulations, data listed above and on attached sheets numbered ,J00C0000000000CCOOL have been examined in accordance with establithad procachuta and found to comply w*h appliCable requirnmentS of the Federal Aviation Reaulelions. INI Recommend Approval et these data I (WI) THEREFORE o Approve these data aloNtrauRgiinoro a t i. ENGINEERINGREe 6EWATIMS) 0664NATIONNUMWM) cutiSSIFICATION(8) 8W-910 ariUnEvara Rama K AI ze 0 /.7C)10.1ZUZINS1 PASYLOP1 ISIM0N c_ri A -• r)e.e5 . TOTAL P.01 SONv_GIvi_02759877 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246799 EFTA01331262 SDNY_GM_02759878 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024680() EFTA01331263 •• 00...••••1 OP IIIMMOSTA.M= "aal...1•IMMUIONI STANDARD AIRY/00711MM C10111FICA72 • ••••••••••••./0 •••• =ten.. Weee•••• MOM BOUM 727-31 20115 122112PORS •••••••Pkir..0 0.10••••••4 B 07-23-90 cum FAA form 81004 oah T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00246801 EFTA01331264 SONY_GM_02759880 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00246802 EFTA01331265 • Approved FOOT, Om% MAJOR REPAIR AND ALTERATION US Department (Airframe, Powerplant, Propeller, or Appliance) or se nly of Transpartation Federal Aviation Administration PAAGONLLAS rA.\, (A/C- MO; INSTRUCTIONS: Print or type ell entries. See FAR 43.9, FAR 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for Instructions and disposition of this form. This form is required bylaw (49 U.S.C. 1421). Failure to report can result in a cm penalty not to taceed S1,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model Boeing 72741 I. Aircraft SCSI No. Nationality and Registration Mark 20115 N500LS Name (As shown onregisfration certificate) Address (As shown on registratbr: cofttecate) 2. Owner Northwest Delaware Corp. 1105 N Market St. Wilmington, DE 19899 3. For FAA Use Only 1. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteralion AIRFRAME (As described in item 1 above) X X POVVERPLAfT PROPELLER Type APPLIANCE Manufacturer 6. Conformity Statement A Agencys Name and Address B. Kind of Agency C. .Certificree Nor- • Associated Air Center U.S. Certificated Mechanic 8201 Lemmon Avenue Foreign Certificated Mechanic •• TX2R203L., .. • • • Dallas, Texas 75220 Class 3 & 4 X Certificates Repair Stason Manufacturer D. I certify that the roper and/or alteration made to the wigs) identified in item 4 above and described on the remise or attachments hereto have been made In accordance with the requirements ci Part 43 of the U.S. Federal Aviation Regulations and that the inforrrigion furnished herein is true and correct to the test of my knowledge. Date Sig of Authorized kern OW 812197 fi . 7. Approval for Re Service Pursuant o the authoritygiven persons specified below, the unit identified tern 4 was inspected in the manner prescrited by the Administrator of the Federal Aviation Administrtmen and is (JAPPROVED QREJECTED FAA FN. Standards Other (Specify) Manufacturer Inspection Authortzation Inspector BY FAA Detente Person Approved hy Transport X Repair Station Canadian Akworthmess Group Dale of Approval a Relection Certificate or Signalise Individual Designation Na S iore. .e_____ 8/2/97 TX2R203L - - - --- SDNY_GIvl_02759881 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246803 EFTA01331266 NOTICE • appropriate aitraft record. An alteration must be Weight and balance or operiling limitation changes shall be entered in the the applicable airworthiness requirements. compatible with all previous alterations to assure continued contort:lily with 8. Description of Work Accomplished kin** with aitaart amount), and regiStatiOn mark and date work corn#eted) Itl mere spice is rtio.iised attach adational sheets Aircraft: Boeing: 727-31 Aircraft Total Time:31,471.2 Registration #: N500LS Aircraft Total Cycles: 21,468 Serial #: 20115 August 2, 1997 The following work was accomplished at Associated Air Center, Dallas, Texas under Work Order 1476. 1)Repair - Airstair Door Actuator Attach Clip in accordance with AAC Repair Drawing 1476-001 IR dated July 16, 1997, 8110-3 approved by D.E.R. SW-916, Jim Martin July 22, 1997. 2) Repair - #1 & #3 Pylon Corrosion on Forward Engine Mounts in accordance with AAC Repair Drawing 1476-002 IR dated July 17, 1997, 8110-3 approved by D.E.R. SW- 916, Jim Martin July 22, 1997. 3) Repair - #8 Leading Edge Slat Crack at 1/B Slat Guide in accordance with AAC Repair Drawing 1476-003 IR dated July 17, 1997, 8110-3 approved by D.E.R. SW-916, Jim Martin July 22, 1997. 4) Repair - Corrosion on R/H Wing Upper Surface at WBL 70.5 Between Str. 1 - 14 in accordance with AAC Repair Drawing 1476-004 IR dated July 21, 1997, 8110-3 approved by D.E.R. SW-916, Jim Martin July 22, 1997. 5) Repair - Floor Beam BS 600, RBL 25 Figure $ Hole in accordance with AAC Repair Drawing 1476-005 IR dated July 22, 1997, 8110-3 approved by D.E.R. SW-916, Jim Martin July 22, 1997. 6) Repair - Aft B/B Door Interior Structure Cracked in accordance with AAC Repair Drawing 1476-006 IR dated July 22, 1997, 8110-3 approved by D.E.R. SW-916, Jim Martin July 22. 1997. 7) Repair - Wing to Body Fairing Damaged Dome Nut in accordance with AAC Repair Drawing 1476-007 IR dated July 25, 1997. 8110-3 approved by D.E.R. SW-916, Jim Martin July 25, 1997. 8) Repair of Center Engine Exhaust Nozzle in accordance with Rohr, Inc. Engineering Repair Data Sheet No. C0625 Rev. A dated July 23, 1007, 8110-3 approved by D.E.R.(s) NM-2731, Jeffrey D. Shutrump for Structures, NM-738, Tony Bradlaugh-Dredge for Powerplant and NM-2182, Michael August for Special Administrative July 23, 1997 and AAC Repair Drawing 1476-008 IR dated July 25. 1997. 8110-3 approved by D.E.R. SW- 916, Jim Martin July 25. 1997. S eAddsonal SIvrais Are AlleNte0 U.S. GOVERNMENT PRINTING OFFICE: 1992.769-012/80157 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, and 17 SDNY 15,027591382 EFTA 00246804 EFTA01331267 Aircraft: Boeing: 727-31 Aircraft Total Time:31,471.2 Registration #: N500LS Aircraft Total Cycles: 21,468 Serial #: 20115 August 2, 1997 9) Autopilot Interface Unit Modification in accordance with AAC Drawing 97-2211- 210 IR dated July 28, 1997, 8110-3 approved by D.E.R. SW-880, John W. Goswick July 28, 1997. END SDNYGlvl_02759883 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246805 EFTA01331268 SDNY_GM_02759884 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246806 EFTA01331269 U.S. DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION 7/22J97 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Alrotene, Radio, Helicopter. etc.) NAME OF APPLICANT BOEING 727-31 AIRPLANE ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-001 4-- REPAIR - AIRSTAIR DOOR ACTUATOR ATTACH CLIP REV. IR 7-16-97 THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 INSPECTION PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (Ust specific sections) CAR 4b.200 .301 .305 .201 .302 .306 .202 ..303 .307(c) .300 .304 CERTIFICATION • Under authority vested by direction of the Administrator and In accordance with conditions and britallons of appoirtment under Part 183 of the Federal Medico Regulations, data listed atom and al attached sheets numbered el oe oC have been exemined In accordance lab established procedures and found to comply vAib applicable requirements of the Federal Aviation Regulations. MI Recommend approval of these data I .00) Therefore I= Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) 57.: . ._..., JIM MARTIN SW-916 STRUCTURES _.. _ GPO 901-613 SDNY_GM_027598B5 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246807 EFTA01331270 SDNY_GM_0275.386 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246808 EFTA01331271 ARC.11.IS1 U.S. DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION 7/22/97 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane. Radio. Helicopter. etc.) NAME OF APPUCANT BOEING 727-31 AIRPLANE ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-0021" REPAIR - # 1 & # 3 PYLON CORROSION ON FWD ENGINE MOUNTS REV. IR 7-17-97 THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 INSPECTION PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List specific sections) CAR 4b.200 .301 .305 .201 .302 .306 .202 - .303 .307(c) .300 .304 CERTIFICATION - Under authority vested by direction of the Administrate' and In accordance with conditions and ambitions of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered te. se 41 have been panned In accordance se established procedures and found to comply with applicable requirements lathe Federal Aviation Regulations. BEI Recommend approval of these data I Ve4 Therefore rXi Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATIONS) JIM MARTIN SW-916 STRUCTURES 7r -76 _.. _ ...._ _ ... _ GPO 901.813 SDNYGIvl_02759887 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246809 EFTA01331272 SDNY_GM_02759888 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246810 EFTA01331273 AitiC•17. ISE U.S. DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION 7/22/97 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio, Helicopter, etc.) NAME OF APPLICANT BOEING 727-31 AIRPLANE ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-00317 REPAIR - # 8 UE SLAT CRACK AT I/B SLAT GUIDE REV. IR 7-17-97 THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 ON INSPECT\ PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List specific sections) CAR 4b.200 .301 .305 .201 .302 .308 .202 - .303 .307(c) .300 .304 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and Imitalims of appointment under Part 183 of the Fedora/ Aviation Regulations, data listed above and on attached sheets numbered re 44. re have been comined in accordance wilts established procedures and found to comply vieh applicable requirements of the Federal Aviation Regulations. (=Recommend approval of these data I 20) Therefore Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) JIM MARTIN SW-916 STRUCTURES 7 : _.. _ can (11-70 EDITION) GPO 9014313 SDNY_GM_02759889 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246811 EFTA01331274 SDNY_GM_02759890 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246812 EFTA01331275 RAC•c11.15 U.S. DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION 7/22/97 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane. Radio, Hetcopter. etc.) NAME OF APPLICANT BOEING 727-31 AIRPLANE ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-004 L." REPAIR CORROSION ON R/H WING UPPER SURFACE AT WBL 70.5 REV. IR 7-21-97 BETWEEN STIR. 1 - 14 THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 INS? ECT ION PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List specific sections) CAR 4b.200 .301 .305 .201 .302 .306 .202 -.303 .307(c) .300 .304 CERTIFICATION - Under authority vested by direction of the AdmInkstrator and In accordance with conditions and riflery; of appointment under Part 183 of the Federal Aviation Reptile/king, data listed above and on attached sheets numbered SC. at re( have been examined in accordance with established procedures and found to comply vett appdcable requirements of the Federal Aviation Regulatiors. NM Recommend approval of these data I (Wic) Therefore II 9 Approve these dela SIONATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) JIM MARTIN SW-916 STRUCTURES " -e -- - - -- -- - -- - GPO 901413 SDNYGlvl02759891 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002468 I 3 EFTA01331276 SDNY_GM_02759892 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246814 EFTA01331277 ARc•ii. lac] U.S. DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION 7/22/97 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio, Helicopter, etc.) NAME OF APPLICANT BOEING 727-31 AIRPLANE ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1478-005v REPAIR - FLOOR BEAM STA. 600 RBL 25 FIGURE 8 HOLE REV. IR 7-22-97 • REPORT NO. 1478-005 (.--- STRUCTURAL SUBSTANTIATION - REPAIR - FLOOR BEAM STA. 600 RBL 25 REV. IR 7-22-97 FIGURE 8 HOLE THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 CTION INSPE PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REOUIREMENTS (Ust swift sections) CAR 4b.200 .301 .305 .201 .302 .308 .202 - .303 .307(c) .300 .304 CERTIFICATION - Under authority vested by direction of the Admiresbator and in accordance wilh cations and limeations of appointment under Pad 183 of the Federal Aviation Regulations, data fisted above and on attached sheets numbered are ex" al have been ermined h accordance %Nth estabEshed procedures and found to complyWM applicable requirements of the Federal Aviation Regulations. MN Recommend approval of these data I 9,0() Therefore I l Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) f.1 7e JIM MARTIN SW-918 STRUCTURES arm 81103 (11-70 SUPERSEDES PREVIOUS EDITION) GPO 901413 SDNYGIvl_02759893 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246815 EFTA01331278 SDNY_GM_02759894 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002468 I 6 EFTA01331279 lifiC•il• Ito I U.S. DEPARTMENT OF TRANSPORTATION DATE • FEDERAL AVIATION ADMINISTRATION 7/22/97 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Ratio Helicopter. etc.) NAME OF APPLICANT BOEING 727-31 AIRPLANE ASSOCIATED AIR CENTER UST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476.006 4-- REPAIR - AFT B/B DOOR INTERIOR STRUCTURE CRACKED REV. IR 7-22-97 REPORT NO. 1476-006 4, SRUCTURAL SUBSTANTIATION - REPAIR - AFT B/B DOOR INTERIOR REV. IR 7-22-97 STRUCTURE CRACKED THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 INSPECTION PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List spectfto sections) CAR 4b.200 .301 .305 .201 .302 .306 .202 .303 .307(c) .300 .304 CERTIFICATION - Under authorfty vested by direction of the Administrator and In accordance web conditions and ImIted:res of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered 60/ ree d have been examined In accordance with established procedures and found to comply %Oh applicable requirements able Federal Aviation Regulations. No Recommend approval of these data I 00 Therefore a) Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) g 7.—te JIM MARTIN SW-916 STRUCTURES orm 81103 (1 • EDITION) GPO 901-613 SDNYGivl_02759895 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246817 EFTA01331280 SDNY_GM_02759896 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002468 I 8 EFTA01331281 fIRC.97, IL. U.S. DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION 7/25/97 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane, Radio. Helicopter. etc.) NAME OF APPLICANT BOEING 727-31 AIRPLANE ASSOCIATED AIR CENTER UST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-007 •-• REPAIR - WING TO BODY FAIRING DAMAGED DOME NUT REV. IR 7-25-97 .---- THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (Ust specific sections) CAR 4b.300 .304 .305 CERTIFICATION - Under authonly vested by drecdon of the Administrator and In accordance HIM anditions and limitations of appoinbnent under Pea 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered o 44 mr- harm been earnined in accordance vats established procedures and found to comply vith applicable requirements of the Federal Aviation Regulations. MI Recommend approval of these data I Opfi; Therefore Ui Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTAT1VE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) f JIM MARTIN SW-916 STRUCTURES -al FAA Farm 8110-3 (11-70 SUPERSEDES PREVIOUS EDMON) GPO 901413 SDNYGlvl_02759897 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246819 EFTA01331282 SDNY_GM_02759898 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246820 EFTA01331283 RAC- J(11. 1CA) . U.S. DEPARTMENT OF TRANSPORTATION DATE FEDERAL AVIATION ADMINISTRATION 7/25/97 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Ain:sane Radio. Helicopter. etc.) NAME OF APPLICANT BOEING 727-31 AIRPLANE ASSOCIATED AIR CENTER UST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-008 (---- REPAIR - OUTER SKIN NOZZLE CENTER ENGINE REV. IR 7-25-97 THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 Mic , ,l ;,..- f^,c-• PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (Ust speak sections) CAR 4b.300 .304 .305 CERTIFICATION - Under authority vested by direction of the Adminislratce and In accordanoe with conditions and lirnitathns of appohtment under Part 183 of the Federal Aviation Regulations, dab fisted above and on stincned sheets numbered De t‘ d have been examined in accordance with established procedures and found to comply all applicable requirements of the Federal Aviation Regulations. imi Reconmend approval of these date I We) Therefore 12g) Amon, dust data SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) JIM MARTIN SW-916 STRUCTURES FAA Fonn 8110-3 (11.70 SUPERSEDES PREVIOUS EDITION) GPO 901-613 SDNYGtvl02759899 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246821 EFTA01331284 SDNY_GM_02759900 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246822 EFTA01331285 JWG 97.084 U.S. DEPARTMENT OF TRANSPORTATION DATE . FEDERAL AVIATION ADMINISTRATION JULY 28, 1997 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. I TYPE (Airplane. Nolan. Helicopter. etc.; NAME OF APPLICANT Boeing 727-100 Airplane Associated Air Center UST OF DATA IDENTIFICATION TITLE Drawing No. 97-2211-210 ,---e" Autopilot Interface Unit Modification W/D. Rev -- Date: 7/28/97 ----------------------- Note: (1) The above data is approved for the electrical/ electronic and avionics design aspects only. PURPOSE OF DATA To Support Major Alteration on S/N 20115 Only. APPLICABLE REQUIRLAIhNTS (Dot specific sections) FAR 25.869(a), 25.1301, 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 X X X X X X X XX have been examined in accordance with established procedures and (mind to comply with applicable requirement, 01 the Federal Aviation Regulation,. Recommend approval of these data I (MIS) Therefore Approve these data tEl sionATune(S) OF DESIGNATED ENGINEERING REPRESENTATIVES) DESIGNATION NUMSER(S) CLASSIFICATIONS) 9' 4 -rA John W. Goswick r—L"—C SW -880 Systems & Equipment SDNY_Givl_02759901 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246523 EFTA01331286 SDNY_GM_02759902 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246824 EFTA01331287 7-23-S7 3:19 PM ;SUPER 27 PROGRAM 6196912232;e 2/ 5 -• • U.8. DEPARTMENT OF TRANSPORTATION DATE PEDERAL AVIATION ADMINISTRATION July 23, 1997 STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Altplam, AMA liellcopor. et) NAME OP APPLICANT Boeing 727-31 Airplane Rohr, InC. LIST OF DATA IDENTIFICATION TITLE Rohr Inc., EROS C0825 l/ Engineering Repair Data Sheet Revision A dated July 23, 1997 • INSPEU n TI CIN PURPOSE OF DATA To submit substantiating data for a repair. This constitutes approval of the repair design only. APPLICABLE REQUIREMENTS gmrspeotosectody (1)(3) FAR 25.301 (2)(3) FAR 25.805 (a) (1)(3) FAR 25.303 (2)(3) FAR 25.609 (1)(3) FAR 25.305 (a)(b) CERTIFICATION — Under authority vested by direction of the Administrator and In accordance vAth conditions and limitations of appointment under part 153 of the Federal Aviation Regulations, data listed aDove 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. Recommend approval of these data I (We) Therefore Approve those data SIGNATURES) OF DESIGNATED ENGINEERING REPRESENTATIVES DESIGNATION NUMBER(S) GLASSIFICATION(S) (1) Jeffrey D. Shutrump ifite NM-2731 structures (2) Tony Bredlaugh-Dredge NM-738 Powerplant (3) Michael August NM-2182 Special Administrative to O•Mfatee br RotV, a a, SDNY_GM_02759903 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246825 EFTA01331288 SDNY_GM_02759904 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246826 EFTA01331289 .4 44,0•44404.440144.4 INIPAMOR C4,14416•04./10 ,4—MPOW. .4.4440.114.114:44 STANDARD PiRWORTHINEES CERTIFICATE 44.0414044.44001.014.4. 4 G41,40044 05001.3 DODD 727-31 20115 ?DISPORT 4.4 ROa • ,...9•Nocagor.• tll rI•reaut) 07-23-90 LEE R. TR 7 0107 mn ra DM .....04 ./I 4M/P 44, Cm, to. 4144.4.0014= 4.14:4414[0.4444424* FAA Ferro D00.2 ow, o.., ••••••• SONY_GM_0275990.5 TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA _00246827 EFTA01331290 i SDNY_GM_02759906 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 00246828 EFTA01331291 • Form Approved ge • OMB No. 2120-0020 MAJOR REPAIR AND ALTERATION CS Onrcsttrco For FAA Use Only a sovccomon (Airframe, Powerplant, Propeller, or Appliance) • . Office(dentification hews sewn= ,4 ?7 CA 0 e UCTIONS: Print or type all entries. See FAR 43.9. FAR 43 Appendix B. and AC 43.9-1 (or subsequ nt revision thereof) torinstructions are and disposition of this form.This report is required by law (49 U.S.C. 1421). Failure toreport can result in a civil penalty not to exceed51.000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Modes BOEING 727-100RE 1. Aircraft Serial No. Nationality and Registration Mark 20115 NSOOLS Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner NORTHWEST DELAWARE CORPORATION Mig ign i,DE. 1;899; 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 r PROPOSER Type APPLIANCE Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. X U.S. Certificated Mechanic THE LIMITED INC. Foreign Certificated Mechanic /A301541619 4387 INTERNATIONAL GATEWAY cenificated hermit Station COLUMBUS, OHIO 43219 Manufacturer 0. I certify that the repairand/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 rAdigion Regulations and that the information furnished herein is true and correct to theaat.ot my. nowledge. . 9:1) 1.11.‘ Date .- Signature • 'z IA al . L>, I ( s . . March 11, 1998 ! Richard R Cady II 7. Approval for Return To Service Pursuant to the authority given persons specified below, the unit identified in item inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is • GI APPROVED 0 E TED FAA Fit. Standards X • er (Specify) Manufacturer Inspection Authorization Inspector 40 FAA Designee Repair Station Person Approved by Transport Cana -worthiness Grou Date of Approval or Rejection Certificate or Si natu of onzed I vld..al Designation No. • . March 13, 1998 IA2185934 T.W. RITCHIE FAA Form 337 riz-sei SDNYGivi02759907 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246829 EFTA01331292 NOTICE Weight andbalance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration compatible with all previous alterations to assure continued must conformity with the applicable airworthiness requirement& 8. Description of Work Accomplished (If more space is required, &trash addltionatsheals. Identify with aircraft nationality and registration mark and date work completed.) • REMOVED THE FOLLOWING EQUIPMENT: 2EA. HONEYWELL DIGITAL AIR DATA COMPUTERSP/N 7000700-962. INSTALLED THE FOLLOWING EQUIPTMENT: 2 EA. HONEYWELL DIGITAL AIR DATA COMPUTERS P/N 7000700-662 WITH STATIC SOURCE ERROR CORRECTION CURVE INSTALLED IN ACCORDANCE WITH AES DRAWING .LIST NO. 97-727-500 REV. B, DATED NOVEMBER 3, 1997 PER SUPPLEMENTAL TYPE• CERTIFICATE ST09364sc. FAA APPROVED FLIGHT MANUAL SUPPLEMENT, DATED OCTOBER 27, 1997 IS REQUIRED AND INSTALLED ON THIS AIRCRAFT. WEIGHT S BALANCE NEGLIBLE. COPY OF STC ST09364SC AND MASTER DRAWING LIST ATTACHED. CONTINUED MAINTENANCE PRACTICES INCLUDED IN THIS PACKAGE. END Additional Sheets Are Attached •U.SGsemeet0665Cnalsa035 SDNY_GM_02759908 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246830 EFTA01331293 THE LIMITED -• UR0859 RECEIVED - U.S.IDepartment Form AP of Ttansportation OM8 Int .05;1996 Federal Aviation MAJOR REPAIR AND ALTERATION -AA Use Only For Admlnistradon (Aidrame, Powerplant,Propeller, or °"grIA.001)2k141iiki.S Appliance) INSTRUCTIONS: Print or type all entries. See FAR SWO5 /Ctr..-C- 43.9, FAR 43 Appendix B, and AC 43.9.1 lor subsequ for !omwallens and disposition of this form. ent revision thereol) This report Is required by law (49 U.S.C. 14211. Faiture i penalty to repen con result Ina dvil not to exceed 01,000 for each toch violatIon (Station 901 Federal Aviation Act of 1958). Make _. .4. Model Boeisg 1. Aircraft 727-81 Seniel No. NS/3~4y end Registration Mark 20115 N50015 Name (As shown on registration conilicate) Address OM shown on registration certilicatot 2. owner Northwest Datawire Corp 1105 N. Market St Nilmington, DE 19899 3. For FAA Lise Only 4. Unit Identifieadon 5. T pe Unit Makt. Model &dal No. Repelt' Altaration ~FRAME -------- -----(As descnbad In Item 1 above) PRATT & WHITNEY POWERPLANT Turbo Fan Engine JT8C-7B P654373 X PROPELLER rype APPLIANCE Manufacturier 6. Confornity Statement A. Agenty's Name and Address 8. Kind of Agency C. Certiflcate No. U.S. Cartificated Mechanic Greenwich Air Services - Texas, LP Foreign Certineated Mechanic 9311 Reoves Street RA1R445K •. Dallas, Texas 75235 X Cenificated Repair Station . Powerplant Class 3 Manufacturer D. I certily that the maak endnor alteration made to Accessory Class 1,2 and 3 the unit( ) identified in Item 4 above and described have been made in accordence with the rei:lui:am on the reverse or attachments hereto ens of Part 43 of the U.S. Federal Aviation furnIshed heroin is true and correct to the best of Regulations and that the Informatica my knowledge. Date Sin I, Authorized Individual /c) - 3 .0-7 24,47 ,1--- 7. APoroval Pursuant to the authorlty given persons specified be w, Return To Service prescribed by the Administrator of the Federal Aviation the unit identified in item 4 was inspected in the menner MA Rh st-evas Administration and is Exil APPROVED orer Iltmayl nREJECTED mouw« aterstessw asmoren Aulhonvelen BV , MA gedane* ~os isoweed °T Truien x filIPM• §.uilen Canada Afrwereeent Onno Dato of Approval or Rejection Certilicate or Signa f Authothed in ividsal Designation No. / O-30 -fri.‘ RA1R445K .---- de' • SDNY_GM_02759909 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024683I EFTA01331294 EFTA01331295 ZE89N:00- Vin LT Pue 'ST 'OT '6 '8 7. SHdV2IDV2:1Vd 8302:10 3ALLD31021d 011J3f8fS 01.66SLZ01^/0ANOS 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 Ofmore space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) • Engine S/N P654373 was removed due to "SERVICE BULLETIN COMPLIANCE." • Engine was disaSsembled, inspected, repaired as required in accordance with Pratt & Whitney JT8D Engine Manual (P/N 481672), and Greenwich Specialized Unit Repair Workscope which are data approved by the Administrator. Inspected/reinstalled Combustion Chamber Outer Case P/N 542155, S/N 243, T.T. & T.C. Unknown, in accordance with P&W Alert S/B 6228, Part I and Part II and AD's 87.11.07 & 95.08-15. Ps4/Drain bosses require reinspection within 6000 cycles and at each Engine shop visit. Rear flange requires reinspection within 12000 cycles and at each Engine shop visit. Case meets inspection requirements of Part III of P&W AS8 6228. Continue timed combustion chambers. Complied with P&W Alert S/B 5729R2 and AD 87-14-01R1; immersion ultrasonic inspect C2 fan blades. Complied with P&W Alert 6038R5 and AD 94-20-01; corrosion inspect high pressure compressor disks. Complied with Pratt & Whitney Alert 5/8 6196R5; #5 bearing seal assembly. Improved oil return & compartment sealing configuration. Complied with P&W Alert S/B 6110 and Alert S/B 6131, AD 94-20.08. This terminates -reinspection requirements for P&W Alert S/B 5913R6, AD 93-06-05. Engine was preserved forshort term storage IAW Pratt & Whitney JT8D Engine Manual (P/N 481672). Engine was subjected to a test run; a post-test borescope inspection was performed and Engine was accepted as serviceable. Engine TT: 32939.0, TC: 22557, TSR 00:00 CSR 0000. Pertinent details of this repair are on file at this Agency under W.O. UR0859 .2 n ADDITIONAL SHEETS ARE ATTACHED FAA AC 72-4906 Form Approved Og, MAJOR REPAIR AND ALTERATION OMB No. 2120-0020 usDemmer* ClbetzgaMen (Airframe, Powerplant, Propeller, or Appliance) For FAA Use Only Iredsoviitelellat Office Identification AdmitMilan SO.FSDO-°9 INSTRUCTIONS: Print or typeall entries. See FAR 43.9, FAR 43Appendix B.endAC43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49U.S.C. 1421).Fadure 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 Boeing 8727-31 1. Aircraft Serial No. Nationality and Registration Mark 20115 N500LS Name (As show,, on registration certificate) Address As shown on registration certificate) Northwest Delaware Corporation 1105 N. Market Street 2. Ovmer Wilmington, DE 19899 3. For FAA Use Only 4. Unll Identification S. Type Unit Make Model Serial No. Repair Alteration AIRFRAME * (As described in Item 1 above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer S. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. ST Mobile Aerospace Engineering, Inc U.S. COMM:Sled Mediank 2100 9th. Street, Brookley Complex Foreign Cenifiatee mechanic MZAR013L Mobile, AL 36615 Limited Airframe X Califkated Repair StallOn Manufacturer D. I certify that therepairand/or alteration made tothe un t(s) identified in item4 aboveanddescribed 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 IndivId November 25, 1995 Clarence Spencer im.......______ 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 SO APPROVED 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 of Approval or Rejection Certificate or Signature of Authorized Individual ---.. Designation No. November 25, 1995 MZAR013L Christopher J. Hil • FAA Form 337'1245) SDNY_GM_02759911 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246833 EFTA01331296 • NOTICE • Weight and balance or operating 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. Description of Work Accomplished (if more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Installed DeVore Aviation Corporation tail flood light installation in engine pylons in accordance with De Vore STC ST09113AC dated 26 May 95. DeVore Top Drawing List #72700003DL Rev "A" dated 5-30-95. Installed Valsan Wmglet Modification in Accordance with Valsan Master Drawing List #VA000007, Rev "N" dated 17 April 1995. STC SA59381%1M. Aircraft Inboard and Outboard Aft Flaps and Ailerons rigged to endure fimctionality and conformity. Aircraft weighed after modification. Weight and balance data provided to customer. Aircraft total time = 31,197 hours. Total cycles = 21,345. END'. O Additional Sheets Are Attached •USGPO:199OO4011-012/400O4 SDNY_GNI_02759912 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246834 EFTA01331297 Fs.", APPrOved O OMB No. 2,20.0020 MAJOR REPAIR AND ALTERATION vlosemen Fot FAA the endy Olicreasso. (Airframe, Powerplanl, Propeller, or Appliance) 15472 ,11:flo i 11141•6111fill•••• iilleil•MISI, INSTRUCTIOIRt Plint CWIY00 tutentriet Sn FAR OA FAR 43 Append.. B. and AC43.9-1(Ortubsequient nnision thereof) tor instroctkons Ona 014.01.06on olMailoin. Tho rop0,11•18.410nln bylaw (401.1.S.C. 14213 Fe luntIO report Canmolt i • cml palony not io oliaila $1.003 kw Mól SKI% allabOa (Section 901 Faleni Aelobon Act ol )9:43 237.r7 - leb lee Yodel T. eaCiA/6- Seed Mt r; o H s••••••• Nosionety end Reoisliotion Mark A/52 , 04. 5 Nas (As *Own on tivairgn cartitIcS) 4 4" Si (As shown on regettrollon catraltalit) /401..D/445. . ., r.O.?ok 1138 aii.sverifinv 31e. /9A3 2. Oa ha tata - S. For MA URI Olik - • . '..' ":. •:;•4\3, .N.3.;4-34 N:O ..tib4 .!`7':•. • ' ,. . 3,4 A ','. ,,\..r,e tr.'34. •.• St .7!, ...r. : t 3. .. . •' • — 4. llellIdiellsellso • '''' ' e. 'TYPO Unit Melee Rend Mention . —.., AdiFRAUE • (As tbactited in ban I 4000VJ '. . • • POWERMANT , r • . 4.. :-.*„"..- -.1 ..... - `2."09,16 ...C!.:., • . r !... , .\".. PROPELS - MMMCI 9brs . epOtt iOret' /IYA, 4406 OW 49 V '1106 173 e ? la ri lryea (ATA 160 X CCOnlornilly 414ffileard A. Agency* Moe and Adding * . t Kind of Arony C. Condlcolo No. . -gr Zatirefaisti us c........ mowne • :V3e2 s/a.. ,...............c 1 ........... ..,..,.,,„. s.. .2,7..)Je 593 5 ari-4393uś ofĄ0 4132 /t D. lennon‚ aha %hemom ondier alletetIon made w the tainl(s)idonlilOP3 In ItOfn 4 •00•• woO °flatbed on OW rOvIna• of anocnnwonungrolo him boon ~Je in occortlance 4/41. the niqUinlonntsb ol Pen 43 of de U.S. Popersi Anaben asouleeone ano Inst IM vuoimation Ismonvd Iwon 4 eve ona correct to UV 0•01 01 toy ..._.... • . De onW Ind, 71779 (i .. - Apr*epilog RetuniNo Softies . PUMAMI. 10 Ule solne/ay gnom poisons sooplied bolos. ther identiliain kun 4 was inloo0441 in the manno/ plesenbod by Ow Assmovonnoo eino Fas Anilan AdnIOWal N. lOn end. APPROVED O REJECTED PAA Ell.Slenderds Oltor (SPOIW MOnolOant" X InKfOCOOn Aillh041/MiON illvaiponbr BY Pelson pea by TunsOon FAA Delligre• Ropier &OCR real. Awto one i auta • O•uperArrernereasposon Grafitowe/ . mew um fled :non. Dronation No. 7 /9/ 9 Cił _1.4-a iss.-crw ... - . .. • ........... .... __ . , I i i. o. ...Je m, ba. ... '••••• anKaisi".••antaflahDealtataelefaagialikraggvi , 1• 01hal SDNY_GM_02759913 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246835 EFTA01331298 FAA AIRCRAFI REGISTRY CMIEIU R0. 3 DATE: je/r/i NOTICE Weight and balance or °fleeting limitation changes shill be entered in the appropriate 'bore t record. An alteration must be compatible with alt preyiOus alberstoons to assure continued conformity with the apPfloalg• allwOrthatods redulremenld 0. Description of WO* Accomdlisned (II more space teound. attach addaronat sheet Identity wen aircraft nalOneary end reaustralson matt snd ale work COmSdritd -rev 9,04,4,bio—ri -kierhse.39--Ar alvise.,4-oet• 72) A- 74, 10660/0.- 964 (Roza.) 3y••:;9—: -. zugatotrestnver • Mmc- yevetz_ c4:2462;m5-.544-1.4)/ atirGefre-D Ai INC fririctIle2> /1/4 44Xtralbvar 23e 4..--‘ A.Z. Grit -0 /-041 t 7VP. . •- .Sys77W a 345) oPerOrieWhia, Cifeezetzn SS. *Sow -34-Seat• 'rev 1 mere) ..1747/984 . 440e.hg- nov.focc.Av hearrAte" la-v2...05 awely 2 7.9,4). ?A .M4' or AD 90-eil-osi dew. 59 -8784.:. "Ok.14,4400,9- 23422.-er 11,46" ihraelle 4.7). 317-/illgaTt. Aveat-Penem -Ver: einoy. .ofi 755s. AD. n 774,- Aay.4.rr- reisor Afthink_ SIAlatoar. egnade 17e- .177-4 - eweb r407- c6rrez. Affiedyrami6 I II:1' APPArtall_ or Agent•Wer mews err" CeilPtionvete • i i... • Oaf ' I t-:.• . tn. Alt Fit.) e j ,• • )' " LI NG.es\ l \,-••, %)"O1\ 1:\ -7" Te1 /4 Se t' • 031'•••• ••• • '<Irv, • •* t.o to...eh/v.101no tetiliC irdpoe ront • moil . ::(ti"aIdot sbora CyilOvl ervoibro rt. • nrns mil 1. I4In tnnItInn41* i• i In St nn,' stilt" I roil Alio minas, , obits. ' sr-S`c‘o: yvi to Roe frL PI 13411:0 . el tin...mi.. i .it • SI \ t Of yd lortlioolovi Winos yeti toniiitgrol µw p NO .v Die;g1tt wit v soss..0 711 .11.7/1 Lt Ont'Oliqua is• a WIC driloiltbeilIDS 1I *VA p.atn - • "- 7. I X ; tooii AM{ tm •• .11Wrt. ri1C;TPi 6131.1• • n;s its..„„,"0 . I...mm. 4 Ain Oberon entoiAiSioo4J .0.7y-oz nit oto;ii..;;;Col Or nom SWAM dakalidnrisQ4 Sri • " ‘• 1n., • SDNY_GM_02759974 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246836 EFTA01331299 FAA AtitteAFT REGISTat CAMERA No. ,3 DATE t y/r/fr TRANSPORT AIRPLANE DIRECTORATE AIRCRAFT CERTIFICATION SERVICE 1.04iANSELES AIRCRAFT CERTIFICATION OFFICE f. • A229 EAST SPRING STREET LONG SEAM CALIFORNIA 40006-242.3 Honeywell Inc. Air Transport Systems Division ATTN: Mr. F. W. (Will) Lynch " 21111 North 19th Avenue Phoenix, Arizona 85021 References: a) Honeywell letter, dated Fe5hary 17, 1994 b) Honeywell letter, dated March 1, 1994 • Approval of an Alternate Means of Compliance • our review of.the data submitted ig response to your letter of March 1. 1994,compliance fh'support of a proposed alternate means of with paragraph C. of AD 4066010-901, -902 94-01-04 regarding Conversion of Honeywell TCAS II part No. completed. and -903 (My Mod) to part No. 4066010-904 (Mos G), has been Service Bulletin We concur that method and procedures outlined in your revised 4066010-34-S W16 Revision 1, dated February 17, 1994 provides an acceptable No. 93- level of safety in accordance with paragraph C. of AD 94-01-04 Docket MA-68-AD; Amendment 39-8786. further question, please contact Mr. Abby Alan Y. Shinseki Manager, Systems and Equipment Branch 1.% SDNV_GM_02759915 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246837 EFTA01331300 FAA AIRCRAFT REGISTRY . CAMERA NO. 3 -. DATE; -90,/f/ir IT01264Ili 331V*2 VxvaI.1;41PU • re..?".noli14. V.O/T477.1CH.1:1 ;:!;:7.:51;f4 :!1.31.144 tfLt DItTr.M.:" • nonotrAlo^lh'i 771S-a01:;;' nri0cm::-rtn:A. .1O".39 A:10.1 • • W.t. r .': II:fit A: . CS2C! •srioshr. .... • v•Hon- r: /0 Ltig';.!* :74.scrtnlifit.bpiooll. 5 to .71tc,!ur ;Cr ‘• ;0:4 a9)1! II WI II:4rcsr.O1:1.6 'notroinoT ottirzgrr .bn,nIcco? notqi fl.d : • uel)':•912-0103":". .cr-hng (1123‘a10_,:c r:- atiurruti nty-H2 betl..401.iuoi nt nnntf;uq zvinnzinicf•iiisiboil/Orn indf :Own ofgetqq”c 1t flasittil( Mir Klcrviv% b1sb :f .r17 1 III.12-'+C-0100itC) •••:?•.on neteutr.o-ttr fil, nt •••.,,, t/.... 10 fi v9! • • ,7;1!I.V.: .1 ".t.C!, bns F SDNY:NA02759916 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246838 EFTA01331301 FAA AIRCRAFT ltGISTZT CAMERA MO. ,3 DATtt "6/9/11 5- sit -; : anitwoRTfitiiEss DIRECTIVE FLIGHTSTANDARDS SERVICE olTransportMon REGULATORY SUPPORT DPASION Federal Adage° P.O. BOX 26460 Admits's:n*6On • OKLAHOMA an. OKLAHOMA 73126003 aisSio• a s•r ar r 0.1./SAMmak•Paosea 0 .0 •••••••... 0•••••••••111.Ow /SS *OS Mkeittet i•••• •••••••v__ we as IlkeSts dolmans".es•Snip•••• sialeaussl ,m•••• • ...i.e. sea bass mow ••••••••••••••••••4 es sq.•••••a0kahm 0••••••• amt... IP. PO pawl WIMP mai bluer milemo••••••0•••••••••••••••• Mary 94-o1434 HONEYWELL: Aniersdnicist 39-8786. Docket 9$411.1.68-AD . (TCASHI computer units: pert Applicability: Traffic Alert and Collision Avoidance Speen to, the goliowtragittrpiiia numbers 4066010.901. -OM. and -003i as installed on, but not limited testthested m an category: • and A34O Maim Airbus Induatrie Model A3OO-6OO. A31O-2OO. A31O-3OO. A32O4.OO. Mrptusees -500: 747-100. -200. Boeing Model '727.100 and -200: 737-100. -200. 400. -400. and 400. -400 and 747SP 757.200: and 767-200 and -300 aeries enplanes: Ell and VU Cessna Citation Model 0550 end 0560 eerie, airplanes. and Omens Citation series airplanes: Canadair Challenger Model a-800.2516 and -2.0112 saics airplanes: British Aerospace Model 125-8OOA: OM/stream Model GIL 0 LLB. CIO. and GEV Genes airplanes: -:• • 2r47, Lockheed Model 4101 l series airplanes: -15.30. and -40;.,,:4 McDonnell Douglas Model DC-9-1O. -20. -30-. -40 and -50: DC./ 0-10. series airplane& and Model MD-88 airplanes: . . MD-11: and DC-9-8O . i I • Dassault Aviation Model Mystere•Paloon 50 and 900 arias airplanes: • Short Brothers Model 603-60 series airplanes: de Havilland Model DHC-8-1OO and DEIC-7 series airplanes; iiti f Fokker Model F27 series airplanes: and airplanes. Corporate Jets ]lotted Model BAe 125.8OOA and Brio 125-1OOOA series —••••• • • Compliance: Required as indicated. unless accomplished previously. the TCAS U To prevent collision, or near misses caused by isionnpatibility between prooraeors and the current au name control system- accomplish the plowing: latilnuad • . (s) Before December 31. 1994. accomplish the requirements of paragraph, WI6. -dated 3. al(2) of this AD in accordance with Henri/ell Service Bulletin 4O66O1O-34-S December 20. 1993. • numbers Iii Remove ranting Honeywell TCAS U computer units. part updated 4066010-901. -902. and .903. and replace those units with new units that incorporate CoMskin avoidance system ICAS) logic, kleuttiled es Version 6.O4A in Mitre letter FO46-1.4O69 .id • • dated September 21. 1993. units, • 1 L21 Modify the computersuricIllance {ogle on Honeywell TCAS II computer Mode C • put numbers 4066010.901. -902. and -903, to ensure that these units accommodate coordinated by altitude input o( 1OO-foot increments and that the system will be tracked and Intruding aircraft when the Mode S transponder CA field Is act at CA•7. • (bl- WPrtor to Anther' flight 'after accompUshin,i the requinneents- otperageapir (eat this?. °Obit s l hing'dthee -.W.—nrylle di/ ittinrie . night - Maittlitl"ant) 'ol'AFM- Suppleoient. paragraph (bX II or (On) of this AD: (1) Revue the Normal Procedures Section of the AIM to include the tiFiroPelete AD. In TCAS operating ellaniCtertst1C relative to the modifications required by paragraph (al of this Certification OOIce acconianee with a method approved by the Manager. Los Angeles Aircraft (iCO). FAA. Transport Airplane Directorate. Or following! 12) Revise the Normal Procedure Section of the AFM. to include the (a) of this AD. TCAS operating ellaineterbtle relative to the modification rundrod by paragraph This nay be seem:mit/had by Inierting a-copy of this AD in the AFM or AIM Vi e: • 1' • . F 5. dew. SDNY GM_O2759917 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246839 EFTA01331302 • .• . .• • . .4'ist g;1 r3 41 to tA !a nizailaaas;y: l',,4 1,3 • fx • . : It • T...., sstallea arc (TM aural ase .' Ad vis ory (R AI and Traffic Advisory above ground Iced (Mal 'All Resolution 00 feet altitude of less than 1.1ling Inhibited at AGL deweea ce time that s tha n 90 0 fed of the complian daubing. and lea tho d of co mp lian ce or adjustment Manager. Los Angeles Aircraft ve me the er1 An alternati el of safety may be used If approved by . °pennon shall submit their provides an acceptab le lev pe rt Alr pLaae Directorate add commenta and OL FAA. Tra ns pector. who may Certifleatiota Office IAC propriate FAA Principal Avionics Ins ap requests through an es ACO. ernative methods of n sen d it to the Manager. Los Angel the cd retos ce of approved alt the on coneenang les ACO. NOTE: Informati d from the Los Ange and 21.199 to wi th thi s AD . If an y. may be obtaine ac co rda nc e with PAR 21.107 compliance ma y be bo we d in be ea ror ep liaD •A ht perm its s AD ta n (dl Special flig s:an= what the requatments of thi in ac cordance with Plo neywell ne te ak be dem o operate the airpla ement and mo dif ica tio n sh all rpa ral loa by MkSIZEkte (el The replac 1993. This Laco )3. • ted December 20. .C. 5521a) and I CM 68010.34-5W16, da zdano: with 5 US Servic e Su nta n 40 tor of the Fe de ral Re gis ter is ac co erc ial Fli gh t Systems Group. Mr, — was approved by the Direc m lio ne ywell Inc. Comm s may be inspected at y be obtat he d he cona 8503 8. Co pie Part 51. Copies ma ision. P.O. Box 21111. Phoenix. An n. Wa sh ing ton : at an FAA. Div ue. SW.. Rento t. • Transport Systems c. 1601 Lind Aven ication 01110t. 3229 ,East Spring Stree Airplane Directiemt NW.. the FAA. Transpen ge les Ma rn a Certif Ca pit ol Str ee t. Directorate. Lee An gister. 800 North Transport Aftplarie of the Federal Re Be ach . Ca lifo rni a: or at the Ofnce Loos 1994. ton. DC. ive on February 4. suitc 700. Washing ent becomes effect (0 Th is am en dm MATION CONTACT: FOR FURTHER INFOR FAA. Transport nt Branch. Mitsi-l= ce rin glo o•e . Sy stems and Equipme Ocoee. 3229 East Spring Stmt. pa Abby Melina. Aeros craft Certification 10. . Los Angeles Air 51; fax (310/988-52 Airplane Directorate 90808.2425: telephone (31019M-53 Long Be ac h Ca lifo rni a s Date Aircraft Fligftt Ai rcr aft/APO • Tall No. Prod. No. Hours . MX. . . Gill CJCe %O. GI GI I • 'off MI . - NOT APPLICAWIBLTHE - COMPLIED .,, - . - DEFERRED UNTIL E ON LIED WITH. THE ABOVE ITEM IS DU THE ITEM IS COMP FO RM MO SE1O IT IN WHEN PLEASE COMPLETE THIS N . sammum • t /1•1.fttr:ill pat t Tr.e` - • •-•I • •i, • • Ha' WI . :Anil ' al bt , ;:4kini., • .44 • • - 14. 4 1 1 S4 7;* ••• - • ER PARA GRAPHS 7, —876/0.4-ffg§a r --- S UBJECT T O PROTECTIVE ORD 8, 9, 10, 15, and 17 o EFTA 00244Z:1n EFTA01331303 •IAA AERCEAET RECISTRT CAMERA NO. DATE 8 a- - Fenn eaneveg 0 OMB No. 2120.0CE0 Oanoweni MAJOR REPAIR AND ALTERATION . Per FAA Lem Only ohmomowv (AMrame, Powell:4ml, Propeller, or Appliance) Nowntrateiten m........ - °tilt...V:14'9110-15 INSTRUCTIONS:Print or late eat entries. See FAR43.9. FAR 43 Appendix EL end AC43.9-1 for suissequent revision thereof) for instruction and disposition of the form. This moon is moulted by law (49U.S.C. 1421). Failursto reportcan resort in aciriNnalty no110exceed $1.000 for each such violation (Section 901 Federal Aviation Act of 1958). , Make Model N. BOEING 727-31 :I 1. Altar Soma No. Nationality end Rsoesustion MW 20115 NSOOLS Marne (As mown on tegISNIAIOn artflkika) Address (As shown an migration cortzikats) 2. Owiwor NORTHWEST HOLDING CORP. 1105 N. MARKET STREET WILMINGTON, DE 19899 3. Far FAA Use ofty 4. Unit identification 5. Type Unit WM Modal Serif No. Repair Alterman AMRUNE (AS described in hem I share) . X PCNIERPLANT • • PROPELLER . Type APPLIANCE • Mansdalurer IL Ceniareity Itatemme A Agency's Herne and Acklins O. lid A Agency C. Cirtificade No. U.S.Cesiikated easchame PAGE AVJET CORPORATION Foreign Ceslareo sfecherde ' 9809 TRADEPORT DRIVE OSORA25M X Consume Am.' Slay. ORLANDO, FLORIDA 32827 Menuleconer D. I certify that the few and/or alteration made to the un't(s) 'dent,' ied in item 4 above and des< ' me reverse or attachments hereto have been infra in accordance with the requirements of Pan 43 of Ow U.S Federal Ana egeta end information furnished herein is use end correct to ihe heel of my memos.. Date Signature of Authorized Indi --..„, • • 20 79)err /9944 e.i....iragmbge- va.,,,) 7 Approval ler Ran To Sereloe • Kaye 1 to the authority Oren persons specinsa below. the It identified in kern 4 was. Inepeeled in the monster proectibed by Bp Apronistnnor or he Fothemi Ayisnion Administration end le I APPROVED 0 REJECTED - FAA Ft Standards Cam Inspector MSnufsctunor Inspection MAhorizetion (wry) BY FAA Desiree 51.1105 Person Approved.by Transport X Repair rross yCarod Group ... DM* of royal o Retention Cenamtte or Strew. Author:LS Ossigneho- No. geedrictms as ) 0 g / /C- g 0S4R4251( C „ •-•• SDNY_GM_02759919 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024684 I EFTA01331304 FAA AIRCRAFT REGISTRY CAA NO. 2/1 DATE: !U-/h2- yr.[ I NOTICE Satirisation must be Weight and balance or opera NV limitation changes shall be entered in the apPlaCdiste Wiesen secede:. reptanaments. compatible with all previous ShOhniCteNrro assure continued conformity with the applicable airworthiness & Deoctiption of Mot Amontplehed date work completed.) mote space is requited attach Additional sheets. hawses with circlet naliOnelay ens1 registration mw* end 127-31 S 20115 peas (ELT) SYSTEM IN 1. INSTALLED A DOANE 6 MARGOLIN EMERGENCY LOCATION TRANSMITTER PAGE AVJET REPORT. PR 41-22 REV. A, DATED 8/15/94 AND ISDI.- ACCORDANCE WITH BY DER MARION SHIN, 91-02 REV. 8, DATED 8/10/94 AHD APPROVED PER 8110-3 SCE-339, DATED AUGUST 16, 1994. SUMMARY: 1. PROVIDED WEIGHT E. BALANCE UPDATE. 2. EQUIPMENT LIST UPDATED ACCORDINGLY. OTHER SYSTEMS. 3. ALL SYSTEMS OPS CHECKED AND DO NOT INTERFERE WITH OF WORK ACCOMPLISHED ARE ON PILE AT THIS REPAIR STATION' 4. ALL PERTINET DETAILS 0S4R425M UNDER WORK ORDER 60298, DATED SEIMMNBER 2, 1994. • - - END-- a Addlibrolli MOMSIWAIIIChed 0.0041•61-044•01..:03: SONY GM 02759920 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246842 EFTA01331305 -FAA AIRCRAFT IEGISTRT CAMERA NO. DATE: - . FormAproosi 4:, 0 mwmmon MAJOR REPAIR AND ALTERATION O1W No. 2120-0020 Few FAA Use Oaly wanes- w .• (Airframe, Powerptant, Propeller, or Appliance) • '---Si Mc letePIDO -15 Miniywow. MSTRUCnONSMmt or type allmeMc Sn FAR Alt FAR 43Anendia&and AC4394 Or submmuent mean thateW kw Malmmtims and dimmsitim 0 Mis Wm.T his mpon is maMted bylaw(49 US.C.1421), dims to mph um remitIn a WM pmelty mate encmW WAX kw sun such violation Mecum 901 Envoi Aviation Act 04 1WW. Maim WWI • - Boeing 727-31 1. Minna Nationality and RegisUstion Mork Serial No. 20115 NSOOLS ' Nwrie Ms shown on mgoVehon Vindicate) Andress (As aeon OM 9 SO W a rtOn ceninhan'n , • , 1105 N. -Market Street 2. Chimer NORTHWEST HOLDING CORP. , Wilmington, DE 19899 1 For FAA Use 4. Unit iderellowdm S. Type ...-, Um Man Model Sabi Nlo. Week Alleinikin AIRFRAME (As described ,n hem 1 anon) x P0WERPLANT MOPELUM Tam APPLIANCE Mensdettwor S. Onsformity StMetnerd A. ArnallNeer and Sam B. Kind of Agency C. Ovulate NO. ti.S.Ceniecattecl tAichank Page Avjet Corporation Foreln Certinuted klechanie 9809 Tradeport Drive n Swa 08,18425M , Orlando, Florida 32827 X Merhttectutet Ceterednape. im , D. I certify that the repair and/or etwation made to the UMW identilied in item4above and den ham been mode in accordance with the tectioliennliti oiPanOot the US. Feder& AN furnished het0n Is true end collect to the best 0 my noolnew. Date Signature 0 AvenorM0 MOM 2, StPrEivIaa 1993 /4 eaellegre-LAAUT SICAIel) Swaim L Awmowl kw Rolum To Pursuant o R. wAnollY Onin persona kinifin Wow, the unit WentilM0 in AM'4 was Inspect In the manner prescribed by the ACIMM4tistor el 1M Federal Aviation Administration AM is CI APPROVED 0 REJECTED aver Minivy) FAA n Standards Mmolonum Mg*CtionAulterOWNm BY lor Mrprct . FAA Desire* I X Rep* Station Cmwda Werair= Date 01Appeoval Or Rejection toniticoto Or .. SPriat el AO In .1 i .esoc÷gL om fr e ... Designation No. . rit1 41 01 ! 2 SEPT:93 /4 CoS4R425M A a-- SDNY_GM_02759921 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246843 EFTA01331306 -FAA AIRCRAFT REGISTRY CAMERA N0.3,:/ DATE: /0.-Ig.-/I4 a. NOTICE Weight and balanceat Oporatind lineation changasShall be enteredin the &uproot's"(t advertise-owl An aneiation must compatible with all previous alunanons to assure continue be d conformity with the +Placable airworrhonas mammon's. • bescrIption el Work Accomplished Or more space le toptinad. Minh OddrtiOnal shNn. identify with • waren nationality and rogweration maw and are work compiled.) 727-1k SIN 2011 psoor.s. 1. REPAIRED CORROSION ON THE LOWER FORWARD CORNER OF THE AFT CARGO DOOR BEAR STRAP IN ACCORDANCE WITH PAGE AVJET E.O. NO. 53-30- 02838 DATED 8/11/9a AND APPROVED PER 8110-3 BY DER MARION SHIN, SO-339,' DATED AUGUST 22, 1994. 2. REPAIRED DOUBLE DRILLED HOLES IN B.S. 940 MOD KIT BRACKET IN ACCORDANCE WITH PAGE AVJET E.O. NO. 53-10-02839 DATED 8/10/94 AND APPROVED PER'8110-3 BY ORR MARIO N SHIN, 50-339 DATED AUGUST 22, 1994. SUMMARY • 1. ALL PERTINENT DETAILS OF WORK ACCOMPLISHED ARE ON FILE AT THIS REPAIR STATION 054R425M reIDER WORK ORDER 60298, DATED SA Pr.cit. END 0 Additional Shafts Are Allhched cadwadieleModiavOU --- MbNyaoffcg9i2 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246844 EFTA01331307 -FAA AtSCRAFT REGISTAr tahERA No.,W DATE: jogg-,44 fr • Form ApprOved 01•13 No 21204020 0 MAJOR REPAIR AND ALTERATION scaraienes For FAA Use Only a bresenceot (Airf faille. Powerplant, Propellor, or Appliance) OffiASIOn DO— 15 leasemensis• •••••••••140 INSTRUCTIONS.Pnnt Or fee ail envies. Sae FAR N.Y.FAR 43 Appendix ELandAC43.9d (or subsequent tension thipreog frif irsiruclIons anthespositionol Mb tarn. The report is rewired by law legU.S.C. t421). Failure bravest can result in a civil penalty not to emceedEt .000 for Nen such vielellan Mattoon 901 Fedorel Armen Act al 19581. • was Nodal Boeing 727-31 Ertel NO. 20115 NatIonelity end Alma?. Nan* (AI Mown on registration aveldicata) MIdnissIt i ftrrIgginrInteE 2. Owner 'NOR1MWEST HOLDING CORP. Wilmington, DE 19899 .• t Far FAA Us• Owls • .. .: A Unit Ideallikellee 5- Ins Unit Make Model Wet NO. Etna Mango' ... IJAPPAME (As denuded in flare I abere) - X POWEIIPLAPIT • PROPELLER • V Type 0 ANUANCE . • Manuesturer • • d 11..Cegforolef Illeleibeed A. Agency's Name and Ades . 8. KIM Of Arty C. Cartillosla No. • A Page Avjet Corporation , U.S. Caretcara keersaschank Cerliscased sic . F 9809 Tradeport Drive OS4R425H X CarriatantoPupit t andart Orlando, Florida 32827 lianulacktor 0. Id0r1Ity that 1.00 mink and/rmIllt010000m04010 the yogis) klentilied initem 42Snenddescribed on the revere. or Miedunents hereto. have teen nets in &cordon:* with the requirenteints of Pan 43 of the U E. 44410•1Aylati Ind that m ion ' futnished hadan A Ind and correct to the Wee aity luta...WSW .e - DOI ; egnelura of Authoring' Inevid ei 2. 6EP7E/raile. 1 4; 9 3‘ 4,3,6€21"7.4.0>2 4.,/ "it L Award for Ran To Bake Natu011110 IN 1011001117 rat persons specified below. Vie unit Mobbed in item 4 was I Win 100 manned prescribed by Ma Administrator of the Federal Aviation Administration and 'e ' . Xl APPROVED O REJECTED FAA Ft Standards Othe (Specify) Manulecturet . leveler. Autharialien Inipscior SY Person by Transport FAA Desiree. X Ramie SeliOn Canada Group ol Auth, Dee of Approval or Refection Cordlivile or Designation No. Signal 4" gew7i-itn"4 • [2. SEPT 90 OS4R425M FAA Ions 337 Ma, SDNY_GM_02759923 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246845 EFTA01331308 •PAA A&'CRAFT REG/SERI CAMERA .:n,?Ai NOTICE Weight andMattel or operating limitation changes shall be enteredin the appropriate aircraft record. An alteration "lust be corneal:We with elf previous alterations to assure continued conlormily with the applicable airworthiness requirements. a. Owalption of Work AccoorpWhof I mote *KO Pi required. Sank addolsOnal SAM. Identity wan akentt nalkallety and iaglaustion mark and data work compered.) 727-31 S/N 20115 N5001 1. RELOCATED ACCESS PANEL FROM B.S. 1183 TO B.S. 1350 LH AND RH BETWEEN STRINGERS S4 TO S7 IN ORDER TO FACILITATE ACCESS FOR FREQUENT INSPECTION TO TERMINAL FITTING IN ACCORDANCE WITH PAGE AVJET E.O. NO. 53-30-02837 DATED 7/428/94 AND APPROVED PER 8110-3 BY DER MARION SHIN, SO-339 DATED AUGUST 22, 1994. SUMMARY 1. ALL PERTINENT DETAILS OF WORK ACCOMPLISHED ARE ON FILE AT THIS REPAIR STATION OS4R425M UNDER WORK ORDER 60298, DATED .2.S.6Pri744 •♦ O Additional Shoots Are Matted eflOPW.9010-61WWilaWDS • • SONY GM 02759924 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246846 EFTA01331309 FAA AIRCRAFT REGISTRY CAMERA DATE: /- 93 Fore Amend OMS No. 2120-0020 0 MAJOR REPAIR AND ALTERATION For FAA Use Only us innmi Otis demn alemo (Airframe, Powerplant, Propeller, or Appliance) Office Identification nersammaaa miammatin 51-ISB0-15 4.19-I (Or subsequent meittiOn ImallO) lor insmmtions INSTRUCTIONS: Print ortype all•MnesiSee FARM.% FAR 43Appandk B. and AC moon can result i a CivilPenalty not to exceed S! WC Falleml0 end dig osit on ol MONer This mport ra requited by law (41I U.S.C. I421). tor sect such violation (Section 901 Federal Aviation Act Ol 19540. Make Model Boeing 727-31 d ,ASR Sera' No. Netionauty and Registration Math 20115 N5001.5 Name (As shown on cogiartarknarPfloa) Addrena (AI Shown on respitnnion ['Waken') 1105 N. Market Strut A Owner Wilmington, DE 19899 NORTHWEST HOLDING CORP. a. For FAA Use &Ay I. tha IderAlkatlen Meal Serial No. Repair Alteration : Unit Make AIRFRAME • • fitadretliddlamie ',teen R '-«, POWERPIANT , PROPELLER Type APPLIANCE -Manulecturer liy.eneerealty 9~ & Kind ot Agency C. CerlAket• No. A. Agency's Plante and Address us. cee~ hum« Page Avjet Corporation Fame/ Ceninesma Immune OSeR425M 9809 Tradeport Drive Orlando, FL 32827 g Ceramic., name Saloon limulson • in dem 4 above and insonom on the reverie of attachment* hereto D. I Certify inn thermal/ and/or iilttttt ion msd• to the un tO) identified Federal Aviation Regulations and AN the hrikanation hove been made in eteoidente with the requirement* 04 Pest 43 of the U.S. !tarnished herein is IAN end correct to the bath el my nowledge. Date Signature eked Individual /Pbenflt.my V. etc.,,' /S 3 Y iei‘0 04-; • gl i % 7. Ice serww • , Pursuant tc. the authority given persons awaked below, the unit Identified in hem 4 was InsO/cled In the manner prescribed by the 10 APPROVED 0 RE ECTED ' AdmIMstrator of the Federal Aviation Administration and a own (Spurr/ , FAA Flt Standards Mainulachow InsORCHOn niAreillizenOn klepeClor Dy Peon AppriAM by TranSpen Date.'7 Mk glengen r.25-/f3 royal w emection x Repel( SUNK CortIlkete or DesIgnellon No. 0S4R425/1 _ nnes Cars «Mm ini Gram Signal sol Authorised oat IC*" di gmea, A -A./Potvi . '3 / r FAA Fom 337 Fiat, RDNY_Ohl_O2759925 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246847 EFTA01331310 FAA AIRCRAFT REGISTRY CAMERA NO. IN DATE: 1,9* WeightandbalanceOr Operating NOTICE limitation Changes shall be compatible, with all previous enteredin the appropriate aircra alteration: (0 assure continuery ft record. An alteration must conformity with the applicable be airworthinest requirements. .5Z 0 U. DeseMpt ono R. Acconosbed (If more space is required. attach echlaionar sneers. Wad y with aircraft nationaufrand regatranon mark and dare wore • comp...4dd B727-31 'SIN 20115 - .N5OOLS 1. INSTALLED HONEYWELL SCAM II SYSTEM IN ACCORDANCE WITH STC SA309450. PAGE AVJET CORPORATION • SUMMIT: AIRCRAFT WEIGHT AND BALA NCE UPDATED ACCORDINGLY. 2. EQUIPMENT LIST UPDATED ACCORDINGLY. 3. ALL SYSTEMS INSTALLED OPER ATIONALLY CHECKED AND DO NOT OTHER SYSTEMS. INTERFERE WITH ANY 4. ALL ENGINEERING AND WORK ACCOMPLISHED AT PAGE AVJET STATION UNDER WORK ORDERS CORPORATION REPAIR 7492, 8112 AND 9301. 5. AIRCRAFT TEST FLOWN BY FAA FLIGHT TEST ACO ATLA NORMAL. ALL WORK ACCO NTA. ALL SYSTEMS CHECKED MPLISHED IN ACCORDANCE WITH APPLICABLE DATA. • • M • '!4!.)21.!:, ' AdeNioneu shateswintaine *US PRINTING orncc, inl-ali-.012 10117' MONYMA4_0 926 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246848 EFTA01331311 FAA AIRCRAFT acCISTAT CAMARA ND. 2,r4DATZA 1/ - 4 - 9a • .- 74% , • • Form Approved MAJOR REPAIR AND ALTERATION OMB NO. 2120-0020 vs waine's .. o bovecnoinn (Airframe, Powerplanl, Propeller, or Appliance)`' ' For FAA Um Only ...•• 4.4,4•4 • . Office mantill as lc ...../........ • HP INS trivet IONS: NMI or type all entries. See FAA 43.9. FAR 43Appentli, Band AC 43.9-I (Or subsenuentralsIo n thereof) Mr instrucdons and cintioseion oldds Iona This Minn Is required by law (49 U S.C. /42n. Failure to report an coattail a civil penally loi tact' such violation (Section 901 Federal.A.Sation AO ol not toeaceed 31.000 ISM. mote . Model Boeing 727-31 I. Newel _- Serial No. - Nationality and Registration Mark 20115 N5OOLS Name (At gammon isolAitallOnnellikalo) r. Address (As shown on rooISItallon OnlificolO) I 2. OsnWI Northwest Holding Corporation P.O. Box 7138 Wilmington. DE 19803 - 3. For FAA Use Only 4. Unit identification L Type Unit Mae Model Soria No. Rep, Alletstion AIRFRAME (A 0 0 0 I 442, / X POWEILPI.ANI roproun l ype • APPLIANCE • emdochnel __.., ,.. 4 CORIOS RA IllalaiM•II ' A AyusiErs. Mane Mid &Muni. El Kind of AElencY C. Cadilitlite No. u s Caner-nee mown Page Avjut Corporation tent. cmainared meehanic 9009 TY a tItfiius' I. I)i. i VI3 3 entm‘neennmustam • 0S4R425M Orlando, Florida 223327 . - hilmw4clumw I) I curio, mai 4i..c.4-)Mei aalign ..IIV.400.5 MOO PO Rig• imill(4)6026Itilmed In item 4 moon and doomedon Int ieverse or allachmentahmoo k ri...e wen ...Jo a...no... e anis he rectuliammla or Pon 430 Me U S Fmmerd Aviation Regulations and that U.. 4404414H011 is....t.Ai swop'. ib buy aid 4.4.0:l to die WM ol my knuelcd(le • .- ineiv . Sly, owe Le A. i hs...duel 4 met,.KWrigiti- „5_11LAICr ) •i+ 1 2 17? • 7 al km Rouen To Service ewe., to Inc 4,4,....., Ione pqa...4.4 sprcilkad Wen'. the RINI adetiliblia Adinnisti.oei or the I ouni.a An Iwo AdmInialrallon and Es . ft .AFINSOI/ED in Awn 4 *es anpacred in ma manner az. gultricribed by the 0 Mt EC I 30 I AA I II $4440444I. °V14, ISPOC.4) lowalul M.Rlielatluott InilputIANI Aull'OMMICIO LP? I- AA llestonw X !grime Station NOM, AIIPIIned Or IlltinPart Canada Ait *tinniness Grove Vole LA A. Iluvalut Ihneconsit CcitthCalt Of Skilialuly Of AillA00110 Individual Na.o.:O hi aer--nant-..-1 Demenation No. ..:11 NfilLeSt lillip- '0548425H f / 51.0.0 it Lfrnni-sr SDNY_GM_02759927 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246849 EFTA01331312 FAA A/ RCRAPI REGISTIE CAKEIA NO. 3PATZ4 //-4-4a • NOTICE Weight and balance or operating limitatio n Menges shall be entered in the appropii compatible with all previous alteratio ale aircraft record. An alteiatron must ns to assure continued conformity with be the applicable airworthiness reutorem ents. g n arl) et Watt Acceenollshed &pee et neutral attach edehloOnia Sheets. Identity with *heist: naloOnahly and reeilltelopn milli and dale were teingthle d B723-31 ' 5/N 20115 45001,5 1. MODIFIED SECOND BATTERY SYSTEM PER PAGE AVJET CORPORATION STC SA309250, MASTER DRAWING LIST PIDL-91.-37, REV. A. 2. MODIFIED ED 805 EFIS PER PAGE, AVJET CORPORATION STC SA3085S0, MASTER DRAWING LIST MDL-91-44, REV: A. • 3. MODIFIED FMS-800 FLIGHT MANAGEMENT SYSTEM PER PAGE AVJET CORPORATION STC SA3089SO, MASTER DRAWING LIST MDL-91-43, REV. A (NZ-9112 SOFTWARE). SUMMARY: 1. PROVIDED WEIGHT AND BALANCE UPDATE. 2. EQUIPMENT LIST UPDATED ACCORDINGL Y. 3. ALL SYSTEMS OPS CHECKED AND DO NOT INTERFERE WITH OTHER SYSTEMS. 4. ALL PERTINENT DETAILS.Opk. WORK ACCOMPLISHED ARE ON FILE AT PAGE AVJET CORPORATION UNDER. WORK ORDER 9286, DATED AUGUST 31, 1992. END 0 Additional StoatsAte Attached O • SDNY GM_02759928 -- SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246850 EFTA01331313 PAK-AIRCRAFT REGISTRY CAMERA no. Zi t DATES q- 9a, • Form Approved 0 " MAJOR REPAIR AND ALTERATION . OMS No. 2120-0O20 uSOwaserate For FAA tfoe Only atoracarron (Airframe, Powerplant, Propeller, or Appliance) 011ice Idenolicauon _ Newt smarim AdwatIvann 30-fS00-15 INSTRUCTIONS:Printer rye el entries. See FAR 419.FARA3Apkodis ill. and AC43.9.1 (or subsequent revision Memo() lot insloudions end Oisposnion Of thi4 (atm.This report 4requited by law (49 US.C.14211. Failure IC NOON can topsoil❑in spoilpenalty not lo escood 61.000 for each such viola6on (Section 901 Federal Aviation Act o119541, Mee Model Boeing 727-31 I. Aircraaal Serial No Notionalily and Registration NW 20115 N5OOLS Name (Al shawl on rogisitanencerrificon. A4Onass (As shown on enistestion califaft) • 2. 0•044 ' Northwest Bolding Corporation , •P.O. Box 7138• - -. - • - • • Wilmington, DE 19803 ... - • . Fee PAA Mee Ord/ ' . . . 4. UnR Identilicalion S. Try. Model swim Met' mention • -, • AIRFRAME (Asa bad I I fl own X . . • ROPtrotAsir - Menem& . Type APPLIANCE WNW B. Conlonally Slalemeni A A or 4 NOM and &Mem B Kind of Agency C. Conflict,' No. U S Catainataa mautente Page Avjet Corporation rw«gn Catoicatto hlecninc 9809 Tradeport Drive X Cott/caw Roam stalwn O54R425M Orlando Florida 32827 leNectiov D. I Gently Owl Ube tepair andfot alteration made to IN un li at idenithed in ileni A altrotli And deMeibed On UN(erne Or •INCliments Nnolo hate been mod* In eccenwice with iho taqvleornenla of P 11 43 tat Ina U.S Fecletat Aviation RintulaboM and that IN sat ininiOn • Banished baton is his and cot tool to the INN of my nuatledge Dole SIgnelwe e , •-.-:- 2- r JOH., 1- at all Nir 7. Ann, Retro To Souk* Pu want to Inn authatity Oven persons IIPICIPod below. In ml Al•ntilta0 in nem 4 was inspected In the manner YeelKbbei by let Adauflealat of the Fedei al Ac onion Administration and a ib (1, APPROVED 0 RE ECTED FAA Fit Standards ISpOeligi ilitspuder anulacturer Inapoc000 YonlObiaben BY /AA Charm Pet son stormed by rtansoon I Repair Shallots Cam& AlretifINness GIOIA Dale al Apµ Oval et RegicUon CotIbiCed• 04 SI lure of Aulhonzed I Designation No. - Zt JAN ),$2 03411425N Ad ak..4.- _MOM H I-frill-tat • AA Fenn la/ •• me . •' SDNY_GM_02759929 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024685 I EFTA01331314 NOTICE Weight end balance or Operettaglimitation changes shall be enteredin Ms appropriate aircraIf record. An anerationmoilM compatible with ell previous alterations ro enure continued conformity with (he applicable airworthiness requimments. a. Oneripoon of won iktemopoolloo qt mom space is required. attar, eddilionsl sheets. kleatty with arced, nationally and regiataion m✓t and dew wort comolearil E727-31. LAN 2n1li 1. INSTALLED SUNDSTRAND MARK VII WINDSHEAR DETECTION/GROUND PROXIMITY WARNING SYSTEM (GPWS) IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA311350. SUMMARY: 1. AIRCRAFT WEIGHED AND NEW WEIGHT AND BALANCE COMPUTED. 2. EQUIPMENT FURNISHING LIST UPDATED ACCORDINGLY. 3. ALL SYSTEMS INSTALLED. OPERATIONALLY CHECKED AND DO NOT INTERFERE WITH ANY OTHER SYSTEMS. 4. ALL WORX ACCOMPLISHED AT PAGE AVJET CORPORATION REPAIR STATION AND IS ON FILE UNDER WORK ORDERS 4784 AND 8112. 5. AIRCRAFT TEST FLOWN BY CUSTOMER AND ALL SYSTEMS CHECKED NORMAL. AIRCRAFT TEST FLOWN BY FAA FLIGHT TEST ACO ATLANTA. ALL SYSTEMS CHECKED NORMAL. ALL WORK ACCOMPLISHED IN ACCORDANCE WITH APPLICABLE DATA. 0 Addition& Shims No AMC'S OleneefltieeleIVIII SDNY GM 02759930 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246852 EFTA01331315 FAA AIRCRAFT REGISTRT CANCRA NO. iv DAM _ 9 07_ I Form FIPProved , OMB 51).21204Xr20 0 MAJOR REPAIR AND ALTERATION F LNG usosonses ce) (Airframe, Powerplant, Propeller. Or Applian Onkel" rhilicsiion or FAA Only wkwasavown 90:1100 -15 mi.... tedani Mamas . INSTRUCTIONS:PARof type ellantries.Se1FAR 411 low FARbAppercla 0. and AC 419-1(or Subsequent 1421). owision thereoll Tor instructions Failure to foetid can result In *civil penalty not to **coed 51.000 Isnquhe d by (49U.S.C . and disposition of this icon This report violation (Section 901 Cedes* AMNIA Act 01 10!1). toe *fah such Model Make 1 Boeing 727-3 1 likaell Nationally and Regialialscw Mock • . WM No. ., N5OOLS 20115, geplOration citrialcoN) Aadtaaa (As *P0PP on !ulna (As shown on flu mica C•StitiCarin ,P.O. Box 7138•..i.. ! - 2. /Nome Northwest Holding Corporation Wilmington, DH 19803 . 3. Pei FAA Use Only R 1114/ I. Unit klenttlIcelless SOAPING, 'Repair Alteration Model I Unit Mad , (As OM tad ' Mae I above) X AIRFRAME • i POWERPLANt . PROPELLER TYPO *FALANGE • Mobilactueer t Conlertint Ilabtrosel fl. Kind 01 Agency C. CeRilltate No. A Agency's Myna end heltinnif u I. CA...lawny waving I wow Ovulated Mycboroc Page Avjet Corporation C....fain Raw pas.. . OS41142514 x 9809 Tradeport Drive uswisckaa• Orlando Flor da 32827 Imola and dantat006 onIna Mafia 0. anaChinenis made to the unit's)idantilie0 innano abOra D. I candy Malilia mow and/0, alientlion Ragullatiani and Mat IN InkirinatiOn nts ol Pail 43 ol the U.S Fadagoi Aviation have Wen made in atcuidanCts with the tagoLf•Ma nowledge. larniatiod herein is Ina awl CO4 MCI 10 thll best °tiny Date • Sawatute ol *obeli/ad Individual arnt.5 r. 191l1- Jr. 1 9Z - 22 . 4_AK!,lAtif ..._9 . _": tor Rattan Te Sento, pintaibil4 by the was Inspeclad In the manner Mow. UM unit identilied in hem 4 Po manic ma stithtway We Naar* specilied B APPROVED CI REJECTED MIOn and is Mnbn.Ili &ICH Ones Fade, I bvibliab AOMAIMI ONMISANOW FAA AR 51403.101 Manufacturer Inspection Aushorlowon Instwv-Wr BY bibtOn Apppod by lialnyal FAA Designee X Sept, SWOP.. Canada Airwoilhinem Gioup OMe ol noon:nal*. Reloction Cs/Inhale ea Crosignaton No. Sig - .. 41-1,11-,,,,e.4 Ds.) F./ Nee of Authoring Individual 1471/0/4 ,p.11.3rh-) (19a OS4R425H I'M% Yuan 337 .o mm e: SDNY_GM_02759931 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246853 EFTA01331316 FAA AIRCRAFT REGISTRY CAMERA NO. /,y DATE t _ q_. 9a NOTICE WHO: and balance or operating limitation changes shall be aniseedin the appropriate aircral record An alteration must be compatible with ellprevious alteratiOns to mute continued conformity with the applicable airworthinen regiulatinentS. OneApliantitottAecompialed Of more space Is required. nown additional sheeti tclontily with WiciaknotiOnstity and regulation mark and We work completed.) A727-3I 4/A ,n115 1: INSTALLED- EXECUTIVE INTERIOR IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA313750. 2. INSTALLED HONEYWELL EDZ-805 ELECTRONIC FLIGHT INSTRUMENT SYSTEM (EPIS) IN ACCORDANCE WITH PAGE AVJET CORPORATIO N STC SA308550. 3. INSTALLED MODE "S" TRANSPONDER IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA309550. 4. INSTALLED JAMCO SMOKE DETECTORS IN ACCORDANCE WITH PAGE-AVJET CORPORATION STC SA313250. 5. INSTALLED DUAL HONEYWELL AA-300 RADIO ALTIMETER SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3087S0. 6. INSTALLED HONEYWELL PRIMUS 870 RADAR SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3086S0. INSTALLED HONEYWELL PMZ-800 PLIGHT MANAGEMENT SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA308950. 8. INSTALLED DUAL COLLINS PROLINE II COMMUNICATION AND NAVIGATION SYSTEM IN ACCORDANCE WITH.PAGE AVJET CORPORATION STC SA3090S0. 9. INSTALLED HONEYWELL TCAS II SYSTEM PROVISIONS IN ACCORDANCE PAGE AVJET CORPORATION STC SA309450. 10. RELOCATED FIRE "T" HANDLES IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA311150. 11. INSTALLED FAIRCHILD II PARAMETER FLIGHT DATA RECORDER IN ACCORDANCE WITIOPAGE AVJET CORPORATION STC SA309180. 12. INSTALLED DUAL 40 AMP HR NICKEL CADMIUM BATTERY SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC 5A309250. 13: INSTALLED DUAL. HONEYWELL ADZ-800 DIGITAL AIR DATA SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA308850. 14. INSTALLED AES AUTOPILOT INTERFACE UNIT IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA309350. AddeVerurl SMell Am Anached SDNY GM 02759932- - SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246854 EFTA01331317 FAA AIBLEAZT ■oGIEUT cans so. i# 6_1_ 9a, rya. • ..a•••••• 'WIN* - PAGE 3 OF 3 - 15. INSTALLED HYDRAULIC ACOUSTICAL FILTER IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA313650. INSTALLED RSSENTIAL POWER SELECTION SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC 5A25985t, SUMMARY•: AIRCRAFT WEIGHED AND NEW WEIGHT AND BALANCE COMPUTED. EQUIPMENT FURNISHING LIST UPDATED ACCORDINGLY:, ALL SYSTEMS INSTALLED. OPERATIONALLY CHECKED AND DO NOT INTERFERE WITH ANY OTHER SYSTEMS. ALL WORK ACCOMPLISHED AT PAGE AVJET CORPORATION REPAIR STATION AND IS ON FILE UNDER WORK ORDERS 4784 AND 8112. AIRCRAFT.TEST FLOWN BY CUSTOMER AND ALL SYSTEMS CHECKED NORMAL. AIRCRAFT TEST FLOWN BY FAA FLIGHT TEST ACO ATLANTA. ALL SYSTEMS CHECKED NORMAL. ALL WORK ACCOMPLISHED IN ACCORDANCE WITH APPLICABLE DATA. • END- • _- - - _ SDNY GM_02759933 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246855 EFTA01331318 SDNY GM_02759934 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246856 EFTA01331319 • FAA AIRCRAFT REGISTRY CAMERA NO3 M DATE: 9 . Tam AppeOve• lot pt100p1 APPLICATION FOR INSTRUCTION1 —•••••••• typo 00 tool voila in 0.603vem untpaine• .thete we lorFAA koncesisa . AIRWORTHINESS -" ISO*. dobed Ongietanmay an Repeektv4on• 11500bon0 IDKIIII•lqVire0.440snalladienimi 50FIDIC•ir ==•• coo /.....9 CERTIFICATE ll among iall •55053•50.1. ipmperrnA5C0,00115.ccw.th• LAIONITAA • . - II ANZLA• . rf•VILOI.010•MBE/005; a main VOW. 000005/Cad 47* NM t 8 St)Sc --ti.obEiNG. 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On HAI C5.070.CAI 04 04.4.5•005" R WA bat; rdnI*5 x kno00;m0dSS OwiLtUrt ..,......a...A3W e StOwatedairt..A0.(0•050.•••••••••;(00 ....--- --1,91)Yo -6)- -I 1555“1051C.Alln.u..,.... et00•SIC pit ta. X,X7 4'131 34. 1amv 3NM il igzi 07-3, /99•0 arowren i C. NOCIt4/T 0 5•001105•••••••04051.44tt MOMS X Y Sam 03. IVO, IN VIAL /aimed 0 0%00 v 53001.4.8145 MVO's. Non .299/4. / "'" 5'44.7 AV,. 'slew Ilwai.crsa.0.0.00+1 0. C0IIInCATIOlv - I...0; tvwv or I a 0. •••••00•••• Ateseaserson nact4.00.••••• 5.0...• IC •••. ese......m.• ad ••• sown atw•••• 004 (.0./.....••••••••0•A MA •••••••••••••Isid at". mI me 0.a 0 ••••••••0; •••• *fa in• 5/000 5.0••• 00 0960 ••• •••• 5...05.5kinsiett_00 544 int ..00005 •rt0/05500 '-'•'•••"••‘• ;a40 . CIAll Of APPLICAVON nia.".:77Z-nhe 45. " 0 ;MI ••• ....Pe" tresei < T1ucu50 1 3 i 99° ec. A. He Alidaail 0.30•000•••vg 0.43. 519CCII0 MAD amicalmtlIr itsmalar in- . . i 1 TARTAR,IZI, Idi in CIIII•CM Ki.04.4.5 4.0...IPAPIll Atha ; CwWew COlli•CATICIROWICK.,* a- C•••••••••• LOMICATIDPU0.01/51000•••CanAta• len NICSJ t WNW ACIWCPii a).• nor eI tems ' d • ..c. .. .. - . ti• I Mil lenn•Al4 esvreanets. a dna 5 nee • ••••••••d••••••••no41010 knee I la VII det IntC000ILAII ALOLII5150 sm. re.0.550••• 1. • sthamose•rf 04M001•0110. • 0 .0100 050 .0)4 0 •54,1055•05005 If 0. 405060•••0 ly ••t•••• 0 155• 03•00SSealerell ' 75.5 0•305CnIR 0 ••••••••0fi 05040;55 s COIINIC•55 1•CaCi• Walt .; I I Mn OGIACI 000 W M I Irma..me Iasi f Pm li b .. MAdtf••00•560440.015 r" 71.7bfri6 ir r ' kb e , . CAA mm 11106 ill el; -00145.EttS Pn&Y.OUSC Uothe - - F5- I\IM Oti SDNY_GM_02759935 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246857 EFTA01331320 FAA AIRCRAFT REGISTRY CAMERA NO) A' DATE: 9 - 27 - 97 • •73:CM:MO-2U -471.10.1) • .......ACTLPRO. - HAW Ai • MS* I Migais 0 rir mooLICTIONCARTSCAltIG ral•001010.4410.4~/ MIECEIttlf1OO1O611.y . ANTOVIDPII0OIXT011.1111C10.SYSTEM C.G.KOWITITTOP CIATIII0•113410,POWD101101ISTINOPWS serontuat 0•VrtO/AMICATICNI NMII MO MU I40•00•0.0.01 A.0.5041P,ON OF AIRCPArt 11.1t0IMAIDO•040 • .1.006 SWICCACM.0.1 PlGtiTtAlttiMIN• • UMW MtIMISCR ji./ Tow otmoranvaco WOWS O Kb +moose, • 000.1•1010M10411 To -. 2 11TURECIAtt 1 110/ r'-inaT O. n . . ' 2 C env Kowa° /0 OK4O.1 g 7.4.*scion Mailittfluthftpol . Inns I I COA.OT I IT* 00 I I Oint.rtate.y. bit A/YMCAS"•••••000.naSS nCO2041•0114ASIOL LOWS 2 0 TN A.Cian Ott POT WO .. . . to . . . 5 G 1 1 i I 'caw. 24 ...o. ........... ........,. & : ma.•0.Lcm..G r.t.”.c1,0-....., cc,.....c..••..cciesan. 1 .0 5 t ccranc,„0“_,.........1........s....„..1..0.,: e.a .; 11 . 4... . . ...1.......:6 .t..?":..9 ..... L1.4.- ,..4".. .1!” .. I.e-11.". ” ....t r I.' r i 1,94 ; • nint." ..'S.a.,''''"erear."....."•Xidar...ar"...." ...PT .0•04.4 • . . LT: •. ".....I. ~11G1fl IM' . I. WI NAME MO MU WSW 4, Val ^ • , . O...loirI*a GIMI.Sp.rAA fem030•614019040.20400~0.- 0 C.4..../.*mak • C4.4 " 0,-,-"Pnr,.,......^n ' sl ti el 3168004.<re I f s., O. .g. ., 0, . Os::: •-o n ::::::: :7 • . . ar- it aty-m-a -a.. . .. . °"1"4- ..""4".. al?It 4.. -I A.- 1".b. 0.....ia natal • r La row-emboss 4-11 A Cons0 Wpm 6,4 11.Y.-0 iftwouate .„ a 00.... la... ••••• ." 1/4 1.aine• .0 g V 41••••••••••..../AlemeoMM 1...1), Gareth ~wean Mani linos . f rut -21 • I _ Kew woke 1 1-Mb lf.K1SI4esibe• „P- spir-f .ctiS§a43 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246858 EFTA01331321 FAA AIRCRAFT REGISTRY CAMERA NO3 N DATE: 9 27 :91 IMMOMalt Op 614.e.• eitPARTMOIT OF TRAMIPCSITATION-MOW. AVIATION ADIAOUSTRATION “. • STANDARD AIRWORTHINESS CERTIFICATE. . I Prlawn , NC I ONOISAC7100I1 WOK 3 &SCA.? MIt Wa41. N505C BOEING 727-31 20115 TRANSPORT ▪ NJTMORITIPMO &WS roo. MUNK, • lidelaalnes aiit• pothmalIOW fed**, ..1104•13 of II] IIint [Mg. pap net um*. Omura we w ow. le • 110 Moog M l••• •••••014 rel !oar icresor rem bype •••••N•It Peeler Not a 'a wn. vo OS I. ••• TS or..e. M..* ........P 00 " ^ "K"C•••ef e,a• • • ••• • • by Seems eta re Grew .ak.nertrweat ON Mare* @..p Si roma Peon t emplet* ▪ WIWI reb CObriTCrl Yrs MOWsurnames use,. ar.••••. IV • 06•Imii••• Iona 011•••••• nianann et.N ...ay.... at •••••••••••••••••••• • e•C.• a W fl ew PairlInns eristra••• Oman. Dna • Caleit•••••••••2 a Nati oneeareA.seanopow••• as into* seal •••• I ....Wad ! DATE CSIOLYNCE switire•ar 'A Mt 13t1GNATKINNWOVI 7/23/90 WING C. CHIN DAR-61-FS-NN . lOpeAS.0.4. fir ...And Monica. ow a•pardiSI• 1, <Of Crailp40.000 . •atnelela33, Tait r sn THIS rrrrr CATC WS, Ni DYWID • INC Allieltall N ACCOSCONCt %min Met011it 'IMAM • TantlIULMIC•45. FAA Fona $3100.2 •••••••.— SDNY_GM_02759937 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246859 EFTA01331322 FAA AIRCRAFT REGISTRY CAMERA NO3 N DATE: 9 - - 91 SDNY_GM_02759938 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246860 EFTA01331323 a 0•00, P.,1 MAJOR REPAIR Form McKeelel areverves (Airframe, powerpien AND ALTERATION , Sams ban • t, Propeller, OMIINer Z120-0020 lavirsenvien or Appliance ) foe FAA the On ly INSTRUCTIO NS. Print am* Mee lele p nDlic5 .73 end eseemiienMinis NI ectuns.See FA lamMisrepor t 's/poemA 43.9, FAR 43 APPONI,x. E. and AC C>A I R ..- 0— 0 / for each turn vro :toy Irm I4R U.S.C. 142 43 I (Or Weerant irnsiO tegOnlannon 901 Fedora Adob es ACt of Ise 11. F ;ere to Tr:R- newneolIlot instructio -1 W as ). Demean nounin • en elp ero lty nauseated n, 31.000 I. Alston B0E1AD Mott* ' Udall No. . 727-10D.• 20115 i Natiameny on ton(As Mem 00 teg o Registration talwa . 2. elite. atstrettoncedlik an). N5OSC Adds* IA: ab ort ors regrstr NORTHWEST HOLDING - 1409 Faulk Road adon cenidco nd CORPORATION Foulkstone Plaza, P.O. Box 7138 • Wilmington. Dela , SuitI8a2 3. kirsauarosi ware 1 . t . A IAA monia Unit lcoruso .. . MO* , A0001 Iv TM - AIRFRAME Weft. Prep* • Attention /AS Ss< tea ISM I DOH) POWCRPLAtir 1 , X PROPELLER TTIM •— •----• - --•,— 4,,t(ANCE Manureclurer A. Agency, An & Caraw oint) Adore ay sear !. -. North American e. WOO Of Asiore Rockwell Intern Aircraft - U.S. Ceneemrameetene 2825 E. Avenue Pational Corporation C. Ceti tate Fere", Cameos) Alecen , No. Airframe Class Palmdale. Cat 93 Limited Powerp 4 e 550 X CA necerelReset Serer 0. lawny mettn _M muerawer Class 3 lant e repaltenWo hen Veen Merle in em eor ralterinne ma de 10 Oa unite) klenageoln ' ctin ce Ra h Vie leillaftri• of P dem tenend cil NXAR688K alt 4341Ine U.S. oa (visioned Minn Federal Avineiat ed On On ws* or alteCn le true and cor ri ReeuraeMmise rect to ma ba Oslo r of my nomMe mento rm lee. Mel I mionnatieno n Signature of Au Mortal inelnv i \ July 20, 1990 Olial D. A. Perazzo Pursuant to the ountored given 7, anwewe I Rerun. ACITISSItIllOr Demme umoca To Senna. ol the F•0001 Av tect Wow. our urn iation Aanin imm eo n an d is 0 APPROVEDnennied in Re m 4 as aker* FAA Fn. SIMINV 011 Me 0 REJECTM in lecleenner prime /as' by TO . Y VOSPOCIOf l nulactiver Findocuon Au ED ... . Other tattecOn .....:,..,„,„,A.,...on menzahon FAA Qesign" k Ian" . July 20, 1990 Swan }Cornmeal* a 01H19141/C41 No ... NXAR688K . I iC nrn anadlaA nitsntiVe of bYT ssEG( AUNDIUM) har ve cwi Meteorite, . r I ' i1 ' ) • U. A. Perazzo' ' ./ i, .• -- SDW-GtA 0275993r SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9 ,1 0, 15, and 17 EFTA_002461 EFTA01331324 FAA AIRCRAFT REGISTRY CAMERA NOJ N DAIE: 9 - 27 - 91 • - - SDNY GM 02759940 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10,-15, and 17 EFTA_00246862 EFTA01331325 FAA AIRCRAFT REGISTRY CAMERA NOJ N DATE: 9 - 27 - 97 Is NOTICE • must be •• • • aircraft morel Pri alteration alin the aOProprial able airwortniness requtramantS. ting limitation changes Snell be enter applic Weight and balance or opera Contin ued conformity with the to assure compatible with all previous attentions trati0n mem an; lo completed.) U. oteecnpnon et Went Acton /.dewed, Identity with aircraft nation ality and fit* (II mot e Ana 4 rdance with supple- ' al Number 20115, in acco A. Modified Boeing Model 727-100 , Seri Sept embe r 1, 1989 as follows: 3101, amended mental type certificate SA436 ing Docu ment VA00 0001, Revision F, dated January 1. Valsan-Boeing 727- 200 Re-e ngin 15, 1990. tion to the neering orders (E0's) are in addi 2. The following drawings and engi aboVe document: NOTE: "VA" denotes Valsan Drawing. a. Chapter 24 ELECTRICAL POWER Strut E.O.: 003A, 101 ' . VA240000 A Llectrical System Intl. - fication E.O.: 003A, 004, 005, Pane l-Lo ad Cont rol Cent er Modi VA240007 E & 006 , STRUT '"-- b. Chapter 28 FUEL SYSTEM INSTALLATION Fuel Strut Feed Thru E.O.: 100 VA280001 8 Tube Assy - c. Chapter 48 MISC . 48-727 E.O.: 101, 102 VA48I100 A Pressure Buldhead Reinforcement Sect Sta 1263 E.O. : .101 , 103 VA481200 C Frame Assy 116 VA481300 C Fuselage Skin E.O.: 106, 114A, 114, 1243 W/L244.39 E.0: 106- VA481324 NC Intercostal Assy - BSTA 1223 lo BSTA 1243 W/L234.06 E.0: 105 VA481325 NC. Intercostal Any - BSTA 1223 to BSTA CTURE d. Chapter 53 FUSELAGE STRU 0001 B Ball ast Weight Installation E.0: 100, 102 VAs3 . E.O.: 002,100 VA530003 C Ball ast Weight, Support Structure Assy Ball ast Weig ht Inst l. STA 312 - 360 E.O.: 002, 100 VA530004 NC NS e. Chapter 54 NACELLES & PYLO E.O.: 003 VA543000 C Main Strut Assy (Sh. 1, 2, & 5)36A, 003A Firewall Rib, Side Engi ne E.0: • 1A543100 D f.' Chapter 71 POKER PLANT. . V7Z7RE E.O.: 002, 1058, VA/10000 Mt Power Plant Instl. - Engine Pod 001A , 104A , 005A , 004, 110, 003, 111, 006A 109, 108, ROL g. Chapter 73 ENGINE FUEL AND CONT Diagram E.0: 002(Rev L), VAJ32301 K Approach Idle Solenoid Wiring 002 (Rev. MI, 003(Rev. M) ndid E.O.: 103, 003, 1008 VA732303 0 Relay Instl. - Approach Idle Sole Ligh t Inst l - Appr oach Idle E.O.: 002, VA732304 0 Switch/IND Approach idle E.O.: 103 Nose Gear Posi tion VA732310 A Switch Instl. - l E.O.: 100, 002, 101 head Pane VA732315 NC Relay instl. Pilots Over h. Chapter 76 ENGINE CONTROL E.O.: 002A VA7SUUOU A Engine Controls Instl. - Strut : Cont rols E.O. 100, 101 VA760014 A Drum Instl. - Eng. A Brac ket Assy - Pull ey ESTA 100 E.O.: 105 VA760015 AMMO In Aeldattonal Sheet Act BUSCIOI•6110443 lit -e • GRAPHS 7, 8, 9, 10, 15, and SONY Ga4-027-549;i1 SUBJECT TO PROTECTIVE ORDER PARA 17 EFTA_00246863 EFTA01331326 SDNY_GM_02759942 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246864 EFTA01331327 FAA AIRCRAFT REGISTRY CAMERA NO3 N DATE: 9 - 27 - 97 (2) DESCRIPTION OF WORK ACCOMPLISHED (Continued). Serial No. 20115 1. Chapter 77 ENGINE INDICATING 9A771005 NC Indicator Engine Pressure Ratio EPR, E.O.: 001 j. Chapter 78 ENGINE EXHAUST • • 11A780000 B Engine Strut Controls Instl. E.O.: 002. VA783010 E Fit Deck -Indicator Instl. T/R Sys. E.O.: 003, 004 VA783011• F Thrust Reverser System Wiring Diagram E.O.: 002 (Rev. G) • VA783013 D Support Bracket Assy - T/R Control Valve R/S E.O.: 100 VA783017 J (Rev. E Placards E.O.: 007. 008 VA783024 B Relay Instl. - Thrust Reverser Control E.0.: 003 VA783028 A Mixer. Exhaust - Instl. 727E E.O.: 100 VA783101 C. No. 2 Engine T/R Wiring Deactiviation E.O.: 002 • k: Chapter 91 CUARTS VA910002 • A Instl. - Electrical Wire Harness E.O.: 003, 004, 005,006, 007 • VA910008 NC : Wire List V727RE E.O.: 001, 002. 003 •NEW DRAWINGS ADDED TO MODIFICATION B. Boeing 727 Service Bulletin 727-53A0171, dated December 14, • 1989. Subject: Fuselage - Station 1182 Pressure Bulkhead web, Crack Repair and Preventive Modification • C. The aircraft empty weight and center of gravity was revised in accordance with Boeing Weight and Balance Manual D6-21100. Weight and Blanace Manual attached. Supplement, VA-CR279 is D. VA000003, Rev. A, Dated 4-4-90 is equivalent to VA000001. Rev. F. dated 1-15-90. END SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246865 EFTA01331328 FAA ►IRCRAFT CAMERA M0I M. REGISTRY•, DATE 27 - 91 SDNY_GM_02759944 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246866 EFTA01331329 FAA AIRCRAFT REGISTRY CAMERA NO.? t DATE: 9.- - 27 . 97 . WEIGHING RECORD & CHECK LIST STATKIN 13t - DATE 9-19- 5 -C TER. NO. AIRCRAFT MODEL h 72.7-- kV REG. NO. 1 AC /eta/We - /Of 44/eiteil NC INTERIOR CONFIGURATION IT tra In IN. Amount..... CHECK LEST WILL INITIAL LACK - T. PERSONNEL ACCOMPLISHING THEBEING WEIGHED. . NOT APPLICAB LE TO A/C CLOCKS CONDITION. SHOULD PE IN NORMAL OPERATIONAL 2. ALL BOTTLES (02102.1420) INSPECTOR OR HIS DESIGNE E: LIST MUST SE COOR DINA ES WITH CHIEF WILL CHECK 6 SIGN FORM SE. 3. ANY DEVIATION FROM THIS FOR E mAN/LEA D MECHANIC OR A ssicp E 0 INSPECTOR A THROUG H 0 THE ,-- & DR COMPLETION OF PARTS G. PORE PROCEEDING WITH WEIGHIN Chick. -- T IC ) FLUIDS Checked r BY D • VACIJUM ED • I.!iLLINO. OIL SYMMS • TANKS FULL rt:ILI A B. LAVATORIES CLEANE & SEAT SACK se 4.) ALL MAGAZINES. NEWSPAPERS lIc t. 2. ALL FUEL T KS DRAINED PLUGS WI PHAN USING AIRCRAFT Livia ORAI - sza mer iPi T. - LITERATURE REMOVE D I.L.41' .a IV ifit • PROTECTiNE ENTRY. AISLE a STAIR COVERS , y DRINKING 6 WASH WATER TA,IFILE POISONED DRAINED an FILLED I... I - 'AP O. WINDSCREEN STOWAGE EMPTY • CLEAN K. HYDRAU LIC SYSTEMS FULL • • % ISM. -A1= AFT. LAY. .1,411 .rf , A .sPrisoy 'STOWAGE COMPARTAIENTS0N FssOft Y . OULKNIATM EMPTY I tik ••/V S. TOILETSSERVICED TO NORMAI: QUANTIT Fit '- : ' & DRAIN Wilt • WINO FLOATS SEAPLANE&TELY COMPLE (DI CONTROL CABIN ALL INSTRUMENT PANELS COMPLET E 34 . (:) • • CARGO, LANDING GEAR a . POWERPLANT - ; 1. q,1 • 0/ 1 ENGINE FIRE SOTTLES CHARGED , ALL MANUALS; CHECKLISTS. LOG BOORS, L REMOVED OClie 211# 1. FORMES OTHER WRITTEN MATERIA -1 t eilATf ACtr .:Ii it Call sw oLETE Virm SEAT BELTS • 44., 2 ALL .U.IT ' ENG HISS cOMPUTE ;E. ACCESSORIES. PLUMBING. ETC. • 9 2fig, . 3. ALL COWLING • PANELS IN PLACE • FLIGHT ENGINEERSTAOLE EMPTY CLEAN EXCEPT FOR STRETCHER KIT ' a . 'RAKE AIR 00171-1 CHARGED e sh. C) PASSENGER CABIN EXCEPT ED - is • REMOVE ALL ITEMS FROM HAT RACKS Oxlf. ti O S. ALL AVIONICS GOUIPMINT INSTALL 1. MEGAPHONES. FIRST AID tut MOUNTED IN BOTTLES. DEMO OXY. MASK • UPS VEST EMPTY B. FWD. A APT. CARGO COMPARTMENT " POUCH a CLEANED ....Z.Z.; MAIM OXYGEN SYSTEM SERVICED ALL PASSENGER SERVICE EOUWMENT REMOVE*" II w.S.11 . FULL ...Y.; 2. . FROM GALLEY MAIN 'PATTERN • AUX SATTERY IM USED) ALL SERVICE EQUIPMENT REMOVED glat & INSTALLED • q Pf:1 3. FROM PRO. • APT. LAVATORIES --. - . - 4 r4 yaw DoORS • SAWN= CLOSED • 44. -:. ALL GALLEY AREAS CLEANED a O. LATMEND SP;4' • VACUUMED ..) ,.-- ' • „r i p, , o. g ligi ulit INFLATOO TO OtaiLintiO _-W G. PASSENGER PATEN CLEANED • NACtRIMED THROUGH ® CROWD &COMMIE fredmanitemlMan. O. Paw I. PARTS O LIST COMPLETED 2. STANDARD INTERIOR CONFIG. EQUIP. Forwnw/LosolMat O. hewn. .rAIRCRAFT READY FOR WEIGHING Foteamn/Lse4 Meek Or Moque, r .4 0/4.4 h PAGE I OF 3 MSS SIO OLON SIGN OFF COPY • SDNY_GM 02759945 15, SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, and 17 EFTA_00246867 EFTA01331330 figlifliNigl"R"."4"147.4" . "bcfa*"'" *14 SDNY ;0271994: ""ell SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246868 EFTA01331331 1 FAA AIRCRAFT REGISTRY CAMERA N03 N DATE: 9 - 27 - 91 AincnArt WEIGHING SCALES: MAKE Eva-iced-Ey MODEL 73)c SERIAL NO. 10499 CALIBRATION DATE S . - 3 - 9 .0 •• CALIERATION CELL DRIFT TARE NET WEIGHT REACTION SCALE READING CORRECTION -20 -0- 4/ 7 7/5- . LEFT S•Gtat 4 7735- RIGHT S, G0 98/0 0 - SO - 4 7- O - 4/87so 65?TAIL pia q3 VC +I 0 - ,9^2- or - 4 3 .55- NET WEIGHT TOTAL /041.20 I / CIRCLE REACTION MCI SECOND WEIGH CALIERATION CELL DRIFT TARE NET WEIGHT REACTION SCALE REAOINO .CORRECTION LEFT MIA 4/7750 -SO -te 41 419 .OO WING RIGHT MLG itegi0 #/z) -e -61- its570 WINO NOSE/TAIL ii3&5- 4 1- -es,- ZI g4S ' ...24L / 00/ 6, Cr...0 NET WEIGHT TOTAL WOMOAREACTIONUM I. MIMIC COWLETEO aaN esd NAN. 0, fo 2. WITNESSED • ACCEPTED . 11/b44Wil 4134 • Ovisrow 00•IM•0• 4•et, BY THE DUALITY CONTROL SECTION. NOTE: PART F. AND SUBSEQUENT PARTS TO BE ACCOmPLISHED NET WEIGHT AVERAGE LIFT il .9T„Q-- 4- 40 RIGHT M NOUNAll. FIRST WEIGH 1 / 7 1 /g . 11,750 1-t35-5- SECOND WE 1/7900 lag 20 11145- TOTAL 95-& /5 - 91/ 70 X -72O AVERAGE 97801.5 V1575— q3oto 6sf CHEOCED•Y PAGE 20F 3 • .••••.....• •• SDNY_GM_02759947 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246869 EFTA01331332 SDNY_GM_02759948 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246870 EFTA01331333 FAA AIRCRAFT REGISTRY CAMERA NO3 N DATE: 9 - 27 - 91 • SIC EMPTYWEIGHT COMPUTATION P2 515c GATE --/q- 70 , REACTION NETWEIGHT ARM MOMENT I.,/ CIRCLEREACTIONSUSED. 2. ENTER LEFT /OWING F. NETWEIGHTS 'RIGHT AVERAGED ?gal 45, inkiakr6 S FROM/ART 0 NG I t? Crat- 5- I i7:575 - (15 Z, t 2 lief , /#5, 447 )97, 752 ..-OrAIL I n 3b0 / 75. at 7_ 2. -277, ListO -N itnr - - b 200 IO TOTAL&SE/SIGHED q9,552.s 925:27 ?:;4:;;;;; :,S BEwITEMSNOTONAIRCRAFTATWEIGHING , ".ri?::,,yIs'4! IFISATTACHSUPPLEMENT FIEGIAREDSPACE ADDITIONAL I (3 SUBTOTAL (4 )— 111 4 / ITEMSWEIGHED INDEW OUTNOTTOBEINCLUDED ATTACH SUPPLEMENT IFISREQUIREDSPACE ADDITIONAL O SUETOTAL () BASIC EMPTY WEIGHT • .. ci t?, .532s 1 725,27 9 2,1/ 3, 1/6.5: 5- °ea®. PREPARED IT BY CHISCHEO II PAGE30F3 SDNY GNL02759949 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF-EA_00246871 EFTA01331334 FAA AIRCRAFT REGISTRY CAMERA 10.1 Y DATE: 9 - 27 - 91 SCH•IY_GM_0 9950 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246872 EFTA01331335 FAA AIRCRAFT REGISTRY CAMERA NO3 A' DATE: 9 - 27 - 91 • • ocoto•V_SI ot wrists,* oy • hoo notel THE AO.W.IT tie citation Sy," DE DISPLAYED wsegnan. pootoporots now.*or bon INK CESITICATE aces*. 3 vest REGULATION& posoranl MI • AVIATION APFISAIllt FECOW. Accoitont-E %NTH SDNY_GM_02759951 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246873 EFTA01331336 FAA AIRCRAFT REGISTRY CAMERA t4O.3 a DATE: 9 - 27 - 91J The orwoolunaw Mutes* ea iliPAO View Mt aulhonly 01 the 2108,0 AvissonAci SSW A imash•Rops Awaton PogulatiOnS (MR). . This altwonlunes crlihate Buten:SOO Want/actor netted On On nww$1118NIOCCOdu CI MIN. Ho PrOduCtiOn 11.01 NUL and Only peCitluctien floghl ICON. 01San teptsuwed in CuOduChon IligN WSW Or OMs cortehale 01 Clurting Pet OnCON B Melon May conduct P604cC not toserdal to did papas ol . . (2) Carrying properly /01COrNiOnfahon or hue. anal& t., IN We reverse 0011lot Ind alrwOnhntida abrUltcato atnhOuNts the Mghl upacifOclonthe C Mown in alock b. . rho atowOrItOnnuCen.hcalo oerules [rotas ot the dale 0111avanea. the staaftle ' 1810.1•2 has tworonspacied and lound to meet the requirements WONWheal , FAN Trdaftern8 doe code an not mew ihe to:tokenism, of the aDO1calUe corntuonensive and detailed anawthinwaS Meson May Operate D Otowded by Anon 0 lo the Contention On Wend's:oaf Caul Aviation. No Wien< Snit (I ) excepi in accoedancewin Me KOlicaleFAII and MU bode dolcobcd on Ow rin in arxoslance Yam ctaxmons and linwati0m much may be yr eicntod twtheAdminisuato 111•1 pen 01 Ors commie-Mt 121 over any tOccuan coLoiry without Ina tOecdllutontiSiOn of country. • owtilicawn effective 10f E unless sooner aurrendone. Satpan:100. Or revoked. and airmen/1nm Section 21.1810F 21217. . We duvets:in end undid the condthona prescribed in FAR Pon 21. SDNY_GM 02759952 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246874 EFTA01331337 FAA AIRCRAFT REGISTRY I--OsnERA NO3 & DATE: 9 - 27 91 • '4 US Worn oflonspyroncn FederalMa:Ma AdministrotIon Manufacturing /nspection District Office 7300 Perimeter -Road South Seattle, WA 98108 May 1, 1990 EXPERIMENTAL - SHOW COMPLIANCE WITH FAR's/MARKET SURVEY MAKE:_Boeinq_ MODEL: 727-31 SERIAL NO. 20115. REG. NO. N505C THESE OPERATING LIMITATIONS SHALL BE ACCESSIBLE TO THE PILOT This aircraft must be operated in accordance with the following limitations: 1. No person may operate this aircraft for other than the purpose of Show Compliance with the FAR's and Market Survey to accomplish the tests outlined in the applicant's program letter dated May 1, 1990 describing compliance with FAR 21.193(d). Additionally, this aircraft shall be operated in accordance with applicable air traffic and general operating rules of FAR 91, and all additional limitations herein prescribed under the provisions of FAR 91.42(e). 2. All flights shall be conducted within the geographical areas described as follows: 1. Western United States of America bounded on the East by the Mississippi River, on the- North by the U.S.A./Canadian border, on the South by the U.S.A./Mexico border, and bounded on the West by no more than 200 miles from the West Coast of the United States of America. .2. Base of operations is Palmdale/Lancaster Airport, Palmdale, California and secondary base of operation to be Moses Lake Airport, Moses Lake, Washington. 3. The pilot-in-command of aircraft must, as applicable, hold an appropriate category/class rating, have an aircraft type rating, have a flight instructor's log book endorsement or possess a 'Letter of Authorization" issued by an FAA General Aviation or Air Carrier Operations Inspector. 4. This aircraft shall not be flown unless it is maintained and operated in accordance with Boeing Low Utilization Program, I/A/W FAR 91.169(f)(4). 5. Upon changing between operating purposes of a Multiple Purpose Certificate, the operator shall determine that the aircraft is in a condition appropriate for the purpose intended and has documented that finding in the aircraft log. 6. This aircraft shall contain the placards; markings, etc. required by FAR 91.31. SDNY GM_02759953 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246875 EFTA01331338 FAA AIRCRAFT REGISTRY CAMERA 10.3 N DATE: 9- 27 - 91. • t :z - r .:,th 7;• 7.7 gt 7 2,, ‘7:. ..77.11 r:c• *7 2:I,• • • :.!! •; r; • 7! :Sta.: • • i?;•!:f•V; ▪ Ct • ▪ eieiT J • .. . SDNY_GM_02759954 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246876 EFTA01331339 FAA AIRCRAFT REGISTRY CAMERA NO) N DATE: 9 - 27 - 91 . 1-4. . .1 • Federal Aviation Administration Manufacturing Inspection District Office Experimental - Show Compliance with FARis/Market Survey, Cont'd Page 2 of 2 7. The cognizant PAA office must be notified and their response received in writing prior to flying this aircraft after incorporating a major change as defined by FAR 21.93. 8. This aircraft approved for day/night VFR/IFR only. 9. 'No operations shall be conducted over densely populated areas or in congested airways except for takeoffs and landings, and when under ATC control. 10. No person may be carried in this aircraft during flight unless that person is essential for the purpose of the flight while in the Show Compliance category. • 11. This aircraft is prohibited (Tom aerobatic flight; that is, an intentional maneuver involving an abrupt change in the aircraft's attitude, an abnormal attitude or abnormal acceleration not necessary for normal flight unless approved by the cognizant FAA office. 12. if aircraft, engine or propeller operating limitations are exceeded, an appropriate entry will be made in the historical records. 13. After the aircraft has been re-engined, the pilot-in -command must make a log book entry stating the aircraft complies with FAR 91.42(a) and FAR 91.42(b). hie ael J. Aviation Sa ty Inspector (Mfg) SEA-MIDO, ANM-1085 These limitations will expire on August 1, 1990. I • SONY GM_02759955 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246877 EFTA01331340 FAA AIRCRAFT REGISTRY CAMERA Nod h. DATE: 9 - 27 - 91 -_ - SDNY GM 02759956 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10,-15, and 17 EFTA 00246878 EFTA01331341 . 0 14 0103csacni MAJOR REPAIR AND ALTERATION - - • Form A00towd OMB NO. 2170-0020 a samtotatca (Airframe, Powerplant, Propeller, or Appliance) Fee FAA Uwe Of* Ietsusulistmen woe MOMMOM0a Amambaram . PRY FSOti INSTRUCTIONS: Print Of tyCieall OMAN. See FAR 03.9, FAR 43 Appenlia B. and AC 43.9-1(or end disposition og thbs form. Thy mow is requital by law (49 U.S.C. ICI 1 stable/NW revision dIereffb 124011nAlIOns FailuM10 rePOCI Can romounocfrolPaten). MX la •InOEEIEDE tor ascii such vIONOMI (Seaton 901 Federal Aviation Act of 19581 nEggiUrn FAA wan wool 1. Aircraft • BOEING 12L-100 ' Serial No. tletionalay end Racietterion Mark ' Ail 2 4 ao 20115 N505C Name (As shown on rogistran0n cerohmele) AddrIlia(A4 Mown en fRiarration oaMAXAV - 1409 Foulk Road, P.O. Box 7138 rc°1) 2. Owner NORTHWEST HOLDING CORPORATION ' . Pitieln;t2:1:f:WaSuil;8032 i Far PRA 1.18•Only • • • . . -• • A Unit IdmitlecatIon tribe - • • . Unit Mate ' Modal t . WS RapiIIT Al MINOR AIRFRAME (As dincithol In nom t abort) • X • • POWENRANT, ' I PROPELLER . Type APPLUNCE Manufacturer • 6. CoMormi Starent i A. Agency's Name and Address • B. Kind of Agency C. Certificate No. North Amt..ican Aircraft Rockwel international Corporation US Gentians rnsnic roar Canificac Manic Airframe Class 4- Lilited Powerplant 2825 E. Avenue P X Certiricatea hop. Station Class 3 Palmdale. Ca, 9a5.50 -- Menteig fat _ N1CAR688K 0. I tett;iy that the maw and/or situationnode toMen 1(11Mar/tined in ItemI eatlee end 0600100.00fitN.Monitor tlechments hereto Mn been made in eaconlanos with the refttilfemeMS of Pan 43.0, the U.S. Fliderld AvlationtRectutallo lurMshed herein Is ,we ono Carla 10 the heat of my nowledpe ns and inforKation Oats Signature of AuthorMadRiclividual • July 20, 1990 A. Perazzo O. - k «L. 7. Aerial ter Ram" Te Swiss l ih Putan! m M the authority given persons swirled below. Dm taut enidentified fn 'ism 4 ass i ea ...red In the manner prescribed by Ihe , Administrator 01 the Federal Aviation noannionnice and Is %APPROVED CI REJECTED t FAA Pi. Statiderds I CRON (SOscriyi Impede. Manutectunor IrsoactiOn AelhOreabon BY FAA Designee A x Ronan Stun I •Cr wal ,"" T n' Tj, ""P r, ' Dote or Approve, or Rejection Conontno or Signature of Authorized Individual Oesignahon No. July 20, 1990 NEARERBK U. A. Perazzo k ;4.,„... ,. SbNY_GM_02759957 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246879 EFTA01331342 I 146TICE Weight and balance or operatinplimittilion changes OW be entered ln the sOpropfiale Wreath record. An eller&ion must in compatible with all previous alterations to assure oOntinUei COnfOrtittly with the 'DOUG'S &Matthews. requirements. Modified Boeing Model 727-100 , Serial Number 20115, in accordance with supple- mental type certificate SA4363101, amended September 1, 1989 as follows: 1. Valsan-Boeing 727-200 Re-engining Document YA000001, Revision F, dated January 15. 1990. 2. The following drawings and engineering orders (E0's) are in addition to the above document:: ROTE: 'VA' denotes Yalsan Drawing. a. Chapter 24 ELECTRICAL POWER A24(1000 A Electrical System Instl. - Strut E.O.: 003A, 101 YA240007 E Panel-Load Control Center Modification E.O.: 003A, 004, 005, & 006 100 A Pressure Buldhead Reinforcement Sect. 48-727 E.O.: 101, 102 200 C Frame Assy Sta 1263 E.O.: 101, 103 300 C Fuselage Skin E.O.: 106s 114A, 114, 116 324' NC Intercostal Assy - BSTA 1223 to BSTA 1243 W/L244.39 E.0: 106 325 NC Intercostal Assy - BSTA 1223 to BSTA 1243 II/L234.06 E.0: 105 Chapter 53 FUSELAGE STRUCTURE 001 8 Ballast Weight Installation E.0: 100, 102 003 C Ballast Weight, Support Structure Assy. E.O.: .002,100 004 NC Ballast Weight Instl. STA 312 - 360 E.O.: 002, 100 Chapter 54 NACELLES & PYLONS • 000- C Main Strut Assy (Sh. 1, 2, & 5) E.O.: 003 100 D Firewall Rib, Side Engine E.0: 36A, 003A VA/10000 NC Power Plant Instl. - Engine Pod Y727RE E.O.: 002, 1058, 109, 108, 001A, 104A, 005A, 004, 110, 003, 111, 0064 Cha ter 73 ENGINE FUEL AND CONTROL 301 K Approach Idle Solenoid Wiring Diagram E.0: 002(Rev 002 (Rev. M), 003(Rev. M) 303 D Relay Instl.— Approach Idle Solenoid E.O.: 103, 003, 100B 304 D Switch/IND Light Instl - Approach rdle E.O.: 002, 310 A Switch Instl. - Nose Gear Position Approach Idle E.O.: 103 315 NC Relay Instl. Pilots Overhead Panel E.O.: 100, 002, 101 76 ENGINE CONTROL • 000 A Engine Controls Instl. Strut E.O.: 002A 014 A Drum Instl. - Eng. Controls E.O.: 100, 101 015 A Bracket Assy - Pulley ESTA 100 E.O.: 105 SDNY_GM 02759958 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246880 EFTA01331343 • s*-il, ,t..^% .DESCRIPTION OF WORK rCOMPLISHEO y:- Serial No. 20115 1. Chapter 77 ENGINE INDICATING VA771005 NC Indicator Engine Pressure Ratio EPR, E.D.: 001 J. Chapter 78 ENGINE EXHAUST • VA780000 B Engine Strut controls Instl. E.O.: 002 VA783010 E Flt Deck Indicator Instl. T/R Sys. E.0.• 003, 004 VA783011 Thrust Reverser System Wiring Diagram E:O.: 002 (Rev. G) VA783013 Support Bracket AsSy - T/R Control Valve R/S E.O.: 100 (Rev. E) VA783017 Placards E.O.: 007,, 008 VA783024 Relay Insti. - Thrust Reverser Control E.O.: 003 VA783028 Mixer, Exhaust - Instl. 727E £:0.: 100 VA783101 No. 2 Engine T/R Wiring Deactiviatfon E.O.: 002 k. Chapter 91 CHARTS VA910002 A Intl. - Electrical Wire Harness E.O.: 003, 004, 005, 006, 007 • VA910008 NC Wire List V727RE E.O.: 001, 002, 003 *Hew dr/Linos added to modification. B. Boeing 727 Service Bullekln 127-53A0171, dated December 14, 1989. Subject: Fuselage - Station 1182 Pressure Bulkhead Web, Crack Repair and Preventive Modification C. The aircraft empty weight and center of gravity was revised in accordance with Boeing Weight and Balance Manual U6-21200. Weight and Balance Manual Supplement, VA-CR279 is attached. • x. SDNY_GM_02759959 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFrA_0024688 I EFTA01331344 IIMONShs- SDNY_GM_02759960 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246882 EFTA01331345 IAN AIRCRAFT It CISTRT CAKES FS. DATE: 4.2 - g- 0 • No 2I7J-0018 • APPLICATION FOR ...mucnoges — Porn or typ• DO ROI NAIDAIOD AMA We BOO IAA DOM , WAN •••••140O to WOMMI IAA ADADOUID OJOIMII mmo' 0 loomo AIRWORTHINESS ---- IWO NOMMIOnonatloord o'o.e 'wino-am MOWN DOW . ...... cco ey c iiCERTIFICATE ........ 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SDNY_Gli 62759961 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246883 EFTA01331346 tam$ area PROMICTIOM COITIOCATC /Wm paactb•arborto saran TYnalartreaellOhn . ie moon° /110DLCTION itetetiON MIMI Ora WONT. OP CiliniraTa Mi. ,/Oa 0000•174010200 an Or AnurATION isle Me MS Ma • Pal OONANOS S. Milasinel Of AMOVOI lif.atnerrt0 044.40. AOCASI IMOLA iMer) WOE. Mitt Nowaei ittooymATOI•44/0, 11. C407.71.0010M,Onr, • • CUSTOloaletiorlaTION PU3HTi 13 /do aNotate) TO vt& OVOinulit On . • Mamie.' . i C. CAPV MOuMID TO MONTI THE **CAM ANO in tOJII.IONT, — F - TFLOT O. ilit Mown I 1 COALOT 004.3 NOT MEET THE AMC, . I I imviOATOT. I I OTKO4 'Swain i AIIIISOMPIOAS 141O01.444.41i M POu.Ora . .. . I I i L fit • OLLO•nri0 fittoKrais in ectisacatO Nititn•Prt 105 WI OPOyl v aI *ram« a *smart) ... r 5 . ... g • ... Th Oihnisenii dwienioneeme vaniomplilt moats ...no rodeo Ana.....Amos. 4. V.CangCA/1081- I heensetir Oio I ono monivileans hinC044 Oslo. wt of Wow Mims *Maw Ml ,TO4.04, .ant weer Wei 4.4444.m . • . . 4 'Jan . paw .YD Tate IMII Oun,l; . siONATLOW 0,54.4•4.4. a C....444., FAA f‘r. alai/Arm. .tee now, Own*, LimiTos es/MMTIy. a Orii.d.c.40 PM i e. tni ilsi400.444 I r e I 4Iasi: Armenirors,Cerno wbDolor Novi Afre..A ill I v - - "" * " ° """ 0 I . CDs. prom. Otato••• rd.ikon Mr mai/ I. pow.. hala•••••• CanhaiteliNga. in AttenlagaSIOI 1 bi O. Oarrovori end asps Warm Mos 4.I.I.oun /MPG /9/Ih) ea gm,.....9 " g....,......u.anis, Ii4Aterm/S1(Asp. — e4onVII J.C.en.ma* Gina 'mow VoIlOST•41 . 0 t, r .. IP. Ty inns (woe; manwitarcrs cm _41,191(6)6re) (P) 'Cc. ante/ —" .• • SDNY ak4_02759962 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246884 EFTA01331347 TAA• AIRCRAFT TMOTU CAMERA 140. DIM 2— g wino 'Urn 01 *LUCA nAINSMATONIi IM.PAPIVAte . nuAssommou (OEM AVIATIOPI SPECIAL AIRWORIIIINESS CERTIFICATE SERIALS°. 20115 BUILDER 2OflG MARY 08-01-10 DATE OF ISSUANCE 05411410 Alt A PMT OF THIS CERTIFIC ATE OPERATING LIMTATIONS DATED DESIONATIC*4 OR OFFICE RD. E. sen•Tilt017AIL sointaCar SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15,and 17 EFTA_00246885 EFTA01331348 • AAs AIRCRAFT RECTSTIT CAMERA PD. IN DATE: „.2 - g -Q/ of 1F68 • A Mb airWOrthl(wSr tertitcate laissubribraell}atifibtily ottha FeoralAvt*Ice. AU 010Inefixteral Aviation Regu/14 1:3rts WART. .. . ..... TIN Wpp111t1certifweaumord9Mb nia.h6feclvoti nomtgl On the reroevaThrtla lo Conduct PrOOXIbb le *Mt arb, ally prOcluGtiOn lgot4 l_a 01literal'I ragistared In 115 nacre. No Careyng persons or B WPM SW Conduct production flight lab Older Mb bort:buds (I) of properly km corropeossuon or Nnr. and/or (2) Carrying persOne no OWIMIlto the pulp= IN Ibult TNerwrrommesseerlocalo aulhorizte the flight speciCerd on the moms skle kgmamma. C roan n BOO A. . The snorisnaki avolancerures that POI Modaleof imams.thosiraaftlovatth itstard has been imPecled ond lewnd to rite•4 the legurernenta 01theaDigteoble FAR Thbalreran does coda Ls nal morn thomiqueemere atm spoise.stre cam/nibs:mho and detaDed aliwortbiness may oxrate D l.nrrided by Ann.. (I lo the Convereran On Intern:40ns. CM Analion Noperson ihnircraft Or/sated cn the revorsiouchz 11I areePOn SCCOrdrinc. mlb the 0POicable FAR an, In•O:Oldtanamothcenctthafn and inutatonswhch may be treschtea GY tt,0 Acti nm'Mita. 45 pan of thm certitude: (2! cre an/ Idai9n aaurarY ' ,thou! 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I 14.0JATZ Mai nes OP IIIPPONO CAIRO, ernes IT •• Wacira cm a OPIPATION NT .1ICIUM CT 10•101lui• CIATIFICATTO TNICOIT Wag l<•••••• Ross Cr MY ..Mono el 74701.11/ • oommo oft ducat 1.61 1 mammy. IU041 MTM '4 CUSTOINA 00001•114010. Furoal C It I MULTIPLE MCOOTITHILILIS CITITITC•14 (C•••• *IOW 'Ponce Os•e•b•E ••• 110•••fle lass 4 •••••••• • ' SICOISTITICO *Se i•• ••••• •• ants if ••••••••••••••• —. • GOYA ORB WM --.. I rum ..„. i • Pa nn rat 3iC 4.21TIE NAV. • swre 0.), ao ant*AA V klOarMa t67 gOlanslt. goODronnort 1Lk4 One idarniutats1 bcrustioth letro3 • ParalAPT CEIMICATION Pa Idea Meet- anal I gIVION.11•11.1.0 ...107.1 •WICIL0T S•tOTICATIO4 OR TIME CLATIFICATII ir 4 401111•0••• VOL Jull•OTITHIPALSSOINCThill Cane ••• ••••••• AO I 0/0•••• ea OTI••• . oneIassINci IstA0 NI • • ...CRAFT LISTIMO/0000•MS /••••••••410.• TM CUITSITAIII ITS MOW ••••••StCasprors ••• . I ;.• i C. PALMY" OITINTION MD UPAITMOICI ALIC0.04 i - -- DIVA INCA •I TOTH. IMICIAVit NOUN - OPtOtser*L040.. 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Oa at at • I3.1 PAX." :II Dm Oa ir•PICTORIPSSAWill • OiSTPICTOSICII , 5 EA- mtbo 0 OCMAIIS SI001•404 Me s) 1 , e id uar.... ' ••••• ,0 9 - 0/ - a5 a s MM o 1 - 1 FM Fenn 41304 I,24.4 TuKtisr3C3 InInnOu5 Menem eC ti soir-t ti-offabe8 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246887 EFTA01331350 tire -M -027544es— — SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246888 EFTA01331351 VALSAA:OARTNERS 3014 Westchester &venni) FAA form 8130-6, ,Application for Airworthiness for adding •Margot Survey* to the authorised our Experimental Airworthiness Certificate. The aircraft is • Boeing 727-100 which has been retrofitted with P G W JTBD-219 engines on tho POD positions and -78 in the center position. We have flown the aircraft approximately 17 hours under the presently issued Experimental CertificateS' We aro requesting •Market Survey" so that we may take a TV reporter and cameraman from Paine Field, Everett, Washington to Grant County Airport, Moses Lake, Washington on 1 May 1990 for demonstration of the Stage IIV Noise Characteristics. The duration of the "Market Survey* portidn of this Experimental Certificate will be only for the one, flight from Paine Field to Grant County Airport. The certificate will then revert to 'Show Compliance with DM's' until expiration of the certificate on 1 August, 1990. b SDNY_GM_02759967 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246889 EFTA01331352 [7 FAR AIRCRAFT REGISTRY CARIRA 10. I DAUS s- SDNY GM 988 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10,-15, and 17 EFTA 00246890 EFTA01331353 .FAA AIRCRAFT Picts/at CAXERA SD. 1 DATES - 8-9/ USOmennen: efren:PC0114s Feclen0Adelion AdmWastreeon ,Manufacturing Inspection' District Office 7300 Perimeter Road South Seattle, WA 98108 May 1, 1990 EXPERIMENTAL - SHOW COMPLIANCE WITH PAR's/MARKET SURVEY MAKE: Boeing MODEL: 727-31 SERIAL NO. 20115 REG. NO. N505C THESE OPERATING LIMITATIONS SHALL BE ACCESSIBLE TO THE PILOT This aircraft must be operated in accordance with the following limitations: 1. No person may operate this aircraft for other than the purpose of Show Compliance with the FAR's and Market survey to accomplish the tests outlined in the applicant's program letter dated May 1, 1990 describing compliance with FAR 21.193(d). . Additionally, this aircraft shall be operated in accordance with applicable air traffic and general operating rules of FAR 91, and all additional limitations herein prescribed under the provisions of FAR 91.42(e). 2. All flights shall be conducted within the geographical areas described as follows: 1. Western United States of America bounded on the East by the Mississippi RiOer, on the North by the U.S.A./Canadian border, on the South by the U.S.A./Mexico border, and bounded on the West by no more than 200 miles from the Neat Coast of the United States of America. 2. Base of operations is Palmdale/Lancaster Airport, Palmdale, California and secondary base of operation to -be Moses Lake Airport, Moses Lake, Washington. 3. The pilot-in-command of aircraft must, as applicable, hold an appropriate category/class rating, have an aircraft type rating, have a flight instructor's log book endorsement or possess a "ratter of Authorization'Oissued by an FAA General Aviation or Air CaYrier Operations Inspector. 4. This aircraft shall not be flown unless it is maintained and operated in accordance with Boeing. Low U441ization Program, I/A/W FAR 91.169(f)(4). 5. Upon changing between operating purposes of a Multiple Purpose Certificate, the operator shall determine that the aircraft is in a condition appropriate for the purpose intended and has documented that finding in the aircraft log. 6. This, aircraft shall contain the placards, markings, etc. required by FAR 91.31. ! • ''..7.1:40 -4 2- • SDNY_GM_0275998.9 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024689 I EFTA01331354 FAA AIRCRAFT A GIST&T CAMERA AO.._I PAM 02 g .Federal Avia Manufacturin tion Administration g Inspection District Offi Experimental ce - Show Compliance • Page 2 of 2 with FAR's/Ma • rket Surv ey, Cont'd 7. The.co - received in gnizant FAA office must wr be incorporatin iting prior to flying thnotified and their resp g a major ch onse ange as defi is aircraft after ned by FAR 21 S. This aircraft .93. approved for day/night VP • • 9. No operat R/ IFR only. or in conges ions shall be conducte te d ai rw ays except fo d ov er de ns under ATC co ntrol. r takeoffs an ely populated areas d landings, and when 10. No pers on may be ca that person rried in this is essentia aircraft du Show compli l ance category for the purpose of the ring flight unless . flight while in the 11. Thin ai intentional rc ra ft is prohibited ma from attitude, an neuver involving an ab aerobatic flight; that necessary fo abnormal attitude or ab rupt change in the airc is, an r normal flig no ra office. ht unless ap rmal acceleration riot ft's proved by th e cognizant 12. If airc AAA raft, engine exceeded, an 'or propelle appropriate r records. entry will beoperating limitations ar made in the e historical 13. After th must make a e aircraft has been re-e lo ng 91.42(a) and g book entry stating th ined, the pilot-in-com PAR 91.42(b) e aircraft co ma . mplies with nd PAR • Michael J. Aviation Sa ty Inspector SEA-M100, ANN- LOBS (Mfg) These limita tions will ex pire on Augu st -1, 1990. • sparacerabio P R P A SUBJECT TO OTECTIVE ORDER RAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002461 EFTA01331355 FAA. AIRCRAFT RTG1STRT CAMERA ND. S1 DATES VALSAN PARTNERS 3014 Westchester Avenue PuraiS77 May le 1990 ' FAA, ANM--108S 7300 Perimeter Rd. Seattle, WA 98108 Dear Sir, Attached is FAA 'form 8130-6. Application for Certificate, for adding Airworthiness "Market Survey" to the operations of our Experime ntal Airworthiness Certific authorised ate. The aircraft 'is a Boeing 727-100 which has been P 4 W JT8D-219 engines retrofitted with on the POD positions position. We have flown and -78 in the center the aircraft'approximatel the presently issued y 17 hours under Experimental Certificate. We are requesting "Market Survey" so that we may take and caaaaaaan from Paine a TV reporter Field, Everett, Washingt Airport, Moses Lake. on to Grant County Washington on 1 May 1990 the Stage IIV Noise for demonstration of Characteristics. The duration of the "Mar ket Survey" portion of Certificate will be only this Experimental for the one.ilight'from Grant County Airport. Paine Field to The certificate will Compliance with FARIa• then revert to *Show until expiration of the 1 August, 1990. certificate on Sincerely yours, Cheryl BZoyd fotlS.J. Wright Valean Project Pilot SDNY_GM_02759971 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246893 EFTA01331356 SDM'_GM_02759972 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246894 EFTA01331357 I FAA A I REP.AFT REGISTRY Il C lOt IRA NO. I DATEt .2 - g - qi • UNITED STATER OF AMERICA . 0113tAPTIMENT OF TRANSPO RTATION— FEDERAL AVIATION ADMINISTRATOR ' • • S'ECIAL AIRWORTHINESS A CA • ORIMDESIONATION CERTIFICATE Punt OM 8 maw). Ns) " p FACTURE ADDRESS C FLIGHT FROM TO O "- — R 10. •UILDER I • MODE I A DATE OF ISSUANCE a E °P oat 0 0 FAA T,1sY %PART OF THIS CERTIFIC ATE A a ORATION oft OFFICE NO. CH RT S A •PRIV•Iwor wan* .1am Cenfloo DAR-48-AC-NM emadis4 3 ram or 70. TWO on by • I— ea says 7100 w A CERTIFICATE MUST MI Es LATID espissanns AN Al AWATIAN menus •rinvy MIKE AMA-Ian IN ACCOADANCE WITH FAA POSH SIII0> (7.70) Wt milv sou! EDITION 888 REVITASS SIDS . • SONY GM_02759973 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246895 EFTA01331358 I FAA AIRCRAFT PICIST RT CAVARA PO. .1(4 DAT! , 2 — 8-9/ ---- --,,,hotyFT‘ sh>4 . A Thb OblOgratthett autlfla t hart ow Fecterh/ A vition atbl fithAaRROAtity Of the FalethlAVi ii SPX ... IF tloetitaat Tbit altwortIgneu mace. . . duct production Mat nits. ad auttutitha tA• aliMittater fumed on the oily prodnetke RI* tote. of nine Wilt. coo- , B nuns No pence may conduc sitaaft reidwered al Us sone or wpm>. for t production night tuts undo; this certfEcate: (1)Cur moon of the MOI. COMPPLIt4011(II hut; and/or (2) Carrying parsec. not e a ybrm per. to the rc Thb airworthiness certificate pew abown le Block A. authorize. the (bah, apecifird oo the men. site lax the put. This sintorthineu cortillcate Sued has been trawled andcertifies that. as of tho data of issuthm., the simm to theraft does not mew the found to mon the repot:unmet which of the spoilable FAR. The n D worthiness code u noddednquinewrou of the ep-Araba comprehend,' and duelled a- No pawn InrY Operate the by Anna 8 to the Connmeloo On laterunboal Ord Minion. with IS applicable FAR andWendt ditscribea on the mean side: In accordance with (I) exaspt In accordance ponalb by an Admin istrator ea part of thisco conditions and linutailoos which may be pure ed special permisdon of that countr rtilkata ;(2) one any fccelvt coulay with. y. .• _ Vann wooer oatnedered, oispen E for the dentioe and under ded. or revoked, this airworthiness the conditi ons preseth catillate a 21.211. ed in FAR Part 21. Section 21.101 or soiiiWA_:62757thiC SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246896 EFTA01331359 tAAr.kiRCRAFT REOIStf! • • CAMERA MO. j DARLA oia - 8-en Manufacturing Inspection District Office 16501 Sherman Way.-Suite 200 • Van Nuys, CA 91406 February 2, 1990 EXPERIMENTAL - SHOW COMPLIANCE WITH FAR's MAKE:'Boeinn MODEL: 727-31 SERIAL NO. 20116 REG. NO. N505C " THESE OPERATING LIMITATIONS SHALL BE ACCESSIBLE TO THE PILOT This aircraft must -be operated in accordance with the following limitations: 1. No person may operate this aircraft for-other than-the purpose of Show Compliance with the FAR's to accomplish the tests outlined in the applicant's program letter dated February 2, 1990 describing compliance with FAR 21.193(d). Additionally, this aircraft shall be operated in accordance with applicable air traffic and general operating rules of FAR 91, and all additional limitations herein prescribed under the provisions of FAR 91.42(e). 2. All flights shall be conducted within the geographical areas described as follows: . - _ 1. Western United States of America bounded on the East by the Mississippi River. on the North by the U.S.A./Canadian border. on the South by the U.S.A./Mexico border, and bounded on the West by no more than 200 miles from the West Coast of the United States of America. 2. Base of operations is Palmdale/Lancaster Airport, Palmdale, California and secondary base of operation to.be Moses Lake Airport, Moses Lake, Washington. 3. The pilot-in-command of aircraft most, as applicable, hold an appropriate • categmry/cIpss r In aircreft type rating, have a flight instructor's tootiirdatOme ssl"Letthr of Authorttatlon'-issued'by an FAA General Aviation or Air Carrier Operations Inspector. 4. This aircraft shall not be flown unless it is maintained and operated in accordance with Boeing Low Utilization Program. I/A/M FAR 91.169(f)(4). 5. This aircraft shall contain the platards; markings, etc: required by FAR 91.31. 6. The cognizant FAA office must be notified and their response received in writing prior to flying this aircraft after incorporating a major change as defined by FAR 21.93. :7. This aircraft approved for daY/hight VFR/1FR only. :2f' SDNY_GM_02759975 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246897 EFTA01331360 TAX AIRCRAFT RICISTILT CAF.ERA NO. / DATER 2 - lc- eiv • • '.7. 'Federal Aviation AffieiflstYdtoi-i Manufacturing Intpection DiStritkOffit8:- ExperimeNtal - Show Compliance with FAR's, cont'd Page 2 8. No operations shall be conducted over densely populated areas or in congested airways except for takeoffs and landings, and when under ATC control. 9. No person may be carried in this aircraft during flight unless that person_ is essential for the purpose of the flight. 10. This aircraft is prohibited from aerobatic flight; that is, in. intentional maneuver involving an abrupt change in the aircraft's attitude, an abnormal attitude or abnormal acceleration not necessary for normal flight unless approved by the cognizant FAA office. 11. If aircraft, engine or propeller operating limitations are exceeded, an appropriate entry will be Made in the historical records. 12. After the aircraft has been re-engined, the pilot-in-command must make a log book entry stating the aircraft complies with FAR 91.42(a) and FAR 91.42(b). These limitations will expire on August 1, 1990. -• awit ALtoc99i6 SUBJECT TO PROTEC TIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246898 EFTA01331361 Tat Al ECM/ I 'ITCH TIT CAX88.1 Ar DATES 12—S- ' Form Approved 0 MAJOR REPAIR AND ALTERATION OMB No 2120-0O20 eatromew. oftwendu (Airframe. Poworplanl, Propeller, or APO:num) Fat FAA the Ore meteMen Oda Idemilication Ameraments fSb0-isr SO- INSTRUCTIONS:1feet WOWSinew. See FAR 439. FAR 43 Amanda, S. areAC43.041(Or sublievent revisionmm.00R for infittections end disposilen Of this term. This revert is rebuked by law (49 U.S.C.14211. Fallen/IC moonrunnel M la anil penalty nottearcendS1.000 fraellaCh such violation (Section 901 Fleets/ emotion Act of 19551. Mete Model i. Adman Boeing 8727-31 Serial No Nationality and Registration Mart 20115 85001.3 Name OR Shown on reptstraion Cerribra) kerne (As shore on nopisteafkal Certilkalfl . . • 1 Ownat .•. • forthweet • Holding Corporation . • ' P:O. Box 7138 1 • . -rn Milaington, DE 19803 3. Per FAA Mee Only - - 4 a • I. UM lemilliesike t 5. Type the Make • Meal Side Ng. Repair Alteration AIRFRAME lAd SWOONIn nom lobe ) x POWERPLANT t.' PROW : t Type APPLIANCE Manumetutm ( — S. Conk/rate Stalemate A. Adeney's Nene and Addams J a Kind of agency C. Choi rale No. ua Centaur madame Page Avjet Corporation . Fenian Canneeme Mae 9809 Tradeport Dr4ve ' a Ceneenve Ate) SUCe. 0848425H Orlando, Florida 32827 vauftows 0. leorIllyttnat the repair ancifor enetelionmum tat oon ID) idemnied in non 4 above and deiented on the reverse of attachments hereto have bee made in accortlence Mtn the reQuillarienta °IP ri 43 ol the US. FOtt* Aviation famished herein is true and Cermet to the best of my Regulations and that the iNormatiOn • Dila • sure 0l Auye dlndS4dual • / Ae ' 8' 6•Pr /970 ' ''... 7. APPlevel lot Re um To Service . Pareent to the authority Lee persons specified Wow• the jinn rdmitined in item 4 Mintage/Mot Of the Feces, MiadOn Adninntratl0n end Is 43 APPROVED was mental In the TOMx preKribed by the CI REJECTED ' Pearl,. Starearcit . Omer again Immusof Manufacturer insundonAuthorttation - BY . • FAA DM*" x Floss Station Person Kee/WOW nangen Carleas AirmanhInesa &outs OateolApproaetaReeMIon Certificate or crYAbilionsed Individual Sig / Designation No. /4 4 ' elef 0 r. 90 054842511 L ,C, -; :a /6 0 1 -1.4-7 -4 /2.4-2/1-1-- wirwailiaz‘a.L." .. • L.. SDNY_GM_02759977 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246899 EFTA01331362 FAA AIRCRAFT 1E61ST1I CARIPA N0./ N DATER 12 1-90' Weight antibalvies at operatinglimita NOTICE tion compatible with all prewous initiations changes Visa be enteredin the appropriate sorcraft locoed. Ameli to assure continued conformity with oration mull be the applicable iitworthiness requiremen ts. • y well auctin nar onatdyowl regatr ithon mart and date *Cy* COmpt•led.) B727-31 115001,5 $/N 20115 1. MODIFIED POW PRODUCTION FOR ERPLANT INSTALLATION TO FACILITATE RE-ENG AIRCRAFT HAVING REMO TE ENGINE OIL REFILL SYSTEMINE ACCORDANCE WITH VA 7100 IN 0, REV. CURRAN NM-383, APPROVED BY 8110 DATEB) DRAWINGS PER DER THOMAS F. D SEPTEMBER 4, 1990. 2. PERFORMED AIRSTAIR INSTALLATION IN ACCO (STRUCTURAL SUBS TANTIATION OF EXTERNAL DOUBRDANCE WITH REPORT 442 COMPONENTS FOR INST ALLA TION LER AND MISCELLANEOUS OF FORW (INSTALLATION INSTRUCTIONS, BOEING 727- ARD AIRSTA/R) AND REPORT 444 IN ACCORDANCE WITH N.D.L. 750-1-002 100 FORWARD AIRSTAIR) AND BOYD SMITH SO-351. DATED 9-10-1990 BY D.E.R. SUMMARY* 1. PROVIDED WEIGHT AND BALANCE UPDA TE. 2. EQUIPMENT LIST UPDATED ACCORDIN GLY. 3. ALL SYSTEMS OPSCHECICED AND DO INTE RFERE WITH OTHER SYSTEMS. 4. ALL PERTINENT DETAILS OF WORK ACCO MPLISHED ARE ON FILE AT. PAGE. AVJETIDRPORATIa5 UNDER WORK ORDE DATED i*:5".or./9 19(.7 . RS 4706 AND 6278, • . SDNY_GM_02759978 -- SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 002469(X) EFTA01331363 TAIL AIRCUTT XECISTIIT CAEttA II0.1 N DAM / 7 21 90 totatOPAYLI MCC. ATION TIW4PORTATICOI—FECSAL AVIAtiONOMNISM WM WENT Of STANDARD AIRWORTHINESS CERTIFICATE CAntipor .the WOO. {) 4.440 4441 1.0444... 14 rociPoitYr., •••3 IMIS.• sl:41,444C44•00441 • 1150013 BOEING /27-31 20115 TWJWFWN ...,16650.1/•MCI 1613 fro:: I:U....a ost.lootamotinwns tr4 SMIA4.40•Ma it WA sencorti. on.cio n....0.3....1....,10.OF ot4 ben 44044:1440 444 .14.112 to••• 0 Ole 448 (.444.4614 week 4 lotto% DoOsitato 4:0•Vonntira ats•ad haf..totnas 1•01at oProl.• tr'd sat*. trieo".0 It% ••••••••tootnt.. oocootos orma Nom aMENbAw. • wC44/0010 1•04110 144. 11414(44 I C444 *seat EM. s. • 6 TEM., 66.0 6 0.1:611066 owe.. saes. w r.• Airmsyster v..• onset Y tennwilo••••• • Von% 6:-...• soSibrat 0441114.4.44 Y. 01•6610.1 et 06.10.6.64 es . IWO 4.4001.40 60•616.14.160 4 Arnit4 4443 0411402/1 On•Cos• osavron. win •••0401.it oinoise> MCOIWC6 ,..taastilainill et yeFoln. AasPeossem SUS k'...eilop!'• • 1 SDNY_GM_02759979 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024690 I EFTA01331364 r-iAA A)F:AAFT MEGISTRI Ck,-.ELA IND.7 # Dent 72-27-90 I ;its; • sorit :A6O89saa SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246902 EFTA01331365 FAA AlICIA TT AEG111117 CAXTEA RD.; fei DATSI• Zia/ —90 • • ' • t. OEPARTMENT of TPANSPOIVItgaMITZ CZ/lATIOPIPalllarnt ATION STANDARD AIRWORTHINESS CERTIFICATE • 1.410.•trIvne P wine. • cam • m000. 3 A10.41 11....14 ICOISTMTVP. Man N505C BOEI.NG 727-31 20115 7RANSPORT AUTIOWTY NC AS* 'OA 11.10.10C.1 14•4•••••••~fletatSeeluage.....••••Sefilaila0Anill•nAcniltilitlo W4.1kniMi $10•01...• •Lteagre ihr • loatI01 hi iSc *Mall IV twit ••••NIN rd loWneSiinst.PreCIPPMAPM.I•Sir Ina it.../..r.t• 14. 011011•Ork NV No Non re.r. new,* •••••••••••• r w 01.001,0 rolsowerweir. patairy AMIN I Oft CC"..0100 a lolorranr C./ at.s.an yam a•O • • - 4010.1.• • I Tata NONE uo CON:01010 lb.m• scri vireo. wsiev.• two.* ✓.w..Mrm wt t fawn. twessys a... tr.' 1 Nast...u.Pes: nen aineinnspo modes.* OW.* a tap SW. ...ratan sofninnti• COMO stulasegow11....went ay. .traes when.. a II septet ntiati A “Ipaenn.••1••••• JAY( OF ig$VANCC liCtiK500 Alta VS % •••• DiSed.0 0414P/W4A 7/23/90 VINO C. CNINW DAR-41.4S-NM iltryaima."•••••agaastolenwdm e.••••••11<sona. twOrnywes Oian, re nalinbett .; COP to ap..w.onsort.u.nno.-11 7..15 COMMA C IC DISKAVIO TI.L.WCAM T ACCOOIONCE AVATONFILGuLATOOwS APNallt It Of AM FAA Form 81004 o••••• ' • ••• • • .4170 c S. • .• _ _ SDNY_GM 02759981 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246903 EFTA01331366 ref. FAA AIP:FAFT REGISTRY CA,JF-A A. O. s DATE: _ !nit ar.• • • _L_ SDNY GMOffc9982 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246904 EFTA01331367 AA AIRCRAFT REGISTRY C RA O. I N DATE: 8- 15. 90 neer ••••• ••• • E.• ram AtOrtref 0. APPLICATION % .44 011 ‘.. FOR Inlealellella — Pe• m Os Do ea urli• in 1•06 ••••1•0 eat Tag on fc• /AA AIRWORTHINESS ww ally Sun* moo on• Ns., g m .. •••••••••• CO Peprnenlene H i4c.'scow AMCION0.0011.Men sltnemen •••••••••• CERTIFICATE FM*Os lir corn enom Sec lion nommotAintipW.Aew " T nnAtb:""W. Ausatuyenalluielit Ilda•O# \seen* eltol*z.0M•lattrei • ell. ••• b5o5C IAA 007 Boeing 'A' •. S. AICAMT 141440 727 - 31 03 • 0.40.• WA ours NN ' 69 ' /maw • poet .4000. oneOn 24:101.0 .,... . one 20115 Pratt & Whitney me •••••••• Of •••••••• 3 - A na•ntat is 00 5 NAY* 0••••• J780 - 711 IA •••••••••• soaci.o.eyourco P29,5 st. ArACANT IS Wan • eeeknes) ArIVCAlliCe 4 NNW Omer Fa (Goa •••••••• Ant IMAM A I STANDAR*mffireaborlia• - COUVICAlteleme eibeila I LIMO& I • I UTIUIV I lAlaelealet YUMA utabilyelbUIC 1114•41001 1 100001 HON:LOOM OMOCAltreaeins.40005•My `I IWO) € I PROVOICMM. esimolaii I • woo . g COMM • F. I, • Ale•ClallatO/0007 Cann Pa Metw•Alni•41040 I SOL SISIMICI • leno MC=ne* • ••••••••••• 74•••• § 4 0000210014••••••••••••/ • fATIOLL0.0 ,g iFO IssliOlepoL neon in -•C,> . y a WOO! OF WA* se sum. se waterlog! . • I' OTennessen • VICATNIDO•wrilel I NAOMI loun.T •I 40.4401 lonesome* • RAC•4 • Oa Menai I I NM NSW TO SNOW COSIPWOICOW INIPM I war negro.; wet ...truaricsi IMMTliaget O IT maw FLOIT Iilliert &ands • • avacuon no. WAOf asSIO •••••••••• SA ad CANON •••Aires •••P.•lries.v.tee m is I Of•A•TION •• MAU OF SUIGNA. • . . COUIIICATO) T404-0ff Maar . • 0•44.04141. OM Weer ' - f aI pii0oucncei tuna Tunic C lel II a.morsua 40.60.6TOATION MIATVIANIIIISITISNEMCW0Cotla FlOC3 .sUA•OK Ornserf .see lommees *nog , e wenTIVID)MOMMoine e.Melenn •••••••••••1••••••••••••• Audi IF SUR, OAP a i Northwest Holding latag Foulkstone Plaza. Corooratioi Suite 102 • Ana. UMWCATION4AINIC 1409 Foulk Road , ••••••••••••• am1•••••••••••• P.O. Box 7138, Vilmington.DE AMAMIMO/CAMS CM My same salArran.N•1 CUMICAllDMAIMP Ham Al• •EnegiorrnieSS MCCAW 19803 A3WE I x :3Mew •51•••••••••••••• ••• ea ••••••• ..ACOL80 7 IssaADssiAL 90; t0 c0 LellegiOinen.~0.1, 2- rli ncA9 „r„, Rev. 18 5 Dated February 20. ......sio C.I4OCIOVirt ortatatiCa MO 1987 iiArtIPIMaCI ateore0 *CCU OleCOICON . TI Toni MOW* MOM •g X Catissaaffh. WilingliiThlOitillY Mar hike IRano✓A • 1e leis. •,.•..p ..... orWar• ' 29820 Hours -0- a COITOCATIO0 - 1roe . alesevinamontleares ea Yoe Owl ell Oneell noe sop lets elm el we 41•111dI So es••••••••••011 Osioneobea en we or* Inner* same mo ons.- yenomer er Ma innione• Imo nom emaolleeineemen /Wain memo semen w1- Ono one oneetimmtoone eon cm MPLICATION IT re yy alsan Program & February 2 1040 7 7 1:14Y: lik 4 IONIC•On 040•040••0* noinperino Hanaoer OS Pam *WIC Tgio NO FOUM) ,b..,...1...,..............c.,..... Wpm,' in On In Cilltry.CATI .4000.1 0.11•0117NY ay etisoble Pe •••••••••••F•Al , rotar...vo itll I/14. lc.......a., i0o• b pI laminCAZD a re•Onnelles w 11 . TI ,..... ALL arra.. •••••• •••••• • seIlb (Tint mo I Alia. Os es stun •••••••••••••• X THICalliCMCNOlartal, I it nol••••••••••••• Y • _ •••00110(r046 .1 ii.41.040I•41•114•111#10••••• fl .00, FICATIONOF0.101•04T•IANGIOPM .• • ier Ilalluall • O•CM Milt ilIPCATe so weVOW IAA 040•Cere 1 2 Crean EtAA Need/ WS 04•••• OU . . *Con teen wits f 'fault>. in.. IAA NORA TOR 6 YANA Tyne 4--[..,„ V. 4-!•-• ansy.S I ------- - ft " I C' a .. . -. tvityt- $r - "re -,- Ain i 4. • en"- - SDNYfilt02-7r9983 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTAS00246905 EFTA01331368 lA AIRCRAFT REGISTRY NO. 1 N DATE t 8- 15- 90 IL wimeSACTJUX ... last SOUS ... , . -- -_ 1I in niCouCTIONMSOIOM. Ogaftn.M.9 —- - - .CA.cIt."— 4 4 .. - /3 \b -c .• Nr --.‘ . I 0.00X1IONCUMOCATIMP4Kneadm.S.•00......M.A , L.., Tin connininisava • A -: - <G 1/ • 1 " • I; 4 ‘ , MUM° 0.0ournoltealtatiColnips C OW MAMMY OF CeRrintialinameo Ka COSMO hirtgO Tinnig NOITIVE Omi rine/ Vomiting MR Of OniCATiOix I Miff/S.7Mo O. anatT Kola Mimi I/004a UAW laelial latinlIATICOIWM ' • O1.101/r4. Of Ivan . ' ainC400104010714.4110•0000 1 CI gam ovinaloi WM TO Cogniavng OM • . ISM.. W4 1 1 C ailvolvOunin TO MOOTS T.4 kinigan NOVI War. Into, [ coaLca I loom:worn I prhaiss.ort wing Arlawfi 004.• *OW ImEnnomoott durvoOPOfNM ntOu•VOONTS PA POW:4ft . ' 1 I 1 •- tai; • '64:, • • I a tuimasonmarktrawgtooted°seam • red. . ipmar area• rommort . .. _ . _ . . ., . . . • - • 1 min. tatotil...am.. in.Nem, fr.simmomeasia.. taVOTCATOS- • onVIcolor miiI m ihgeOvvmm 4s Wm 00441•40mansomenom ......., v. ' ,WOO\ elpiNVIS sae. Masi III -- w noel .-. .. .... . . Out 10014 NO Taut S. to toot 6M...rust . . c, kw...a, 0,..,....,,. Su Ara 2130* Mann *Asa •••••••••/ I X 17: .= M. ............ " 0116. Cary illibine MA • I woo.mm...... c.,mom s 1•9001..{..41 (4.0~•••••••01 i >LS C4m.gommiliLaing.. men 1 II COS. 0••••••• ••••••••• IN rum. ~over, 3 Xo.C....1~••••••••••••••••••••ASSIOSAMIlt • 'IM-2 N 22 aim... a ..atanSerr err .".'es'..." . moms. ma i iTu *aniownwn - I. WOW IWO. W /SOW Wiles O OSINO WWI _..nil , A Cur. Aomrtme E I. f...I UAWsulkosenu n usniniironi• es. at. MI (b) Kau ...nu v SDNY GM_40498C- SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246906 EFTA01331369 AA AIRCRAFT RECISTIT RA NO. I PATS, 8- 15- 90 VW= STATE* CS AISCA j ,yr DEPARTMENT OF TRANSPORTATION • KOOK AVIATION ACAPPASTRAThiOIS ' SPECIAL AIRWORTHINESS CERTIFICATE SAIEGORY/DMIGNATION / A PURPOSE Alga . i MANKI- NAME 4,10 FAG-TOREN ADDRESS C fl.NIPC FI:3° .,W aziar D P - ftEcc rais SERIAL NO /Ar BUILDER MODEL 02y; . DATE OF IEXWAFICE•AtAlrty /#'t,9 EXPIRY / Va. OMNI ISA/TATIONS DAM) ,r E A PART OF THIS CERTIFICATE E ming DESIGNATION OR OFFICE NO. • - — . 27 4 WO.'" • .... anosanon. traaaceir tat= IN. coeScarriegtbe tg • Ins Ng ••••••10A01.7: ..ronocantni ••:• ap•Anx 3 VON. at coin IRIS CERTWICAT1runatuti* MUST IX Oi3PtATIO Oa IRE Al ACC-OACAACE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. Sll SIKASE SIDE • cir SDNY_GM_0219985 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246907 EFTA01331370 A A This obsrocilsinliscorldwals is 19Sult1 under 11111 up see Fedora, AviiliOn PlOottistion• sat* of M hen AselitmAr3 Of 1951k (PAM. TM elniewihirten een if cateauthertenitternenutechee proijosiion leper lasts and city th, OckCtiort eehl *Ste ofname:Ion Ile Mine Ws loc0rlduel B ,earls repaired in NS nine. WO porsOn msy conduct proOscros soN tests unit.' Insi etallfiesis. (11 Goyim pinta or properly lot compensetio.n of hriP 0°310. 121C tem Mont orryail PerSOos ha saribidloOrriOurPOSOI . .., .• Thissinsociiteces conduits as:bonzes the Hight specilesd on this C shows in Bock 01 resomillti0t for Its surpass This heworminisss conilicillireroodres lost n arms Oats nn boon isspricifslionO mound 10 neer Iristechssemerus onisusneo. Iheeitasn lo which owed no. meet the cetteremente Of Info •PPUCIWO COmOrthenSwit 01 thes011hersbili FAR- Try sirses11000” Phireilled by Arnett 11 to the COreenttOn On IntemetitYleCtet end date*, Itintierthhhale 00de re o Anehteit No Oman may opal* .the &retell drlOthed On the revoltletele III Ceeept et accottlincetetate What* FAR end In SCCorchirio. isrlh Concsisans and limitations which may be pert 01 Mrs °nice* (2) over any !onus., osontry *Sete pasted tiy treAdminisirsior as C0 AWy. the peed prioninion 04 Ina Unless100ost surreoileso0.ssisq0000.or revoked rho is mon/Incas soraissto isomichssior E Is din hon tad 'ander the eeroltens petterebed n FM Pan a Serlion 21 III or 21217 ' . . • SDNYNA_027599136 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246908 EFTA01331371 AA AIRCRAFT RECISTST C. RA WO. I N DArtt 8- 15z 90 DEPARTMCHT Or NAT= 0' astAi T•ANSPORTATION-910ENN. ra AVIATION AOMINI STANDARD AIRWOR ESA CERTIFICATE motto,. 141404 MCA "Ns ,...NNAPTPON 1.4.40 *oh o:••••••••••••• ••••••••••••I 4••••C•• • 1••••• eitneh I• •••••••••••••••• .0 ire • IMIC Or ICS•••••CC Exchange 06 64.1•MabOn NUNIIM WP-FS00-10 IS CI *Lott In • wain. IICA•••• vfl N 011eLATID IN AMMO': IN ACCOID. SDNY_GM_02759987 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246909 EFTA01331372 ?AA AIRCRAFT REGISTRY C RA NO. 7 4 DATE: 8- /5- 90 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246910 EFTA01331373 AA AIRCRAFT REGISTRY C. ZIA WO. 1 N DATZ: 8- 15- 90 • — . UNITED STATES OF DEPARTMENT OP AMERICA TFtANSPORTATION - FEDER AL AVIATION'AO SPECIAL AIRWORTHINESS MINISTRATION 1 CATEGORY DESIGNATION CERTIFICATE Pt; RPOSE 8 AN,. NAME OM AR 000mu C •LIONT FROM TO 0 N- OW/0EN II DATE OF ISSuANCE 14000 . e I• E OP T ON V VI o No 0 2 FART OF THIS CC ',TIP MAT( DONATION ON OFFICE NO. R t.• --- As sralamo• onalm•shile madly 3 ...mose elbas AN be DAR-48-AC-IIN TOG CERTIFICATE MUST st 'mans N. IN ow NamElism Er onsAara MI AMAIION 0120ui roost DttmAyto 04 THE mm MICA/0TM ACCOADOia WITH SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024691 I EFTA01331374 AA AIRCRAFT RECISTRT ERA NO. 1 N DATE: 8- 15- 90 A artifices l le sailor* of the Fate Aviatioes'Act of TSS of the FMtral AvietimiReedece IN an (PARh. ml. ewes gee authorizes the menufactern mewl es the roe 61e to con. duct Fief we DS: Mk ea ce Weak* Welt a of *bath ressesi la his B mete. No pee eftey edam proclortIon Matt teat vet this catillkste: 01Canying pet- was or p competIon as hie: atiffee (2) CliffIRS Pme eel tette to Od pep— of c Tab tenrcelltire wilifIcete 'those the let eptichled cm the me aide lot the pm. pow the la Block A. Tit eremites oertitlate cadre% that,. es of the On of hatmee. the ties l to which burst hes beta Wreak, ad led to meat ti. reiremeats of the applable FAR. The deft don not meet the niquIrementt of the tippet& compteedve and clouded thi- n, rookies cede as pewit.. by Amex Ito the Commotion Os latereationel CIMI Mese. •-• No pence may copes the diet dewed co tise tan We: (I) except In saccade with the applIcebk FAR and in eccodtace with comillikos and balutIons which may he prescribed fey the meet Ike centres;(2) ewe my fore misty teeth pot the epee penalsion of thet matey. AA Unless tomer winederad. eameneed. ot levet. this itiniorthbas renifkaM is elTecelot E fat the thine ad toe the cordlike. prescribed la FAR Part 21. Seen 21.111 or 21.317. SDNY_GM_02759990 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246912 EFTA01331375 AA AIRCRAFT REGISTRY MERA NO. I N DATE: 8- 15- 90 Manufacturing Inspection District Office 16501 Sherman Way, Suite 200 Van Nuys, CA 91406 February, 2. 1990 EXPERIMENTAL - SHOW COMPLIANCE WITH FAR's MAKE: Boeing MODEL: 727-31 SERIAL NO. 20115 _ REG. NO. N505C THESE; OPERATING LIMITATIONS SHALL BE ACCESSIBLE TO THE PILOT This aircraft must be operated in accordance with the following limitations: 1. no person may operate this aircraft for other thaerthe purpose of Show Compliance with the FAR's to accomplish the tests outlined in the applicant's program letter dated February 2. 1990 describing compliance with FAR 21.193(d). Additionally. this aircraft shall be operated in accordance with applicable air traffic and general operating rules of FAR 91. and all additional limitations herein prescribed under the provisions of FAR 91.42(e). °. All flights shall ,be conducted within the geographical areas described as follows: 1. Western United States of America bounded on the East by the Mississippi River, on the North by the U.S.A./Canadian border, -on the South by the U.S.A./Mexico border, and bounded on the West by no more than 200 miles front the West Coast of the United States of America. . • . 2. Base of operations is Palmdalegincaster Airport, Palmdale, California and secondary base of operation to be loses Lake Airport, Moses Lake. Washington. f 3. The pilot-in-command of aircraft must, as applicable, hold an appropriate category/class rating, have an aircraft type rating, have a flight instructor's log book -endorseienf orposseli a 'Letter of Authorizattorrissued by an FAA General Aviation or Air Carrier Operations Inspector. A. This aircraft shall not be flown unless it is maintained and operated in accordance with Boeing Low Utilization Program, I/A/W FAR 91.169(f)(4). 5. This aircraft shall contain the placards; markings, etc. required by FAR 91.31. 6. The cognizant FM office must be notified and their response received in writing prior to flying this aircraft after incorporating a major change as defined by FAR 21.93. 7. This aircraft approved for day/night VFR/IFR only. SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246913 EFTA01331376 taletArr lumina ERA NO. / A. DATE: 8- IS- 90 Federal Aviation Administration Manufacturing Inspection District Office. Experimental - Show Compliance with FAR's. cont'd - • Page 2 of 2 8. No °aerations shall be conducted over densely populated areas or in congested airways except for takeoffs andlandings, and when under ATC control. ,9. No person may De carried in this aircraft during flight unless that person is essential for the purpose of the flight. 10. This aircraft is prohibited from aerobatic flight; that is, an intentional maneuver involving an abrupt change in the aircraft's attitude, an abnormal attitude or abnormal acceleration not necessary for normal flight unless approved.by the cognizant FAA office. 11. If aircraft, engine or propeller operating limitations are exceeded, an appropriate entry will be made in the histofical records'. ' 12. After the aircraft has been re-engined, the pilot-in-command must make a log book entry stating the aircraft complies with FAR 91.42(a) and FAR 91.42(b). These limitations will expire on August 1, 1990. SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246914 EFTA01331377 pen OttIce: - Febrti1Py 2' 1990 - . %OS LonsseAchSivo.#206 TO Fax Mr. Bud Martell, Manager. Federal Aviation Administration Manufacturing Inspection District Office .16501 Sherman Way. Suite 200 refer to Van Nuys, CA 91406 001020290 Subject: Application for Experimental Airworthiness Certificate (To Show Compliance with F.A.R.) - Gentlemen: • This letter is to infone\you that'Valsan intends to operate Boeing 727-31 , Registration N505C, Serial 120115 owned by Northwest Holding Corporation. Foulkstone Plaza. Suite 102. 1409 Foulk Road. P.O. Box 7138, Millington, Delaware 19803 in an experimental flight test program. The flight test program is in support of . the Valsan JT80-219 Re-Engining Program TIA NM-100S-1320. Tents and conditions of the Experimental Airworthiness Certificate are as follows: . Valid for Six (6) months from effective date of the certificate. 2. Geographic area is the. Western United States of America. Operation of aircraft will be in accordance with all . applicable F.A.R.'s and F.A.A. 8130-6 (attached). 1. Aircraft to be maintained in accordance with Federal Aviation Regulations Part 91.169(f)(4). a current . inspection program recommended by the manufacturer (Boeing low Utilization Maintenance Program). Very truly yours. R.A. Broulik Valsan Program/Engineering Manager C/O - Rockwell International 2825'East Avenue P Palmdale, CA 93550 Attachment RAB:Ig SDNY_GM_02759993 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246915 EFTA01331378 . 74matitsin itztittitt th ifts. NO. 1 N . DATE: 8- 15- 90 ro,9!cb s.r‘!.91:rr n r. r• ", ✓-;64. 1 km44; SDNY_GM_02759994 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246916 EFTA01331379 AIRCRAFT REGISTRY CAMERA NO. 1 ?V DATE: 8- 15- 90 us otyurnovrr or IllANIPOWANCY. flOCRAt. AVIATION AtOMSTRATKIN i SaMOSIS MAMIE RPM AND ALTERATION . POI FAA WI ONLY (Airframe, Plwerplint, Propeller, or Apr, liana) OITICE IDENNocAna. • ' WP-PHX-FSDD iNstRucTIONS Prod or type ell eon,. te FAR 410. INA if Append., 8. aed AC For inoraroont tad dispearoon of 43,-I (Ore Natitent ~in 'his form. MAXI .TIC/Oft . I. AllaAFT BOEING • 1 27:.3 ISTRIA1 NO, sNATIONAWY NW liCASTRA TION Man I 20115 . ,: T .... • I. ME '. t ~St iota . Ms twat a at I tatintertettationalot otO • 1110Eftat y A. AGENCY'S .4&491 ANO ADM» rt L MO Of AGENCY • • . C. CIETOICATE NO. v... aitICAreir ratoot DYNAIR TECH OF ARIZONA. INC. rot. Orr Cirttiart 'Otto 3737 E. BONANZA WAY. . .CRS .407-36 . ciamcas isle raw» PROENLE, ARIZONA 85034 - • AIRFRAME IV 0. I cent that rho Nepali eat of alttttt too sat to the larrila I ;totaled to •nKhee•µe taco Ito St sat in too 4 Ktlledaµo oat. the requetotts of Pan 43 ofAte utd that the Ifi4011•4400^ for ea bed boron sad diKeted on the 04 the C.S. Tittel Arena» Itigulation, is owe e d torten Ira the trio of at kroNNYEEY. GAT! SIONANIII Of AWINOIIIMI • . INDIVIOUAC . AUGUST • 10; 1989 . RENNETH ROW80111AMkr Ra„,, - — ; fitinaaas nit Natty One peract tio Alsielarnot of do ION& Ansoor,riaortd bolot the old °tote' in ore i on curd ao the eater proontod,br Aonoroloo NE i• APPROVED htlft . laf NA fat total onnoNCIVISA ~KIP orntatrsON . IN No osmor -. GA11 CO APPIOVAI OR ~KATE OE Ø ING4ONATION NO. AUGUST 10, 1989 CRS 407-36 1111 .a 4g , al SDNY_GM027&D9 G6~ SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246917 EFTA01331380 AIRCRAFT REGISTRY CAKtRA NO. 1 IV DATE: 8- 75- 90 it- 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 (II more space is required. attach additional sheets Identify with aircraft nationality and registration mark and date work completed.) 1. FABRICATED 6 INSTALLED REPAIR ANGLE ON LOWER EDGE OF • FUSELAGE .SEIN FOR NO. 2 ENGINE SIDE COWL AT FIREBALL SUL/BEAD 'APPROXIMATELY PS 1455 PER SRN 51-40-4. 2. REWIRED CRACK AT RH HORIZONTAL STABILIZER LEADING EDGE APPROXIMATEL Y STA 78.3- , 88.8 PER SRIC55-10-3. 3. REMOVED CORROSION. CUT OUT BULGED AREA IN EXTERIOR FUSELAGE SKIN. INSTALLED DOUBLER APPROXIMATELY FS 1157 AT STRINGER 27R PER SRN 53-30-3. 4. REPAIRED FUSELAGE' SKIN CORROSION DAMAGE ES 1166 - 1174 AT STRINGER 271. IN ACCORDANCE WITH BOEING REPAIR MESSAGE NO. ISPN23200D. END 0 12011001 SHEETS ARE ATTADIFI) 6 COvir MMMMMM TtriC orricg. itl4.6.16.631/ NMI ea i ghigtar t gaW S 'SDNY GM 02759996 -- SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024691S EFTA01331381 Vasswie....~.me AA AIRCRAFT RECIStRT RA No. 1 N DATE: 8- 75- 90 • US DIAUTUNIO Of IIIANYORTAION /14 AA • '. ' , • IltDCRAL AVIAT/ON ADMINISTRATION Fewer ~N ed 4 eprit.artffiå den` ~fen Nor. Os -IMO, MAJOR REPAIR AND ALTERATION FOR 41.44 LIE ONLY (Alrfrems, P•vearplaM, Pa/pollen, or Appliance) VNY FSDC "a pwipkinnif.—_ IWI CH4 onyaoot ONE: Prim ar gyp. di rs -05', for Inetrandien• Ned dIspnelMan sewn. In FAR IIA/. FAR 41 Append% S. et Ihb fern. sad AC 431..1 lei aubenw ne nr.i.Na Sawn /Ant RECEIVED FM imam I. AIRCRAFT BOEING %east . ' • 727-100 INATODNAM AND REGISTRATIpN MAU . 20115 MAY 0 ii 1990 N505C WANE /4,8 Maas An totein/Nan ortiAni tumy Fspo !ADDRESS IN aaln... F. LIMITED INCORPORATED ' I' . • •I;an 4NIAtoN) • 1 4387 InternationalSateuaX -• 'Columbus, Ohio • 43219 . 1. POE fu USE ØT • • 4. UN( ID1312±Wle We S. TM ~0 MIA. 9BO• &Mt , i «WO Anon AGNAJAC A* duscried in own I Wen) X POLVERNAIR X PROPELLES YIN AIMUANCI manniviili • • e A. AGENCY'S NAIVE AND 4. Clili011UTI STATEMDIT • rase "MSS S. KIND Of AGENCY North American Aircraft C. CERTIFICATE NO. - . .. .. 44. CittOIWIO oLOCM.41,0t Rockwell International Corpo ration weep. alrtnicann asaInmec t11;;EgW e PhiW?)1Int 2825 E. Avenue P Class 3 amscane mom, 'NNW Palmdale, Ca. 93550 • ' V aswinanvere NXAR688K D. I nnify WI the Link ai/d/as snaeltmws Mine Mn Ina mule dramatis -Ns& ea the ualiN) id...Lila in INN 4 awe en fa Arandanet aids IN requltasent. of Pan‘ips &mint ea the wen* et and that on laktafinIaa twalabo d Awl. In tn. and coma Is Ma Rest et abe U eraI Aviation Rtgulstiont el donne...Wu. DATE . SIGNATURE Of AU114O# FDI MO .2Y n9d • . D. A. Perazzo • .• 1. DUO ,m POE *Max 10 servi å , ~own ea the • MI• ASNIILENNNted i enatek W4 baler W nit ryriied le he 4 watelt.rd ra nZIalslatimlen and k fe. W sa....,er pr..cRim i by APPAOVED RE) i IAA fit.IITANNADI ACIFICKM awasiesa aVIDIETIWALINGNIANON Ewan elesan ST I Eameil l •ILLSLANA l IAA SSW Yaw. ttanON Of TWINGE, DATE Of ATTIOVAL OR DI MOAN CIIIIINCATE OR SIGNATURE AUT ED INDIVIDUAL DESIONATION EC 179:2 ;11 r? V /9q,f) • - NXAR688K e-- e-- _ a,-.. .....v.....,c41. SDNv GM_02759997 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00246919 EFTA01331382 sorii ikoff994 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246920 EFTA01331383 ?PAA AIRCRAFT REGIS/MR CAMERA BO. 1 N DAM 8- 15- 90 NOTICE Wiight andinfante 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 alnvorthiness requirements 8. DESCRIPTION OF WORK ACCOMPLISHED (IF more space is required, attach /den ti y with atrcra/tnet/dn;lity arkt registradon mark and date wVv/t completed.) additional sheets. • • .. • A. Modi Model 727-100 , Serial Number 20115, in accordance with supple- ' menta, type certificate SA4363NM. .amended- September 1, 1989 as follows: 1. Valsan-Boeing 727-200 Re-engining Document VA000001, Revision F, dated January 15, 1990. . • 2. The following drawings and engineering orders (EU's) are in addition to the above document: NOTE: ' fliAs denotes Valsan Dealing. a: Chapter 24 ELECTRICAL POWER • A240000 A Electrical System !esti. - Strut E.O.: 003A,'101 VA240007 E Panel-Load Control Center Modification E.O.: 003A, 004, 005, 006 b. Chapter 28 FUEL SYSTEM INSTALLATION STRUT- - A280001 B Tube Assy - Fue Strut Feed Thru E.O.: 100 c. Chapter 48. MISC A481100 A Pressure Buldhead Reinforcement Sect. 48-727 E.O.: 101, 102 VA481200 C Frame AssyoSta 1263 E.O.: 101. 103 VA481300 C Fuselage Skin E.O.: 100, 114A, 114, 116 . VA481324 NC Intercostal Assy - BSTA 1223 to BSTA 1243 W/L244.39 E.0: 106 VA481325 NC Intercostal Assy - BSTA 1223 to BSTA 1243 W/t234.06 E.0: 105 d. Chapter 53 FUSELAGE STRUCTURE VA530001 - B 'Ballast Weight Instillation E.0: 100, 102 VA530003 C Ballast Weight. Support Structure Assy. E.O.: 002,100 VA530004 NC Ballast Weight Instl. STA 312 - 360.E.O.: 002, 100 e. Chapter 54 NACELLES & PYLONS A543000 C Main Strut Assy (Sh. 1, 2. & 5) E.O.: 003 VA543100 0 Firewill Rib, Side Engine E.0: 36A, 003A f. Chapter 71 POWER PLANT • A/10000 NC Power Plant Instl. - Engine Pod V727RE (.0:: 002, 1058, 109, 108, 001A, 104A, 005A. 004, 110. 003, 111, 006A g. Chapter 73 ENGINE FUEL AND CONTROL • VA732301 K Approach dle Solenoid iring Diagram E.0: 002(Rev 002 (Rei.IM), 003(Rev. W VA732303 0 Relay but'. - Approach Idle Solenoid E.O.: 103. 003, 1008 VA732304 Switch/IND Light Instl -.Approach Idle E.O.: 002. VA732310 A Switch Instl. - Nose Gear Position Approach IdleE.O.: )03 VA732315 NC Relay Instl. Pilots Overhead Panel E.O.: 140, 002; 101 Chapter 76 ENGINE NTROI, 9A760000 A ngine Controls 'Intl. - StrutE.O.: 002A VA760014 A. Drum Instl. - Eng. Controls E.O.: 100. 101 VA760015 A Bracket Assy - Pulley ESTA 100 E.O.: 105 ACCIIIONK SKITS A17/040 •1/.11•00VillIMIIIST INVINTIOIO Or net me 4111.raligrin SDNY_GM_02759999 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024692I EFTA01331384 , %- . , " • plrevriSairrl -5*.41.‘ smisacoatio SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246922 EFTA01331385 DESCRIPTION OF WORK ACCOPPLISHiD (COAtinUeN) Serial No. 2011S i. Chapter 77 ENGINE INDICATING VA771005 NC Indicator Engine Pressure Ratio EPR, J. Chapter 78 ENGINE EXHAUST VA/80000 B Engine Strut controls Insti. E.O.; 002.. VA783010 E Flt DecknIndicator Testi. T/R Sys. E.O.: 003. 004 VA783011 F Thrust Reverser System Wiring Diagram 402 (Rev. G) VA783013 D. Support Bracket Assy - .T/R Control Valve R/S E.O.: 100 (Rev. 10 VA783017 J Placards E.O.: 007.. 008 VA783024 B Relay Instl. - Thrust leverser Control E.O.: 003 VA783028 A. Mixer, Exhaust ‘. Inst1. 727E 100 VA78310I C NO: 2 Engine T/R Wiring DeaCtiviation E.O.: 002 Chapter 91f.HARTS • VA910002 A Inst1. - Electrical Wire Harness E.O.: 003. 004, 005, 006, 007 * VA910008 NC Wire List V727RE E.0.:- 00.1, 002, 003 *New drawings added to modification. .8. Boeing 727 Service Bulletin 727-53A0171, dated December 14, 1989..: Subject: Fuselage Station .1182 Pressure Bulkhead Web, Crack Repair'and Preventive 1 Modification C. The aircraft empty weight and center of gravity was revised in accordance with Boeing Weight and Balance Manual D6-21200. Weight and Balance Manual Supplement, VA-CR279 is attached:. SDNY GM 02780001 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246923 EFTA01331386 ,FAA AIRCRAFT REGISTRY CAMERA NO. 1 N DATE:. 8- 15- SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246924 EFTA01331387 IAA AIRCRAFT REGISTRY - kg . AuggA No. / N DATE: 8- 15- 90 41 r . 727 - 100 / 200 Weighing Form . . . :r' 1:e2 Dote ' ict .7 i .4.144kr gt:‘ 'a:. Model 'Serial Number Place Weighed 4/18/90 eohnic lan: 727-100 2011B- 8505C EALMDALE 1 POLE" REACTIONS . SCALE . TARE NET ARM READING ..:, WEIGHT, 4 .49. 1* 6 Left Outboard' Main 24402 it Left Inboard Nolo 6 244 10: . a..drale...s..trre..1.... 21066 21_ 2186 A. 0 - 4' la ,..v.J.:,- . 4 ' Right Outboard Main 23687 • -4 • -4 23603 c Right Inboard Main 23381 -.-, ''• ...-:.. % -...mie.a.....i. ipildr 23304:U ail a Pd. N Taw e ie Subtotal (Mains) 93335 : H - 7 93342 A 4 .1 CAMatriLIE,Mt$ AWID::: ' 688101 Left Nose 13351+ n 0 1339 Right Nose 1498 ..dde..2-4.*,,,m.4.4r),41.2- - .‘vh... 0 14 8 en- Subtotal (Nose) 2837r, ,-ma-4.emosna--4.144:e"vemsracavaric: 0 2837 s 311 V- . 2 TOTAL 1 96172 'ar.f. , 7 9617 931.20 89 9364 . LESS Items NOT pare of Basic Weight 'zt 1155, 4 .1c..., .41 .,.. , Iiii ,-;:::!:..t 4, PLUS EAL iv Items part of BasiC Weightl:ut not Weighe .710.1maz,drpkt41,0 141,1,, ,x. r 1.76804 er 1-..feh:i: s * !' I zee d -1 208347 AIRCRAFT BASIC'WEIGHT 1... .iwactipt.i ‘vfa c igro:4.7'31W- reaMinfielillihaAN....td 7, calpett 96278j 930.65 1 38.991 89600897 z. . „.., .1 •..., E, 2 ?.•••7,-.4:...1.: ciSteiNVU.4* .:05b(411740:61 CORRECTIONS W.-:,e1,i6c1 'i 7 MOT Part of . : .. l ei? . ,r.,,,1 Items NOT weighed but not i Basle WekOht r et' Description Weight Arm 'Moment Basic Weight Usable Foal Description Weight Arm • Moment Orelosetlerunnable 7reee•i1 177.0 1001.0 137277 'feel Intim Inlet 0119 --- Ind Tanks 171.0 9111.0 92.0 1100.0 110002 Se$00 27.0 tetra Overige*. 407.0 I I Wien 427 17.0 - 1031.0 ''. 9290 1017 ' eel 14119 Cl) 41 0 On 0 tOTAL. . 188 176804 Total . 264 208347 afriA t... - !...1 ' .1.,4• • ' Itrimoans1 ,4:ii _,,,. fr, -“. ...e..!:...:• ;:: taj :. z.z.:-... 4-n-ii-..vr - i* ,-... - •• r 111.12 • (MI) Olsten fl aw the 319 point to The mole ale centerline 210. 11 a (MI) Dineen* between tie 1•14'nce e sale centerline and the 419 point. 115.05 a (MO) Meters t.t.na the flint nese Salt centerline and the Pa point. 110.90 a (MI) Oletellee free the reference Sam two the Cie point of the aircraft. 960.12 • (A) Ness eau llosalert . A a NOM . 311 • tin ens /ale Mallen e • 111•(42•111)/2 . e r, "-^ lit e; ' -4.E.A.'1‘, ' T' REMARKS e.le.,:'•,....,," - • ras..3 r - . 'Alp..! 0 •:,• • . ,... 1.. The aircraft was weighed in a level attitude and in an • enclosed hanger,. ...c • 2. The wing panel jack point was used for the aircraft Jig point. 3. This is the summation of 'the 3 weighing°. 4. Baseline Weight Results for Post Mod Flight Test, dated 4/18/9D. . . SONY .61.132760003 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0O246925 EFTA01331388 eNr-r••••••Sailrorr",osar cr. SDNY GA4_02760004 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246926 EFTA01331389 *PAL AIRCRAFT REGISTRY CAMERA NO. / N DATE: 8- /5- 90 727 — 100 / 200 Weighing Form Model ri•I Number Place Weighed echniclan /27-100 0115 9505C •ALMDALE FOLEY SCALE TARE NET ARAI MOMENT READING WEIGHT Left Outboard Main . Left Inboard Main • • t Outboa Main ght Inboard 'Main 23378 Subtota (Mains 93329 93336 • 950.12 t• 'urn. Left Nose 1340 Right 'Hose 1497 ubtotal Nose 2837 it 311.37 883357 96166 96173 89563757 tees NOT part of Basic Weis PLUS Ai-44r4,4:-4y teas part of basic Weiat. t not Weighed 0 I RCRAFT BASIC WEIGHT iltriri Tfr.Wirli.332 89563'57 1Atfitlitt-0:74. CORREcTlogg NOT Part of AV Items NOT weighed but Part of Basic Weight Description Weight Basic Weight Arm Moment Descr ption Weight Arm Moment 00.11 • (Ng) Distant* between the left roes axle conterl no mad cm Jig point. gill.•5 • (10) Distince between the right nowe'ons center Ire anti the Jig pint. 530.10 • (II) Distance Ira the referenc datum e to the 31 point of the aircraft. SSO.12 • (a) Mein MU Unction A ADM • 311.371 . (I) mss. Ail. ancessft a • DI-Ottwant WI; .1.REMMUIS %-p- :5-1/ • Rif/ tit$ 11.V.H ' 4 t. The aircraft was weigh ed in a level attitude and in an enclosed hanger. 2. The wing panel Jack point was used for the aircraft jig 3. This is weighing 1 of 3 point. SDNY GM_02760005 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246927 EFTA01331390 r •vass-c-302.-- stseibW. • - - - - — — —• • — 7,4 SDNY GM_0276u006 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246928 EFTA01331391 Wok AIRCRAFT REGISTRY CAMERA NO. 1 N DATE: 8- 15- 80 • SDNY_GM_02780007 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246929 EFTA01331392 sserVilattRWSlagell,behrit--, SDPit_GM -627606CTS SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246930 EFTA01331393 FAA AIRCRAFT REGISTRY AMEBA NO. I DATE: 8- 15- 90 72 7 - 1 00 / 200 • Weighing Form tI.V4 ,x l -C7976 -. 4:4 Dote . Id 8.411•3 Number Place Weighed Technician , 4 18/ 0 - - N505C —\7ALMDALE FOLEY 'REACTIONS .: SCALE 1 ..4 ; TARE NET ARM MOMENT READING ' x ...414 . WEIGHT Left Outboard Main 14401 t .!•4 _ 6 24407 Left Inboard Main 11882 i,1i 2 21864 ° N Right Outboard Main ; 23688 , - -4 23684 Right Inboard Main 23388 23391 5 . h-lt.Ittiitilain;) Se —" . Bait/ 7 93346 a 950.12 88689902 a. . Left Nose 1339 0 1339 . Right Nose 14 0 4 74J . .‘‘ 4:,,I. .: 2, ,., r, Subtotal (Nose 2834 y. 0 2834 5 311.37 882423 r . . t. • ' -• Ars. -s Y• •N, r, A. „, ,t„ n' n3 , .. TOTAL • 96173) eicrila 1 96180 ♦ 931,30 69572324 Lar - 1143,;44:7ghjel: 1441a14 3-4. 4:. ' : 'teas NOT part of Basic Weight o I o PLUS I i. ,T,-.0:44.(26,71”0,2:614-1-4.'...PeOce" tees part of . sic Weight but not Weighed °I ' ' '1--- o AIRCRAFT' BASIC WEI I 96180 031.30 39.35x 89572324 4,7 1:1,t$47: W eTt ..tc:‘ c 7 ,1 .i : .. 2S1 CORRECTIONS .79, .. - ! . .13 'V et' ,1,41”..\ ' 1 ' ' t.t.._W eTt1:3f@te. 14 4.,,rf ". , .• NOT Part , of )5tItrE Items NOT weighed but Part of Swan Weight Basic Weight fleacriplion Weight Arm Moment /Description Weight Arm Moment `,T 1 0 TOTAL . . 1 :41‘14. '''y;.a•. . liEASUREKENTS N r ii est r5 .1l 7.1 II• 42 • OH) Distance trio the JIG point to the thin axle caritorlIne Sg0.11 • (Nl) Distance totroon the left now axle oenterlino and the 34 point. San • PO) Diortarce Mthion the right roes sale centerline and fp, Iii point. SiO.O0 • ell) Distance free the rogiirinico ata to th• 31, point of the etreaft• 960. t2 • IA) Slain ono ...mt••• • . moll 311.37 • (I) ogee Axle wafts . • s 51-012•10)/t Y4i . . ••ier“: /14 ,,,i4 a v REMARKS Li • a -. -k,„c-..... .A.p, ca,$.4-zatargc...4- - 1. The aircraft was weighed in a level attitude and in an enclosed hanger. 2. The wing panel jack point was used for the aircraft jig point. 3. This is weighing 3 of 3 .;•ts SDNY_GM_02760009 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024693 I EFTA01331394 • '‘,^'•"" SDNY GM_027(0010 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246932 EFTA01331395 FAA AIRCRAF REGISTRY CAMERA MO. • DATE: 1- g9 c„,„..,,,,„,,o, WNW PAIALA).. ADALNUTILAIION 4,sfec..,... 04-R060. I MAJOR REPAIR AND ALTERATION FOR FAA USE ONLY (Airframe, Powerplont, Propeller, or Appliance) na l-- '4 e INSTRUCTIONS: Enos or type all snows See FAR USA. MR 4, Appeadin for isstrucnoni end disposition of ebb Eons. ft. and AC 1 5.9-I See subsequent 'TANN Turd) DAME ACM Boeing - . 727-31 I. AIINPAFT Mina . NATIONALITY AND IIKILSTILADCA4 wee NO15 201 N505T NM (As Penn en rogietiOhts tertiRosiNI ADDRESS (As than co sg)serotocs ) T. Orli Tenneco Inc. 16951 J.F. K. Blvd. Houston. TX 77032 I. FOR NA ISE CORY 4. UNIT IDININKATION 5 ITM win no. ALMA NAM mica. AINSILANLE (As thoothod 'NAL I &ANN - - xx powwwa TM ' IT MATING A noeticrs NAME MM ACCESS S. KIND Of AGENCY C. CEIMFICAll NO. us. ONINCALTO ANKANIC . Tenneco Inc. fOltO644 SeenticAsto ANNUM 16951 J.F.K. Blvd. CIONICAIVO WAN AIMION . 205-10 Houston, TX 77032 OINIVPACTUNIt • D. I rosily that as mob and/cte idteretion sae to the NOUN identified in itemising,. and leScribed ea tilt mint er sesebseiencs Nebo base bees bade in istordosee sich at reqsireesmis of Put end ma the informasion furnished herein is tear and 0 of dm US alml Avinko Ilatmatbm (O MR COcbe bes or try knowledge. DATE . SIGNATURE Of ALTIOVED INDNIDUAl 04-04-85 I .110a•- it ,_ -gii i--- 7. WNW FOR El= TQ Silvia 'cumin coo. falforictfiryen. Roos Verified below the snit identified is i..., I As, •••LLA-.....1 A IS. •s..... pin:sr...I the Adoiaistruor of the navel Aviation Ationiantistice end it S. ®APPROVED °RUE( ca) 0.4 Re PASS _ — ofeenfaumet itarealom eimioaranine OM* flow', 06.1001 wog*. Olitattrailid NA INNONN ISM SPOON Or ITarelIOOT litY6C1011 X OF an DATE Of APPROVAL OS CSIMOUE 04 SIGNATURE Of AUTHORIZED INDIVIDUAL DISIONATION NO leKnell - 0‘85 . - 20510 . - ..24ft.... t -re-sr FAA Fens 227 17-671 f 83201 SONY GM 02760011 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10,15, and 17 EFTA_00246933 EFTA01331396 NOTICE Weight and balance or operating limitation dsonges shall be entered in the appropriate aircraft record. Are alteration most be compatible with all previous alterations to assure continued conformity with the applicabli airworthiness requirements. I. DEXRIPTION Of YAM MtOliftISIAD (If more space is required, attach additional sheets. Identify with Mr. craft nationality and registration mark and date work completed.) CREW AREA CHAIR INSTALLATION I. REA0Ved folding.couch from L/H crew compartment station 400. II. Installed (1 each) Tosington 71150M24 F/A AFT facing single chair on sliding rails from station 420 to station 180. ' III. This alteration was completed in accordance with Threshold Engineering Company of San Antonio. TX. drawing 0270 and instructions identified in report 0259. IV. All engineering drawing and reports were drafted and approved on FAA Form 8110-3 by J. A. Dugelby D.E.R. (designation number.SW-256) and are available to the administrator on request. V. All work performed utilizing acceptable methods, techniques, and practices per AC 43.13-1A. VI. Aircraft weight and balance amended, 0 ADOITIONA3 SHEETS ARE ATTACIIO OVi ooroarrain rowingIona rm-rneratom 'Pr • ' • SDNY_GM_C0000i SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246934 EFTA01331397 wax Isamu An teXtu. AriAnON ApoicensinON badsiflett i S. 0.-/OMOI MAJQR REPAIR AND ALTERATION Alcfccone, oseerplool, Propeller, or AppliOthal) , . . INSTRUCTIONS: Pint or sype all entries. See FAR 41.9. VAR 4) APploti D. ANI ACR1-9- 1 Co. 066640mM id•WOO S fi r Seaw:Owss sad disposition of this form. .....,4,0.45, POR FAA USE ONLY OFFICE IDENTIFICATION Nan Boeing • N4(41 . 717.-31 • I. NEM NSW NO.2011 4 .0- NATIONALITY' AND REGISTRATION MARX ...1 ••••• . . . N5051 HARE (As dam en neelereeien esirlattthal •-•-' ADDRESS (As d an negiereeics ceenEctON SIN . TanneCIP Igo • 16951JIMBlvd. • , .Bonston. Texas 77032 • • 3 RR MIZE OKI • ••• ddstsdools• seethes stn. proona SO. aimo$0.• - . . dre.464•••• tollsOsorms .n it .slur! re. Ins as.' encore own soften is etorresily .nt ono:. se oases • 4• • • , ••••••• 664 6 ••• 6- Oa ..• /.2_.r. - Ode - 4. T INIMDCATICel . ? 3. TN MOT ' SOW WO. MTh. MOM • ARAM! (As chiscitod in dee 1 above) II • • PO%VENIANT • . Pal* •• Tine AMAMI MAMPFACWPItt 4. 0NF0UNITWINE A. AMID'S HAMI .110 ADDRESS I. *ND CO A00401 C. °INTRICATE NO. Tenneco Inc u.s. armeicAno asionsiE melon edlirsgANIC 16951 JIM Blvd. Ctema1tp y asiltrUJCIS MACS 11571051 HOoRtoo, Tx. 77032 , 205.14 . OintUfACIVIde D. I certify thee the repels Nadler Abandon .Me re the nairity ideno6ed in k4 4 than sad described es the recant of •Ctoctsimetit. Invite ban bee rode is words< with the reiltdreasems of Pan 4) of dee U.S. reinsil Aciadtha Revelations sad that the lefonnaiise fenisbcd heeds is true and menu to the ben of by kzewledet DATE • • - SIGNATURE Of . reit ' 7. mnv*t FIX unit 70 R1fl Penned to die endeethy_plyea pussies specified Slow the aniigniiiied injele 4 ...Sal .n site mum, rent:bed by she Athelehrthece a/ the Nisi Mission Administration sod ii• APPROVED ORE) IAA Rt.mamba papapapipi 011et Mead NDICIRe, nutheenthen DIMON IIT ' CM4AOMPt NPANIMEM Ow DOOM , . ,Ic OMNI MAD Or lareGoon 0410•00. Of LOCOIT DATE OP APPROVAL OR CERTIFICATE OR SIONAIURE Of AL iltIZEIrrVIII ,...__ MACRON DESIGNATION NO. /.2' ^SO "' /C ,to 4r - re' .41, 2 1 61 SDNY_Gtd_02760013 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246935 EFTA01331398 NOTICE . Weight and balance o• operating limitation changer shall be entered in the appropriate aircraft record. An alteration must be compatible with oil previous alterations to assure continued conformity with the applicable airworthiness toquitamenti. I. WAMITION Of WORK WONKIER° (If more spore is required, clinch additional sheets. croft nationality and registration mark and date work completed.) INSTALLATION ASINC, INC. AIRSEOW 100 SYSTEM I. Mounted T.T.G. (Tine to go) Preset Unit forwaid of center console, below existing Radar Indicator. (.50 @ Sta 210) IL Mounted Rotary Selector Switch above existing T.V. Monitor. (.050 Sta 808) /II. Mounted Remote Video Relay. Switch on shelf behind T.V. Monitor, game cabinet. (.5° @ Sta 820) N. Mounted D.I.U. (Digital Interface Unit) with suppliers rack on shelf adjacent to ATC-1 Transponder in A 6 E Bey, R/Ii Side. (80 @ Ste 463) V. Iostalled 2 amp Elixon CB on-forward end of 02'Essential Radio Bus CB.Panel, Left sideofcockpit. (Ste 26)) . Installed wiring and associated hardware, connectors, etc. (4i @ Sta 640) Complete system installed, tested, and operationally checked, in accordance with the manufacturers manual 0910600, Tenneco Inc. Interface Wiring Diagram - 011586 and acceptable methods, techniques, and practices per AC 43.13-1A Chapter 5, Chapter 11 Sections 2 thru 7, Chapter 15, AC 43.13-2A Chapters 1 and 2. SDNY_GM 02760014 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246936 EFTA01331399 • FAA A /RCRAF REGISTRY„ CAMERA MO. DATE: '1 Ale AC Li WAAL( A AD4s Deu VI OArrOAVA4 • 0~51 PEE Oat LO5 el*/ SPA Min. O Cassie Ala Pik alle 30:10* t.TirrAko v.. vine AS RfY at; Of Is ALL *MO. 'GDP's: aft' .5 Sijii.t1/4 5 • • • -7b 600~ atone it On astuf. A .1wriyeregana nt Offur PM 21 &ND AND Pee . SO OPaW rilLOS WO Dalai. 0.5.0 MO: e...0 O454.4F. Peiv2 .9 OPEN AND ~30 OnirdAr: pant on* AND 0.3 sc. ~se atreteartS Peat *MD AND Per 30 &vs ORD< IMO 0.5Ft•r. loom Tut Ire sat Aaiun taeCn ia pL re0 Comikrrue . a der car Mr Awe AA Ayr as ass ow wet teem- ourra~ or min• tee matt sureue mar sr or ~en Ines) zee." 5.~.4. ~rw Inal. son air • an xi Te BATA tor sr rt Tna TecTo Sale ad sari taraca e are sP•7 Noe to' am ram TIT ~ern Dr an. 4.~.4 man arse ser earrassor on/ AO et awe of ~Psi Assis r corla wart rave err • on: Wine< Meta earne terna r sasnase wane me nauti r0. •LrIrta art Arne "too FRON Anon ar Ats.< ^Ws: fa air leartse ~Er • rot r0 ow 0, rnat reeler ar -Zei arawa -As to pis if. art,- q TO eve o Asia Na Abs ar It well let ~TM Q AS as« • fait ilea 0, Oar COOKTUD. at omir Lr ONO, 540.5 OW at DIgio '" ADS NOT ~D. Iv at in Witt • IOC Pe At M. 107). .2 erne Ana L Sc ecrelcrE0 w ~matt awe mower ~NO Marrs. St went ~Cc SWAPr —we ~re* are AtearAWN erararr. senora. tatPar: a Ail NeD050 allE• r0 save ne SC 5~0 TO amsterot rent ~on N ~nee $00 Am racy ne. pas. eralijat;r00, ~rap a s de oral or cos wordreAX Jaffa ;sire fa areake al Arta) an AMR ~Or. ()ann. 0, ~ tarn Mts.** Nairn ArnateralepeNt IntariCO, eakretrOA rasa M CdraterSi 1 a a 4/14/E i.e sanStrnterSserir ITOCt-s-tt af0011 • PS orierOCS••••S itrant lar ltE31240.10-OP rl.teNyK CaS017 311' IISISEEINI - iel , au« MD A f-Toie Pa V51.1•41” normra 77.318% to sumo »WC waste m .16 i;•tbid it* GRAPHS 7, 8, 9, 10, 15, and 17 SDitY_GM_Oc0015 SUBJECT TO PROTECTIVE ORDER PARA EFTA_00246937 EFTA01331400 . f 7.zt0,flarllnfWrrgffnwEaw-n - - r•rgfitaa,--.-L--t ---A-marec4s --- rn\o CUM= SDNY_GM_02760016 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246938 EFTA01331401 ocu R •ASC 1fanS are ateA 1PI 9100 X A Aso CoCo Inaba o v oC wow AY t AL Min OW Cali.,INflan Airt • CL IMM OC • OWN at *CAI LOA • %Ours cola your - '-4 Pat 05.• • Oil • Sale O V. a tint ICI 00a 414 dr R•N --- "inPai • its an OAR Sete K IS !Iran, so Vino 4,4040 WU. sr: Rea la 4 off tan. M 0744 III AL L *rant Posinnfr: An/ StAIREIC IOC.* -fi g Ilalotriata CIl CO lb RIMY ful, nee Woof et ow eas A antra RN 2 11 Gab AIM totestalla De P.W an. SO *KW MLitt Me tolfriAt 0.4/0 naps Soo cc Po o Awn Peen one AND egttAireS O Atm 00 Oaf?' Alt 2 pv.tv WtM AII CND MOS OW 042 0•2 non ONO are* Pa* SO tar ere s ANM Nµ ewe; Po ne 22. cam ewes MM CM "Ilista•901. A Coatz7 70 No m' A so us& MI 3•4ee ••••011• AS ?NW OW SOL -ewec ep fan d xenon ge sun espy, ear arc on ree . nal lits•P1100 ottete 3.4tuant CS mo na :eye as priait•P•manl !Ono ' a Fs. in • Mn T an tar Sr an vs Sas., ea / f+ et. EIONI14) miser Lase S tee a atark /*newt a• steer ~Os Oat Oat le Rat solP0114.9.01 mostea• seer Oral scan moon -04 Wa wa OE sea r its we AMC et V/MO O< "OD OM ~one lafe ellip• AWL: a/M Ramer teetli arillet ~ors Act teli C. le MAC en eater Ma n AO Dien° oneet• Meer ~Nat A en erect latrit Al-ZOL [Mare 0 AAR Rraaa. As-417 MM; to PiN27. • fRIA- el 10 pre Ir eta Oat 0•OTAt •03 avOur.0 •C & at fl at , war 0. Pt ••••• Cat St VIC O MO tert Oa It Oat CO ADS net Oslo. [We It nor 24. ''SV at Ins 01 1101 11 2 WIR E MD t nano OA OW, iaf. .0.0t r We ise at Oast 1212 r AaavA Ana .0vrAo att er MO M. wont pan[ a Arab <yore* Cow alairt awl ftwante Otk la tarro await aga 000 nen TO awe ora reetat arta Ml Wi 142020•0 10 Joittat IV at tee Oa Osir At Act20.• WO COS. toe Asswerfe erefOt SAC a , At .L.V0 At ala eam IATD tof f ~M O St a•P oat we /am I ay Ana ae t wet). on otror reair (treat n :Pawn Sr ronteteracoo t2 tOtaellta 12.2 mac Ave I oderimpre Orr efe/Prei rte lt fl ea. cO IN WINVeattlatao West rnpooe-n ZIA coroctear Glatt • 2F.10-a0 SPI JaSSIR 44,10-411 44. 1017 t• 091 11/ 32: lentitl-Na 6t5018 Svc awe Aro 'PE 01$4.50 IV= I 020•1101,120 m MIS Ca 94110 atoll /M041) INITIT0NMECT WIRINGOCU MRSNOW 100 WI TH het CarAfW14) , a76n00d17 17 • RA G RA PH S 7, 8 , 9, 1SO0NY, 1W5.02 ECTIVE OR DER PA SUBJECT TO PROT ERA_ 00246910 EFTA01331402 AA AIRCRAFTliEG CRY NO. DATE: 11-; ,;?..a re la ilir_ipt...„ • • waren or ItoiSPONIAIXM r..... PM DAL AVIATION ADMACillATION liageotress j No. 04-A040.i ' POI FAA USE ONLY MAJOR REPAIR AND ALTERATION OFFILEAo7Fa cts (Airframe, Ponplant, Propeller, or ApplIona) INSTRUC11ONS: PAM or lone aLl 0:0 4. Se• PAR O.S. PAR 0 Aprodis B. ad AC 0.9-I (se 0040404401.0 ' for lartroctIoo• 04 dispesidon of this form. AfflAff MOOR I. UMW 80F ior. 727-31 SERIAL NO. . NATIONALITY AND INGISTPATION MARK mils LISA NSOST NAME (Ar elan • r5 nolisfrallo onthlaslo) ADDRESS (As Ian es 0,10•04 cortio040 L HIM ' 16951'0.F.K. Blvd. MINIM INC Houston: TX 77032, , 3. r rot ma us iv II arm tti-"Y'''''" ob.. 4000 filli a n ". : 7 / 410, IS 4, IIIIIT IKAWKATIDII. ' S ITN WM SRA ' WM MO. • um. sA01. AMNIA (Al 4100401; the I obsool /I POWEIMANT t." • .1 a 11040101 C. INY aw00404444 ' • train'? STAMM • A. AOINCIII NASA MO WPM S. ILAID OP AGENCY C. COMPICAR NO. G. C. Kolb .... ClitTleICATID 01101•10C Tenneco Inc. IONS. OPHIMATIM ilOODISC 16951 J.F.K. Blvd. X 'KATI. SSA ITISTION 205-10 Haus top TX 77n12 OAMVPM01.1.11 D. Ian* Sat Si npoir 401/or alarbrisa aka* so Go .0(.) Idesdiod is In 4 Abe. 041 40001 0 Sc Mono sr ottodumean Mato bon bon sea S 40000 rib cb• rogoinarso of P.m 0 0 Si U.S. Poderal AnI408 P.040604 W AN 0 isforambra fanaod leas la O4 ad own= to S. bon of ay konflodis DATE SIGNATURE OP AUTNOVIEI) INDIVIDUAL December 21. 1984 — il t - d 4_ 1- r ''' Y. mtak g I TO HMI ' Preset to S. 0thaley bins p.04 opecihd bola b ooll Icbrodird la In 4 04.Mosel Is de noon pros:00 by Jr Adaakalscrotoe d 0 ISM ANNiss AAsbasomiso and /a CLUJRAPP/OVID Ore ..- - 1,4410. ITOADAIN ,,,w,...novo. IMPKI104•10102.00.1 ~ IOW IT 0004. bratalscr 44.4 40404 ✓Rea gum« X 01 MANPOIT ~COS 01 MOPS DATE OP APPROYM 011 CERTIFICATE ce SONATUAI OP WHOM= INDOODUAL ItLIECITON DEMONATON NO A2C- ...7 / /f e n eRe-SM .1 41 ...4e1.• -4 _Z....air — MA FOND 337 (' -on 11320) SDNY_GM_02760018 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246940 EFTA01331403 NOTICE Weight and balance or opwatin limitation changes shall beaten(' fro the appropriete okay* record. An Stratton must be compatible with all proviow alterations to can contlemed cortformity with the applicable ainvorthMost romtkonwmte a. OeiCietTION Of wets wows (If man space it required, attach ecklitiliald sheets. identify with ob. croft nationality and niplitmlion mark mid date wan centplohodl TRASH COMPACTOR Removed Thenaador Trash Compactor P/N THC-288 S/N 3060438, Having i AMP load. approved on 337 dated 9/19/83. . • Installed Montgomery Ward Trash -Compactor P/N SBW-5235=c S/t1, 48H;00442.. " - Having 10 AMP Load. • • Unit function tested satisfactoiily:. onit operation does not adversely affect thi safe operation of the aircraft. Installation was same as previously approvet on-NSOST 4/01/81 for - - Airesearch Aviation Co. ,'Los Angeles; CA. (See previous weight and Balance Data Report fC-3688.1 . _ Installation using acceptable methods, techhiques, and .practices in accor- dance with AC43-13-1A Chapter 11, and Chapter 13. Weight and Balance and Equipment List Revised. • 410.....) .2ni aiZnyt-F . • • - . • •• val styli. >, lc.?It • •2 ,.• , " • • SDNY GM 02760018 -- SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024694 I EFTA01331404 , nA AIRCRAFT ILE TRY rERA NO. DATE: _55 44•TAMPIetreme— 'SG • • i I *4 OigitroAr.n 0, n....0•Onieror Fso• Mensal ' MA AvIATCN acmumunmnOm Ihst niters Na 04-1t000.1 ., . FOR FAA USE ONLY MAJOR REPAIR AND ALTERATION r, (Alefromt (Alrhama, Powplont, or Propellor, or Appliance) .Sr Z - INSTIRUCTIONS: Pint or type di 'rotten See FAR e5.9. EAR 45 Append.. B. sad AC 4RP-I Or roboloror EniA40 atiater5 for InsanEtiostli sad disposition or shit form MARE I. AWAIT Boeing 727-31. VENAL NO. NATIONAL= AND tEGISITIATION WAR 20115 , 11303T NAME (A. than., on topithelion ortigosio) ADDIESS (As Am. co nryipPrefien aseraxon t M O , Tenneco Inc. 16951 J.F.K. Blvd. Houston. TX 77032 1. EON OA ESE 10 T promoOmOmmoomboomMi etsmoste Rd hi Odds, idol NNW te Seat e te I 1 /04. - - 4. LIPIT gelltWATIMI S. ries — AM. mum ems - moo AIURAME - ••••••••••••••••••••••Th Llowilod in Rs I Son/ • • xx POWEIWOUR I ) • ": i Ns I • t . • *NUANCE V auciPACMIllt • ' 6, Pstassor SATES! . A. AGOCT'S NAME ASP WOOS I END a C. CERIWICATI NO. vs. 011WICAITO NOUJOIC Tenneco Inc. SIMON 011tielC4RO IGNOWIC . . ... . 16951 J.F.K. Bled. x ctenocao Worn 51411000 Houston, TX 77032 , '205-10 D. I eenify dm the tepele sod/or dorreties alt to de smalls) Idestilled la Se I sten sod deserted es the mane es ; ettacheseste buds here heat sok la nteedeoce with the reisirestses of Pen 0 dew U.S. AWN Av.isthas Regslettes tel due dr befonseake Finished, herds b use sod managed, bomM.rkawledge. DATE 8/3/84 . . P. 1/PORTAL PM IMMO TO a Pumas to dr mask, re* bora walled twin the *rah &NSW is hen 4 m imed l• the sat pesseelbed by de Meisimmem dale tempi Addles Adatlettstba sad Is ®APPROVED OM TaiRtniNNIS4 - aviumfluma RN1Pr AIRMONZARON . . ... . Cel.1.'49 -.. hY . COODOM OITAIMIIINI no mem y ON maim OF TIMPOIFF •OFICTOI 06 anin DATE a APPItt7VAL 04 mown OR EIGNATU a . 2.- 2 y DEUGNATION NO Athr•/ 0 .... O,O1_ (1320) fry "re- /no 719/ 57 • . • i. SDNY_GM_02760020 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246942 EFTA01331405 NOTICE Weight and bolanc• or operating limitation changes thrill be ordered in the appropriate aircraft record; An alteration must be compatible with all previous alterations to assure continued conformity with the applicable ainnirthinois rapiirefwants. a. 0601IfTI011 Of eilltACCOWtI9II0 (If more space is requked, attach addit(onal sheets. Identify with air• craft nationality and registration mark and date work completed.) • \ ' VIDEO PONITOR AND VCR'INSTALLATION ‘.. I. Revised interior (which was previously installed and /*wowed by Airesearth' Aviation Co.. Los Angeles, CA 4/7/81 on report No..0-3688) as follows: . A. Modified coat closet (R/H side Ste. 814,5) to receive.mounts for installation of the following: • •-- 1... Viiies. Recorder - Mitsubishi NS-33OUR Monitor. -"Mitsubishi -'Mitsubishi, CM-1901 3. Infra-Red Transmitter - Nady 1RT-200 4. Altitude Cut-Out Switch - Asinc 90500 S. 'Poiei Receptacle : 7777K1 . . • 6. Power Supply AC-DC Adaptor--. Nady.LA-2420 II. Modification of coat closet in accordance with Structural Substantiation Report No. 243 and Drawing No. 266. -submitted and approved.on FAA form 8110-3 by J. A. Dugelby, D.E.R.:, Threshold Engineering .Company, San Antonio, TX. Reports and drawings are available to the Administrator on request. III. Power Supply as follows: A. 28V DC Bus No. 1.(Drain Valve. Shower 3 amp CB, existing). B. 115V AC 60Hz (Utility Outlets Aft Cabin - 15 amp CB, existing). IV. Utilized existing Altec 755E Speakers at.Sta. 2730.0 Systems installation is in accordance with.Tenneio Inc. Drawing '1505T Vides. System" dated 7/26/84. . VI. All work performed utilizing acceptable methods, techniques, and practices per AC 43.13-1A, Chpt.1S and AC 43.13,2A Chirta..1.16.2. . VII-. - Installation was functionally tested at ground level and at altitude during performance check flight,ailtd operated satisfactorily anctdid not adversly affect the operation of any Other:systems. VIII. Aircraft weighed. lieighttand Balance and.Equipment list amended. . • . Ai! 51.111016411111Ctr...rr. soW:5Proffeedi SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246943 EFTA01331406 A LAitatie IIX - Affro4.1 NOAL IAIION ADIAPOSIRMION 4 Rare Iona No. Ro-R06o.1 ' MAJOR REPAIR AND ALTERATION , FOR FAA USF ONLY (Airframe, FernyleM, Propellor, et Appliance' MinTs) .4 . N INSTRUCT OM: Past et e ell treks See FAR 4)1, FAR 45 Appendlea sad AC 4)1-I (oe adnemet enlace thereat) foe inuttatiens sad dineliM of Ws Ma. MAKE MOIL I. MEM Boeing 727-31 SERIAL NO. ' NAI/ONAUIY AND REOISTRATION AtAAR 20115 N50ST NAME ft Min al etitideedIta aehlad•J ' ADOUSS (As "0" , " ni***frotio` chrteratO I. OM 16951 J.F.K. Blvd. — Tenneco Inc. Houston, TX 77032 ' I. IN Mt LISE MI I VSE MMO I. T martuicino• .• -we ,Maw W. I 11TE "AM MICK ANISSAIN (As thienbal In Ass I am) XX POVitelAlif • PlOPELIS an AMINNQ esnivacrese 6. COPOUllY SWUM ' A. MOO'S NAM MC WAS 4.: ONO Of 'AGENCY C. came. TE NO. US. teenacsiee tesoud4 Tenneco Inc. POW" CIRMICANO lOGIANC 1695! J.F.K. Blvd. . , i : r. X awls am sus,... . . .... Houston, TX 77032' ..205-10- *e a " D. I amity late the Nee eadtac skiesdia jai. se tn. ato 44444444 istscleamt nor ism 4 flow* abl dsicribel " "4 tern.. w bias to Is atatedsaag widt ;is sequined., i.hn W thee on laStemlas ahlefehed herelads rt. sed awns th the,bes of 4) atiSs US Metal Ashdod Itagadetioao o w keewledo. • DAR • SIONATUNE Of ADRM 8/3/84 . 7, HNCWA EN NMI TO WM I Forma to dui *shaft Sara Ent veiled Idea she wok Idessifild is Im 4 ensit... a. Adadeitenses a( dr Masi Avionics Adtaisheradea ad I. MAPPROVID RIU Smaid lathes/me p.__ 5-d sr mileICICalA4MOWAntill SY. HA ODOM • 1 ass DAMON a MAKIN especial a SWMI DATE OF APPROVALpe.. CERORCATE Olt SEONATIAIA .711 _ IITTIOttAl IWO* . • oisiosnnom le 8/3/84 • 205-10 . FAA Fenn 337 tr-on (or) ose% coolecoeMpapj,_ SDNY_GM_02760022 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246944 EFTA01331407 NOTICE • Weight and balance or operating limitation changes shrill be entered in thnoppropriot• aircraft record. An alteration must be compatible with oil previoui.altetertions to 'assure continued conformity with the applicable airworthiness requirement.. I. &sonnies OF WOOS WOIMISKED (if more space is required attach ad:linen& sheen. Identify with *e- ach nationality and registration mark.ond dare work completed.) BODY STATION 950 BUL31EAD FORGING REPAIR Repaired left and right BS 950 forging, lower section, in accordance with instructions provided by Threshold .Engineering Company of San Antonio, TX. Subject instructions are identified in reports No. 242 and No. 244. Reports were drafted and approved on FM form 8110-3 by J. A. Dugelby, D.E.R., and are available to the Administrator on request. II. All.work Performed utilizing acceptable methods; techniques, and practices per AC 43.13-1A. . , III. Aircraft weighed.. Weight and Balance amended. • SDI•he_Ghi:62760013 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246945 EFTA01331408 ( 1Litat a IMMPOILIOCIPI ip eat". !Wes FOSNIa AvIA110.4 PaNNISMArkis =t i lt 04-1040.1 FOR FAA USE ONLY MAJOR REPAIR AND ALTERATION aF %Mrm mom l y (Airframe, Power/dont Propellor, co Appliance) o.--,-Zi INSTRUCTIONS, Pith( or type all tomes. Set FAR 41.9, FAR 43 Appta R.FM AC 41.9-I !Or itibitiveat reviaoryboreal) for inirrupions end disposition of tale form. MARE Alolle I. MME( Boeing 727:31. ' MAL NO. 14.411001AUIV AND REOISMATIOS MARK 20115 U.S.A. - HSOST N (As chum a. tegutrolnu arhAcx.0 AMISS (Pa Ara on InainaNen arrSoste) • 1. MOO Tenneco Inc. 16951 J.F.K. Blvd. Houston. TX 77032 3. NI HA ME 0IRY . : NI An Alme leilate0 05 Sr= ., ri ty, • moinoms we iii earn doh VW " thIrper Yr swim* jos fa r ..3, ... ,,.. :417 1 . ± . 7 6fo IOBRIfIGTIOU 5 TM moan *MP IMe • . (As denoted A Oa I Sem) X rRGFeIa FM - - 4- Wain Rumen A. AOSPICY1 NMI AND ADM'S l i.e Of AGENCY C. COMPICATI MO. Y. csaintheth maths • Tenneco tne. aeon annum ran 16951 J.F:.K. Blvd. X a enfant* nimal naiad. VJ5-10 . Houston, TA 77032 .a.wec,vs D. I candy that the ether, endthe abandon mode to the maitre) identified is ices 4 above and thin-rhea on the isnot e. attlIdiatill, lento hate Inn nude in ancotersot with i.e rethunthente f Panne( the VA Federal Avarice thytheions and dal the kifensetios banished betels Is tin s d comet to the best of my keewledge. DAR SIGNA11,1 Of AUDIOUZLO DIOMDUAL 7/19/841 _s r& - GF -- .,2.7L1 X NN0VAL Mit MUIR to DM As. sun to tie thrborig plyt . pence 'flair., below she snit idnuifwel in then 4 oasianed in the saes pthArlbal by the Adsiaisaster al she Aide& Finials ArbeItheauloo mad a r ' ROVED RF/DCTID ens RIAlortheADI fleipanom . One Mean winthatini ANICIELthithi 06111001 ST ta• Mae . X en stars Or Tian IMPICEIN Of INDen DATE OF APPROVAL OR annexe toe srauavet OF AUTHORIZED INDIVIDUAL . REJECTIOrl DISIONATION Pa SDNY_OM_02760024 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246946 EFTA01331409 RCRAFf REG NO. DATE; -Ys. gab NOTICE k •I Weight and balance or operaing limitation changes shall be entered in the onroarialo Oit a aft "On /. An alteration must be compatible with all previous alterations to ouure continued conformity with the applkable airworthiness requirements 8. 88$88181108 08108/ 8880IMIUE0 (If men space is required, anode additional sheets. Identify with air crab nationality and registration mark and dare work completed.) • INSTALLATION OF US VOLT SOCKET A HAND VACUUM VITA CHARGER RASE • '1. Installed 1 each Cutler.- Hammer aircraft electric safety socket P/N/7777-Kl An rear closet. left hand side. station 1137. Wired new f0t0-1010Prillig 75/115Ivolt AC supply from utility plug in vanity. II. The safety socket incorporates a switch, which connects the supply to the .vacuum.batterYcharger when the charger plug is inserted in the socket, and As protected by a 250-PIA:fuse. , . III. Installed.( follcnving placard adjacent to safety socket. i IMO (Mal (U &IR WILL VACUUM CLEANER CHARGER ONLY 0.1.11•0“*.• ...u.,..• I Ian I® L air AM OS isaiiinoierie osaattilloba scs. a . w.,a Whicialni....0diliblia 010..elistWealifij.ilto••4 an , * t . "" •• • : Added Electrical -Plug P/N 7777-K1 .. • • -V . . Lou. IV. Instilled 1 each Black E Dicker cordless vacuum cleaner w th battery charger base P/N 680982-00. This.unit is Underwriters Laboratories approved and has the following specifications: 120 volts 60HZ. 5 watts! 7.2 Y.D.C., 125 MA. The total voltage draw fran'the,power supply will be approxinmtely 1.06MA. . . • . V. The charger base is mounted adjacent to the electrical outlet at station 1137 and attached using AN526-8-32 screws, AN970-3 large area washers and AN305-8-32 fiber,lock nuts. .- . • VI. Weighi 6 Balance and Equipeent List amended. 0 ADOMONAL miens AI2 AltU)*D Aruaamtn.mm neser000 010.4X, Istr..vricrinve r• ' • SDNY_GM_02760025 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246947 EFTA01331410 . I Peer Apposord . HOLMAVei.L.S7ti Ari.nitIMATiOnt (4. I Blidiff IMMos 114..01—S060.1 FOR FAA WE OEM). MAJOR REPAIR AND ALTERATION OP PION (Airborne, Powerplont, Propellor, of Appllona) at.° .5" INSTRUCTIONS: Print or sr crt all write. See PAR 4).9. PAR 4) Aireellz Et Rad AC4).9 toe tartan; /critics. thaw° tot instruction, and ditpotioion of tins loan. MARE MOOR I. MIKRAFT BOEING .727-31 SERIAL NO. . NADONAUTY .. AND REGISTRATION MARK 20115 • IAA N5057 MAME (As thou, on regat.telen toctilicolt) - ADDRESS (As Amm on vs.i**E4n NA/ ) . 7. OWNER ' - 16951 J.F.K. BLVD. TENNECO INC. - . .HOUSTON. TEXAS 77032 I. IN ILA USE OIRT 4 WRIT (NIINFILITIOI S. TIN Limn wJ. AOPII, fetal NA AIRFRAME (As deleted ?nit'''. I °boa) . . pOWEISLANT PROPELLER Net APPLIANCE MAAAIIICIVIIII •• 4. YiMFOtRITT STATEMENT — • A. AGSM NAME NO MOMS E. IND CO AGENCY C. CERTIREAlt NO. G. C. Kolb /•• • . . X. US. ;unman* SIC 84 Tenneco Inc. i MUSA fitrIOICATIO AlltitutC ) --A:+ p 16951 J.F.K. Blvd. - Milan° MAI* ittalOiti 1337480 HoOston Texas • 77032 ' • • D. I :men& ant the gnat Andire Altern/ion Int to 'be nista) identified in item 4 shove sad encelbei ea ige tt eerie i.e easchattou Irmo In. beim made in tctotente skit the replier/neat of Part 0 Lal the U.S. Federal Aviation Rigelatians and dm the afeasaital furnished herein Li Ira and COMO 10 the bat ,N m7 inesledge. -- DATE . WINANS( Of ANNORIZED IIVM94 AI • • September 19 1983 •-.. 7 NNOVAI. FOR MVO TO SEIM Ratan to the auctiorks ens person. ilpeeilletl Wow: the snit yEentifted la Item 4 was Inspectedio the manner piarribed bY the Adminittatoe of the Federal Avignon Adalaistrasion nod Is EA APPROVED IDREJEC1 IAA FM somas - ;,,,,,i,Acuit e" am,o.e lo. . ... -... . ...-... . •... .. . .... . IIE CAHADADe Offlambee • • /AA Dellic•Ill I Emu LIM or PLANSIOIll IIISPOCION . . 01 AlhOLOT -L DATE Of APPROVAL OR CERTIFICATE 02 L. SIGNATINE•.OF. AUTHORIZED . DUAL REEKTION DESIGNAION NO • September 19, 193•3 IA 1337480 SDNY_Ght02760026 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246948 EFTA01331411 • NOTICE H .•• . Weight and balance or operating limiteice, Changes shall be entered in the appropriate oiraaft record. An alterotian must be compatible with all previous alterations To casaba continued conforinity with the applicable airworthiness requirements. ' B. OESCIIIITION OF WOOK•ACCOMPLIS14E0 (If mote space is required, attach, additional sheets.: Identity with air- craft nationality and registration mark and date work completed.) , I. Removed Montgomery Ward Trash Compactor P/N SSW-5621A S/N 08D-00489. Having 10 NIP Lead. ' II. Installed Thermador Trash' DompactSr P/N THC:2811 S/N 306043,3:Waving 6 AMP _ load .sere location Dnit'fjnetion tested satisfactorily;, unit operation.does not adversely affect the safe operation of •.the aircraft. IV. Installation was replacement Of'nnit previdusly approved 4-07-81 for Airesearch Aviation Co., Los'Angeles, Ca. (See previous weight and Balance 'Data Report IC-3688.) V. Installation using acceptable methods. techniques, and,practices in accor- dance with AC43-13-1A'Chapter 11, and Chapter 13. • VI. Weight and Balance and Equipment List Revised. ADOMOKAL SHUTS AU AffAOOD SDNY_GAA_02760027 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246949 EFTA01331412 DATE: q-aa-Ys FID(* Of UM Iota 30.11044 ADANDYIATIOS Form Anent, Bordin Berra PAL 04-R060.1 FOR FAA USE ONLY MAJOR REPAIR AND ALTERATION OFFICE IDENTIFICATION (Airframe, Powerplant, Propeller, or Appliance) • gi••-"le rso acts INSTRUCTIONS: Print or 'Tin all entries. Ste FAR 41.9. FAR 4) AOpen.3.• R. and AC 43.9 I (or subonotot revlolOod.44030 . lot instrunions and dopotiLion of this for.. . I. AMOJIT "«1R1 sax°. • Im" , , 72741 NATIONALITY AND RICIRAOtt . AWE U.S.A. $ NAME (A, thoo, on Mr frelf 'CO OMtilted. i Man i gt :him: 11 ;rubel ...dodo) . E OMER Ta ws. lac. liessas. Was 71215 J. Mt fL4 USE QRtr IIIIIIVIDMIll S. TYR ' MAW. HO. /S A ' ATM* • . reidasenbee in es:. I obewrioNowirgrainitentoor• I PeDIfl16 •• me . • • AFfl ANCE ROT Slane A. AGINCY'S HMV AND ARMES a Ep10 pr AORNOI „ ...ari E.MATE NO. AiressardiAirtatIss Cs. • 0... NIR4tlo ainClunIC '. NC CLARA 2.3.4 ALSO Donald Desslas Or. . . ... t eon FITOKARD AtCAASIC. NADIO CLASS i.vs Lai Such. CA 90610 - .. , GUTMAN, SMIll SIMON tomirEciINSTRUMENT ramillACTIONS SPECUI.LIZED SERVICE D. I certify ace slo ...fat andiew alteraeloa made io DO eiols) identified ia keen 4 above sod described on do sem w sttlicitacnit hereto have ben made in roccodasee with rt. teluieroseats of Part 45 of the US. Aviation Revelations Federal end dun the alocifeciao feraiased Main It owe and correct to the bat of ay itrowlasi. ' DAN . . OF A RUM AM I 7 1981. .— • . r • • I. APPIMYAl RIM TD Urea - . Po- osint to the ovisaky Pin renews mailed below, the .at eristified in ittos 4 was iaansped fa them 0Af bF ate Adadoiserma of the Rees /Mean Athaniteravioo lad is APPROVED Rffl . .• .. Pm At. Ism iDASEd - • 5' • Otte Ras% • . is.Yepatmagn INIONTICAINSICINIMIOM • POROCA ey sr tder - • IAA 01/.0.1 I lona PATEM C• TW.IAZAT 04101CIOt ..- L. - So o ) Of SL DAN Of APPROVAL OR CEMPICATE OR- b LURE AUT DUAL litleCTIPIPR i 7 1981 cur mo E. It. \filetst FAA Fenn 337 17-tn .• SDNY_GM_02760028 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00246950 EFTA01331413 tiOTICE Weight and balance or operating limitation chanter shall be entered in the appropriate aircraft record. An alteration must be compatible with oil previous alterations to assure continued conformity with the applicable airworthineu requirement's. I. OFS(IIIPTION OF WM ea011itISHEO (IF more space is required, attach additional sheets. Identify with on,. croft nationality and registration mark and dote work completed.) Installation of Dual Delco Carousel IVA Inertial.AaVigation System in k• --accordance with STC SA4164VE, emeendment dated April 16, 1981 to include . 727-31 model. Flight manual Supplement.issued detedAPril 16. 1981. , It has been determined that the interreletionShiP between these changes and any other previously approved modifications will not adversely effect the airworthiness of. this aircraft. Aircraft has been weighed. iieight and balance and equipment list revised. ..The end. • MORIONAL WES OE MIAOW),O .sae a-- SDNY_GAA_02760029 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024695 I EFTA01331414 Orr OP lepeassMatt* IWO VitlAtiOes nOtitiallbstiOns 2,— i ,,,,resca No. 04-It060-I . MAJOR REPAIR AND ALTERATION FOR FAA USE ONLY • (Airframe, Powerplont, Propellor, or Appliance) cola IDENTIFICATION t .1—F 5 00 —by INSTRUCTIONS: Prat or type ell mann for lanettaions and disposition of this faro. See MP 45.9. FARO Appredi• B. and AC4)9 i pie orbaeReent raisins then) MARE MOOR I. MOM Boeing 7r-31 SOMA NO. NATION/1ln AND REGISTIADON MARK 20116 USA N505T Huge (M show. on apititelion nooSameI ADDRESS (Ai dine at niptinlhopa comeose) 2. 01111 " ••• •• • 16951 JFK Blvd. Tenneco. Inc HoUston. Texas '77205 3 Ha 4. 4 ll ICIWITKATI0N 5 THE noon MIA\ no. MOON APAPPJJEt (As de abed' I &rye) x POValtPIANT PROPELLER fin APPLIANCE WPM 4. !IMAM PAIDIBTI A. AGENCY'S NAME AND ARGUS! P. SIC OP AGENCY C. C ITIPICAN NO. C. C. COLE X h aresstro asatArate Tenneco, Inc. late. CATOICAITO INIIOWCIC 16951 JFK Blvd. COMIKARO NMI staleis Houston, Texas 77205 puunixanun 205-1 D. I tend, this the reps,. andare obsession male to the kindlier) ha in nItts) 4 above sod described o. de senate or rancher.. hereto have ban mph in accordion with the roninamets of Pen 43 of the U.S hdetal Aektion god that the snionnstiOa fanistsed herein Is the and omen tetaletien to the best of my kenledr. DATE SIGNATURE Of INDIVIDUAL 4-22-81 A xa I. IMO AL f0RW lama Po stoat to the noikaily jinn persons *pacified below the NMI Mr/1MS io Ise 4 wasimud athe sumer pearcnbed by Ow Adainistrathe of the Navel Aetna. restos tad I. I: ROVED M anti Ore am* POPICIO• NAIOJeAcsuses menrnonallOOMMIOM /T • WAX, t4OPPOtet fl ea IITOCIPI OP MANS•047 IMMICI011 OP AdDleit DATE OF APPTIOVAl Ot CIVIRCATE OR WHAM! Of AWN IUD INDIVIDUAL It NOON DESIGNATION NO Q / ' • '4-24-81 1337480 ' IbC FAA Form.337 17-411 . • • \ • • StaM_02760030- SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246952 EFTA01331415 NOTICE Weight and balance or opina limitation changes shall be entered the appropriate aircraft record. An alteration most be compatible with oll previous alterations to assure continued conformity with the applicable airworthiness requirements. . I. DESMITION Of fl ! ACCOMPLISH° (If more space is required, attach additions/ sheet. 'Identify with air- craft nationality and registration mark and date work completed.) Grimes Supplementary Lighting System installed on wing tips.. Installation was in accordance with shop oration. per AC43.13-1A Chapter S. Set. 1, and Chater 6, Para. 48 and 249; Chapter 7, Sec. 1, Chapter 11, Sec. 1-2-3-4-5-7; Mfgs. cifications; and Alresearch Aviation Co. Drawings /1359002'A" ( ical) and #1783009 "NC' (Electrical). System was functionally checked and operation was nonnal. Weight and Balance and Equipment List revised. •••••-•••• • SDNY GM 02766651 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246953 EFTA01331416 AA AIRCRAFT RETRY NO. DATE: ii -A? _ZS --.••••••••••• • ' 57r 4, Of••••••2•11 /141.."4",t70•1.00.1•7 ow 4,77 ME VA I •VLATC, ADM, NISMATP31•1 c= No. 01-1040.$ MAJOR REPAIR AND ALTERATION . FOR FAA USE ONLY ORS (Airframe, Powerplant, Propeller, or Appliance) DENTSICATION 10-'‘ . INSTAUCTIONS: Print or ryn .0 ..,•4.., Sr FAA eh% FAR 4 3 Appendix H. sad AC 4SP-I (or 'automat ft ebla &moo° Mr inuncNons cod diepodion of thb form. MARE MCOEL • I. AIRCRAFT Sim 727-10 SERIAL NO. nAmo...Aurr AND RfOISTRATICre MASK MN O.N.A. .MtT • NAME (As shown on rogoVatiat osetifkotN ADDRESS (As shown ce negIoremon aeletons) t oillo ,177f5 4.Ict Illvd. Itletal, III. NANstra.Ta MOS • 3. fal FAA MI OILY A . ti us. 4. T IIIIIIIIMIN S. Dm • , AIRIIWAE Me einalkoarie Ile I ' a • POWEPPIANT e PROPELLER 0 WM APPLINCE none•Clenlit . . . • . "6, LINFOUITT Waal A. AGFNCYS NAME AND AVORM IL EWA OP ARIOACY • " • C. OIRTIPICAM Eq. us.cumeamee•OCRIANIC R. S. 4023 A AIP/SURCH AVIATION We rime* parrarsne seiXemer A/C CLASS 2.34 4150 ONION Covina Dr. ji 911101CAND MANI PATIO. • ta RADIO CLASS lag In& CA Kai $6.....-..... Lomita) untRumItmr SP/CLAILJPern emote •A D.) entity thot the ropeI; orNer •krietie• ads te the *WO Idemlle0 I. Rae ..Inn Led &scribed a. Nerreems• or ettecheeencs hereto hoe bete made Ia iweaddia whist reettienwea or Peet 41 of the US ?.MO Madam Meader sod cher Ow infonotioo fezeiamel Met le wee SA Cenlill to the Inn of en hoostledpe. • . . ,. .• t.- .. • DATE D DUAL APR, 0 3 SO - • 7. AMR Al WW &Sir 10 Pornr to the swim* Mee Fenced opeclied Wks the ushijArnsilo1 is inel valacuS a the manner peon:bed by the Adokeimene of die lbdeni /blocky., AdanielstAdloo -d b IIIIPAPSOVIII) IRE;r Inn RI.SIAMMlipli ORM Oteoh/ . IANNUIWIIII•t MIPICX1004WOOPOILIC1 ecINC101 SY hut OWN& 1 RPM VAPOR . •• Of RANSPOR ••••400• Ot DATE Of APPROVAL OR CARYWICATI OR ' IN AUDI REJECTION APR 0 3 !981 DEPONATION NO . • RS ARRA • • •• ' SDNY GM 027€0032 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246954 EFTA01331417 weight and balance or operating limitation changes shall be entered hp aircraft record. An alteration must be compatible with all previous alteration* to apart. aed.conformity with the oppticable airvrorthiness requirements. 8. OFSCRIP11011 OF WOIII WOMISMEO (II more space is required, attach oeilHenel dna. !Seely will? ok- croft nationality anill registration mark and dote work completed.)' Installation of dual Delco Carousel IVA Inertial Nsvigatibl System in accord— ance with STC SA4164HE. Flight Hanual Supplement issued dated June 27, 1980. Installation of dual HF Canicaticeis System wing a vertical fin loading edge slotted antenna in accordance with Eastern Airlines STC ST51050 except for the following deviations: MC Drawing 1518198 - HF - 1 System Central Head Ned. MC Drawing 1518199 - HF - 2 System Control Head PW. It has been determined that the interrelationship between these changes and any other previously approved modifications will not adversely affect the air- worthiness ofithis aircraft. Aircraft hay bee weighed. Height and Balance and Equipment List Revised. THE BID s-a SDNY_GM_02780033 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246955 EFTA01331418 onathirilts twavonstant Fn Append - FEDERAL AVERIP4 ADIANISTRAFKIR leapt be Na. 04-A060., . tf4AJOR REPAIR AND ALTERATION FOR F44 fist ONLY (Airframe, Po*etplant, Props!ler, or ApeHamm) . • - ODIC! DENTOK 41•••e P5r7oATION ,le CC INSTRUCTIONS: Print or type all main. Sth PAR 43.9, FARO! Amiga,I. sod for kaironioni and dieppaltion of this (ono AC0.9 I Pm IRDIERRO, thnT646 thethe) MODEL "Lein 727-31 I. AIIK4AFI SERI4L jt0d, ItI0XITT Aggo tirSTRA MARE 40/17 rye) NAME (AI thorn on regitfrolionanataged ' ADDRESS (Aa don on atom 1. OWNER . 177795 John F. Blvd. Tennoso. IOC. nur_.:_L_:_i Houston. T i,e FAA IN pi T , . tea 63141 identitiadlwrem complies with AGPI 6 ainvoithiness ‘requIrements and is approve Y for above described aircraft subject to conformity, inspoction bz a - :mth ets.cd„vARA...4::7- „ ch. . 0 ,,- - - I., ,..,._ . 4. WM IDENTIFICATION 5 TYPE nth • 0004t ten WYWY . .. . ATIVRAME ••• CM demand If Om= Lobe* -.. .. A POWEPPUNT • 1 • APPLIANCE nowdeaeunth I RMO,- - lir 6. Xliftellif STAMM • A. AGENCY'S NAME AND AQ0eS -. I. END Of AGENCY . C. CM IFICATE NO. AIRonnarch Artatioo Co. R. b. SVZZ A VS. ONTOKARD .sonai•C •! 4150 Donald Douglas Dr. • NC CLASS .3.4 moo CITIMVIE0 aitaubit Long Belch. CA 90808 RADIO CLASS 1.2* ERIVICARD sous StARIVO LEHRER INSTRIMICNT• AWARNACTUtte i SPECIALTY°, SERMCJI“,./ D. I OrnifY Ass the ;fps;ned/or Attalla. ma . so the nilIt) ichneiled in hem 4 above and meschmems Mato Imo Wax ash liraccordtato with the tetikarna of Pan 0 of the US Podia' dentibad on OR and ibis she information fornished twono. is ans. and ten to the best of ledge. Aviation Regaining's 04,44 , SI I No APR 0 3 19,8' . tor, 7. wont F Ulan fa AMU Pot min so she mahmity Meth persons spasikd below On mit the Athoinisanew of the hand Avignon Administrant> and is hi tinned Mitem 4 entstiasted in the manner premised by . APPROVED m kW - • to to. El PARNFAERRER INIFICDOM AURC0IRLEIX*1 - me pomp; • RW102 - BY 1).• DRIG141 I eta ITAbON OP MARKER ININCEOR V DATE CI APPROVAL OR • CEIGNIC.ATE 0* SIG f TM I VISUAL. REJECTION NAT NO APR 0 3 1981 • E. 'fill. ar FAA Form 337 ri-eri aiaintinhainpi, ...: 7' . ..aaw,rm.tEns- -- Siiiiird11627673b14 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246956 EFTA01331419 FAA AIRCRA -AL +lit `SRA NO. I DAM •q_za - St, • • - NOTICE Weight and balance or operating a:reflation changes shall bra rend in the appropriate aircraft rowed. An olloratilm mint be eompdwble•WHb dl Proe8801 eiteraHons te enure cot.tinued conformity with the applicable ainvorIblaus requkements. • IL MOON* Of WON AECC00DSHE0 DI more space ii required, attach addilionol Ants. Identify with-air. ' croft nationality and registration mark and, date work completed.) - - The fol owing systems were installed complete and in accortance with manufacturer's. speclfic ions;ACCS-32 all sections; AC4.3.13-2 Chapter 2, para. 21,22,23, Chapter Ikl82, 183. e.f.g; AC43-1A Chapter 16, settions 1,2,3.4,5; AiResearch 11, para. Aviation Co. drawings M. 1500553 avionici radio, DI. 1600562 avionics elect and Will Kennedy DER FM 8110-3 data approval. Dual Collins 618M-3A coma system . . . ... Dual Collins 51RV-1 VHF navigation sYStasp. -- Dual Collins FD-109Y flight director syStMe..:.... Dual Collins DME-40 DIE system. . . _. ' . . .. - . s . Dual Collins TDR-90 transponder system . . • ' l i, c Dual Collins DF-206 kW system • Collins FPC-75 ground proximity warning Systel‘we -.. .......-...„„, ..- . Collins 54W1C comparator warning system .. .• Collins 512-4 marker beacon system RCA Primus-400 HKO coloradar system Wulfsberg fligbtfone III air to ground radiotelephone r Flight Instrmuents: . . 2 1DC 521-28007005 servoed encoding altimeters . . 2 1DC 422-30510-130 static_defect corrector.and SAT/TAS =Peters 2 IDC 575-25820-739 mach/airspeed indicators. 2 1DC 513-24660-101 TAS/SAT/TAT indicators. . 1 IOC 540-25100-001 altitude alerter. - 3 Davtron 8118 digital clock/flight time recorder . • 2 Collins 329B-8Y approach horizon indicators 2 Collins 331A-98 course indicators .Rosemount 102/01-2A6 dual tmaperature probe Cabin audio entertainment system The following systems interface and wiring else installed in accordance with AC 43.13-IA chapter 11 all sections: . . 1607032 shaver outfits, mod - 1608092 utility outlets, fwd cabin 1608093 utility outlets, aft cabin' ,. 1608099 service outlets. mod - 161613' ac power distribution - • 161013: ac power galley service. 1611031 Freq.conv. static 115 vac. 60,-KZ 1636212 dc power distribution . 1668006 engi0e oiler remote pump 1683354 sch-electric oven. mod `stern-air) 1683355 electric oven. cod uenn-air). 1683371 galley, fwd unit 1683372 galley, aft unit. 4 . .. , ,-.. U.. ^ MI AltACMED "FWi . *11171-0.P.0.-1101141/1111r>e10/1111 • IP • . SDNY_GM_02760035 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246957 EFTA01331420 / The following systems interface and Wiring also chapter 11 all sections: installed in accordance with AC 43.13-1A. . 1684011 sch-pneu, zone air cond. . 1684012 sch-ckt. air cond.lzone temp,.conl.) • 1684013 sch-ckt, air cond. overheat cont. 1685073 air cond.zone temp control 1687047 air cond. sensor.fans 1692239 . water Mister, galley.6 gal. • 1692240 water heater, master lay. 20 gal. 1692241 water system line heaters,fwd.. 1692242 water system line heaters, aft . 1692316 water heaters, lavatories, mod 1700040 vent blower galley 1755039 air cond. zone temp. indicatiin 1782110 aisle lights, cabin . . . 1. • ssroe i • 1784137 storige comet and closet lights 1789059 ceiling Its essential power .. 1792150 cove tights. era compt • 1792151 cove lights, galley . 1792152 cove lights', lounge.: . 1792153- cove lights, fWd..state.room 1792164 ceiling 1, read Its..creo comPi., 1793268 ceiling %ts galley.. . . 1793269 ceiling 8 read Its. lounge 1793276 ceiling 8 read..lts, totstateroom 1793271 ceiling 8 read..ltas.aft stateroom 1793272 ceiling its, aft:lavatory: 1807045 . table lamps cabin. 1808212 shower fan/ It Aliain.Valvn 1813061 panel Itg. 3rd Mreaman'e 1813062 switch 8 panel ltg,.cmbin 1821059 ceiling its. fwd.vettibule 1821060 ceiling Its, aft vestibule , 1824242 work 8 effect Its, lounge bar, 1824243 vanity lights, aft vestibule 1624244 work Its, fwd anelaft.attendait's 1832400 attendant's panel, feed vest. 1832401 attendant's panel galley . 1832402 attendant's panel.aft vest ----1832403 vanity disconnects. lavatories. . 1832004 circuit breaker panel, galley.): 1832405 circuit breaker panel. mid cabin 1832406 control panels. cabin 1832407 electrical equipment.instl. g411eY 1832408 electrical equip. instl, mid cabin 1837026 spare wires, electrical 1838211 electrical flush.toilets, mod_. 1838212 drain valves water system 1838213 air comer. 8 qty Ind. water system 1880028 air cond. overheat control 1883071 emergency exit ltg, omd 1886193 call system relay assy. . 1886194 call system cabin , 1886195 call system crew.. , arac He''' -Srrns-:ff' 4.°S 'VE)N"?: .Eal_&7r0036--- -- SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246958 EFTA01331421 , • • - • SONY - - SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246959 EFTA01331422 FAA AIRCRAFT RECT,STRY 4,,aERA NO. .•:../\) DATE: the following systems interfa a and miring also installed Inc cordance with AC 43.13-1A chapter 11 all sections:. 1887205 passenger warning signs. 1888050 smoke and flame.det..sensor spy 1888053 smoke and flame.det. bag cosi* . 15(31388 redact power feed; . , 1502232. . radio lights . . .1503I78 ADF-1 system DF,206 .1504137 • ADF-2 system DF.206 . . 1505264 NAY-1 system 512V-1 1506266 NAV-2 system 518V-1._ 1507304 FD-1 system F0-1097.: 1508276 FD-2 system FD-1091 1509281 • EVE-1 system DHEr40 1510184 ONE-2 system . 1511058 DC indicator r. . .1513193 marker syrtem . 1514066 Selcal totem 4560, modif , .1615205 VHF-1 system 6188.3.516207 .. • 1616207 VHF-2 system 618H-3A- 1520127 flitefone system • . 1521225 etc system tdr-90 (duel) 1523254 pe/inph (modif). 1524057 stereo system (cabin). 1525090 tvantenna (prov) -1527211 cockpit audio (modif), 1529137 comparator system 54W-1C 1530149 weather, radar priams-400 . . 1533204 no. 1 radar altimeter ale-51A.imodifi 1531205 no. 2 radar altimeter ale-514. modif 1535205 autopilot system interface , 1536231 comp-1 system interface. 1537221 comp-2 system interface. 1538174• altitude systmn interface. 1541186 Ins-1 system CIVA 1541188 Ins-1 system Interface, 1541187 fns-2 system CIVA 1541189 ins-2 system interface 1544264 1.h. altimeter/alerter , 1544265 r.h. altimeter indicator 1544266 stby altimeter indicator 1545117 mach/airspeed indicators 1547116 1.h. sat/tas system 1547117 r.h. sat/tas system . . 1548034 (2) scat system (modif) 1549249 ennon system . 1550178 `taco accessory box 1551077 digital clock system 1552007 oat indicator (modif) _ 1551091 data select system 1558010 rate of turn system (modif) 1560020 GPWS system (modif) .1571017 ins relay unit 157(1028 nav relay unit 1592046 annunciator cplr diagram . 1594097 cockpit hf/inph control 1594098 cabin flitofone/inph control :.. -3- ' SDNY GM 02760038 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246960 EFTA01331423 An electrical CC-AC load analysis has bet emie,per Misspent Asians Co. report C-3724 in accordance with AC 43.13-1A-426, end. 621.. TOU1,DC.elpseity is 150 cops. Total nortial cruise DC load Is 81.9 ..ape. . .Total MISS AC lea . 57,3 KVA. - Aircraft weighed. Weight and balance and soilpeen4 list frelited. . • 3.13NAte02760039 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_0024696I EFTA01331424 • • . Fan. i .., . Soko San.. No. 04-41060.1 Fraci4 AvIA AfsmarstrAnoN FOR FAA USE ONLY - MAJOR REPAIR AND ALTERATION . oWICE IMMICATION.......' • (Airframe, Powarplael,, Propeller, or Appliance) Wer/F5D0 6 0 INSTRUCTIONS, 'stint or type ell moor. Ste PAR 43.9. FAR 43 Append,* e, and AC 43.9-1 (or sobeerareit.revbio• canoe° to. Irietnectioeis end dupopuon of chit form. • MAKE • • 804119 PACOa72-31 I. NATIONALS,' AND RIGISISARON MARX DELVE MAL NO. : 20155 GM 115057 NONE (At shot. on respiher(cei certificate) .. ADOIESS A. skews on retrhorkin rirlifirote) I I 177% J.F.IL Blvd. l ' "In - - Timone, lac. • • . . MIMIRIMI. Teats 77205 • 1. KR Fil USE OILY The data igernilied hetein Compute with Applicable , aillatliiMMS requirements. and is approvedonlyharebovia ' 'dotal aircraft subject to conformity InspectIontyft " MOIJ In fAR 4.3i7.' - ' • ' ,i IT 'DENMAN • • . MON. semi NO. Arm port MINA snow . • " " - .., MIIIIIAJa . (AO drocribed p4 crew Lis.* -• a 10WINNANT . -".: • mg • ' APPUANCE .. kurStacrtiate 4 EORTOMITT gammen wnearict .... AGni i crsiw .wie 00.soess . .. pod AGENCY C. CDRIPICAR NO. wI w • . M. .. .: 3 - la7ASPRproitatre itallOIANIC it it 4022 A : ..... SVC CASS 244 4150 Domed DOIRJ144 BP. ;'• ....i . _ "SOON CIFEIPICAITD WOW.< - RADIO CLASS 1.2.4 Long Beach. CA 50105 • • . . . .. ...ate-Tian° MAI. StAn°W UNITED INSINUMICSfr - -• • leANWACIV/111, SPECIALIZED Arosnrr . D. I mails ' chef Use. repair suid/o. id44444 be made to the oak( 0 idencikd in ;tab 4 @Son tad es.sibm1 on the or • ,. enschments benne here limo made in *mordent. *Ada the reqvinesans of Peer 43 of the U.S. eders1 Marion Resularions ' sod dug the itsforitiarion Sanitised herein is mot cad coma to the bent of y licreededge. DATE :' ' ' APR . 0 3 MII • - : TO Etna WIos. Munit milted la hem 4 ... keneoga Is the Rammer prescribed bl • Yoe oat to the •AboScy Oven Venom NS the Adnalithustoe of S. Pedal Atleflo• -tr agiOli sad if APPROVED altEJ ~Kra er csecaotur tanniwiffd . . • IM NSW. I • firma in..i.o4 05 TOANSPOCT 1140100/1 00 ... . DATE 01 APPROVAL Oa, alIMICATE- OR . SIG U E R INDIVIDUAL S. REACTOR • ler, . tite APR 0 3 19M 3 tra . • 7 4} t rAdarladlairmat . )414:.4(*" "nitaAra SONY OliC0040 —‘ SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10,-15, and 17 EFTA 00246962 EFTA01331425 NOTICE Weight and baiance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alteration, to assure continued conformity with the oppiicable airworthiness requirements. 3. Otstiar001 OF WORK MCOMISMED (If more space is required, attach additional sheet,. Ident;fy croft nationality and registration mark and date work completed.) 1. Inskalled the followim1-61:40yMehina with RCCS-36 all, sections. AC43.13-2 chapter 1 pars. 1-46÷7-8-9-10-1142 AiReseerch Aviation drawings. 01.130050 1•W 9 tOrs011 %Ural analysis contained 1n Howard Pattmlpi. 1 . geN 1102034 Installation table, eoCktall. lemOV1614. 1(02014' 310244- ° table, cocktail .. 1102046 table, cocktail wi:foliliee tiff . 1104065 r, table, foldout .9 41141.--- • 1124232 " divan, r.h. 3 plea- 1124235 ° divan. 1.h. 2 plaCe.berthable 1124236 ° divan, curved. 4 place. . . 1124237 " divan, transverse,.3 plate . 1124238 " divan. riviena, 3place_ftrd. facing 1124939 " divan. riviera, 3.place aft facing 1124241 " kibitzer seat 1130090 " closet/ desk, 1130093 t closet 1.h. =,i.._, . 1130094 1130096 : cripo coatroomicart.Stnitia 1130097 closet linen, outboar01-.. 1139111 " ledge _ ..... 1142171 " cabinet. refreshment 1144127 " table, with folding.lnYea ..... 1146114 a pull-out table 1147184 a cabinet overhead . • 1147185 " cabinet overhead .. . 1160200 fabrication bulkhead andtkaers 1160201 Fabrication turn. pamolt 1160228 Fabricatiorbeilkham1400 Math 1160233 Installati0n life raft. .01eathwad 161-STD-052 Installation std...blteroirt door end.bulkhad prof. 1164038 Installation fitting..bulthead 1164046 " belkheld and partition upper ate* . . . 1164050 ' partitions. fed, end aft ... ... • 1164052 " pass partition and attach 1165470 ' galley, r.h. fwd,fied.faming, 1165478 " galley. r.h. fed aft.fatelree 1176173' ° cabinet, vanity wi.194t... 1176174 ' cabinet, aft Imv. 1214196 " 'shower 1214200 "" aux. water tank . .4. 1214271 hot water tank . 1214329 ° aux. water tank. aft 1220153 ' pallet, single seat., 1220155 " pallet. single seat. . . 1220158 " pallet. 4th crew asober. 1220159 ' floor support med. Pallet e. jszomoi.fm SnErtS Amt ATTACNED •".".14'.!;:::caligaSeffiwars4a2askarWattstlisPV11..1.. ,___._ _ 1-_,__ _.._4.4:14veSe...:Jsr.:ste .iitrf.f Z. • soniv_em 02780041 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246963 EFTA01331426 M AIRCRAFT' RV [RI NO. Z DATE: 41. : • I. , OORIMo 20116 Tenets Inc. 727-31 N5057 1. Installed the following inaCconiene with ACC:646.'11 sections. AC43.13-2 chtptar 1 pere. 1-47$44-0-0-10-11-12 SA1Research Aviation co. drawings. m1300517, 140041$ end tincture! analysis contained in Baird battens CIER sort Mo. C-1.254 1242022 Installation. crew t 2. Installed the following in accords, with AC26-44, all actions aid Aintanch Aviation Co. thawing*. 1245409 Floorplen - nstallitienef 7.5.0..appantod seats in ralattiE to argency exits... . 3. .Installed the *Mating intaterdine with CAA 44.369 all victim; 4.0162 all sections, th.3I3 art (a) and (A) AC 43.13-2 chants' 12. para. 201. 2132' 2°3' 2°4, 2°60 206 (b) 1211117 baggage tats pas* at:UW.0e 4. Installed the follninl 'caftan with ACCS-$2 all tents. ACCS-33 all sections. AC 43.13-1A chapter 16 sect. 1-2-3-4-5 chapter 16, sect. 1-2-3-4-5. AC 43.13-2.achaptur 2, pan. 21-22-23 chapter 3. an. 31-33-34-35-36-37-38 sad AiRettaarch Aviation Co. drawls. 1410337 Layout- redlo rick Et. E3 1410338 layout - radio rack E4. E5 1425272 Installation flint's sans 1461190 Installation weather radar rit W let. 5. Installed the Collodi., on-structaral its b accordant with the foliation Annearch Aviation Co. drawings: 1117075 titillation- rum sir actuator Wen 1222666 • flat ceiling peal. . 1145047 mtgazine rick„ . It$6169 One how . 1172074 placards 4 4 44. 1249014 cabin tamp seen_ . 1262139 4 zone tan costrol I 1255029 mate oil fill .alltea 1092093 anificatica- hem air nee 1167341-603 oitattionag air Act 6. Installed the following le accordant viltlia* ell action. AC 43. 13-IA. chapter 11 tactical 1-2t3-4-6-6-7, Sattarlhip -intiome 1-2-3.4-5 and Albanian% 'viatica Co. drafts 1181405 layout insummant 1233269 Unmet control ,heel — _ t. /391/17 449441M1- Modification pitotistatit Sentla 1401205 layout. radio coatrols 1411225 Installation- sensor Mal tn. , 1448005 layout overhead panel ite0D4 Layout fit mgr. statics t • • • 1. • .. SDIVY GMOge-0042- SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246964 EFTA01331427 - Cooing 20116 TemaseAla. irz-sx MOST C 7. Inata1latlaa sada 1, adoareaaa id* AC 43.134 doge 4 sad AC 43.13-1A chanter 6 section 1, cAaptar.f. thaditar T actin 1 ,, aster 11 sections 1-2-3-4-6 and 7. chapter 11 and seettectinelgolicIfitatlame. - • - at — or:. • • SDNY —al lied-073 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246965 EFTA01331428 ON 'Er DATE APR 0 • ISM ' OF FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS ‘ AIRCRAFT OR AIRCRAFT CONFONTITIT 'KAMM CATION MODEL NO. . TV,. (M e. bee. Nollapin Walt OF APPLICANT SAAR . BOEING - 727-31 AIRPLANE - AIRESEARCH AVIATION CO. LIST OF DATA . lint IININTIFICATION STRUCTURAL SUBSTANTIATION - Interior Installation for C-3825 TENNECO. INC. 727-31, 5/N 20115. C-3688 Weight and Balance for 5/N 20115. DL-1300517 NC . Data List ; Interior Furnishings. DL-1400319NC Data List - Avionics Meth. PLIAPOSA OF DA TA No. 20115 ONLY. Substantiate BOEING 727-31 Interior Modification byon N5057, Serial Final Apgroval of the Modification will bepade FM. APPLICARLE AtOuisawas (Nat spat,* ...ow.) 4b.306, 4b.260, 4b.358 and 4.101 CAR 4b.202. 4b.301, whk maths* ad labatau CERTIFICATION • Thar ..lolly mad by anafte .1 the Melanesia sod la atanlea ad a ataka am• asand --.— of mamma oda P.n 1ST el la Faml Avads lagaetae. Oa lima /am a amply ad, wilt Oa km bat naiad la .mooch * alb saabllead madam ad load "aalseassu el do radial Ayala laplakoa . RammaO manna a tam Ma I oik main ol ll Apnea J••• eau CLATMFICATiONISI SIONATORION Of DE eNATr 7EIVISNO apanonanvaa ORSONATION eisseeks) NE-663 STRUCTURES ..927M -4,0 -- -- --- ---- Taltitst.••_=--• • •_L.11. ...:26;04101/`• '' SDNY_GM_02760044 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246966 EFTA01331429 wercaCigiFereZ SDNY GM_02760045 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246967 EFTA01331430 M AIRCRAFT REG TRY No. 2ndDATE: 1.-/-); -5's • • Irlorsit 04-1.030.3 MUM svuncy. 30/St • INSIIISTOSSISuns. a .7.17•1 se. 0.• ••• sera s trocriMFOR +sant. ..... ann ...0-0 "'Is...* AIRWORTHINESS CEITIRCATE ISIS SA II•pmesso shlsol ••••• wised IIIS III SPISO•0111. I. Malt I. 4110.41 SS 3. SIMS AS 0010lale 89 SOST Meths 727-31 77744 , ,i 4. 1•00.01 MO MO. 3. SKS WAN l MOM ICS OISICOWKIN 20115 % Pratt & Plattmay JS -7 a?. 101 777 7. IC Of INNS O. II0/1310 WS I. PIONSIS SOS OISIONIMON. II. tl aac SIMS Three 11/A WA A. 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DATE: ', I VNITE0 sTA DEPARTMENT OF TR ANSPORTATIO AI. AVIATION AOMINI ON • - -rrAtiaRo aigwtin $$ SENTIFilITE MEI I. aTITAN NGetrant.• Nang AV • Si.,14 N7897 1- 72741 • S. ill T.0RITT AM) sun MR 1ST j tls •IrmeiNe•••• antis* sew a havens. Po NT64 siLowitee ets•aa • I • . th•Nior. to b• arrip•Nme..• W rieHamr . " /141.4len, •Ii.ssiM As roes ta mp•-••••• Nom ▪ ¶1•41 PA0 COI•OITNNIS Pt.. tart imen.1•••1. NN tplifinisr Is is/•••••••I ormrsl•••• with IN es4cr•R Is •••••••••d CA a ti 0CINNaTCR MIRO Juan 30.1969 NUR 0129 • samsam. ••••••••• P•hassnom sot •Noplke 3 •••room vs b•A. no▪ s airman nom Of IPSILIN0 IN Iltt.' 47=PI MPC iskrejeT ARO, WM APPLICANT NNW AVIATION ETINRATIONA FM No II 00-2 (t-en •<••••••utkv rAw room Ism $ • • • • f. . - •••••••••gainatr...G.... SDNY GM_OffE0048 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246970 EFTA01331433 _ SDNY GM - SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246971 EFTA01331434