EFTA01328448

FormNyasa (Meow Truk"; Nabs' el lbv CMS No 2120-0D20 2126201. MAJOR REPAIR AND ALTERATION For ma use Oar LS Opolnel of Twee:nolo, (Airframe, Powerplant, Propeller, or Appliance) Aware AVIMI011 Awieranneea INSTRUCTIONS. Print or type all entries. See Trtle 14 CFR 443.9. Part 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and deposition of this form. This report is required by law (49 U.S.C. §4470%). Fain to repot can result in a civil penalty fa each such wolabon. (49 U.S.C. §46301(a)) Nationality arid Registration Mani Stoat No. N405PJ 53375 1. Aircraft Make Model Series Bell 407 206 Name (As shown on regstratan certificate) Address (As shown on re9sbahoncertficare) Asssw 9n1I engirt Way 2. Owner cry fjgg Bluff new CA , Nelibro LLc. LO 96080 Co", USA 3. For FAA Use Only 4. Type 5. Unit iciontificaeon Repair Alteration Unit Make Model Serial NO. 0 AIRFRAME (As describedin Nem 1 above) 0 O O POWERPLANT . O PROPELLER Type O APPLIANCE O Manufacturer 6 Conformity Statement A Agency's Name and Address B Kind of Agency run is I Redirrinters Inc. U S. COSCOVIO Mechanic 1 Ma rulacturer Aeons 903 Langley Way Foreign Corbkatod mechanic C Cenifoate No en Red Bluff ties CA ./ COrbfiteled Repair Staten re 96080 cc..., USA Cereficewa marnawianceOrpentzerion Awm306o 0. I certify mai tne repay and/or alteration made to the unit( ) identified in item 5 above and described on tne reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation RegLtati at the information furnished herein is true and coned to the best of my knowledge. Extended range fuel Signature/Date or Authorized Individual per II CFR Pan 43 O APP. El Dan McDevitt 3/29/2021 PJH 7. Approval for Return to Service 60tt Pursuant to the authority given persons specified below, the and r0entthe(1 in deco 5 was iMpeded n the manner presaged by the Administrator of the Federal Aviation Administration and is pi Approved O Rejected FM Fe. Standards PigeonsADOrOvOO by Canadian Inspector Manufacturer Ma Menai-ice Organization Deperweint of Iron:wort BY Omer r FAA Designee if Repair Station Inspection Aulhausbon Certficate or Signature/Date of Authonzed Inddual ivi • Designabon No. AVVTR306C Dan McDevitt 3/29/2021 --P-JH FAA Form 137 ro-os) 600 SDNY_Glvl_02756410 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243332 EFTA01328448 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 fo assure continued conformity with the applicable airworthiness requirements. It Description of Work Accomplished Of more space is ntquintd. attach additional sheets. Identify weft &Erase nationality andregistration mirk and date *a* completed) N405PJ 3/29/2021 Nationales aid Registration Mark Date Aircraft Total Time: 3747.8 Aircraft Serial Number 53375 1. Verified Installation of Onboard Systems International Human External Cargo Hook System STC itSR02724LA. 2. Instructions for Continued Airworthiness to be performed referencing Onboard Systems ICA Document #123-049-00. 3. Weight and Balance and Equipment List have been updated and inserted into the Flight Manual. 4. Flight Manual Supplement #121-070-00 has been inserted into the Flight Manual. 5. An appropriate logbook entry has been made. -END ❑ Additional Sheets Are married FAA Foos 137 iio-op SDNY_GM_02756411 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243333 EFTA01328449 FAA FORM 8130-6, APPUCAHON FOR U.S. AIRWORTHINESS CERTIFICATE OMB Control Number 2120-0018 Ex bon Dale 01/37/2021 0 U$ ONNYVIOM APPLICATION FOR US AIRWORTHINESS ourneuenotos .Pml ot typil. DO nOl wItOnShialsO MM.ROW anIN FM NO Nay. SUNNI MOS OW * an 4011043.0 FM R4priNNIEW• If 0 01 Tnracortom ETIONOMI EOMII MOOT. No EllEcTinerl For spell 11.14 permits ooreolele SectIons II, M. and VII Es Eppbadde 0 ARMS ARMEN CERTIFICATE 0 Amdmeorailen 1 REGISTRATION NARK 2 AIRCRAFT GUNDER'S NAME nom/ 3 AIRCRAFT MODEL DESIGNATION 4 YR IMR FM CODING Bell Hell0394014 407 Do Ater cow DEit 0 i { ANCRAF T SERIAL NO S. 6Pj a ENGINE °ULCER'S NAME Mow Y ENGINE MODEL DESIGNATION 53375 Honeywell HTS900 13130.?-1" O 8 NUIABER OF ENGINES 4 PROPOSER °MOMS NAME WS. 10 PROPELLER MODEL DESIGNATION 1999 I AriceAFT IS 0340. I•4444•FIN •a i OM N/A N/A 1 IMPORT APPLICATION IS MOM MADE FOR MeeNom* raw/ A 1 [STANDARD ARWORTIMESS CERTSCATE macs warn I vow Noma NRHAN4 Tamm. I ewes *am . , SPECIAL AIRINORDNVESS CERTIFICATE /Coco asercom 444.) 7 PR...ARV 0 LIGHT-SPORT Oen Or IMOWS PONII.Pgradva VANamantiOnci Cadet WEN insn ke 2 LIMITED . CLASS I 5 PROwNOWL peausnons) 2 CLASS I 1 AGRICULTURE MID PEST CONTROL 2 AERIAL SURVEY 3 AERIAL ADVERTISING 3 ow RESTRICTED RemmarmI/ 4 FOREST mom Towne. 5 PATROLLING 6 WEATHER CONTROL amennon 0 OTHER isooll I I RESEARCH AND DEVELOPLENT 2 AMATEUR BUILT 3 EXHIBITION 4 AN MONO CREW TRAINING 6 WRITE/ SURVEY i a 0 SHOW COMPLIANCE WITH THE CFR 2 OPERATING My, Camps KIT BUILT AIRCRAFT EA OMNIRoe vabw. Fn molow.• conics.. 4. MAN MEN $1031 I S OPERATING LIGHT•SPORT 6B Combo WE-SRO 44941 4 _/ EXPERIMENTALmem ommeno V re toetenchiel BC OP...6M 10.400r1pram* mai Wm° WOW atioor2 MOITEPOSS corMame wet 5 21 ITO § a OA RESEARCHMO DEVELOPMENT UNIMMED 9 9B MARKET SURVEY 90 EXHIBITOR MCRAE T 9C CREW TRADEIG 9E SNOW COWL WEE WITH THE CFR I FERRY AUGHT FOR REPAIRS. ALTERATIONS. MAINTENANCE. OR STORAGE SPECIAL FLIGHT PERMIT (mica 2 EVACUATE FROM AREA OF IMPENDINGDANGER commas 4.maw Oen omens US 3 CERTIFICATED TAKEOFF WEIGHT II Mr TON 100/00/4 aura VON OPERATION IN EXCESS OF Man 4 DEUVERING OR EXPORTING ISI I PROMICTON FLIGHT TESTING 6 CUSTOMER DEMONSTRATION FLIGHTS C I6 MU TWEE ANWORINNESS CERTIFICATE Moo MOW veramMtainim- ow Irmssr4 Tanen anami A REGISTEREO OWNER As rewompars• ormstoommag IF DEALER. CHECK HERE n I NAME ADDRESS Helibro. LLC 903 Langley Way, Red Blurt, CA 96080 ET AIRCRAFT CERTIFICATION BASIS (Gm.00. 6"."...° Mg"' ...." a ..."" NRCRAFT SPECIFICATION OR TYPE CERTIFICATE DATA SHEET I044 Mw , ASMORINNESS ORECTNES (CNN somaraw Aca ammwmat avowse i RdS• Nal 1 non...roar AD SLPPlagnir F. e n ets canna, a o C a vis sin 0 antenten N/A 201922: 10/M2019. 10/27/2019 ARCA.1 T VOW tangpionatall SUPPLEMENTAL TYPE CERTIFICATE AMmar a ea*ISTC nersewed) N/A i C AIRCRAFT OPERATION NO IMINTENANCE RECORDS CHECK F RECORDS IN COWLEVICE TOTAL AIRFRAME HOURS EMMENTAL ONLY immeawmammt. ammer. V WITH 14 CFR NINTH 91 417 3117.8 3 ANNcfemT0 0 CERTVICKTON. I cieN3 NMI em TN topelred 04044 TM BS OW) of IN. WWI deleted WOW EWEN MOAN mare] tEl INF Milton Admwsnitoon lecordavane Tee 49d U NNW SUM Co% 44101 ILSO Mal Oplable FENNO Aasbm Readoot FM 44. or wa.II has Wel niprel40 RPACRIT/ OldNOM be IS tent MIS 08044010 npolnelol DATE Of APPLICATION NAME NC TITLE An 4 844 n ie 10/29/2019 Mark Summits. Member v ex, A TIE AIRCRAFT DESCRIBED MOVE HAS SEEN INSPECTED Al•OFOUNO AIRWORTHY BY amigo FM Mien Cs. • I4 ON/ o nit Min 14 OFR PI/1121 CERTIFICATE HOLDER CERTIFICATED MEOMMC (G.400•100.000.0 CER TED REPAIR ION tOs. Cam. MO i l l 5 2 IOW OtWAAW NO 3 5 AIRCRAFT MANUFACTURER tow Awe rm. DATE TITLE SIGNATURE i (Oleg ALL MIRY YDS Aws A adili THE CERTIFICATE REOUESTED AbedEtna AMR Slated Ti Sanity VII rates gi rooms* 4 AMENDMENT OR MODOCATKIN Of CURRENT ARVICRTHOIESS CERTIFICATE < 4 891.12.dan kr Em401.0.6m OREM wide Swam FMINSPECTOR FMDESIGNEE VII was conducied w CERTIFICATE HOLIER UNDER 14 114C". 121 ER 135 I I 14Offl pia 145 S DATE ROOF= FM INSPECTORS SIGNAT wDE ERTIFICA ILL REVIEW SIGNATURE ai 0 7 EMI/ OFFICE 4 SIGNATURE NO a ASO /fat f 11.- Zan& Cot 5V769115D— Slattrie7e- Aso( FM Forrn 61304 (392018) AA Prins=1Edwin Superseded EIeditew Fan, • PDF Par 1ol 2 SDNY_GM_02756412 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243334 EFTA01328450 A MANUFACTURER ItME POORESS I I II PRODUCTION SAM MOTO Aticgli:•6* ten) PROOUCTION CERTIFICATE (Cs cocOualts OIALION• NORM TYPE CERTIFICATE OTHER C GM QUANTITY OF CERTIFICATES REOURED FOR OPERATING NEEDS DATE OF APPLICATION NONE MO TALE (After WO) SIGNATURE A DESCRIPTION OF AIRCRAFT REGISTERED WRIER AGGRESS SUNDER !URN MODEL SERIAL NuMSER REGISTRATIONIMRE S DESCRIPTION OF FLIGHT CUSTO/AER DEMCSISTRATODN FLIGHTS El ittecklacplatity FROM TO VIA DEPARTuRE DATE DURATION C CREW REWIRED TO OPERATE THE AIRCRAFT AND ITS EOUIPMENT I PLOT I I COPILOT I I FUOHT ENGINEER I OTHER (Sonly1 I 0 TM ARCRAFT DOES NOT NEET THE APPLICABLE AIRWORTHNESS REQUIREMENTS AS FOLLOWS I 1 I I THE F °LIMNING RESTRICTIONS ARE CONSCERED NECESSARY FOR SAFE OPERATION Ns essowasa Inecnaly) 1 i 4 F CERTIFICATION- Hirst, catty Rol I as Me ro04asal eta (a ha awn/ cl iho rain daialtaci cos RN mm at a Novato win Fitoonl Arco' Aamnatrisenn accaaanca myth TOR 40 ol Me UMW STaNn Coda 42'01 sum ard makable Fain RANO,Rey/Rana ard that NA ANNA Pas DM.nspladd we a RN la i.e Som onalboct DATE lIME NO TITLE (Ave or Om) SIGNATURE / A li potaina lenamokra oral Manergo n Carotins, Htr. 14 CFR Sams 91.9. 0 Statenwe al Conlanray. FM Fenn 8130-0 (MRS aeon .manic .-. f NMdpbN H Farr Anatolia Carulcatien tor Roan Amin I ; 1i 1 8 Ono, Opening Lattelons Alward Oath 00017001.0•40 IN F aII.SS i c Dia Drassaa. Raeognast R Mach anonISOWO) 1 0 Carl WV* and Dance Hannigan Antes A Ara. I I Provos Arocartorsa Collar Hamad H Aecedanc•Wet la CFR Ssaan J CaronMoat's 21.185 CAR GUM* lima aNkoratroo WON MardiattocaseU E Map Rips we mansion. FMForm 337 (Morn nom regured) g I 1 14CFR Spew 2110100 (Coo.tisessn ... , MatReconlo K LegriScal Anna Stotvaent d Canolarct FM Form 813DIS MINA anon f F Th. raPochonRoarel•SH nand) FM FORT 51306(03-20115) Al ROMPS BROM Superseded Electronic FoTnat • PDF Pao 252 SDNY_GM_02758413 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243335 EFTA01328451 UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATIONTEDERAL AVIATION ADMINISTRATION SPECIAL AIRWORTHINESS CERTIFICATE CATEGORY/DESIGNATION EXPERIME PURPOSE MANU- NAME N/A ,0 4 104 FACTURER ADORESS /..? 0, *W. FROM FUGHT TO A 45 -'• __. N 405PJ MODEL 4' I SERIAL Nd 8 75 BUILDER Bel Hellc. [DATE ISSUANCE 07 Nov 2019 linens sooner surrenderedIifOsOmodott. wooed. or IS Mannar= de a( Nov 2019 en einvoreenese .HALM le ellechre under the conchbonswjesnbed in 14 CFR. Peri 21. Section 21 21.211. SIGNATURE OF FAA REPRE TION OR CAME MG (‘ k 547098732 ThiniftwidesFoilloplenue irsoinAlcar al AY lb a OS OFhard Monied* Aft Sam maw nimkslleals elaielmilFume Alta wilsologer, so secara Iva ant moommorri MI FOITIO1OF THE CIERTIltAlt WIT Illi 0SIAVIONI TM AffillWATIER TIC AFAUC.ARIMOIA.A11014 Conditions antLimitations -- 1. This aircraft does not meet the airworthiness standards of Annex 8 to the Convention on International Civil Aviation. Operations in airspace outside of the United States will require the permission of the applicable foreign authority. That permission must be carried aboard the aircraft together with this U.S. airworthiness certificate and, upon request, be made available to an FAA inspector or the applicable foreign authority in the country of operation. Operations may be further restricted by the applicable foreign authority. This may include not allowing use of an airport, requiring specific routing, and restricting flight over specific areas. The operator must comply with any additional limitation prescribed by the applicable foreign authority when operating in its airspace. (1) 2. These operating limitations do not provide any relief from any applicable law or regulation. This aircraft must be operated per applicable regulations and the additional limitations prescribed herein. Note that a clearance from air traffic control (ATC) is not authorization for a pilot to deviate from any rule, regulation, operating limitation, or minimum altitude, or to conduct unsafe operation of the aircraft. If ATC issues a clearance that would cause a pilot to deviate from a rule, regulation, or operating limitation, or in the pilot's opinion, would place the aircraft in jeopardy, it is the pilot's responsibility to request an amended clearance. These operating limitations are a part of FM Form 8130-7 and are to be carried in the aircraft at all times and to be available to the pilot in command of the aircraft. (2) 3. This special airworthiness certificate is not in effect during public aircraft operations (PAO). Concurrent public/civil operations are not permitted; the aircraft cannot be operated as a civil aircraft and as a public aircraft at the same time. No weapons or special military mission systems may be added to the aircraft. This airworthiness certificate is not in effect during flights related to providing military services (that is, air combat maneuvering, air-to-air gunnery, target towing, electronic countermeasures simulation, cruise missile simulation, and air refueling). These activities are inherent military, not civil activities. The FM makes the distinction between the authorized flights for experimental purposes, and PAO. Before operating this aircraft under this special airworthiness certificate following a PAO, the aircraft must be returned to the condition and configuration at the time of inspection for the issuance of this airworthiness certificate. The operator must have written procedures for returning the aircraft to the civil configuration. This action must be documented in the maintenance records. The maintenance records and entries must clearly differentiate between a civil experimental flight per this certificate and any other flights. (3) 4. Application to amend this certificate must be made to the local Flight Standards District Office (FSDO) or FAA Form 8130.7 (11/2016) Previous Edison Dated 04-2011 May be Used oriel Depleted Page 1 of 3 SDNY_CM_02758414 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243336 EFTA01328452 SDNY_GM_02756415 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243337 EFTA01328453 Manufacturing Inspection District Office (MIDO). (4) 5. The pilot in command must hold rotorcraft category and helicopter class certificate or privilege. The pilot in command must hold all required ratings or authorizations and endorsements required by part 61. (7) 6. When filing a flight plan, the experimental nature of this aircraft must be listed in the remarks section. (11) ..., .. 7. This aircraft must not be used /for Oft,including, burript‘ 'mited to glider towing, banner towing, target towing, or towing electronic eCeivers or emitters. Thitjai raft must not be used for intentional parachute jumping. (13) • • , 8. If aircraft or engine operating Ilfnlations are exceeded outsickof planned test conditions, an appropriate entry will be made irithe maintenance records. (14) ‘ 9. No person may operate this airc cat, unless it is maintained R:it n inspection program meeting the scope and content described in § 91.409( .-tpe operator must seleet d identify in the aircraft maintenance records one of the following program for.tbe inspections, aircraft: (a) For type-certificated aircraft, a current inspection program recommen ektythegiallaf . urer; or (b) For former-military aircraft, an inspection program recommended by the manufactu r or North Atlantic Treaty Organization (NATO) military service; or (c) An FAA-approved inspection program. Inspections must be recorded in the aircraft maintenance records showing the following, or a similarly worded, statement: "I certify that this aircraft has been inspected on (insert date) per (identify applicable inspection program) and found to be in a condition for safe operation." Note: To extend an inspection interval, the owner/operator must submit a request for that extension with supporting documentation and data to the local FSDO and obtain concurrence from that FSDO. (15) 10. Only FAA-certificated repair stations, FM-certificated mechanics with appropriate ratings, or a manufacturer as authorized by § 43.3 may perform inspections required by these operating limitations. (19) 11. The aircraft may not be operated unless the replacement for life-limited articles specified in the applicable technical publications pertaining to the aircraft and its articles are complied with in one of the following manners: (a) Type-Certificated Products: Replacement of life-limited parts required by § 91.409(e) applies to experimental aircraft when the required replacement times are specified in the U.S. aircraft specifications or type certificate data sheets. (b) Non-Type-Certificated Products: All articles installed in non-type-certificated products operated under an airworthiness certificate issued for an experimental purpose, in which the manufacturer has specified limits, must include in their program an equivalent level of safety for those articles. These limits must be evaluated for their current operating environment and addressed in the approved inspection program. All articles installed in non-type- certificated products in which the manufacturer has specified limits, must include in their program an equivalent level of safety for those articles. The article must be inspected to ensure the equivalent level of safety still renders the product in a serviceable condition for safe operation. (20) 12. For aircraft originally incorporating fatigue life recording systems, the owner/operator must maintain and use the system as prescribed by the aircraft manufacturer and comply with the manufacturer's fatigue life limits. (21) 13. When changing between experimental operating purposes, the operator must determine that the aircraft is in a condition for safe operation and appropriate for the purpose intended. A record entry will be made by an appropriately rated person to document that finding in the maintenance records. (26) 14. Enhanced Flight Vision System (EFVS) operations for the purpose of research and development and/or showing compliance with regulations are not authorized if any component associated with the instrument approach procedure being flown, or any component of the approach lighting system associated with the FAA Form 8130-7 (11/2016) Previous Edibon Dated 044011 May be Used tail Depleted Page 2 of 3 SDNY_GM_02758416 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00243338 EFTA01328454 SDNY_GM_02756417 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243339 EFTA01328455 instrument approach, is inoperative. (40) 15. Kinds of operations authorized: Day VFR flight operations are authorized (47) 16. Night flight operations are authorized If the instruments specified in § 91.205(c) are installed, operational, and maintained per the applicable requirements of part 91. (48) 17. Instrument flight operations are author' the in ruments specified in § 91.205(d) are installed, operational, compliant with the per:;7 KetequIretherlt f, and maintained per the applicable regulations.The pilot in command Afieve a method tctco, ly with the § 91.319(c) prohibition from operating over densely populated yreas or in congested ainrns. All maintenance or inspection of this equipment must be recorded in tI701rcraft maintenance recor14 nd include the following items: date, work performed, and name and certificate number of person reoining aircraft to service. (50) r , 18. All flights must be conducted Within the geographical area desfribed as follows: Aircraft must remain within the area defined on the attred sectional, while avoiding ensely populated areas, restricted areas, and congested airspace. (53 • 19. Flight over a densely populated a a-Ocip a congestectai ay is authorized per § 91.319(c) only for the purpose of takeoff and landing. The area-ktbe seta cubed by the term "only for the purpose of takeoff and landing" is the traffic pattern. Fertile-purpose of this limitation, the term "only for the purpose of takeoff and landing" does not allow multiple traffic patterns for operations such as training or maintenance checks. This does not restrict a go-around/rejected landing for safety reasons. When avoiding populated areas, aircraft speed and weight must be considered. The information in FM Order 8900.1, Flight Standards Information Management System (FSIMS), regarding set-back distances from spectator areas for aviation events such as air shows or air races may assist in determining a suitable space to fly the aircraft. (55) 20. Flight in RVSM-designated airspace is prohibited. (58) 21. No person may be carried in this aircraft during flight unless that person is essential to the purpose of the flight. (61) Larrie Ricca, DAR 547098732, Seattle MIDO, AIR-872 - END - FAA Form 8130-7 (11/2016) Previous Edibon Dated 04-2011 May be Used until Depleted Page 3 of 3 SDNY_GM_02758418 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00243340 EFTA01328456 SDNY_GM_02756419 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243341 EFTA01328457 \ wi 17 4 0$ h • sty , t • 44-222. SA, 0500 MU ; p.4. Aft:),:: I •'; 12.500 V!. e 14/31. r. • S I; 122.214 . :$4 , . .c-FMNO PI CISO - • f 110 8 :421 - lite 1).ThiOR:: 2229A " ' rif t ISO IROFF(Ill$1 St, I ASOS I Zell, pS4/11 .5.7 At.s.0 G , s ..o.eoceuti..i. tat. Q411 • $5 W r WA i y A 1 . I1 law etunico a 1 ..." . ..1 % • ' L unc*It I 4-14 ',OCAS (IMO PP •car !, MOS OS .0 e 12 f $ • Tat3. Wfst?'44."—^—i ert: yo, ( %. $1CMIMI • • WI011.07' - 33. atplas nitre ILL ..Nhpt 7?4, 11 0000 - 1- +se.) • REVIEWED AND ACCEPTED SAC: VS00 .. • ) .P., q. i I • .1- Waal° MI $' . 'l ...la. -. .05 Atte 12 I ink). 24 •k re****.IM6 .2 tftww2c224.. CC. I ! e • 1 ikaWiqr*P7 ise'767,.. 5 i Me . ..,':,, . • ., 02 ? I, . ,f; gar gleg t. • l ItION4eAlf ' 1 AS $ pa. ' ..L es- ,_...2i4 r.s......____ • • .L esiapi; ....att.. rc. -',..-1, .-.. _ ... _ . _ .7112%...10•L _...... --I•S" A --1 - 1 • • :' .1/4 .1 SDNY_GM_02756420 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243342 EFTA01328458 SDNY_GM_02756421 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243343 EFTA01328459 SPECIAL AIRWORTHINESS CERTIFICATE CATEGORY/DESIGNATION EXPERIME PURPOSE R A griebPiiiiil , r MANU• NAME N/A ,y %I • FACTURER ADDRESS N/ %;;:". sA FROM A • Co& " FLIGHT 't? TO st N405PJ MODEL 4O SERIN. 75 BUILDER Bell Hellcop I DA ISSUANCE 07 Nov 2019 Unless sooner StaraticIsted re wrrunaeon dale 42 Nov 7019 th4 ainnoelttineSS ourodicata i: sfleune under lee ..• in 14 et 21. Section21.t921217. SIGNATURE OF FMREPRESktital .kt, 71040401MM NO. \ ,i e , 1'4 547098732 : - -•1,- me MY_ 441144•444 woman Sao* MeeT 140.1•••101dte••••••••1••••••1Cho Maui* Mr WRIT DethiArtitnalle mato/ KA ME atusoiohis .....Z.,:grat=.4:trrere=r it -- C f%itions andLimitations -- 1. This aircraft does not meet the air hiness standards of Annex 8 to the Convention on International Civil Aviation. Operations in airspace o side of the United States will require the permission of the applicable foreign authority. Th ermission must be carried aboard the aircraft together with this U.S. airworthiness certificate an n request, be made available to an FAA inspector or the applicable foreign authority in the count o eration. Operations may be further restricted by the applicable foreign authority. This may inc not allowing use of an airport, requiring specific routing, and restricting flight over specific areas. The operator must comply with any additional limitation prescribed by the applicable foreign author' y when operating in its airspace. (1) 2. These operating limitati do not provide any relief from any applicable law or regulation. This aircraft must be operated per pl le regulations and the additional limitations prescribed herein. Note that a clearance from air traff ol (ATC) is not authorization for a pilot to deviate from any rule, regulation, operating limitation, or Ximum altitude, or to conduct unsafe operation of the aircraft. If ATC issues a clearance that would a pilot to deviate from a rule, regulation, or operating limitation, or in the pilot's opinion, would ce the aircraft in jeopardy, it is the pilot's responsibility to request an amended clearance. These op ng limitations are a part of FAA Form 8130-7 and are to be carried in the aircraft at all times and to be table to the pilot in command of the aircraft. (2) 3. This special ai iness certificate is not in effect during public aircraft operations (PAO). Concurrent public/civil perakion re not permitted; the aircraft cannot be operated as a civil aircraft and as a public aircraft at th aVtime. No weapons or special military mission systems may be added to the aircraft. This airworthine certificate is not in effect during flights related to providing military services (that is, air combat maneuvering, air-to-air gunnery, target towing, electronic countermeasures simulation, cruise missile simulation, and air refueling). These activities are inherent military, not civil activities. The FAA makes the distinction between the authorized flights for experimental purposes, and PAO. Before operating this aircraft under this special airworthiness certificate following a PAO, the aircraft must be returned to the condition and configuration at the time of inspection for the issuance of this airworthiness certificate/The operator must have written procedures for returning the aircraft to the civil configuration. This actioii must be documented in the maintenance records. The maintenance records and entries must clearly / (fferentiate between a civil experimental flight per this certificate and any other flights. (3) 4. Ap ication to amend this certificate must be made to the local Flight Standards District Office (FSDO) or FM Form 6130.7 (11/2016) Previous Edition Dated 04.2011 May be Used until Depleted Page 1 of 3 SDNY_GM_02756422 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00243344 EFTA01328460 SDNY_GM_02756423 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243345 EFTA01328461 Manufacturing Inspection District Office (MIDO). (4) 5. The pilot in command must hold rotorcraft category and helicopter class certificate or privilege. The pilot in command must hold all required ratings or authorizations and endorsementOequired by part 61. (7) i / 6. When filing a flight plan, the experimental nature of this aircraft must bVitJed in the remarks section. (11) --..:- • 7. This aircraft must not be used for ,.,win—&including, bu 1 1‘ nipt 'm der towing, banner towing, target towing, or towing electronic eceivers or emitters. Thfstai‘ ust not be used for intentional parachute jumping. (13) .. / 8. If aircraft or engine operating limitations are exceeded outs f planned test conditions, an appropriate entry will be made in the maintenance rec 9. No person may operate this aircrafs unless it is mai n inspection program meeting the scope and content described in § 91.409( Ate operator mu d identify in the aircraft maintenance records one of the following program for the inspectio aircraft: (a) For type-certificated aircraft, a current inspection program recommen by,th trio urer; or (b) For former-military aircraft, an inspection program recommended by the man urtei or North Atlantic Treaty Organization (NATO) military service; or (c) An FAA-approved inspect' ogram. Inspections must be recorded in the aircraft maintenance records showing the following, r similarly worded, statement: "I certify that this aircraft has been inspected on [insert date] per [iden applicable inspection program) and found to be in a condition for safe operation." Note: To extend n inspection interval, the owner/operator must submit a request for that extension with supporting documentation and data to the local FSDO and obtain concurrence from that FSDO. (15) ‘,„' 10. Only FAA-certificated repair statio '4:FAA-certificated mechanics with appropriate ratings, or a manufacturer as authorized by *I \ 3 y perform inspections required by these operating limitations. (19) \\ '.1j 1 11. The aircraft may not be opera unless the replacement for life-limited articles specified in the applicable technical publicatio irtaining to the aircraft and its articles are complied with in one of the following manners: (a) Type- cated Products: Replacement of life-limited parts required by § 91.409(e) applies to exper' al aircraft when the required replacement times are specified in the U.S. aircraft specificatio or ty rtificate data sheets. (b) Non-Type-Certificated Products: All articles installed in non-ty ed products operated under an airworthiness certificate issued for an experimental purp h the manufacturer has specified limits, must include in their program an equivalent level of t ose articles. These limits must be evaluated for their current operating environment and dre ed in the approved inspection program. All articles installed in non-type- certificated products iry hich the manufacturer has specified limits, must include in their program an equivalent level of saf&y for those articles. The article must be inspected to ensure the equivalent level of safety still renders the product in a serviceable condition for safe operation. (20) 12. For aircraft originally incorporating fatigue life recording systems, the owner/operator must maintain and use the systein as prescribed by the aircraft manufacturer and comply with the manufacturer's fatigue life limits. (21)/ 13. When chinging between experimental operating purposes, the operator must determine that the aircraft is irla condition for safe operation and appropriate for the purpose intended. A record entry will be made J,fy an appropriately rated person to document that finding in the maintenance records. (26) 14. Enj nced Flight Vision System (EFVS) operations for the purpose of research and development and/or show' g compliance with regulations are not authorized if any component associated with the instrument app ach procedure being flown, or any component of the approach lighting system associated with the FM Form 8130-7 (11f2016) Previous Edition Need 04-2011 May be Used until Depleted Page 2 of 3 SONY_Gld_02756424 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243346 EFTA01328462 1 SDNY_GM_02756425 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243347 EFTA01328463 Instrument approach, is inoperative. (40) 15. Kinds of operations authorized: Day VFR flight operations are au orized (47) 16. Night flight operations are authorized if the instruments speci ed in § 91.205(c) are installed, operational, and maintained per the applicable requireme is of+art 91. (48) 17. Instrument flight operations are auths5Ozed-ittb-el ents specified in § 91.205(d) are installed, operational, compliant with the perfornit acice require f, and maintained per the applicable regulations. The pilot in command ,spiave a meAl • van ly with the § 91.319(c) prohibition from operating over densely populated areas or in coil( " airways. All maintenance or inspection of this equipment must be recorded in tleaircraft mainte arice records nd include the following items: date, work performed, and name and certificate number of person rEo ning aircraft to service. (50) I t.: / --.., 18. All flights must be conducted;\ ithin the ge grAiphical area. des' ribed as follows: Aircraft must remain within the area defined on the at ched se al, while avoiding ensely populated areas, restricted areas, and congested airspace. (53 ::. ( 5-) e;•:' 19. Flight over a densely populated ar to a congested., ay is authorized per § 91.319(c) only for the purpose of takeoff and landing. The ar A it* susfee cribed by the term "only for the purpose of takeoff and landing" is the traffic patter . Flirthe-pur ose of this limitation, the term "only for the purpose of takeoff and landing" does no How ultiple traffic patterns for operations such as training or maintenance checks. This does strict a go-around/rejected landing for safety reasons. When avoiding populated areas, aircraft spe eight must be considered. The information in FAA Order 8900.1, Flight Standards Information a a ement System (FSIMS), regarding set-back distances from spectator areas for aviation events such / it shows or air races may assist in determining a suitable space to fly the aircraft. (55) / 20. Flight in RV5M-des' ed'airspace is prohibited. (58) 21. No person may be d in this aircraft during flight unless that person is essential to the purpose of the flight. (61) Carrie Ricca, DAR 8732, Seattle MIDO, AIR-872 • END - FM Fart 8130-7 (11/2018) Previous Edition Dated 04-2011 May tN Used snail Depleted Page 3 of 3 SDNY_GM_02756426 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243348 EFTA01328464 SDNY_GM_02756427 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243349 EFTA01328465 •-x 4 .• Clots DM 0500 :r%4 --- • 7. 12,503 1 4 • I ••• 0/14(K sPos ITIGN MA) 630 - 2\ r••• 3WELI. a 14 A ?\ • Xl° 1,S"..'.•. . cal O •C• 4 X:MetVciii earl /Pia ku REVIEWED AND ACCEPTED SACS VSDO ' Ogg ZitoI i2 4 ' :. %-tat nwcar c L:;:z SDNY_GM_02756428 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243350 EFTA01328466 SDNY_GM_02756429 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243351 EFTA01328467 • VOTED STATES Of AME/OCA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATIO N ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE 1 NATIONALITY ANO 2 MANUFACTURER AND 41000. REGISTRATION MARLS 3 ARCRAFT SEROL I CATEGORY Bell Helicopter Textron KAISER Canada Model 407 $ Al/114CRITY ANO BASIS FOR iSSWACE 53375 Normal Ilks mows.coVcat %sad "Aunt,/ USC $ WO. map* bat atenetrobaiucinten ia be in,man as c2 Pe Salt attar* mot New rocatienteret, 414040, 3W kr fa MS 44V OK•as n t nbnM'baNIOWA 0:4NASOIRI Ns pen NCetMidarotwtocoNyn pen*!Om.. UN Cane ieinnou OW Myer taw n %ea ErA04044 ***None*** 6 TERNS AI..13CONVUONIS ovennow anars moNNIof onlie •• bowersLo • eb claw abateNry FAA ea NWIWOIS cs*gs Own +Ws AIN tranaiwo ovonolmo flying°. aid II 3456 staslow vs ovIanmo NRNYO• ellFYN 3 43 RN Make Nitta** nignoile arn tar OATS Cs ISSUANCE ettil thaw SINN SERRE DESIGNATION NUMBER 05 APR 2016 T Tha ssYRVIGelree AN swan "nolo, e. none d wetsnet ".44,4•4444 ableac** z oART/106I7VVP 11 CERTSCATE BE OISPIAIED II 3•9 OP, 40 44440,44. egoNIMI 3104540043 ARCWT ASEORDANCE wilN/P/UCASIE FEDERAL FM Fee• 6100.2 OH-Ill Sup4•114•0104‘444 AMINREGULAIGIS Ed.300 kemis 7747Eo 08 /40 Q 7013 SDNY_GM_02756430 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243352 EFTA01328468 SDNY_GM_02756431 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243353 EFTA01328469 HELIBRO LLC APPOINTMENT OF AUTHORIZED REPRESENTATIVE To whom it may concern. e may conduct Man Ownerftrustee of Helibro LLC Mar% Gunsauls as an authorized representativ Gunsauls s also knarm as a legal "tviember to business and has signatory authority for Helibro LLC Mark conduct business and has signatory authority to do so as a Member. Signature M aliiller Rife 6 11-/ r1 Dale Notary 511 CIALCILfirt Signature Notary Confirmation Wow: SDNY_GM_02756432 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243354 EFTA01328470 SDNY_GM_02756433 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243355 EFTA01328471 CALIFORNIA ALL-PURPOSE ACKWOWLEDGMERIT CIVIL CODE § 1189 ,CdSaCajcsjsSaerrattesrma t •r, rOCAV4S4CaliCALCOCCACCIteCettealtairrel,"Wn,"raWe el"..Wall A notary public or other officer completing this certificate verifies only the identity of the individual who signed the document to which this certificate is attached, and not the truthfulness, accuracy, or validity of that document. State of California County of 4/ katvra On Mau, LS+, 0i before L -Dean/la F7em ;visi Date Insert Name and flue he Officer personalty appeared KG r C aust ift cti :Arc Name(s) of Signeifs) who proved to me on the basis of satisfactory evidence to be the person(s) whose names) is/are subscribed to the within instrument and acknowledged to me that he/she/they executed the same in his/her/their authorized capacity(ies), and that by his/her/their signature:O) on the instrument the person(s), or the entity upon behalf of which the person(s) acted, executed the instrument. I certify under PENALTY OF PERJURY under the laws of the State of California that the foregoing paragraph r is true and correct. TRISH MANNA RISS WITNESS my hand and official seal. sEr pionwypow - CaMornia ara • COLN)/ ", e 2160218 - M Comm E res Jul i8 2020 Signature, triAbelk.00.10 4 itAtivi Signature of Notary Public Place Notary Seal Above OPTIONAL Though this section is optional, completing this information can deter alteration of the document or fraudulent reattachment of this form to an unintended document Description of Attached Document &pa 't vrictite_ Title or Type of DoCument: AffolirErnitivf t k14-0,-acuocument Date: D5/o//aei7 Number of Pages: t Signer(s) Other Than Named Above: r -/A Capacity(les) Claimed by Shreds) Signer's Name: Signer's Name: fl Corporate Officer — Title(s): O Corporate Officer — Title(s): Partner — O Limited O General O Partner — C.) Limited O General _I Individual O Attorney in Fact ❑ Individual O Attorney in Fact fl Trustee O Guardian or Conservator O Trustee O Guardian or Conservator :1Other: O Other: Signer Is Representing: Signer Is Representing: 02014 National Notary Association • vAvw.NationalNotary.org • Item 45907 SDNY_GM_02756434 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243356 EFTA01328472 SDNY_GM_02756435 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243357 EFTA01328473 October 29, 2019 Federal Aviation Administration Attn.: James Sprecher 2200 S. 216th Street Des Moines, Washington, 98198 SUBJECT: Program Letter for Special Airworthiness Certification REGISTERED OWNER: Helibro, LLC DESIGN CRITERIA: Research & Development BUILDER: Bell NUMBER OF ENGINES: I MODEL: 407 NUMBER OF SEATS: 7 SERIAL NO: 53375 REGISTRATION NO.: N405PJ Dear Mr. Sprecher: The purpose of this letter is to request a special airworthiness certificate, in the experimental category, for a Research & Development Airworthiness Certificate in accordance with Title 14 Code of Federal Regulations (14 CFR), § 21.191(a). This request is made to support company flight testing in support of FAA Project Number ST17247LA-R. The STC will be for the installation of a Dual Cargo Hook System on Bell Model 206 and 407 aircraft. The proposed Flight Testing will be conducted over I — 3 hours on or around the 7th of November, 2019. We request the designee hold the Standard Airworthiness in suspension until the completion of flight testing. The aircraft will be located at 13.1 Helicopters facilities in Red Bluff, Ca. The aircraft is within current maintenance, has been conformed to the TCDS and the following has been accomplished: • FAA Form 8130-6, with sections I, II, and III completed is enclosed. • The aircraft has been properly registered. • We have weighed the aircraft to determine that the most forward and aft center of gravity positions are within established limits. The weight and balance report is available at the aircraft. • The marking requirements of 14 CFR Part 45 have been complied with, including permanent application of appropriate registration marks and the word "EXPERIMENTAL" near each entrance to the cabin or cockpit. • The aircraft is inspected and maintained in accordance with the Bell Helicopter Maintenance Manuals. The following is a description of the requested geographical areas for flight testing: within the box defined on the attached sectional, while avoiding densely populated areas and congested airways. I request Larrie Ricca, DARF 547098732, be delegated to issue the requested airworthiness certificate. My telephone number is: (530) 527-5059. Please contact me at this number if there are any questions or if additional information is needed. Sincerely, David McCammon, Director of Maintenance - 135 Helibro, LLC Page I of I SDNY_GM_02756436 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243358 EFTA01328474 SDNY_GM_02756437 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243359 EFTA01328475 • I. FAA FORM 8130-6, APPLICATION FOR U.S. AIRWORTHINESS CERTIFICATE OMB Control Number 2120-0018 Expiration Date 01/31/2021 0 U 5 ONAFIRAN U.S. APPLICATION FOR AIR WORTHINESS INSTRUCTIONS -Pm or type. 04 noll *We In Macled areas. these we for FAA use °Sy Storni WORN only b an aulhartred FAA Resesemese it a 0 cd Tamp~a •00borai space n ralursa, We alladorneK Fat Ks* II9o4 994913 0 nen mimeo CERTIFICATE compSte Secbons II. VI. and VIIR 11904601e. AdWalental I. REGISTRATION MARX 2. ~RAFT BUOSERS NAME Mos 3. AIRCRAFT MOOS DESIGNATION 4 YR 6WR FAA COOING N405FU BINHelicopter3 407 1999 Do nter colt Dix I S AIRCRAFT SERIAL NO G. ENGINE BUILDERS NM! Mewl 7 ENGINE MODEL DESIGNATION 53375 Honeywell 1478900 $ib° O. P..-1- -• a SAUER OF ENGINES 9. PROPELLER BUILDERS NAME Mew ID PROPELLER MODEL DESIGNATION 1 AIRCRAFT IS temp emowsst One WA WA I IMPORT APPLCA14344 IS HERESY MADE FOR raw whom ammfr A 1 [ STANDARD AIRWORTHINESS CERTFCATE Momorao~t I 4~ pour, ~at twain areas Mutat, fats • I SPECIAL AMWORTHINESS CERTWICATE ~ ms444.4 SW) 7 PESSARY I I LIGHT-SPORT ~ pm ANTNne POneraCtsA0 WaimadraPPConetd 0104 lateen At 2 LISTED 1 CLAW I 5 PROVISO/Mt solow cow 2 CLASS II 1 AGRICULTURE ND PEST CONTROL 2 AERIAL SURVEY 3 AERIAL ADVERTISING 3 RESTRICTED nows~orma 4 FOREST nen ~mow 6 PATROLLING I MEATIER CONTROL ~~~ 0 OTHER /7~0 C I e RESEARCH NO DEVELOPMENT 2 AMATEUR BUILT 3 EXIMITION 4 MR RACING S CREW TRIMaIG 6 KW SURVEY 0 SHOW COMPUANCE PATH THE CFR ) OPERATING Mamoyessont KIT SALT AIRCRAFT I SA Enorm imate 4~4 a, Nromosemss ottalleas IS OF ra ~5103 I I 0 OPERATING SO 0914~ UWWSsel rasa USTI-SPORT 4 z ExPE RAW Wm. tHanos c44.44.40) OPIWIRO I044031~~TIMISSIMMW 10 4. 44144NOTIN steolhaym S IC arillano~X 5 21.193 al 9A RESEARCH AND DEVELOPMENT ~WINE° 9 90 ~BET SURVEY 90 ONDITION /PROMPT SC CREW TRAINING SE SHOW COMPVANCE WITH THE OFR I FERRY 11.~ FOR REPAIRS. ALTERATIONS. AAWIENANCE. OR STCMAGE SKOP/ FLIGHT PUSSY PM.F. 2 EVACUATE FROM AREA Of 80040.4 DANGER en* lit~act enste Sean OPERATION IN EXCESS OF MAXIMUM CERIFFCATIO TAKEOFF, MGM' a Ow Vt444404aVe almew 4441 4 DEUvERAFG OR EXPORTING 6 PROIXICNONFUOI4T MUM 6 CUSTOMER DEMONSTRATION FLIGHTS C I6 MU MU AIRWORTIINESS CERTIFICATE stmorson1444~044~anslamNee.~4•4as 4PRKIN A REGISTERED OWNER /M mos 0•10,01;* CIebnitatifesiall IF outman= HERE I n NAME ADDRESS lielibro. LLC 903 Langley Way, Reg Bluff CA 98080 BAIRCRAFT CERTWICADON BASIS Kees men .am.meortsa 4.... mnom* AIRCRAFT SPECIFICATION OR TYPE CERTFICATE DATA SHEET or~ as AMINORTHINESS DIRECTIVES asatesseariceMAINlets~. ~no pare ; ~am i *waren mIbe tuAtEMERf was a • army mm• a ea.es elstem N/A A ING(04~4~0 SUPPLEMENTAL TYPE CERTIFICATE 0.0Ise4440444414C arevann i C.NRCRAFT OPERATION MOMAINTENMICE RECORDS CHECK F RECORDS IN COMP/ONCE TOTAL ~RARE HOURS EXPERIMENTS. ONLY gaspert~an rsto4s~ 1 WITH 14 CFR ~on 91.417 3 .44~~441 d o CERAM/01CM- Ihanto, wry MN I ma OW 'awed owner (a its aowo CI ens arum deserted itom, that eta swan 4 regniered we fie ~Ka ACRontoltaben It acandams meDM 49 el te UMW ~NCO% 44101 MIN ma appwatmFerel AvonRoisolMan RP MN re main ma men ..—...d Finals Am Nod. kr be § 2 64~~~4•14 requeskod. DATE OF APPLICATION NAME MID TITLE ~a Fog 10/29/2019 Mark Guinan. Member A TIE AIRCRAFT OESCRITED MOW HAS BEEN INSPECTED MID FOUND MRWORIWY BY ~sr or• 44~449 a' 44 aFismat law _.....i 4'41 1 :LOPS port Ig ?MISDATE HOLDER 3 I CERTIFICATED MECHANIC /Om/ CMIAININM AIRCRAFT MANUFACTURER rtmsala• 4* am el I TED REPAIR S ION ram ~on 444i i i DATE Toil/ SIGNATURE Matta •••••••hbatilime•A DWI/ TEE CERTFICATE REQUESTED e A I Ira INF Ira shool ~DP m &octal I ot VII ~Is 4 PMENDMUIT OR NOINICATION OF CURRENT AIRWORTHINESS CERRFCATE a § aar/TWIII ke a, IL IMPIC•Cal fir • 4~4 ~MPS under Slawsca FM INSPECTOR FAA OESIONEE 0 VII Ras contasi by CERTIFICATE HERDER UNDER 14 14 121 OR 135 I 114 CFR OM 146 1 DATE MOSSO° FAA INSPECTOR'S DONA ROE RTFICA a REVIEW TURE • 0 7 41AI OFFICE 4 SiGNATURE MO .4 nig *attn. LOW424 en 6 40 0 5r75-- • vilier2C4672- AA FMF=151304 (042010)AI Primus Edbcm Smeramlad Eketrarae Format • PDF age 1 o12 SDNY_GM_02756438 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243360 EFTA01328476 IP • A MANUFACTURER WE MMUS II 8 PROOUCTOI MSG (CAMS* MN PRODUCTION CERTIFCATE IGHT FROMM DAMAN AMC TYPE CERTIFICATE OTHER_ C GIVE OLIANTITY CA CERTIMATES REQUIREDFM OPERATIC NEEDS DATE CC APPLICATION NAME NC NILE IRWW MRI VONATURE A OESCRMTK/NOF AIRCRAFT REGISTERED OMER REGRESS SOLDER MIN/ at SERIAL NUMBER REGISTITATON MAK 8 DESCRIPTION OF FLX3HT CUSTMER DEIMSTMTION FLIGHTS n Mon teal FROM 10 vIA CEP/ATOM DATE CURATOR VII. SPECIAL FLIGHT PERMIT PURPOSES OTHER THAN PRODUCTION RIGHT TWIT C CREW REQUIRED TO OPERATE THE AftCMAT MDITS EQUIPMENT I PILOT I I COMM I I FLIGHT ENGINEER I OTHER (SPAM 0 THE AIRCRAFT DOES NOT MEET TIC APPLICABLE AIRWORTHNESS REQUIREMENTS AS FOLLOWS. - - E THE FOU.OAING RESTRICTIONS ANL CONSIDERED NECESSARY FOR SAIL OPERATION (Use Sim,* Oneonta% i CERTICATION • 1Imp coley Tull tenths itelend eons fix Ns Rang all* rain closated atom. Mat re yawl is wavedRd!' Ire IT sickcal AnstalMorn a. in sccordsros win T449 al M. UMW Sens Code 44101Km Mwale Finical Miaon Roptielow weMt to was, hall peen wupeclad in, S sale kr re 4.{11Resat*, DATE MANE NO TITLE (Print of Inn) SIMILTURE / Ar ms Loralces MWarps nCaleillfa Will 14 OrR Smon 919. platls G Sasesnwe el Collorrniy. FMFam 81334 ANTAMMA MAID 1 2 i • A . . C•anai CIMMIP2 LYMICCSAltsched li Far Angeleno CilesS01001fOr MIKA Anna MMOISIATOuilla9 y 2I I Provos Anteetess Cortgaes Read inMorderce We F 14 1 C Oil. DITRAIL PMAAMIN. OK (AIRCO efMn reksors0 gie 14CFR Sam 21.185 cait I ; 1 0 CuTIn W.gtl ardency* MemalcaAnammArat / .1 Curnint Ancertasss Conte* MARRS in ACONCIAAC• Wel,f°79n4"athid) I lAa Wes an1Minion, FMFM XII Mach Wen nikailM) • la cili SOMA 21•191(a) Won teacneo) g a l Fps AMAMIRomlw et ARMIMAM 1( Oehl-Spcn Anna SIS*WII OCanplanot FM Tam 8130-1S (Mach **PI 1 leaned) FAA Emmen°. (0820IS)Al PRISM Edhqns SuptItiMed Elea Fame • POF Moo 2d2 SDNY_GM_02758439 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024336I EFTA01328477 . . SPECIAL AIRWORTHINESS CERTIFICATE CATEGORY/DESIGNATION EXPERT PURPOSE & Qftvelopfroyht- MANU- NAME N/A ,C.,•‘ FACTURER ADDRESS N/ 4.,.."4 • FROM FLIGHT TO WA N 405PJ MODEL SERIAL 75 BUILDER BSI Hebcopte DATE a ISSUANCE 07 Nov 2019 Ural= sooner sorrerclered, revoked. or the sennonstion dere cd tit elookilliness <edifice* o IINICIIVO undo. the cordibonseitordbed in 14 CFR. Pert 21, Secbon 21 1.217. • Se3r4ATude Of FAA REPRESENT NO. TON OR OFFICE MO 547098732 Me *noes % Oinirca• • a4. was. O.• .000/ MT ard TON dena eald NOMItaa A ..S* ales ea M.SC. In twaYeed vow. *Ms awillica4•••••• MO11.10‘ fr•. wd iro noliestet THOPOIMONC• IN ccoaccoe oust at osivnto I no ARCRAII Mt oc M•IXASIIPIEGIJA -- Conditions and Limitations -- 1. This aircraft does not meet the airworthiness standards of Annex 8 to the Convention on International Civil Aviation. Operations in airspace outside of the United States will require the permission of the applicable foreign authority. That permission must be carried aboard the aircraft together with this U.S. airworthiness certificate and, upon request, be made available to an FAA inspector or the applicable foreign authority in the country of operation. Operations may be further restricted by the applicable foreign authority. This may include not allowing use of an airport, requiring specific routing, and restricting flight over specific areas. The operator must comply with any additional limitation prescribed by the applicable foreign authority when operating in its airspace. (1) 2. These operating limitations do not provide any relief from any applicable law or regulation. This aircraft must be operated per applicable regulations and the additional limitations prescribed herein. Note that a clearance from air traffic control (ATC) is not authorization for a pilot to deviate from any rule, regulation, operating limitation, or minimum altitude, or to conduct unsafe operation of the aircraft. If ATC issues a clearance that would cause a pilot to deviate from a rule, regulation, or operating limitation, or in the pilot's opinion, would place the aircraft in jeopardy, it is the pilot's responsibility to request an amended clearance. These operating limitations are a part of FAA Form 8130-7 and are to be carried in the aircraft at all times and to be available to the pilot in command of the aircraft. (2) 3. This special airworthiness certificate is not in effect during public aircraft operations (PAO). Concurrent public/civil operations are not permitted; the aircraft cannot be operated as a civil aircraft and as a public aircraft at the same time. No weapons or special military mission systems may be added to the aircraft. This airworthiness certificate is not in effect during flights related to providing military services (that is, air combat maneuvering, air-to-air gunnery, target towing, electronic countermeasures simulation, cruise missile simulation, and air refueling). These activities are inherent military, not civil activities. The FAA makes the distinction between the authorized flights for experimental purposes, and PAO. Before operating this aircraft under this special airworthiness certificate following a PAO, the aircraft must be returned to the condition and configuration at the time of inspection for the issuance of this airworthiness certificate. The operator must have written procedures for returning the aircraft to the civil configuration. This action must be documented in the maintenance records. The maintenance records and entries must clearly differentiate between a civil experimental flight per this certificate and any other flights. (3) 4. Application to amend this certificate must be made to the local Flight Standards District Office (FSDO) or FAA Font. 81304 (11/2016) Previous Edidon Dined 04-2011 May t Used until Depiered Page I of 3 SDNY_GM_02756440 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243362 EFTA01328478 SDNY_GM_02756441 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243363 EFTA01328479 Manufacturing Inspection District Office (MIDO). (4) 5. The pilot in command must hold rotorcraft category and helicopter class certificate or privilege. The pilot in command must hold all required ratings or authorizations and endorsements required by part 61. (7) 6. When filing a flight plan, the experimental nature of this aircraft must be listed in the remarks section. (11) 7. This aircraft must not be used for 'mited to glider towing, banner towing, target towing, or towing electronic eceivers or emitters. Thrt,ai raft must not be used for intentional parachute jumping. (13) .,• 8. If aircraft or engine operating ((inflations are exceeded outsick f planned test conditions, an appropriate entry will be made in,the maintenance records. (14) 9. No person may operate this airecgt.unless it is maintained Ref. n inspection program meeting the scope and content described in § 91.409(f) The operator must selectd identify in the aircraft maintenance records one of the following program for.ttie inspection,oftfre aircraft: (a) For type-certificated aircraft, a current inspection program recommen bytttelpariafaeturer; or (b) For former-military aircraft, an inspection program recommended by the ma ufacturtsror North Atlantic Treaty Organization (NATO) military service; or (c) An FAA-approved inspection program. Inspections must be recorded in the aircraft maintenance records showing the following, or a similarly worded, statement: "I certify that this aircraft has been inspected on [insert date] per (identify applicable inspection program] and found to be in a condition for safe operation." Note: To extend an inspection interval, the owner/operator must submit a request for that extension with supporting documentation and data to the local FSDO and obtain concurrence from that FSDO. (15) 10. Only FAA-certificated repair stations, FAA-certificated mechanics with appropriate ratings, or a manufacturer as authorized by § 43.3 may perform inspections required by these operating limitations. (19) 11. The aircraft may not be operated unless the replacement for life-limited articles specified in the applicable technical publications pertaining to the aircraft and its articles are complied with in one of the following manners: (a) Type-Certificated Products: Replacement of life-limited parts required by § 91.409(e) applies to experimental aircraft when the required replacement times are specified in the U.S. aircraft specifications or type certificate data sheets. (b) Non-Type-Certificated Products: All articles installed in non-type-certificated products operated under an airworthiness certificate issued for an experimental purpose, in which the manufacturer has specified limits, must include in their program an equivalent level of safety for those articles. These limits must be evaluated for their current operating environment and addressed in the approved inspection program. All articles installed in non-type- certificated products in which the manufacturer has specified limits, must include in their program an equivalent level of safety for those articles. The article must be inspected to ensure the equivalent level of safety still renders the product in a serviceable condition for safe operation. (20) 12. For aircraft originally incorporating fatigue life recording systems, the owner/operator must maintain and use the system as prescribed by the aircraft manufacturer and comply with the manufacturer's fatigue life limits. (21) 13. When changing between experimental operating purposes, the operator must determine that the aircraft is in a condition for safe operation and appropriate for the purpose intended. A record entry will be made by an appropriately rated person to document that finding in the maintenance records. (26) 14. Enhanced Flight Vision System (EFVS) operations for the purpose of research and development and/or showing compliance with regulations are not authorized if any component associated with the instrument approach procedure being flown, or any component of the approach lighting system associated with the FM Form 8130-7 (11auls) Previous Edition Dad 04-2011 May be Used until Dealed Par 2 of 3 SDNY_GM_02756442 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00243364 EFTA01328480 SDNY_GM_02756443 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243365 EFTA01328481 instrument approach, is inoperative. (40) 15. Kinds of operations authorized: Day VFR flight operations are authorized (47) 16. Night flight operations are authorized if the instruments specified in § 91.205(c) are installed, operational, and maintained per the applicable requirements of part 91. (48) 17. Instrument flight operations are authofizeslittbAin ruments specified in § 91.205(d) are installed, operational, compliant with the pe;pilvirequileiiiere, f, and maintained per the applicable regulations. The pilot in command /*Kaye a method tetig, ly with the § 91.319(c) prohibition from operating over densely populated s eas or in congested airways. All maintenance or inspection of this equipment must be recorded in ;t te.)zircraft maintenance recor•sls nd include the following items: date, work performed, and name and rtificate number of person rofp ning aircraft to service. (50) 18. All flights must be conducted within the geographical area described as follows: Aircraft must remain within the area defined on the attrilited sectional, while avoidipg ensely populated areas, restricted areas, and congested airspace. (53) ..:-:, ...) ,e..,-` 6,a..:- 19. Flight over a densely populated \a : or,p i a congestechlf ay is authorized per § 91.319(c) only for the purpose of takeoff and landing. The area- stgla_ce cribed by the term "only for the purpose of takeoff and landing" is the traffic pattern. For the purpose of this limitation, the term "only for the purpose of takeoff and landing" does not allow multiple traffic patterns for operations such as training or maintenance checks. This does not restrict a go-around/rejected landing for safety reasons. When avoiding populated areas, aircraft speed and weight must be considered. The information in FAA Order 8900.1, Flight Standards Information Management System (FSIMS), regarding set-back distances from spectator areas for aviation events such as air shows or air races may assist in determining a suitable space to fly the aircraft. (55) 20. Flight in RVSM-designated airspace is prohibited. (58) 21. No person may be carried in this aircraft during flight unless that person is essential to the purpose of the flight. (61) Larrie Ricca, DAR 547098732, Seattle MIDO, AIR-872 - END - FAA Form 81304 (11/2016) Previous Edition Dated 04-2011 May be Used until Depleted Page 3 of 3 SDNY_GM_02756444 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243366 EFTA01328482 SDNY_GM_02756445 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243367 EFTA01328483 SDNY_GM_02756446 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243368 EFTA01328484 SDNY_GM_02756447 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243369 EFTA01328485 UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION SPECIAL AIRWORTHINESS CERTIFICATE CATEGORY/DESIGNATION EXPERIME.NIAIr--__, PURPOSE A Ibvikoarofti 7'N MANU- NAME N/A ‹, Tv FACTURER ADDRESS N/ A:::' J. 0.•... FLIGHT FROM A- .) TO t N405PJ MODEL SERIAL N 75 BUILDER Bell Halo* I DA ISSUANCE 07 Nov 2019 Wins mow surrendered _ rasa. tormInmon SO 2 2019. IN a Maness ceMicaie 4 Olson order tm Creilaastral n NNa14 2I.Sectim 21. 21217. SIGNATuRE OF FM RePRESartar .,‘ TON OR OFFCE NO N.' •• ft% 547098732 The sincean ovals • Mel ' *4 beterry .1* ore TM II t of faimIlteatcn, Mn SIMISS.IISINW renglan kg •••••••• faseaevilo MON* My sea044 Ine. eV fa Mellionvelt MIS KIMONO ME CUM CAR 'AUSTIN/ DISOLOMED IN1141/MOWT PER MI MOULAMNII w., -- C rifitions and Limitations -- 1. This aircraft does not meet the air hiness standards of Annex 8 to the Convention on International Civil Aviation. Operations in airspace outside of the United States will require the permission of the applicable foreign authority. Th ermission must be carried aboard the aircraft together with this U.S. airworthiness certificate an n request, be made available to an FAA inspector or the applicable foreign authority in the count o eration. Operations may be further restricted by the applicable foreign authority. This may inc not allowing use of an airport, requiring specific routing, and restricting flight over specific areas. The operator must comply with any additional limitation prescribed by the applicable foreign author' y when operating in its airspace. (1) 2. These operating limitati do not provide any relief from any applicable law or regulation. This aircraft must be operated per pl le regulations and the additional limitations prescribed herein. Note that a clearance from air traff trot (ATC) is not authorization for a pilot to deviate from any rule, regulation, operating limitation, or icimum altitude, or to conduct unsafe operation of the aircraft. If ATC issues a clearance that would cii#e a pilot to deviate from a rule, regulation, or operating limitation, or in the pilot's opinion, would ce the aircraft in jeopardy, it is the pilot's responsibility to request an amended clearance. These op ng limitations are a part of FAA Form 8130-7 and are to be carried in the aircraft at all times and to be fable to the pilot in command of the aircraft. (2) 3. This spec&il airy" hiness certificate is not in effect during public aircraft operations (PAO). Concurrent public/civil dperakon re not permitted; the aircraft cannot be operated as a civil aircraft and as a public 41 time. No weapons or special military mission systems may be added to the aircraft. aircraft at th a This airworthine certificate is not in effect during flights related to providing military services (that is, air combat maneuvering, air-to-air gunnery, target towing, electronic countermeasures simulation, cruise missile simulation, and air refueling). These activities are inherent military, not civil activities. The FAA makes the distinction between the authorized flights for experimental purposes, and PAO. Before operating thjs aircraft under this special airworthiness certificate following a PAO, the aircraft must be returned to-'the condition and configuration at the time of inspection for the issuance of this airworthiness certificate/The operator must have written procedures for returning the aircraft to the civil configuration. This actioh must be documented in the maintenance records. The maintenance records and entries must clearly ffferentiate between a civil experimental flight per this certificate and any other flights. (3) 4. Ap ation to amend this certificate must be made to the local Flight Standards District Office (FSDO) or FM Form 8130-7 (11/2018) Premiss Eaton Dated 04-2011 May be Used onte Depleted Page 1 of 3 SDNY_GM_02758448 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243370 EFTA01328486 SDNYGM0275.49 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243371 EFTA01328487 Manufacturing Inspection District Office (MIDO). (4) 5. The pilot in command must hold rotorcraft category and helicopter class certificate or privilege. The pilot in command must hold all required ratings or authorizations and endorsemen required by part 61. (7) 6. When filing a flight plan, the experimental nature of this aircraft must bat tea in the remarks section. ., (11) firt 7. This aircraft must not be used for i.wing,-including, btiti ng‘t, mi tniider towing, banner towing, target towing, or towing electronic edeivers or emitters. Thlshpi ust not be used for intentional parachute jumping. (13) '•:' •.- 8. If aircraft or engine operating I Stations are exceeded outs of planned test conditions, an appropriate entry will be made inkthe maintenance rec 9. No person may operate this airccatt unless it is mai n inspection program meeting the scope and content described in § 91.409(f) The operator mu d identify in the aircraft maintenance records one of the following progranis‘48r,tbe inspectio aircraft: (a) For type-certificated aircraft, a current inspection program recommend &OA itrib urer; or (b) For former-military aircraft, an inspection program recommended by the man. urO'or North Atlantic Treaty Organization (NATO) military service; or (c) An FAA-approved inspecti ogram. Inspections must be recorded in the aircraft maintenance records showing the following, r similarly worded, statement: "I certify that this aircraft has been inspected on (insert date] per (iden applicable inspection program) and found to be in a condition for safe operation." Note: To extend n inspection interval, the owner/operator must submit a request for that extension with supporting documentation and data to the local FSDO and obtain concurrence from that FSDO. (15) t ti , 10. Only FAA-certificated repair statlo FAA-certificated mechanics with appropriate ratings, or a manufacturer as authorized by § 4 perform inspections required by these operating limitations. (19) 11. The aircraft may not be ope unless the replacement for life-limited articles specified in the applicable technical publicatio rtaining to the aircraft and its articles are complied with in one of the following manners: (a) Type ated Products: Replacement of life-limited parts required by § 91.409(e) applies to experim al aircraft when the required replacement times are specified in the U.S. aircraft specificatio or ty rtificate data sheets. (b) Non-Type-Certificated Products: All articles installed in non-ty certif ed products operated under an airworthiness certificate issued for an experimental purp se, in h the manufacturer has specified limits, must include in their program an equivalent level of f r t ose articles. These limits must be evaluated for their current operating environment and dre ed in the approved inspection program. All articles installed in non-type- certificated products i hich the manufacturer has specified limits, must include in their program an equivalent level of safty for those articles. The article must be inspected to ensure the equivalent level of safety still renders tile product in a serviceable condition for safe operation. (20) 12. For aircraft originally incorporating fatigue life recording systems, the owner/operator must maintain and use the system as prescribed by the aircraft manufacturer and comply with the manufacturer's fatigue life limits. (21)4. 13. When changing between experimental operating purposes, the operator must determine that the aircraft is irt'a condition for safe operation and appropriate for the purpose intended. A record entry will be made Jf y an appropriately rated person to document that finding in the maintenance records. (26) 14. En nced Flight Vision System (EFVS) operations for the purpose of research and development and/or show' g compliance with regulations are not authorized if any component associated with the instrument app ach procedure being flown, or any component of the approach lighting system associated with the FAA Ppm 6130.7 (1112016) Previous Edition Dated 04-2011 May be Used until Depleted Page 2 of 3 SDNY_GM_02756450 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243372 EFTA01328488 1 SDNY_GM_02756451 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243373 EFTA01328489 Instrument approach, is inoperative. (40) . 15. Kinds of operations authorized: Day VFR flight operations are au °red (47) u 16. Night flight operations are authorized if the instruments spec. fed in § 91.205(c) are installed, operational, and maintained per the applicable requireme o art 91. (48) 17. Instrument flight operations are authorizentlicin u e/nts specified in § 91.205(d) are installed, operational, compliant with the per friice requite f, and maintained per the applicable regulations. The pilot in command st,Save a me ly with the § 91.319(c) prohibition from operating over densely populated ias or in contij /airwkys. All maintenance or inspection of this equipment must be recorded in tIle'pircraft mainte pce records nd include the following items: date, work performed, and name and certificate IO number of person rOpsning aircraft to service. (50) / 18. All flights must be conducted ithin the Agtiphical area des ribed as follows: Aircraft must remain O within the area defined on the at cited sect*ojal, while avoiding ensely populated areas, restricted 4:0,I areas, and congested airspace. (53 --* ,....- 19. Flight over a densely populated ar ,Ili a congested# ay is authorized per § 91.319(c) only for the purpose of takeoff and landing. The ar the suffice cribed by the term "only for the purpose of takeoff and landing" is the traffic patter Foithe-pur ose of this limitation, the term "only for the purpose of takeoff and landing" does no Ilow ultiple traffic patterns for operations such as training or maintenance checks. This does tract a go-around/rejected landing for safety reasons. When avoiding populated areas, aircraft spe eight must be considered. The information in FAA Order 8900.1, Flight Standards Information ement System (FSIMS), regarding set-back distances from spectator areas for aviation events such r shows or air races may assist in determining a suitable space to fly the aircraft. (55) 20. Flight in RVSM-des' )ted'airspace is prohibited. (58) 21. No person may be ' - din this aircraft during flight unless that person is essential to the purpose of the flight. (61) Larrie Ricca, DAR 8732, Seattle MIDO, AIR-872 - END - FM Form 8130-7 (11/2018)Preaus EtonDad 042011 Mey be Used until Depleted Page 3 of 3 SONY_GM_02756452 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243374 EFTA01328490 SDNY_GM_02756453 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243375 EFTA01328491 • • 0500 '•• tap --C m°41 ' 12.503 ,171 51SL ‘,". A ,r 1 RIO litufilital £3CS q0. 7e I 0410`6117 IS .o J 1914 ym.k 60/.4130Weralk A4/3 - 11 1NELL a PA I .4 MI E _cf:se Par4040 :45:-7(..„• no ay •91 itEo will ..-•• ce.ikat ike? 1D1.4V4.1 (.480 - 37 .r. • tr .! e„. ■rr4 50.1 ENM -Tr REVIEWED AND ACCEPTED SAC: VrS00 Y .** ag 1511O I 12 , l*L 7t 17 4 tan St eN ti+ 116""1"1I L r" 'IV P A 4-±-xcn-r -n I 7...Lamy tvniffszyz La.:, • SONY_GM_02756454 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243376 EFTA01328492 SDNY_GM_02756455 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243377 EFTA01328493 - - _ UNITED STATES Of AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATIO N ADMINISTRATION NATIONALITY MO STANDARD AIRWORTHINESS CERTIFICATE 2 MANUFACTURER MD 'soon 3 AIRCRAFT SERIAL REGISTRATION MARLS 4 CATEGORY Bell Helicopter Textron NUMBER N405PJ Canada Model 407 S AUINORiTY MO MSG FOR ISSUANCE 53375 Normal ancramsMtoa :NW Armilie49 U SC $ max sa Newel tit at te nee Yalta MYntflb MenaiNW ird boa *antra te /fie ardor. INretem Wawa. .ffl 'Iamb AMIN comenra at• 'Ma* conetMest of Nam , kr We mostax 44/ AN ton 47.11•00 a reanstoge *waren Mt as $4444M IT Aim I NM Axma. From es con tem EmpI444 ***None*** ... 6 TERNS AND CONDITIONS :nom soxs scon:444 snowed recto eta venvIen On is *Ache a b^I a N eramennc yegnirpt martnect. camine eM4MTfF a, h TM 4411440INNISOMO N W. re Warms Amara tePaytl, CIN nt e40MM Omar Repairs as *pop** rd gird N apf. Seal AM‘M.0 SDI. DATE OF ISSUANCE "ESLWLSW DESIGNATION IMIASER 05 APR 2016 T ftery Moir vreAtIc4.ce444.4 4, Ns ca.* Mato...M OO 43 fat sol etusfe.; 4, X6 anc4O1443,4ce us/Slake DARTI10617WP TNG CERTFCATE WV D.IFIA4E0 4i 04.74447 AZCOR..14ACE MTN APIWALE /Slat. FM Form SI00.2 104.111 $.44,494..4 Prtvon E4604 'WAN. 49101C4/ AMMONS R.& /4/5 /74-7E45 o 8 /400 toc, SDNY_GM_02756456 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243378 EFTA01328494 SDNY_GM_02756457 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243379 EFTA01328495 MEL' RO LLC •FIr IND ESENTATIVE APPOINTMENT OF AUTHORIZED REPR To whom it may concern: as an authorized representative may conduct As an Owneantstee of Helibro LLC Mar's Gunsauls Gunsauls is also Ptricesm as a legal °Member° to business and has signatory authority for liebbro LLC. Mark as a Member. conduct business and has signatory authority to do so Title Date Notary rq f °Ale( CLU2A Signature Notary Confirmation Below SDNY_GM_02756458 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243380 EFTA01328496 SDNY_GM_02756459 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 002433R1 EFTA01328497 CALIFORNIA ALL-PURPOSE ACKNOWLEOGPAEW CIVIL CODE § 1189 sarcomaitaiirazenc .c.cr.ccr..--tcss: notary public or other officer completing this certificate verifies only the identity of the individual who signed the j document to which Ibis certificate is attached, and not the truthfulness, accuracy, or validity of that document. State of California I -111(taneta County of ) on Ma L\ Lc+ R0O before me, "1ink L.. -Ozanne Fle 114 'Act Date Insert Name and Title ofithe Officer personally appeared Ha r k E ati111(.O ILA. 47" } Narne(s)of Signer(s) who proved to me on the basis of satisfactory evidence to be the person(s) whose name(s) is/are subscribed to the within instrument and acknowledged to me that he/she/they executed the same in his/her/their authorized capacityries), and that by his/her/their signature(s) on the instrument the person(s): or the entity upon behalf of which the person(s) acted, executed the instrument. I certify under PENALTY OF PERJURY under the laws of the State of California that the foregoing paragraph Is true and correct. TRISH DIPS ROMIG WITNESS my hand and official seal. Notary Public California cr..; Tenarru County Commission o 2160216 Ma Comm E ires Jul 18 2020 - Signature. ibitofaciel, O 0Andr. ea Signature of Notary Public • Place Notary Seal Above OPTIONAL Though this section is optional, completing this information can deter alteration of the document or fraudulent reattachment of this form to an unintended document. Description of Attached Document Title or Type of DoCiiment: &ANL) lAtto!rent Date: 1.6/0( fa°, Number of Pages: Signer(s) Other Than Named Above: N/A Capacity(les) Claimed by Signer(s) Signer's Name: Signer's Name: LI Corporate Officer — Title(s): U Corporate Officer — Title(s): L1Partner — ii Limited General 0 Partner — O Limited O General U Individual 7. Attorney in Fact Individual 0 Attorney in Fact II Trustee 7 Guardian or Conservator 0 Trustee 17 Guardian or Conservator Other. Other Signer la Representing: Signer is Representing: 092014 National Notary Association • www.NatiOnalNotary.org • Item 15907 SDNY_GM_02756460 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_OO243382 EFTA01328498 SDNY_GM_02756461 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243383 EFTA01328499 October 29, 2019 Federal Aviation Administration Attn.: James Sprecher 2200 S. 216th Street Des Moines, Washington, 98198 SUBJECT: Program Letter for Special Airworthiness Certification REGISTERED OWNER: Helibro, LLC DESIGN CRITERIA: Research & Development BUILDER: Bell NUMBER OF ENGINES: 1 MODEL: 407 NUMBER OF SEATS: 7 SERIAL NO: 53375 REGISTRATION NO.: N405PJ Dear Mr. Sprccher: The purpose of this letter is to request a special airworthiness certificate, in the experimental category, for a Research & Development Airworthiness Certificate in accordance with Title 14 Code of Federal Regulations (14 CFR), § 21.191(a). This request is made to support company flight testing in support of FAA Project Number ST17247LA-R. The STC will be for the installation of a Dual Cargo Hook System on Bell Model 206 and 407 aircraft. The proposed Flight Testing will be conducted over 1 — 3 hours on or around the 7th of November, 2019. We request the designee hold the Standard Airworthiness in suspension until the completion of flight testing. The aircraft will be located at Pi Helicopters facilities in Red Bluff, Ca. The aircraft is within current maintenance, has been conformed to the TCDS and the following has been accomplished: • FAA Form 8130-6, with sections I, II, and Ill completed is enclosed. • The aircraft has been properly registered. • We have weighed the aircraft to determine that the most forward and aft center of gravity positions arc within established limits. The weight and balance report is available at the aircraft. • The marking requirements of 14 CFR Part 45 have been complied with, including permanent application of appropriate registration marks and the word "EXPERIMENTAL" near each entrance to the cabin or cockpit. • The aircraft is inspected and maintained in accordance with the Bell Helicopter Maintenance Manuals. The following is a description of the requested geographical areas for flight testing: within the box defined on the attached sectional, while avoiding densely populated areas and congested airways. I request Larrie Ricca, DARF 547098732, be delegated to issue the requested airworthiness certificate. My telephone number is: Please contact me at this number if there are any questions or if additional information is needed. Sincerely, David McCammon, Director of Maintenance - 135 Helibro, LLC Page 1 of 1 SDNY_GM_02756462 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243384 EFTA01328500 SDNY_GM_02756463 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243385 EFTA01328501 ran 4W0 d Dewar Tfficlorp Wooer 0W No 21204020 MAJOR REPAIR AND ALTERATION 0 2/2e4011 or fAA WOOS/ d1raliprlaaa's (Airframe, Powerplant, Propeller, or Appliance) Fears Adobe Adtrithelnakon INSTRUCTIONS. kid or type as entries. See Title 14 CFR §43.9. Part 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form This report is required by law (49 U.S.C. §44701). Failure to report can result in penalty for each such violation. (49 U.S.C. §46301(0) Nationality and Registration Mark Serial No. I. Aircraft N405PJ make 53375 Model Series Bell Helicopter 407 407 Name (As shown on registration certificate) Address (As shown on registration certificate) scent 401 i anglev Way 2. Owner car San Rid Bluff CA Helibro. LLC. zit 96080 Casey USA 3. For FAA Use Only 4. Type 5. Unit Identification Repair Alteration UnN mate Model Serial No . 0 AIRFRAME (As described in item 1 above) O o POWERPLANT • O PROPELLER - Tyre O APPLIANCE . Itoniocsain 6 Conformity Statement A. Agency's Name and Address B Kind of Agency Nave p J Helicopter < Inc Ii S Cendooteci riechanc I uarvinickirer Menu CM I anglev Way Foreign Cortthcated Phlecran pc C Certificate No. oi, Red Bluff sew CA j corer cote] ReOor Senor, zu 96080 caves USA tartrate@ Morotenanee Orgaltrabon AVVTR306C D. testify that the repair and/or alteration made to the tab( ) Wearied in it/NS/Cove and described on the reverse or ett*Chment$ hereto have been made in accordance with the rersitemenls of Pan 43 of the U.S. Federal Aviation Regulations and that the informal= fornIShed herein is true and eared 10 the best of my knowledge. Extended range fuel Signature/Date of Authorized Individual n f1 per 14 CFR Part 43 O 1/2)JMi APP. 8 Derek Spooner 3/21/2019 -,7,/,-- fon 7. Approval for Return to Service E2 Pursuant to the authority given persons specified below. the unit Identified in item 5 was inspected in the manner prescribed by Me Administrator of the Federal Aviation Administration and is Approved El Rejected FM Fil. Standards Person Aeproved by Canedon lAanufackrer Maintenance Organization Inspector Department or TraMpOrt BY Other (Specify) FM Designee I Repair Station Inspection Authorization Certificate or SigraturerDate of Authorized Individual Designation No. Pc.i$ AVVTR306C Derek Spooner 3/21/2019 . ../..---- 85S FAA Form 33700.011 SDNY_GM_02756464 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243386 EFTA01328502 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 e. Descdpaon of Work Accomplished (amore space is required. attach add.tional sheets. Wendy with aircraft nabonamy and recestratton mark and date via* competed) N405PJ 3/21/2019 Nationality and Registration Mark Dale Aircraft Total Time: 2852.4 SIN 53375 Installation of Garmin GTX 345 Transponder STC#SR02124SE. 1. Installed Garmin GTX 345 Transponder referencing Garmin STC SR02124SE. 2. Instructions for continued airworthiness to be performed referencing Garmin ICA Document 190-00734-21 of the latest FAA approved revision. 3. Flight Manual Supplement has been inserted into the Flight Manual. 4. Change to aircraft weight and balance negligible. Aircraft equipment list has been updated. 5. An appropriate logbook entry has been made. END ❑ Additional Sheets Are Attached FAA Form 337 noes} SDNY_GM_02756465 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243387 EFTA01328503 Leen Apparel Eleatin< Trealler Pthirtier 0 CMG no 21204:020 VS Onarnm.r, MAJOR REPAIR AND ALTERATION 2a9/7011 Far Fla use Only at Travispottato, (Airframe, Powerplant, Propeller, or Appliance) agent Minton ArlialresvatIon INSTRUCTIONS Print or typc all entries See Tale 14 CFR 5439. Part 43 Appendix B. and AC 43.9-1 (or subsequent raglan thereon for instruction and rkSpOSnion of this form This report * required by law (49 U S.C. 544701). Failure to repot can testa in a ova penalty for each such violation (49 U.S.C. 546301(a)) Nationality and Registration Mark Senai No. N405PJ 53375 1. Aircraft Mae Model Series Bell 407 206 Name (As show,' On sagestnsion certificate) Address (As shown on registration certificate) Ann. WWI Anatil May 2. Owner SUN CA c" , Red Bluff lielibro. LLC 4 96080 cant USA 3. For FAA Use Only 4. Type 5. Unit Identification Repair Alteration Unit Make Model Sera No. • 0 AIRFRAME (As deathbed on hem I above) O O POWERPLANT ED ii PROPELLER Type O n APPLIANCE Manufacturer 8 Conformity Statement A. Agency's Name and Address B. Kind of Agency Wee p I Halirnpuwx Int. U 5 Canaria Mechanic I Madinat Mena 903 Langley Way Far Cankaled Maher* C. Cerbficate No coy Red Bluff sta. ('A j certificated Rook Simon to 96080 c....«., USA Carticaled Mantenance Orgarnatan AWTR306C D. I certify that the repair anWor alteration made to the unit( ) identified in item 5 above and (*stilted on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 Or the U S Federal Aviation RegulaNanS and that the information furnished herein is true and correct to the best of my knowledge. Emended range fuel SynatucerDate of Authorized Individual per 14 CFR Part 43 O MO. B James Tierno 3/26/2018 ./..,_ vi_a_S.J14 7. Approval for Return to Service b ,50 Pursuant to the authority given persons speared below. the unit identified in Rem 5 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is APPrOved 21 El Rerected FM Fe Standards Manufacturer Panne* 4P1r0Verl Dy Careldela Maintenance Orgarmation Department of Transport Inspector BY Other (Specify) FAADesignee 1 Repair Station Inspection Aute04241.44 Certificate or SgnaturetDate of Authorized individual Designation No. AWTR306C Brandon Niewinski 3/26/2018 FAA Form 337 no -oh SDNY_GM_02756466 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243388 EFTA01328504 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 (If more space Is requvrect, attach additional sheets Identify 'Oh aerie natIonatey and registration mark and date woe* completed.) N405RJ 3/26/2018 Nabccialty and Registration Mark Date Aircraft Total Time: 2564.8 Serial Number. 53375 Installation of Aeronautical Accessories, Inc. Slide Window Latch Kit STC# SR01074AT 1. Installed Aeronautical Accessories Slide Window Latch Kit P/N 407-552-300 referencing installation instructions report number AA-96178 revision H. 2. There are no instructions for continued airworthiness provided for the slide window latch kit 3.There is no flight manual supplement provided for the slide window latch kit. 4. Change to weight and balance is negligible. 5. An appropriate logbook entry has been made. —END-- 0 Additional Sheets Are Anached FAA Fenn 337 occ31 SDNY_GM_02758487 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243389 EFTA01328505 Fool Porene Emaccric Trockng Panto. el....- COON* 2i200220 us Onsewir MAJOR REPAIR AND ALTERATION zdenon Fee FAA Use Mb et trinspalann (Airframe, Powerplant, Propeller, or Appliance) Federal A.41*. AbnInIstreeee INSTRUCTIONS: Print or type al mines See Title 14 CFR §43.9. Part 43 Agenda 8. and AC 43.9-1 (or SubSequerd revision thereof) for estrudbons and disposition of Me form This report is required by raw (49 U.S C §44701). Flukey to report can remit in a awl penalty for each such violation. (49 U.S.C. §4630I(an 'Nabonality and Registration Mark Serial No N405PJ 53375 Make Model Series Bell 407 206 same (As shown on regstration co/Meeks) Address (As shown on regarnsuon cernficate) mem QM I anglAy way t. Owner CA. Red Bluff Pan Ca Helibro, LLC zo 96080 cower USA 3. For FAA Use Only 4. Typo S. Unit Identification Repair Alteration Unit Make model Sens No. IZI AIRFRAME (As descnoed in green I above) El O O PCMERPLANT O El PROPELLER Type D APPLIANCE ( O 6 Conformity Statement A. Agency's Name and Address B Kind Of Agency en p I Willman% Inr USCeftfiCated MOChane I Manulatturat Adam 903 Langley Way Feemn Certificated mechanic C. Certificate No ca Red Me see CA i Celli-MOS Repasr Stake se 96080 Canty USA Coftlateol Manlennce Oreanuabeo AVVTR306C 0. Icemen/ nal the repair andlor alteration made IC the unit( ) identified in item 5 above and described on the reverse or anachmeMs hereto have teen made in accordance with the regteermmts of Pan 43 of the U S Federal Aviation Regulations and that the information furnished herein is true fend correct to the best of my krxmledge Extended range fuel Sgrunure/Date of Aul110ezed Individual per 14 CFR Pad 43 O APP. El James Tierno 3/26/2018 j"..aJI-1 7. Approval for Return to Se ' 530 Pursua t to the authority given persons specified below. the urn KleAllried in item 5 was Inspected in the manner presented by the Aominisvator of the Federal Aviation Administration and is g Approved . Rejected FAA Flit. Standards Persons Approves by Camden Manufacturer Maintenance Organization or Tranipan Inspector BY Other (Specify) FAA Designee I Repair Station Inspection Aurri0OZahOO Certreale or Signature/Dale of Authorized Individual Desgnalron No. AWTR306C Brandon Niewinski 3/26/2018 FAA Form 337 noon SDNY_GM_02756468 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA JX)243390 EFTA01328506 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. DoscrIptIon of Work Accomplished (If more space is 'sootier( Oath eddeldnal sheets. Identify with aircraft slalom,* end togistration mark and dale work completed) N405PJ 3/26/2018 Nationality and Registration Mark Dale Aircraft Total Time: 2564.8 S/N 53375 Installation of AFRO Design Ltd. Cyclic Friction Replacement STC# SR03283NY 1. Installed AERO Design Ltd. Cyclic Friction Replacement Kit P/N 95201-01 referencing AERO Design Ltd drawing number 95201 revision 1. 2. Instructions for continued airworthiness to be performed referencing AFRO Design Ltd. ICA 952 90 of the latest FM approved revision. 3. Installed FM approved AERO Design Ltd. Rotorcraft Flight Manual Supplement document number FMS952.91 into the aircraft flight manual. 4 Change to aircraft weight and balance negligible. Aircraft equipment list has been updated. 5 An appropriate logbook entry has been made. --END Additional Sheets Are Attached FAA Form 337(loon SDNY_GM_02768489 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243391 EFTA01328507 Fenn Approved Eiconic Trec.teg Motet 0 041A No 21200)20 MAJOR REPAIR AND ALTERATION 2/2,300I or FAA Um Only La owenflow et Tranponaton (Airframe, Powerplant, Propeller, or Appliance) resins, Minion AbniNsintion INSTRUCTIONS. Pnnl or type all entries. Seo Title 14 CFR §43.9. Pan 43 Appendix B. and AC 439-1 (or subsequent revision thereof) for instructions and disposition of this form. Ibis report is required by law (09 U.S.C. §44701) Failure to report can result in a civil penalty for each such violate). (49 U.S.C. 446301(0 Nationality and Registration Mark Serial No. N405PJ 53375 I. Aircraft Make Model Senes Bell 407 206 Name (As shown on tegistrabon cerntcate) Address (As shown on registration certificate) AO&44S onv i an(ry Way 2. Owner fted Bluff sine CA Helibro. LLC zo 86080 Cost, VSA 3. For FAA Use Only 4. Type 5. Unit Identification Repair Alteration Unit Make Model Serial No. Ga AIRFRAME (AS cfestiftwd in Hem f above) El El O POWERPLANT 0 El PROPELLER Type El APPLIANCE El Manufriclorer I. Conformity Statement A. Agency's Name and Address B. Kind of Agency Nary P II 14Miewiwort low U. S Certresed Mechanic I Manularturar Mites 903 Langley Way Freon unrested Madame C. Cerblicate No. ear Bled Bluff at,. CA Certificated Raper Mallon de 96080 twee USA Certificated Maintenance Organization /AW7R306C D. I certify that the repair andlor alteration made to me unll( ) dentified in item 5 above and deserted on the reverse a 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 MAI and correct to trio best of my knowledge. Extended range fuel SignalurerDate of Authorized Individual App.BCFR Part 43 I JI, 7. Ape:twat for Return t. Service Pursuant to the authority given persons specified below. the unit identified in item 5 was inspected in the manner presented by the Administraior of the Federal Aviation Administration and is n Approved . O Needed FM Ft Standards Persons Approved by Camden Manslacturer Maintenance Organization InspeCtor Dimenment of Tampon BY Other (Specny) FAA Designee I Repair Station Inspection Mtn:Mallon CeetifiCidt or Signalure/Date of Authorized Indmdual Designation No. PJH AWTR306C --- ----r------- n7r- FM Form 237 Vocal SDNY_Givl_02756470 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243392 EFTA01328508 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 Me applicable airworthiness requirements. 8. Description of Work Accomplished (IImore space u required. attach addattaratt sheets. Identify with aircraft nafionaldy and registration mark and date work completed) N405PJ 2/14/2018 Nationality and Registration Mark Date Aircraft Total Time: 2553.3 Aircraft Serial Number: 53375 1. Installed Onboard Systems Secondary External Load Hard Point STC ttSR02651LA referencing Aerocraft Inc. Master Data List ARC-407-MDL Revision "NC". 2. Instructions for Continued Airworthiness to be performed referencing Aerocraft Inc. Master Data List ARC-407-MDL of the latest approved revision and AC 43.13-16. 3. Weight and Balance and Equipment List have been updated and inserted into Flight Manual. 4 Flight Manual Supplement ARC-407HP-RFMS has been inserted into the Flight Manual. 5. An appropriate logbook entry has been made END ❑ Additional Sheets Are Attached FAA Form 337, • SDNY_GM_02756471 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243393 EFTA01328509 fOm:7rd BOCiraft Tian; Nunte 0% SO us oweewi MAJOR REPAIR AND ALTERATION Mena. write owe* of Tramcdemir (Airframe, Powerplant, Propeller, or Appliance) Feelers, MINI*, mennwinuon INSTRUCTIONS. Pnnt or type all entries. See Title 14 CFR IC.% Pert 43 Appendix B. and AC 419.1 (or subsequent revision thereon for instructions and dispostion of tnis fan. This report is required by law (49 U.S.C. §44701). Figure to report can result native penalty for each such violate (49 U S C. §46301(a)) Nationality and Registration Mark Serial No. N405PJ 53375 1. Aircraft Make /MSS Series Bell Helicopter 407 N/A Name (As shown on regishaeon CCMICOIC) Address (As shown on nigistMtn meta) PJ Helicopters Inc. mews 001 tonality way 2. Owner CA. Reg Bluff sus CA go 060130 Comer United Steles 3. For FAA Use Only 4. Typo 5. Unit Identification Repair Metall*, In Make model Sena No 0 2 AIRFRAME (As deschted in item I above) 0 • PONERPLANT 0 0 PROPELLER rys• 0 O APPLIANCE Menutodurer 4 Coaformity Statement A. Agency's Name and Actress B. Kind of Agency Isms Fagg, CAnten Maintananre U.S.C.:Mates Mechmic bleaufectuel mem 823 McTavish Road NE Fo.e Cabkaled thchenc C. Cenificate No. c4 rotary Sm. AR Centeeptod Rem* Slalom re T2E 7G9 mow Canada f CoMmeled Marten*** 0rmitidebon 5-81 D. leerily that the repair and/or alteration made to the wig ) identified in nom 5 above and described on ne reverse or attachments hereto have been made in accordance will the requiremwts of Part 43 of the U $ Federal Aviation Regulations and mat the information furnished herein is true and coned to the best of it knotteoge Exr 14 tended C range fuel SignaturerD e o MIndividual pe FR Pan 43 0 App. B / /({Feb aotS 7. Approval for Return to Benda Pursuant to the authority given persons swaged belle, the ung mentde_o m Wen 5 was inspected in the mannaIMMCAMet by the MMAS.13101 of the Federal Aviation Administration and IS U Approved Rejected FM Fri Standards Persons Approved by Credal WISPeCtOr Malinttlfer / Maintenance Organization DepelMel al TraMpal EP/ Other (Specoy) FAA Designee Rept, Station Inspection Authorization Cern cam o S7 1 ezed /Da Individual DesignationrNo s-81 fig /r7 PI lag 41 FAA Form 337 once; SDNY_GM_02756472 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243394 EFTA01328510 • NOTICE Weight and balance or operating limitation changes shall be entered in the appropnate aircraft record. An alteration must be compatible with all previous alterations fo assure continued conformity with the applicable ainwrthiness requirements 8. Description of Work Accomplished (amore space is required. tech additional sheets CCM(, witwithaircraft nationetty and registration mark and date work completed) N405PJ February 13, 2018 Nationality and Registration Mark Date Sell 407 N405PJ SIN 53375 AFTT: 2553.3 Installed Eagle Copters Maintenance Ltd. Honeywell HTS900-2-1D Engine Conversion P/N E407-789-011.1 in accordance with Supplemental Type Certificate SR03496NY. The installation of this kit was carried out IAW Eagle Installation Instructions IIN-E407-789. Revision D. dated 16.05.04 Items for continued airworthiness to be canted out IAW Eagle Instructions for Continued Airworthiness (ICA) ICA-E407-789, Revision 2, dated 16.07.15. Flight Manual Supplement (FMS) FMS-E407-789.1. Revision 1. dated 23 Aug 2016, is associated with this installation. The above work was carried out on Eagle Copiers Maintenance Work Order N55000. This aircraft was reweighed, weight and balance equipment list was updated by Eagle Coolers Ltd at this time to reflect the installation of this kit. —End Adabonal Sheets At Attached FM Fenn 337 moon SDNY_GM_02756473 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243395 EFTA01328511 kenr;coal Eimoonc Tn. , Paaveor el file MAJOR REPAIR AND ALTERATION 2.00/2011 vsmoan or IAA On** al inniontan (Airframe, Powerplant, Propeller, or Appliance) Falersi I Adminifereles N INSTRUCTORS: Pnnt or type all entries. See Title 14 CFR §43.9. Part 43 Appendix 0. and AC 43.91 (or subsegueM revision tnereon for instructions and disposition 01lNs form. Tha report is required by Law (49 U.S.C. §44701). Failure to report can result racier penMy for each such wolabon. (49 US.C. §46301(a)) Slatienably and Recesumien Mark Serial No. 14405PJ 53375 t. MrcraB Make Model Series Bell Helicopter 407 NIA Name (As shown on AististratiOn certificate) Address (AS shown on regisbitsbon ceatiCele) PJ Helicopters Inc. omens relit anginy Way 2. Owner Car Red Bluff sox CA no 96080 coon United SIAM 3. For FAA Use OnN 4. Typo 5. Unk identification Repair Attention UM make Model Serial No. El AIRFRAME (As descnbed in Mere I above) El CI O POWERPLANT . • PROPELLER 'Type El O APPUANCE aremissiew 6. Conlomety Statement A. Agency's Name and Address 8.1Und of Agency Plem Papa Contain Maintenance U. S. Ceiliacaled Mechanic ] Menseacturei Ia... 823 McTavish Road NE Forego Caracoled Mechanic C. Certificate No. or Calgary awn AB C•MOCeled Rep* Slain as T2E 7G9 cow, Canada ,e. Cectificoned Maintenance Oragriaation 16-81 0. I coney mat the repair amber Menem made to the unit( ) kleMilled in item 5 above and deserted on the reverse or altadinents hereto have been made in accordance with the reourements ot Part 43 of the U.S. cadent AMMIOn RecULMICK and tilt the informatke furnished herein is true and correct to the best of my Snowcap. Extended range fuel Segnatore(Da of *Melted IneWidual per 14 CFR Part 43 O APP. 8 trir irkt PI reb aois 0 7. Approval for Pan to SioMca Pursuant to the Whiny g ven persons specified below. the tare Matted in Item 5 was inspected In the manner prescribed by the Admintstrator of the Federal Avanon Administration and is 0 Approved Rejected FMFt Standards Manufacturer 1 Maintenance Organization Person. Mamma by Canadian Inspector al /ransom Si' (Sealy) FM Designee Repair Station Inspection Aulhortzelim Cereficat or Signal ate Inndniddt Dennallon NO /)) pi * 13 jolt* 41. 6-81 FAA Form 337 oe-oh SDNY_GIll_027564 74 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243396 EFTA01328512 NOTICE Weight and balance or operating limitation changes shall be entered in die appropriate aircraft record An alteration must be compatible with ail previous alterations to assure continued conformtly voth the applicable einvorthiness requirements 8. Demean or Work Accomplished Of more space u mewed. attach adosonai sheets ldentlfy WO aircraft nationality and registration maw and date vO✓k contswiect) N405PJ February 13, 2018 Naticnarrty and Registration Mark Date Bell 407 N405PJ S/N 53375 AFTT 2553.3 Installed Eagle Copters Maintenance Ltd. Inlet Barrier Filter P/N 1003.01-001 in accordance with Supplemental Type Certificate SR03706NY. The installation of this kit was carried out Eagle Installation Instructions 1003-MI-001. Revision B, dated 16 02 17 Items for continued airworthiness to be earned out lAW Eagle Instructions for Continued Airworthiness (ICA) 1003-CA-001, Revision 0. dated 15.09.21. Flight Manual Supplement (FMS) 1003-FM-001. Revision A, dated 16.03.17. is associated with this installation The above work was carried out on Eagle Copters Maintenance Work Order #55000. This aircraft was reweighed, weight and balance equipment list was updated by Eagle Copiers Ltd. at this time to reflect the installation of this kit. End O Additional Sheets Are Attached FAA Form 337 nest SDNY_GM_02756475 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243397 EFTA01328513 Farr AO9roved Eicctroc TwangMete Owe .63 2110-0O20 0 US OspirloWil MAJOR REPAIR AND ALTERATION 2/20/2011 Pot PM Vegteref Orr 1....P51. 62' (Airframe, Powerplant, Propeller, or Appliance) fetal Aviation Painisbuion INSTRUCTIONS Print or type all entries. See Tide 14 CFR §43.9, Part 43 Appendix B. arid AC 43.9-1 (or subsequent revision thereof) for instrucbcas and disposition of this form This report is required by law (49 U.S.C. §44701). Failure o report can restil in a CMI penalty for each such violation. (49 V.S.C. §48301(a)) Telabonality and Registration Mark Serial No. N405PJ 53375 t. AlrcrNt Make Model Series Bell Helicopter 407 206 Name (As Shawn on refastraoon certificate) Address (As shown on registration cerebrate) &nen gm, 1 anoby Way 2. Owner cry Red Bluff sate CA Helibro LLD. to 96080 cony USA 3. For FAA Use Only 4. Type 6. Unit IdentilkatIon Rate Attention UM Make Model Serial No. O izi AIRFRAME (As described in Item 1above) O . PCOAERPLANT O O PROPELLER ' TAW O APPLIANCE menuracrwer O 6 Conformity Statement A. Agency's Name and Address 8. Kind of Agency NI^. PJ Helirnntiora Inf. U. S. Graeae Medusas I Msrolacturer Ansa 903 Langley Way Forego Certificated MeCherk C. Certificate No. co Raab Bluff sue DA .i Cerefleated Row Sumo se 98080 c.....v, USA Certalabld lidedenela Oftleniate AWTR306C D I certify that the repair and/or aeration made to the urit( ) identified in item 5 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the Information furnished herein is true and correct to the best of my knowledge nn Exterxled range fuel SignaturaDate of AuthonzeO Indwidual / PJI-i per 14 CFR Part 43 Ape 8 Wesley Clark 5/25/2017 Ce14_ 910 7. Approval for Return to service PurSuant 10 the authority given persons specified below. the unit identified in item 5 was nspected In the manner prescribed by the Administrator of the Federal Aviation Administration and is 2 Approved • Rejected FAA FP Standards Manufacturer Maintenance Organization Persons Approved by Canadian Inspector Department of Tramper' BY Other (Specify) FAA Deafens.. I Repair Station Inspection Authorization Ceti cote or Signature/Date of Authorized Individual Designation No. ag PJH AINTR306C Daniel McDevitt 5/25/2017 Ann FAA Form 33700CM SDNY_GM_02756476 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243398 EFTA01328514 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all prewous alterations to assure continued conformity with The applicable airworthiness requirements. S. Description of Work Accomplished (lt more space is required. attach additional sheets Mewl), with aircraft nationality and registration mark and date work completed) N405PJ 512512017 Nabonaltly and Registration Mark Dale Aircraft Total Time: 2311.3 Serial Number: 53375 Installation of Dart Aerospace Bearpaws STC# SH1031NE. 1. Dart Aerospace Bearpaws kit D206.559 installed or removed referencing Dart Installation Instructions D206-559 revision L or later approved revisions 2. Instructions for continued airworthiness to be performed referencing Dan ICA-D206-559 revision 4 or later approved revisions. 3. There is no flight manual supplement provided with the Dart Bearpaw kit. 4. Aircraft weight and balance to be updated upon installation or removal of Bearpaws 5. An appropriate logbook entry wil be made. —END-- Additional Skeels Are Attached FAA Form 337 hods) SDNY_GM_02756477 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA ({)243399 EFTA01328515 FtnnAporoyos Etectionic Tracking Number MAJOR REPAIR AND ALTERATION OW 460 21204020 0 I ray20:ff Trau6mponstont Oeisemson a (Airframe, Powerplant, Propeller. or Appliance) For FAA Use Only Foams Await. ariwasinison INSTRUCTIONS. Print or type as (mines. See FAR 43.9. FAR 43 Apperda B. and AC 439-1 (or subeequent testiOn fiere00 for Mau:Wm and esposacn of Inia form. this repon us required by in (49 U.S.C. 1421). mem to abort can ream • <he penakY nOt beached 31.000 for each MO1Pcfabon (Section 901 Federal Aviation A* 196$) Nateinalrty and Regiftreltn Mark 501W No. N405PJ 53375 1. Aleoraft Make Model Sense Bell 407 Nine (As :Mown an reptstration cettleato) tomes (As snow, on repistsabon cornikaaw Helibro LLC. Amee.903 Lanalev Way 2. Owner coRed Bluff stma6 ze96080 Carm71.15.8 3. For FAA Us* Only The data Penelled herein temples wen Me arpltabla airworthiness Requirements and Is approved on for me above aerates arum AOKI te oteremlib mermen bye person aurceired in 14 R rt A25.7 3 / . / H I H 0' firlfri r 4. Type 9 Us Identification Repay Memnon Uns, Make Model Sens Number O a AIRFRAME (AS &tweed An nem f above) O o POWERPLANT • PROPELLER O on. APPLIANCE O O u.....,), e,,e, 6. Conformity Statement A. Apercys Name and Address B K rd of AgitnCy rarref) J Helicopters Inc. 0 U S Certscetee mechanic 01Maniitacarei AostatAf(7 lanalev Way 0 Foreign ceemsed Simmons C cetrraie No cryRed Bluff sierCA 2 Certneated Repair Station AVVTR306C 4936 !1_84 ca.- USA 0 cent aced ktentonance Organization o Immo mat be repair wicror a:aeration node to Me unnis) centI ed in item 6 above and descreed an the reverse or attachments hereto have boon made in aosordesce MN the temerernents of Pan 43 of tie U S. Federal Maim Rogulatons and Nat The onformaticn futadned herein s true and corm*bra beet 01my knonfedge Extended range fuel Semmureirtme °Muttered per 14 CFR Part 43 Metal RNA O ACP. 8 "are Siws---- 5 7%2,3.- i 7 850 7. Approval for Return to Service Pursuant 10 to authority peers pose woofed below. No test Panelled In *ern Ss Inspected in the memo (444104X41 by the Admirer/966a 01the recommitted:in Admntstraton and Is r APPROVED O ROM= FAA Fa Standards Person Approved by Conlon inepeam Manufacturer Mantua:* Orgeorston Oepertmets 01 BY Oleo Meerite FAA Oemanee dc Repair Sieben Inspection Auelonaton Carona* or Deagnalson No. Signature/Dab) N Authorized Individual PJH Alerte_SPia C. --- wi 5.4.--- 5 -13(9 850 FM Poem 337 ito-oet SDNY_GM_02756478 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243400 EFTA01328516 NOTICE Weight and balance or operating limitation changes shall be enteredki 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 (If more space as required, attach additional sheets Identify with aircraft nationally and registration mark and date work completed) N405PJ [3.16.17 Nationality and Registration Mark Date ACFT TOTAL TIME 2259 5 ACFT SN 53375 Installed FreeFlight Radar Altimeter RA4000 system with Radar Altimeter Display to satisfy FAA mandate 14 CFR 135 160. 1 ) Mounted new TSO'd RAD 40 Display to existing panel blanking plate in the aircraft instrument panel at sta. 40 with 'MS' hardware Mounted new TSO'd Radar Altimeter MN RA4000 behind aircraft hatrack at sta 157 vath WS* hardware and 202473x.040" aluminum doubler. alodined and painted. Mounted new TSO'd Radar AttaMeter Antennas to existing STC'd Radar Altimeter Antenna Brackets on aircraft belly behind aft aosstube at sta. 168. All power supplied from avionics buss through 3A Circuil Breaker PIN M5265743. placarded 'FtAD ALT. All single conductor wire M22759/18 series. As shielded wire M27500 series 2.) All work performed referencing BHT407.mm. FreeFipta Systems Operationfinstaeation Manual 484948, FreeFhght Equipment Installation Manual #84629, and AC43.13-1B chapters 4. 7 8 11. latest revisions. Operation portion of the Freight Operation/Installation Manual placed on board the aircraft as a guide to equipment operation. 3.) This install is for VFR use, altitude above the terrain is advisory information only. 4.) Weight and Balance computed. and equipment list updated. 5.) An electrical load analysis determined that the electrical load of the aircraft does not exceed 80% of the rated generator capacity. 8.) Installed equipment does not interfere with or displace required equipment or otherwise interfere with the safe operation and ainvoethMeSS of the aircraft. Failure of this equipment would not prevent continued safe flight and landing of the *Craft 7.) Performed ground functional test referencing manufacturers installation manual procedures that determined the operations and functions olexisling systems and components previously instated are not adversely affected by this alteration 8.) This equipment was found not to exceed the guidelines in FAA Roiorcraft Directorate policy letter ASW.2001-4, dated Apri 25. 2003 for FADEC controlled aircraft and is considered to be "equipment not known to have potential for interference. 9.) CONTINUED AIRWORTHINESS' Requires operational test and visual inspection in accordance wan FAR Part 43 Appendix I) Annually. Reference manufacturers publications END ❑ Additional Sheets Are Attached FAA Form 337 (1006) SDNY_GIvi_02756479 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024340I EFTA01328517 CO', AWMCI Exam= Tracery M.tsr OMB No 1120{020 2011.20ti 0 MAJOR REPAIR AND ALTERATION of FAA Um OM, USOstamment et Tremaeneten (Airframe, Powerplant, Propeller, or Appliance) !Sorel Aveiro AsIminisermlen INSTRUCTIONS: Print or type all entries. See Tree 14 CFR §43.9. Pal 43 Appendix 8. and AC 43.94 (or subsequent revision thereof) for Instrucbons and disposnon of this form. This report a required by law (49 U.S.C. §44701). Failure o report can result in a civil penalty for each such violation. (49 U.S.C. §46301(a)) Nationality and Registration Mad Serial No. N405PJ 53375 1. Aircraft Make Model Series Bell 407 206 Name (As shown on registration certtricate) Address (As shown on registration certhcare) MM. 901 Langley Way 2. Owner Cyr Red Bluff sate CA Helibro, LLC. zo 96080 ca' a l i USA 3. For FAA Use Only 4. Typo 6. Unit identification Rep* Mandel Unit Make Model Serial NO. El AIRFRAME (As described in Nero 1above) O . O POWEFtPtANT O El PROPELLER bee O O APPLIANCE msninedurer S. Conformity Statement A. Agency's Name and AddreSS B. Kind of Agency inn P,1 Helicooters Inc U S Connate, Methane I Manufacture. Man 903 Lanotey Way Foreign Carl/awe Mechanic C Certificate No. on Red Bluff sue . CA i Caveats, Repay Staten r.. 96080 c.v., USA Carbf)C0030 Maintenance 0reanabce AWTR306C 0. leerily that the repair and/or alteration made to the unit( ) identified in ACM 5 above and desalted on the reverse or attachments hereto have been made in accordance with the reqoarements of Pad 43 of the U.S. Federal Avistion Regulations and that the Information furnished herein is true and correct to the best of my knowledge. Extended range fuel SignatureiDate of Authorized Individual pet 14 CFR Part 43 0 APP. 8 Brandon Hall 12/1/2016 el: 7-- - 7.------ -CH.7(1 7:01 PJ 7. Approval for Return to Service 915 Ras, to the authority given persons specifiedandbelow. is the aid identified in Item 5 was respected in the manner presorted by the Administrator of the Federal Aviation Administration 0 Approved O Reacted FAA Fit Standards Persons ADOMeed by GAMMA Manufacturer Maintenance Organization D•Palment or Transco, Inspector BY Other (Specify) FAA Designee I Repair Station inspection Authorization Certificate or Straturol3ate of Authorized Individual P,JH Designation No. AVVIR306C Joseph Tierno 12/1/2016 525 FAA Form 337 1, ..! SDNY_Glvl_02756480 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243402 EFTA01328518 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. S. Description of Work Accomplished (If mote space is required attach additional sheets Identify well worm? nationality and registration mark and date work Completed) N405PJ 12/1/2016 Nationality and Repetration Mark Date Aircraft Total Time: 2210.0 Serial Number: 53375 Installation of PJ Helicopters External Cargo Container STC# SR02494LA 1. Installed PJ Helicopters External Cargo Container referencing PJ Helicopters FAA Approved Master Data List, Document No. PJ9001006-MDL Rev. A dated 1/23/2014. 2. Instructions for continued airworthiness to be performed referencing PJ Helicopters ICA Report No. PJ9001006-ICA initial release dated 10/25/2013 or the latest FAA approved revision. 3. Updated the Flight Manual with the PJ Helicopters FAA Approved Rotorcraft Flight Manual Supplement Document No. PJ9001000B-RFMS initial release dated 3/10/2014. 4. Aircraft weight and balance and equipment list has been updated. Permanent structural provisions entered in the aircraft weight and balance at the time of installation. Cargo container and cargo weight has been deemed removable equipment, weight and balance to be determined upon time of installation/removal, reference Rotorcraft Flight Manual Supplement. 5. An appropriate logbook entry has been made. END Additional Sheets Are Attached FAA Form 337 nom: SDNYGivl_02756481 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243403 EFTA01328519 Fan fl ays! Elscimm -Ado ram.. OMB NO 2120W20 0 usOidamien MAJOR REPAIR AND ALTERATION 2410011 ter IAA UN Ority of Triratowcn (Airframe, Powerplant, Propeller, or Appliance) /Swill A•istion AtiminIstniton INSTRUCTIONS. Print or type all entries. See Title 14 CFR §43.9. Part 43 Appendix B, and AC 43.9-1 (or subsea sit revision thereof) For instructions and disposition of this form. This report is required by law (49 V.S.C. §44701). Failure to report can result In a Civil penalty for each such violation. (49 U S.C. 546301(a)) Nationality and Registration Mark Serial No. N405PJ 53375 Y. Aircraft Make Model Series Bell 407 Name (As snovm On regisfrahOn certeicare) Address (As ShOwn On registration certificate) AeSen am I anglay Way 3. Owner cry Red Bluff f.'s. CA Helibro LLC. bp 96080 CO.F.Y Lan, 3. For FAA Use Only 4. Type S. Unit Identification Repair Alerabon Unit Make Model Serial No. El (As descnbed In hem I above) El AIRFRAME O O pemERptANT O O PROPELLER Type O APPLIANCE El Menerectwer 6 Conformity Statement A. Agency's Name and Address B. Kind of Agency N. P II Heliemphara Inc U S CerbficaYa Mechanic I ManulaClunn Nova 903 Lenin') Way Foreign Can/a...a Mechanc C. Certificate No. on Red Bluff Yee elk if artilcaled papaw station ze 96080 cur., USA Conificatoe Mantileunn Orgaihni/On AVVTR306C 0. I certify that the repair and/or Iteration made to the unit( )identified In item 5 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Pmt 43 of the U.S. Federal Aviation Regulations and that the nformation furnished heran is true and co rect to the best o4 my knovAedge. Extended range fuel Signature/Dale Of Authorized Individual per 14 CFR Part 43 . .7..."....._ .. NH APP B Derek Spooner 1/5/2017 $50 T. Ancona' for Return to Service Pursuant to tne authority g von perAXS speeded below, the unit identified in 4em 5 was rtspeded in the mangle prescribed by the Administrator of the Federal Aviation Administration and is Ei Approved O Rejected FAA Fs standards Persons Approved by Canadian Manufacturer Maintenance Organization ciimanniont or Transport inspector BY Other (Specify) FAA Designee I Repair Station Inspection Authorization Cart, Late or Signature/Date of Authorized Individual Designation No. -- .:,.. s--- RIK AVVTR306C Derek Spooner 1/512017 850 FAA Form 337 mice) SDNY_GM_02756482 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243404 EFTA01328520 NOTICE Weight and balance or operating kmilation changes shall be entered in the appropriate aireratt record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. DescripUon of Work Accomplished (II mom space is mewed. attach acketionai sheets Identity wah aircraft nations/4e and registrabon mark and date work completed) N405PJ 1/5/2017 Nationality and Regetration Mark Date Aircraft Total Time: 2223.3 Aircraft Serial Number: 53375 • ' Installed Helifab Inc. STC #SR02597LA Radar Altimeter Antenna in accordance with Helifab Inc. Installation Instructions Document #HF-N-7-6 Rev. A. Helifab Inc. Master Drawing List Document #HF-MDL-7.6 Rev. A, and Helifab Inc. Instructions For Continued Airworthiness Document #HF-CA-7-6 Rev. IR. • Instructions For Continued Airworthiness to be complied with in accordance with Helifab Inc. Instructions For Continued Airworthiness Document #HF-CA-7-6. • Weight and Balance and Equipment List have been updated. ' No Flight Manual Supplement was provided from Helifab Inc • An appropriate logbook entry has been made. Addeional sneets Are Attached FAA Form 337 noon SDNY_GM_02756483 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243405 EFTA01328521 0 8 FAA FORM 81304, APPLICATION FOR U.S. AIRWORTHINESS CERTIFICATE 0 Form APproved o M.a No 2120-0018 tO Ex Konen Dow 000.020 I I TI 0 0 US. OsorMNII APPLICATION FOR U.S. AIRWORTHINESS INSTRUCTIONS -Pmt or lope. Oo Parole in shoka ma,. men ant fa FM uwasf SWAN *Vim' Prey lo we solkelmd FM Ropreseminvo IF Addionel FATS *Pool • Few* uN 44•Mment Fee WPM Sr Penni+ emirate StOroms 444/10•144441104 INSIONIO. CERTIFICATE ".and VII RIRPONNIA 1 REGISTRATIC/411MOC 2 NRCRAIT EPALCEITS NAME wow 3 AIRCRAFT MODEL COGNATION 4 YR PPR FM CCCZA 1 AIRCRAF1 SERIAL 1.0 6 ENGINE SULDERSNAUE Mow 407 I ENGINE 11000. DESOKATIEN 1999 PP Cato 53375 R2im Royce 250-C476 Otani 1,00,g II a RUINER CF EONS N4°5Pj 9: MEIER COWERS HARE Vsp 10 acetate waft DESKAMON lit luSCPMT IS me. • %weepy j H7eiib One NIAIF lI 9608 PPPLICA R.n.,TIGN mo IS NE tThi REBY RACE FOR 4:4414 4444.44 es* I 11 STANDNIDAMACRTIIIRESSCERTIFCATE Pea angwal U "." 4 ) I." . I means Imms,cl I ,••••,- I I-" J l• -a - I Ir.. B i SPECIAL APIWORTFINES4 CERRACATIOsaftwermsway) ro LLc PRI II man-SPORT ft...is Arpin Pasearaluie WNEAStalltatol OW Low Mon Pa 2 WINO i CLASS i 5 MONSIONAL mars wee a ,—.. 0/S5 It 2 ii N. CERTIRCATION REOUESTED AdliCuL lull AND FIST CONTROL I 2 a SLIMY 3 IS MMM. POVERTISING RESTRICTED 0...w. osAmmi liAlIATEVROJILT 3 FOREST way rre. 0 PATROLLING 6 II WAINER CONROE bionerOnnt IM 0 1 4 OTHER tscAm / RESEARCH ANDOEVELOPMENT Mt RACING 2 S CREW TRYING I 3 ii EXNENTO1 PARKET OWNER S TO NONCENVELLNCE MMUS cs* I °MAWS IfIerr easesitga SULT AIRCMFT .,' OA Emirs astrefustrei on siwilvais NNW% & WO mad 3 CCU 4 st EXPERIMENTAL A.A.r. no /NAY • P. 44•44444 OPERATP4 OS ° PP. 'S USIRSPRI Fault 4 UGHTSPORT ec Owen) etelleet preeiceary *sod IONS WOW Cain OrtgifIling.. wean war 0 21193 lia/AAPEO IA RESEARCH AND DERELCINIENT I RC j JCREIN INNING e ANCRACT as &CARNET SURREY : I PERRY FUert FOR REPAIRS. ALTERA AGNS seiertemetece ORSTORMS 4 Sofa/ER.0S PERROT Ames 2 EVACUATE FROM AREA OF IMPENUNG CANCER 0 Ss. •boar.4441 N. ~IN 3 CP:GRAMME ELMS OF IMAIMAI CERTSCATIOTANSOFF PIDGIN Leta Mr Ora 444444 eat 4 DEUVERIVG OR EXPORTI443 IS I I PRODUCTION RIGHT TESTINO S 0/STORER CENCINSIMTION FUGNIS CI 6 -17U.LTPLE MAPANIFRAESS CERTIFICATE Mom Matt me.. swam. seelmeser.%sawsurearral A REGISTERED OMER 0., "An m m.mantmormmomm) IF DEALER.CNECII NEM I NA 903 Langley Way, Red Blue.MPORTCA 0 NRCAAFT see TON OR TYPE CE KATE OATA SHEET 1.3404. SI neveness ORECT1WS R ear EIMOIS/100••••••••ONSIed rfaef•••••• § 3 1 MOM ✓tirserteoSuPVUliPer sae pe army ens arra e so c✓ 1702/2010-12/250018 neerider o = NRCIMFI USING MIRNFRAPNAGU / SUPPLEMENTAL TYPE CERTIFCATE pm AFT ear Netnews* ° Ilf WA 13 r c NACRol7 OPERATION ANO UMPTEILOCE RECORDS 1 CQIIWARICESOARC64n4 j COCO( a RE IN 'TOTAL mRFRostE HO EXPEINIENTAL ONLY PLIWPSIPass sIMINNONINIMmle 2222.7 3 sm••••• 4..m.},, 14CFR NS, SIMI d 0 WarallON . I Nolesoonty Sue I wi re mpIINNI mar IN At EOM el MI Moll Onart01 item. MN Ms aval • maim, i.e the SRNSMace Achwince m acorn Rol Tin 0)01 to Ulna NanCom 4001 Ms at amilatIt F•Pire RAMS Rostaioni. Ina to mosemA Ni Own aseas0 at onmetts at woos Id ON ~vivo, cons mown DATE OF APPUCATION NAME NO TITLE preertm) 03 Jan. 2017 Mark Gunsauls, Member' ;tgite A ISE NROTAFT E ll NAS SEEN INSPECTEONO FOUND NIMORTHY SY Swami IN mom Pe14 Mts.. 7. i § 2 14 CFR pz 121 CERTIFICATE SOLDER An II I !CERTIFICATED MECNANC No. molar RN le l 1 ,C:rill-ICA REPAIR STATION AN Gioia 1 i V 5 GTE AiRCRArr ILANJFACIINER Moo momegag TITLE SIGNATURE flea AU sad. OP 444s 4.40 0 INE COGIFICAlt REQUESTED . 4 Allan. o• amyl burped Si say 0 INPNETR In woos RV paw mar Secowni Li a vi mots rooms FM INSPECTOR CERTIFICATE 1.82t0ER ta40ER kw Al AINICRIENI OR /400SCATION OF CURRENT Airman mess unman FM OC WI DE NUR WIG U14CFRosi IN CCM LI to CFR poi NS 4 i i ono alma. 87 s 1 DATE IICOCSDO FM INSPECTORS 5 a CE FM INONECTCNI CERTIFICATION FILE REVIEW COME 3Kittor SIGNA71.888 •s 05 Nu o 1 Orli Mil 'V ti Alcrof snipe 7a4t.t. A.L.,-) A$' Se -^b4 FM Form 81304 (0c201 ) PrevIma adept Superseded Elec000ic Formal -POE 4sge I of SDNY_GM_02756484 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243406 EFTA01328522 A MANUFACTURER TIME AOORESS MIN . § i II PROCUCTON BASIS (Ordi MM PROOUCTION CERTFICATE (Gwomxlverm cioN6PIN mm e? V TYPE CERTFICATE 5 OINElt C GIVE OLIMITTEY Of CERTIFICATES RIMMED FOR OPERATING NEEDS ' DATE a APPLICATOR I NAME AND TITLE (Pen Wipe) SIGNATURE A CESCRIPTION OF MCRAE! REGISTERED OWNER AGGRESS (OLDER (Mon MODEL SERIAL MANIER REGISTRATION MARX r. B DESCRIPTION OF FLOG CUSTOMER ODADHSTRATON FLORES Li ,enc.,,,c,..., i FROV TO i VA C CREW REQUIREDTOOPERATE THE ARCRAFT AND DIOUF/AM DEPARTURE DATE I DURATION PILOT I I COPILOT i I FUGHT DIGNEER L OTHER (SpooFol 0. AIRCRAFT 0055 NOT IIEET THE APPLICABLE ARVANTINMESS REGUREMENTS AS FOLLOWS g 5 g 0 • i . I •i E TNE FOLLOWING RESTRICTIONS ARE CONSGEREO PECESSARV FOR SAFE OPERATION (Um oteachormidmootwy) i g 5 g F CERMICATION • I Ant, welly mm I am me rep arm caw (or Ns gyro at me awe *end aboa ihs re alcraltamploteml web Me W.A./Waal Admen:talon in axaconce mei Mend irpe Vr•ed Slaws Cod* 4410! sag Bed Acole.aele Foyeim Aragon RspoMmo. MO Mil ire SUM ft Ma, nopooM sed e SIN AYH lighl itInat•il DATE NAME MO TITLE (NM of DEO SIGNATURE A rows Unpin one Ilirkelpo .1Conpienoo Will I4 CFR Saco -an 9I p G Stoned co Colon* FMFenn $1509 Moen whoa maw.* i N romp Armewnwo Cornice*, Ivo MARI Aaron /Ana ow Alan** w E a Guns Olmnillop Latta'''.Maas: Bi =E v, C Dec. Oramp. Protopraph. Ma (Mach...Nen Pey.wid) V I Plevan Armamom OPIEcote Nmed a Accadtros NM la CFR Baron 21.183(IN CAR (0apeuto•RAIE9 Is ri l F 4 i /DO -two Waco aid Bane Irfonirolai Owlifta in Aram EVAN Radar end Mack FMPam 337 (holm !Mon foquo0) 1 Omni Araccovess Conical. Ismod on Acconance With 1 11 CFR SKIICti 21.191(a) ICON PROCEVCO PC Loh.40,1Matt SIOIron d tertolonce. FMram $130-15 WAWA roam requivd) i F Ow maim RacaGod mMoat Rocmis FAA Fam 11304400-201IOM PrerOus EdMIS SLIPOROSed Eledmcdc Formal • POF Pops 2 d2 SDNY_GM_02756485 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243407 EFTA01328523 UNITED STATES OF AMERICA DEPORTMENT OF TRANSPORTATION • FEDERAL maATiON ADIAMSTRAPON SPECIAL AIRWORTHINESS CERTIFICATE A CATEGORY/DESIGNATION EXPERIMENTAL, PURPOSE RESEARCH & DEVELOPMENT MANU- NAME NIA'. B FACTURER ADDRESS N7A - '';'7,-...::- ".. FROM . .... ...... -. C FLIGHT TO N/A • ,- N- 405P1 SERIAL NO. 53375 D BUILDER Bell MODEL 407 DATE OF ISSUANCE 05 Jan, 20, 7 .EXPIRY 04 Feb, 20)7 OPERATING LIMITATIONS DATED 05 Jab, 2011 ' 'ARE PART OF THIS CERTIFICATE E W all /RE OF "A nffiCSENTATIvt . • s py., DESIGNATION OR OFFICE NO. Carrie Ricca -t • . ' 547098732 a Any ateretal, rep( misuse of ito certificate may be punishable Inaba not exceeding SI,C00 or imprisonment not weeding 3 yews, or WI. THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE TITLE IA, CODE OF FEDERAL REGULATIONS (CFR). : FMFgm 51*7 i0v1OmPohosi Sion 0701Ay be Utaket10~ SDNY_GM_02756486 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243408 EFTA01328524 SDNYGM02756487 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243409 EFTA01328525 Operating limitations for 14405FU U.S. Department of Transportation Bell 407, S/N 53375 Federal Aviation Administration 05 Jan 2017 1. This aircraft does not meet the airworthiness requirements specified in Annex 8 to the Convention on International Civil Aviation. Operations In civil airspace outside of the United States will require the written permission of the applicable Civil Aviation Authorities (CAA). That written permission must be carried aboard the aircraft together with the U.S. airworthiness certificate and, upon request, be made available to an FAA inspector or the CAA in the country of operation. Operations may be further restricted by the foreign CAA. This may include not allowing use of an airport, requiring specific routing, and restricting flight over specific areas. The operator must comply with any additional limitation prescribed by the CAA when operating in its airspace. (1) 2. No person may operate this aircraft for any other purpose specified on the face of the FAA Form 8130-7. These operating limitations do not provide any relief from any applicable law or regulation. This aircraft must be operated in accordance with applicable regulations and the additional limitations prescribed herein. Note that a clearance from air traffic control (ATC) is not authorization for a pilot to deviate from any rule, regulation, operating limitation, or minimum altitude, or to conduct unsafe operation of the aircraft. If ATC issues a clearance that would cause a pilot to deviate from a rule. regulation, or operating limitation, or in the pilot's opinion, would place the aircraft in jeopardy, it is the pilot's responsibility to request an amended clearance. These operating limitations are a part of FAA Form 8130-7 and are to be carried in the aircraft at all times and to be available to the pilot in command of the aircraft. (2) 3. This special airworthiness certificate and attached operating limitations are not in effect during public aircraft operations (MO). Concurrent public/civil operations are not permitted; the aircraft cannot be operated as a civil aircraft and as a public aircraft at the same time. This airworthiness certificate is not in effect during flights related to providing military services (that is. air combat maneuvering, air-to-air gunnery, target towing, electronic countermeasures simulation, cruise missile simulation, and air refueling). These activities are inherent military training activities, not civil activities. The FAA makes the distinction between the authorized flights for experimental purposes, as described in the program letter, and PAO. Before operating this aircraft under this special airworthiness certificate following a PAO, the aircraft must be returned via an approved method to the condition and configuration at the time of airworthiness certification. This action must be documented in the aircraft records. The aircraft records and entries must clearly differentiate between a civil experimental flight per this certificate and any other flights. (3) 4. Application to amend these operating limitations must be made to the local Flight Standards District Office (FSDO) or Manufacturing Inspection District Office (MIDO). (6) 5. The pilot in command of this aircraft must hold Rotorcraft category and Helicopter class certificate or privilege. The pilot in command must hold all required ratings or authorizations, and endorsements required by 14 CFR pan 61. (7) 6. The pilot in command must hold: (a) An appropriate type rating (if one has been established); or (b) An experimental aircraft authorization, by make and model, on their pilot certificate; or (c) A temporary LOA issued by an FAA Flight Standards Operations Inspector. (d) For the purpose of completing the practical test for the issuance of an experimental aircraft authorization, a qualified instructor may make a logbook endorsement permitting limited local solo operations for a period of not more than 30 days. (8) 7. When filing a flight plan, the experimental nature of this aircraft must be listed in the remarks section. (10) 8. This aircraft must not be used for towing, including, but not limited to glider towing, banner towing, target towing or towing electronic receivers or emitters. This aircraft must not be used for intentional parachute jumping. (12) Page 1 of 3 SDNY_GM_02756488 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243410 EFTA01328526 SDNYGM02756489 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243411 EFTA01328527 Operating limitations for N405PJ U.S.Department of Transportation Bell 407, S/N 53375 Federal Aviation Administration 05 Jan 2017 9. If aircraft, engine, or propeller operating limitations are exceeded outside of planned test conditions, an appropriate entry will be made in the aircraft records. (13) 10. No person may operate this aircraft unless it is maintained in accordance with an inspection program meeting the scope and content as described in 14 CFR 91.409(f). The operator must select and identify in the aircraft maintenance records, one of the following programs for the inspection of the aircraft: (1) For type certificated aircraft a current inspection program recommended by the manufacturer; or (2) For former military aircraft an inspection program recommended by the manufacturer or North Atlantic Treaty Organization (NATO) military service; or (3) An FAA-approved inspection program. Note: To extend an inspection interval, the owner/operator must submit a request for that extension with supporting documentation and data to the local FSDO and obtain concurrence from that FSDO. Inspections must be recorded in the aircraft maintenance records showing the following, or a similarly worded, statement: 1 certify that this aircraft has been inspected on (insert date) per (identify applicable inspection program] and found to be in a condition for safe operation? (14) 11. Only FAA-certificated repair stations, FAA-certificated mechanics with appropriate ratings, or a manufacturer as authorized by § 43.3 may perform inspections required by these operating limitations. (18) 12. The aircraft may not be operated unless the replacement for life-limited articles specified in the applicable technical publications pertaining to the aircraft and its articles are complied with in one of the following manners: (a) Type-Certificated Products: Replacement of life-limited parts required by § 91.409(e) applies to experimental aircraft when the required replacement times are specified in the U.S. aircraft specifications, or type certificate data sheets. (b) Non-Type-Certificated Products: All articles installed in non-type-certificated products operated under an airworthiness certificate issued for an experimental purpose, in which the manufacturer has specified limits, must include in their program an equivalent level of safety for those articles. These limits must be evaluated for their current operating environment and addressed in the approved inspection program. All articles installed in non-type-certificated products in which the manufacturer has specified limits, must include In their program an equivalent level of safety for those articles. The article must be inspected to ensure that the equivalent level of safety still renders the product in a serviceable condition for safe operation. (19) 13. For aircraft originally incorporating fatigue life recording systems, the owner/operator must maintain and use the system as prescribed by the aircraft manufacturer and comply with the manufacturer's fatigue life limits. (20) 14. Day VFR flight operations are authorized. Night flight operations are authorized if the instruments specified in § 91.205(c) are installed, operational, and maintained in accordance with the applicable requirements of part 91. Instrument flight operations are authorized if the instruments specified in § 91.205(d) are installed, operational, and maintained in accordance with the applicable requirements of part 91. The pilot in command must have a method to comply with the § 91.319(c) prohibition from operating over densely populated areas or in congested airways. All maintenance or inspection of this equipment must be recorded in the aircraft maintenance records and include the following items: date, work performed, and name and certificate number of person returning aircraft to service. (41) 15. All flights must be conducted within the geographic area described as follows (there may be areas within the geographical area that are not suitable for operation and may include ingress/egress routes). Aircraft based at the Red Bluff Municipal Airport. Aircraft must operate within the area identified on the attached Page 2 of 3 SDNY_GM_02756490 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243412 EFTA01328528 SDNYGM027564.1 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243413 EFTA01328529 Operating limitations for N405P1 U.S. Department of Transportation Bell 407, S/N 53375 Federal Aviation Administration 05 Jan 2017 sectional dated 10/10/12, while avoiding densely populated areas, and congested airways. (44) 16. Flight over a densely populated area or in a congested airway is authorized in accordance with 4 91.319(c) only for the purpose of takeoff and landing. The area on the surface described by the term "only for the purpose of takeoff and landing' is the traffic pattern. For the purpose of this limitation, the term "only for the purpose of takeoff and landing' does not allow multiple traffic patterns for operations such as training or maintenance checks. This DOES NOT restrict a go-around/rejected landing for safety reasons. When avoiding populated areas, aircraft speed and weight must be considered. The information in FAA Order 8900.1, Flight Standards Information Management System (FSIMS), regarding set-back distances from spectator areas for aviation events such as air shows or air races may assist in determining a suitable space to fly the aircraft. (46) 17. No person may be carried in this aircraft during flight unless that person is essential to the purpose of the flight. 154) arrie Ricca DAR 547098732, Seattle MIDO, NM-51 Page 3 of 3 SDNY_GM_02756492 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 002434(4 EFTA01328530 SDNYGAL02756493 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243415 EFTA01328531 REVIEWED AND ACCEPTED SAC: FSDO SDNY_GM_02756494 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243416 EFTA01328532 SDNYGM02756495 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243417 EFTA01328533 January 3s, 2017 Federal Aviation Administration Attn.: James Sprecher 1601 Lind Avenue SW Renton, WA 98057 SUBJECT: Program Letter for Special Airworthiness Certification REGISTERED OWNER: Helibro, LLC DESIGN CRITERIA: Research & Development BUILDER: Bell NUMBER OF ENGINES: I MODEL: 407 NUMBER OF SEATS: 7 SERIAL NO: 53375 REGISTRATION NO.: N405PJ Dear Mr. Sprecher: The purpose of this letter is to request a special airworthiness certificate, in the experimental category, for a Research & Development Airworthiness Certificate in accordance with Title 14 Code of Federal Regulations (14 CFR), § 21.191(a). This request is made to support company flight testing in support ofFAA Project Number ST16493LA-R. The STC will be for the installation of a Secondary Hardpoint Installation on Bell Model 206 and 407 aircraft. The proposed Flight Testing will be conducted over I — 3 hours on or around the 5th of January, 2017. We request the designee hold the Standard Airworthiness in suspension until the completion of flight testing. The aircraft will be located at PJ Helicopters facilities in Red Bluff, Ca. The aircraft is within current maintenance, has been conformed to the TCDS and the following has been accomplished: • FAA Form 8130-6, with sections I, II, and III completed is enclosed. • The aircraft has been properly registered. • We have weighed the aircraft to determine that the most forward and aft center of gravity positions are within established limits. The weight and balance report is available at the aircraft. • The marking requirements of 14 CFR Part 45 have been complied with, including permanent application of appropriate registration marks and the word "EXPERIMENTAL" near each entrance to the cabin or cockpit. • The aircraft is inspected and maintained in accordance with the Bell Helicopter Maintenance Manuals. The following is a description of the requested geographical areas for flight testing: within the box defined on the attached sectional, while avoiding densely populated areas and congested airways. I request Larrie Ricca, DARF 547098732, be delegated to issue the requested airworthiness certificate. My telephone number is: Please contact me at this number if there are any questions or if additional information is needed. Sincerely, Dave McCanunon, Director of Maintenatice Operations Helibro, LLC Page I of I SDNY_GM_02756496 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00243418 EFTA01328534 SDNYGM02756497 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243419 EFTA01328535 SDNY_GM_02756498 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243420 EFTA01328536 SDNY_GM02756499 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243421 EFTA01328537 WOO STOW/ MOISICA PIPAR1VPrt OF IAPTIPORTAIIT•eNDIPATINIUMNACINPOISTOV • SPECIAL AIRWORTHINESS CERTIFICATE CATEOCEIWOEKIIARCN EXPERIMENTAL PURPOSE RERARCIll A DEVELOPMENT , IIANU. NAVE N/A • SACILRER ADDRESS N/A I FRCSS N/A C i TO N/A D N. 405P1 SERIN. NO EULDER Bell l 407 DATE Cf ssumit-E IM, 2017 DPW a rCKNTI 7 Q_PERATINO LIM DATED ARE PART OF 1143 CERTICCAll E wo.,70.• c• ..... cesouncrom I:frit( NO R Kr NIT0911732 Any Sake ea.my a PAU* nut te Ftereetre te a Rear swede, VAN BISVIrell AM c.a." 1 ark ar teet 1149. CERTINCATE RUST Ilt OSPLAY10 N TNT APCRIAl NI 52:91ROya MTHIOWA! TOW IA COOT Ce FIEDFAM. RFOLLADOVS (MN p metro.W SONY_GM_0275650D T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 002434?? EFTA01328538 A Tit Sitinilti• Oink.lamaate OA ilitatirdniCia•IOU,laUllealitil Cat a (=WU "011ie S4 Ca d Nan RI9AakralCFR) . 11 arsatreta ant* wham.re ^YetladaW raraticolonasew as Omelet a patxdoiIran ardcak pradscknfidt awn al wool aphelia lora It portray Wife catexko Wags tante cello. 1, I Carr° omen CFMOMONCONfaitcno, Illtr r6 (2)Caryna noon natosional b Os psposa alretail ,.. 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S0NY_GM_02756501 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00243423 EFTA01328539 UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE I NATINAUTY AND 2 MANUFACTURER MO MOOS. 3 AIRCRAFT SERLS4. 4 CATEOORY REGISTRATION MARKS Bell Helicopter Textron NUMBER N40511.1 Canadi Model 407 5337$ Normal 5 AITCRITY ANOBMIS FOR ISSUANCE Riebration onto* 5 Mod pesue6 40111C4.44701.1orOss N.adle Oro dmock he aisnibutids Seta eeee sendird bedb&dmb te Pike liettkr. tut n cram b we Stem Veen b ant IS manna onto Sone caradhense SS'S alum code a pea by eaces Re Cwoverim Werratensl CM AS esat4 a roar tem EstReols • ***None"' 6 TERMS MO COMMONS • OS are sww0e44. saxeCed recktice a iimivIceIS a Minim estektel bite MAY skeethale101.1011, a ate a bi; aisle nerbaira:Faeclato =edema. Siloamn phenolInueoloone Pals 21. A ea 11dre Fein ASA es /MN eacree NedUSd SOU. DATE OF ISSUANCE _. FityPRE HT TN e 0E5IGNATION PRIMER 05 APR 2016 'an cfrekee DART710617WP alleratat rept:6410w nand en colt* tose be pfita%Wale MemetsbeS1MeiImeeenst waft /pays kit NS WarCATE VAT BE DISPLAYED PI ttE MICRIST M AnillruatE NTH Okra( FOOML Awnpazommots. FM Faze 8103-2 (04-11) Swerzetes Previous Ed.non AEN6Pititair0 o& TAA) ()(91-7 SDNY_GM_02756502 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243424 EFTA01328540 SDNYGAL02756503 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243425 EFTA01328541 Operating limitations for N4435P1 U.S. Department of Transportation Bell 407, S/N 53375 Federal Aviation Administration 05 Jan 2017 1. This aircraft does not meet the airworthiness requirements specified in Annex 8 to the/ on/vention on International Civil Aviation. Operations in civil airspace outside of the United States will equire the written permission of the applicable Civil Aviation Authorities (CAA). That written permission lust be carried aboard the aircraft together with the U.S. airworthiness certificate and, upon request, be m,de available to an FAA inspector or the CAA in the country of operation. Operations may be further restricted by the foreign CAA. This may include not allowing use of an airport, requiring specific routing, a rettricting flight over specific areas. The operator must comply with any additional limitation ores& b fie CAA when operating in its airspace. (1) 2. No person may operate this aircraft for any other purpose speci ti)i the face of the FAA Form 8130-7. These operating limitations do not provide any relief from any app is € law or regulation. This aircraft must be operated in accordance with applicable regulations and the additi al limitations prescribed herein. Note that a clearance from air traffic control (ATC) is not authorization -ei pilot to deviate from any rule, regulation, operating limitation, or minimum altitude, or to co unsafe operation of the aircraft. If ATC issues a clearance that would cause a pilot to deviate from egulation, or operating limitation, or in the pilot's opinion, would place the aircraft in jeopardy, it is th s responsibility to request an amended clearance. These operating limitations are a part of FAA Fo 30-7 and are to be carried in the aircraft at all times and to be available to the pilot in command of the air a . (2) 3. This special airworthiness certificate and attache epe ting limitations are not in effect during public aircraft operations (PAO). Concurrent public/civil o ei ions are not permitted; the aircraft cannot be operated as a civil aircraft and as a public aircraft at t same time. This airworthiness certificate is not in effect during flights related to providing military services at is, air combat maneuvering, air-to-air gunnery, target towing, electronic countermeasures simulati n, cr Ise missile simulation, and air refueling). These activities are inherent military training activities, not ci I Itivities. The FAA makes the distinction between the authorized flights for experimental purposes described in the program letter, and PAO. Before operating this aircraft under this special airwonhines ificate following a PAO, the aircraft must be returned via an approved method to the condition and c guration at the time of airworthiness certification. This action must be documented in the aircraft rec The aircraft records and entries must clearly differentiate between a civil experimental flight pe s certificate and any other flights. (3) 4. Application to amend thes %per ng limitations must be made to the local Flight Standards District Office (FSDO) or Manufacturing Inspctio trict Office (MIDO). (6) 5. The pilot in command of this ircraft must hold Rotorcraft category and Helicopter class certificate or privilege. The pilot in comma must hold all required ratings or authorizations, and endorsements required by 14 CFR part 61. (7) 6. The pilot in command ust hold: (a) An appropri e type rating (if one has been established); or (b) An expen ental aircraft authorization, by make and model, on their pilot certificate; or (c) A tempor ry WA issued by an FAA Flight Standards Operations Inspector. (d) For the urpose of completing the practical test for the issuance of an experimental aircraft authorization, a q lified instructor may make a logbook endorsement permitting limited local solo operations for a od of not more than 30 days. (8) 7. When filing4light plan, the experimental nature of this aircraft must be listed in the remarks section. (10) 8. This aircraft must not be used for towing, including, but not limited to glider towing, banner towing, target towing or towing electronic receivers or emitters. This aircraft must not be used for intentional parachute jumping. (12) Page 1 of 3 SDNY_GM_02756504 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243426 EFTA01328542 SDNY_GM02756505 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243427 EFTA01328543 Operating limitations for N4091 U.S.Department of Transportation Bell 407, S/N 53375 Federal Aviation Administration OS Jan 2017 9. If aircraft, engine, or propeller operating limitations are exceeded outside of planned t t conditions, an appropriate entry will be made in the aircraft records. (73) 10. No person may operate this aircraft unless it is maintained in accordance A, inspection program meeting the scope and content as described in 14 CFR 91.409((). The open kttust select and identify in the aircraft maintenance records, one of the following programs for the insp ti n/ of the aircraft: (1) For type certificated aircraft, a current inspection program reco ended by the manufacturer; or (2) For former military aircraft, an inspection program recomm@gded by the manufacturer or North Atlantic Treaty Organization (NATO) military service; or (3) An FAA-approved inspection program. Note: To extend an inspection interval, the owner/operir st submit a request for that extension with supporting documentation and data to the local FSDO and obt in concurrence from that FSDO. Inspections must be recorded in the aircraft maintenance record owing the following, or a similarly worded, statement: 1 certify that this aircraft has been ins on (insert date) per [identify applicable inspection program) and found to be in a condition for sa tion." (14) 11. Only FAA-certificated repair stations, FAA-certificated hanics with appropriate ratings, or a manufacturer as authorized by § 43.3 may perfor ons required by these operating limitations. (18) 12. The aircraft may not be operated unless the ment for life-limited articles specified in the applicable technical publications pertaining to the aircraft a s articles are complied with in one of the following manners: (a) Type-Certificated Products: Repla nt of life-limited parts required by § 91.409(e) applies to experimental aircraft when the required replg ment times are specified in the U.S. aircraft specifications, or type certificate data sheets. (b) Non-Type-Certificated Produces All articles installed in non-type-certificated products operated under an airworthiness certificate su r n experimental purpose, in which the manufacturer has specified limits, must include in their progr m quwalent level of safety for those articles. These limits must be evaluated for their current ()pecan g vironment and addressed in the approved inspection program. All articles installed in non-type-cercific ed products in which the manufacturer has specified limits, must include in their program an equivalent lev of safety for those articles. The article must be inspected to ensure that the equivalent level of safety still enders the product in a serviceable condition for safe operation. (19) 13. For aircraft originally inc porating fatigue life recording systems, the owner/operator must maintain and use the system as prescribe by the aircraft manufacturer and comply with the manufacturers fatigue life limits. (20) 14. Day VFR flight op ations are authorized. Night flight perations are authorized if the instruments specified in § 91.205(c) are installed, operational, and *ntained in accordance with the applicable requirements of part 91. Instrum t flight operations are authorized if the instruments specified in § 91.205(d) are installed, operational, an maintained in accordance with the applicable requirements of part 91. The pilot in command must have a shod to comply with the § 91.319(c) prohibition from operating over densely populated areas or in conger airways. All maintenance or inspection of this equipment must be recorded in the aircraft maintenanc ecords and include the following items: date, work performed, and name and certificate number of person returning aircraft to service. (41) 15. All flights must be conducted within the geographic area described as follows (there may be areas within the geographical area that are not suitable for operation and may include ingress/egress routes). Aircraft based at the Red Bluff Municipal Airport. Aircraft must operate within the area identified on the attached Page 2 of 3 SDNY_GM_02756506 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA _00243428 EFTA01328544 SDNYGM02756507 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243429 EFTA01328545 0 U.S. Department of Transportation Operating limitations for N405P1 Bell 407, S/N 53375 Federal Aviation Administration 05 Jan 2017 sectional dated 10/10/12, while avoiding densely populated areas, and congested airways. (44) 16. Flight over a densely populated area or i7 a congested airway is authorized in accordance with 5 91.319(c) only for the purpose of takeoff and la dingy' The area on the surface desp dby the term "only for the purpose of takeoff and landing" is the traffic pattern. For the purpose of this li tion, the term "only for the purpose of takeoff and landing" does not allow multiple traffic patterns fo ations such as training or maintenance checks. This DOES NOT restrict a go-around/rejected landing for ty reasons. When avoiding popular areas, aircraft speed and weight must be considered. The information in FAA Order 8900.1, Flight Standardilnformation Management System (FSIMS), regarding set-back distances from spectator areas for avi. vents such as air shows or air races may assist in determining a suitable space to fly the aircraft. (46) 17. No person may be cark n this aircraft during flight unless that person is essential to the purpose of the flight. (54) ( Larrie Ricca OAR 547098732. the MIDO, NM-51 Page 3 of 3 SDNY_GM_02756508 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243430 EFTA01328546 SDNY_GM02756509 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243431 EFTA01328547 REVIEWED AND ACCEPTED SACi FSDO SDNY_GM_02756510 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243432 EFTA01328548 SDNYGM02756511 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243433 EFTA01328549 Tcoo Ftoroct C.d'ac Truro /Anew Ort0 W 2120=20 0 MAJOR REPAIR AND ALTERATION m°7p1I 444 ?AA Use O4 of Tortcorvalcri New* (Airframe, Powerplant, Propeller, or Appliance) Minion aerravarreen INSTRUCTIONS. Pnnt or type al entries See Title 14 CFR 943.9. Part 43 Appemla B. and AC 43.91 (or subsequent revision thereof) for instructions and disposifion of an lam. This report is required by law (49 U.S.C. §44701). Failure 0 report can result in a ova penalty for each such violation. (49 U.S.C. §46301(a)) Nationality and Registration Mark Sens No. N405PJ 53375 1. Aircraft Make MOOS Series Bell Hellicopter 407 206 Warne (As shown On regiStratiOn Cernaelde) Address (As shown on regstration Ger:Scots) 401•44 Cent annoy Way 2. Owner Do Red Bluff Sr. CA Helibro. LLC. Le 96090 cons USA 3. For FAA Use Only 4. Type 6. Unit Identification Ropes Metabon Unit Make Model Serial No. ig AIRFRAME (As describedinItem I above) El . POIAERPLANT El O PROPELLER TYPO CI o APPLIANCE manta:bar 6. Conformity Statement A. Agencjs NNW and Address B. Kind of Agency Nino p I liplirrotArs inr U s condone MOON!IC I Itanoloclorer mem 903 Lumley Fortran CertfitAted Methent C. Certificate No co Red Rhin shift CA ./ Celle-mos Repay Sieben so 96080 cam, USA Caricale0 Maintenance Organ:Alan AWTR306C D. I certify that the repair and/or alteration made to the wilts) identified in Kern 5 above and described on the reverse or attachments hereto have teen made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furry:tied herein is true and correct to the best of my lino.../edge. Extended range fuel SagnatureiDate of Autiscsized Inervkluai per 14 CFR Part 43 APP. 8 Joseph Tierno 5/31/2016 P 7. Approval for Return to So ieur. irt Rada to the authoring 9 van Persons specified below. the ail identified in item 5 was nspected n the manner prescribed by the Administralor of the Federal Aviation Administration and Is p Approved • Rejected FAA Flt. Standards Peisoni 4910.114 by Camden Manufacturer Maintenance Organization Department of Transport Inspector BY Other (SNOW FM Designee 1 . Repair Sleben Inspection Authonzation Certificate or Signature/Dale of Authorized Individual Designation No. AvV7R306C Joseph Tierno 5/31/2016 C,".wc-a"----93,t, FAA Form 337 000si SDNY_GM_0275&512 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243434 EFTA01328550 NOTICE Weight and balance or operating limitation changes shall be entered in the appropnate aircraft record. An alteration must be compatible with allprevious alterations to assure continued conformity with the applicable airworthiness requirements. a. Description of Work Accomplished firmore space Is required. SA addieonal sheets Identify with aircraft nationality and regisbation mark and date work completed.) N405PJ 5/31/2016 Nationality and Registration Mark Date Aircraft Total Time: 2013.1 Serial Number. 53375 Installation of USFS required certified secondary belly hard point to provide the capability for installation of a government provided secondary external load safety retainer and safety retainer manual release. 1. Installed USFS required secondary belly hard point referencing data and installation instructions contained in Aerocraft Drawing No. ARC-407 Rev. A dated 3/31/2016 and FM form 8110-3 dated 4/1/2016. 2. Instructions for continued airworthiness to be performed referencing Aerocraft Drawing No. ARC-407 of the latest approved revision and AC 43.13-18. 3. Weight and balance and equipment list has been updated. 4. An appropriate logbook entry has been made. END O Additional Sheets Are Attached FAA Form 337 (1301) SDNY_GM_02756513 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243435 EFTA01328551 Fan, Aprow3 flank Tracione %nes OVB No 21202020 et) VS Cepsientet MAJOR REPAIR AND ALTERATION 2125,011 Pet FAA Use 001 of Triroportelon (Airframe, Powerplant, Propeller, or Appliance) Federal *Seen AdfiVilitt/a011 INSTRUCTIONS: Print or type all entries. See True 14 CFR §43.9, Part 43 Appends( B, and AC 43.94 (or subsequent revision thereon for instructions and disposition of this form. This report is required by law (49 U.S.C. §44701). False to raped can result native penalty for each such violation (49 U.S.C. §46301(a)) Nationality and Registration Mark Serial No. N405PJ 53375 I. Aircraft Make Model Series Bell Hellicopter 407 206 Name (As shown on registration corticate) Address (As shown on registranon certificate) mew AM I anolety Way 2. Owner an fted Sluff s'aN CA Hehbro. LLC. Do q60841 cevirn USA 3. For FAA Use Only A TYP• 5. Unit Identification Repair Alleratatin UM %lake Model Serial No . 0 AIRFRAME (As described In Item 1 above) . O POWERPLANT • a PROPELLER Tyra O O APPLIANCE sarnuredurin 6. Conformity Statement A Agency* Name and Address B. Kind of Agency Nn P I Helienmers Int- u S Certificated Weitanc I Manuleclurer /east 903 Lamle), Way Fetter Ceckficateo MOOS* C Certificate No. co end Bluff Slits flA I Ceilecalipd Row SIMOn be 96080 o...,, USA ceetaeo MomenanceOpnization AWTR306C D. leerily that the repair andrcr alteration made to the unit( ) klentilled on Item 5 above and described on the reverse or enactments hereto have been made in accordance with the requirements of Pan 43 of the U.S. Federal Amation Revisions and that the information furnished herein is true and correct to the best of my knowledge. Extended range fuel Signature/Date of nutnicetzeO Ino vid nal PJH per 14 CFR Part 43 El App 8 Wesley Clark 6/1/2016 910 7. Approval for Return to Service Pursuant to the audio* given persons specified below, the um identified In Item was inspected it the manner Pfesned by Rya Administrator of the Federal Avlabon Administration and is WA Approved O Rejected FM Flt. Standards Persons Approved by Canaan Manufacturer Maintenance Organization Near:mentor TranSped Inspector BY Other (SPeCifY) FM Designee I Repair Station Inspection Authorization Certifiate or SignaturerOale of AUVIOriZed 11101VIdlial Designation No. pii -i AWTR306C Joseph Tierno 6/1/2016 .5 -.a___ -__,s25 FAA Form 337(agei SONY_GM_02756514 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243436 EFTA01328552 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. D. Description of Work Accomplished (amore space is required attach additional sheets. Identity wan aircraft nationality and registrat.on mark and date work completed) N405PJ 6/1/2016 Nationally and Registration Mark Date Aircraft Total Time: 2013.1 Serial Number: 53375 Installation of Aeronautical Accessories, Inc. Collective Safety Cover STCe SH2373S0. 1. Installed Aeronautical Accessories Collective Safety Cover P/N 407-929-001 referencing report number AA-96162 revision A. 2. There are no instructions for continued airworthiness provided with the MI Collective Safety Cover. 3. Weight and balance and equipment list has been updated. 4. An appropriate logbook entry has been made. --------END O Adcklional Sheets No Attached FAA Form 337 ilea) SDNYGtvl _02756515 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243437 EFTA01328553 Form Popped Electronic Tradong Number melt 120.0020 0 MAJOR REPAIR AND ALTERATION ii 7 u 5 Cepannwt or twee.. S (Airframe, Powerplant, Propeller, or Appliance) for FAA Use Only Vee Mian adeetioreaen INSTRUCTIONS Print or type ail muses See FAR 43.0, FAR 43 Apperdw B. and AC 43.91 (or subsequent revision TOMO fOr InSbV0303$ and discosiboo et Was km. This report is re,ured bylaw (49 U.S.C. 1421) Failure to Med Can resit in • mil Nat/ nit batted SIND for eels such Relation (Section 901 Federal Aviation Act 10ST NOTnallY and Re904rabon Mark Serial No. N405PJ 53375 1. Aircraft Mike Model Senes Bell 407 Nan* (As Sheen on registration certificate) Address (A7 shown on tegstraton awaken, ) Helibro LLC. weee903 Langley Way 2. Owner cuRed Bluff seeCA ze96080 Conn USA 3. For FAA Use Only The data identified tieren complies with me appicarte airworthiness moderns:nes and is approved only fo• the aberce &Mated arcairt. subject to confornuty insoection Tap/money. - 'Ism n 43 7 62,06 . 'XAN St" 4. Type 5. Unit ideritillcatIon FITTS Alteration Um Make Mx* Serial Number . C.1 AIRFRAME (As deserted in Rem 1 Stove) POWERPLANT 0 O . PROPELLER . T,st El El APPLIANCE vw,rtwrww 6. Conformity Statement A Agency's Name and Address 0 Kind of Agency ew.P.J. Helicopters. Inc O V S Certer-attAl Mechanic O Manufacturer stausu.903 I anoley Way O Fortson Cerlthealed Mechanic C Certficate No ceFted Bluff seecS Cill Certificated Repair Mason AWTR306C zo96080 Courwyl-ISS O Certificated mantenance Organizaton D I Del* that the repair snot« afternoon made to the unn(s) Klettbd n nem 5 above and descnted on the reverse or attachments hereto have been made in accordance*. the repurernentS of Pact 43 of the U.S Federal Aviation RegLiaxen and that the nternation furnished herein Is true and correct to tne east of my army/sedge EXIMIlld range TM SignatureDate of Aultoontied trimneval Per 14 CFR Part 43 Apra O Derek Spooner r .02 . ,...... i .57strfid. PJ0I 850 7. Approval for Return to Senile* Pinuant to me authority given persons maned bestow. the unit identified n item 5 was inspected in the manner pewit. by to Actnintstrabtx ea the Federal Aviation Adminsnttn and is I2TAPPROVED . REJECTED FAA Fit Standards Person Approved by Caned. Marniacturer Mentenance Organgabsa Department of Transport Inspector BY Other apart FAA Pawnee ,( Repair Station Inspeotan Autionzation Cortificele or Desbnanon No. Sign ture(Date of Autixerred Indrnduel PJ§.0 Awrie304,e - .... (,...—_ .s-isttrin, arjk FAA Form 337 11006; SDNY_OM_02756.516 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243438 EFTA01328554 NOTICE Weight and balance o operating limitation changes shall Do *Mewl in the appropriate aircraft record An iteration must De compatible with an previous alterations to assure continued conformity with the applicable airworthiness requirements 8. Description of Work Accomplished Of more space is required. attach additional shoots Identify with aircraft nationality and registration mark and date work completed) N405PJ 5-4747:74/6 Nationality and Registration Mark Date ACFT TOTAL TIME: 2013 I ACFT Si: 53375 Installed Audio Panel, 2 FM Transceivers, Aux FM provisions, Portable Electronic Device provisions. External Public Address (PA) provisions and Remote Hook provisions to satisfy Forest Service contract requirements. 1.) Mounted Dzus Bracket P/N TA05-001 in upper center slant panel with "Mr hardware. Installed AEM/NAT AMS44 Audio Panel into Dzus bracket All wiring previously installed with connectors re-terminated. Power is supplied from avionics bun through existmg 3A Circuit Breaker PIN MS26574-3 placarded 'ICS Audio'. 2.) Mounted Dzus Rail P/N PR35 in center slant panel with 'Mr hardware. Installed 2 NAT NPX136D FM Transceivers into Dzus Rail. Mounted FM 1 Antenna P/NC1293-3 on two aircraft belly in existing antenna location using "Mr hardware. FM 2 Antenna previously installed on upper forward cowling. All single conductor wiring M22759116 seres. All shielded wire M27500 series Coax RG-400 Power to each FM Transceiver is supplied from avionics buss through 3A Circuit Breakers PIN M526574-3 placarded TM I' and TM T.. 3.) Mounted NAT Radio Interface P/N AA34-300 under copilot seat, with 202473x:04r aluminum bracket. alodined and primered Mounted Conant Antenna CI293-3 to aft belly of aircraft, with 2024T3x.032' aluminum doubler alodined and petered. Antenna replaces existing unused. Mounted MS3112E12-IOS Connector to LM side of center console and placarded "AUX FM". Mounted 225398-1 BNC Female Connector to 1/H side of center console and placarded 'AUX FM ANT. Radio Interface system power supplied from avionics buss through IA Circuit Breaker P/N M526574-1 on overhead panel placarded 'AUX FM'. 4.) Mounted RAM bracket assemby P/N RAM-8-202U to instrument glarehield using 2024T3x.050' aluminum doubler. alodined and painted. Doubler secured to glareshield with "MS hardware. Power is provided to the above bracket from the avionics bun through a 5A circuit breaker P/N MS26574-5 on the circuit breaker panel placarded "PED". All wiring M22759116 series. Installed placard below RAM bracket that reads *GPS LIMITED TO VFR USE ONLY'. Performed static load test for I lb. PED and determined acceptable. referencing AC43.13-2B. Chapter 1. Use of any portable electronic devices aboard the aircraft may be prohibited by FAR 91 21. The determination of the affect of any particular portable electronic device may be made by the operator and/or the pilot in command in accordance with 91.21, and Advisory Circular AC 91.21.18. 5.) Mounted AEWNAT AA22 PA Controller in lower avionics console. Controller secured with existing dzus rail Controller power suppled from avionics buss through IA Circuit Breaker P/N 7274.2.1, placarded "PA CONT. Controller wired through PA position on existing audio panel Mounted AEM LSA400 PA Amplifier behind hatred( Amplifier seared with "MS" hardware to 2024T3x 040" aluminum doubler alodined and painted Amplifier power supplied from avionics buss through 20A Circuit Breaker PIN 7274-2-20. placarded 'PA AMP". Wring for speaker capped and slowed under pilot seat All single conductor wiring M22759/16 series. shielded wiring M27500 series. 6.) installed Remote Hook Provisions. Mounted Remote Hook Relay P/N MS24166-D1 under pilot seat with 'Mr hardware and previously installed bracket. Mounted Remote Hook Switch P/N P340185-2 on plot collective control head using 20241'3 aluminum bracket, alodined and painted. Switch placarded 'Remote Haar Mounted Connector P/N 97-3101A-24-11A on aircraft belly. Remote Hook system power supplied from main buss through 50A Circuit Breaker P/N W23-50. located overhead. placarded Remote Hook". Single conductor wires M22759/t0 series used. Ae work accomplished referencing AC43.13-I B chapter 11 and 12. section I & 2: NAT AMS44 Installation and Operation Manual SM19 rev. 4.00 dated November 2003: NAT NPXI36D Installation and Operation Manual SM68 rev. 4.00 dated February 2005: NAT AA34 Installation Manual S1436 issue 4.01 dated January 2010. AEM AA22 Instatabon and Operation Manual SM33-2 rev 2.1 dated May 2013: AEM LSA400 Installation and Operation Manual rev. 1 dated October 2014. Forest Service Drawing FS/OAS-17: AC 20'138c appendix 5: and Bell Standards Practices Manual Biff-AU.-SPM rev. 4 dated June 2011. Performed Ground functional test IAW manufacturers installation manual procedures that determined the operations and functions of existing systems and components previously installed are not adversely affected by this alteration. An electrical load analysis has been computed and it has been determined that the electrical load does not exceed 80% of the rated generator capacity. The aircratts weight and balance was computed. This equipment was found not to exceed the guidelines in FAA Rolorcaft Directorate poky letter ASW-2001.4. dated April 25. 2003 for FADEC controlled aircraft and is considered to be 'equipment not known to have potential for interference'. CONTINUED AIRWORTHINESS: Requires operational checks and visual inspections per FAR part 43 Appendix D annually. Reference manufacturers publications. ••• END 0 Additional Sheets Are Attached FAA Form 337 titian . SDNY_GM_02756517 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243439 EFTA01328555 ranmowed EIKInfle Trad;a9Mite deans memo fllibr MAJOR REPAIR AND ALTERATION M12011 US 3malmeri F.:ea.Use they a Transcorunco (Airframe, Powerplant, Propeller, or Appliance) Rani Amnon Arrestrason INSTRUCTIONS: Pont or type all entnes. Sec True 14 CFR §43.9. Part 43 Appendix 8. and AC 43.9-1 (or subsequent revision thereon for instructions and disposition of this form. This report is required by law (49 U.S.C. §44701). Failure o report can result nacho& penally for each such violation. (49 U.S.0 §46301(a)) Nana-law and Registration Mark Swat No. N405PJ 53375 I. Aircraft Make Series mods Bell 407 206 Name (As shown on registration certificate) Address (As shown on registration certificate) MOWS MI 1 angler), Way 2. Owner Ces Red Bluff owe CA Helibro. LLD. iv 960FID corm USA 3. For FAA Use 0 ly 4. Type S. Unit Identification Repair Alteration Unit Make Model Serial No. • n AIRFRAME (As describedin mem 1 aeon) O II POVVERPLANT O NI PROPELLER Type • APPLIANCE uarwlsaint • 6. Conformity Statement A. Agencys Name and Address B. Kind Of Agency Sr.. Is 1 Hawn/mom Ine u 5 Corsficated Mechanic ll Manufacture tae... 903 Langley Way Foreign Cerebrated Mechanc C. Certificate No. ce Red Muff 610* CA I Certrnana RePes Simon as 96080 -ow USA co unrested Mentenenee Cagenaatten AVVTR306C D Really that the repair and/or alteration made to the Unit( ) Identified in item 5 above and described on he reverse or attachments hereto have been made in accordance vnth the reetarements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnshed herein is true and correct to the best or my knowledge. Extended range fuel Signature/Date of Authorized Individual per la CFR Part 43 O NH NH APP. 8 Derek Spooner 5/19/2016 850 7. Approval for Return to &Wk. Pursuant to the authority given persons speofied belOw. the unit identified In kern 5 was nspected in the miner prescribed by the Admvistrator of the Federal Aviation Administration and n e APProved O Rejected FAA FR. Standards Persons Approves by Ceneclen Manufactwe Maintenance Organization Deparlrnent Of TIIM$0011 inspector BY Omer (SPeolY) FAA Designee 1 Repair Station Inspection Authortzahon Certificate or Signature/Date of Authors ed Indondual Domination No - ...-,-.. ....._ RON AWTR3OSC Derek Spooner 5/19/2016 RSO FAA Form 337 now, SDNY_Gfil_02756518 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243440 EFTA01328556 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with as previous alterations to assure continued conformity with the applicable airworthiness requirements. B. Description of Work Accomplished tit mole space h required. attach additional sheets. Identity mtn secret nationally and registration mark and date work completed) N405RJ Nationality and Registration Mark 1 5/192016 Date Aircraft Total Time: 2013.1 Serial Number: 53375 Installation of Skye Avionics LTD. Audible Check Engine Instrument Alert System STC # SR03008NY. 1. Installed Skye Avionics Audible Check Engine Instrument Alert System referencing Skye Avionics Installation Instructions document AER-2011-007, Rev. B. 2. Instructions for continued airworthiness to be performed referencing Skye Avionics ICA for the Audible Check Engine Instrument Alert System document AER-2011.008 of the latest approved revision. 3. Inserted Skye Avionics flight manual supplement for the Model 407 with ACIAS document AER-FMS-023 Rev. 1 into the aircraft flight manual. 4. Aircraft weight and balance and equipment list has been updated. 5. An appropriate logbook entry has been made. END Addloonal Sheets Ate Attached FAA Form 337 (mai SDNY_GM_02756519 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243441 EFTA01328557 FAA FORM 8130-6, APPLICATION FOR U.S. AIRWORTHINESS CERTIFICATE Rim Appeared 0.M.9. No. 2120-0018 Fipiratiem Dale 02/282013 11 APPLICATION FOR INSTRUCTIONS - RIO Or NW Oa no. vow In %DM wen: Rana M4 FAA u5 Moo es Tremolo% U.S. AIRWORTHINESS uee enly. SAM OHM dray IA an Salweved FM Reponlehe. N GOSH Wm, M NON& use Meclort For sway lloy NAN% complale Solana Fetal Ariake AdmInhosalea CERTIFICATE R. W. and w as NOON. I REGISTRATION MARK 2 AIRCRAFT BUILDERS IWO Now a AIRCRAFT MODEL MIGRATION 4. YR. MFR. FAA C006.43 L AIRCRAFT N405PJ eel 407 1999 S. AIRCRAFT SEPAL IC 6 ENGINE OUILGERS NAVE Waal 7 ENCASE Opel DESIGNATION 0ISCIIPTON 53375 Roils Royce C-478 I HOER CF OOKIES E. PROPELLER WEBERS POE mw 10. WOOLEN MOON OESIGNATION I 11. AVICRAFI Raw 1 wasp) One WA WA ,11 PPM APW1CATION IS NE RE Or MADE FOR tom marimad I A I i STMCARDAwACOMIESSCERTFICATEnemmema Ii l i me` I I tal.' I Pam II Il ....t. .1 I a.. " n "' an I fr es. 0 SPECIAL AOMORI reNESS CERTIFICATE /Ow answ4444.4 7 PRIMARY 0 UGHTSPORT A...or I I So I II PorParach.te I PAINNEMICOM I ION I j OW ra AS 1 OTTO 1 CIASS1 5 PROvISICAMI. ASO 2 COSI IL Cu MUM.. REQUESTED I AGIFOCLETURE NO PEST CONTROL 2 0 AERIAL SURREY 3 14 AERIAL AOVERISC a RESTRICTED Hem varew44 4 FOREST ow eawor S PATROXIN3 6 %FATHER CONTROL Hie essa.0 0 OTHER MN*, 1 RESEARCH MOCIEVELOPHENT 2 AMATEUR MT 3 EXOTICA' a NA RACING 5 CREW TWANG IS MARKET SURVEY 0 TO SHOW COMPUNCE WITH THE CSR 7 OPERATING prawn Casey KR WILT AIRCRAFT OA Iwo son woo on ainvalwas MOM 4 de ra me II 1031 EAPt %RENTAL "ewe %mono) a se a.a.a—C II CREAMING BB COO Liclu-Scol wane LICHTNTORT IC ONO IONSPAI MOW WO/ ONO WOW., 401420171odOss MEM Wider 621.1W VIIIANNED OA RESEARCH ANO 0EvElOPMENT I IC rICREwTRAIINN A AIRCRAFT TM MARKET ONO I FERRY FLIGHT FOR RENON, ALTERATICHS.MOINANCE. OR STORAGE SPOON. Mart PERO Ram 2 EVACUATE FROM AREA OF IIIPENTODANGER a ••••11001110INOSINL•11011.1.11, OPERATION IN EXCESS OF 14041111111 OIRTIFCATED TAKEOFF WEIGHT 1•0•• Me I* MP dillaiii• MIR 3 4 OEUWRIKE OR EXPORTING .LS A_I PROCIUCTON RICO TWO 0 015TCHERDEOSTRATICN FLIGHTS CI 0 WATIPtE ovicarenoss CERT1FC.ATE Owe ode .maramawimrem Mote mast Nosy A REGISTERED OWNER (44 04%on wafts 0.40•Ampleta/N IF DEALER. DECK NOTE i I Nme MCNEES HOMO. LIC 903 La-rgley Way Red Blutt CA 96080 0 AIRCRAFT CERUFICATON BASIS wwwireem Dew me Num* Nur re reveal HRCRAFT SPEOFICATION OR TIRE CERTIFICATE SAM SHEET pm ru w, MCMORT111115$ PRECTNES Want de esieni.A0.a crInee a as/0••••••••• i Am• m mu I no 64.% stoRncref 444646 a ....444.% a 44 ow des 04•44caro 2016-04 AIRCRAFT LOOK tow•ron.Nertu SLOREVENTAL TYPE CERTIFICATE (LinotOre Woe SIC ii••••64.0 5 I See snitched a i C FOOT OPERATIONNO MANTERANCE RECORDS CHECK IF RECCROBIN TOTAL 0.4101MIN TOAS EXPERIMENTAL ONLY Or ram arnamararmeamme i Id COMANCE NTH 3 ram. 14 ca m NOW191 417 2013.1 III D. CERTIFICATION .1 NNW NO Mal 1 an Me ONO ma (or Na Ho WM *on 44400.0 Com CM ER OM is 0.104.1461 .IN IR FORS A•41.101 ' W. 00:0.4•4040411. Ts 49 0 Me Ursa Ors Cede 441101Elo CM opium@ FOCIIII M4111011 ftnit03011.Irid POI M MM'S hOS bon bapecepti MAMBO WIN wohno MOM NOON COATE OF APPUCATION NAME NC TIRE %Scots/ SIGNATURE . 400016 David McCarnmon Director of maintenance °parallax _ I i is I Iz„,,,c„,,,t,....srmo„.......... A THE MOWN CISCO° ABOVE WS BEEN INSPECTEDAND FOUND AIRWORTHY By: (caftwas..4 ram ar, II CM st/I21.141Mentea) 2 us CFR zi121 CIATITICATE Otero. I 1 I CERTIFICATED Ci;red 4A Oft talor. an lig g. 5 avedAvT IWWW0TURFA Me Y••••riel OATE ythi2016 TITLE P ada of Maintenance Operatarts SIONATURE David McCarnmon if*/ Nom ALL 00.4.1400 WA...0) THE CERTIFICATE REQUESTED AIMSINK am amen eremterm $4d0n MI 01448 RION•0 61 6 RI 4 Pli MEMNON CR IROOFCATION OF CURRENT MOVORTHINESSCERTinCATE V. FAA El amPHoldr a sPaolaSEN moot H FM OFECTOR FM DESIGNEE SNOW VII I ju CM pen 12101136 1 REPRESENTATIVE von ocoducled IN CERTIFICATE OZER UNDER OVA pales CFR part 1% I14 OATS MOO/FE00 FM INSPECTORS SIGNATURE a DESIGNEE, FM WSPECIONS CEITIOATO FILE RELE72.ii r e , I , GERMINATOR OFFICE ...MATuRE„Ip ins, MOMIVRE i ai 40 7t &Kasai's . 45.11PR2P( 64 C• PS° ° ONdr 1 • 0 41140 • age/dta• ALAIEI FM Form 1304 (04.201 ) N PreVaa Edelen. Superseded Elea** Foal .PCM Page IR 2 SONY_OM_02768520 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243442 EFTA01328558 SDNYGNI02756521 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243443 EFTA01328559 A. MANSACT UREA NAME ACCRESS IF i S. PRCOJCTION BASS (CAMPS Featt PRODUCTION CERTIFICATE On poloolos Oftiler• a..*. TYPE CERTIFICATE !I --I OTNER C GIVE OUINTITT OF CERTERCAT ES RIOUIRCO FOR OPERATING NEEOS DATE OF APPLICATION NAVE Ate TITLE (PIW a Eva SIGNATURE A DESCRIPTION°, NRCRAFT REGMTEREOCNANER Ai:CRESS MAZER NOW WOEI. SERIAL NUMBER REGISTRATION MARK i.. B DESCRIPTION OF FLIGHT CUSTOMER DEMONSTRATION WOOS ri fence nroceme e FROM TO g VIA DEPARTURE DATE CORRUPT i C CREW REOUTRE J O OPERATE 11TE AIRCRAFT APO ITS EOUIPTIEKT i PILOT I COPILOT I I FLIGHT ENGINEER 1 IFOTHER/Spso81 1 O. THE MRCRAFT DOES NOT MEET DC APPUCABLE AMIWORTIONESS REQUIREMENTS AS COLLOR'S $ 1 0 i I ETRE FOLLOWNGResTmenons ARE CONSCEREO NECESSARY FOR SAFE OPERATIC*. alat eacintent art.:NSW • i1 i S F. CEPTIFKATION • I hiclity MST OW I an Pe legaletedoar Mc Ns wed Me IMMO *WSW Opt NI in* GralirS MUSS, well Vie FORM" ALUOM A... .n 110:0,11.11eel Tile 03 Mu USW SAMOS 0)00 44101ELSE AM IfOloitle Federal AOSTA Rigalka TMINT Pt le teen Memo M NNW* PsINN detaIten DATE NAME AND TITLE (PANOf eft yONATURE ma v e4 ODIPTION; UMW!" SP Mate. In CangeWem Win 11CFR San El 9. G Sweeny.* CaVoiny. FAA Fri 81304 Mame el,* MOIRCI AT APLAPSOO it Comp ArecAnness Calico."' I fowlA*31R I (Arad. nee sem•TO S Cat OperainE Omen Aeadr4 .-- I ReMous NtecelNness Colacme lowed *Accord's WM I I i C COTO. DURSO.. PNROWIONF. etc Mack wee AN•001) 14 TYR Stow CAR fOOMEMAIOTOO) %,/ 0 Cum" VIII MM Balereelnlonnatka Amiable a AnTeR I I //WWI ANALOTPuig CRIIrmt• ?NAM In Aoxotince NM S E WNW Rear one Montan FAA In 337 Mem so IS , * 14 CfR Seam a , . TB 3 ( a ) row/ meow /F. Tim repeclen Mewled n Meal Recods K Ute•SCOI Anne &nowt S Carehence. FM Fan 513015 (AIWA when , eqemec) g FM Ron 01304 101.2011)All Previous Same &mem&Mel Electranc Fame .POP Peee2e/ 2 SDNY_GM_02756522 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243444 EFTA01328560 SDNYGM02756523 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243445 EFTA01328561 UNTIED SLOES O AMER/C4 ORTATION-FEDERAL AVIA TION ADMINISTRATION DEPARTMENT OF TRANSP RTIFICATE CATEGORY STANDARD AIR WORTHINESS CE MO M 3 AIRCRAFT SERW URER ANO 2 IIMAJFACT NUIISER Bell Helicopter Textron I tMMNMTFIRYNW REWSTRATION NARKS 53375 Normal N405PJ Canada Model 007 MANGE d•wra IN utot MIMORITY 08•313 FOR IIIRWIdp•IDNUDUSC FUN+ at WenIV,IRAN Cale n's. vete, Ole DISS•0/0110MOSCIII cat* b to cetfo i *warm M nco•Sien talo Am:tab the 1md to wrtrlut, coed Fisowee4 by NW holmiiptOFOFF4 trati•govt.'s* allSal Flemb•Wernagessett tiOn a to ••• S CM M•la atwi Caritha enMIS Deeps ***None*** lothellireitmei TERMS MC COMITIONS ammo tatiOld W to FM, ed,rrctot x a •••••tal 4as IF ax•oectsbPs21. 4 sif Ultss woe surentesl moni ad *ala s anw kesl y& pcp t nyrkno• 15 ARM alRID t seam nworotte rdDutra a AMMO to Owl Sian DESIGKKOON WibER t' dthFowlhawRtglaeas. r FM 4so ITVE DATE OF ISSUANCE Da til 0617WP Thpa tora 2016 ,*Slitalic 05 APR ntike McceWaes elmar, StallallromdFO 110•06•01Fola kO, ariota log h,* AND/4. ?macaw t*Fil ILE FEOCIAL OWENREM E wiw OPIW TION NE WONT M ACC:MINC MISCOITFICAIE MATIf %RA Ha. 4I) &am ide* Pint as FM faunPO:FM. • SDN,Y_GM_2756524 7, 8, 9, 10 R PARAGRAPHS SUBJECT TO PROTECTIVE ORDE 15,0 and 17 EFTA 00243446 EFTA01328562 SDNYGM02756525 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243447 EFTA01328563 Fare saw., Ouvene NomNaar owe b maxim 0 MAJOR REPAIR AND ALTERATION mom'. lierIAAtinOner a rneweausen (Airframe, Powerplant, Propeller, or Appliance) WWI. AMON" Aritainkineeil INSTRUCTIONS: Print o type all entries. See Title 14 CFR 443.9. Part 43 Appendix B. and AC 43.94 (or subsequent revision thereof) for instructions and disposition of this form. This report Is required by law (49 U.S.C. §44701). Failure o report can result in a civil penalty for each such violation (49 U.S.C. §46301(a)) Nationality and Registration Mark Sera/ No. N405PJ 53375 1. Aircraft make Series Model Bell 407 206 Name (As shown on regisfratiOn certificate) AddleSs (AS Shown on registration certificate) mesa oat I 'Ivey Way 2. Owner chi Red Bluff sun CA Helibro LLC. Ito WOW Coal, uni teglianatspeara 3. For FAA Use Only 4. Type S. Unit Identification Repair Alteration lira Make M00M Serial No. O 0 AIRFRAME (As descnbeci in Item I above) O O POWERPLANT E M PROPELLER Type il • APPLIANCE mardacturer 6. Conformity Statement A. Agencies Name and Address B. Kind of Agency " 0” PJ Heifienntine toe U 5 Cennicaue Mectionc I Manure:luny Pent 903 Langley Way Forego Certificated Mechanic C. Cantata No. ow Red Bluff Sin; r.A / COMICated Repair Station ria 96080 ce.my United Stales of America construe( Maintenance 0igaraaban AVVTR306C D. I certify that the repair and/or Maranon made to the urel(s) identified in item 5 above and described on the reverse or attachments nereio have been made in accordance with the requirements of Part 43 of the U S. Federal Aviation RegultdienS and that the information furnished herein is true and coned to the best of my kn0wledge. Extended range fuel Signaturetate of Authorized Individual per 14 CFR Part 43 In Pill Awe Konrad Paul 4/5/2016 ....--0'4 .... -- `1:2- 925 7. Approval for Return to Service Pursuant to the authority g van persons specified below. the unit identified in ACM 5 was inspected in tne manner prescribed by the Administrator of the Federal Aviation AdMiniStratiOn and is p Approved O Rejected FAA Flt. Standards Persons Aoeewed by Cenadien Impede( Manufacturer Maintenance Organization Department or Transpixl BY Other (Specny) FAA Chnignee 1/ Repair Station inspection Authorization Ceniicate or Designation NO. Signature/Date of AL4hon eel Indivdual PJH _AWTR306C Konrad Paul 415/2016 ... - "re-- --- 925 FM Form 337 heart SDNY_GM_02756526 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243448 EFTA01328564 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. M alteration must be compatible with all previous flotations to assure continued conformity with the applicable airworthiness requirements. S. DescripUon of Work Accomplished (amore space is required, attach addibsnai sheets. Wen* mlh aircraft nahOriany add regatillion mark and date worn completed) N405PJ 4/5/2016 Naticriaraty and Remstralion Mark Oale Aircraft Total Time: 2013.1 Serial Number: 53375 Verified equipment that was previously installed while the aircraft was outside the United States: 1. Aeronautical Accessories Tail Rotor Pedal Lockout Kit STC #SR00513AT. 2. Aeronautical Accessories Flitestep Kit SIC tiSH1322S0. 3. Aeronautical Accessories Replacement Crosstubes For Low and High Skid Gear STC OSR0933ORC. 4. Aeronautical Accessories High Visability Door Kit STC ftSR09376RC-D. 5. Onboard Systems Cargo Hook Suspension System STC #SR01943SE. 6. Dart Aerospace Cargo Mirror STC #SH1031NE. 7. Dart Aerospace Quick Release Heli-Utility Basket & Quick Release Heli-Access-Step STC #SR02996NY. 8. Bristol Aerospace Wire Strike Protection System STC #SR00975AT. 9. Dart Aerospace Interior Trim Panels SIC #SR02726NY. 10. Aeronautical Accessories Skid Tubes STC #SR01697AT 11. Donaldson Filtration Solutions Inlet Barrier Filter System STC HSR09368RC. Instructions for continued airworthiness to be done referencing the applicable STC holders ICA. The appropriate flight manual supplements have been installed in the aircraft flight manual. END Adddlonal Sheets Are Aflached FAA Form 337 mos) SDNY_Givl_02756527 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243449 EFTA01328565 Fern Apnoea ereeirole Tricionp Nall Cede R0 11204020 09' 2.2•201r USe Doernot MAJOR REPAIR AND ALTERATION her IAA Use Only of Trresteraten (Airframe, Powerplant, Propeller, or Appliance) Fedetal Avitio* Aerenharanea INSTRUCTIONS: Print or ripe all entries. See Title 14 CFR §43.9. Part 43 Appendix B. and AC 43.9-1 (or subsequent reviver, thereoh for instructions and disposition of ths Man. This moon is required by law (49 U.S.C. §44701). Failure to report can result in a civil penalty for each such violation. (49 U.S.O. §46301(a)) Nationality and Regisualion Mark Serial No. N491GM 53375 I. Aircraft make Model Series BELL HELICOPTER TEXTRON 407 Name (As shown on regiStrehOn CeitifiCete) Address (As shown on reputation certifiCefi) Address ink Frit II K on 2. Owner co WLMINGTON sirs Lig AIR GHISLAINE, INC zo 19803 Caen li S A 3. For FAA Use Only 4. Type 6. Unit Identification Repair AlteratiOn una make Model Serial No. O gi AIRFRAME (Asdescribed in Rem 1above) O Ei POINERPtANT . O PROPELLER Tye* O O APPLIANCE manufacturer 6. Conformity Statement A. Agency's Name and Address 8. Kind of Agency keno pnvveRns R(ITORCRAFT ON IITIONS INC. U. S. Csnieraies siemens 1 Ilrienureeturer Aron 2011 S. PERIMETER ROAD, SUITE L Forego Cerbfirated Methane C. Certificate No. an FT I AIIDFRDALE sea. Fl °Rim i c•nreao Repair Steven ae 33309 Cooly U.S.A. Certicarecimainterne Orgargtallan 1E9R960Y D. I certify that the repair sear alteration made to the tine( ) Identified in item 5 above and described on the reverse or attachments hereto have been made In accordance wilh the rechirements of Part 43 of the U.S. Federal AVIatIOA Regulations and that the information perished herein is true and correct 10 the best of my knowledge. Extended range fuel Signature/Date of Authonzed Incliv4uat per 14 CFR Part 43 O AC9. 8 June 13th, 2011 ,C-3;rf- ir. 7. Approval for Return to Service Pursuant to the authority given persons specified below. the unit identified in fern 5 was inspected In the manner presumed by the Adnunrstralor of the Federal Aviation Administration and Is Approved a ll Rejected FM Fs Standards Me r Maintenance Organization Persons Popeyed by Cene00n auffaCtUes Deparwirmt or TronspOel inspector BY Caner (Specify) FM Designee I Repair Station Inspection Autlyrization Ceni tate or SignatureMate or Auttaxl ed Individual Designation No. 1E9R960Y June 13th, 2011 FAA Form 337num SDNY_GM_02758528 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243450 EFTA01328566 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. S. Description of Work Accomplished (if more space is required. mach additional sherds. Identify wan aircraft naeonahty andregistration mark and date work completed.) N491GM June 13.2011 Nationality and Registration Mark Date Aircraft Total Time; 791.0 hours. Removed Standard Skid Gear and Installed Bell Helicopter Textron Emergency Floatation System Kit Number 407.706-008-101; Serial Number BP-40 in accordance with BHT-407-II-1. Electrical provisions previously installed. Weight and balance data updated and entered into aircraft flight manual. Flight manual supplement BHT-407-FMS-1 entered into aircraft flight manual. Aircraft equipment list updated and entered into aircraft flight manual. Electrical data not affected. ----•-••-------- O Additional Rhea Are Attached FAA Form 337 Roos) SDNY_GM_02756529 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243451 EFTA01328567 Few Amovio Electronic tracking Number MAJOR REPAIR AND ALTERATION CM No 21204020 0 inOCCO? u.6 ithweise at (Airframe, Powerplant, Propeller, or Appliance) Temputami Foe FAA Use Only thews wawa hesnteirs444 INSTRUCTIONS: Pow CF type all tables See FAR Me FAR 43 Appendix B. and AC 43.9-1 (or supsequent wreath mewl) tor instrucsons and ithipleited Of OW IOW. This tepee is required try Me (49 U.S.0 1421) Failure lo report can result Mame penally natio exceed 3000 for each such Idabel Ithlthica 901 Federal Mason Ad WA Nthonakty end Regelraten Mark SM. NO N491GM 53375 1. Aircraft Make Modal Series BELL HELICOPTER TEXTRON 407 mime (As shawl on registrebon oirShrees) Ackliells (AS Shown on repented certh9Cess) AIR GHISLAINE INC meee•103 FOULK RD 2 Ovmer ce,,WILMINGTON miseig z. 19803 CeerriUSA 3. For FAA Yee Only 4. Type IL UMIdentekatIon Repair Maratha Unit Make Model Sane Number O El AIRFRAME (As *screedin Item I *On) O POWERPLANT 0 O PROPELLER O Tye O O APPLIANCE thwiladve 6 Conformity State/net A. Agency's Name and Address B A rcl cmigther NnEDWARDS AND ASSOCIATES INC CI LI S Certificated Mechanic 0 Ithanutacturer 444.442011 S. PFRIMFTER ROAD SUITE L 0 Foreign Certeciated Mechamc C Certificate No cA.FT. LAUDERDALE sioeFLORIDA CE3 Certificated Repair Station 1E9R960Y zo33309 co.royLISA 0 CarlificaNd Maintenance Organizalion D It:nem* mews( ander( alteration made vi me un4(s) dentified in item S above and detailed on ine reverse or altachineMs WPC have been nude el accordance net me regime-menisci PM 43 of 9N U.S Federal Aviation Regulations and Mal the niceineon lumeshed hew is eve and coma so me best of my thew)ed Extended range fuel SignalunarDate 41Aultenzed Indivcluar per II CFR Pane] O SEPTEMBER 4TH. 2008 APP 8 a k caet. Y. Approval for Return to Service PurSuant $3 Me &WPM men persons Specified ate. the unt idenolled in item 5 4441 inspected in the mann', lagenbed by the Administrator of tie Federal Avian.) Athsnalrebui arid is ®APPROVED O REJECTED FM Flt Standards Parson Approved by Canteen Ms/MacKay Maireenance Organization parimern of Transport Inspector De SY One (Soo*) FM Designee X Repot Staten thWelion Authorization Carlicate or Signature/Dale or Authcrized Individual Desireoor No. 1E9R960Y SEPTEMBER 41", 2008 RkL. Ot emi\ FAA Forty 337 004/0 SDNY_GM_02756530 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243452 EFTA01328568 NOTICE Weight and balance or operating floatation changes shoe be entered in the appropriate eirooft record. An alteration must be compatible with an previous alterations to assure continued conformity with the applicable erneOrMineSe requirements. B. Description of Work Accomplished fir more space is required. attach additional sheets. identify with am:raft nationality andregisrrabon mark and date work completed) N491GM SEP. 4TM. 2008 Nationality and Registration Mark Date REMOVED BELL HELICOPTER TEXTRON EMERGENCY FLOATATION SYSTEM KIT NUMBER. 407.706-008.101 WITH THE EXCEPTION OF THE ELECTRICAL INSTALLATION IN ACCORDANCE WITH BHT-407-Ilil SYSTEM CIRCUIT BREAKER PULLED AND TAGGED. COCKPIT PLACARDED TO STATE 'FLOAT SYSTEM DISABLED. AIRCRAFT WEIGHT AND MOMENT DATA UPDATED AND ENTERED INTO AIRCRAFT FLIGHT MANUAL. AIRCRAFT EQUIPMENT LIST UPDATED AND ENTERED INTO AIRCRAFT FLIGHT MANUAL. FLIGHT MANUAL SUPPLEMENT BHT-407-FMS-1 REMOVED FROM AIRCRAFT FLIGHT MANUAL. ELECTRICAL DATA NOT AFFECTED. END- O Additional Sheets Are Attached FM Form 337 (mash SDNY_GM_02756531 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243453 EFTA01328569 Form Approved e3 MAJOR REPAIR AND ALTERATION (Airframe, Powerplant, Propeller, or Appliance) OMB No. 2120-0020 d I riltIratiMO For FAA Use Only Fe:wit Aviation Office Identification Awninevinkin 10B3P05050 Zrel 6 • INSTRUCTIONS: Print or type all entries. See FAR 43.9. FAR 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition 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 violation Section 901 of Federal Aviation Act Of 1958). Make Mote BELL HELICOPTER TEXTRON 407 1. Aircraft Serial NO. Nationally and Registration Mark 53375 USA N491GM Name (As sham on (*tildes certitude( Address (As shown on regedefion corneae) 2. Owner AIR GHISLAINE, INC. 103 FOULK ROAD WILMINGTON. DE 19803-3742 3. For FAA_Use Only 4. Unit Identification & 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. AgencYs Name and Address B. Kind of Agency C. Certificate No. U.S. Certificated Mechanic EDWARDS & ASSOCIATES . INC Foreign Certificated Mechanic P 0 BOX 3689 X Certified Repair Station FKFR9300 BRISTOL TN 37625 Manufacturer 0. I certify that the repair and/or alteration made to the unit s) identified in rem 4 above and described on the reverse or attachments hereto have been made in acconiance 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,/ SEP/11/2005 ALAN STELZIG ,e4 "------ 7. Approval for Return To Service Pursuant o the authority given persons speofied below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is 0 APPROVED 0 REJECTED FM Flt. Standards Manufacturer Inspection Authorization Other (Specify) Inspector BY FM Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection Certificate or Signature of Authonzed Individual Designation No. SEP/11/2005 FKFR9300 ALAN STELZIG fi •onic, SDNY_GM_02756532 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243454 EFTA01328570 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must he compatible with all previous alterations to assure continued confamily with the applicable airworthiness requirements 8. Description of Work Accomplished mcre space is required. attach additional sheets idenoty with arc ran nationaUy and rogesfration mark and date work completed) S/N 53375 N491GM 9/11/05 Page 1 Removed Marathon Battery and installed Falcon Crest Concorde Lead Acid Battery in accordance with STC No. SR09359RC. Weight change is negligible to the weight and balance. Revised flight manual equipment list. Log book entry made. Ref: W/O C06091EA END U Additional Sheets are Attached FAA Form 337 (1248) SDNY_GM_02756533 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243455 EFTA01328571 Form Approved 0 MAJOR REPAIR AND ALTERATION OMB No. 212041:Q0 uS Deperar (Airframe, Powerplant, Propeller, or Appliance) el nasometen For FAA Use Only /end Federal Aviation Office Identalcatian Administration 49O ,aso0 az INSTRUCTIONS: Print or type all entries. See FAR 43.9. FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U S C. 1421). Finites to report can result in a civil penalty net to exceed 31.000 for each violation (Section 901 of Federal Aviation Act of 1958) Maur Model BELL HELICOPTER TEXTRON 407 1. Aircraft Sena No. Nalimarly and Registration Mak 53375 USA N491GM Nam (As shown on registration certfrete) Address (As show en registration certificate) AIR GHISLAINE INC. 103 FOULK RD. 2. Owner WILMINGTON DE 19803-3712 3. For FAA Use Only The data identified heien compli applcab e airworthiness requirements and is approved for the above d n d aircraft subject to a conformity inspection b a erso on ed in FAR 43. section 13.7 i— /V- 4.3 /. Sig re AS 500-03 Oats / 4. Unit Identification 5 Tvoe Unit Make Model Serial No. Repair Alteration AIRFRAME -- —'--- (As describedin Item 1 above)-------- X POWERPLANT PROPELLER Type APPLIANCE Manufacturer 8. Conformity Statement A Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Certificated Mechanic EDWARDS & ASSOCIATES , INC Foreign Certificated Mechanic FKFR930D P 0 BOX 3689 X Certified Repair Station LIMITED AIRFRAME BRISTOL TN 37625 Manufacturer RADIO CLASS I / II D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse a 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 Individu 1 - 17-0 3 James J . Row nor 7. Approval for Return TO Service Pursuant to the authority given persons specthed below, the unit identified In item 4 was in the man by the Adennistratot of the Federal Aviation Administration and is OD APPROVED 0 REJECTED FAA Flt. Standards Manufacturer Inspection Authorization Other (Specify) Inspector BY FAA Designee Repair Station Person Approved by X Transport Canada Airworthiness Group Date of Approval or Rejection Certificate or Signature of Authorized Individual 1-17-0 3 PIVOTS'S'. James J. Row 4-0 --1-1<; 12 /4 .5 .....--- FAA Fain 337 Mai SDNY_GM_02756534 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 110243456 EFTA01328572 NOTICE Weight and balance or operating limitation changes shag be entered in the appropriate aircraft record. An aeration must be compatible with all previous alterations to assure continued conformiTy with the appicable airworthiness requirements. 8. Description of Work Accomplished (It more SPE* iS rewired. attach additional sheets. Identify with aircraft netionekly endregistration mark and date work completed) SN: 53375 N4910M PAGE 1 of 2 BELL 407 system Removed the PS ENGINEERING PMA6000 Audio Panel. Installed 1 ea PS ENGINEERING PMAT000S AUDIO PANEL C35d; RICA DO-160b, CO-170, 00-143). using InstI/Operation Man. PIN 200-070-0012, Rev. 12 Sept 2000, 8 EA DWG (ISO C50c, Audio Panel was AV6850. The PMA7000 Audio Panel was installed at F. S. 40 in the instrument panelwhere the PMA8000 originally installed reference EA DWG, AV6718. and copilot headset Installed 2 ea BOSE® Series II l X Aviation Headset Plugs in the cockpit, 1 ea adjacent to the standard pilot Headset Plugs in the cabin, two in the center cabin overhead and three in the aft cabin jacks and 5 ea BOSE® Series II/ X Aviation hatbin, adjacent to each cabin seat, ref. EA DWG t AV8719. inverter was relocated Relocated the Sating SPC-5 Static Inverter to facilitate installation of an AirComm Alr Conditioner Kit The behind the cabin 'hat bin' using 202413 .040' doubler attached to from F.S. 176 to F. S. 160 above the baggage compartment, 21, 22 8 25, 8 fig. 2.9. airframe structure with 'AD' revits, attaching the inverter with 'MS' hardware ret AC43.13-2A, Chap. 2 pars. Air Conditioner Kit The Relocated the existing P/N 01-0770028-05 Strobe Power Supply to facilitate installation of an AirComm Strobe Power Supply was relocated from F.S. 176 to F. S. 184 on the doubler listed above using 'MS' hardware. The RS 24 relay was Relocated the existing N.AT. RS24-020 relay unit to facilitate installation of an AirComm Air Conditioner Kit relocated from F.S. 30 to F. S. 24 Inside the instrument panel console structure using 'MS' hardware. 407-7C0-005-103 ELT Relocated the existing AK-450 ELT to facilitate installation of an AirComm Air Conditioner Kit Installed a BHT The AK-450 ELT was relocated from F.S. 35 to F. S. 25 on the 407-706-005-1 03 ELT Mounting Kit listed above. Mounting Kt. MANUAL BHT-ELEC-SPM All work was accomplished referencing BELL HELICOPTER ELECTRICAL STANDARD PRACTICES BHT-ALLSPM dated 11, OCT, dated 15, NOV, 1996, and BELL HELICOPTER TEXTRON STANDARD PRACTICES MANUAL, 8-01 dated Sept 1998; and in 1996. end BELL HELICOPTER TEXTRON MODEL 407 MAINTENANCE MANUAL 407-MM-1 Rev. accordance with the manufacture's installation instructions, AC 43.13-10 Chap. 3, sec. 2, Chap. 4, para. 4-53 thru 4-58. Chap. 6. sec. 11.30. 11-31. 11-32, 1, 8 set. 3, pare. 6-29, & 6-30, Chap. 7, sec. 1 thru 7, Chap. 10, Chap. 11 Sec. 1 para. 11-1, 11.2; Sec. 3 para. Chapters 1, para. 1 thru 11, & 8 11-37; Sec. 4, para. 11.47, thru 11-52; Sec. 5, thru 17, & Chap. 12, Sec. 1. 2 & 3, and AC 43.13-2A of equipment's manufactures Chap. 2. para. 21 thru 27. Al EDWARDS 8 ASSOCIATES drawings were developed from each piece installation instructions/sc hematics. and EIHT`s aircraft wiring schematics. The above installed equipment is excluded from real time with BELL HELICOPTER TEXTRON Technical Data Report No. 407.099-096. EMI testing in relation to the FADEC in accordance REV. B, Dated 29 June 1999, in accordance with aircraft Type Certificate H2SW, Note 38. and balance was The electrical load of the aircraft does not exceed 80% of the rated generator capacity. The aircraft's new weight Provided Instructions for Continued Airworthiness (ICA), as part computed. Revised the aircraft's fight manual equipment list 98-03, using the checklist in of this FAA FORM 337, as addressed by Flight Standards Information Bulletin for Airworthiness FSAW book entry made. REF: W/O HBAW 98-18. The ICA Is now part of the aircraft's Inspection/maintenance requirements. Log 'CO2458E4/2 -=-,END= ---- INSTRUCTIONS FOR CONTINUED AIRWORTHINESS modification is for the installation 1. INTRODUCTION: The Bell Model 407 is a FAR PART 27 certified helicopter. The above listed and relocation of optional systems LAND this field approved FAA FORM 337. to relocate existing equipment 2. DESCRIPTION: The above listed work is to update the aircraft's Audio Panel and ICS System and to facilitate installation on an AirComm Air Conditioner Ka Guides. 3. CONTROL OPERATION INFORMATION: Reference each manufacturers supplied Pilots Operators 4. SERVICING INFORMATION: WA 5. MAINTENANCE INSTRUCTIONS: This modification shall be inspected Annually LIMN (a) The scope and detail contained in FAR 43 Appendix D. as applicable to the particular line item(s). (or later revision), (b) BELL HELICOPTER TEXTRON BELL MAINTENANCE MANUAL 407-iwn-1, Rev. 8-01 dated Sept. 1998, maintenance manuals are available to each aircraft owner from BELL Chap. 5 - INSPECTIONS; ( NOTE aircraft HELICOPTER TEXTRON} repairs are (a) Manufacturer's publications, as referenced in section 8 of this FAA FORM 337. Inspections, maintenance and/or authorized by FAR 43, paragraph 43.3, with the approved current publications, and training. limited to persons NEXT PAGE all Additional Sheets are Attached SONY GM 02758535 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243457 EFTA01328573 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 addrbonal sheets. %den* mth aircraft nabonahty and registration mark and date work completed) BELL 407 SN: 53375 N491GM PAGE 2 of 2 wirlyakasrocoLnapi AIRWORTHINESS (CONTINUED) 8. TROUBLE SHOOTING: If a failure or malfunction is noted, the wiring in the aircraft may be checked for proper connections per installation prints, as referenced in section 8 of this FAA FORM 337 . If no wiring problems are found, refer to item 5. 7. REMOVAL AND REPLACEMENT: Requires no special instructions due to simple installations using accepted methods, techniques, and practices, UANV section 8 of this FAA FORM 337, and must be performed by persons authorized by FAR 43, paragraph 43.3, refer to item 5 8. DIAGRAMS: WA 9. SPECIAL INSPECTIONS REQUIREMENTS: WA 10. APPLICATION OF PROTECTIVE TREATMENTS: N/A 11. DATA: REF: Advisory Circular AC 43.13-1B Chapter 7. 12. LIST OF SPECIAL TOOLS: WA 13. COMMUTER CATEGORY AIRCRAFT: WA 14. RECOMMENDED OVERHAUL PERIODS: No additional overhaul time limitations. 15. AIRWORTHINESS LIMITATION SECTION: No additional airworthiness limitations. 18. Revisions: Any revs. or alterations of this CA must be accepted by the FAA, via FAA Form 337 Field Approval Process —END— O Additional Sheets are Attached SDNY_GM_02758538 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243458 EFTA01328574 1 SONY_GM_02756537 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243459 EFTA01328575 Form Approved 0 MAJOR REPAIR AND ALTERATION OMB No.2120-0020 US Noreen (Airframe, Powerplant, Propeller, or Appliance) d Tramp:dawn For FM Use Only Federal Aviation Administration 014:03041500-03 @NA) INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition 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 violation (Section 901 of Federal Aviation Act of 1958). Make Model BELL HELICOPTER TEXTRON 407 1. Aircraft Serial No. Nadonatly end Registration Mak 53375 USA N491GM Name (As shown on regisbafion certificate) Address (As shown on tegisearial certs6cafe) AIR GHISLAINE, INC. 103 FOULK ROAD 2. Owner WILMINGTON, DE 19803-3742 3. For FAA Use Only 4. Unit IdentfficatIon 5. Type Urit Make Model Serial No. Repair Alteration AIRFRAME ,As describedin dem I above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6. Conformity Statement A Agenoys Name and Address B. Kind of Agency C. Cen Prate No. U.S. Certificated MeChaniC EDWARDS & ASSOCIATES . INC Foreign Certificated Mechanic P 0 BOX 3689 X Certified Repair Station FKFR930D BRISTOL TN 37625 Manufacturer D. I certify that the repair andthr 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 and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized Individual JANUARY 17, 2003 JEFFREY MCKAMEY ..079 .... zsry 7. Approval for Return To Service / te Pursuant to the authority given persons specified below, the unit identified in item 4 was inspect in the manner presirbed by the Administrator of the Federal Aviation Administration and is ® APPROVED 0 REJECTED FM Rt. Standards Manufacturer Inspection Authorization Other (Specify) Inspector BY FM Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection Certificate or Signature of Authorized Individual Designation No. JANUARY 17, 2003 FKFFt930D JEFFREY MCKAMEY 7/44. 0,25.-"yeAntany FAA Form 337 (12.88) SONY_GM_02756538 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243460 EFTA01328576 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 'It more space is required, attach additional sheets Identify ...nth adcran nationality and registration mark and dare work Compieted ) S/N 53375 N491GM Page 1 Removed Skylights, Windshields, Chin Bubbles and High Skid Gear with Flitesteps previously installed at the factory. Removed AAI Crew Door Openers in accordance with STC No. SH1990SO and Air Comm Cabin Fresh Air Ventilation System in accordance with STC No. SR00230DE previously installed on FAA Form 337 dated September 22, 1999. Installed Air Comm Air Conditioner with Dual Forward Evaporators in accordance with STC No. SR00222DE. Installed AERONAUTICAL ACCESSORIES, INC. WIRE STRIKE PROTECTION SYSTEM in accordance with STC No. SR00975AT. Installed AERONAUTICAL ACCESSORIES, INC. REPLACEMENT SKID TUBES in accordance with STC No. SR01697AT. Installed AERONAUTICAL ACCESSORIES, INC. FLOATSTEPS in accordance with STC No. SH1322SO. Installed AERONAUTICAL ACCESSORIES, INC. HIGH VISIBILITY CREW DOORS in accordance with STC No. SR09326RC. Installed AERONAUTICAL ACCESSORIES, INC. HIGH VISIBILITY CREW DOOR OPENERS in accordance with STC No. SR09326RC. Installed AERONAUTICAL ACCESSORIES, INC. BULGED SKYLIGHTS in accordance with STC No. SR09325RC. Installed AERONAUTICAL ACCESSORIES, INC. CHIN BUBBLE WINDOW ASSEMBLY in accordance with SIC No. SR01051AT. Installed AERONAUTICAL ACCESSORIES, INC. REPLACEMENT WINDSHIELDS in accordance with STC No. SR01051AT. Installed AERONAUTICAL ACCESSORIES, INC. REPLACEMENT AFT CROSSTUBE in accordance with STC No. SR09330RC. NEXT PAGE 0 Add.cona' Sheets are Attached FAA Form 337 (17-88) SDNY_GA4_02756539 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024346 I EFTA01328577 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 reguired attach additional sheets Identify with aircraft nationality and registration mark and date work completed) SIN 53375 N491GM Page 2 Installed AERONAUTICAL ACCESSORIES, INC. LOCKING FUEL CAP in accordance with STC No. SR01489AT. Installed AERONAUTICAL ACCESSORIES, INC. SLIDE WINDOW LATCHES in accordance with STC No. SR01051AT. Installed AERONAUTICAL ACCESSORIES, INC. TAIL ROTOR PEDAL LOCKOUT KIT in accordance with STC No. SR00513AT. Installed AERONAUTICAL ACCESSORIES, INC. HEADSET HANGER BRACKETS in accordance with STC No. SR00235AT. Installed BHT serviceable Lightweight Popout Floats in accordance with BHT-407-11-1. Installed BHT Drive Train Modification Kit, P/N 407.704-012-115 in accordance with BHT-407-II-30. Weighed aircraft and computed new weight and balance. Revised flight manual equipment list. Log book entry made. Ref: W/O C02456EA, C02457EA, C02572EA. END Additional Sheets are Attached FAA Form 337 (124S) SDNY GM 02756540 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243462 EFTA01328578 SDNYGM02756541 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243463 EFTA01328579 . Form RowDyed Due. No. 21204018 0GS INOTANT• APPLICATION FOR AIRWORTHINESS INSTRUCTIONS — Foto 0 ITT< OR ow woe .0 ..n.4.1,-.1 areas. Wes. are Ice FAA use Only Submit original only lo an sothorom0 FAA ReDIESTIAiative II 00OPOrtal abr 1.—....tnolon oC 50420ISIP30000 Lae an attachment Fee SReCul ligh, peinviscomoleteSeetiens - CERTIFICATE ii 4,4 vi of %Hi as appliCatie .. 'REGISTRATION MARK SAITO...TT BUILDERS NAME 'mat 1 AIRCRAF T MOM °COGNATION A TA Ufa FAA WOW Na fa 1 GM S. AIRCRAFT SERIAL NO Bell Helicopter Textron IL ENGINE BUILDERS RAW Limit. 407 F (NOME MCW. DESIGNATION 1999 /11.202,06 . 5 3 3 7 5 Rolls-Royce (Allison) 250 -C 47 El -Srtirir a. NUMBER OF ENGINES S. PROPELLER 'WAGER S NAME .40.44F. It PflOPULER PAODEt OLSGromoom N.MRCRATT IS iCtioca of 400hANN.0 one N/A N/A IMPORT APPLICATION IS NEREITY MADE FOR/CANA appWalves•Ns, A I* STANDATIONFTWORTPANES3 CEATiNCATE tenow•NENTERN/ I I NCIOAAT. I !Noun , I 'ACROBATIC' I TRANSPORT I I WWI I I BALLOON B SPECIAL AiRTVOATIRNIESS CERTIFICATE 'CIRO APON4PRN Arm, 2 LIMITED o t CLASS I S PIAEWLSIONALandca•Van/ 2 CLASS II I AGRICULTURE ANDIESTCONTROL 2 AERIAL SURVEYING 3 oath ADVERTISING 3 AESTFACTED/PLeson 004•MORP•0 4 FOREST /MEAN TOWSN.Lapn 5 PATROLLING • WEATHER CONTROL co too&von E CAFMMGE OF CARGO 0 OTHER iScx.srl I ITESEAROL APO OfvELOPMENT 2 AMATEUR GUILT 2 EXPIIIITION EXPERIMENTAL Nyco%P OpF•AL0.A.. • SW SURVEY • RACE S CRIER TRAINING ..., se 04 4010040, u 0 IOSNOW COMPLIANCE WONT AR I FERRYfoGHT FOR REPASS ALTERATIONS MAINTENANCE OFT STORAGE 2 EvACUAIE FROLTAREA OF iMPENINNGOANGEIT SPECIAL FLIGHT PERMIT anima OP•OnOn ION/ COMITYTNIE 1/1•0 S OPERATION 0. (*GESS Or MUMMY CERTIFICATED TALLE-CAF WEIGHT • ccnolen Stasi VI 0 , VNIs NvecogyOle i••••••• pen 4 NUMMI° ORCAROM I 5I I PRDOUCTiON FLIGHT TESTING a CUSTOMER DEMONSTRATION FLIGHTS C j 6 I IALILliOlE AIRWORTHINESS CERTIFICATE tOve• ABOVE 'Ressocreo OsAwNvo NNE -Sinn at lased As AVIOCLICAO i A REGISTERED OXNEWIN vow.R. C•FACP0 01.ros•0 "NOV•Ppen IV MALIK CHECK HERS I PONT ADDRESS Air Ghislaine Inc. 109 Foulk Rd. Wilmington, DE 19809-3742 B NORM T CERTIFICATION BAYS Crock APPlotalit 0005 amICOnoble Hate of .../JC.InIll ALAMO T SPIOOCATION OR TYPE CIIIIWCATE OAIA SHEET .6...• No A•RWEIAININESSOMECTIVES 'Chen a Wo opiate.* ADS compke0 owl. 440 roe .., Pant AO No i '"p A•pROA NO i S H 2 SW Revision 40 Jr AD 2002-21-51 B/W 2002-21 ARICRAFT LIVING /GAR PN/4044NeviLo bus s mcorporatea: SOPPLEMENI AL Int aro if iCATE Floe os.••• °toothPC 4%0. po,Mali •.•4.. SH227WE SH1312S0 SH2243S0 SH3289S0 * SH1388S0 SH1990S0 SR00221DE SR1322S0 i C. m*C0.4, 7 OPERATiON AND WONT ENANCE ALCORI)S SR01411AT SR00230DE SR002200E CHECA IT RECOROS TN TOTAL AIRFRAME HOURS ExPEARANTAL ONLY If FIR MPslumn sole* Iasi no0.4444 COMFIJAHCE WITH I 312. 5 3 IssIAP RIPARPRI/ ' saint" 91.417 0. CEROSICATION - I Twain CANN* NM I Am Alm imosnmes qoPer, Io ry...gyny el TN: :womb ouwoug ANA, mum list maz•A a iroymmo wary Frani Myso. Nomovratoo .... &mamma ALIA 2c00.50 TARA kens Analyn AM 'A 122E NO Feint fointo Asicei hopAadot, It'd rim My mOall roe arts risen n gifA0r1hy No *SOW Orme anyonnens •LIonma DATE OF APPLICATION NAME AND I MAw (A ls swot* , Ma nAviatIon Group bKaAnin November 14, 2002 LA•wARR- l; t • Engineering e• conek A. THE AIRCRAFT DESCRIBED ABOVE HAS GM •4•2010 ANO POUND AMWORTriv BY 'CUM R., . RR Rely a TAI)I BEd, so FAR PART III OR 127 CERliFiCAT POWER Ulm CERTIFICATED IFECHANIC IG.... , CERTIFICATED EPA $TATIONIGN• Kw ill COIJOTIONO I 3 * CanAcoe No . AR 2278237 Alf•COM 1 SAANOIAC IVREA iCON name ol1.“ot it 1 $ 2 DA E Ina S./GRAVURE November 14, 2002 Phillip R.G. Lowe sow. ALL ATempoo• CORN R Sew A Nol ill X X INC Wirer RAI( PEOUESTED A I MO PRI MY MOM' OWASSO N StC100. I O. VII eon,. ManfibffitnIS 1W • AMENIRAENT OR WO 'CAIRN OA CURRENT AIRWORTHINESSCERN/CATE FAA INSPECTOR FAA OESKINEE ; El Li BI a • ics<4.1 WC TRAM NAN Samoa vs It. IN CERTIFICATE PLOWER UNDER FARES I IFAR 121. 127 Of 1331 I FAR 515 "33 II 041f 04TOUCT OFFICE DESIGNLESSIGNAI AND FAA INSPECTORS EIGNATuRE li November IFO - Lon 4 i 14, 2002 • AEA - 35 Manfred Herweg OA RT111001EA FAA Form 8130-61•I 44: sonosCOFS ARE VOA EDITION SDW_GM_02758542 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8,9,10,15, and 17 EFTA_00243464 EFTA01328580 AEM/EIO-Err NH , CI'd*Crtn • A IMMUEACILIIIIR NAME ADDRESS VI. IMODUCT10.4 • H Lr. i & PRODUCTION BASS RCA NA appLcee• AM PROCUCTION CIA TECATE (Gmi pooVegen cvntcas IN.. , RANT TESTING TYPE CERTIFICATE ONLY APPROVED PRODUCTION INSPECTION SYSTEM • CONE OUANTITY OF CIAMICATES REOUIREO FOR OPERATING IL OS DATE OP APPICATION NAM* AmTy TITLE IIN.0 vine) SIGNATURE A. OESCRIPTION OF MAMA?! REGGIERED OWNER ADDRESS SUEDES IFIFM) 1000it MAME NUMBER REOISIFIAT iON NARK • OCSCRIInION OF FLIGHT CUSTONEWDEMONSTRATiON FLIGHTS CI KIRK. 4 istabeari FROM TO VIA DEPARTURE DATE DURATION VII SPeChtt MIGHT PUSiT VIAIPOSIES 07.001 THIS PAODUCTION FOCHT TIST C CREW REWIRE° TOOPERATE THE AIRCRAFT AND ns tOUSAENT . I PILOT I I COSiLOT I I NAVIGATOR 1 I OTHER /Spoors, O. THE MACRAET OEMS NOT MEET 111E APPLICABLE AlfiwORTAITTESS REQUIREMENTS AS FOLLOWS • I THE FOL L &ANC RESTRICTIONS ARE CONSIDERED NECESSARY FOR SAFE OpIRAI PON p Ulf AffeClywary •I neetallti.i R CERTIFICATION- 'AMOY C•naY thanlanh• 10941010 OvAW CON luSSEPAII 01IN sitriIIINNTAN stew. Am liAantall a terSANINTA Int I ten ApaNnApposelhatosiel . IKCCl/CIISCO Nils &Khan SOI ol IN Swaps AAA.' me co Mr ire sppbc•Oht Tide,.' A•41.011 Rapaassans AAR INT IN introit Ns beeNaspecisa one A N.:ohs IN TN ANN cleSCANO CA E NAM( AND Tint gokany Non SIGNATURE Cs SAMNA% 01CcoNsprdir, FAA . Owen 0 IIIPPIAluch sofen NOATTICTI .1 x a, A LASIMMAS SAO ltsfilsogNil Cofteerce Hot FAR A. Ialtrieg 91.9 PO4C. St I °ANN AwpipiNnest CessIcaTiOn IN m•OCti Avoall x' t; 1 ...CtonalOW•SweLtiralaboesAltacinea lattorn.wita ,Np...6) # .D. One. ORPR,RTY METROS He HUNG shoo MP.O.dl I.Nt.'s, A./purples. GANA.* NSoi AIXOTOnewth f. pS i It1 NC O. GANN WAIN &Ad EWAN* INCIIT.PC0 MSS.* e &Kieft • IC FAA 2 1.329 ea tonwawm000to 4o- LHEHHOt A CUIMM AnitAtNINIS °HEEHAW Issue* pep Accordance LLLIn E.Maicte Wait and Manson FAA Form 337 OWNh Nita i' 21.18301 * P. The .0110/0100 WON mAwash FINNS * FAR 'Copy analvai SDNY_Ght02756543 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243465 EFTA01328581 04•ATIAINT nweinistaipmixam. Arum°.•OsiiITOUte. STANDARD AIRWORTHINESS CERTEICATE • am. CVO 1 I- 444 DM Helicopter T%ron N491GM 407 53375 Normal • arnaol*amt rafts natal ••••••1•NAN ••••••• /*INA. ••••••• • •• •••••••••••• •••••••••• •••• -re it., •10.1}•••••• As eons now taam Noah • Tt•••10••00C•OVIC•al 01••••••••••••••••• 4.444.4...440. lievembor 14. 2002 MYI ra0 Harxvp • DART' 11001EA nos canto M IONNIISAA11014 ONw ion Cal. IS toe liallOWT MK. WOW FAA Fat 011/02 444 • as OLCLISNI0 SONY_OM_02756504 ECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, at EFTA_00243466 EFTA01328582 SONY_GM_02756545 ECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, ar EFTA_00243467 EFTA01328583 s UNITED KINGDOM CIVIL AVIATION AUTHORITY CC-tiCCAtt No 1051296/001 CERTIFICATE OF AIRWORTHINESS FOR EXPORT Conan:Wand Constructors Year Cl Constructer Ai rcraft Serial Number Designalke ol Alraalt BELL HELICOPTER TEXTRON CANADA 1999 53375 BELL 407 Country to which exported: UNITED STATES OF AMERICA PRIVATE CATEGORY This certifies that the aircraft idenaied above has been examined and as al the dale of this cortfoate is considered ainawthy in accordance with opened. British Civil Ainsenhness Requtrements end with the special requirements roofed by the &polling country as listed. A flight Manual Icons part of this Cerbficale Special Requiernems None advised. • Date: .. ... 2800T0BER V0L fee hid Ana — * S ins Certificate don rim Constitute an authority for the seat to be ann. No fl ies or endiereementS may be madame* Certificate except by an authorised person. LI this Cortical. is lost. Me Civil Malkin AuthOnly should to informed at no, My person finding this certificate SIIOUld forward hl immediately to the Give notice Authority. Safety Regulation Group. Aviation House. South Area. Gana Airport. West Sussex, RHO OYR. CA1224 090699 SDNY_GM_02756546 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243468 EFTA01328584 SDNYGM02756547 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243469 EFTA01328585 togrODIPsna CO -4/40.. Of/WYDRIer or TRAWOITA110.1-f WOW M•410441..eannow • STANDARD AIRWORTHINESS CERTIFICATE rfrc. • AlOartiliPlat 4404444 4.44. •••••••• Bell Helicopter Textron, x407315 Confide Kodel 407 53375 /Mal. • milyPer..410.01.0• 41111•001 &mons wet my on Woo vane so. \b.., a.m.** Wu •••••••• 6,••••• SW • saws im 1••••••...........ele a• Hone • "IlliMIMOCCatel•pall Imo f tascrenasea 07/02747 • Samuel J 1en 30-70173:1-00R1 vs , n'e• CO.WaTC ral *I IVO AICNOT •• acornora ving OnLICMAS tilDS4 FAA Fenn 5100-2 44. • 411.01.0, 1•14.-11411.10 7 SONY_GIA_02756548 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00243470 EFTA01328586 SONY_Gh1_02756549 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 00243471 EFTA01328587 Log Book Certificate N 1107 RB Date: Sci her( 22330 I hereby confirm that the US. Nations* and Registration Marks have been removed from the aircraft In accordance with FAR 45.33 / Manfred Herweg ASV 1743820 SEW GM_02756550 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 1O,-15, and 17 EFTA_00243472 EFTA01328588 SCINY_GM02756551 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243473 EFTA01328589 0 MAJOR REPAIR AND ALTERATION Form Approved OMB Nccci V US DePartme(tt (Airframe, Powerplant, Propeller, or Appliance) F Fitai d Traaportabon FIRDIMIAYMIXI OffiCeJden AdnilliSITIV003 \‘A #S \ INSTRUCTIONS: Print or typo all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and &position of this form. This report is requirod by lave (49 U.S.C. 1421). Fa lure to report can result n a *MI penalty not to exceed 51,000 for each such violation (Section 901 Federal Aviation Act 1953). Make Model 1. Aircraft Bell 407 Serial No. Nationality and Registration Mark 53375 N407RB Name (As shown on registration certificate) Address (As shown on registration certificate) Bell Helicopter Textron Inc PO Box 482 2. Owner Fort Worth TX 76101-0482 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME ----------(As described in Item 1above) -- POWERPLANT X PROPELLER Type APPLIANCE Manufacturer 8. Conformity Statement A Agency's Name and Address B Kind of Agency C. Certificate No. PILO Lowe X U.S. Certified Mechanic I I Cobbens Mead Foreign Certified Mechanic ARP 276237 Haywards Heath Certified Repair Station West Sussex 81116 37Q England Manufacturer D. I certify that the repair andicr alteration made to the units) identified in item 4 above on the reverse or attachments hsreto have been made in accordance with the requirements of Part 43 of the U.S. Federal A 'ens and that the information funished herein is bye and correct to the bast of my knowledge. Date Signature of A • t Individual 24th March 2000 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit in item 4 was in ed in the manner prescribed by the Administrator of the Federal Aviation Administration and is ir.3 APPROV D 0 REJECTED FMPlight Manufacturer Inspection Authorization Other (Specify) Standards Inspector X FAA Designee Repair Station Person Approved by Trans Canada Airworthiness Cr Data of Approval or Rejection Certificate ce Signature of Authoriz Ind 25th Muth 2000 Designation No. 2276237 FAA Fem. 337 dare SDNIIGM_02756552 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243474 EFTA01328590 NOTICE , in the apptopriatelaircralt record. Ari.elteration.n\us Weight end balance or operating limitation changes shall be entered with the apPticable airworthiness requiremetts compatible with all previous alterations to assure continued conformity S.DesciptIon of Work Accomplished y and regard:fon mark and dare work theapkted) (ifmore space Is reqedrect attach odatonal sheets Mouthwith aireme nationall Registration: N407RB Mobel: Ball 407. Serial No: 53375 TSN: the above Helicopter: 1. The following Avionics equipment has been REMOVED on a)King 1O(165 Nav/Comm System b)Appollo SL60 Comm/GPS System (GPS Stand-alone) c)King KR87/KDA 692JKA44B ADF System d)PS Engineering PMA 6000-S Audio Panel 2. The following equipment has been INSTALLED: a) King KY196 Comm b) King GNS 430 Nav/Comm/GPS c) King KMA24H Audio Control panel radio stack with the King KMA24H The Installed KY196 Comm has been located in the main the original Antenna as provided for the Audio panel and King GNS 430 Nav/Comm/GPS using Appollo SL60. ment and has been installed in accordance Installation of the KMA24 AND KY196 Is optional equip 07-MM-1 Section 97-00-00 with the Manufactures (Bell) Maintenance Manual BHT-4 al reference 006-00695-0003 Rev 3 March 98 And the equipment manufactures installation manu 006-00586-0002 Rev 2 July 94 installed in the previous location used by the The Garmin GNS 430 Nav/Comm/GPS has been installation of GPS equipment as stand-alone Appollo SL60, with reference to AC21-138 covering Rev F Oct 99 which was previously approved Using Installation manual reference 190-00140-02 and placarded as "GPS day VFR operation under STC No SA00705W1 dated October 2 1998 only Post installation checks completed as required. found within the manufactures maintenance Continued Airworthiness evaluated at this time and instructions covering avionics equipment. engineeririg practices. AC43-13-1B complied with as applicable covering good as required. Weight and balance and equipment list up dated Log book entry issued END O Additional Sheets are attached SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, SDNY_G and M_0275 65.53 17 EFTA_00243475 EFTA01328591 Form Approved 0 MAJOR REPAIR AND ALTERATION . OMB No. 2120-0020 US ciiinnusiii . olTranspaithon For FAA Use Only (Airframe, Powerplant, Propeller, or Appliance) Office Identification rerun Ariake AdrninIstfica ", . #D - 35.. . t i, -"--L, INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendtc lit and AC43.94 (ortiubsequent revision:thereof) for insfructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to repbst can result in a civil penalty not-To exceed 31.000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Model Bell 407 1. Aircraft Serial No. Nationality and Registration Mark 53375 N407RB 1 r: t ' Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner Bell Helicopter Textron Inc. PO Box 482 Fort Worth, TX. 76101.0482 3. For FAA Use Only tiltd,e • in crsrnpfine with I've wrath}, airworbinessneratiMattliazd it wend br be • aboredesalled an% subject b corona insomit• inn by 'perm in FAR 43.Seiclea 47 v _re- Da s of HA Inswcbr - 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration J AIRFRAME As described in Item 1 above) X POWERPLANT PROPELLER Type APPLIANCE Manufacturer O. Con ormity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. X U.S. Certified Mechanic Phillip Lowe Foreign Certified Mechanic 11 Cobbotts Mead. Haywards Heath Certificated Repair Station 2276237 West Sussex RH16 3TO. England Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and d on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the V.S. Federal Av on eg lions and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized Ind , -fi • • 4 FAN Winn 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit Identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is g APPROVED O REJECTED FAA Fit Standards Other (Specify) Manufacturer X Inspection Authorization Inspector BY Person Approved by T FM Designee Repair Station Canada Airworthiness Date of Approval or Rejection Certificate or Signature of Authorized I t 4 we gra Designation No. 2276237 FAA Form 337 (1240) • SONY GM 02756554 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00243476 EFTA01328592 NOTICE • & Weight and balance or operating limitation changes shall be enteredin the appropriate aircraft record. An aeration must be compatible with allprevious alterations to assure continued conformity with the applicable alnaordliness requirements. t 1 • • - 45 41 1v . I B. Description of Work Accomplished (Ifmore space is required, attach additional sheets, Identify with aircraft nationality andregistration mark and date work accomplished.) 4 An Allied §ignal Aerospace KCS 305 slaved gyrocompass system consisting of a KSG105 gyro, a KP1 553A HSI, a KMT 112 fkuonilve and liKASIB slaving assembly has been installed. A KGS TSO-C73 inverter model SPC-5 has also been installed to work with this system. The ICSGI05 and the inverter are mounted above the baggage compartment and the HSI is mounted in the instrument panel.. All equipment locations are referenced in the aircraft equipment list. The system is wired per the manufacturers instructions. ' for structural igpaimadon referents DER report no. 2R00330 entitled "Structural Analysis for Installation of Misc. Avionics on a Bell 407 HtlicaPter..3.(q 6075." Dated 08-27-1999 and FAA form 8110-3 dated 08-27-1999. • Triftalliaiiii1WwWilrialifeine in accordance with Ad 43.13.15 chipter 11 on electrical systems, AC 43.13-2A chapters tand'3 on radio and antenna instillations, Allied Signal Aerospace KCS 305 installation manual pn 006-00116-0002, Rev. 2 dated February, 1984, KGS Electronics RemovellInstallarion Manual FAA TSO-C73 Model: SPC-5( ) DWG 51506 dated APR 03, 1996 and Alan Mann Group LTD. wiring diagrams 407-1570-303. Ground test haye been conducted to ensure that the compass system is not a source of objectionable electromagnetic interference and operates properly and safely with the manufacturers instructions. Weight and balance and equipment list have been updated. Fadec EMI test procedures arc not required for this installation. Reference Bell Helicopter letter reference no. 1999090017-1. END- Attachments: FAA form 8110-3 :Instructions for Continued Airworthiness ®,Additional Sheets Are Attached * U.S. G.P.O 1990-761-753 SDNY_GM_02756555 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243477 EFTA01328593 Form Approved 0 • MAJOR REPAIR AND ALTERATION OMB No. 2120-0020 : :it/0+4mM of Transportzion (Airframe, Powerplant, Propeller, or Appliance) For FAA Use Only FedertelArliellm Office Identification AdmInfitntlen INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and deposition 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 1958). Make Model Bell 407 1. Aircraft Serial No. Nationality and Registration Mark 53375 N407RB Name (As shown on registration certificate) Address (As shown on registration certificate) 2. Owner Belt Helicopter Textron Inc. PO Box 482 Fort Worth, TX. 76101-0482 3. For FAA Use On y FA. dab ow/MU helve seirretwa Atte topkak. ainforlimss raquirenwit aM is Waned le abovedesCribed alma; subiactt cotter* Moat- ion by a person autioczed in FAR43Secte43.7 //77./g5 . )_,,-,,,,,,:< P bo;d3r . Dale i.,,, trete Of FAA his 4. Unit Identification 6. 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. X U.S. Certified Mechanic Phillip Lowe Foreign Certified Mechanic 11 Cobbetts Mead. Barmaids Heath Certificated Repair Station 2276237 West Sussex RH16 3TC1. England Manufacturer D. I certify that the repair and/or alteration made to the unit(s) Identified in item 4 and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. F A iation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date Signature of Author. :victual 000Z LIVW k z 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 presorted by the Administrator of the Federal Aviation Administration and is RI APPROVED ID REJECTED FM Fit. Standards Other (9pArify) Inspector Manufacturer X Inspection A dzation BY FM Designee Repair Station Person by Transport Canada AI s Group Date of Approval or Rejection Certificate or Signature or th rized Individual 4 mAR 2000 Designation No. 2276237 orm O2-ra) SDNY_Gf.1_02756556 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243478 EFTA01328594 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must bo compatible milt allprevious alterations to assure continued conformity with the applicable airworthiness requirements. B. Description of Work Accomplished (//more space is inquired, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) A B.F.Goodrich Aerospace SKYWATCH system consisting of a TRC497 Transmitter/Receiver Computer pn 805-10800- 001 , a WX-1000 Skywatch display pa 78-8060-5900-8 and a NYI64 directional antenna pn 805-10890-001 has been installed. This system also includes a WX-1000E stormscope processor pn 78-8060-6086-5 and a stormscope antenna pn 78-8051-9200-8. The TRC and stormscope processor are mounted above the baggage compartment and the display in the instrument panel. The skywatch antenna is mounted above the cockpit on the forward cowling. The storroscope antenna is mounted on the bottom of the fuselage below the baggage compartment. All equipment locations referenced in the aircraft equipment list. The system is wired per the manufacturers instructions. For structural information reference DER report no. ER00330 entitled "Structural Analysis for Installation of Misc. Avionics on a Bell 407 Helicopter; s/n 53375." Dated 08-27-1999 and FAA form 8110-3 dated 08-27-1999. This system has been previously installed in accordance with STC SA00733CH dated August 20, 1997. Installation and wiring has been done in accordance with AC 43.13-IB chapter I 1 on electrical systems, AC 43.13-2A chapters 2 ind 3 on radio and antenna installations, B.F.Goodrich SKYWATCH Traffic Advisory System SKY497 Installation Manual pn 009-10800-001 Rev. A dated 25 April 1997 and Alan Mann Group LTD. wiring diagrams 407-1570-319 and 321. FAR 91.411 and 91.413 have been complied with. A placard has been installed in clear view of the pilot that states " Information shown on the display is provided as an aid to visually acquiring traffic. Pilots should maneuver their aircraft based only on ATC guidance or positive visual acquisition of the conflicting traffic. Maneuver should be consistent with ATC instructions. No maneuvers should be made based only on a Traffic Advisory. ATC should be contacted for resolution of the traffic conflict If the pilot is advised by ATC to disable transponder altitude reporting, Skywatch must be turned off." Ground test have been conducted to ensure that the SKYWATCH system' is not a source of objectionable electromagnetic interference and operates properly and safely with the manufacturers instructions. Weight and balance and equipment list have been updated. Fadec EMI test procedures are not required for this installation. Reference Bell Helicopter letter reference no. 1999090017-1. The I3FGoodrich Pilots Guide pn 009-10801-001, Revision A, dated 06/23/97 (or later applicable revision) must be accessible to the pilot whenever this system is in use. END Attachments: FAA form 8110-3 :Instructions for Continued Airworthiness IA Additional Sheets Am Attached * U.S. O.P.0 1990-761-753 SDNY_GM_02756557 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243479 EFTA01328595 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION DATE STATEMENT OF COMPLIANCE WITH FEDER AVIAT 08-27-1999 AL ION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Aripktne, ratter, NAME OF APPLICANT Helicopter, etc.) Bell 407 Helicopter Mann Avionics Ltd. LIST OF DATA IDENTIFICATION TITLE Engineering report no. ER00330, N/11 "Structural Analysis for Installation of Misc. Avioni Dated 8-27-1999 cs on a bell 407 Helicopter, s/n 53375." Mann drawing nos. 407-1570-107, Rev A "Installation of Avionics Equipment.' Dated 8-99 407-1570-115, Rev A 'Gyro Mount' Dated 7-99 407-1570-117, Rev A Inverter Top Hot, Static Inverter/Strobe Unit." Dated 7-99 NOTES: 1. The structural aspects only of the above data is approved herein. This approval is valid for a Bell 407, s/n 53375 ONLY. 2. The equipment covered by the above data is: Directional Gyro restraint; Static inverter restraint; Skywatch box; skywatch antenna; WX-1000 box; and stormscope box. PURPOSE OF DATA In support of major alteration for s/n 53375 . This approval is designed data approv installation approval. al only and is not APPLICABLE REQUIREMENTS (LIST OF SPECIF IC SECTIONS) FAR part 27.301; .303; .305(a); .307(a); .337; .561(pre-admt 27-25); .601; .603; .607; .609; & .613 .605; CERTIFICATION Under authority vested by ducction of tho Adrnini-stralor and in accordance and limitations of appointments under Part with conditions 183 of the Federal Aviation Regulations, data Attached sheets numbered listed above and on have been examined in accordance with to comply with applicable requirements of the established procedures and found Federal Aviation Regulations. D Recommended approval of these data I (*) Therefore Fl Approve these data SIGNATURE(S) OF DESIGNATED ENGINE ER REPRESENTATIVE DESIGNATION A ric CLASSIFICATIONISI 4. "ifilllitria--- Structures: Chart A: James A. Munda DERV-955065-NE 1A, 4A & 9A -- - - r - -3 (11-70 SUPERSEDES PREVIOUS EDITION) s:Itoxt liaN00330Villtbstr SDNY_Ghl_02756558 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243480 EFTA01328596 SONY_GM_02756559 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243481 EFTA01328597 Bell 407 SN 53375 N407RB Date Instructions For Continued Airworthiness I. Introduction: These Instructions for continued airworthiness are for tire B.F.Goodrich Aerbspace SKY WATCH system referenced in block 8 of FAA form 337 for the aircraft referenced above. 2. Description: Reference block 8 of FAA form 337 for complete description of system installed. 3. Control, operation information: Reference the BFGoodrich Pilot's Guide pn 009-10801-001, Revision A, dated 06/23/97 (or later applicable revision) referenced in block 8 of FAA form 337. ' 4. Servicing Instructions: N/A 5. Maintenance Instructions: The B.F.Goodrich Aerospace SKY WATCH system will be inspected annually for proper operation and visually inspected for damage, security and electrical connections. Inspect in accordance with B.F.Goodrich SKY WATCH Traffic Advisoiy System SKY497 Installation Manual pn 009.10800.001 Rev. A dated 25 April 1997 (or later applicable revision) , chapter 4 , section 4.2 entitled Periodic Maintenance. 6. Troubleshooting Information: Troubleshooting should be accomplished by qualified personal using manuals referenced above. 7. Removal and Replacement Information: Removal and replacement of components in this system may only be accomplished by qualified personnel using manuals referenced above. 8. Diagrams: Wiring diagrams referenced in block 8 of FAA form 337. 9. Special Inspection Requirements: N/A 10. Application of Protective Treatments: N/A II. Data: Reference equipment manufacturers manual referenced in item 5. 12. List of special tools: N/A 13. For Commuter Category Aircraft: N/A 14. Recommended Overhaul Periods: "No additional overhaul time limitations" 15. Airworthiness Limitations Section: See placard located in clear view of the pilot which states "Information shown on the display is provided as an aid to visually acquiring traffic. Pilots should maneuver their aircraft based only on ATC guidance or positive visuabacquisition of the conflicting traffic. Maneuver should be consistent with ATC instructions. No maneuvers should be made based only on a Traffic Advisory. ATC should be contacted for resolution of the traffic conflict. If the pilot is advised by ATC to disable transponder altitude reporting, Skywatch must be turned off." 16. Revision: Revisions to be accomplished using FAA form 337 and the FAA field approval process. Changes should be documented on a form 337. This form and supporting documentation should be presented to the local FAA Avionics Inspector for approval in block 3 of form 337. These instructions have been prepared in accordance with Flight Standards Handbook Bulletin for Airworthiness (HBAW) number HBAW 98-18 dated 10-07-93. 6 'd Z 'OH 1Z160 664T . OZ .ZI 12KINIU SMOONIb4 S31HOIAU'HNUW NO8J SDNY_GM_02756560 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243482 EFTA01328598 SONY_GM_02756561 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243483 EFTA01328599 Form Approved a • . . , • OMB No. 21204 MAJOR REPAIR AND ALTERATION ce) For FAA (Airframe, Powerplant, Propeller, or Applian us papaw. Office identjacatIon &Trans wn Nam Minion tt4 SC ararrannan AC 43.9.1 (or subsequ ent revision thereof) for instructions FAR 43 Appends B. and INSTRUCTIONS: Print or type al entries. See FAR 43.9, a civil penalty not to exceed S1,000 law (49 U.S.C. 1421). Failure to report can result in and imposition of this form. This report is required by Act 195(). for each such violation (Section 901 Federal Aviation Model Make 407 Aircraft Bell 1. Nationality and Registration Mark Serial No. N407R8 53375 • Address (As shown on registration certificate) Name (As shown on registration certificate) PO Box 482 Bell Helicopter Textron Inc Fon Worth TX 7,5101-0482 2. Owner 1. For FAA Use Only 6. Type • 4. Unit identification Serial No. Repair Alteration Make Model Unit ----- AIRFRAME ---------..--(As described rn nom 1 above) ------- X POWERPLANT PROPELLER Type APPLIANCE Manufacturer 6. Conformity Statement C. Certificate No. A. Agency's Name end Address B IBS of Agency X U.S. Certified Mechanic M.G Magill AAP 2543510 Foreign Certified Mechanic 73 Cavendish Mead Certified Repair Station Sunninghill Manufacturer Berkshire SL59TB England reverse or attachments hereto alteratio n made to the unit(s) identified in item 4 above and described on the 0. I certify that the repair sailor Federal Aviation Regulat ions and that the information furnished nts of Part 43 of the U.S. have been made in accordance with the requireme herein is true and correct to the best of my knowledge. 0 Signature of Authorized Individual Date 25th September 1999 M Magill 7. Approval for Return to Service 1. i the manner prescribed by the d below, the unit in item 4 was inspected Pursuant to the authority given persons specifie 0 APPRO VED 0 REJECTED stration and is Administrator of the Federal Av'ation Admini n Authoriz ation r (S oily) FAA Fight. Manufacturer Inspectio X Standards Inspector Repair Station Person Approved by Transport FM Designee Canada APeworthiness Group n. Certifica te or Signature of Authorized Indivi Date of Approva l or Rejectio er 1999 Designa tion No. . 25th Septemb • 2276237 P.Lowe FAA Fenn 337 4414,4 SDNY_GM_02756562 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243484 EFTA01328600 EFTA01328601 58titi:00- VIA3 Li Pue `ST '01 '6 '8 `t SHdVd9V8Vd H3C18O 3ALLDILCM1d O11J3f8fS C9S9SLZO- INO- ANOS 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.DescrtptIon of Work Accomplished ((mare space is required attach additional sheets. )dennft, lath aircraft natiOnahry andresisamition mark and date work completed) Registration: N407RB Model: Bell 407 Serial No: 53375 TSN: 11.6 hours Helicopter VFR Operation Only The following Avionics equipment has been installed on the above Helicopter: 1) King KX165 NaviComm System 2) Appollo SL60 Comm/GPS System (GPS Stand-alone) 3) King KR87/KDA 692/KA448 ADF System 4) King KRA 71 Transponder 5) King KRA 10A Radio Altimeter 6) King KN 63 DME 7) King KCS 305 Compass System 8) PS Engineering PMA 6000-S Audio Panel 9) ELT AK 450 Material and reference material used for the above installation: King KX 165 (optional equipment) 006-00179-006 Rev Oct/94 Appollo SL 60/gps 560-0957-01 March/97 King KR 87/KDR 692/KA 448 (optional equipment) 006-00184-004 Rev 4 Nov/91 King KT 71 (optional equipment) 006-0615-0000 Rev 0 May/92 King KRA 10A 006-0152-03 Rev 3 Nov/86 King KN 63 006-0176-03 Rev 3 oct/79 King KCS 305 006-00116-0002 Rev 2 Feb/84 PMA 6000-S 200-066-002 Rev 2 May/99 Ameri-King ELT Document No IM-450 All Antenna locations have been mounted in the Manufactures recommended locations. All the above equipment installed has been evaluated and found to be Tso equipment All recorded optional equipment has been installed in accordance with the manufactures installation instructions and the Helicopters Maintenance Manual Reference BHT-407-MM-2 Chapter 8 Page 2 Structural Integrity of installed equipment has been provided by Keyston Helicopters under FAA Form 8110-3 dated: 271" August 1999 Static inverter installation and the gyro mount. Installation of the above equipment has been installed using the manufactures installation Kits Electrical bonding has been evaluated and electrical load analyses has be checked with no adverse effects on other systems. Circuit protection has been provided as required by the manufactures to the ratings require by the installed equipment and located in overhead Panel Post installation checks have been completed as required by the manufacture installation instructions. All relevant placards and instructions have been installed. The GPS has been placarded *GPS Limited to VFR used only" : Compass check swing completed All relevant pilots operating handbooks and operating instructions have been made available to the flight crew. FAA Advisory Circular AC 20-138 Complies with reference to AC 20-678 for Appollo SL 60 as applicable. FAA Advisory Circular AC 43-13-18 Chapter 7 Section 2.3.4 &5 Chapter 10.11 Section 3.4.5.6.7.8.15.17 Chapter 12 & AC 43-13 1A Chapter 1.2 FAR 23-1301 Maintenance for the above installed equipment has been made available as required by the manufactures. Weight Balance and equipment list has been updated to reflect the above changes. Log book entry issued a required by FAR 43-9 O Additional Sheets are attached Ram Apceoved 0 M N 2120-0018 APPLICATION FOR INSTRUCTIONS —Primer TYPO. Do not Arne in shaded areas; than are for FAA 0 . use my Sutott origknal only to an OuthCelled FAA Represtnlativ0. IT addstOnal DA Nommen AIRWORTHINESS space Is required. use an attachment For special night parrot complete Sections ft Tewepouum II and VI or VII AS appacable. ,....is " ey e CERTIFICATE Aca T. REGISTRATION MARX 2 mac - r minor RS NAME MMFM 1 AIRCRAFT MODEL DESIGNATION 4. YR. MFR FAA COD/1I3. I. AIRCRAFT 5. AIRCRAFT SERIAL NO. N61161 Bell HeIICODIer Textron, A Division of Textron Canada Limited. IL ENGINE OULDERS taME (Mako) 407 T. ENGINE MODEL DESIGNATION 1999 Hia2 40 IP DESCRIPTION 6 NUMBER OF ENGWES 53375 ALLISON 5. PROPELLER BUILDERS NAME (Mks) 250-C47B IQ pROPELLERNODEL DESIGNATION I 70 305L AIRCRAFT ES Karst ) 1 N/A WA x I Manila APPLICATION IS HERESY MADE FOR (Corot 'Noma/ ems) " A l X STANDARD ARM:AT/MESS CERTIFICATE fmastar °AWN IXI NORMAL I I UTILITY 1 JACROBATIC J TRANSPORT I I GLIDER I I BALLOON Ts SPECIAL AIRWORTHINESS CERTIFICATE (Chock ancOefabAmm9 2 UNITED 1 CLASS I 5 PROIAMNAL anckaN cc3A/ 2 CLASS II a I AGRICULTURE AND PEST CONTROLX. 2 PERM SURVEYING 3 AERIAL ADVERTI5843 RESTRICTED &cedar° °petard/OMo 4 FOREST (m114 tonsealion) 5 a by conatetc0 PATROLLING 6 %SATHER CONTROL P , 1 CARRIAGE Cf CARGO RESEARr-H AND DEVELOPMENT 0 2 OTHER (SpeoW) AMATEUR BUILT 3 EXIIIBRION 4 UPERIMEIRAL PokotoopeolroW) 4 RACING CREW TRAINING to be concro240) 5 ANT. SURVEY G 0 TO SHOW COMPLY/ICE WHIC FAR 1 FERRY EUZOR FOR REPMR.S. ALTERATIONS. MANTENANCE OR STORAGE 2 EVACUATE FROM AREA OF WINDOM DANGER SPECIAL EMIR PERMIT &Mame 5 Fieralco lo be conAmeect Alto 3 OPERATIONDIEXCESS OF MAXNUM CERTIFICATED TAKE.OFFNEIGHT =r i' W*1VT? 4 DELNERING OR EWORT I ama/cm/awn IS Tunic 6 CUSTOMER DEMONSTRATION MGM C is I ARATIPLE AIRWORTHINESS CERTIFICATE ((AerA MOVE Twisted OperallorIAMIMMAlanfer lemitect•snimleabIt) A. REGISTERED OVMER Ms Van a/cep:4ra data:0 replemron) W DEALER. CHECK Mit -Al NAAR ADoRESI3 BE HELICOPTER TEXTRON INC. P.O. BOX 482 FORT WORTH, TEXAS 76101-0482 B. MOW" CERTIFICATION BASIS (Chock saMarOM Vock• ad coorAereRYms m :n034.0) € x AIRCRAFT SPECIFICATION OR TYPE CERTIFICATE DATA SHEET (Gibe Mx en1 RF.:st iaNo ) AIRWORTHINESSDIRECTIVES (Chock 0al**Was /401carp*/ torn °WOW Mut ADMoJ • H2SW REV. 37 X FAA BI-WEEKLY SUPPL ISSUE 99-12 C ° AIRCRAFT USING (Gnome =stern SUPPLEMENTAL TYPE CERTIFICATE Wit Nankir Of each STChworprNo° N)A X SH13228O - SR00220DE ll C. MRCRAFT OPERATION AND /441PRENANCE RECORDS X CHECICIF RECORDS IN COMPLIANCE WIEN FAR 91.417 TOTAL ARTRARE HOURS 5.6 a ORPERIMEMAL ONLY (EM boors !Wien Axe Ltstomiratto Issutew axed; N/A Id D - I lier actir r into or: . retwornssa. incOr ma=lial bee araft denoted otto; out takral Isp?4 .eriertd swill 5;2 4 Foss 2da.A4Alko AdenWitroro, es9bl IN to siren is codAcato nquestol DATE OF APPLICATION MIRE AND TITLE Pint ct type) SIGNATURE July 02, 1999 Joan Rona Premont - Agent A.1HE AIRCRAFT DESCRIBED ABOVE HAS BEEN INSPECTED AND FOUND AIRWORTHY BY: (Compare Ads sozoo Fay dFAREt MOM) 7 IMPART 121 OR 127 CERTIFICATE HOLDERRAN CERTIFTCATE0 MECHANIC (GeeCedikats No.) CERTIFICATE REPAIR STATION (Gmr Cerettoo*Na) 5 g 2 Ceara°.NO) 3 i i 5 AIRCRAFT MANUFACTURER (Ova name MOW PG 5 4 la 5 i V ' DATE TIRE SIGNATURE I (oftmotAEL **Ws NockFInMost A ev4IV TIM CERTIFICATE REOUESTED A. MAIM the MAMA desoto1M Sea*, I ce MO meets requbeceres Mr 4 AmEADNENT OR MODIFICATION OF CURRENT AIRWORININESSCERTIWATE V. FAA FM INSPECTOR FAA DESIGNEE B. IngtoicoIces pedal IRON pellet undo Stertn VII on conducted W REPRESENTATIVE CERTIFICATE HOLDER UNDER. FARES I I FAR 121.127 or 135 I I FAR 14$ DATE °WW1 OFFICE DESIGNEES SIGNATURE AND NO FM INSPECT 3 SIGNA7 CERT.:MATO.' so_ alviqgsk)pbo-Aft . ...,. , FAA FORM 51304 into FVARGFtea MMUS COMO.. SDNY_GIvl _02756564 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243486 EFTA01328602 .p.,..ay.,Num.w.m.dannvs--.), (P.,......Adco) ( n /1481 • It NV' i . $a*ssosPgsof q pesq•P$0100 sveuAlliqufle wow* 7 Oxypbas ~I 400S0') ICE 00S VW 030e.wriCtenedstl MON a _ a Coeirozer<ospo) 0Y3 IIVA pin4Vtil sirptemlIngsagol walsa Om WANlamb V '1,.. Fig $5..$000.xov is prom *VOW% 00$00.0.0V sro$00d 1 (pospbsnap.q0071/) qo Vwdalmoild '50.110•0 .IM •3 I gP •,1 a sootwan 0 $000d0Paimre papw 1:SOIA02/ u$20. 4Pqn) ,.,/ 14 lisarVIxaul iolvaiimps0 switipsacflasnj q i'N $AKIKIsk1/4 so CM VIM 0ainedUaTI IPOY) 6.0C10 Woolyyj Vauuquop p wale's .0 •00• 0$0$10so3 $4•0$1941PA susIWIRTIIMIsmq. -v .i. 2 atillIMOIS 010ic$Med TW1CINV 3WYN MO PNP:s0P SAW otIl l0) kiximile q put paqqaur yeaq sew yent8 am Ism put 'SuOgelnfiqj U0101q, Wapai aignoidde Pug '8561I0 WV italelAV PaPad €4010 tOS uorPas vim a:tapioca': Li$ $10$4e$01M0 PV $0 01A0 mapai eta trympaJam5ai s$ yeast 010 leM wale PNAOsep Venn asap Gook sty "010111A0 POJOISItel (MUM Oft kW* AciaiN I— Now/ammo ,4 1L SPECIAL FLIGHT PERMIT PURPOSES OTHER TPAS PRO0UCOON FLIGHTIEST (Annoa1p POL:40t1J0 0219 ti011V113($0 33VS U0i ASVS030aN 031$331SHOD 32dVSNOLIVIOSnt 00.510110J 3ki. 1 0/000d Stl 811131(3q$000ISS3NINDIOMMV 319v0lidV 3H11030ION 23001SvIONIV MU V (4,10$5/110110 1 HOLVDMMI I I 10V*03 1 i Wild I 1/091.111103111101alitICAIN auIMMO 01intnnCelitnin "3 monvina 31V0 3110thrvd03 MA 01 IROlid AVVP0ds. se *0*40) 0 Wend souvaismormtGIVOISII0 wow 40 NOtldIU0S03 0 MOHNOUNIUSI001 kratirIVINTUMS 130011 (wri)E1301110 SSAIOCIV WHIM 0303100Th avintsre do NO1104f7330 "V minirmn (.4 4•3 Mid) fl u Ow 311VN NOUV0IlddV SO 31V0 < $03311ONU.M1340 Ii04 03011030 SILVailalr) SO ALAIMO 3M0 .0 IGLUS NO11034.• toxioneow MOWS S MHO 31$.0,010333W. gi (*tam q$050tqappaava)uvoutona Notionaosa Pustora:s•I dovastAlstsvo Nousnomm 13 i !rig Vi - . 5Spiacre 3vM4 witiniovinNwi v SDNY_GM_02756565 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243487 EFTA01328603 ISOM0337160•••••Ca 00W11107 TIMPOOPTATO.-PDXIML AMP°, AOIAISPRATION STANDARD Amworknoess corrinc.Are • •••••••••••nue I UOMPICIL.10.04WOM 3 •Viclwal C•IIICOP• ••••••• BELL HEUOOPTER TEXTRON N61161 CANADA MODEL 407 53375 NORIO/ • •T•0•173 MOOS/ woman ••••• SOO. •••••••• ••••••••• •••••••••• ••• ••••• •••••••• Visit. Ina •••••••••• ••••••• /SS 13, 13•••••••••••• •••••••••••••r Cm* one •••••••rowan* If:SS NONE • TOWS 3.00 \S.•• 111 t•••••••••• 11~•••• Tel •• I m.o.. COPY So • •••••••• nab/ •••••••••••••• 30•4333•3•„•C ut OSS'S:3 / 3.• tea michatna wicisaw swoaD°42""1" ••••••••0034.00•1 FAA Fern 61604 oat. • lit SONYGM_02756566 :T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00243488 EFTA01328604 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 00243489 EFTA01328605 Bell Helicopterit a 4.4. t c1.1.)J Une division do Textron Canada nee May 11, 1999 A Division of Textron Canada Ltd. Federal Aviation Administration Southwest Region Headquarters Manufacturing Inspection Office, ASW-180 2601 Meacham Blvd. Fort Worth, TEXAS U.S.A. 76193-0180 Attention: Mr. Michael Stoat SUBJECT: U.S. STANDARD CERTIFICATE OF AIRWORTHINESS Dear Sir. This is an official request to delegate Transport Canada the authority to issue a U.S. Standard Airworthiness Certificate (FAA form 8100-2) on behalf of the FAA for a new Canadian Manufactured Aircraft. Following is the aircraft data necessary to proceed with certification: NC Manufacturer : BELL HELICOPTER TEXTRON CANADA Model: 407 Serial number 53375 Owner. BELL HELICOPTER TEXTRON INC. P.O. BOX 482 FORT WORTH, TEXAS U.S.A. 76101 Target date for certification is May 28, 1999. Should you require further information, please do not hesitate to contact the undersigned. Yours truly, Jean Rene Premont Q.A. Certification Coordinator JRP:fb End. VACESITIR11 12 800, rue do l'Avenir Mirab I ueboc J7J 1R4 www.hallhealitnotertextrnn.com SDNY_GM_02756568 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024349() EFTA01328606 SDNY_GM_02756569 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243491 EFTA01328607 • Transport Canada Transports Canada Safety and Security Sécurité et sûreté EXPORT CERTIFICATE OF CERTIFICAT DE NAVIGABILITÉ AIRWORTHINESS POUR EXPORTATION This certifies that Ma aircraft identified hetow and described ln the relevant type Ce certificat atteste que t'aéronef indiqué O4eSSCuS et décrit par le certificat do type certificate mentioned herein has been examined and as of the date of Mis certificate pertinent ci-mentionnés a été inspecté et quà ta date du présent documents Il eel conforms to the data forming Me basis for Me typo certificat& a In a conaten for sale Conforme aux prostitutions du certificat de typa, est en en état de service et rail operation and complies with any additl0nal aiW0rtNneSS requirements spathe by suerait eta exigences supplémentaires de rovigabike %boutées par te pays the Importing counuy. raionateur. This certificate does not constitute a flight authority. Ce certificat ne constitue pas une autorisation de vol. • Fourexporta: Po exportation rem: UNITED STATES OF AMERICA • Ths ""lee u Cm atome •. Ed. D une Manufacturer Model Social Number Type certificate No. Constructeur Modéle Numéro de série N' du certificat de type (A) Moral( Bell Helicopter Teston, A Aéronef Div. of Textron Canada Ltd. 407 53375 H-92 / H2SW tin eotelriI Allison Engine Company inc. 250-C47B CAB 847407 IH-19 / ElGL (C) Propeller(s) Hélices(s) Witt Additions' airw0rthaleSS feu ramants- Exigences supplémentaires de navigabilt4 "The rotorcraft covered by this certificate has been examined, tested and found to comply with the type design approved under Type. Certification H2SW, and to be in condition for safe Operation." Exceptons Slave equipment (RADIO & ELT) installed for Ferry Plight purposes as detailed in W fie B amendment I dated June 28, 1999. To be removed prior to or upon reaching destination. Remarks • Observations This certifies that the aircraft described bas been manufactured with aircraft build definition Serial Humber: 53375. In addition, the following were embodied: STC SR00220DE: Air Comm Corp. - Installation of Engine Compartment Bleed Air System STC SHI322SO: Aeronautical Accessories Inc. - Installation of Flite Steps NOTE: Pilot seat only issued st ._ eten» 4e, oésess r MIRABEL, QUEBEC, CANADA .- e%le. eate,y, ... -et 9.4 0022 Th ► ce lb. 02 'Iwo( I> July love de te 99 L. . Theriault For the Mitla« of Transport -Pou relie Caplet of the Typo Certificate are avEmlable on request from Transport Canada. Des copies du certificat de type set g:lisp:nit* sur demande is Transports Canada. Ottawa. Canada KIA 0NZI Ottawa. Canada KIA 0NS 24-0049(9745) Canad'â DNYXel'A02 Sb5 /Ci SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243492 EFTA01328608 SDNYC,N10275b571 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243493 EFTA01328609 Transports Canada Transport Canada .Region du Quebec Quebec Region Aviation civile Civil Aviation Navigabilite aeriennethinyorthiness 700 Leigh Capreol, Dorval, Quebec 144Y 1G7 Vete rilbene Yea Ms NAM 5015-6-7248-A 1999 Non rtanse Ow Ale July 02, 1999 SW MID0-42 Mr. Michael Stoat, ASW-180 Date T —I3 „„ VNS Department of Transport BMS Federal Aviation Administration Mm Southwest Region Headquarters BEC Manufacturing Inspection Office DAL 2601 Meacham Blvd. BPM TDM Fort Worth, TEXAS PBS U.S.A. 76193-0180 IAA49 Dear Sir. ICLT ADW Please find enclosed the following documents for. N61161 cc Original Export Certificate of Airworthiness and one (1) copy Copy of notarized letter of authorization from Bell Helicopter Textron Application for Airworthiness Certificate (1) copy FAA form 8130-6 Copy of letter requesting the U.S. Standard Airworthiness Certificate Copy of Canadian Registration telex Copy of Certificate of Registration Copy of Log Book entries Copy of dated Airworthiness Certificate, FAA form 8100-2 Date of filing: Registered on June 07, 1999 Verified on June 30, 1999 at 14:35 local time FAA Registry AAC-250 Contact: Margo Cherry Yours truly, L. J. Theriault Airworthiness Inspection Representative LJT:fb cc: BHTC CANDOTO4 Canadli! SDNYGlvl02756572 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243494 EFTA01328610 SDNY_GM_02756573 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243495 EFTA01328611 STANDARD AJRWORTIONESS CERTIFICATE ZiVews.c..1.••• ."" :ZA • 1raaNnTerl. METRO Can* WON 407 51178 NOME Mil“.••40.14,04 •••••••01 • FAA Fenn 11002 en, ••14•0. •••••••••• SDNY_GM_O2756574 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 00243496 EFTA01328612 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 00243497 EFTA01328613 *me mimes.. OCIWITMOCI 711.1.0•CSTATtOtt-ICOCRAt MUMS. mahuarnwos STANDARD AIRWORTHINESS CERTIFICATE May.1" t tuntettitt140 van Wow CotIO)In •••••••thottoited Ramo BELL HEUCOPTER TEkTRON N61161 CANADA MODEL 407 53375 NORMAL • Itl•MOTe••••••1410•••UOIa notattotimatootetatot tt fit tots amides tad 'Imre mt.% not Al a otos sta.". tot nal to ten state Iwo blow, oast totl *Ha owns. I tptaattoott est. ot worn to tort istottot rata. twoo• vett to moo um, minas. Et tetrtntoto• w totonottotttr t at t toctottort NONE •TONINOCISCOVII• WIN iiiiiinalweinosal. ma. - • ipanitilm ...nue nisi OP ••••••••••••• OS mann amillsin Slain a liimilinsilo vs, Sawa in San liniiieloveil li• •••••••••••••al4aielli IWO. •••••••••••••••••".... -..-- WC OltilittUICt •••••••••RAW. • cameo. sue a 02 013 P. SW 61100-42 St too ton Tel CalttItIC•Xl Wet It ONOWID a M 001:$1•11 niCil MIN ~St Mania ...co. oraare.s. FAA Fan SIC04 Sas . lit•GA0.11.1•111•16 SDNY_GM_02756576 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00243498 EFTA01328614 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00243499 EFTA01328615