SDNY_GM_02756510 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 REVIEWED AND ACCEPTED SACi FSDO EFTA_00243432 EFTA01328548

SDNYGM02756511 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243433 EFTA01328549

0 MAJOR REPAIR AND ALTERATION of New* Tortcorvalcri (Airframe, Powerplant, Propeller, or Appliance) Minion aerravarreen oroct Tcoo Ft Ort0 W 2120=20 I m°7p1 C.d'ac Truro /Anew 444 ?AA Use O4 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)) 1. Aircraft Nationality and Registration Mark N405PJ Sens No. 53375 Make Bell Hellicopter MOOS 407 Series 206 2. Owner Warne (As shown On regiStratiOn Cernaelde) Helibro. LLC. Address (As shown on regstration Ger:Scots) 401•44 Cent annoy Way Do Red Bluff Sr. CA Le 96090 cons USA 3. For FAA Use Only 4. Type 6. Unit Identification Ropes Metabon Unit Make Model Serial No. ig AIRFRAME (As described in Item I above) El . POIAERPLANT El O PROPELLER CI o APPLIANCE TYPO 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 co Red Rhin shift CA Fortran CertfitAted Methent C. Certificate No ./ Celle-mos Repay Sieben AWTR306C so 96080 cam, USA Caricale0 Maintenance Organ:Alan 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 per 14 CFR Part 43 APP. 8 SagnatureiDate of Autiscsized Inervkluai P Joseph Tierno 5/31/2016 irt 7. Approval for Return to So ieur. Rada to the authoring 9 van Persons specified below. the ail identified in item 5 was Administralor of the Federal Aviation Administration and Is p Approved • nspected n the manner prescribed by the Rejected BY FAA Flt. Standards Inspector Manufacturer Maintenance Organization Peisoni 4910.114 by Camden Department of Transport FM Designee 1 . Repair Sleben Inspection Authonzation Other (SNOW Certificate or Designation No. AvV7R306C Signature/Dale of Authorized Individual 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 all previous alterations to assure continued conformity with the applicable airworthiness requirements. a. Description of Work Accomplished fir more space Is required. SA addieonal sheets Identify with aircraft nationality and regisbation mark and date work completed.) N405PJ Nationality and Registration Mark Aircraft Total Time: 2013.1 Serial Number. 53375 5/31/2016 Date 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

et) VS Cepsientet MAJOR REPAIR AND ALTERATION of Triroportelon (Airframe, Powerplant, Propeller, or Appliance) Federal *Seen AdfiVilitt/a011 Fan, Aprow3 OVB No 21202020 2125,011 flank Tracione %nes Pet FAA Use 001 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)) I. Aircraft Nationality and Registration Mark N405PJ Serial No. 53375 Make Bell Hellicopter Model 407 Series 206 2. Owner Name (As shown on registration corticate) Hehbro. LLC. Address (As shown on registranon certificate) mew AM I anolety Way an fted Sluff s'aN CA 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 O O APPLIANCE Tyra 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 AWTR306C be 96080 o...,, USA ceetaeo MomenanceOpnization 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 per 14 CFR Part 43 El App 8 Signature/Date of nutnicetzeO Ino vid nal PJH Wesley Clark 6/1/2016 910 7. Approval for Return to Service Pursuant to the audio* given persons specified below, the um identified Administrator of the Federal Avlabon Administration and is WA In Item was inspected it the manner Pfesned by Rya Approved O Rejected BY FM Flt. Standards Inspector Manufacturer Maintenance Organization Persons Approved by Canaan Near:mentor TranSped FM Designee I Repair Station Inspection Authorization Other (SPeCifY) Certifiate or Designation No. AWTR306C SignaturerOale of AUVIOriZed 11101VIdlial pii -i 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 Nationally and Registration Mark Aircraft Total Time: 2013.1 Serial Number: 53375 Installation of Aeronautical Accessories, Inc. Collective Safety Cover STCe SH2373S0. 6/1/2016 Date 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

0 MAJOR REPAIR AND ALTERATION u 5 Cepannwt or (Airframe, Powerplant, Propeller, or Appliance) twee.. S Vee Mian adeetioreaen Form Popped melt 120.0020 ii 7 Electronic Tradong Number for FAA Use Only 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 1. Aircraft NOTnallY and Re904rabon Mark N405PJ Serial No. 53375 Mike Bell Model 407 Senes 2. Owner Nan* (As Sheen on registration certificate) Helibro LLC. Address (A7 shown on tegstraton awaken,) weee903 Langley Way 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) 0 O POWERPLANT . . PROPELLER El El APPLIANCE T,st 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 Per 14 CFR Part 43 Apra O SignatureDate of Aultoontied trimneval Derek Spooner PJ0I r i.02 . ,...... .57strfid. 850 7. Approval for Return to Senile* Pinuant to me authority given persons maned bestow. the unit identified n item Actnintstrabtx ea the Federal Aviation Adminsnttn and is I2TAPPROVED 5 was . inspected in the manner pewit. by to REJECTED BY FAA Fit Standards Inspector Marniacturer Mentenance Organgabsa Person Approved by Caned. Department of Transport FAA Pawnee ,( Repair Station Inspeotan Autionzation Other apart Cortificele or Desbnanon No. Awrie304,e Sign ture(Date of Autixerred Indrnduel PJ§.0 - .... (,...—_ .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 Nationality and Registration Mark ACFT TOTAL TIME: 2013 I ACFT Si: 53375 5-4747:74/6 Date 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

lflibr US 3malmeri MAJOR REPAIR AND ALTERATION a Transcorunco (Airframe, Powerplant, Propeller, or Appliance) Rani Amnon Arrestrason ran mowed deans memo M12011 EIKInfle Trad;a9 Mite F.:ea.Use they 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)) I. Aircraft Nana-law and Registration Mark N405PJ Swat No. 53375 Make Bell mods 407 Series 206 2. Owner Name (As shown on registration certificate) Helibro. LLD. Address (As shown on registration certificate) MOWS MI 1 angler), Way Ces Red Bluff owe CA 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 described in mem 1 aeon) O II POVVERPLANT O NI PROPELLER • • APPLIANCE Type 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 AVVTR306C as 96080 co-ow USA unrested Mentenenee Cagenaatten 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 per la CFR Part 43 O APP. 8 Signature/Date of Authorized Individual NH Derek Spooner 5/19/2016 NH 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 BY FAA FR. Standards inspector Manufactwe Maintenance Organization Persons Approves by Ceneclen Deparlrnent Of TIIM$0011 FAA Designee 1 Repair Station Inspection Authortzahon Omer (SPeolY) Certificate or Domination No AWTR3OSC Signature/Date of Authors ed Indondual Derek Spooner 5/19/2016 - ...-,-.. ....._ RON 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 15/192016 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 u5 Moo U.S. AIRWORTHINESS es Tremolo% Fetal Ariake CERTIFICATE AdmInhosalea INSTRUCTIONS - RIO Or NW Oa no. vow In %DM wen: Rana M4 FAA SAM IA Salweved FM Reponlehe. N uee enly. OHM dray an GOSH M Meclort For sway lloy complale Solana Wm, NON& use NAN% R. W. and w as NOON. L AIRCRAFT 0ISCIIP TON I REGISTRATION MARK N405PJ 2 AIRCRAFT BUILDERS IWO Now eel a AIRCRAFT MODEL MIGRATION 407 4. YR. MFR. 1999 FAA C006.43 S. AIRCRAFT SEPAL IC 53375 6 ENGINE OUILGERS NAVE Waal Roils Royce 7 ENCASE Opel DESIGNATION C-478 I HOER CF OOKIES One E. PROPELLER WEBERS POE mw WA 10. WOOLEN MOON OESIGNATION 11. AVICRAFI Raw 1 wasp) WA ,11 I PPM IL Cu MUM.. REQUESTED APW1CATION IS NE RE Or MADE FOR tom marimad I A I i STMCARDAwACOMIESSCERTFICATEnemmema Ii lime` I Ital.' I Pam II Il ....t. .1 Ia.. " n "' an I fr es. 0 SPECIAL AOMORI reNESS CERTIFICATE /Ow answ4444.4 7 PRIMARY 0 UGHTSPORT I I I II PorParach.te I PAINNEMICOM I ION I j ra AS 1 A...or So OTTO OW 5 PROvISICAMI. 1 CIASS 1 ASO 2 COSI I AGIFOCLETURE NO PEST CONTROL 2 0 AERIAL SURREY 3 AERIAL AOVERISC a RESTRICTED Hem varew44 4 FOREST ow S PATROXIN3 6 14 %FATHER CONTROL Hie essa.0 0 eawor OTHER MN*, 1 RESEARCH MOCIEVELOPHENT 2 AMATEUR MT IS 3 EXOTICA' a NA RACING 5 CREW TWANG MARKET SURVEY 0 TO SHOW COMPUNCE WITH THE CSR 7 OPERATING prawn Casey KR WILT AIRCRAFT EAPt %RENTAL OA Iwo son woo on ainvalwas MOM 4 dera me II 1031 a "ewe %mono) a. a.a—C II CREAMING BB COO Liclu-Scol wane se LICHTNTORT IC ONO IONSPAI MOW WO/ ONO WOW., 401420171odOss MEM Wider 621.1W A VIIIANNED OA RESEARCH ANO 0EvElOPMENT I IC rICREwTRAIINN 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, 1•0•• Me I* MP dillaiii• MIR 3 OPERATION IN EXCESS OF 14041111111 OIRTIFCATED TAKEOFF WEIGHT 4 OEUWRIKE OR EXPORTING .LS A PROCIUCTON RICO TWO 0 015TCHERDEOSTRATICN _I FLIGHTS CI 0 WATIPtE ovicarenoss CERT1FC.ATE Owe ode . maramawimrem Mote mast Nosy i 5 a i i III A REGISTERED OWNER (44 04% on wafts 0.40•Ampleta/N IF DEALER. DECK NOTE i I Nme HOMO. LIC MCNEES 903 La-rgley Way Red Blutt CA 96080 0 AIRCRAFT CERUFICATON BASIS wwwireem Dew me Num* Nur re reveal SAM HRCRAFT SPEOFICATION OR TIRE CERTIFICATE SHEET pm ru w, A m • m mu I MCMORT111115$ PRECTNES Want de esieni.A0. a crInee a as/0••••••••• no 64.% stoRncref 444646 a ....444.% a 44 ow des 04•44caro 2016-04 LO AIRCRAFT OK tow•ron. Nertu I SLOREVENTAL TYPE CERTIFICATE (LinotOre Woe SIC ii••••64.0 See snitched C FOOT OPERATIONNO MANTERANCE RECORDS CHECK IF RECCROBIN Id COMANCE NTH 14 ca m NOW191 417 TOTAL 0.4101MIN TOAS 2013.1 3 EXPERIMENTAL ONLY Or ram arnamararmeamme ram. D. CERTIFICATION .1 NNW NO Mal 1 00:0.4•4040411. Ts 49 0 Me Ursa Ors wohno MOM NOON an Me ONO ma (or Na Ho WM *on 44400.0 Com CM ER OM Cede 441101Elo CM opium@ FOCIIII M4111011 ftnit03011.Irid POI M is 0.104.1461 .IN IR FORS A•41.101 ' W. MM'S hOS bon bapecepti MAMBO WIN COATE OF APPUCATION 400016 NAME NC TIRE %Scots/ David McCarnmon Director of maintenance °parallax SIGNATURE . _ I i lig 5 g. 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 CERTIFIC 4A ATED Ci ;red Oft talor. an is I Iz„,,,c„,,,t,....srmo„.......... avedAvT IWWW0TURFA Me Y••••riel OATE ythi2016 TITLE P ada of Maintenance Operatarts SIONATURE David McCarnmon if*/ V. FAA REPRESENTATIVE GERMINATOR Nom ALL 00.4.1400 WA...0) THE CERTIFICATE REQUESTED Pli AIMSINK am amen eremterm $4d0n MI 01448 RION•0 61 6 RI 4 MEMNON CR IROOFCATION OF CURRENT MOVORTHINESSCERTinCATE El amPHoldr a sPaolaSEN moot FM OFECTOR FM DESIGNEE SNOW VII von ocoducled IN CERTIFICATE OZER UNDER H OVA pales I ju CM pen 12101136 1 I14 CFR part 1% OATS MOO/FE00 OFFICE FM INSPECTORS SIGNATURE a DESIGNEE, ...MATuRE„Ip ins, e , I , i FM WSPECIONS CEITIOATO FILE RELE72.ii r MOMIVRE 45.11PR2P( 64 C• PS° ° ai 40 7t &Kasai's 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 I i F NAME ACCRESS S. PRCOJCTION BASS (CAMPS Featt !I PRODUCTION CERTIFICATE On poloolos Oftiler• a..*. --I TYPE CERTIFICATE OTNER C GIVE OUINTITT OF CERTERCAT ES RIOUIRCO FOR OPERATING NEEOS DATE OF APPLICATION NAVE Ate TITLE (PIW a Eva SIGNATURE i.. e g VIA i 1 $ 1 0 i I i1 ETRE • i S A DESCRIPTION°, NRCRAFT REGMTEREOCNANER Ai:CRESS MAZER NOW WOE I. SERIAL NUMBER REGISTRATION MARK B DESCRIPTION OF FLIGHT CUSTOMER DEMONSTRATION WOOS ri fence nroceme FROM TO DEPARTURE DATE CORRUPT C CREW REOUTRE O OPERATE 11TE AIRCRAFT APO ITS EOUIPTIEKT i PILOT I J COPILOT I I FLIGHT ENGINEER 1 IFOTHER/Spso81 O. THE MRCRAFT DOES NOT MEET DC APPUCABLE AMIWORTIONESS REQUIREMENTS AS COLLOR'S FOLLOWNG ResTmenons ARE CONSCEREO NECESSARY FOR SAFE OPERATIC*. al a t eacintent art.:NSW F. CEPTIFKATION • I hiclity MST OW I an Pe legaleted oar Mc Ns wed Me IMMO *WSW Opt NI in* GralirS MUSS, well Vie FORM" ALUOM A... .n 110:0,11.11 eel Tile 03 Mu USW SAMOS 0)0044101ELSE AM IfOloitle Federal AOSTA Rigalka TM INT Pt le teen Memo M NNW* Ps INN detaIten DATE NAME AND TITLE (PAN Of eft yONATURE ma I I I i I I S g v e4 ODIPTION; UMW!" SP Mate. In CangeWem Win 11 CFR San El 9. AT APLAPSOO G Sweeny.* CaVoiny. FAA Fri 81304 Mame el,* MOIRCI .-- it Comp ArecAnness Calico."' I fowlA*31R (Arad. nee sem•TO S Cat OperainE Omen Aeadr4 C COTO. DURSO.. PNROWIONF. etc Mack wee AN•001) I ReMous NtecelNness Colacme lowed *Accord's WM 14 TYR Stow CAR fOOMEMAIOTOO) %,/ 0 Cum" VIII MM Balereelnlonnatka Amiable a AnTeR E WNW Rear one Montan FAA In 337 Mem so IS , * //WWI ANALOTPuig CRIIrmt• ?NAM In Aoxotince NM 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) 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 DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION • STANDARD AIRWORTHINESS CERTIFICATE I tMMNMTFIRYNW 2 IIMAJFACTURER ANO MOM 3 AIRCRAFT SERW CATEGORY REWSTRATION NARKS Bell Helicopter Textron NUIISER N405PJ Canada Model 007 53375 Normal MIMORITY 08•313 FOR MANGE DISS•0/0110MOSCIIIIIIRWIdp•IDNUDUSC FUN+ at Wen IV, IRAN Caled•wra IN utot NW holm iiptOFOFF41md to cat* b to cetfoi *warm M nco•Sien talon's. vete, Ole Flemb•Wernagessett tiOntrati• govt.'s* all Sal wrtrlut, coed Fisowee4 by Am:tab the Caritha en MISS CM M•la atwi a to ••• Deeps ***None*** TERMS MC COMITIONS Ultss woe surentesl monied, rrctot x a •••••tal 4as IF ammo tatiOld W to FM, lothellireit mei 15 ARM al RI D t seamy& pcp t nyrkno• ad *alas anwkeslax•oectsbPs21. 4 sif t' d th Fowl haw Rtglaeas. nworotte rd Dutra a AMMO to Owl Sian DATE OF ISSUANCE FM ITVE4sor DESIGKKOON WibER 05 APR 2016 Thpa Mcce es Datil 0617WP ?macaw ntiket*Fil,*Slitalicariota log torah,* Wa el mar, Stallallromd FO 110•06•01Fola kO, MISCOITFICAIE MAT If %RATION NE WONT M ACC:MINCE wiw OPIWILE FEOCIAL OWEN REMAND/4. FM faun PO:FM.4 I) &amide* Pintas Ha. SDNY_GM_2756524 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15,0 and 17 EFTA 00243446 EFTA01328562

SDNYGM02756525 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243447 EFTA01328563

0 MAJOR REPAIR AND ALTERATION Fare saw., b maxim mom'. uvene Nom Naar O owe 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)) 1. Aircraft Nationality and Registration Mark N405PJ Sera/ No. 53375 make Bell Model 407 Series 206 2. Owner Name (As shown on regisfratiOn certificate) Helibro LLC. AddleSs (AS Shown on registration certificate) mesa oat I 'Ivey Way chi Red Bluff sun CA Ito WOW Coal, uniteglianatspeara 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 il • APPLIANCE Type 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 per 14 CFR Part 43 Awe In Signaturetate of Authorized Individual Pill 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 BY FAA Flt. Standards Impede( Manufacturer Maintenance Organization Persons Aoeewed by Cenadien Department or Transpixl FAA Chnignee 1/ Repair Station inspection Authorization Other (Specny) Ceniicate or Designation _AWTR30 NO. 6C Signature/Date of AL4hon eel Indivdual PJH 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 Naticriaraty and Remstralion Mark Aircraft Total Time: 2013.1 Serial Number: 53375 4/5/2016 Verified equipment that was previously installed while the aircraft was outside the United States: Oale 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

09' MAJOR REPAIR AND ALTERATION US D e oernot of Trresteraten (Airframe, Powerplant, Propeller, or Appliance) Fedetal Avitio* Aerenharanea Fern Apnoea Cede R0 11204020 2.2•201r ereeirole Tricionp Nall her IAA Use Only 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)) I. Aircraft Nationality and Regisualion Mark N491GM Serial No. 53375 make BELL HELICOPTER TEXTRON Model 407 Series 2. Owner Name (As shown on regiStrehOn CeitifiCete) AIR GHISLAINE, INC Address (As shown on reputation certifiCefi) Address ink Frit II K on co WLMINGTON sirs Lig 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 1 above) O Ei POINERPtANT . O PROPELLER O O APPLIANCE Tye* 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 1E9R960Y ae 33309 Cooly U.S.A. Certicarecimainterne Orgargtallan 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 per 14 CFR Part 43 O AC9. 8 Signature/Date of Authonzed Incliv4uat June 13th, 2011 ,C-3;rf-ir. 7. Approval for Return to Service Pursuant to the authority given persons specified below. the unit identified Adnunrstralor of the Federal Aviation Administration and Is a in fern 5 Approved was ll inspected In the manner presumed by the Rejected BY FM Fs Standards inspector Me Persons r auffaCtUes Organization Maintenance Popeyed by Cene00n Deparwirmt or TronspOel FM Designee I Repair Station Inspection Autlyrization Caner (Specify) Ceni tate or Designation No. 1E9R960Y SignatureMate or Auttaxl ed Individual June 13th, 2011 FAA Form 337 num SDNY_GM_02 758528 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 all previous 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 and registration mark and date work completed.) N491GM Nationality and Registration Mark Aircraft Total Time; 791.0 hours. June 13.2011 Date 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

0 MAJOR REPAIR AND ALTERATION u.6 ithweise Few Amovio CM No 21204020 inOCCO? Electronic tracking Number 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 N491GM SM. NO 53375 1. Aircraft Make BELL HELICOPTER TEXTRON Modal 407 Series 2 Ovmer mime (As shawl on registrebon oirShrees) AIR GHISLAINE INC Ackliells (AS Shown on repented certh9Cess) meee•103 FOULK RD ce,,WILMINGTON miseig z. 19803 CeerriUSA 3. For FAA Yee Only 4. Type IL UM IdentekatIon Repair Maratha Unit Make Model Sane Number O El AIRFRAME (As *screed in Item I *On) 0 O POWERPLANT O O PROPELLER O O APPLIANCE Tye 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 444.44201 1 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 per II CFR Pane] O APP 8 SignalunarDate 41Aultenzed Indivcluar SEPTEMBER 4TH. 2008 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 SY FM Flt Standards Inspector Ms/MacKay Maireenance Organization De parimern Parson Approved by Canteen of Transport FM Designee X Repot Staten thWelion Authorization One (Soo*) Carlicate or Desireoor No. 1 E9R960Y Signature/Dale or Authcrized Individual SEPTEMBER 41", 2008 RkL. Ot emi\ FAA Forty 337 004/0 SDNY_GM_02 756530 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 and regisrrabon mark and date work completed) N491GM Nationality and Registration Mark SEP. 4TM. 2008 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

e3 MAJOR REPAIR AND ALTERATION Form Approved OMB No. 2120-0020 (Airframe, Powerplant, Propeller, or Appliance) d I riltIratiMO For FAA Use Only Fe:wit Aviation Awninevinkin Office Identification 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). 1. Aircraft Make BELL HELICOPTER TEXTRON Mote 407 Serial NO. 53375 Nationally and Registration Mark USA N491GM 2. Owner Name (As sham on (*tildes certitude( AIR GHISLAINE, INC. Address (As shown on regedefion corneae) 103 FOULK ROAD WILMINGTON. DE 19803-3742 3. For FAA_Use Only 4. Unit Identification & Type Unit Make Model Serial No. Repair Alteration AIRFRAME X (As described in Item I above) POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. AgencYs Name and Address B. Kind of Agency C. Certificate No. EDWARDS & ASSOCIATES . INC P 0 BOX 3689 BRISTOL TN 37625 U.S. Certificated Mechanic FKFR9300 Foreign Certificated Mechanic X Certified Repair Station 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 SEP/11/2005 Signature of Authorized Individual,/ 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 Inspector Manufacturer Inspection Authorization Other (Specify) BY FM Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection SEP/11/2005 Certificate or Designation No. FKFR9300 Signature of Authonzed Individual ALAN STELZIG fi • onic, SDNY_GM_02 756532 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 con family 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

0 MAJOR REPAIR AND ALTERATION uS Deperar (Airframe, Powerplant, Propeller, or Appliance) el nasometen Federal Aviation Administration Form Approved OMB No. 212041:Q0 For FAA Use Only /end Office Identalcatian 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) 1. Aircraft Maur BELL HELICOPTER TEXTRON Model 407 Sena No. 53375 Nalimarly and Registration Mak USA N491GM 2. Owner Nam (As shown on registration certfrete) AIR GHISLAINE INC. Address (As show en registration certificate) 103 FOULK RD. 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 APPLIANCE Type Manufacturer 8. Conformity Statement A Agency's Name and Address B. Kind of Agency C. Certificate No. EDWARDS & ASSOCIATES , INC P 0 BOX 3689 BRISTOL TN 37625 U.S. Certificated Mechanic FKFR930D LIMITED AIRFRAME RADIO CLASS I / II Foreign Certificated Mechanic X Certified Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse 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 1 - 1 7-0 3 Signature of Authorized Individu James J . Row 7. Approval for Return TO Service Pursuant to the authority given persons specthed below, the unit identified In item 4 was in the man the by nor Adennistratot of the Federal Aviation Administration and is OD APPROVED 0 REJECTED FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) BY FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection 1-1 7-0 3 Certificate or PIVOTS'S'. Signature of Authorized Individual James J. Row 4-0 --1-1<; 12 /4 .5 .....--- FAA Fain 337 Mai SDNY_GM_02 756534 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 end registration mark and date work completed) BELL 407 SN: 53375 N4910M PAGE 1 of 2 Removed the PS ENGINEERING PMA6000 Audio Panel. Installed 1 ea PS ENGINEERING PMAT000S AUDIO PANEL system (ISO C50c, C35d; RICA DO-160b, CO-170, 00-143). using InstI/Operation Man. PIN 200-070-0012, Rev. 12 Sept 2000, 8 EA DWG AV6850. The PMA7000 Audio Panel was installed at F. S. 40 in the instrument panelwhere the PMA8000 Audio Panel was originally installed reference EA DWG, AV6718. Installed 2 ea BOSE@ Series II l X Aviation Headset Plugs in the cockpit, 1 ea adjacent to the standard pilot and copilot headset jacks and 5 ea BOSE@ Series II/ X Aviation Headset Plugs in the cabin, two in the center cabin overhead and three in the aft cabin hatbin, adjacent to each cabin seat, ref. EA DWG t AV8719. Relocated the Sating SPC-5 Static Inverter to facilitate installation of an AirComm Alr Conditioner Kit The inverter was relocated from F.S. 176 to F. S. 160 above the baggage compartment, behind the cabin 'hat bin' using 202413 .040' doubler attached to airframe structure with 'AD' revits, attaching the inverter with 'MS' hardware ret AC43.13-2A, Chap. 2 pars. 21, 22 8 25, 8 fig. 2.9. Relocated the existing P/N 01-0770028-05 Strobe Power Supply to facilitate installation of an AirComm Air Conditioner Kit The Strobe Power Supply was relocated from F.S. 176 to F. S. 184 on the doubler listed above using 'MS' hardware. Relocated the existing N.AT. RS24-020 relay unit to facilitate installation of an AirComm Air Conditioner Kit The RS 24 relay was relocated from F.S. 30 to F. S. 24 Inside the instrument panel console structure using 'MS' hardware. Relocated the existing AK-450 ELT to facilitate installation of an AirComm Air Conditioner Kit Installed a BHT 407-7C0-005-103 ELT Mounting Kt. The AK-450 ELT was relocated from F.S. 35 to F. S. 25 on the 407-706-005-103 ELT Mounting Kit listed above. All work was accomplished referencing BELL HELICOPTER ELECTRICAL STANDARD PRACTICES MANUAL BHT-ELEC-SPM dated 15, NOV, 1996, and BELL HELICOPTER TEXTRON STANDARD PRACTICES MANUAL, BHT-ALLSPM dated 11, OCT, 1996. end BELL HELICOPTER TEXTRON MODEL 407 MAINTENANCE MANUAL 407-MM-1 Rev. 8-01 dated Sept 1998; and in 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. 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. 11.30. 11-31. 11-32, 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 Chapters 1, para. 1 thru 11, & Chap. 2. para. 21 thru 27. Al EDWARDS 8 ASSOCIATES drawings were developed from each piece of equipment's manufactures installation instructions/schematics. and EIHT`s aircraft wiring schematics. The above installed equipment is excluded from real time EMI testing in relation to the FADEC in accordance with BELL HELICOPTER TEXTRON Technical Data Report No. 407.099-096. REV. B, Dated 29 June 1999, in accordance with aircraft Type Certificate H2SW, Note 38. The electrical load of the aircraft does not exceed 80% of the rated generator capacity. The aircraft's new weight and balance was computed. Revised the aircraft's fight manual equipment list Provided Instructions for Continued Airworthiness (ICA), as part of this FAA FORM 337, as addressed by Flight Standards Information Bulletin for Airworthiness FSAW 98-03, using the checklist in HBAW 98-18. The ICA Is now part of the aircraft's Inspection/maintenance requirements. Log book entry made. REF: W/O 'CO2458E4/2-=-,END=---- INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 1. INTRODUCTION: The Bell Model 407 is a FAR PART 27 certified helicopter. The above listed modification is for the installation and relocation of optional systems LAND this field approved FAA FORM 337. 2. DESCRIPTION: The above listed work is to update the aircraft's Audio Panel and ICS System and to relocate existing equipment to facilitate installation on an AirComm Air Conditioner Ka 3. CONTROL OPERATION INFORMATION: Reference each manufacturers supplied Pilots Operators Guides. 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). (b) BELL HELICOPTER TEXTRON BELL MAINTENANCE MANUAL 407-iwn-1, Rev. 8-01 dated Sept. 1998, (or later revision), Chap. 5 - INSPECTIONS; ( NOTE aircraft maintenance manuals are available to each aircraft owner from BELL HELICOPTER TEXTRON} (a) Manufacturer's publications, as referenced in section 8 of this FAA FORM 337. Inspections, maintenance and/or repairs are limited to persons authorized by FAR 43, paragraph 43.3, with the approved current publications, and training. 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 AIRWORTHINESS wirlyakasrocoLnapi (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_02 758538 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

0 MAJOR REPAIR AND ALTERATION US Noreen (Airframe, Powerplant, Propeller, or Appliance) d Tramp:dawn Federal Aviation Administration Form Approved OMB No .2120-0020 For FM Use Only 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). 1. Aircraft Make BELL HELICOPTER TEXTRON Model 407 Serial No. 53375 Nadonatly end Registration Mak USA N491GM 2. Owner Name (As shown on regisbafion certificate) AIR GHISLAINE, INC. Address (As shown on tegisearial certs6cafe) 103 FOULK ROAD WILMINGTON, DE 19803-3742 3. For FAA Use Only 4. Unit IdentfficatIon 5. Type Urit Make Model Serial No. Repair Alteration AIRFRAME described in dem I X ,As above) POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A Agenoys Name and Address B. Kind of Agency C. Cen Prate No. EDWARDS & ASSOCIATES . INC P 0 BOX 3689 BRISTOL TN 37625 U.S. Certificated MeChaniC FKFR930D Foreign Certificated Mechanic X Certified Repair Station 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 JANUARY 17, 2003 Signature of Authorized Individual JEFFREY MCKAMEY ..079 .... sr z y 7. Approval for Return To Service / e t 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 Inspector Manufacturer Inspection Authorization Other (Specify) BY FM Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection JANUARY 17, 2003 Certificate or Designation No. FKFFt930D Signature of Authorized Individual 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 0 APPLICATION FOR GS INOTANT• AIRWORTHINESS abr oC .. 1.—....tnolon - CERTIFICATE 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 50420ISIP30000 Lae an attachment Fee SReCul ligh, peinviscomoleteSeetiens ii 4,4 vi of %Hi as appliCatie 'REGISTRATION MARK Na fa 1 GM SAITO...TT BUILDERS NAME 'mat Bell Helicopter Textron 1 AIRCRAF T MOM °COGNATION 407 A TA Ufa 1999 FAA WOW /11.202,06 S. AIRCRAFT SERIAL NO 5 3 3 7 5 IL ENGINE BUILDERS RAW Limit. Rolls-Royce (Allison) F (NOME MCW. DESIGNATION 250 -C 47 El . -Srtirir a. NUMBER OF ENGINES one S. PROPELLER 'WAGER S NAME .40.44F. N/A It PflOPULER PAODEt OLSGromoom N.MRCRATT IS iCtioca of 400hANN. 0 N/A IMPORT o ..., u 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 t CLASS I S PIAEWLSIONALandca•Van/ 2 CLASS II I AGRICULTURE ANDIESTCONTROL 2 AERIAL SURVEYING 3 oath ADVERTISING 3 AESTFACTED/PLeson 004•MORP•0 co too& von 4 FOREST /MEAN TOWSN.Lapn 5 PATROLLING • WEATHER CONTROL E CAFMMGE OF CARGO 0 OTHER iScx.srl I ITESEAROL APO OfvELOPMENT 2 AMATEUR GUILT 2 EXPIIIITION • EXPERIMENTAL Nyco% P OpF•AL0.A.. se 04 4010040, • RACE S CRIER TRAINING SW SURVEY 0 IOSNOW COMPLIANCE WONT AR I FERRYfoGHT FOR REPASS ALTERATIONS MAINTENANCE OFT STORAGE SPECIAL FLIGHT PERMIT anima 2 EvACUAIE FROLTAREA OF iMPENINNGOANGEIT • OP•OnOn ION/ COMITYTNIE 1/1•0 Stasi VI 0, VN Is S OPERATION 0. (*GESS Or MUMMY CERTIFICATED TALLE-CAF WEIGHT ccnolen NvecogyOle i••••••• pen 4 NUMMI° OR CAROM I 5 I 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 S 4.. •.• i I REGISTERED OXNEWIN • 0 "NOV•Ppen IV MALIK CHECK HERS I A vow. R. C•FACP0 01 .ros PONT Air Ghislaine Inc. ADDRESS 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 '"p A• pROA NO i H 2 SW Revision 40 .., Jr A•RWEIAININESSOMECT IVES Pant AO No i AD 2002-21-51 'Chen a Wo opiate.* ADS compke0 owl. 440 roe B/W 2002-21 ARICRAFT LIVING /GAR PN/4044NeviLo bus s mcorporatea: SH227WE SH1312S0 SH2243S0 SH3289S0 * SOPPLEMENI AL Int aro SH1388S0 SH1990S0 if iCATE Floe os.••• °toothPC 4%0 . po , Mali SR00221DE SR1322S0 C. m*C0.4, 7 OPERATiON AND WONT ENANCE ALCORI)S SR01411AT SR00230DE SR002200E CHECA IT RECOROS TN COMFIJAHCE WITH 'saint" 91.417 TOTAL AIRFRAME HOURS 312. 5 3 ExPEA RANTAL ONLY If FIR MPslumn sole* Iasi no 0.4444 IssIAP RIPARPRI/ 0. CEROSICATION - I Twain CANN* NM I Nomovratoo .... &mamma ALIA 2c00.50 gifA0r1hy No *SOW Orme anyonnens Am Alm imosnmes qoPer, Io ry...gyny el TN: :womb ouwoug ANA, mum list maz•A TARA kens Analyn AM 'A 122E NO Feint fointo Asicei hopAadot, It'd •LIonma a iroymmo wary Frani Myso. rim My mOall roe arts risen n DATE OF APPLICATION November 14, 2002 Ma nAviatIon Group NA AND ME I MAw (A ls swot* , LA•wARR- l; t • Engineering bKaAnin e• conek ill it 1 2 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 COIJOTIONO I 3 * CERTIFICATED IFECHANIC IG.... CanAcoe No . AR 2278237 , CERTIFICATED EPA $TATIONIGN• Kw $ Alf•COM 1 SAANOIAC IVREA iCON name ol 1.“ot DA E November 14, 2002 Ina Phillip R.G. Lowe S./GRAVURE El BI Li ; "33 II li 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 It. • ics<4.1 WC TRAM NAN Samoa vs FAA INSPECTOR FAA OESKINEE a IN CERTIFICATE PLOWER UNDER FARES I IFAR 121. 127 Of 1331 I FAR 515 041f November 14, 2002 04TOUCT OFFICE IFO - Lon • AEA - 35 4 DESIGNLESSIGNAI AND Manfred Herweg OA RT111001EA i FAA INSPECTORS EIGNATuRE 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 • VI. IMODUCT10.4 RANT TESTING A IMMUEACILIIIIR NAME Lr i ADDRESS • H . & PRODUCT ION BASS RCA NA appLcee• AM PROCUCTION CIA TECATE (Gm i pooVegen cvntcas IN.. , TYPE CERTIFICATE ONLY APPROVED PRODUCTION INSPECTION SYSTEM • CONE OUANTITY OF CIAMICATES FOR OPERATING REOUIREO IL OS DATE OP APPICATION NAM* AmTy TITLE IIN.0 vine) SIGNATURE VII SPeChtt MIGHT PUSiT VIAIPOSIES 07.001 THIS PAODUCTION FOCHT TIST 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 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 nee tallti. i R CERTIFICATION- 'AMOY C•naY than lanh• 10941010 OvAW CON luSSEPAII 01 IN 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 goka ny Non SIGNATURE t PO4C. .1 x ' ; 1 f. Sp i It 1 4 o - 'i x A. Ialtrieg a, A LASIMMAS SAO ltsfilsogNil Cofteerce Hot FAR 91.9 Cs SAMNA% 01CcoNsprdir, FAA . Owen 0 IIIPPIAluch sofen NOATTICTI St I °ANN AwpipiNnest CessIcaTiOn IN m•OCti Avoall lattorn.wita ,Np...6) ...CtonalOW•SweLtiralaboesAltacinea # .D. One. ORPR,RTY METROS He HUNG shoo MP.O.dl IC I.Nt.'s, A./purples. GANA.* NSoi AIXOTOnewth FAA 2 1.329 ea tonwawm000to NC O. GANN WAIN &Ad EWAN* INCIIT.PC0 MSS.* e &Kieft • E.Maicte Wait and Manson FAA Form 337 OWN h Nita LHEHHOt * A CUIMM AnitAtNINIS °HEEHAW Issue* pep Accordance LLLIn FAR 21.18301 'Copy analvai * P. The .0110/0100 WON mAwash FINNS 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 N491GM • arnaol*amt rafts natal ••••••1•NAN ••••••• /*INA. ••••••• • •• •••••••••••• •••••••••• •••• -re it., •10.1}•••••• As eons now taam Noah • am. CVO DM Helicopter T%ron 407 1 I- 53375 444 Normal • Tt•••10••00C•OVIC•al 01••••••••••••••••• 4.444.4...440. lievembor 14. 2002 MYI ra0 Harxvp • DART' 11001EA M ONw nos canto ion Cal. IS toe liallOWT MK. WOW IONNIISAA11014 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 CC-tiCCAtt No 1051296/001 UNITED KINGDOM CIVIL AVIATION AUTHORITY CERTIFICATE OF AIRWORTHINESS FOR EXPORT Year Cl Constructer Conan:Wand Constructors Designalke ol Alraalt Aircraft Serial Number 1999 BELL HELICOPTER TEXTRON CANADA 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 Requiernems Special 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 4404444 4.44. x407315 • 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 rfrc. Bell Helicopter Textron, Confide Kodel 407 • AlOartiliPlat •••••••• 53375 /Mal. • "IlliMIMOCCatel•pall Imo 07/02747 •Samuel J 1 en f tascrena sea 30-70173:1-00R1 vs , n'e• CO.WaTC ral *I IVO AI CNOT •• acornora ving OnLICMAS tilDS4 FAA Fenn 5100-2 44. • 411.01.0, 1•14.-11411.10 7 SONY_GIA_02 756548 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 US DePartme(tt d Traaportabon (Airframe, Powerplant, Propeller, or Appliance) FIRDIMIAYMIXI AdnilliSITIV003 Form Approved OMB Ncci V F Fitai OffiCeJden \‘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). 1. Aircraft Make Bell Model 407 Serial No. 53375 Nationality and Registration Mark N407RB 2. Owner Name (As shown on registration certificate) Bell Helicopter Textron Inc Address (As shown on registration certificate) PO Box 482 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 1 above) -- X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 8. Conformity Statement A Agency's Name and Address B Kind of Agency C. Certificate No. PILO Lowe I I Cobbens Mead Haywards Heath West Sussex 81116 37Q England X U.S. Certified Mechanic ARP 276237 Foreign Certified Mechanic Certified Repair Station 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 24th March 2000 Signature of A • t Individual 7. Approval for Return to Service Pursuant to the authority given Administrator of the Federal Aviation persons specified below, the unit in item 4 was in ed in the manner prescribed by the Administration and is ir.3 APPROV D 0 REJECTED FM Plight Standards Inspector Manufacturer X Inspection Authorization Other (Specify) FAA Designee Repair Station Person Approved by Trans Canada Airworthiness Cr Data of Approval or Rejection 25th Muth 2000 Certificate ce Designation No. 2276237 Signature of Authoriz Ind FAA Fem. 337 dare SDNIIGM_027 56552 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243474 EFTA01328590

NOTICE , Weight end balance or operating limitation changes shall be entered in the apptopriatelaircralt record. Ari.elteration.n\us compatible with all previous alterations to assure continued conformity with the apPticable airworthiness requiremetts S.DesciptIon of Work Accomplished (if more space Is reqedrect attach odatonal sheets Mouthwith aireme nationally and regard:fon mark and dare work theapkted) Registration: N407RB Mobel: Ball 407. Serial No: 53375 TSN: 1. The following Avionics equipment has been REMOVED on the above Helicopter: 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 The Installed KY196 Comm has been located in the main radio stack with the King KMA24H Audio panel and King GNS 430 Nav/Comm/GPS using the original Antenna as provided for the Appollo SL60. Installation of the KMA24 AND KY196 Is optional equipment and has been installed in accordance with the Manufactures (Bell) Maintenance Manual BHT-407-MM-1 Section 97-00-00 And the equipment manufactures installation manual reference 006-00695-0003 Rev 3 March 98 006-00586-0002 Rev 2 July 94 The Garmin GNS 430 Nav/Comm/GPS has been installed in the previous location used by the Appollo SL60, with reference to AC21-138 covering installation of GPS equipment as stand-alone Using Installation manual reference 190-00140-02 Rev F Oct 99 which was previously approved under STC No SA00705W1 dated October 2 1998 and placarded as "GPS day VFR operation only Post installation checks completed as required. Continued Airworthiness evaluated at this time and found within the manufactures maintenance instructions covering avionics equipment. AC43-13-1B complied with as applicable covering good engineeririg practices. Weight and balance and equipment list up dated as required. Log book entry issued END O Additional Sheets are attached SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, SDNY_GM_027565.53 15, and 17 EFTA_00243475 EFTA01328591

0 US ciiinnusiii olTranspaithon rerun AdrninIstfi . MAJOR REPAIR AND ALTERATION . (Airframe, Powerplant, Propeller, or Appliance) Ariake ca ", .-"--L, Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification #D - 35.. . t i, INSTRUCTIONS: and disposition 31.000 Print or type all entries. See FAR 43.9 Appendtc lit and AC43.94 (ortiubsequent revision:thereof) for insfructions 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 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft 1 Make Bell Model 407 Serial No. 53375 r : Nationality and Registration Mark N407RB 2. Owner t ' Name (As shown on registration certificate) Bell Helicopter Textron Inc. Address (As shown on registration certificate) PO Box 482 Fort Worth, TX. 76101.0482 3. For FAA Use Only tiltd,e • in crsrnpfine with I've • airworbinessneratiMattliazd aboredesalled inn wrath}, it wend br be an% subject b corona insomit• by 'perm in FAR 43.Seiclea 47 _re- v 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 APPLIANCE Type Manufacturer O. Con ormity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. Phillip Lowe 11 Cobbotts Mead. Haywards Heath West Sussex RH16 3TO. England X U.S. Certified Mechanic 2276237 Foreign Certified Mechanic Certificated Repair Station Manufacturer D. I certify have furnished that the repair and/or alteration made to the unit(s) identified in item 4 above and been made in accordance with the requirements of Part 43 of the V.S. Federal Av herein is true and correct to the best of my knowledge. d on the reverse or attachments hereto on eg lions and that the information Date , -fi • • 4 FAN Winn Signature of Authorized Ind 7. Approval for Return to Service Pursuant Administrator BY to the authority given persons specified below, the unit Identified in item 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and is g APPROVED O REJECTED FAA Fit Standards Inspector Manufacturer X Inspection Authorization Other (Specify) FM Designee Repair Station Person Approved by T Canada Airworthiness Date of Approval or Rejection t 4 we gra Certificate or Designation No. 2276237 Signature of Authorized I 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 entered in the appropriate aircraft record. An aeration must be compatible with all previous alterations to assure continued conformity with the applicable alnaordliness requirements. t 1 • 45 41 1 v I • - . B. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration 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

0 • MAJOR : :it/0+4mM of Transportzion (Airframe, FedertelArliellm AdmInfitntlen REPAIR AND ALTERATION Powerplant, Propeller, or Appliance) Form A OMB pproved No. 2120-0020 For FAA Use Only Office Identification INSTRUCTIONS: Print or type all and deposition of this form. This report 51.000 for each such violation (Section entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions is required by law (49 U.S.C. 1421). Failure to report can re ult in a civil penalty not to exceed 901 Federal Aviation Act of 1958). 1. Aircraft Make Bell Model 407 Serial No. 53375 Nationality and Registration Mark N407RB 2. Owner Name (As shown on Belt Helicopter registration certificate) Textron Inc. Address (As shown on registration certificate) 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 FAAhis 4. Unit Identification 6. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) x POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. 2276237 Phillip Lowe 11 Cobbetts Mead. Barmaids West Sussex RH16 3TC1. Heath England X U.S. Certified Mechanic Foreign Certified Mechanic Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration have been made in accordance with furnished herein is true and correct made to the unit(s) Identified in item 4 and described on the reverse or attachments hereto the requirements of Part 43 of the U.S. F A iation Regulations and that the information to the best of my knowledge. Date 000 LIVW k Z z Signature of Author. :victual 7. Approval for Return to Service Pursuant Administrator BY to the authority given persons of the Federal Aviation specified below, the unit Identified in item 4 was Inspected in the manner presorted by the Administration and is RI APPROVED ID REJECTED FM Fit. Standards Inspector Manufacturer X Inspection A dzation Other (9pArify) FM Designee Repair Station Person Canada by Transport AI s Group Date of Approval or Rejection 4 mAR 2000 Certificate Designation or No. 2276237 Signature or th rized Individual 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 all previous 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_027 56557 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243479 EFTA01328595

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH FEDERAL AVIATION REGULATIONS DATE 08-27-1999 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MODEL NO. MAKE Bell 407 TYPE (Aripktne, ratter, Helicopter, etc.) Helicopter NAME OF APPLICANT Mann Avionics Ltd. LIST OF DATA IDENTIFICATION TITLE Engineering report no. ER00330, N/11 Dated 8-27-1999 Mann drawing nos. 407-1570-107, Rev A Dated 8-99 407-1570-115, Rev A Dated 7-99 407-1570-117, Rev A Dated 7-99 "Structural Analysis for Installation of Misc. Avionics on a bell 407 Helicopter, s/n 53375." "Installation of Avionics Equipment.' 'Gyro Mount' Inverter Top Hot, Static Inverter/Strobe Unit." 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 approval only and is not installation approval. APPLICABLE REQUIREMENTS (LIST OF SPECIFIC SECTIONS) FAR part 27.301; .303; .305(a); .307(a); .337; .561(pre-admt 27-25); .601; .603; .605; .607; .609; & .613 CERTIFICATION Under authority vested by ducction of tho Adrnini-stralor and in accordance with conditions and limitations of appointments under Part 183 of the Federal Aviation Regulations, data listed above and on Attached sheets numbered have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. D Recommended approval of these data I (*) Therefore Fl Approve these data SIGNATURE(S) OF DESIGNATED ENGINEER REPRESENTATIVE DESIGNATION CLASSIFICATIONISI A ric 4. "ifilllitria--- James A. Munda DERV-955065-NE Structures: Chart A: 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

. , • . a MAJOR REPAIR AND ALTERATION us papaw. (Airframe, Powerplant, Propeller, or Appliance) &Trans wn Nam Minion ararrannan Form Approved OMB No. 21204 • For FAA Office identjacatIon tt4 SC INSTRUCTIONS: Print or type al entries. See FAR 43.9, FAR 43 Appends B. and AC 43.9.1 (or subsequent revision thereof) for instructions and imposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed S1,000 for each such violation (Section 901 Federal Aviation Act 195(). 1. Aircraft Make Bell Model 407 Serial No. • 53375 Nationality and Registration Mark N407R8 2. Owner Name (As shown on registration certificate) Bell Helicopter Textron Inc Address (As shown on registration certificate) PO Box 482 Fon Worth TX 7,5101-0482 1. For FAA Use Only 4. Unit identification 6. Type • Unit Make Model Serial No. Repair Alteration AIRFRAME ---------..--(As described rn nom 1 above) ------------ X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name end Address B IBS of Agency C. Certificate No. M.G Magill 73 Cavendish Mead Sunninghill Berkshire SL59TB England X U.S. Certified Mechanic AAP 2543510 Foreign Certified Mechanic Certified Repair Station Manufacturer 0. I certify that the repair sailor alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date 25th September 1999 0 Signature of Authorized Individual M Magill 1. 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit in item 4 was inspected i the manner prescribed by the Administrator of the Federal Av'ation Administration and is 0 APPROVED 0 REJECTED FAA Fight. Standards Inspector Manufacturer X Inspection Authorization r (S oily) FM Designee Repair Station Person Approved by Transport Canada APeworthiness Group Date of Approval or Rejection. . 25th September 1999 Certificate or Designation No. • 2276237 Signature of Authorized Indivi 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

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 and resisamition 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 EFTA01328601

Ram Apceoved 0 M N 2120-0018 0 APPLICATION FOR . DA Nommen AIRWORTHINESS ft Tewepouum ,....is " ey e CERTIFICATE Aca INSTRUCTIONS —Primer TYPO. Do not Arne in shaded areas; than are for FAA use my Sutott origknal only to an OuthCelled FAA Represtnlativ0. IT addstOnal space Is required. use an attachment For special night parrot complete Sections II and VI or VII AS appacable. I. AIRCRAFT DESCRIPTION T. REGISTRATION MARX N61161 2 mac - r minor RS NAME MMFM Bell HeIICODIer Textron, A Division of Textron Canada Limited. 1 AIRCRAFT MODEL DESIGNATION 407 4. YR. MFR 1999 FAA COD/1I3. Hia2 40 IP 5. AIRCRAFT SERIAL NO. 53375 IL ENGINE OULDERS taME (Mako) ALLISON T. ENGINE MODEL DESIGNATION 250-C47B 70 3 05L 6 NUMBER OF ENGWES 1 5. PROPELLER BUILDERS NAME (Mks) N/A IQ pROPELLERNODEL DESIGNATION I AIRCRAFT ES Karst ) WA x I Manila a P , G APPLICATION IS HERESY MADE FOR (Corot 'Noma/ ems) " A l X STANDARD ARM:AT/MESS CERTIFICATE fmastar °AWN IX I 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 I AGRICULTURE AND PEST CONTROLX. 2 PERM SURVEYING 3 AERIAL ADVERTI5843 a RESTRICTED &cedar° °petard/OMo by conatetc0 4 FOREST (m114 tonsealion) 5 PATROLLING 6 %SATHER CONTROL CARRIAGE Cf CARGO 0 OTHER (SpeoW) 1 RESEARr-H AND DEVELOPMENT 2 AMATEUR BUILT 3 EXIIIBRION 4 UPERIMEIRAL PokotoopeolroW) to be concro240) 4 RACING 5 CREW TRAINING ANT. SURVEY 0 TO SHOW COMPLY/ICE WHIC FAR 1 FERRY EUZOR FOR REPMR.S. ALTERATIONS. MANTENANCE OR STORAGE SPECIAL EMIR PERMIT &Mame 2 EVACUATE FROM AREA OF WINDOM DANGER 5 Fieralco lo be conAmeect Alto W*1 VT? 3 OPERATION DI EXCESS OF MAXNUM CERTIFICATED TAKE.OFFNEIGHT =r i' 4 DELNERING OR EWORT IS I ama/cm/awn Tunic 6 CUSTOMER DEMONSTRATION MGM C is I ARATIPLE AIRWORTHINESS CERTIFICATE ( (AerA MOVE Twisted OperallorIAMIMMAlanfer lemitect•snimleabIt) € • C ° ll Id A. REGISTERED OVMER Ms Van a/cep:4ra data:0 replemron) W DEALER. CHECK Mit -Al NAAR BE HELICOPTER TEXTRON INC. ADoRESI3 P.O. BOX 482 FORT WORTH, TEXAS 76101-0482 B. MOW" CERTIFICATION BASIS (Chock saMarOM Vock• ad coorAere RYms m :n034.0) x AIRCRAFT SPECIFICATION OR TYPE CERTIFICATE DATA SHEET (Gibe Mx en 1 R F.: s t i a No ) H2SW REV. 37 X AIRWORTHINESSDIRECTIVES AD MoJ FAA BI (Chock -WEEKLY 0 al **Was /401 carp */ torn °WOW Mut SUPPL ISSUE 99-12 AIRCRAFT USING (Gnome =stern N)A X SUPPLEMENTAL TYPE CERTIFICATE SH13228O Wit Nankir Of each STChworprNo° - SR00220DE C. MRCRAFT OPERATION AND /441PRENANCE RECORDS X CHECICIF RECORDS IN COMPLIANCE WIEN FAR 91.417 TOTAL ARTRARE HOURS 5.6 a ORPERIMEMAL Issutew ONLY (EM boors !Wien Axe Ltstomiratto axed; N/A D to - I lier actir r into or: . retwornssa. incOrma=lial bee araft siren is codAcato nquestol denoted otto; out takral Isp?4.eriertd swill 5;24 Foss 2da.A4Alko AdenWitroro, es9bl IN DATE July OF APPLICATION 02, 1999 MIRE AND TITLE Pin t ct type) Joan Rona Premont - Agent SIGNATURE 5 g i i 5 PG 5 4 la i V A.1HE AIRCRAFT DESCRIBED ABOVE HAS BEEN INSPECTED AND FOUND AIRWORTHY BY: (Compare Ads sozoo Fay d FAR Et MOM) 7 2 IMPART 121 OR 127 CERTIFICATE HOLDERRAN Ceara°. NO) 3 CERTIFTCATE0 MECHANIC (GeeCedikats No.) CERTIFICATE REPAIR STATION (Gmr Cerettoo*Na) 5 AIRCRAFT MANUFACTURER (Ova name MOW ' DATE TIRE SIGNATURE V. FAA REPRESENTATIVE CERT.:MATO.' I (oftmotAEL **Ws Nock F In Most A ev4 IV TIM CERTIFICATE REOUESTED A. MAIM the MAMA desoto1M Sea*, I ce MO meets requbeceres Mr 4 AmEADNENT OR MODIFICATION OF CURRENT AIRWORININESSCERTIWATE B. Ingtoico Ices pedal IRON pellet undo Stertn VII on FM INSPECTOR FAA DESIGNEE conducted W CERTIFICATE HOLDER UNDER. FARES I I FAR 121.127 or 135 I I FAR 14$ DATE so_ al viqg °WW1 OFFICE sk) pbo-Aft . DESIGNEES SIGNATURE AND NO ...,. , FM INSPECT 3 SIGNA7 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--.), _ a (P.,......Adco) ( n 1/481 • It NV' $a*ssosPgsof q pesq•P$0100 sveuAlliqufle wow* 7 i . Oxypbas ~I 400S0') ICE 00S VW 030e.wriCtenedstl MON a pin4Vtil sirpteml Ingsagol walsa Om WAN lamb V '1,.. Fig I g P Coeirozer<ospo) 0Y3 IIVA $5..$000.xov is prom *VOW% 00$00.0.0V sro$00d 1 (pospbsnap.q0071/) qo Vwdalmoild '50.110•0 .IM •3 1:SOIA02/ u$20. 4Pqn) lisarVIxaul iolvaiimps0 switipsacflasnj q ,.,/ papw a soot wan 0 $000d0Paim re •,1 14 2 i'N $A KIKIsk1/4 so CM VIM •0 0$0$ 0• 10so3 $4•0$1941 PA susIWIRTIIMIsmq. -v .i. 0ainedUaTI IPOY) 6.0C 10 Woolyyj Vauuquop p wale's .0 atillIMOIS 010 ic$ Med TW1 CINV 3WYN MO 1L SPECIAL FLIGHT PERMIT PURPOSES OTHER TPAS PRO0UCOON FLIGHTIEST PNP:s0P SAW otIl l0) kiximile q put paqqaur yeaq sew yent8 am Ism put 'SuOgelnfiqj U0101q, Wapai aignoidde Pug '8561 I0 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* A ciaiN I— Now/ammo ,4 (Annoa 1 p POL:40t1J0 0219 ti011V113($0 33VS U0i ASVS030aN 031$331SHOD 32dVSNOLIVIOSnt 00.510110J 3ki. 1 0/000d Stl 811131(3q$000ISS3NINDIOMMV 319v0lidV 3H11030 ION 23001SvIONIV MU V (4,10$5/110110 1 HOLVDMMI I I 10V*03 1 i Wild I 1/091.111103111101alitICAIN au IMMO 01 intnnCelitnin "3 monvina 31V0 3110thrvd03 MA 01 IROlid AVVP0ds. se *0*40) 0 Wend souvaismormtGIVOISII0 wow 40 NOtldIU0S03 0 MOH NOUNIUSI001 kratirIVINTUMS 130011 (wri)E1301110 SSAIOCIV WHIM 0303100Th avintsre do NO1104f7330 "V minirmn (.44•3 Mid) fl u Ow 311VN NOUV0IlddV SO 31V0 S gi Vii !rig . Ii04 03011030 SILVailalr) SO ALAIMO 3M0.0 < $03311 ONU.M1340 IGLUS NO11034.• toxioneow MOWS MHO 31$.0,010333W. (*tam q$050tqappaava)uvoutona Notionaosa Pustora:s • I d ovastAlstsvo Nousnomm 13 5Spiacre - 3vM4 witiniovinNwi v SDNY_GM_02756565 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243487 EFTA01328603

ISOM 0337160•••••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 3.00 111 \S.•• t•••••••••• 11~•••• Tel •• I m.o.. So • •••••••• nab/ •••••••••••••• COPY michatna wicisaw swoaD°42""1" ut OSS'S:3 / 3.• 30•4333•3•„•C tea ••••••••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 May 11, 1999 Une division do Textron Canada nee 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 Safety and Security Transports Canada Sécurité et sûreté EXPORT CERTIFICATE OF AIRWORTHINESS This certifies that Ma aircraft identified hetow and described ln the relevant type certificate mentioned herein has been examined and as of the date of Mis certificate conforms to the data forming Me basis for Me typo certificat& a In a conaten for sale operation and complies with any additl0nal aiW0rtNneSS requirements spathe by the Importing counuy. This certificate does not constitute a flight authority. CERTIFICAT DE NAVIGABILITÉ POUR EXPORTATION Ce certificat atteste que t'aéronef indiqué O4eSSCuS et décrit par le certificat do type pertinent ci-mentionnés a été inspecté et quà ta date du présent documents Il eel Conforme aux prostitutions du certificat de typa, est en en état de service et rail suerait eta exigences supplémentaires de rovigabike %boutées par te pays raionateur. Ce certificat ne constitue pas une autorisation de vol. • exporta: Four Po exportation rem: UNITED STATES OF AMERICA • Ths ""lee Cm atome u •. Ed. D une Manufacturer Constructeur Model Modéle Social Number Numéro de série Type certificate No. N' du certificat de type (A) Moral( Aéronef Bell Helicopter Teston, A 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 ._ oésess r MIRABEL, QUEBEC, CANADA .- eten» 4e, % eate,y, ... e . le -et 9 .4 0022 Th lb. 02 'Iwo( I> July te 99 ce ► love de L. . Theriault For the Mitla« of Transport -Pou relie Caplet of the Typo Certificate are avEmlable on request from Transport Canada. Ottawa. Canada KIA 0NZI 24-0049(9745) Des copies du certificat de type set g:lisp:nit* sur demande is Transports Canada. Ottawa. Canada KIA 0NS 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 July 02, 1999 Mr. Michael Stoat, ASW-180 Department of Transport Federal Aviation Administration Southwest Region Headquarters Manufacturing Inspection Office 2601 Meacham Blvd. Fort Worth, TEXAS U.S.A. 76193-0180 Dear Sir. Vete rilbene Yea Ms NAM 5015-6-7248-A 1999 Non rtanse Ow Ale SW MID0-42 Date T —I3 „„ VNS BMS Mm BEC DAL BPM TDM PBS IAA49 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.••• 1 .""raaNnTerl.:ZA • 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 BELL HEUCOPTER TEkTRON Ramo N61161 CANADA MODEL 407 53375 NORMAL notattotimatootetatot tt fit tots amides tad 'Imre mt.% not Al a otos sta.". tot nal to ten state Iwo blow, oast totl *Ha owns. Itptaattoott est. ot worn to tort istottot rata. twoo• vett to moo um, minas. Et tetrtntoto• w totonottotttr tat t toctottort NONE • Itl•MOTe••••••1410•••UOIa • TONINOCISCOVII• WIN iiiiiinalweinosal. ma. - • ipanitilm ...nue nisi OP ••••••••••••• OS mann amillsin Slain a liimilinsilo vs, Sawa in San liniiieloveil li• •••••••••••••al4aielli •••••••••••••••••".... IWO. -..-- a 02 013 •••••••••RAW. • cameo. sue P. SW 61100-42 WC OltilittUICt 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