el lbv MAJOR REPAIR AND ALTERATION LS Opolnel of Twee:nolo, (Airframe, Powerplant, Propeller, or Appliance) Aware AVIMI011 Awieranneea FormNyasa CMS No 2120-0D20 2126201. (Meow Truk"; Nabs' For ma use Oar INSTRUCTIONS. Print or type all entries. See Trtle 14 CFR 443.9. Part 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and deposition of this form. This report is required by law (49 U.S.C. §4470%). Fain to repot can result in a civil penalty fa each such wolabon. (49 U.S.C. §46301(a)) 1. Aircraft Nationality arid Registration Mani N405PJ Stoat No. 53375 Make Bell Model 407 Series 206 2. Owner Name (As shown on regstrat an certificate) Nelibro LLc. Address (As shown on re9sbahoncertficare) Asssw 9n1 I engirt Way cry fjgg Bluff new CA , LO 96080 Co", USA 3. For FAA Use Only 4. Type 5. Unit iciontificaeon Repair Alteration Unit Make Model Serial NO. 0 0 AIRFRAME (As described in Nem 1 above) O O POWERPLANT . O PROPELLER O O APPLIANCE Type Manufacturer 6 Conformity Statement A Agency's Name and Address B Kind of Agency run is I Redirrinters Inc. U S. COSCOVIO Mechanic 1 Ma rulacturer Aeons 903 Langley Way Foreign Corbkatod mechanic C Cenifoate No en Red Bluff ties CA ./ COrbfiteled Repair Staten Awm306o re 96080 cc..., USA Cereficewa marnawianceOrpentzerion 0. I certify mai tne repay and/or alteration made to the unit( ) identified in item 5 above and described on tne reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation RegLtati at the information furnished herein is true and coned to the best of my knowledge. Extended range fuel per II CFR Pan 43 O APP. El Signature/Date or Authorized Individual Dan McDevitt 3/29/2021 PJH 7. Approval for Return to Service 60tt Pursuant to the authority given persons specified below, the and r0entthe(1 in deco 5 was iMpeded n the manner presaged by the Administrator of the Federal Aviation Administration and is pi Approved O Rejected BY FM Fe. Standards Inspector Manufacturer Ma Menai-ice Organization Pigeons ADOrOvOO by Canadian Deperweint of Iron:wort FAA Designee if Repair Station Inspection Aulhausbon Omer r Certficate or Designabon No. AVVTR306C Signature/Date of Auth ivi onzed Inddual • Dan McDevitt 3/29/2021 --P-JH FAA Form 137 ro-os) 600 SDNY_Glvl_02756410 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243332 EFTA01328448

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record An alteration must be compatible with all previous alterations fo assure continued conformity with the applicable airworthiness requirements. It Description of Work Accomplished Of more space is ntquintd. attach additional sheets. Identify weft &Erase nationality and registration mirk and date *a* completed) N405PJ Nationales aid Registration Mark 3/29/2021 Date Aircraft Total Time: 3747.8 Aircraft Serial Number 53375 1. Verified Installation of Onboard Systems International Human External Cargo Hook System STC itSR02724LA. 2. Instructions for Continued Airworthiness to be performed referencing Onboard Systems ICA Document #123-049-00. 3. Weight and Balance and Equipment List have been updated and inserted into the Flight Manual. 4. Flight Manual Supplement #121-070-00 has been inserted into the Flight Manual. 5. An appropriate logbook entry has been made. -END K Additional Sheets Are married FAA Foos 137 iio-op SDNY_GM_02756411 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243333 EFTA01328449

FAA FORM 8130-6, APPUCAHON FOR U.S. AIRWORTHINESS CERTIFICATE OMB Control Number 2120-0018 Ex bon Dale 01/37/2021 0 APPLICATION FOR U$ ONNYVIOM US AIRWORTHINESS 01 Tnracortom ARMS ARMEN CERTIFICATE Amdmeorailen ourneuenotos .Pml ot typil. DO nOl wItOnShialsO MM. ROW an IN FM NO Nay. SUNNI MOS OW * an 4011043.0 FM R4priNNIEW• If ETIONOMI EOM II MOOT. No EllEcTinerl For spell 11.14 permits ooreolele SectIons II, M. and VII Es Eppbadde { i •a i 1 REGISTRATION NARK 2 AIRCRAFT GUNDER'S NAME nom/ Bell Hell0394014 3 AIRCRAFT MODEL DESIGNATION 407 4 YR IMR 1999 FM CODING Do Ater cow DEit S. ANCRAF 6Pj T SERIAL NO 53375 a ENGI NE °ULCER'S NAME Mow Honeywell Y ENGINE MODEL DESIGNATION HTS900 13130.?-1" 8 NUIABER OF ENGINES OM 4 PROPOSER °MOMS NAME WS. N/A 10 PROPELLER MODEL DESIGNATION I AriceAFT IS 0340. I•4444•FIN N/A 1 IMPORT i a I EA § a APPLICATION IS MOM MADE FOR Mee Nom* raw/ A 1 ARWORTIMESS CERTSCATE macs warn I vow Noma NRHAN4 Tamm. I ewes *am . [STANDARD , SPECIAL AIRINORDNVESS CERTIFICATE /Coco asercom 444.) 7 PR...ARV 0 LIGHT-SPORT Oen Or IMOWS PONII.Pgradva VANamantiOnci Cadet WEN insn ke 2 LIMITED . CLASS I 5 PROwNOWL peausnons) 2 CLASS I 1 AGRICULTURE MID PEST CONTROL 2 AERIAL SURVEY 3 AERIAL ADVERTISING 3 Row ESTRICTED Rem marmI/ 4 FOREST mom 5 PATROLLING 6 WEATHER CONTROL amennon 0 Towne. OTHER isooll I I RESEARCH AND DEVELOPLENT 2 AMATEUR BUILT 3 EXHIBITION 4 AN MONO CREW TRAINING 6 WRITE/ SURVEY 0 SHOW COMPLIANCE WITH THE CFR 2 OPERATING My, Camps KIT BUILT AIRCRAFT OMNIRoe vabw. Fn molow.• conics.. 4. MAN MEN $1031 EXPERIMENTALmem S OPERATING LIGHT•SPORT 6B Combo WE-SRO 44941 4 _ / V ommeno re toetenchiel BC OP...6M 10.400r1 corMame wet 5 pram* mai Wm° WOW atioor2 MOITEPOSS 21 ITO OA RESEARCH MO DEVELOPMENT 9 UNIMMED MCRAE T 9 B MARKET SURVEY 90 EXHIBITOR 9C CREW TRADEIG 9E SNOW COWL WEE WITH THE CFR I FERRY AUGHT FOR REPAIRS. ALTERATIONS. MAINTENANCE. OR STORAGE SPECIAL FLIGHT PERMIT (mica 2 EVACUATE FROM AREA OF IMPENDINGDANGER II commas 4. maw Oen omens US Mr TON 100/00/4 aura VON 3 OPERATION IN EXCESS OF Man CERTIFICATED TAKEOFF WEIGHT 4 DEUVERING OR EXPORTING ISI I PROMICTON FLIGHT TESTING 6 CUSTOMER DEMONSTRATION FLIGHTS C I6 MU TWEE ANWOR INNESS CERTIFICATE Moo MOW veramMtainim- ow Irmssr 4 Tanen anami i i A REGISTEREO OWNER As rewompars• ormstoommag IF DEALER. CHECK HERE n I NAME Helibro. LLC ADDRESS 903 Langley Way, Red Blurt, CA 96080 ET AIRCRAFT CERTIFICATION BASIS (Gm. 00. 6"."...° Mg"' ...." a ..."" NRCRAFT SPECIFICATION OR TYPE CERTIFICATE DATA SHEET I044 Mw , AS o MORINNESS ORECTNES AD SL PPlagnir (CNN somaraw Aca ammwmat avowse e ets anna, a C a vis sin 0 antenten c RdS• N al N/A 1 non...roar 201922: 10/M2019. F. n 10/27/2019 ARCA. 1 T VOW tang pionatall N/A SUPPLEMENTAL TYPE CERTIFICATE AM mar a ea* ISTC nersewed) C AIRCRAFT OPERATION NO IMINTENANCE RECORDS V CHECK F RECORDS IN COWLEVICE WITH 14 CFR NINTH 91 417 TOTAL AIRFRAME HOURS 3117.8 3 EMMENTAL ONLY immeawmammt. ammer. ANN cfemT0 0 CERTVICKTON. I cieN3 NMI em TN topelred lecordavane Tee 49d U NNW SUM Co% 44101 tent MIS 08044010 npolnelol 04044 TM BS OW) of IN. WWI deleted WOW EWEN MOAN mare] tEl INF Milton Admwsnitoon ILSO Mal Oplable FENNO Aasbm Readoot FM 44. or wa.II has Wel niprel40 RPACRIT/ Old NOM be IS DATE Of APPLICATION 10/29/2019 NAME NC TITLE An 4 844 Mark Summits. Member n ie v ex i l l i AIRCRAFT DESCRIBED MOVE HAS SEEN INSPECTED A TIE A , Al•OFOUNO AIRWORTHY BY amigo Mien Cs. • I4 ON / o nit Min FM 25 14 OFR PI/1121 CERTIFICATE HOLDER IOW OtWAAW NO CERTIFICATED MEOMMC (G.400•100.000 3 .0 5 CER TED REPAIR ION tOs. Cam. MO AIRCRAFT MANUFACTURER tow Awe rm. DATE TITLE SIGNATURE g i < 4 S ai a (Oleg ALL MIRY YDS Aws A adili THE CERTIFICATE REOUESTED Abed Etna AMR Slated Ti Sanity VII rates rooms* 4 AMENDMENT OR MODOCATKIN Of CURRENT ARVICRTHOIESS CERTIFICATE 891.12.dan kr Em401.0.6m OREM wide Swam FM INSPECTOR FM DESIGNEE VII was conducied w CERTIFICATE HOLIER UNDER 14 114C". 121 ER 135 I I 14Offl pia 145 DATE ROOF= FM INSPECTORS SIGNAT wDE ERTIFICA ILL REVIEW SIGNATURE 0 7 EMI/ ASO OFFICE /fat f 11.- 4 SIGNATURE NO Zan& Cot 5V76911 5D— Slattrie7e- Aso( FM Forrn 61304 (392018) AA Prins=1 Edwin Superseded EIeditew Fan, • PDF Par 1 ol 2 SDNY_GM_02756412 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 0 0 0 0 O EFTA_00243334 EFTA01328450

I I A MANUFACTURER ItME POORESS II PRODUCTION SAM MOTO Aticgli:•6* ten) PROOUCTION CERTIFICATE (Cs cocOualts OIALION• NORM TYPE CERTIFICATE OTHER C GM QUANTITY OF CERTIFICATES REOURED FOR OPERATING NEEDS DATE OF APPLICATION NONE MO TALE (After WO) SIGNATURE I 0 I 1 I 1 i 4 A DESCRIPTION OF AIRCRAFT REGISTERED WRIER AGGRESS SUNDER !URN MODEL SERIAL NuMSER REGISTRATION IMRE S DESCRIPTION OF FLIGHT CUSTO/AER DEMCSISTRATODN FLIGHTS El ittecklacplatity FROM TO VIA DEPARTuRE DATE DURATION C CREW REWIRED TO OPERATE THE AIRCRAFT AND ITS EOUIPMENT I PLOT I I COPILOT I I FUOHT ENGINEER I OTHER (Sonly1 TM ARCRAFT DOES NOT NEET THE APPLICABLE AIRWORTHNESS REQUIREMENTS AS FOLLOWS I THE F °LIMNING RESTRICTIONS ARE CONSCERED NECESSARY FOR SAFE OPERATION Ns essowasa Inecnaly) F CERTIFICATION- Hirst, catty Rol I as Me ro04asal eta (a ha awn/ cl iho rain daialtaci cos RN mm at a Novato win Fitoonl Arco' Aamnatrisenn accaaanca myth TOR 40 ol Me UMW STaNn Coda 42'01 sum ard makable Fain RA NO, Rey/Rana ard that NA ANNA Pas DM . nspladd we a RN la i.e Som onalboct DATE lIME NO TITLE (Ave or Om) SIGNATURE .-. I 1 ; i F aII.SS IN g I ... / f NMdpbN A li potaina lenamokra oral Manergo n Carotins, Htr. 14 CFR Sams 91.9. 0 Statenwe al Conlanray. FM Fenn 81 30-0 (MRS aeon .manic H Farr Anatolia Carulcatien tor Roan Amin Oath 00017001.0•40 1 8 Ono, Opening Lattelons Alward i c Dia Drassaa. Raeognast I I Provos Arocartorsa Collar Hamad H Aecedanc•Wet la CFR Ssaan 21.185 CAR Mardi attocaseU R Mach anon ISOWO) 1 0 Carl WV* and Dance Hannigan Antes A Ara. E Map Rips we mansion. FM Form 337 (Morn nom regured) 1 J Caron Moat's GUM* lima aNkoratroo WON 14CFR Spew 2110100 (Coo.tisessn , f F Th. raPochon Roarel•SH MatReconlo K LegriScal Anna Stotvaent d Canolarct FM Form 813DIS MINA anon nand) FM FORT 51306(03-20115) Al ROMPS BROM Superseded Electronic FoTnat • PDF Pao 252 SDNY_GM_02758413 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243335 EFTA01328451

UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATIONTEDERAL AVIATION ADMINISTRATION SPECIAL AIRWORTHINESS CERTIFICATE CATEGORY/DESIGNATION EXPERIME PURPOSE 104 MANU- NAME N/A ,0 4 FACTURER ADORESS /..? 0, *W. FUGHT FROM 45 TO A -'• __. N 405PJ MODEL 4' I SERIAL Nd 8 75 BUILDER Bel Hellc. [DATE ISSUANCE 07 Nov 2019 linens sooner surrenderedI ifOsOmodott. wooed. or IS Mannar= ellechre under the conchbonswjesnbed in 14 CFR. Peri 21. Section de a( Nov 2019 en einvoreenese .HALM le 21 21.211. SIGNATURE OF FAA Thiniftwides REPRE (‘ TION OR CAME MG k 547098732 lb a OS hard Monied* nue Foillople irsoinAlcar al AY OF Aft Sam maw elaielmil so Iva moommorri MI FOITIO1 OF THE CIERTIltAlt nimkslleals Fume Alta wilsologer, secara ant WIT Illi 0SIAVIONI TM AffillWATIER TIC AFAUC.ARIMOIA.A11014 Conditions antLimitations -- 1. This aircraft does not meet the airworthiness standards of Annex 8 to the Convention on International Civil Aviation. Operations in airspace outside of the United States will require the permission of the applicable foreign authority. That permission must be carried aboard the aircraft together with this U.S. airworthiness certificate and, upon request, be made available to an FAA inspector or the applicable foreign authority in the country of operation. Operations may be further restricted by the applicable foreign authority. This may include not allowing use of an airport, requiring specific routing, and restricting flight over specific areas. The operator must comply with any additional limitation prescribed by the applicable foreign authority when operating in its airspace. (1) 2. These operating limitations do not provide any relief from any applicable law or regulation. This aircraft must be operated per applicable regulations and the additional limitations prescribed herein. Note that a clearance from air traffic control (ATC) is not authorization for a pilot to deviate from any rule, regulation, operating limitation, or minimum altitude, or to conduct unsafe operation of the aircraft. If ATC issues a clearance that would cause a pilot to deviate from a rule, regulation, or operating limitation, or in the pilot's opinion, would place the aircraft in jeopardy, it is the pilot's responsibility to request an amended clearance. These operating limitations are a part of FM Form 8130-7 and are to be carried in the aircraft at all times and to be available to the pilot in command of the aircraft. (2) 3. This special airworthiness certificate is not in effect during public aircraft operations (PAO). Concurrent public/civil operations are not permitted; the aircraft cannot be operated as a civil aircraft and as a public aircraft at the same time. No weapons or special military mission systems may be added to the aircraft. This airworthiness certificate is not in effect during flights related to providing military services (that is, air combat maneuvering, air-to-air gunnery, target towing, electronic countermeasures simulation, cruise missile simulation, and air refueling). These activities are inherent military, not civil activities. The FM makes the distinction between the authorized flights for experimental purposes, and PAO. Before operating this aircraft under this special airworthiness certificate following a PAO, the aircraft must be returned to the condition and configuration at the time of inspection for the issuance of this airworthiness certificate. The operator must have written procedures for returning the aircraft to the civil configuration. This action must be documented in the maintenance records. The maintenance records and entries must clearly differentiate between a civil experimental flight per this certificate and any other flights. (3) 4. Application to amend this certificate must be made to the local Flight Standards District Office (FSDO) or FAA Form 8130.7 (11/2016) Previous Edison Dated 04-2011 May be Used oriel Depleted Page 1 of 3 SDNY_CM_02758414 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243336 EFTA01328452

SDNY_GM_02756415 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243337 EFTA01328453

Manufacturing Inspection District Office (MIDO). (4) 5. The pilot in command must hold rotorcraft category and helicopter class certificate or privilege. The pilot in command must hold all required ratings or authorizations and endorsements required by part 61. (7) 6. When filing a flight plan, the experimental nature of this aircraft must be listed in the remarks section. (11) ..., .. 7. This aircraft must not be used for Oft, including, burript‘ 'mited to glider towing, banner towing, / target towing, or towing electronic eCeivers or emitters. Thitjai raft must not be used for intentional parachute jumping. (13) 8. If aircraft or engine operating Ilfnlations are exceeded outsickof planned test conditions, an appropriate entry will be made irithe maintenance records. (14) ‘ cat, 9. No person may operate this airc unless it is maintained R:it n inspection program meeting the scope and content described in § 91.409( .-tpe operator must seleet d identify in the aircraft maintenance records one of the following program for.tbe inspections, aircraft: (a) For type-certificated aircraft, a current inspection program recommen ektythegiallaf . urer; or (b) For former-military aircraft, an inspection program recommended by the manufactu r or North Atlantic Treaty Organization (NATO) military service; or (c) An FAA-approved inspection program. Inspections must be recorded in the aircraft maintenance records showing the following, or a similarly worded, statement: "I certify that this aircraft has been inspected on (insert date) per (identify applicable inspection program) and found to be in a condition for safe operation." Note: To extend an inspection interval, the owner/operator must submit a request for that extension with supporting documentation and data to the local FSDO and obtain concurrence from that FSDO. (15) 10. Only FAA-certificated repair stations, FM-certificated mechanics with appropriate ratings, or a manufacturer as authorized by § 43.3 may perform inspections required by these operating limitations. (19) 11. The aircraft may not be operated unless the replacement for life-limited articles specified in the applicable technical publications pertaining to the aircraft and its articles are complied with in one of the following manners: (a) Type-Certificated Products: Replacement of life-limited parts required by § 91.409(e) applies to experimental aircraft when the required replacement times are specified in the U.S. aircraft specifications or type certificate data sheets. (b) Non-Type-Certificated Products: All articles installed in non-type-certificated products operated under an airworthiness certificate issued for an experimental purpose, in which the manufacturer has specified limits, must include in their program an equivalent level of safety for those articles. These limits must be evaluated for their current operating environment and addressed in the approved inspection program. All articles installed in non-type- certificated products in which the manufacturer has specified limits, must include in their program an equivalent level of safety for those articles. The article must be inspected to ensure the equivalent level of safety still renders the product in a serviceable condition for safe operation. (20) 12. For aircraft originally incorporating fatigue life recording systems, the owner/operator must maintain and use the system as prescribed by the aircraft manufacturer and comply with the manufacturer's fatigue life limits. (21) 13. When changing between experimental operating purposes, the operator must determine that the aircraft is in a condition for safe operation and appropriate for the purpose intended. A record entry will be made by an appropriately rated person to document that finding in the maintenance records. (26) 14. Enhanced Flight Vision System (EFVS) operations for the purpose of research and development and/or showing compliance with regulations are not authorized if any component associated with the instrument approach procedure being flown, or any component of the approach lighting system associated with the • • , FAA Form 8130-7 (11/2016) Previous Edibon Dated 044011 May be Used tail Depleted Page 2 of 3 SDNY_GM_02758416 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00243338 EFTA01328454

SDNY_GM_02756417 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243339 EFTA01328455

instrument approach, is inoperative. (40) 15. Kinds of operations authorized: Day VFR flight operations are authorized (47) 16. Night flight operations are authorized If the instruments specified in § 91.205(c) are installed, operational, and maintained per the applicable requirements of part 91. (48) 17. Instrument flight operations are author' the in ruments specified in § 91.205(d) are installed, operational, compliant with the perr:;7 KetequIretherlt f, and maintained per the applicable regulations.The pilot in command Afieve a method tctco, ly with the § 91.319(c) prohibition from operating over densely populated yreas or in congested ainrns. All maintenance or inspection of this equipment must be recorded in tI701rcraft maintenance recor14 nd include the following items: date, work performed, and name and certificate number of person reoining aircraft to service. (50) r , 18. All flights must be conducted Within the geographical area desfribed as follows: Aircraft must remain within the area defined on the attred sectional, while avoiding ensely populated areas, restricted areas, and congested airspace. (53 • 19. Flight over a densely populated a a-Ocip a congestectai ay is authorized per § 91.319(c) only for the purpose of takeoff and landing. The area-ktbe seta cubed by the term "only for the purpose of takeoff and landing" is the traffic pattern. Fertile-purpose of this limitation, the term "only for the purpose of takeoff and landing" does not allow multiple traffic patterns for operations such as training or maintenance checks. This does not restrict a go-around/rejected landing for safety reasons. When avoiding populated areas, aircraft speed and weight must be considered. The information in FM Order 8900.1, Flight Standards Information Management System (FSIMS), regarding set-back distances from spectator areas for aviation events such as air shows or air races may assist in determining a suitable space to fly the aircraft. (55) 20. Flight in RVSM-designated airspace is prohibited. (58) 21. No person may be carried in this aircraft during flight unless that person is essential to the purpose of the flight. (61) Larrie Ricca, DAR 547098732, Seattle MIDO, AIR-872 - END - FAA Form 8130-7 (11/2016) Previous Edibon Dated 04-2011 May be Used until Depleted Page 3 of 3 SDNY_GM_02758418 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00243340 EFTA01328456

SDNY_GM_02756419 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243341 EFTA01328457

\ wi t • , 44-222. SA, ; p.4. V!. r. • :421 17 4 0$ h • sty .c-FMNO PI CISO - rif t ISO IROFF(Ill$1 St, I ASOS I Zell, pS4/11 .5.7 At.s.0 G , s ..o.eoceuti..i. tat. Q411 • $5 WA i y W r A a I 1 . 1 law etunico ..." 1 . ..1 % • ' Lunc*It I Tat3. ( WI011.07' %. $1C MIMI • • - 33. atplas nitre 1- +se.) • .. • .P., q. i I • .1- . ...la. -. k ) Waal° MI $' IM6 tftww2c224.. CC. I ! 'l e • 1 I ink). 24 • re****. .2 . ..,':,, . • ., 02 ? I, . ,f; gar gleg t. ' L es- • .. ,_...2i4 r.s......____ • pa. .L esiapi; _ ... _ . _ .7112%...10•L _...... ILL lite 1).ThiOR:: 2229A " ' 4-14 ',OCAS (IMO PP MOS OS .0 e 12 f car $ • ! • , Wfst?'44."—^—i ert: yo, ..Nhpt 7?4,11 0000 - REVIEWED AND ACCEPTED SAC: VS00 .05 Atte 12 1 Me • l ItION 4eAlf ....att.. -',..-1, .-.. rc. AS $ --I•S" A --1 - 1 • • :' .1/4 .1 0500 MU • S I; 122.214 . :$4 Aft:),:: I •'; 12.500 e 14/31. , . f 1 1 0 8 - i ikaWiqr*P7 ise'767,.. 5 ' SDNY_GM_02756420 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243342 EFTA01328458

SDNY_GM_02756421 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243343 EFTA01328459

SPECIAL AIRWORTHINESS CERTIFICATE CATEGORY/DESIGNATION EXPERIME PURPOSE R A griebPiiiiil , r MANU• NAME N/A , y %I • FACTURER ADDRESS N/ %;;:". sA Co& FLIGHT FROM A • " 't? TO st N405PJ MODEL 4O SERIN. 75 BUILDER Bell Hellcop I DA ISSUANCE 07 Nov 2019 Unless sooner StaraticIsted re wrrunaeon sfleune under lee ..• in 14 et 21. Section21.t921217. dale 42 Nov 7019 th4 ainnoelttineSS ourodicata i: SIGNATURE OF FMREPRESktital .kt, \ ,i e , 1'4 : - -•1,- 71040401MM NO. 547098732 me MY_ 441144•444 woman Sao* MeeT .....Z.,:grat=.4:trre re=r it 140.1•••101dte••••••••1••••••1 Cho Maui* Mr WRIT DethiArtitnalle mato/ KA ME atusoiohis -- C f%itions andLimitations -- 1. This aircraft does not meet the air hiness standards of Annex 8 to the Convention on International Civil Aviation. Operations in airspace o side of the United States will require the permission of the applicable foreign authority. Th ermission must be carried aboard the aircraft together with this U.S. airworthiness certificate an n request, be made available to an FAA inspector or the applicable foreign authority in the count o eration. Operations may be further restricted by the applicable foreign authority. This may inc not allowing use of an airport, requiring specific routing, and restricting flight over specific areas. The operator must comply with any additional limitation prescribed by the applicable foreign author' y when operating in its airspace. (1) 2. These operating limitati do not provide any relief from any applicable law or regulation. This aircraft must be operated per pl le regulations and the additional limitations prescribed herein. Note that a clearance from air traff ol (ATC) is not authorization for a pilot to deviate from any rule, regulation, operating limitation, or Ximum altitude, or to conduct unsafe operation of the aircraft. If ATC issues a clearance that would a pilot to deviate from a rule, regulation, or operating limitation, or in the pilot's opinion, would ce the aircraft in jeopardy, it is the pilot's responsibility to request an amended clearance. These op ng limitations are a part of FAA Form 8130-7 and are to be carried in the aircraft at all times and to be table to the pilot in command of the aircraft. (2) 3. This special ai iness certificate is not in effect during public aircraft operations (PAO). Concurrent public/civil perakion re not permitted; the aircraft cannot be operated as a civil aircraft and as a public aircraft at th aVtime. No weapons or special military mission systems may be added to the aircraft. This airworthine certificate is not in effect during flights related to providing military services (that is, air combat maneuvering, air-to-air gunnery, target towing, electronic countermeasures simulation, cruise missile simulation, and air refueling). These activities are inherent military, not civil activities. The FAA makes the distinction between the authorized flights for experimental purposes, and PAO. Before operating this aircraft under this special airworthiness certificate following a PAO, the aircraft must be returned to the condition and configuration at the time of inspection for the issuance of this airworthiness certificate/The operator must have written procedures for returning the aircraft to the civil configuration. This actioii must be documented in the maintenance records. The maintenance records and entries must clearly (fferentiate between a civil experimental flight per this certificate and any other flights. (3) 4. Ap ic / ation to amend this certificate must be made to the local Flight Standards District Office (FSDO) or FM Form 6130.7 (11/2016) Previous Edition Dated 04.2011 May be Used until Depleted Page 1 of 3 SDNY_GM_02756422 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00243344 EFTA01328460

SDNY_GM_02756423 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243345 EFTA01328461

Manufacturing Inspection District Office (MIDO). (4) 5. The pilot in command must hold rotorcraft category and helicopter class certificate or privilege. The pilot in command must hold all required ratings or authorizations and endorsementOequired by part 61. (7) i 6. When filing a flight plan, the experimental nature of this aircraft must b Jed / Vit in the remarks section. (11) --..:- • 1 1‘ 7. This aircraft must not be used for win — &including, bu nipt 'm der towing, banner towing, ,., target towing, or towing electronic eceivers or emitters. Thfstai‘ ust not be used for intentional parachute jumping. (13) .. / 8. If aircraft or engine operating limitations are exceeded outs f planned test conditions, an appropriate entry will be made in the maintenance rec 9. No person may operate this aircrafs unless it is mai n inspection program meeting the scope and content described in § 91.409( Ate operator mu d identify in the aircraft maintenance records one of the following program for the inspectio aircraft: (a) For type-certificated aircraft, a current inspection program recommen by,th trio urer; or (b) For former-military aircraft, an inspection program recommended by the man urtei or North Atlantic Treaty Organization (NATO) military service; or (c) An FAA-approved inspect' ogram. Inspections must be recorded in the aircraft maintenance records showing the following, r similarly worded, statement: "I certify that this aircraft has been inspected on [insert date] per [iden applicable inspection program) and found to be in a condition for safe operation." Note: To extend n inspection interval, the owner/operator must submit a request for that extension with supporting documentation and data to the local FSDO and obtain concurrence from that FSDO. (15) ‘,„' 10. Only FAA-certificated repair statio '4:FAA-certificated mechanics with appropriate ratings, or a manufacturer as authorized by *I \ 3 y perform inspections required by these operating limitations. (19) \\1 '.1j 11. The aircraft may not be opera unless the replacement for life-limited articles specified in the applicable technical publicatio irtaining to the aircraft and its articles are complied with in one of the following manners: (a) Type- cated Products: Replacement of life-limited parts required by § 91.409(e) applies to exper' al aircraft when the required replacement times are specified in the U.S. aircraft specificatio or ty rtificate data sheets. (b) Non-Type-Certificated Products: All articles installed in non-ty ed products operated under an airworthiness certificate issued for an experimental purp h the manufacturer has specified limits, must include in their program an equivalent level of t ose articles. These limits must be evaluated for their current operating environment and dre ed in the approved inspection program. All articles installed in non-type- certificated products iry hich the manufacturer has specified limits, must include in their program an equivalent level of saf&y for those articles. The article must be inspected to ensure the equivalent level of safety still renders the product in a serviceable condition for safe operation. (20) 12. For aircraft originally incorporating fatigue life recording systems, the owner/operator must maintain and use the systein as prescribed by the aircraft manufacturer and comply with the manufacturer's fatigue life limits. (21)/ 13. When chinging between experimental operating purposes, the operator must determine that the aircraft is irla condition for safe operation and appropriate for the purpose intended. A record entry will be made J,fy an appropriately rated person to document that finding in the maintenance records. (26) 14. Enj nced Flight Vision System (EFVS) operations for the purpose of research and development and/or show' g compliance with regulations are not authorized if any component associated with the instrument app ach procedure being flown, or any component of the approach lighting system associated with the FM Form 8130-7 (11f2016) Previous Edition Need 04-2011 May be Used until Depleted Page 2 of 3 SONY_Gld_02756424 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243346 EFTA01328462

1 SDNY_GM_02756425 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243347 EFTA01328463

Instrument approach, is inoperative. (40) 15. Kinds of operations authorized: Day VFR flight operations are au orized (47) 16. Night flight operations are authorized if the instruments speci ed in § 91.205(c) are installed, operational, and maintained per the applicable requireme is of+art 91. (48) 17. Instrument flight operations are auths5Ozed-ittb-el ents specified in § 91.205(d) are installed, operational, compliant with the perfor acice require f, and maintained per the applicable nit regulations. The pilot in command ,spiave a me Al • van ly with the § 91.319(c) prohibition from operating over densely populated areas or in coil( " airways. All maintenance or inspection of this equipment must be recorded in tleaircraft mainte arice records nd include the following items: date, work performed, and name and certificate number of person rEo ning aircraft to service. (50) I t.: / --.., ;\ 18. All flights must be conducted ithin the ge grAiphical area. des' ribed as follows: Aircraft must remain within the area defined on the at ched se al, while avoiding ensely populated areas, restricted areas, and congested airspace. (53 ::. ( 5-) e;•:' 19. Flight over a densely populated ar to a congested., ay is authorized per § 91.319(c) only for the purpose of takeoff and landing. The ar A it* susfee cribed by the term "only for the purpose of takeoff and landing" is the traffic patter . Flirthe-pur ose of this limitation, the term "only for the purpose of takeoff and landing" does no How ultiple traffic patterns for operations such as training or maintenance checks. This does strict a go-around/rejected landing for safety reasons. When avoiding populated areas, aircraft spe eight must be considered. The information in FAA Order 8900.1, Flight Standards Information a a ement System (FSIMS), regarding set-back distances from spectator areas for aviation events such / it shows or air races may assist in determining a suitable space to fly the aircraft. (55) / 20. Flight in RV5M-des' ed'airspace is prohibited. (58) 21. No person may be the flight. (61) d in this aircraft during flight unless that person is essential to the purpose of Carrie Ricca, DAR 8732, Seattle MIDO, AIR-872 • END - FM Fart 8130-7 (11/2018) Previous Edition Dated 04-2011 May tN Used snail Depleted Page 3 of 3 SDNY_GM_02756426 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243348 EFTA01328464

SDNY_GM_02756427 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243349 EFTA01328465

ITIGN MA) 630 - 2\ r••• 3WELI. a 14 A ?\ • Xl° 1,S"..'.•. . Clots DM cal O •C• 4 X:MetVciii earl /Pia ku 4 ' :. %-tat nwcar c L:;:z SDNY_GM_02756428 •-x . • 4 0500 :r%4 --- • 7. 12,503 1 4 • I ••• 0/14(K sPos REVIEWED AND ACCEPTED SACS VSDO ' Ogg Zito I i2 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243350 EFTA01328466

SDNY_GM_02756429 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243351 EFTA01328467

• VOTED STATES Of AME/OCA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE 1 NATIONALITY ANO 2 MANUFACTURER AND 41000. 3 ARCRAFT SEROL I CATEGORY REGISTRATION MARLS Bell Helicopter Textron Canada Model 407 KAISER 53375 Normal $ Al/114CRITY ANO BASIS FOR iSSWACE Ilks mows. coVcat %sad "Aunt,/ USC $ WO. in, man as c2 Pe Salt attar* mot New map* bat atenetrobaiucinten ia be rocatienteret, 414040, 3W kr fa MS 44V Ns pen OK•as n t nbnM'baN IOWA 0:4NASOIRINCetMidarotwtocoNyn pen* !Om.. UN Cane ieinnou OW Myer taw n %ea ErA04044 ***None*** 6 TERNS AI..13CONVUONIS • oven now anars moNNIof onlie •• bowersLoeb claw abate N ry FAA ea NWIWOIS cs*gs Own +Ws AIN tranaiwo ovonolmo flying°. aid staslow vs ovIanmo NRNYO• ell FYN 3 43 RN II 3456 Make Nitta** nignoile arn tar ettil thaw SINN OATS Cs ISSUANCE SERRE DESIGNATION NUMBER 05 APR 2016 T Tha ssYRVIGelree z oART/106I7VVP 11 AN swan "nolo, e. none d wetsnet ".44,4•4444 able ac**3•9 OP, 40 44440,44. egoNIMI 3104540043 CERTSCATE BE OISPIAIED II ARCWT ASEORDANCE wilN/P/UCASIE FEDERAL AMIN REGULAIGIS FM Fe e• 6100.2 OH-Ill Sup4•114•0104‘444 Ed.300 kemis 7747Eo 08 /40 Q 7013 SDNY_GM_02756430 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243352 EFTA01328468

SDNY_GM_02756431 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243353 EFTA01328469

HELIBRO LLC APPOINTMENT OF AUTHORIZED REPRESENTATIVE To whom it may concern. Man Ownerftrustee of Helibro LLC Mar% Gunsauls as an authorized representative may conduct business and has signatory authority for Helibro LLC Mark Gunsauls s also knarm as a legal "tviember to conduct business and has signatory authority to do so as a Member. Signature Maliiller 6 11-/ r1 Notary 511 CIALCILfirt Signature Notary Confirmation Wow: Rife Dale SDNY_GM_02756432 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243354 EFTA01328470

SDNY_GM_02756433 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243355 EFTA01328471

CALIFORNIA ALL-PURPOSE ACKWOWLEDGMERIT CIVIL CODE § 1189 ,CdSaCajcsjsSaerrattesrma t •r, rOCAV4S4CaliCALCOCCACCIteCettealtairrel,"Wn,"raWe el"..Wall A notary public or other officer completing this certificate verifies only the identity of the individual who signed the document to which this certificate is attached, and not the truthfulness, accuracy, or validity of that document. State of California County of 4/ katvra On Mau, LS+, 0i before L -Dean/la F7em ;visi Date Insert Name and flue he Officer personalty appeared KG r C aust ift cti :Arc Name(s) of Signeifs) who proved to me on the basis of satisfactory evidence to be the person(s) whose names) is/are subscribed to the within instrument and acknowledged to me that he/she/they executed the same in his/her/their authorized capacity(ies), and that by his/her/their signature:O) on the instrument the person(s), or the entity upon behalf of which the person(s) acted, executed the instrument. r sEr pionwy pow - CaMornia TRISH MANNA RISS ara • COLN)/ ", e 2160218 - M Comm E res Jul i8 2020 Place Notary Seal Above I certify under PENALTY OF PERJURY under the laws of the State of California that the foregoing paragraph is true and correct. WITNESS my hand and official seal. Signature, triAbelk.00.1 0 4 itAtivi Signature of Notary Public OPTIONAL Though this section is optional, completing this information can deter alteration of the document or fraudulent reattachment of this form to an unintended document Description of Attached Document &pa 't vrictite_ Title or Type of DoCument: AffolirErnitivf t k14-0,-acuocument Date: D5/o//aei7 Number of Pages: t Signer(s) Other Than Named Above: r -/A Capacity(les) Claimed by Shreds) Signer's Name: fl Corporate Officer — Title(s): O Corporate Officer — Title(s): Partner — O Limited O General O Partner — C.) Limited O General _I Individual O Attorney in Fact K Individual O Attorney in Fact fl Trustee O Guardian or Conservator O Trustee O Guardian or Conservator :1 Other: O Other: Signer Is Representing: Signer Is Representing: Signer's Name: 02014 National Notary Association • vAvw.NationalNotary.org • Item 45907 SDNY_GM_02756434 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243356 EFTA01328472

SDNY_GM_02756435 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243357 EFTA01328473

October 29, 2019 Federal Aviation Administration Attn.: James Sprecher 2200 S. 216th Street Des Moines, Washington, 98198 SUBJECT: Program Letter for Special Airworthiness Certification REGISTERED OWNER: Helibro, LLC BUILDER: Bell MODEL: 407 SERIAL NO: 53375 Dear Mr. Sprecher: DESIGN CRITERIA: Research & Development NUMBER OF ENGINES: I NUMBER OF SEATS: 7 REGISTRATION NO.: N405PJ The purpose of this letter is to request a special airworthiness certificate, in the experimental category, for a Research & Development Airworthiness Certificate in accordance with Title 14 Code of Federal Regulations (14 CFR), § 21.191(a). This request is made to support company flight testing in support of FAA Project Number ST17247LA-R. The STC will be for the installation of a Dual Cargo Hook System on Bell Model 206 and 407 aircraft. The proposed Flight Testing will be conducted over I — 3 hours on or around the 7th of November, 2019. We request the designee hold the Standard Airworthiness in suspension until the completion of flight testing. The aircraft will be located at 13.1 Helicopters facilities in Red Bluff, Ca. The aircraft is within current maintenance, has been conformed to the TCDS and the following has been accomplished: • FAA Form 8130-6, with sections I, II, and III completed is enclosed. • The aircraft has been properly registered. • We have weighed the aircraft to determine that the most forward and aft center of gravity positions are within established limits. The weight and balance report is available at the aircraft. • The marking requirements of 14 CFR Part 45 have been complied with, including permanent application of appropriate registration marks and the word "EXPERIMENTAL" near each entrance to the cabin or cockpit. • The aircraft is inspected and maintained in accordance with the Bell Helicopter Maintenance Manuals. The following is a description of the requested geographical areas for flight testing: within the box defined on the attached sectional, while avoiding densely populated areas and congested airways. I request Larrie Ricca, DARF 547098732, be delegated to issue the requested airworthiness certificate. My telephone number is: (530) 527-5059. Please contact me at this number if there are any questions or if additional information is needed. Sincerely, David McCammon, Director of Maintenance - 135 Helibro, LLC Page I of I SDNY_GM_02756436 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243358 EFTA01328474

SDNY_GM_02756437 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243359 EFTA01328475

• I. FAA FORM 8130-6, APPLICATION FOR U.S. AIRWORTHINESS CERTIFICATE OMB Control Number 2120-0018 Expiration Date 01/31/2021 0 APPLICATION FOR U 5 ONAFIRAN U.S. AIR WORTHINESS cd Tamp~a nen mimeo CERTIFICATE AdWalental INSTRUCTIONS -Pm or type. 04 noll *We In Macled areas. these we for FAA use °Sy Storni WORN only b an aulhartred FAA Resesemese it Fat II9o4 •00borai space n ralursa, We alladorneK Ks* 994913 compSte Secbons II. VI. and VI IR 11904601e. I -• I. REGISTRATION MARX N405FU 2. ~RAFT BUOSERS NAME Mos BINHelicopter3 3. AIRCRAFT MOOS DESIGNATION 407 4 YR 6WR 1999 FAA COOING Do nter colt Dix S AIRCRAFT SERIAL NO 53375 G. ENGINE BUILDERS NM! Mewl Honeywell 7 ENGINE MODEL DESIGNATION 1478900 $ib° O. P..-1- a SAUER OF ENGINES One 9. PROPELLER BUILDERS NAME Mew WA ID PROPELLER MODEL DESIGNATION 1 AIRCRAFT IS temp emowsst WA I IMPORT C I I SA S al APPLCA14344 IS HERESY MADE FOR raw whom ammfr ~at twain areas Mutat, fats A 1 STANDARD AIRWORTHINESS CERTFCATE Momorao~t I 4~ pour, • I SPECIAL AMWORTHINESS CERTWICATE ~ ms444.4 SW) [ 7 PESSARY I I LIGHT-SPORT ~ pm ANTNne POneraCtsA0 WaimadraPPConetd 0104 lateen At 2 LISTED 1 CLAW I 5 PROVISO/Mt solow cow 2 CLASS II 1 AGRICULTURE ND PEST CONTROL 2 AERIAL SURVEY 3 AERIAL ADVERTISING 3 RESTRICTED nows~orma ~~~ 4 FOREST nen ~mow 6 PATROLLING I MEATIER CONTROL 0 OTHER /7~0 I e RESEARCH NO DEVELOPMENT 2 AMATEUR BUILT 3 EXIMITION 4 MR RACING S CREW TRIMaIG 6 KW SURVEY 0 SHOW COMPUANCE PATH THE CFR ) OPERATING Mamoyessont KIT SALT AIRCRAFT Enorm imate 4~4 a, Nromosemss ottalleas IS OF ra ~5103 I ExPE RAW Wm. 0 OPERATING USTI-SPORT SO 0914~ UWWSsel rasa 4 z tHa c44 nos .44.40) IC OPIWIRO I044031~~TIMISSIMMW10 4. 44144NOTIN arillano ~X 5 steolhaym 21.193 9A RESEARCH AND DEVELOPMENT 9 ~WINE° /PROMPT 90 ~BET SURVEY 90 ONDITION SC CREW TRAINING SE SHOW COMPVANCE WITH THE OFR I FERRY 11.~ FOR REPAIRS. ALTERATIONS. AAWIENANCE. OR STCMAGE SKOP/ FLIGHT PUSSY PM.F. 2 EVACUATE FROM AREA Of 80040.4 DANGER a en* lit ~act enste Sean Ow Vt 444404aVe al mew 4441 OPERATION IN EXCESS OF MAXIMUM CERIFFCATIO TAKEOFF, MGM' 4 DEUvERAFG OR EXPORTING 6 PROIXICNONFUOI4T MUM 6 CUSTOMER DEMONSTRATION FLIGHTS C I6 MU MU AIRWORTIINESS CERTIFICATE stmorson 1444~044~anslamNee.~4•4as 4PRKIN ; i d A REGISTERED OWNER /M mos 0•10,01;* CI ebnitatifesiall IF outman= HERE n I NAME lielibro. LLC ADDRESS 903 Langley Way, Reg Bluff CA 98080 BAIRCRAFT CERTWICADON BASIS Kees men .am. meortsa 4.... m nom* AIRCRAFT SPECIFICATION OR TYPE CERTFICATE DATA SHEET or~ as ~am N/A i AMINORTHINESS DIRECTIVES *waren m I be tuAtEMER asatesseariceMAIN lets~. ~no pa re f was a • army mm• a ea. es el stem A ING(04~4~0 SUPPLEMENTAL TYPE CERTIFICATE 0.0Ise4440444414C arevann C.NRCRAFT OPERATION MOMAINTENMICE RECORDS 1 CHECK F RECORDS IN COMP/ONCE WITH 14 CFR ~on 91.417 TOT TOTAL ~RARE HOURS 3 EXPERIMENTS. ONLY gaspert ~an rsto4s~ .44~~441 o acandams 64~~~4•14 CERAM/01CM- Ihanto, wry MN I ma OW 'awed me DM 49 el te UMW ~NCO% 44101 requeskod. owner (a its aowo CI ens arum deserted itom, that eta swan MIN ma appwatmFerel Avon RoisolMan RP MN re main 4 regniered we fie ~Ka ACRontoltaben It ma men ..—...d Finals Am Nod. kr be DATE OF APPLICATION 10/29/2019 NAME MID TITLE ~a Fog Mark Guinan. Member 41 § 1 i i A TIE AIRCRAFT OESCRITED MOW HAS BEEN _.....i 4' INSPECTED MID FOUND MRWORIWY BY ~sr or• 44~449 a' 44 aFismat law 2 :LOPS port Ig ?MISDATE HOLDER 3 I CERTIFICATED MECHANIC /Om/ CMIAININM el I TED REPAIR S ION ram ~on 444i AIRCRAFT MANUFACTURER rtmsala• 4* am DATE Toil/ SIGNATURE e § a a, 0 1 • .4 Matta ••••••• hbatilime•A DWI/ TEE CERTFICATE REQUESTED A I Ira INF Ira shool ~DP m &octal I ot VII ~Is aar/TWIII ke 4 PMENDMUIT OR NOINICATION OF CURRENT AIRWORTHINESS CERRFCATE IL IMPIC•Cal fir • 4~4 ~MPS under Slawsca FM INSPECTOR FAA OESIONEE VII Ras contasi by CERTIFICATE HERDER UNDER 14 14 121 OR 135 I 114 CFR OM 146 DATE 0 7 41 AI nig MOSSO° OFFICE *attn. 4 FAA INSPECTOR'S DONA ROE SiGNATURE MO LOW424 en 6 40 05r75-- RTFICA a REVIEW TURE • vilier2C4672- AA FMF=151304 (042010)AI Primus Edbcm Smeramlad Eketrarae Format • PDF age 1 o12 a 0 0 SDNY_GM_02756438 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243360 EFTA01328476

IP • II A MANUFACTURER WE MMUS 8 PROOUCTOI MSG (CAMS* MN PRODUCTION CERTIFCATE IGHT FROMM DAMAN AMC TYPE CERTIFICATE OTHER_ C GIVE OLIANTITY CA CERTIMATES REQUIREDFM OPERATIC NEEDS DATE CC APPLICATION NAME NC NILE IRWW MRI VONATURE - - VII. SPECIAL FLIGHT PERMIT PURPOSES OTHER THAN PRODUCTION RIGHT TWIT A OESCRMTK/NOF AIRCRAFT REGISTERED OMER REGRESS SOLDER MIN/ at SERIAL NUMBER REGISTITATON MAK 8 DESCRIPTION OF FLX3HT CUSTMER DEIMSTMTION FLIGHTS n Mon teal FROM 10 vIA CEP/ATOM DATE CURATOR C CREW REQUIRED TO OPERATE THE AftCMAT MD ITS EQUIPMENT I PILOT I I COMM I I FLIGHT ENGINEER I OTHER (SPAM 0 THE AIRCRAFT DOES NOT MEET TIC APPLICABLE AIRWORTHNESS REQUIREMENTS AS FOLLOWS. E THE FOU.OAING RESTRICTIONS ANL CONSIDERED NECESSARY FOR SAIL OPERATION (Use Sim,* Oneonta% i CERTICAT ION • 1 Imp coley Tull tenths itelend eons fix Ns Rang all* rain closated atom. Mat re yawl is waved Rd!' Ire IT sickcal Anstal Morn a. in sccordsros win T449 al M. UMW Sens Code 44101 Km Mwale Finical Miaon Roptielow we Mt to was, hall peen wupeclad in, S sale kr re 4.{11 Resat*, DATE MANE NO TITLE (Print of Inn) SIMILTURE 2 i 1 y 2 I F 4 I gie ; 1 g a l / Ar ms Loralces MWarps nCaleillfa Will 14 OrR Smon 919. platls G Sasesnwe el Collorrniy. FM Fam 81334 ANTAMMA MAID li Far Angeleno CilesS01001fOr MIKA Anna MMOISIATOuilla9 A • . . C•anai CIMMIP2 LYMICCSAltsched 1 C Oil. DITRAIL PMAAMIN. OK (AIRCO efMn reksors0 I Provos Anteetess Cortgaes Read in Morderce We 14CFR Sam 21.185 cait 1 0 CuTIn W.gtl ardency* MemalcaAnammArat I lAa Wes an1 Minion, FM FM XII Mach Wen nikailM) / • .1 Curnint Ancertasss Conte* MARRS in ACONCIAAC• Wel,f°79n4"athid) la cili SOMA 21•191(a) Won teacneo) 1 Fps AMAMI Romlw et ARM IMAM 1( Oehl-Spcn Anna SIS*WII OCanplanot FM Tam 8130-1S (Mach **PI leaned) FAA Emmen°. (0820 IS)Al PRISM Edhqns SuptItiMed Elea Fame • POF Moo 2d2 SDNY_GM_02758439 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024336 I EFTA01328477

. . SPECIAL AIRWORTHINESS CERTIFICATE CATEGORY/DESIGNATION EXPERT PURPOSE & Qftvelopfroyht- MANU- FACTURER NAME N/A ,C.,•‘ ADDRESS N/ 4.,.."4 • FLIGHT FROM TO WA N 405PJ MODEL SERIAL 75 BUILDER BSI Hebcopte DATE a ISSUANCE 07 Nov 2019 • Ural= sooner sorrerclered, revoked. or the sennonstion dere cd tit elookilliness <edifice* o IINICIIVO undo. the cordibonseitordbed in 14 CFR. Pert 21, Secbon 21 1.217. Se3r4ATude Of FAA REPRESENT TON OR OFFICE NO. 547098732 MO Me *noes % Oinirca• • a4. was. O. • .000/ MT ard TON den a eald NOMItaa A ..S* ales ea M.SC. In twaYeed vow. *Ms awillica4•••••• MO 11.10‘ fr•. wd iro noliestet THOPOIMONC• IN ccoaccoe oust at osivnto I no ARCRAII Mt oc M•IXASIIPIEGIJA -- Conditions and Limitations -- 1. This aircraft does not meet the airworthiness standards of Annex 8 to the Convention on International Civil Aviation. Operations in airspace outside of the United States will require the permission of the applicable foreign authority. That permission must be carried aboard the aircraft together with this U.S. airworthiness certificate and, upon request, be made available to an FAA inspector or the applicable foreign authority in the country of operation. Operations may be further restricted by the applicable foreign authority. This may include not allowing use of an airport, requiring specific routing, and restricting flight over specific areas. The operator must comply with any additional limitation prescribed by the applicable foreign authority when operating in its airspace. (1) 2. These operating limitations do not provide any relief from any applicable law or regulation. This aircraft must be operated per applicable regulations and the additional limitations prescribed herein. Note that a clearance from air traffic control (ATC) is not authorization for a pilot to deviate from any rule, regulation, operating limitation, or minimum altitude, or to conduct unsafe operation of the aircraft. If ATC issues a clearance that would cause a pilot to deviate from a rule, regulation, or operating limitation, or in the pilot's opinion, would place the aircraft in jeopardy, it is the pilot's responsibility to request an amended clearance. These operating limitations are a part of FAA Form 8130-7 and are to be carried in the aircraft at all times and to be available to the pilot in command of the aircraft. (2) 3. This special airworthiness certificate is not in effect during public aircraft operations (PAO). Concurrent public/civil operations are not permitted; the aircraft cannot be operated as a civil aircraft and as a public aircraft at the same time. No weapons or special military mission systems may be added to the aircraft. This airworthiness certificate is not in effect during flights related to providing military services (that is, air combat maneuvering, air-to-air gunnery, target towing, electronic countermeasures simulation, cruise missile simulation, and air refueling). These activities are inherent military, not civil activities. The FAA makes the distinction between the authorized flights for experimental purposes, and PAO. Before operating this aircraft under this special airworthiness certificate following a PAO, the aircraft must be returned to the condition and configuration at the time of inspection for the issuance of this airworthiness certificate. The operator must have written procedures for returning the aircraft to the civil configuration. This action must be documented in the maintenance records. The maintenance records and entries must clearly differentiate between a civil experimental flight per this certificate and any other flights. (3) 4. Application to amend this certificate must be made to the local Flight Standards District Office (FSDO) or FAA Font. 81304 (11/2016) Previous Edidon Dined 04-2011 May t Used until Depiered Page I of 3 SDNY_GM_02756440 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243362 EFTA01328478

SDNY_GM_02756441 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243363 EFTA01328479

Manufacturing Inspection District Office (MIDO). (4) 5. The pilot in command must hold rotorcraft category and helicopter class certificate or privilege. The pilot in command must hold all required ratings or authorizations and endorsements required by part 61. (7) 6. When filing a flight plan, the experimental nature of this aircraft must be listed in the remarks section. (11) 7. This aircraft must not be used for 'mited to glider towing, banner towing, target towing, or towing electronic eceivers or emitters. Thrt,ai raft must not be used for intentional parachute jumping. (13) .,• 8. If aircraft or engine operating ((inflations are exceeded outsick f planned test conditions, an appropriate entry will be made in,the maintenance records. (14) 9. No person may operate this airecgt.unless it is maintained Ref. n inspection program meeting the scope and content described in § 91.409(f) The operator must selectd identify in the aircraft maintenance records one of the following program for.ttie inspection,oftfre aircraft: (a) For type-certificated aircraft, a current inspection program recommen bytttelpariafaeturer; or (b) For former-military aircraft, an inspection program recommended by the ma ufacturtsror North Atlantic Treaty Organization (NATO) military service; or (c) An FAA-approved inspection program. Inspections must be recorded in the aircraft maintenance records showing the following, or a similarly worded, statement: "I certify that this aircraft has been inspected on [insert date] per (identify applicable inspection program] and found to be in a condition for safe operation." Note: To extend an inspection interval, the owner/operator must submit a request for that extension with supporting documentation and data to the local FSDO and obtain concurrence from that FSDO. (15) 10. Only FAA-certificated repair stations, FAA-certificated mechanics with appropriate ratings, or a manufacturer as authorized by § 43.3 may perform inspections required by these operating limitations. (19) 11. The aircraft may not be operated unless the replacement for life-limited articles specified in the applicable technical publications pertaining to the aircraft and its articles are complied with in one of the following manners: (a) Type-Certificated Products: Replacement of life-limited parts required by § 91.409(e) applies to experimental aircraft when the required replacement times are specified in the U.S. aircraft specifications or type certificate data sheets. (b) Non-Type-Certificated Products: All articles installed in non-type-certificated products operated under an airworthiness certificate issued for an experimental purpose, in which the manufacturer has specified limits, must include in their program an equivalent level of safety for those articles. These limits must be evaluated for their current operating environment and addressed in the approved inspection program. All articles installed in non-type- certificated products in which the manufacturer has specified limits, must include in their program an equivalent level of safety for those articles. The article must be inspected to ensure the equivalent level of safety still renders the product in a serviceable condition for safe operation. (20) 12. For aircraft originally incorporating fatigue life recording systems, the owner/operator must maintain and use the system as prescribed by the aircraft manufacturer and comply with the manufacturer's fatigue life limits. (21) 13. When changing between experimental operating purposes, the operator must determine that the aircraft is in a condition for safe operation and appropriate for the purpose intended. A record entry will be made by an appropriately rated person to document that finding in the maintenance records. (26) 14. Enhanced Flight Vision System (EFVS) operations for the purpose of research and development and/or showing compliance with regulations are not authorized if any component associated with the instrument approach procedure being flown, or any component of the approach lighting system associated with the FM Form 8130-7 (11auls) Previous Edition Dad 04-2011 May be Used until Dealed Par 2 of 3 SDNY_GM_02 756442 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00243364 EFTA01328480

SDNY_GM_02756443 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243365 EFTA01328481

instrument approach, is inoperative. (40) 15. Kinds of operations authorized: Day VFR flight operations are authorized (47) 16. Night flight operations are authorized if the instruments specified in § 91.205(c) are installed, operational, and maintained per the applicable requirements of part 91. (48) 17. Instrument flight operations are authofizeslittbAin ruments specified in § 91.205(d) are installed, operational, compliant with the pe;pilvirequileiiiere, f, and maintained per the applicable regulations. The pilot in command /*Kaye a method tetig, ly with the § 91.319(c) prohibition from operating over densely populated s eas or in congested airways. All maintenance or inspection of this ; equipment must be recorded in t te.)zircraft maintenance recor•sls nd include the following items: date, work performed, and name and rtificate number of person rofp ning aircraft to service. (50) 18. All flights must be conducted within the geographical area described as follows: Aircraft must remain within the area defined on the attrilited sectional, while avoidipg ensely populated areas, restricted areas, and congested airspace. (53) ..:- : i :, \ ...) a..:- 19. Flight over a densely populated a or,p a congestechlf ay is authorized per § 91.319(c) only for the . ,e..,-` 6, purpose of takeoff and landing. The area- stgla_ce cribed by the term "only for the purpose of takeoff and landing" is the traffic pattern. For the purpose of this limitation, the term "only for the purpose of takeoff and landing" does not allow multiple traffic patterns for operations such as training or maintenance checks. This does not restrict a go-around/rejected landing for safety reasons. When avoiding populated areas, aircraft speed and weight must be considered. The information in FAA Order 8900.1, Flight Standards Information Management System (FSIMS), regarding set-back distances from spectator areas for aviation events such as air shows or air races may assist in determining a suitable space to fly the aircraft. (55) 20. Flight in RVSM-designated airspace is prohibited. (58) 21. No person may be carried in this aircraft during flight unless that person is essential to the purpose of the flight. (61) Larrie Ricca, DAR 547098732, Seattle MIDO, AIR-872 - END - FAA Form 81304 (11/2016) Previous Edition Dated 04-2011 May be Used until Depleted Page 3 of 3 SDNY_GM_02756444 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243366 EFTA01328482

SDNY_GM_02756445 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243367 EFTA01328483

SDNY_GM_02756446 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243368 EFTA01328484

SDNY_GM_02756447 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243369 EFTA01328485

UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION SPECIAL AIRWORTHINESS CERTIFICATE CATEGORY/DESIGNATION EXPERIME.NIAIr --__, PURPOSE A Ibvikoarofti 7'N MANU- FACTURER NAME N/A ‹, Tv Tv ADDRESS N/ A:::' J. 0.•... FLIGHT FROM A- .) TO t N405PJ MODEL SERIAL N 75 BUILDER Bell Halo* I DA ISSUANCE 07 Nov 2019 Wins mow surrendered _ rasa. NNa tormInmon Olson order tm Creilaastral n 14 2I.Sectim SO 2 2019. IN a Maness ceMicaie 4 21. 21217. SIGNATuRE OF FM RePRESartar .,‘ N.' ft% TON OR OFFCE NO 547098732 •• The sincean ovals • Mel ' *4 beterry .1* ore TM II t of faimIlteatcn, Mn SIMISS.IISINW renglan kg •••••••• faseaevilo MON* My sea044 Ine. eV fa Mellionvelt MIS KIMONO ME CUM CAR 'AUSTIN/ DISOLOMED IN 1141/MOWT PER MI MOULAMNII w., -- C rifitions and Limitations -- 1. This aircraft does not meet the air hiness standards of Annex 8 to the Convention on International Civil Aviation. Operations in airspace outside of the United States will require the permission of the applicable foreign authority. Th ermission must be carried aboard the aircraft together with this U.S. airworthiness certificate an n request, be made available to an FAA inspector or the applicable foreign authority in the count o eration. Operations may be further restricted by the applicable foreign authority. This may inc not allowing use of an airport, requiring specific routing, and restricting flight over specific areas. The operator must comply with any additional limitation prescribed by the applicable foreign author' y when operating in its airspace. (1) 2. These operating limitati do not provide any relief from any applicable law or regulation. This aircraft must be operated per pl le regulations and the additional limitations prescribed herein. Note that a clearance from air traff trot (ATC) is not authorization for a pilot to deviate from any rule, regulation, operating limitation, or icimum altitude, or to conduct unsafe operation of the aircraft. If ATC issues a clearance that would cii#e a pilot to deviate from a rule, regulation, or operating limitation, or in the pilot's opinion, would ce the aircraft in jeopardy, it is the pilot's responsibility to request an amended clearance. These op ng limitations are a part of FAA Form 8130-7 and are to be carried in the aircraft at all times and to be fable to the pilot in command of the aircraft. (2) 3. This spec&il airy" hiness certificate is not in effect during public aircraft operations (PAO). Concurrent public/civil dperakon re not permitted; the aircraft cannot be operated as a civil aircraft and as a public 41 military aircraft at th a time. No weapons or special mission systems may be added to the aircraft. This airworthine certificate is not in effect during flights related to providing military services (that is, air combat maneuvering, air-to-air gunnery, target towing, electronic countermeasures simulation, cruise missile simulation, and air refueling). These activities are inherent military, not civil activities. The FAA makes the distinction between the authorized flights for experimental purposes, and PAO. Before operating thjs aircraft under this special airworthiness certificate following a PAO, the aircraft must be returned to-'the condition and configuration at the time of inspection for the issuance of this airworthiness certificate/The operator must have written procedures for returning the aircraft to the civil configuration. This actioh must be documented in the maintenance records. The maintenance records and entries must clearly ffferentiate between a civil experimental flight per this certificate and any other flights. (3) 4. Ap ation to amend this certificate must be made to the local Flight Standards District Office (FSDO) or FM Form 8130-7 (11/2018) Premiss Eaton Dated 04-2011 May be Used onte Depleted Page 1 of 3 SDNY_GM_02758448 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243370 EFTA01328486

SDNYGM0275.49 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243371 EFTA01328487

Manufacturing Inspection District Office (MIDO). (4) 5. The pilot in command must hold rotorcraft category and helicopter class certificate or privilege. The pilot in command must hold all required ratings or authorizations and endorsemen required by part 61. (7) 6. When filing a flight plan, the experimental nature of this aircraft must bat tea in the remarks section. ., (11) firt 7. This aircraft must not be used for i.wing,-including, btiting‘t, mi tniider towing, banner towing, target towing, or towing electronic edeivers or emitters. Thlshpi ust not be used for intentional parachute jumping. (13) '•:' •.- 8. If aircraft or engine operating I Stations are exceeded outs appropriate entry will be made ink the maintenance rec 9. No person may operate this airccatt unless it is mai n inspection program meeting the scope and content described in § 91.409(f) The operator mu d identify in the aircraft maintenance records one of the following progranis‘48r,tbe inspectio aircraft: (a) For type-certificated aircraft, a current inspection program recommend &OA itrib urer; or (b) For former-military aircraft, an inspection program recommended by the man. urO'or North Atlantic Treaty Organization (NATO) military service; or (c) An FAA-approved inspecti ogram. Inspections must be recorded in the aircraft maintenance records showing the following, r similarly worded, statement: "I certify that this aircraft has been inspected on (insert date] per (iden applicable inspection program) and found to be in a condition for safe operation." Note: To extend n inspection interval, the owner/operator must submit a request for that extension with supporting documentation and data to the local FSDO and obtain concurrence from that FSDO. (15) t ti, FAA-certificated mechanics with appropriate ratings, or a perform inspections required by these operating limitations. 10. Only FAA-certificated repair statlo manufacturer as authorized by § 4 (19) of planned test conditions, an 11. The aircraft may not be ope unless the replacement for life-limited articles specified in the applicable technical publicatio rtaining to the aircraft and its articles are complied with in one of the following manners: (a) Type ated Products: Replacement of life-limited parts required by § 91.409(e) applies to experim al aircraft when the required replacement times are specified in the U.S. aircraft specificatio or ty rtificate data sheets. (b) Non-Type-Certificated Products: All articles installed in non-ty certif ed products operated under an airworthiness certificate issued for an experimental purp se, in h the manufacturer has specified limits, must include in their program an equivalent level of f r t ose articles. These limits must be evaluated for their current operating environment and dre ed in the approved inspection program. All articles installed in non-type- certificated products i hich the manufacturer has specified limits, must include in their program an equivalent level of safty for those articles. The article must be inspected to ensure the equivalent level of safety still renders tile product in a serviceable condition for safe operation. (20) 12. For aircraft originally incorporating fatigue life recording systems, the owner/operator must maintain and use the system as prescribed by the aircraft manufacturer and comply with the manufacturer's fatigue life limits. (21)4. 13. When changing between experimental operating purposes, the operator must determine that the aircraft is irt'a condition for safe operation and appropriate for the purpose intended. A record entry will be made Jf y an appropriately rated person to document that finding in the maintenance records. (26) 14. En nced Flight Vision System (EFVS) operations for the purpose of research and development and/or show' g compliance with regulations are not authorized if any component associated with the instrument app ach procedure being flown, or any component of the approach lighting system associated with the FAA Ppm 6130.7 (1112016) Previous Edition Dated 04-2011 May be Used until Depleted Page 2 of 3 SDNY_GM_02 756450 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243372 EFTA01328488

1 SDNY_GM_02756451 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243373 EFTA01328489

Instrument approach, is inoperative. (40) . u 15. Kinds of operations authorized: Day VFR flight operations are au °red (47) 16. Night flight operations are authorized if the instruments spec. fed in § 91.205(c) are installed, operational, and maintained per the applicable requireme o art 91. (48) 17. Instrument flight operations are authorizentlicin u e /nts specified in § 91.205(d) are installed, operational, compliant with the perfriice requite regulations. The pilot in command st,Save a me ly with the § 91.319(c) prohibition from f, and maintained per the applicable operating over densely populated ias or in contij /airwkys. All maintenance or inspection of this equipment must be recorded in tIle'pircraft mainte pce records nd include the following items: date, work performed, and name and certificate number of person rOpsning aircraft to service. (50) I O / 18. All flights must be conducted ithin the Agtiphical area des ribed as follows: Aircraft must remain within the area defined on the at cited sect*ojal, while avoi O ding ensely populated areas, restricted areas, and congested airspace. (53 --* 4:0,I ,....- 19. Flight over a densely populated ar Ili a congested# ay is authorized per § 91.319(c) only for the , purpose of takeoff and landing. The ar the suffice cribed by the term "only for the purpose of takeoff and landing" is the traffic patter Foithe-pur ose of this limitation, the term "only for the purpose of takeoff and landing" does no Ilow ultiple traffic patterns for operations such as training or maintenance checks. This does tract a go-around/rejected landing for safety reasons. When avoiding populated areas, aircraft spe eight must be considered. The information in FAA Order 8900.1, Flight Standards Information ement System (FSIMS), regarding set-back distances from spectator areas for aviation events such r shows or air races may assist in determining a suitable space to fly the aircraft. (55) 20. Flight in RVSM-des' )ted'airspace is prohibited. (58) 21. No person may be ' - din this aircraft during flight unless that person is essential to the purpose of the flight. (61) Larrie Ricca, DAR 8732, Seattle MIDO, AIR-872 - END - FM Form 8130-7 (1 1/2018) Preaus Eton Dad 042011 Mey be Used until Depleted Page 3 of 3 SONY_GM_02756452 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243374 EFTA01328490

SDNY_GM_02756453 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243375 EFTA01328491

RIO litufilital £3CS q0. 7e I 0410`6117 IS .o J 1914 60/.4130Weralk A4/3 - 11 I .4 MI _cf:se Par4040 itEo will ..-•• ce.ikat ym.k E • 1NELL a PA :45:-7(..„ ay •91 no ike? 1D1.4V4.1 (.480 - 37 ■rr4 50.1 ENM Y .** , 7t l*L 17 4 tan St eN ti+ 116""1"1 I L r" 'IVP A 4-±-xcn-r - In 7...Lamy tvniffszyz La.:, .r. • tr .! e„. • 0500 '• • --C m°41 • tap ' 12.503 ,171 51SL ‘,". -Tr REVIEWED AND ACCEPTED SAC: VrS00 SONY_GM_02756454 ag 1511O I 12 • A ,r 1 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243376 EFTA01328492

SDNY_GM_02756455 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243377 EFTA01328493

- - _ UNITED STATES Of AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE NATIONALITY MO 2 MANUFACTURER MD 'soon 3 AIRCRAFT SERIAL 4 CATEGORY REGISTRATION MARLS N405PJ Bell Helicopter Textron Canada Model 407 NUMBER 53375 Normal S AUINORiTY MO MSG FOR ISSUANCE ancrams Mtoa :NW Armilie49 U SC $ max sa Newel tit at te nee Yalta MYntflb.ffl Menai NW ird boa *antra te /fie ardor. INretem Wawa., kr We mostax 44/ AN ton 'Iamb AM IN comenra at• 'Ma* conetMest of Nam *waren Mt as $4444M IT Aim I NM 47.11•00 a reanstoge Axma. From es con tem EmpI444 ***None*** ... 6 TERNS AND CONDITIONS :nom soxs scon:444 snowed recto eta venvIen On is camine eM4MTfF a, h TM 4411440INNISOMOCIN *Ache a b^I a N eramennc yegnirpt martnect. N W. re Warms Amara tePaytl, gird nt e40MM Omar Repairs as *pop** rd N apf. Seal AM ‘M.0 SDI. DATE OF ISSUANCE "ESLWLSW DESIGNATION IMIASER 05 APR 2016 T DARTI10617WP ftery Moir vreAtIc4.ce444.4 4, Ns ca.* Mato...MOO 43 fat sol etusfe.; 4, X6 anc4O1443,4ce us/Slake /Slat. TNG CERTFCATE WV D.IFIA4E0 4i 04.74447 AZCOR..14ACE MTN APIWALE 'WAN. 49101C4/ AMMONS FM Form SI00.2 104.111 $.44,494..4 Prtvon E4604 R.& /4/5 /74-7E45 o 8 /400 toc, SDNY_GM_02756456 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243378 EFTA01328494

SDNY_GM_02756457 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243379 EFTA01328495

MEL' RO LLC •FIr IND APPOINTMENT OF AUTHORIZED REPRESENTATIVE To whom it may concern: As an Owneantstee of Helibro LLC Mar's Gunsauls as an authorized representative may conduct business and has signatory authority for liebbro LLC. Mark Gunsauls is also Ptricesm as a legal °Member° to conduct business and has signatory authority to do so as a Member. Title Date Notary rq f °Ale( CLU2A Signature Notary Confirmation Below SDNY_GM_02756458 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243380 EFTA01328496

SDNY_GM_02756459 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 002433R1 EFTA01328497

CALIFORNIA ALL-PURPOSE ACKNOWLEOGPAEW sarcomaitaiirazenc .c.cr.ccr..--tcss: CIVIL CODE § 1189 j Ibis certificate notary public or other officer completing this certificate verifies only the identity of the individual who signed the document to which certificate is attached, and not the truthfulness, accuracy, or validity of that document. State of California County of -11(taneta on Ma L\ Lc+ R0O before me, "1ink L.. -Ozanne Fle 114 'Act Date Insert Name and Title ofithe Officer I ) personally appeared Ha r k E ati111(.O ILA.47"} Narne(s)of Signer(s) who proved to me on the basis of satisfactory evidence to be the person(s) whose name(s) is/are subscribed to the within instrument and acknowledged to me that he/she/they executed the same in his/her/their authorized capacityries), and that by his/her/their signature(s) on the instrument the person(s): or the entity upon behalf of which the person(s) acted, executed the instrument. cr..; TRISH DIPS ROMIG Notary Public California Tenarru County Commission o 2160216 - Ma Comm E ires Jul 18 2020 Place Notary Seal Above I certify under PENALTY OF PERJURY under the laws of the State of California that the foregoing paragraph Is true and correct. WITNESS my hand and official seal. Signature. ibitofaciel, O 0Andr. ea • Signature of Notary Public OPTIONAL Though this section is optional, completing this information can deter alteration of the document or fraudulent reattachment of this form to an unintended document. Description of Attached Document Title or Type of DoCiiment: &ANL) lAtto!rent Date: 1.6/0( fa°, Number of Pages: Signer(s) Other Than Named Above: N/A Capacity(les) Claimed by Signer(s) Signer's Name: LI Corporate Officer — Title(s): L1 Partner — i i Limited General U Individual 7. Attorney in Fact II Trustee 7 Guardian or Conservator Other. Signer la Representing: Signer's Name: U Corporate Officer — Title(s): 0 Partner — O Limited O General Individual 0 Attorney in Fact 0 Trustee 17 Guardian or Conservator Other Signer is Representing: 092014 National Notary Association • www.NatiOnalNotary.org • Item 15907 SDNY_GM_02756460 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_OO243382 EFTA01328498

SDNY_GM_02756461 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243383 EFTA01328499

October 29, 2019 Federal Aviation Administration Attn.: James Sprecher 2200 S. 216th Street Des Moines, Washington, 98198 SUBJECT: Program Letter for Special Airworthiness Certification REGISTERED OWNER: Helibro, LLC BUILDER: Bell MODEL: 407 SERIAL NO: 53375 Dear Mr. Sprccher: DESIGN CRITERIA: Research & Development NUMBER OF ENGINES: 1 NUMBER OF SEATS: 7 REGISTRATION NO.: N405PJ The purpose of this letter is to request a special airworthiness certificate, in the experimental category, for a Research & Development Airworthiness Certificate in accordance with Title 14 Code of Federal Regulations (14 CFR), § 21.191(a). This request is made to support company flight testing in support of FAA Project Number ST17247LA-R. The STC will be for the installation of a Dual Cargo Hook System on Bell Model 206 and 407 aircraft. The proposed Flight Testing will be conducted over 1 — 3 hours on or around the 7th of November, 2019. We request the designee hold the Standard Airworthiness in suspension until the completion of flight testing. The aircraft will be located at Pi Helicopters facilities in Red Bluff, Ca. The aircraft is within current maintenance, has been conformed to the TCDS and the following has been accomplished: • FAA Form 8130-6, with sections I, II, and Ill completed is enclosed. • The aircraft has been properly registered. • We have weighed the aircraft to determine that the most forward and aft center of gravity positions arc within established limits. The weight and balance report is available at the aircraft. • The marking requirements of 14 CFR Part 45 have been complied with, including permanent application of appropriate registration marks and the word "EXPERIMENTAL" near each entrance to the cabin or cockpit. • The aircraft is inspected and maintained in accordance with the Bell Helicopter Maintenance Manuals. The following is a description of the requested geographical areas for flight testing: within the box defined on the attached sectional, while avoiding densely populated areas and congested airways. I request Larrie Ricca, DARF 547098732, be delegated to issue the requested airworthiness certificate. My telephone number is: additional information is needed. Sincerely, Please contact me at this number if there are any questions or if David McCammon, Director of Maintenance - 135 Helibro, LLC Page 1 of 1 SDNY_GM_02756462 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243384 EFTA01328500

SDNY_GM_02756463 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243385 EFTA01328501

0 MAJOR REPAIR AND ALTERATION d 1 raliprlaaa's (Airframe, Powerplant, Propeller, or Appliance) Fears Adobe Adtrithelnakon ran 4W0 d r0W No 21204020 2/2e4011 Dewar Tfficl orp Wooer or f AA WOOS/ INSTRUCTIONS. kid or type as entries. See Title 14 CFR §43.9. Part 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form This report is required by law (49 U.S.C. §44701). Failure to report can result in penalty for each such violation. (49 U.S.C. §46301(0) I. Aircraft Nationality and Registration Mark N405PJ Serial No. 53375 make Bell Helicopter Model 407 Series 407 2. Owner Name (As shown on registration certificate) Helibro. LLC. Address (As shown on registration certificate) scent 401 i anglev Way car Rid Bluff San CA zit 96080 Casey USA 3. For FAA Use Only 4. Type 5. Unit Identification Repair Alteration UnN mate Model Serial No . 0 (As described in item 1 above) AIRFRAME O o POWERPLANT • O PROPELLER -Tyre . O APPLIANCE Itoniocsain 6 Conformity Statement A. Agency's Name and Address B Kind of Agency Nave p J Helicopter < Inc Ii S Cendooteci riechanc I uarvinickirer Menu CM I anglev Way Foreign Cortthcated Phlecran pc C Certificate No. oi, Red Bluff sew CA j corer cote] ReOor Senor, AVVTR306C zu 96080 caves USA tartrate@ Morotenanee Orgaltrabon D. testify that the repair and/or alteration made to the tab( ) Wearied in it/NS/Cove and described on the reverse or ett*Chment$ hereto have been made in accordance with the rersitemenls of Pan 43 of the U.S. Federal Aviation Regulations and that the informal= fornIShed herein is true and eared 10 the best of my knowledge. Extended range fuel per 14 CFR Part 43 O APP. 8 Signature/Date of Authorized Individual n f1 1/2)JMi Derek Spooner 3/21/2019 -,7,/,-- fon 7. Approval for Return to Service Pursuant to the authority given persons specified below. the unit Identified in item 5 was inspected in the manner prescribed by Me Administrator of the Federal Aviation Administration and is E2 Approved El Rejected BY FM Fil. Standards Inspector lAanufackrer Maintenance Organization Person Aeproved by Canedon Department or TraMpOrt FM Designee I Repair Station Inspection Authorization Other (Specify) Certificate or Designation No. AVVTR306C SigraturerDate of Authorized Individual Pc. i$ Derek Spooner 3/21/2019 . ../..---- 85S FAA Form 33700.011 SDNY_GM_02756464 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243386 EFTA01328502

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements e. Descdpaon of Work Accomplished (amore space is required. attach add.tional sheets. Wendy with aircraft nabonamy and recestratton mark and date via* competed) N405PJ Nationality and Registration Mark 3/21/2019 Dale Aircraft Total Time: 2852.4 SIN 53375 Installation of Garmin GTX 345 Transponder STC#SR02124SE. 1. Installed Garmin GTX 345 Transponder referencing Garmin STC SR02124SE. 2. Instructions for continued airworthiness to be performed referencing Garmin ICA Document 190-00734-21 of the latest FAA approved revision. 3. Flight Manual Supplement has been inserted into the Flight Manual. 4. Change to aircraft weight and balance negligible. Aircraft equipment list has been updated. 5. An appropriate logbook entry has been made. END K Additional Sheets Are Attached FAA Form 337 noes} SDNY_GM_02756465 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243387 EFTA01328503

0 VS Onarnm.r, MAJOR REPAIR AND ALTERATION at Travispottato, (Airframe, Powerplant, Propeller, or Appliance) agent Minton ArlialresvatIon Leen Apparel CMG no 21204:020 2a9/7011 Eleatin< Trealler Pthirtier Far Fla use Only INSTRUCTIONS Print or typc all entries See Tale 14 CFR 5439. Part 43 Appendix B. and AC 43.9-1 (or subsequent raglan thereon for instruction and rkSpOSnion of this form This report * required by law (49 U S.C. 544701). Failure to repot can testa in a ova penalty for each such violation (49 U.S.C. 546301(a)) 1. Aircraft Nationality and Registration Mark N405PJ Senai No. 53375 Mae Bell Model 407 Series 206 2. Owner Name (As show,' On sagestnsion certificate) lielibro. LLC Address (As shown on registration certificate) Ann. WWI Anatil May c" , Red Bluff SUN CA 4 96080 cant USA 3. For FAA Use Only 4. Type 5. Unit Identification Repair Alteration Unit Make Model Sera No. • 0 AIRFRAME (As deathbed on hem I above) O O POWERPLANT ED ii PROPELLER O n APPLIANCE Type Manufacturer 8 Conformity Statement A. Agency's Name and Address B. Kind of Agency Wee p I Halirnpuwx Int. U 5 Canaria Mechanic I Madinat Mena 903 Langley Way Far Cankaled Maher* C. Cerbficate No coy Red Bluff sta. ('A j certificated Rook Simon AWTR306C to 96080 c....«., USA Carticaled Mantenance Orgarnatan D. I certify that the repair anWor alteration made to the unit( ) identified in item 5 above and (*stilted on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 Or the U S Federal Aviation RegulaNanS and that the information furnished herein is true and correct to the best of my knowledge. Emended range fuel per 14 CFR Part 43 O MO. B SynatucerDate of Authorized Individual James Tierno 3/26/2018 vi_a_S.J14 7. Approval for Return to Service b ,50 ./..,_ Pursuant to the authority given persons speared below. the unit identified in Rem 5 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is 21 APPrOved El Rerected BY FM Fe Standards Inspector Manufacturer Maintenance Orgarmation Panne* 4P1r0Verl Dy Careldela Department of Transport FAADesignee 1 Repair Station Inspection Aute04241.44 Other (Specify) Certificate or Designation No. AWTR306C SgnaturetDate of Authorized individual Brandon Niewinski 3/26/2018 FAA Form 337 no-oh SDNY_GM_02756466 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243388 EFTA01328504

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space Is requvrect, attach additional sheets Identify 'Oh aerie natIonatey and registration mark and date woe* completed.) N405RJ Nabccialty and Registration Mark 3/26/2018 Date Aircraft Total Time: 2564.8 Serial Number. 53375 Installation of Aeronautical Accessories, Inc. Slide Window Latch Kit STC# SR01074AT 1. Installed Aeronautical Accessories Slide Window Latch Kit P/N 407-552-300 referencing installation instructions report number AA-96178 revision H. 2. There are no instructions for continued airworthiness provided for the slide window latch kit 3.There is no flight manual supplement provided for the slide window latch kit. 4. Change to weight and balance is negligible. 5. An appropriate logbook entry has been made. —END-- 0 Additional Sheets Are Anached FAA Fenn 337 occ31 SDNY_GM_02758487 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243389 EFTA01328505

el ....- us Onsewir MAJOR REPAIR AND ALTERATION et trinspalann (Airframe, Powerplant, Propeller, or Appliance) Federal A.41*. AbnInIstreeee Fool Porene COON* 2i200220 zdenon Emaccric Trockng Panto. Fee FAA Use Mb INSTRUCTIONS: Print or type al mines See Title 14 CFR §43.9. Part 43 Agenda 8. and AC 43.9-1 (or SubSequerd revision thereof) for estrudbons and disposition of Me form This report is required by raw (49 U.S C §44701). Flukey to report can remit in a awl penalty for each such violation. (49 U.S.C. §4630I(an 'Nabonality and Registration Mark N405PJ Serial No 53375 Make Bell Model 407 Series 206 t. Owner same (As shown on regstration co/Meeks) Helibro, LLC Address (As shown on regarnsuon cernficate) mem QM I anglAy way CA. Red Bluff Pan Ca zo 96080 cower USA 3. For FAA Use Only 4. Typo S. Unit Identification Repair Alteration Unit Make model Sens No. El IZI AIRFRAME (As descnoed in green I above) O O PCMERPLANT O El PROPELLER O D APPLIANCE ( Type 6 Conformity Statement A. Agency's Name and Address B Kind Of Agency en p I Willman% Inr USCeftfiCated MOChane I Manulatturat Adam 903 Langley Way Feemn Certificated mechanic C. Certificate No ca Red Me see CA i Celli-MOS Repasr Stake AVVTR306C se 96080 Canty USA Coftlateol Manlennce Oreanuabeo 0. Icemen/ nal the repair andlor alteration made IC the unit( ) identified in item 5 above and described on the reverse or anachmeMs hereto have teen made in accordance with the regteermmts of Pan 43 of the U S Federal Aviation Regulations and that the information furnished herein is true fend correct to the best of my krxmledge Extended range fuel per 14 CFR Pad 43 O APP. El Sgrunure/Date of Aul110ezed Individual James Tierno 3/26/2018 j"..aJI-1 7. Approval for Return to Se ' 530 Pursua t to the authority given persons specified below. the urn KleAllried in item 5 was Aominisvator of the Federal Aviation Administration and is g Approved . Inspected in the manner presented by the Rejected BY FAA Flit. Standards Inspector Manufacturer Maintenance Organization Persons Approves by Camden or Tranipan FAA Designee I Repair Station Inspection Aurri0OZahOO Other (Specify) Certreale or Desgnalron No. AWTR306C Signature/Dale of Authorized Individual Brandon Niewinski 3/26/2018 FAA Form 337 noon SDNY_GM_02756468 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA JX)243390 EFTA01328506

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements 8. DoscrIptIon of Work Accomplished (If more space is 'sootier( Oath eddeldnal sheets. Identify with aircraft slalom,* end togistration mark and dale work completed) N405PJ Nationality and Registration Mark Aircraft Total Time: 2564.8 S/N 53375 Installation of AFRO Design Ltd. Cyclic Friction Replacement STC# SR03283NY 3/26/2018 Dale 1. Installed AERO Design Ltd. Cyclic Friction Replacement Kit P/N 95201-01 referencing AERO Design Ltd drawing number 95201 revision 1. 2. Instructions for continued airworthiness to be performed referencing AFRO Design Ltd. ICA 952 90 of the latest FM approved revision. 3. Installed FM approved AERO Design Ltd. Rotorcraft Flight Manual Supplement document number FMS952.91 into the aircraft flight manual. 4 Change to aircraft weight and balance negligible. Aircraft equipment list has been updated. 5 An appropriate logbook entry has been made. --END Additional Sheets Are Attached FAA Form 337(loon SDNY_GM_02768489 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243391 EFTA01328507

0 La owenflow MAJOR REPAIR AND ALTERATION et Tranponaton (Airframe, Powerplant, Propeller, or Appliance) resins, Minion AbniNsintion Fenn Approved 041A No 21200)20 2/2,300 I Eiconic Trec.teg Motet or FAA Um Only INSTRUCTIONS. Pnnl or type all entries. Seo Title 14 CFR §43.9. Pan 43 Appendix B. and AC 439-1 (or subsequent revision thereof) for instructions and disposition of this form. Ibis report is required by law (09 U.S.C. §44701) Failure to report can result in a civil penalty for each such violate). (49 U.S.C. 446301(0 I. Aircraft Nationality and Registration Mark N405PJ Serial No. 53375 Make Bell Model 407 Senes 206 2. Owner Name (As shown on tegistrabon cerntcate) Helibro. LLC Address (As shown on registration certificate) AO&44S onv i an(ry Way fted Bluff sine CA zo 86080 Cost, VSA 3. For FAA Use Only 4. Type 5. Unit Identification Repair Alteration Unit Make Model Serial No. El Ga AIRFRAME (AS cfestiftwd in Hem f above) El O POWERPLANT 0 El PROPELLER El El APPLIANCE Type Manufriclorer I. Conformity Statement A. Agency's Name and Address B. Kind of Agency Nary P II 14Miewiwort low U. S Certresed Mechanic I Manularturar Mites 903 Langley Way Freon unrested Madame C. Cerblicate No. ear Bled Bluff at,. CA Certificated Raper Mallon de 96080 twee USA Certificated Maintenance Organization /AW7R306C D. I certify that the repair andlor alteration made to me unll( ) dentified in item 5 above and deserted on the reverse a attachments hereto have been made in accordance with the requirements of Part 43 of the U S. Federal Aviation Regulations and that the information furnished herein is MAI and correct to trio best of my knowledge. Extended range fuel App. CFR Part 43 I B SignalurerDate of Authorized Individual JI, 7. Ape:twat for Return t. Service Pursuant to the authority given persons specified below. the unit identified in item 5 was inspected in the manner presented by the Administraior of the Federal Aviation Administration and is n Approved . O Needed BY FM Ft Standards InspeCtor Manslacturer Maintenance Organization Persons Approved by Camden Dimenment of Tampon FAA Designee I Repair Station Inspection Mtn:Mallon Other (Specny) CeetifiCidt or Designation No. AWTR306C Signalure/Date of Authorized Indmdual --- ----r------- PJH n7r- FM Form 237 Vocal SDNY_Givl_02756470 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243392 EFTA01328508

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record An alteration must be compatible with all previous alterations to assure continued conformity with Me applicable airworthiness requirements. 8. Description of Work Accomplished (II more space u required. attach addattaratt sheets. Identify with aircraft nafionaldy and registration mark and date work completed) N405PJ Nationality and Registration Mark Aircraft Total Time: 2553.3 Aircraft Serial Number: 53375 2/14/2018 Date 1. Installed Onboard Systems Secondary External Load Hard Point STC ttSR02651LA referencing Aerocraft Inc. Master Data List ARC-407-MDL Revision "NC". 2. Instructions for Continued Airworthiness to be performed referencing Aerocraft Inc. Master Data List ARC-407-MDL of the latest approved revision and AC 43.13-16. 3. Weight and Balance and Equipment List have been updated and inserted into Flight Manual. 4 Flight Manual Supplement ARC-407HP-RFMS has been inserted into the Flight Manual. 5. An appropriate logbook entry has been made END K Additional Sheets Are Attached FAA Form 337, • SDNY_GM_02756471 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243393 EFTA01328509

f Om:7rd BOCiraft Tian; Nunte SO 0% Mena. us oweewi MAJOR REPAIR AND ALTERATION write owe* of Tramcdemir (Airframe, Powerplant, Propeller, or Appliance) Feelers, MINI*, mennwinuon INSTRUCTIONS. Pnnt or type all entries. See Title 14 CFR IC.% Pert 43 Appendix B. and AC 419.1 (or subsequent revision thereon for instructions and dispostion of tnis fan. This report is required by law (49 U.S.C. §44701). Figure to report can result native penalty for each such violate (49 U S C. §46301(a)) Nationality and Registration Mark N405PJ Serial No. 53375 1. Aircraft Make Bell Helicopter /MSS 407 Series N/A Name (As shown on regishaeon CCMICOIC) PJ Helicopters Inc. Address (As shown on nigistMtn meta) mews 001 tonality way 2. Owner CA. Reg Bluff sus CA go 060130 Comer United Steles 3. For FAA Use Only 4. Typo 5. Unit Identification Repair Metall*, In Make model Sena No 0 2 AIRFRAME (As deschted in item I above) 0 • PONERPLANT 0 0 PROPELLER 0 O APPLIANCE rys• Menutodurer 4 Coaformity Statement A. Agency's Name and Actress B. Kind of Agency Isms Fagg, CAnten Maintananre U.S.C.:Mates Mechmic bleaufectuel mem 823 McTavish Road NE Fo.e Cabkaled thchenc C. Cenificate No. c4 rotary Sm. AR Centeeptod Rem* Slalom 5-81 re T2E 7G9 mow Canada f CoMmeled Marten*** 0rmitidebon D. leerily that the repair and/or alteration made to the wig ) identified in nom 5 above and described on ne reverse or attachments hereto have been made in accordance will the requiremwts of Part 43 of the U $ Federal Aviation Regulations and mat the information furnished herein is true and coned to the best of it knotteoge Exr 14 C tended range fuel pe FR Pan 43 0 App. B SignaturerD e o MIndividual / /({Feb aotS 7. Approval for Return to Benda Pursuant to the belle, the mentde_o m Wen 5 was inspected in the mannaIMMCAMet by the authority given persons swaged ung MMAS.13101 of the Federal Aviation Administration and IS U Approved Rejected EP/ FM Fri Standards WISPeCtOr Malinttlfer / Maintenance Persons Organization Approved by Credal DepelMel al TraMpal FAA Designee Rept, Station Inspection Authorization Other (Specoy) Cern cam o Designationr No -81 S7 1/Da ezed Individual s /r7 PI fig lag 41 FAA Form 337 once; SDNY_GM_02756472 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243394 EFTA01328510

• NOTICE Weight and balance or operating limitation changes shall be entered in the appropnate aircraft record. An alteration must be compatible with all previous alterations fo assure continued conformity with the applicable ainwrthiness requirements 8. Description of Work Accomplished (amore space is required. tech additional sheets CCM(, witwith aircraft nationetty and registration mark and date work completed) N405PJ Nationality and Registration Mark Sell 407 N405PJ SIN 53375 AFTT: 2553.3 February 13, 2018 Date Installed Eagle Copters Maintenance Ltd. Honeywell HTS900-2-1D Engine Conversion P/N E407-789-011.1 in accordance with Supplemental Type Certificate SR03496NY. The installation of this kit was carried out IAW Eagle Installation Instructions IIN-E407-789. Revision D. dated 16.05.04 Items for continued airworthiness to be canted out IAW Eagle Instructions for Continued Airworthiness (ICA) ICA-E407-789, Revision 2, dated 16.07.15. Flight Manual Supplement (FMS) FMS-E407-789.1. Revision 1. dated 23 Aug 2016, is associated with this installation. The above work was carried out on Eagle Copiers Maintenance Work Order N55000. This aircraft was reweighed, weight and balance equipment list was updated by Eagle Coolers Ltd at this time to reflect the installation of this kit. —End Adabonal Sheets At Attached FM Fenn 337 moon SDNY_GM_02756473 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243395 EFTA01328511

el file ken r;coal 2.00/2011 Eimoo n. nc T , Paaveor vs moan MAJOR REPAIR AND ALTERATION or IAA On** al inniontan (Airframe, Powerplant, Propeller, or Appliance) I Falersi N Adminifereles INSTRUCTORS: Pnnt or type all entries. See Title 14 CFR §43.9. Part 43 Appendix 0. and AC 43.91 (or subsegueM revision tnereon for instructions and disposition 01lNs form. Tha report is required by Law (49 U.S.C. §44701). Failure to report can result racier penMy for each such wolabon. (49 U S.C. §46301(a)) t. MrcraB Slatienably and Recesumien Mark 14405PJ Serial No. 53375 Make Bell Helicopter Model 407 Series NIA 2. Owner Name (As shown on AististratiOn certificate) PJ Helicopters Inc. Address (AS shown on regisbitsbon ceatiCele) omens relit anginy Way Car Red Bluff sox CA no 96080 coon United SIAM 3. For FAA Use OnN 4. Typo 5. Unk identification Repair Attention UM make Model Serial No. El El AIRFRAME (As descnbed in Mere I above) CI O POWERPLANT . • PROPELLER El O 'Type APPUANCE aremissiew 6. Conlomety Statement A. Agency's Name and Address 8.1Und of Agency Plem Papa Contain Maintenance U. S. Ceiliacaled Mechanic ] Menseacturei Ia... 823 McTavish Road NE Forego Caracoled Mechanic C. Certificate No. or Calgary awn AB C•MOCeled Rep* Slain as T2E 7G9 cow, Canada ,e. Cectificoned Maintenance Oragriaation 16-81 0. I coney mat the repair amber Menem made to the unit( ) kleMilled in item 5 above and deserted on the reverse or altadinents hereto have been made in accordance with the reourements ot Part 43 of the U.S. cadent AMMIOn RecULMICK and tilt the informatke furnished herein is true and correct to the best of my Snowcap. Extended range fuel per 14 CFR Part 43 O APP. 8 Segnatore(Da of *Melted IneWidual trir irkt PI reb aois 0 7. Approval for Pan to SioMca Pursuant to the Whiny g ven persons specified below. the tare Matted in Item 5 was inspected In the manner prescribed by the Admintstrator of the Federal Avanon Administration and is 0 Approved Rejected Si' FM Ft Standards Inspector Manufacturer Manufacturer 1 Maintenance Organization Person. Mamma by Canadian al /ransom FM Designee Repair Station Inspection Aulhortzelim (Sealy) Cereficat or Dennallon NO 6-81 Signal ate Inndniddt /)) pi * 1 3 jolt* 41. FAA Form 337 oe-oh SDNY_GIll_027564 74 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243396 EFTA01328512

NOTICE Weight and balance or operating limitation changes shall be entered in die appropriate aircraft record An alteration must be compatible with ail previous alterations to assure continued conformtly voth the applicable einvorthiness requirements 8. Demean or Work Accomplished Of more space u mewed. attach adosonai sheets ldentlfy WO aircraft nationality and registration maw and date vO✓k contswiect) N405PJ Naticnarrty and Registration Mark Bell 407 N405PJ S/N 53375 AFTT 2553.3 February 13, 2018 Date Installed Eagle Copters Maintenance Ltd. Inlet Barrier Filter P/N 1003.01-001 in accordance with Supplemental Type Certificate SR03706NY. The installation of this kit was carried out Eagle Installation Instructions 1003-MI-001. Revision B, dated 16 02 17 Items for continued airworthiness to be earned out lAW Eagle Instructions for Continued Airworthiness (ICA) 1003-CA-001, Revision 0. dated 15.09.21. Flight Manual Supplement (FMS) 1003-FM-001. Revision A, dated 16.03.17. is associated with this installation The above work was carried out on Eagle Copters Maintenance Work Order #55000. This aircraft was reweighed, weight and balance equipment list was updated by Eagle Copiers Ltd. at this time to reflect the installation of this kit. End O Additional Sheets Are Attached FAA Form 337 nest SDNY_GM_02756475 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243397 EFTA01328513

0 MAJOR REPAIR AND ALTERATION US OspirloWil Orr 1 ....P51. 62' (Airframe, Powerplant, Propeller, or Appliance) fetal Aviation Painisbuion Farr AO9roved Owe .63 2110-0O20 2/20/2011 Eicctroc TwangMete Pot PM Vegteref INSTRUCTIONS Print or type all entries. See Tide 14 CFR §43.9, Part 43 Appendix B. arid AC 43.9-1 (or subsequent revision thereof) for instrucbcas and disposition of this form This report is required by law (49 U.S.C. §44701). Failure o report can restil in a CMI penalty for each such violation. (49 V.S.C. §48301(a)) t. AlrcrNt Telabonality and Registration Mark N405PJ Serial No. 53375 Make Bell Helicopter Model 407 Series 206 2. Owner Name (As Shawn on refastraoon certificate) Helibro LLD. Address (As shown on registration cerebrate) &nen gm, 1 anoby Way cry Red Bluff sate CA to 96080 cony USA 3. For FAA Use Only 4. Type 6. Unit IdentilkatIon Rate Attention UM Make Model Serial No. O izi AIRFRAME (As described in Item 1 above) O . PCOAERPLANT O O PROPELLER O O APPLIANCE 'TAW menuracrwer 6 Conformity Statement A. Agency's Name and Address 8. Kind of Agency NI^. PJ Helirnntiora Inf. U. S. Graeae Medusas I Msrolacturer Ansa 903 Langley Way Forego Certificated MeCherk C. Certificate No. co Raab Bluff sue DA .i Cerefleated Row Sumo AWTR306C se 98080 c.....v, USA Certalabld lidedenela Oftleniate D I certify that the repair and/or aeration made to the urit( ) identified in item 5 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the Information furnished herein is true and correct to the best of my knowledge nn Exterxled range fuel per 14 CFR Part 43 Ape 8 SignaturaDate of AuthonzeO Indwidual Wesley Clark 5/25/2017 / PJI-i 910 Ce14_ 7. Approval for Return to service PurSuant 10 the authority given persons specified below. the unit identified in item 5 was Administrator of the Federal Aviation Administration and is 2 Approved • nspected In the manner prescribed by the Rejected FAA FP Standards Inspector Manufacturer Maintenance Organization Persons Approved by Canadian Department of Tramper' BY FAA Deafens.. I Repair Station Other (Specify) Inspection Authorization Ceti cote or Des ignation No. INTR306C A Signature/Date of Authorized Individual PJH 5/25/2017 Daniel McDevitt ag Ann FAA Form 33700CM SDNY_GM_02756476 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243398 EFTA01328514

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all prewous alterations to assure continued conformity with The applicable airworthiness requirements. S. Description of Work Accomplished (lt more space is required. attach additional sheets Mewl), with aircraft nationality and registration mark and date work completed) N405PJ 512512017 Nabonaltly and Registration Mark Dale Aircraft Total Time: 2311.3 Serial Number: 53375 Installation of Dart Aerospace Bearpaws STC# SH1031NE. 1. Dart Aerospace Bearpaws kit D206.559 installed or removed referencing Dart Installation Instructions D206-559 revision L or later approved revisions 2. Instructions for continued airworthiness to be performed referencing Dan ICA-D206-559 revision 4 or later approved revisions. 3. There is no flight manual supplement provided with the Dart Bearpaw kit. 4. Aircraft weight and balance to be updated upon installation or removal of Bearpaws 5. An appropriate logbook entry wil be made. —END-- Additional Skeels Are Attached FAA Form 337 hods) SDNY_GM_02756477 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA ({)243399 EFTA01328515

0 MAJOR REPAIR AND ALTERATION mponstont a Trau 6 Oeisemson (Airframe, Powerplant, Propeller. or Appliance) Foams Await. ariwasinison FtnnAporoyos OW 460 21204020 I ray20:ff Etectionic Tracking Number For FAA Use Only INSTRUCTIONS. Print or type as (mines. See FAR 43.9. FAR 43 Apperda B. and AC 439-1 (or subeequent testiOn fiere00 for Mau:Wm and esposacn of Inia form. this repon us required by in (49 U.S.C. 1421). mem to abort can ream • <he penakY nOt beached 31.000 for each MO1 Pcfabon (Section 901 Federal Aviation A* 196$) 1. Aleoraft Nateinalrty and Regiftreltn Mark N405PJ 501W No. 53375 Make Bell Model 407 Sense 2. Owner Nine (As :Mown an reptstration cettleato) Helibro LLC. tomes (As snow, on repistsabon cornikaaw Amee.903 Lanalev Way coRed Bluff stma6 ze96080 Carm71.15.8 3. For FAA Us* Only The data Penelled herein temples wen Me arpltabla airworthiness Requirements and Is approved on for me above aerates arum AOKI te oteremlib mermen bye person aurceired in 14 R rt A25.7 3 / . / H I H 0' firlfrir 4. Type 9 Us Identification Repay Memnon Uns, Make Model Sens Number O a AIRFRAME (AS &tweed An nem f above) O o POWERPLANT O • PROPELLER O O APPLIANCE on. u.....,),e,,e, 6. Conformity Statement A. Apercys Name and Address B K rd of AgitnCy rarref) J Helicopters Inc. 0 U S Certscetee mechanic 01Maniitacarei AostatAf(7 lanalev Way 0 Foreign ceemsed Simmons C cetrraie No cryRed Bluff sierCA 2 Certneated Repair Station AVVTR306C 4936 !1_84 ca.- USA 0 cent aced ktentonance Organization o Immo mat be repair wicror a:aeration node to Me unnis) cent I ed in item 6 above and descreed an the reverse or attachments hereto have boon made in aosordesce MN the temerernents of Pan 43 of tie U S. Federal Maim Rogulatons and Nat The onformaticn futadned herein s true and corm*bra beet 01 my knonfedge Extended range fuel per 14 CFR Part 43 ACP. 8 O Semmureirtme °Muttered Metal RNA "are Siws---- 5 7%2,3. - i 7 850 7. Approval for Return to Service Pursuant 10 to authority peers pose woofed below. No test Admirer/966a 01 the recommitted:in Admntstraton and Is Panelled In *ern Ss Inspected in the memo (444104X41 by the r APPROVED O ROM= BY FAA Fa Standards inepeam Mantua:* Orgeorston Person Approved by Conlon Manufacturer Oepertmets 01 FAA Oemanee dc Repair Sieben Inspection Auelon aton eerit Oleo M e Carona* or Deagnalson No. Alerte_SPia C. Signature/Dab) N Authorized Individual PJH --- wi 5.4.--- 5 -13(9 850 FM Poem 337 ito-oet SDNY_GM_02756478 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243400 EFTA01328516

NOTICE Weight and balance or operating limitation changes shall be entered ki 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 as required, attach additional sheets Identify with aircraft nationally and registration mark and date work completed) N405PJ Nationality and Registration Mark ACFT TOTAL TIME 2259 5 ACFT SN 53375 [3.16.17 Date Installed FreeFlight Radar Altimeter RA4000 system with Radar Altimeter Display to satisfy FAA mandate 14 CFR 135 160. 1 ) Mounted new TSO'd RAD 40 Display to existing panel blanking plate in the aircraft instrument panel at sta. 40 with 'MS' hardware Mounted new TSO'd Radar Altimeter MN RA4000 behind aircraft hatrack at sta 157 vath WS* hardware and 202473x.040" aluminum doubler. alodined and painted. Mounted new TSO'd Radar AttaMeter Antennas to existing STC'd Radar Altimeter Antenna Brackets on aircraft belly behind aft aosstube at sta. 168. All power supplied from avionics buss through 3A Circuil Breaker PIN M5265743. placarded 'FtAD ALT. All single conductor wire M22759/18 series. As shielded wire M27500 series 2.) All work performed referencing BHT407.mm. FreeFipta Systems Operationfinstaeation Manual 484948, FreeFhght Equipment Installation Manual #84629, and AC43.13-1B chapters 4. 7 8 11. latest revisions. Operation portion of the Freight Operation/Installation Manual placed on board the aircraft as a guide to equipment operation. 3.) This install is for VFR use, altitude above the terrain is advisory information only. 4.) Weight and Balance computed. and equipment list updated. 5.) An electrical load analysis determined that the electrical load of the aircraft does not exceed 80% of the rated generator capacity. 8.) Installed equipment does not interfere with or displace required equipment or otherwise interfere with the safe operation and ainvoethMeSS of the aircraft. Failure of this equipment would not prevent continued safe flight and landing of the *Craft 7.) Performed ground functional test referencing manufacturers installation manual procedures that determined the operations and functions olexisling systems and components previously instated are not adversely affected by this alteration 8.) This equipment was found not to exceed the guidelines in FAA Roiorcraft Directorate policy letter ASW.2001-4, dated Apri 25. 2003 for FADEC controlled aircraft and is considered to be "equipment not known to have potential for interference. 9.) CONTINUED AIRWORTHINESS' Requires operational test and visual inspection in accordance wan FAR Part 43 Appendix I) Annually. Reference manufacturers publications END K Additional Sheets Are Attached FAA Form 337 (1006) SDNY_GIvi_02756479 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024340 I EFTA01328517

0 CO', AWMCI OMB No 1120{020 2011.20ti Exam= Tracery M.tsr MAJOR REPAIR AND ALTERATION USOstamment of FAA Um OM, et Tremaeneten (Airframe, Powerplant, Propeller, or Appliance) !Sorel Aveiro AsIminisermlen INSTRUCTIONS: Print or type all entries. See Tree 14 CFR §43.9. Pal 43 Appendix 8. and AC 43.94 (or subsequent revision thereof) for Instrucbons and disposnon of this form. This report a required by law (49 U.S.C. §44701). Failure o report can result in a civil penalty for each such violation. (49 U.S.C. §46301(a)) Nationality and Registration Mad N405PJ Serial No. 53375 1. Aircraft Make Bell Model 407 Series 206 Name (As shown on registration certtricate) Address (As shown on registration certhcare) MM. 901 Langley Way 2. Owner Cyr Red Bluff sate CA Helibro, LLC. zo 96080 ca' a l i USA 3. For FAA Use Only 4. Typo 6. Unit identification Rep* Mandel Unit Make Model Serial NO. O El AIRFRAME (As described in Nero 1 above) . O POWEFtPtANT O El PROPELLER O O APPLIANCE bee msninedurer S. Conformity Statement A. Agency's Name and AddreSS B. Kind of Agency inn P,1 Helicooters Inc U S Connate, Methane I Manufacture. Man 903 Lanotey Way Foreign Carl/awe Mechanic C Certificate No. on Red Bluff sue . CA i Caveats, Repay Staten AWTR306C r.. 96080 c.v., USA Carbf)C0030 Maintenance 0reanabce 0. leerily that the repair and/or alteration made to the unit( ) identified in ACM 5 above and desalted on the reverse or attachments hereto have been made in accordance with the reqoarements of Pad 43 of the U.S. Federal Avistion Regulations and that the Information furnished herein is true and correct to the best of my knowledge. Extended range fuel pet 14 CFR Part 43 APP. 8 0 SignatureiDate of Authorized Individual el: 7-- - 7.-------CH.7(1 7:01 Brandon Hall 12/1/2016 PJ 7. Approval for Return to Service 91 Ras, to the authority given persons specified below. the aid identified in Item 5 was respected in the manner presorted by the Administrator of the Federal Aviation Administration and is 0 Approved O Reacted FAA Fit Standards Inspector Manufacturer Maintenance Organization Persons ADOMeed by GAMMA D•Palment or Transco, BY FAA Designee I Repair Station inspection Authorization Other (Specify) Certificate or Designation No. AVVIR306C Straturol3ate of Authorized Individual P,JH Joseph Tierno 12/1/2016 525 FAA Form 337 1, ..! SDNY_Glvl_02756480 5 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243402 EFTA01328518

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. S. Description of Work Accomplished (If mote space is required attach additional sheets Identify well worm? nationality and registration mark and date work Completed) N405PJ Nationality and Repetration Mark Aircraft Total Time: 2210.0 Serial Number: 53375 Installation of PJ Helicopters External Cargo Container STC# SR02494LA 12/1/2016 Date 1. Installed PJ Helicopters External Cargo Container referencing PJ Helicopters FAA Approved Master Data List, Document No. PJ9001006-MDL Rev. A dated 1/23/2014. 2. Instructions for continued airworthiness to be performed referencing PJ Helicopters ICA Report No. PJ9001006-ICA initial release dated 10/25/2013 or the latest FAA approved revision. 3. Updated the Flight Manual with the PJ Helicopters FAA Approved Rotorcraft Flight Manual Supplement Document No. PJ9001000B-RFMS initial release dated 3/10/2014. 4. Aircraft weight and balance and equipment list has been updated. Permanent structural provisions entered in the aircraft weight and balance at the time of installation. Cargo container and cargo weight has been deemed removable equipment, weight and balance to be determined upon time of installation/removal, reference Rotorcraft Flight Manual Supplement. 5. An appropriate logbook entry has been made. END Additional Sheets Are Attached FAA Form 337 nom: SDNYGivl_02756481 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243403 EFTA01328519

0 usOidamien MAJOR REPAIR AND ALTERATION of Triratowcn (Airframe, Powerplant, Propeller, or Appliance) /Swill A•istion AtiminIstniton Fan fl ays! OMB NO 2120W20 2410011 Elscimm -Ado ram.. ter IAA UN Ority INSTRUCTIONS. Print or type all entries. See Title 14 CFR §43.9. Part 43 Appendix B, and AC 43.9-1 (or subsea sit revision thereof) For instructions and disposition of this form. This report is required by law (49 V.S.C. §44701). Failure to report can result In a Civil penalty for each such violation. (49 U S.C. 546301(a)) Y. Aircraft Nationality and Registration Mark N405PJ Serial No. 53375 Make Bell Model 407 Series 3. Owner Name (As snovm On regisfrahOn certeicare) Helibro LLC. Address (As ShOwn On registration certificate) AeSen am I anglay Way cry Red Bluff f.'s. CA bp 96080 CO.F.Y Lan, 3. For FAA Use Only 4. Type S. Unit Identification Repair Alerabon Unit Make Model Serial No. El El (As descnbed In hem I above) AIRFRAME O O pemERptANT O O PROPELLER El O APPLIANCE Type Menerectwer 6 Conformity Statement A. Agency's Name and Address B. Kind of Agency N. P II Heliemphara Inc U S CerbficaYa Mechanic I ManulaClunn Nova 903 Lenin') Way Foreign Can/a...a Mechanc C. Certificate No. on Red Bluff Yee elk i f artilcaled papaw station AVVTR306C ze 96080 cur., USA Conificatoe Mantileunn Orgaihni/On 0. I certify that the repair and/or Iteration made to the unit( )identified In item 5 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Pmt 43 of the U.S. Federal Aviation Regulations and that the nformation furnished heran is true and co rect to the best o4 my knovAedge. Extended range fuel per 14 CFR Part 43 APP B . Signature/Dale Of Authorized Individual Derek Spooner 1/5/2017 ...7..."....._ NH $50 T. Ancona' for Return to Service Pursuant to tne authority g von perAXS speeded below, the unit identified in 4em 5 was rtspeded in the mangle prescribed by the Administrator of the Federal Aviation Administration and is Ei Approved O Rejected BY FAA Fs standards inspector Manufacturer Maintenance Organization Persons Approved by Canadian ciimanniont or Transport FAA Designee I Repair Station Inspection Authorization Other (Specify) Cart, Late or Designation No. AVVTR306C Signature/Date of Authorized Individual RIK Derek Spooner 1/512017 -- .:,.. s--- 850 FAA Form 337 mice) SDNY_GM_02756482 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243404 EFTA01328520

NOTICE Weight and balance or operating kmilation changes shall be entered in the appropriate aireratt record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. DescripUon of Work Accomplished (II mom space is mewed. attach acketionai sheets Identity wah aircraft nations/4e and registrabon mark and date work completed) N405PJ Nationality and Regetration Mark 1/5/2017 Date Aircraft Total Time: 2223.3 Aircraft Serial Number: 53375 • ' Installed Helifab Inc. STC #SR02597LA Radar Altimeter Antenna in accordance with Helifab Inc. Installation Instructions Document #HF-N-7-6 Rev. A. Helifab Inc. Master Drawing List Document #HF-MDL-7.6 Rev. A, and Helifab Inc. Instructions For Continued Airworthiness Document #HF-CA-7-6 Rev. IR. • Instructions For Continued Airworthiness to be complied with in accordance with Helifab Inc. Instructions For Continued Airworthiness Document #HF-CA-7-6. • Weight and Balance and Equipment List have been updated. 'No Flight Manual Supplement was provided from Helifab Inc • An appropriate logbook entry has been made. Addeional sneets Are Attached FAA Form 337 noon SDNY_GM_02756483 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243405 EFTA01328521

0 8 FAA FORM 81304, APPLICATION FOR U.S. AIRWORTHINESS CERTIFICATE 0 Form APproved o M.a No 2120-0018 tO 0 TI Ex Konen Dow 000.020 I I 0 APPLICATION FOR US. OsorMNII U.S. AIRWORTHINESS FATS 444/10•144441104 CERTIFICATE INSIONIO. INSTRUCTIONS -Pmt or lope. Oo Parole in shoka ma,. men ant fa FM uwasf SWAN *Vim' Prey lo we solkelmd FM Ropreseminvo IF Addionel *Pool • Few* uN 44•Mment Fee WPM Sr Penni+ emirate StOroms ".and VII RIRPONNIA II 1 REGISTRATIC/411MOC N4°5Pj 2 NRCRAIT EPALCEITS NAME wow 3 AIRCRAFT MODEL COGNATION 407 4 YR PPR FM CCCZA 1999 PP Cato 1 AIRCRAF1 SERIAL 1.0 53375 6 ENGINE SULDERSNAUE Mow R2im Royce I ENGINE 11000. DESOKATIEN 250-C476 Otani 1,00,g a RUINER CF EONS One 9: MEIER COWERS HARE Vsp NIA 10 acetate waft DESKAMON luSCPMT IS me. • %weepy lit NA lI MPORTCA N. CERTIRCATION REOUESTED PPPLICA R.n.,TIGN mo IS NE tThi REBY RACE FOR 4:4414 4444.44 es* I STANDNIDAMACRTIIIRESSCERTIFCATE U "." 4 I." . I Imms,cl I ,••••,- I I-" l•-a - I Ir.. 11 B i Pea angwal SPECIAL APIWORTFINES4 CERRACATIOsaftwermsway) J II man-SPORT ft...is Arpin Pasearaluie WNEAStalltatol OW Low Mon Pa 2 WINO i CLASS i 5 MONSIONAL mars wee 2 a 0/S5 It ,—.. I AdliCuL lull AND FIST CONTROL 2 ii a SLIMY 3 IS MMM. POVERTISING 3 RESTRICTED 0...w. osAmmi FOREST way rre. 0 PATROLLING 6 WAINER CONROE IM bionerOnnt 0 OTHER tscAm II 1 / RESEARCH ANDOEVELOPMENT 2 3 ii EXNENTO1 4 Mt RACING S CREW TRYING liAlIATEVROJILT I PARKET OWNER S .,' TO NONCENVELLNCE MMUS cs* I °MAWS If I err easesitga SULT AIRCMFT EXPERIMENTAL OA Emirs astrefustrei on siwilvais NNW% & WO mad 3 CCU 4 st A.A.r. no /NAY • P. 44•44444 4 OPERATP4 OS ° PP. 'S USIRSPRI Fault UGHTSPORT ec Owen) etelleet preeiceary *sod IONS WOW Cain OrtgifIling.. wean war 0 21193 lia/AAPEO IA RESEARCH AND DERELCINIENT I RC j JCREIN INNING e ANCRACT as &CARNET SURREY : I PERRY FUert FOR REPAIRS. ALTERA AGNS seiertemetece ORSTORMS 4 Sofa/ER.0S PERROT Ames 2 EVACUATE FROM AREA OF IMPENUNG CANCER 0 Ss. •boar.4441 N. ~IN Leta Mr Ora 444444 eat 3 CP:GRAMME ELMS OF IMAIMAI CERTSCATIOTANSOFF PIDGIN 4 DEUVERIVG OR EXPORTI443 IS I I PRODUCTION RIGHT TESTINO S 0/STORER CENCINSIMTION FUGNIS CI 6 -17U.LTPLE MAPANIFRAESS CERTIFICATE Mom Matt me.. swam. seelmeser. %saw surearral § 3 o = ° 13 r 1 d A REGISTERED OMER 0., "An m m.mantmormmomm) IF DEALER.CNECII NEM I H7eiib roPRI LLc means ) 903 Langley Way, Red Blue. 0 9608 IF NRCAAFT see TON OR TYPE CE KATE OATA SHEET 1.3404. SI j 1 neveness ORECT1WS Rear EIMOIS/100••••••••ONSIed rfaef•••••• ✓tirserteoSuPVUliPer sae pe army ens arra e so c✓neerider MOM 1702/2010-12/250018 NRCIMF I USING MIRNFRAPNAGU / Ilf SUPPLEMENTAL TYPE CERTIFCATE pm AFT ear Netnews* WA c NACRol7 OPERATION ANO UMPTEILOCE RECORDS j COCO( a RE CQIIWARICESOARC64n4 3 IN 14CFR NS, SIMI 'TOTAL mRFRostE HO 2222.7 EXPEINIENTAL ONLY PLIWPSIPass sIMINNONINIMmle sm••••• 0 WarallON . I Nolesoonty Sue I acorn Rol Tin 0)01 to Ulna NanCom ~vivo, cons mown wi re mpIINNI mar IN At EOM el MI Moll Onart01 4001 Ms at amilatIt F•Pire RAMS Rostaioni. item. MN Ms aval • maim, i.e the SRNS Mace Achwince m Ina to mosemA Ni Own aseas0 at onmetts at woos Id ON DATE OF APPUCATION 03 Jan. 2017 NAME NO TITLE preertm) Mark Gunsauls, Member' ;tgite 4..m.},, i § 1 i V A ISE NROTAFT E ll NAS SEEN INSPECTEONO FOUND NIMORTHY SY Swami IN mom Pe14 Mts.. 7. 2 14 CFR pz 121 CERTIFICATE SOLDER An I I I !CERTIFICATED MECNANC No. molar RN l e l 1 ,C:rill-ICA REPAIR STATION AN Gioia 5 AiRCRArr ILANJFACIINER Moo momegag GTE TITLE SIGNATURE . 4 4 i i s 1 • s Nu flea AU sad. OP 444s 4.40 0 INE COGIFICAlt REQUESTED Allan. o• amyl burped Si say a vi mots rooms kw Al AINICRIENI OR /400SCATION OF CURRENT Airman mess unman 0 INPNETR In woos RV paw mar FM INSPECTOR FM OC Secowni ono alma. 87 CERTIFICATE 1.82t0ER ta40ER Li WIDE NUR WIG U14CFRosi IN CCM LI to CFR poi NS DATE 05 Orli IICOCSDO COME Mil 'V o FM INSPECTORS 5 a CE 3Kittor ti Alcrof snipe 1 FM INONECTCNI CERTIFICATION FILE REVIEW SIGNA71.888 7a4t.t. A.L.,-) A $ ' Se -^b4 FM Form 81304 (0c201 ) PrevIma adept Superseded Elec000ic Formal -POE 4sge I of SDNY_GM_02756484 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243406 EFTA01328522

§ i V 5 A MANUFACTURER TIME AOORESS II PROCUCTON BASIS (Ordi MM MIN . PROOUCTION CERTFICATE (Gwomxlverm cioN6PIN mm e? TYPE CERTFICATE OINElt C GIVE OLIMITTEY Of CERTIFICATES RIMMED FOR OPERATING NEEDS ' DATE a APPLICATOR I NAME AND TITLE (Pen Wipe) SIGNATURE r. i i VA g 5 g 0 • i . I • i E i g 5 g A CESCRIPTION OF MCRAE! REGISTERED OWNER AGGRESS (OLDER (Mon MODEL SERIAL MANIER REGISTRATION MARX B DESCRIPTION OF FLOG CUSTOMER ODADHSTRATON FLORES Li ,enc.,,,c,..., FROV TO DEPARTURE DATE I DURATION C CREW REQUIREDTOOPERATE THE ARCRAFT AND DIOUF/AM PILOT I I COPILOT i I FUGHT DIGNEER L OTHER (SpooFol 0. AIRCRAFT 0055 NOT IIEET THE APPLICABLE ARVANTINMESS REGUREMENTS AS FOLLOWS TNE FOLLOWING RESTRICTIONS ARE CONSGEREO PECESSARV FOR SAFE OPERATION (Um oteachormidmootwy) F CERMICATION • I Ant, welly mm I am me rep arm caw (or Ns gyro at me awe *end aboa ihs re alcraltamploteml web Me W.A./Waal Admen:talon in axaconce mei Mend irpe Vr•ed Slaws Cod* 4410! sag Bed Acole.aele Foyeim Aragon RspoMmo. MO Mil ire SUM ft Ma, nopooM sed e SIN AYH lighl itInat•il DATE NAME MO TITLE (NM of DEO SIGNATURE w = Bi E I 4F i s ri l i A rows Unpin one Ilirkelpo .1 Conpienoo Will I4 CFR Saco-an 9I p G Stoned co Colon* FM Fenn $1509 Moen whoa maw.* N romp Armewnwo Cornice*, Ivo MARI Aaron /Ana ow Alan** E a Guns Olmnillop Latta'''. Maas: v , C Dec. Oramp. Protopraph. Ma (Mach ...Nen Pey.wid) V I Plevan Armamom OPIEcote Nmed a Accadtros NM la CFR Baron 21.183(IN CAR (0apeuto•RAIE9 /DO -two Waco aid Bane Irfonirolai Owlifta in Aram EVAN Radar end Mack FM Pam 337 (holm !Mon foquo0) 1 1 Omni Araccovess Conical. Ismod on Acconance With 11 CFR SKIICti 21.191(a) ICON PROCEVCO i F Ow maim RacaGod m Moat Rocmis PC Loh.40,1 Matt SIOIron d tertolonce. FM ram $130-15 WAWA roam requivd) FAA Fam 11304400-201 IOM PrerOus EdMIS SLIPOROSed Eledmcdc Formal • POF Pops 2 d2 SDNY_GM_02756485 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243407 EFTA01328523

UNITED STATES OF AMERICA DEPORTMENT OF TRANSPORTATION • FEDERAL maATiON ADIAMSTRAPON SPECIAL AIRWORTHINESS CERTIFICATE A CATEGORY/DESIGNATION EXPERIMENTAL, PURPOSE RESEARCH & DEVELOPMENT B MANU- FACTURER NAME NIA'. ADDRESS N7A - '';'7,-...::- ".. C FLIGHT FROM . .... ...... .- TO N/A • ,- D N- 405P1 SERIAL NO. 53375 BUILDER Bell MODEL 407 E DATE OF ISSUANCE 05 Jan, 20, 7 .EXPIRY 04 Feb, 20)7 OPERATING LIMITATIONS DATED 05 Jab, 2011 ' 'ARE PART OF THIS CERTIFICATE W all /RE OF "A nffiCSENTATIvt . • Carrie Ricca a -t • . ' s py., DESIGNATION OR OFFICE NO. 547098732 Any ateretal, rep( misuse of ito certificate may be punishable Inaba not exceeding SI,C00 or imprisonment not weeding 3 yews, or WI. THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE TITLE IA, CODE OF FEDERAL REGULATIONS (CFR). : FMFgm 51*7 i0v1OmPohosi Sion 0701 Ay be Utaket10~ SDNY_GM_02756486 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243408 EFTA01328524

SDNYGM02756487 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243409 EFTA01328525

U.S. Department of Transportation Federal Aviation Administration Operating limitations for 14405FU Bell 407, S/N 53375 05 Jan 2017 1. This aircraft does not meet the airworthiness requirements specified in Annex 8 to the Convention on International Civil Aviation. Operations In civil airspace outside of the United States will require the written permission of the applicable Civil Aviation Authorities (CAA). That written permission must be carried aboard the aircraft together with the U.S. airworthiness certificate and, upon request, be made available to an FAA inspector or the CAA in the country of operation. Operations may be further restricted by the foreign CAA. This may include not allowing use of an airport, requiring specific routing, and restricting flight over specific areas. The operator must comply with any additional limitation prescribed by the CAA when operating in its airspace. (1) 2. No person may operate this aircraft for any other purpose specified on the face of the FAA Form 8130-7. These operating limitations do not provide any relief from any applicable law or regulation. This aircraft must be operated in accordance with applicable regulations and the additional limitations prescribed herein. Note that a clearance from air traffic control (ATC) is not authorization for a pilot to deviate from any rule, regulation, operating limitation, or minimum altitude, or to conduct unsafe operation of the aircraft. If ATC issues a clearance that would cause a pilot to deviate from a rule. regulation, or operating limitation, or in the pilot's opinion, would place the aircraft in jeopardy, it is the pilot's responsibility to request an amended clearance. These operating limitations are a part of FAA Form 8130-7 and are to be carried in the aircraft at all times and to be available to the pilot in command of the aircraft. (2) 3. This special airworthiness certificate and attached operating limitations are not in effect during public aircraft operations (MO). Concurrent public/civil operations are not permitted; the aircraft cannot be operated as a civil aircraft and as a public aircraft at the same time. This airworthiness certificate is not in effect during flights related to providing military services (that is. air combat maneuvering, air-to-air gunnery, target towing, electronic countermeasures simulation, cruise missile simulation, and air refueling). These activities are inherent military training activities, not civil activities. The FAA makes the distinction between the authorized flights for experimental purposes, as described in the program letter, and PAO. Before operating this aircraft under this special airworthiness certificate following a PAO, the aircraft must be returned via an approved method to the condition and configuration at the time of airworthiness certification. This action must be documented in the aircraft records. The aircraft records and entries must clearly differentiate between a civil experimental flight per this certificate and any other flights. (3) 4. Application to amend these operating limitations must be made to the local Flight Standards District Office (FSDO) or Manufacturing Inspection District Office (MIDO). (6) 5. The pilot in command of this aircraft must hold Rotorcraft category and Helicopter class certificate or privilege. The pilot in command must hold all required ratings or authorizations, and endorsements required by 14 CFR pan 61. (7) 6. The pilot in command must hold: (a) An appropriate type rating (if one has been established); or (b) An experimental aircraft authorization, by make and model, on their pilot certificate; or (c) A temporary LOA issued by an FAA Flight Standards Operations Inspector. (d) For the purpose of completing the practical test for the issuance of an experimental aircraft authorization, a qualified instructor may make a logbook endorsement permitting limited local solo operations for a period of not more than 30 days. (8) 7. When filing a flight plan, the experimental nature of this aircraft must be listed in the remarks section. (10) 8. This aircraft must not be used for towing, including, but not limited to glider towing, banner towing, target towing or towing electronic receivers or emitters. This aircraft must not be used for intentional parachute jumping. (12) Page 1 of 3 SDNY_GM_02756488 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243410 EFTA01328526

SDNYGM02756489 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243411 EFTA01328527

U.S. Department of Transportation Federal Aviation Administration Operating limitations for N405PJ Bell 407, S/N 53375 05 Jan 2017 9. If aircraft, engine, or propeller operating limitations are exceeded outside of planned test conditions, an appropriate entry will be made in the aircraft records. (13) 10. No person may operate this aircraft unless it is maintained in accordance with an inspection program meeting the scope and content as described in 14 CFR 91.409(f). The operator must select and identify in the aircraft maintenance records, one of the following programs for the inspection of the aircraft: (1) For type certificated aircraft a current inspection program recommended by the manufacturer; or (2) For former military aircraft an inspection program recommended by the manufacturer or North Atlantic Treaty Organization (NATO) military service; or (3) An FAA-approved inspection program. Note: To extend an inspection interval, the owner/operator must submit a request for that extension with supporting documentation and data to the local FSDO and obtain concurrence from that FSDO. Inspections must be recorded in the aircraft maintenance records showing the following, or a similarly worded, statement: 1 certify that this aircraft has been inspected on (insert date) per (identify applicable inspection program] and found to be in a condition for safe operation? (14) 11. Only FAA-certificated repair stations, FAA-certificated mechanics with appropriate ratings, or a manufacturer as authorized by § 43.3 may perform inspections required by these operating limitations. (18) 12. The aircraft may not be operated unless the replacement for life-limited articles specified in the applicable technical publications pertaining to the aircraft and its articles are complied with in one of the following manners: (a) Type-Certificated Products: Replacement of life-limited parts required by § 91.409(e) applies to experimental aircraft when the required replacement times are specified in the U.S. aircraft specifications, or type certificate data sheets. (b) Non-Type-Certificated Products: All articles installed in non-type-certificated products operated under an airworthiness certificate issued for an experimental purpose, in which the manufacturer has specified limits, must include in their program an equivalent level of safety for those articles. These limits must be evaluated for their current operating environment and addressed in the approved inspection program. All articles installed in non-type-certificated products in which the manufacturer has specified limits, must include In their program an equivalent level of safety for those articles. The article must be inspected to ensure that the equivalent level of safety still renders the product in a serviceable condition for safe operation. (19) 13. For aircraft originally incorporating fatigue life recording systems, the owner/operator must maintain and use the system as prescribed by the aircraft manufacturer and comply with the manufacturer's fatigue life limits. (20) 14. Day VFR flight operations are authorized. Night flight operations are authorized if the instruments specified in § 91.205(c) are installed, operational, and maintained in accordance with the applicable requirements of part 91. Instrument flight operations are authorized if the instruments specified in § 91.205(d) are installed, operational, and maintained in accordance with the applicable requirements of part 91. The pilot in command must have a method to comply with the § 91.319(c) prohibition from operating over densely populated areas or in congested airways. All maintenance or inspection of this equipment must be recorded in the aircraft maintenance records and include the following items: date, work performed, and name and certificate number of person returning aircraft to service. (41) 15. All flights must be conducted within the geographic area described as follows (there may be areas within the geographical area that are not suitable for operation and may include ingress/egress routes). Aircraft based at the Red Bluff Municipal Airport. Aircraft must operate within the area identified on the attached Page 2 of 3 SDNY_GM_02756490 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243412 EFTA01328528

SDNYGM027564.1 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243413 EFTA01328529

U.S. Department of Transportation Federal Aviation Administration Operating limitations for N405P1 Bell 407, S/N 53375 sectional dated 10/10/12, while avoiding densely populated areas, and congested airways. (44) 05 Jan 2017 16. Flight over a densely populated area or in a congested airway is authorized in accordance with 4 91.319(c) only for the purpose of takeoff and landing. The area on the surface described by the term "only for the purpose of takeoff and landing' is the traffic pattern. For the purpose of this limitation, the term "only for the purpose of takeoff and landing' does not allow multiple traffic patterns for operations such as training or maintenance checks. This DOES NOT restrict a go-around/rejected landing for safety reasons. When avoiding populated areas, aircraft speed and weight must be considered. The information in FAA Order 8900.1, Flight Standards Information Management System (FSIMS), regarding set-back distances from spectator areas for aviation events such as air shows or air races may assist in determining a suitable space to fly the aircraft. (46) 17. No person may be carried in this aircraft during flight unless that person is essential to the purpose of the flight. 154) arrie Ricca DAR 547098732, Seattle MIDO, NM-51 Page 3 of 3 SDNY_GM_02756492 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 002434(4 EFTA01328530

SDNYGAL02756493 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243415 EFTA01328531

SDNY_GM_02756494 REVIEWED AND ACCEPTED SAC: FSDO SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243416 EFTA01328532

SDNYGM02756495 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243417 EFTA01328533

January 3s, 2017 Federal Aviation Administration Attn.: James Sprecher 1601 Lind Avenue SW Renton, WA 98057 SUBJECT: Program Letter for Special Airworthiness Certification REGISTERED OWNER: Helibro, LLC BUILDER: Bell MODEL: 407 SERIAL NO: 53375 Dear Mr. Sprecher: DESIGN CRITERIA: Research & Development NUMBER OF ENGINES: I NUMBER OF SEATS: 7 REGISTRATION NO.: N405PJ The purpose of this letter is to request a special airworthiness certificate, in the experimental category, for a Research & Development Airworthiness Certificate in accordance with Title 14 Code of Federal Regulations (14 CFR), § 21.191(a). This request is made to support company flight testing in support of FAA Project Number ST16493LA-R. The STC will be for the installation of a Secondary Hardpoint Installation on Bell Model 206 and 407 aircraft. The proposed Flight Testing will be conducted over I — 3 hours on or around the 5th of January, 2017. We request the designee hold the Standard Airworthiness in suspension until the completion of flight testing. The aircraft will be located at PJ Helicopters facilities in Red Bluff, Ca. The aircraft is within current maintenance, has been conformed to the TCDS and the following has been accomplished: • FAA Form 8130-6, with sections I, II, and III completed is enclosed. • The aircraft has been properly registered. • We have weighed the aircraft to determine that the most forward and aft center of gravity positions are within established limits. The weight and balance report is available at the aircraft. • The marking requirements of 14 CFR Part 45 have been complied with, including permanent application of appropriate registration marks and the word "EXPERIMENTAL" near each entrance to the cabin or cockpit. • The aircraft is inspected and maintained in accordance with the Bell Helicopter Maintenance Manuals. The following is a description of the requested geographical areas for flight testing: within the box defined on the attached sectional, while avoiding densely populated areas and congested airways. I request Larrie Ricca, DARF 547098732, be delegated to issue the requested airworthiness certificate. My telephone number is: additional information is needed. Sincerely, Please contact me at this number if there are any questions or if Dave McCanunon, Director of Maintenatice Operations Helibro, LLC Page I of I SDNY_GM_02756496 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00243418 EFTA01328534

SDNYGM02756497 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243419 EFTA01328535

SDNY_GM_02756498 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243420 EFTA01328536

SDNY_GM02756499 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243421 EFTA01328537

WOO STOW/ MOISICA PIPAR1VPrt OF IAPTIPORTAIIT•eNDIPATINIUMNACINPOISTOV • SPECIAL AIRWORTHINESS CERTIFICATE CATEOCEIWOEKIIARCN EXPERIMENTAL PURPOSE RERARCIll A DEVELOPMENT , • IIANU. NAVE N/A SACILRER ADDRESS N/A C I FRCSS N/A i TO N/A D N. 405P1 SERIN. NO EULDER Bell l 407 E DATE Cf ssumit-E IM, 2017 DPW a rCKNTI 7 Q_PERATINO LIM DATED ARE PART OF 1143 CERTICCAll wo.,70.• c• ..... .my R Kr cesouncrom I:frit( NO NIT0911732 Any Sake ea a PAU* nut te Ftereetre te a Rear swede, VAN BISVIrell AM c.a." 1 ark ar teet 1149. CERTINCATE RUST Ilt OSPLAY10 N TNT APCRIAl NI 52:91ROya MTH IOWA! TOW IA COOT Ce FIEDFAM. RFOLLADOVS (MN p metro. W SONY_GM_0275650D T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 002434?? EFTA01328538

A a Tit Sitinilti• Oink. lamaate OA ilitatirdniCia• IOU, laUllealitil Cat (=WU "011ie S4 Ca d Nan RI9AakralCFR) . a 11 arsatreta ant* wham. re ^Ye tladaW raraticolonasew as Omelet patxdoi Iran ardcak pradscknfidt awn al wool aphelia lora It portray Wife catexko Wags tante cello. 1, I Carr° omen CFMOMONCONfaitcno, Illtr r6 (2)Caryna noon natosional b Os psposa al retail ,.. v On an•oitims oink:* atoms too eel SPPAN Pre tom oda bt hi pawn obi., ir, bed A D TM am:Motu craw* °Wm tat aid Nan d wan N want * onto mown.; Wen ',spy:WNW b..4 kited3e WPftot.hdtve 'MadeCFR The moll kora wit. •40 4•Wea d 70 IPPCX4 COloallin• an: Mallme:MAUS COO* K acyeal ty Arra So Ot Grotto Ch tratmaaral eel Andre lb am, ,,, own to woe hotel en to ...wt. to. (9e.cid ON /0XeSiXt ter, no ndeaft CFR ea l• aissruxe min mown rd :among onatnay to :ascot,' ay no FiaMPAccen, Onta, r. 2, ow 2Prowf, coal Meath Neu wisest). &CO carry E sorer iarenlers1 heontcd cr ' ,Kee: Min.othrto collate a dleche bat O.nw eta taw no °maws poncobe n SI CFR Pitl /1 Sorton 21 ,61 a 2121? S0NY_GM_02756501 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00243423 EFTA01328539

UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE I NATINAUTY AND 2 MANUFACTURER MO MOOS. 3 AIRCRAFT SERLS4. 4 CATEOORY REGISTRATION MARKS N40511.1 Bell Helicopter Textron Canadi Model 407 NUMBER 5337$ Normal 5 AITCRITY ANOBMIS FOR ISSUANCE Riebration onto* 5 Mod pesue6 40111C4.44701.1 orOss N. ad le Oro d mock he aisnibutids Seta eeee send ird bedb &dm b te Pike liettkr. tut n cram b we Stem Veen b ant IS manna onto Sone caradhense SS'S alum code a pea by eaces Re Cwoveri m Werratensl CM AS esat4 a roar tem EstReols • ***None"' 6 TERMS MO COMMONS • OS are sww0e44. saxeCed recktice a iimivIce IS a Minim estektel bite MAY skeethale101.1011, a ate a bi; aisle nerbaira:Faeclato =edema. Siloam n phenol Inueoloone Pals 21. A ea 11 d re Fein ASA es /MN eacree Ned USd SOU. DATE OF ISSUANCE HT TN e 0E5IGNATION PRIMER _. FityPRE 05 APR 2016 'an cfrekee DART710617WP alleratat rept:6410w nand en colt* tose be pfita%Wale MemetsbeS1 Mei Imeeenst waft /pays kit NS War CATE VAT BE DISPLAYED PI ttE MICRIST M AnillruatE NTH Okra( FOOML Awnpazommots. FM Faze 8103-2 (04-11) Swerzetes Previous Ed.non AEN6Pititair0 o& TAA) ()(91-7 SDNY_GM_02756502 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243424 EFTA01328540

SDNYGAL02756503 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243425 EFTA01328541

U.S. Department of Transportation Federal Aviation Administration Operating limitations for N4435P1 Bell 407, S/N 53375 1. This aircraft does not meet the airworthiness requirements specified in Annex 8 to the/ on /vention on International Civil Aviation. Operations in civil airspace outside of the United States will equire the written permission of the applicable Civil Aviation Authorities (CAA). That written permission lust be carried aboard the aircraft together with the U.S. airworthiness certificate and, upon request, be m,de available to an FAA inspector or the CAA in the country of operation. Operations may be further restricted by the foreign CAA. This may include not allowing use of an airport, requiring specific routing, a rettricting flight over specific areas. The operator must comply with any additional limitation ores& b fie CAA when operating in its airspace. (1) 2. No person may operate this aircraft for any other purpose speci ti)i the face of the FAA Form 8130-7. These operating limitations do not provide any relief from any app is € law or regulation. This aircraft must be operated in accordance with applicable regulations and the additi al limitations prescribed herein. Note that a clearance from air traffic control (ATC) is not authorization -ei pilot to deviate from any rule, regulation, operating limitation, or minimum altitude, or to co unsafe operation of the aircraft. If ATC issues a clearance that would cause a pilot to deviate from egulation, or operating limitation, or in the pilot's opinion, would place the aircraft in jeopardy, it is th s responsibility to request an amended clearance. These operating limitations are a part of FAA Fo 30-7 and are to be carried in the aircraft at all times and to be available to the pilot in command of the air a . (2) 05 Jan 2017 3. This special airworthiness certificate and attache e p ting limitations are not in effect during public e aircraft operations (PAO). Concurrent public/civil o ei ions are not permitted; the aircraft cannot be operated as a civil aircraft and as a public aircraft at t same time. This airworthiness certificate is not in effect during flights related to providing military services at is, air combat maneuvering, air-to-air gunnery, target towing, electronic countermeasures simulati n, cr Ise missile simulation, and air refueling). These activities are inherent military training activities, not ci I Itivities. The FAA makes the distinction between the authorized flights for experimental purposes described in the program letter, and PAO. Before operating this aircraft under this special airwonhines ificate following a PAO, the aircraft must be returned via an approved method to the condition and c guration at the time of airworthiness certification. This action must be documented in the aircraft rec The aircraft records and entries must clearly differentiate between a civil experimental flight pe s certificate and any other flights. (3) 4. Application to amend thes %per ng limitations must be made to the local Flight Standards District Office (FSDO) or Manufacturing Inspctio trict Office (MIDO). (6) 5. The pilot in command of this ircraft must hold Rotorcraft category and Helicopter class certificate or privilege. The pilot in comma must hold all required ratings or authorizations, and endorsements required by 14 CFR part 61. (7) 6. The pilot in command ust hold: (a) An appropri e type rating (if one has been established); or (b) An expen ental aircraft authorization, by make and model, on their pilot certificate; or (c) A tempor ry WA issued by an FAA Flight Standards Operations Inspector. (d) For the urpose of completing the practical test for the issuance of an experimental aircraft authorization, a q lified instructor may make a logbook endorsement permitting limited local solo operations for a od of not more than 30 days. (8) 7. When filing4light plan, the experimental nature of this aircraft must be listed in the remarks section. (10) 8. This aircraft must not be used for towing, including, but not limited to glider towing, banner towing, target towing or towing electronic receivers or emitters. This aircraft must not be used for intentional parachute jumping. (12) Page 1 of 3 SDNY_GM_02756504 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243426 EFTA01328542

SDNY_GM02756505 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00243427 EFTA01328543

U.S. Department of Transportation Federal Aviation Administration Operating limitations for N4091 Bell 407, S/N 53375 OS Jan 2017 9. If aircraft, engine, or propeller operating limitations are exceeded outside of planned t t conditions, an appropriate entry will be made in the aircraft records. (73) 10. No person may operate this aircraft unless it is maintained in accordance A, inspection program meeting the scope and content as described in 14 CFR 91.409((). The open kttust select and identify in the aircraft maintenance records, one of the following programs for the insp ti n/of the aircraft: (1) For type certificated aircraft, a current inspection program reco ended by the manufacturer; or (2) For former military aircraft, an inspection program recomm@gded by the manufacturer or North Atlantic Treaty Organization (NATO) military service; or (3) An FAA-approved inspection program. Note: To extend an inspection interval, the owner/operir st submit a request for that extension with supporting documentation and data to the local FSDO and obt in concurrence from that FSDO. Inspections must be recorded in the aircraft maintenance record owing the following, or a similarly worded, statement: 1 certify that this aircraft has been ins on (insert date) per [identify applicable inspection program) and found to be in a condition for sa tion." (14) 11. Only FAA-certificated repair stations, FAA-certificated manufacturer as authorized by § 43.3 may perfor hanics with appropriate ratings, or a ons required by these operating limitations. (18) 12. The aircraft may not be operated unless the ment for life-limited articles specified in the applicable technical publications pertaining to the aircraft a s articles are complied with in one of the following manners: (a) Type-Certificated Products: Repla nt of life-limited parts required by § 91.409(e) applies to experimental aircraft when the required replg ment times are specified in the U.S. aircraft specifications, or type certificate data sheets. (b) Non-Type-Certificated Produces All articles installed in non-type-certificated products operated under an airworthiness certificate su r n experimental purpose, in which the manufacturer has specified limits, must include in their progr m quwalent level of safety for those articles. These limits must be evaluated for their current ()pecan g vironment and addressed in the approved inspection program. All articles installed in non-type-cercific ed products in which the manufacturer has specified limits, must include in their program an equivalent lev of safety for those articles. The article must be inspected to ensure that the equivalent level of safety still enders the product in a serviceable condition for safe operation. (19) 13. For aircraft originally inc porating fatigue life recording systems, the owner/operator must maintain and use the system as prescribe by the aircraft manufacturer and comply with the manufacturers fatigue life limits. (20) 14. Day VFR flight op ations are authorized. Night flight perations are authorized if the instruments specified in § 91.205(c) are installed, operational, and *ntained in accordance with the applicable requirements of part 91. Instrum t flight operations are authorized if the instruments specified in § 91.205(d) are installed, operational, an maintained in accordance with the applicable requirements of part 91. The pilot in command must have a shod to comply with the § 91.319(c) prohibition from operating over densely populated areas or in conger airways. All maintenance or inspection of this equipment must be recorded in the aircraft maintenanc ecords and include the following items: date, work performed, and name and certificate number of person returning aircraft to service. (41) 15. All flights must be conducted within the geographic area described as follows (there may be areas within the geographical area that are not suitable for operation and may include ingress/egress routes). Aircraft based at the Red Bluff Municipal Airport. Aircraft must operate within the area identified on the attached Page 2 of 3 SDNY_GM_02756506 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA _00243428 EFTA01328544

SDNYGM02756507 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243429 EFTA01328545

0 U.S. Department of Transportation Federal Aviation Administration Operating limitations for N405P1 Bell 407, S/N 53375 sectional dated 10/10/12, while avoiding densely populated areas, and congested airways. (44) 05 Jan 2017 16. Flight over a densely populated area or i7 a congested airway is authorized in accordance with 5 91.319(c) only for the purpose of takeoff and la dingy' The area on the surface desp dby the term "only for the purpose of takeoff and landing" is the traffic pattern. For the purpose of this li tion, the term "only for the purpose of takeoff and landing" does not allow multiple traffic patterns fo ations such as training or maintenance checks. This DOES NOT restrict a go-around/rejected landing for ty reasons. When avoiding popular areas, aircraft speed and weight must be considered. The information in FAA Order 8900.1, Flight Standardilnformation Management System (FSIMS), regarding set-back distances from spectator areas for avi. vents such as air shows or air races may assist in determining a suitable space to fly the aircraft. (46) 17. No person may be car n this aircraft during flight unless that person is essential to the purpose of the k flight. (54) ( Larrie Ricca OAR 547098732. the MIDO, NM-51 Page 3 of 3 SDNY_GM_02756508 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243430 EFTA01328546

SDNY_GM02756509 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00243431 EFTA01328547