UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE 1 NATIONALITY AND 2 MANUFACTURER AND MODEL 3 AIRCRAFT SERIAL 4 CATEGORY REGISTRATION MARKS Raytheon Aircraft NUMBER N188TS Company 400A RK-244 Transport 5 AUTHORITY AND BASIS FOR ISSUANCE This airworthiness certificate is issued pursuant to 49 U.S.C. § 44704 and certifies that, as of the date of issuance, the aircraft to which issued has been inspected and found to conform to the type certificate therefor, to be in condition for safe operation, and has been shown to meet the requirements of the applicable comprehensive and detailed airworthiness code as provided by Annex 8 to the Convention on International Civil Aviation, except as noted herein. Exceptions: -None- xtoz/tt/Aem 6 TERMS AND CONDITIONS Unless sooner surrendered, suspended, revoked, or a termination date is otherwise established by the FAA, this airworthiness certificate is effective as long as the maintenance, preventative maintenance, and alterations are performed in accordance with Parts 21, 43, and 91 of the Federal Aviation Regulations, as appropriate, and the aircraft is registered in the United States. DATE OF ISSUANCE R3/06/2014 Arnold Wolfe,(52:, „ s4? C,),VAL_. FM REPRESENTATIVE Any alteration, reproduction, or misuse of this certificate may be punishable by a fine not exceeding $1,000 or imprisonment not exceeding 3 years or both. THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. DESIGNATION NUMBER GL-25 FAA Form 8100-2 (04-11) Supersedes Previous Edition SOMIGM_02754903 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 I 825 EFTA01326943

SDNY_GM_02754904 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 I 826 EFTA01326944

• 0 MAJOR REPAIR AND ALTERATION US Otooftrroft a Triespalatten (Airframe, Powerplant, Propeller, or Appliance) Federal ANSI AtiniMalereen erra la 2, 204020 Err SOWOIS Ottarcedt RCN Maw foe MA Use Only INSTRUCTIONS: Print or type an entries. See Title 14 CFR §43.9. Pal 43 Amender It 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. g44701). FaIn to repx1 can resultant:we penally lot each such violation. (49 U.S.C. 946301019 1. Aircraft Nationality and Registration Mew UNITED STATES / N188TS Sent No. RK-244 /flake RAYTHEON AIRCRAFT COMPANY Model 400A Series 2. owner Name (As shoal en regatrarion csrtMcate) THORAIR LLC Address (As shown on nyistration CV: ea) Amen PO BOX 2218 SANDUSKY Pa" OHIO re 44871-2218 Caret UNITED STATES 3. For FAA Use Only 4. Type 6. Unit Identilleadon - Reese Mention tall Mae Model Serial No. 7 in AIRFRAME PAYTMONeetts./teONAWe (As described M Item / show) me244 POWERPLANT O nPROPELLER APPLIANCE Typo arinurackar 8. Conformity Statement A. Agency's Name and Address B. Kind et Agency Nee. Constant Aviation LLC a a Caritated Methane Altai:barer ram 355 RICHMOND ROAD Folio CellicM•11A•shanle C. Catificate No. Ph CLEVELAND as. OH 7 Crallaslad Rasa Saari CRS#WC7R348J a 44143 ea ," USA Crailuad Maintananos Oraarristion D. I certify DUI the repair anaor alteration made to the unas have been made In accordance Wm the requremorks of furnished herein is true and correct to the best of my km i _ Warned In Plan 6 above and described on the reverse or attachments hereto Pad 43 al me U.S. Federal Aviation Regulatens and that the InfomiatIon Extended TIMO0 SI prir 14 CFR Put 43 App. 8 fid ar Silkily I / Steven A. Watkins 10/04/2019 , vat for RMiletitillervice Punsuanl to the authority Administrator of the Federal below. the wit in item 5 Adml end Is 1 eyed nnspected .n Inc manner prescribed by Inc Rejected BY - FAA Ft Standards Inspector Manufacturer Maintenance Organization — Pence* Areemed by Camden Deporiereal al Ming:toe — Other ._., FM Designee MI  Repair Staler) neaten Authorization (SPec4 Certi cat or DesVation No CRS# WC7R346J SIgnaturaTM 7 / ---P---- ----- *Mud David Kerr 10/04/2019 FAA Form 337 (10/06) Page I SDNY_GM_02754905 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241827 EFTA01326945

NOTICE Weight and balance or operating limitabon changes shag be entered In the appropriate aircraft record_ M alteration must be compabble with all previous alterations to assure continued conformity with the eppricable airworthiness requirements. a. Description of Work Acton"liked pt mote apace brewer:oft attach plcStional sheets. Wen* wth aircraft nalicoally and regiftrallon ma* end dale were Cask* red) UNITED STATESMinn tOAW20I9 Plogioniay and Ribaeleslon Waal DMa Engine Inlet Rivet Repair Installed blind rivets in place of the damaged solid rivets on the lip of the right hand engine inlet forebody assembly part number 541000-004, serial number R0010, in accordance with nextant aerospace engineering order NT-EO-1118-31 rev IR dated 11/29/2018 with FM form 8110-3 dated 11/30/2018. Instructions for Continued Airworthiness: Follow the maintenance inspection practices in the aircraft maintenance manual. Inspection intervals shall remain as indicated in the aircraft maintenance manual or operators approved inspection program as appropriate. Weight and Balance unaffected. Reference Constant Aviation work order CCM-3160 END MAGUS:nal Sews NO needled FM Form 337 (10/06) Page 2 SDNY_GM_02754906 • • • SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241828 EFTA01326946

• • • U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION POMMSTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS 1. DATE November 30, 2018 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MARE Textron Aviation 1 MODEL NO. N541000-004 4. TYPE Meal &pia Papaw. MO Forebody Assy &NAME OF APPLICANT Nextant Aerospace LLC Cleveland, Ohio LIST OF DATA IL ICENTIREATION 7 TIRE NT-E0-1118-31 Rev. IR November 29, 2018 ------ ----- ----- Engine Inlet Rivet Repair. data are approved herein. This the data listed above specified by paragraph and engineering data necessary for for the entire repair. --END Notes: 1) The structural aspects only of the above listed approval Is only for the engineering data. It Indicates demonstrates compliance only with the regulations subparagraph listed below as "Appicabie Requirements." 2) This form constitutes FAA approval of as the substantiation of compliance to necessary requirements s Pun Pose or OATA: Englneedng data to support repair procedure for Textron 400A Forebody Assy P/N N541000-004, SIN R0010 under Nextant Aerospace Work Order No.10565.1.1. a APFUCMAI REQUIREMENTS (UM spa seated) CFR Tide 14 Part 25.301(25-23], 25.303(25-23], 25.305(eXbXcX25-231, 25.307(aX25-23], 25.801(25-00], 25.803i0b)(cX25-38], 25.605(8)(25-00], 25.807(25-23), 25.609(aXbX25-00), 25.611(25-23), 25.613(aXb)(cX25-00], 25.61%25-23], and 25.625(eXbXcX25-231 10. CERTIRCATION - Under Son Pan la on few above end an nelleen teginimmla el InAlmomnies o Recommend veMed by Senn of the AdmInIetralet end Pt manna MM co,20a4 end emtetione of spinning order 14 CM ached inn illabtal a MVO ben eurrinod In scan:Ince et nalbtolietl teoceOns ale lowellocanolyMe Sunders Used. op/Novel of then dale then dela I OW Trenrere 0 APProve II. SIONATUREMICF DESIGNATED ENE4NEERND RE pRESENTATNEMI 12. DESIGNATION NUIMERS1M 13. CUSSFICATIONNI 0 0j24.4":„...,7: Paul Nodding DERT-410115-CE StrurAures FAA Form 8110-3 (01101 SUPERSEDES PREVIOUS EDITION File Number: H18777-01 Page 1011 SDNY_GM_02754907 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241829 EFTA01326947

• • • SDNY_GM_02754908 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 I 830 EFTA01326948

• nextant aerospace //elimaaRel0 /AMU //RUJORN EO t HM0.111841 I Title: Engine Inlet Rivet Repair ENGINEERING ORDER ARTICLE DESCRIPTION fficlotWodl."401 Team &Won 100A Mast snomen:3 See Ramona —1 - 711— .....m...... Ds parpote cilia E0 Pio aloe for Na raulato of PM web (PM (R7212-540t)of mpqpiste lerpeti• pace d Pe dyne* NM Met (PM: 1620426A0540() al M seine ktel kxstotfastoenet The regal's' te Owomphhed en OM Fal /pre PIN forecdy mean* (RN 1154100X01. Sett R0010). REGULATORY . •••••••••pithsoolleaan oar citeilluandllialt Oa erpaanapkid to dIatchomarim 10.6:4 OYES ONO maw OYES 0 NZI let OYES ONO kip.* lerbibtred OYES 0 PO PeWoveliloistIsperesallos OYES ONO Dom ON EOPpleconey Yed might. tudana. tad stremb. Writ ;stoma. Lowniant aorta ION dnledwa a Mc airtellisse aempR OYES MICR ONO pale Cal It El) be exargished bp:aped palm or elarbropereket? MINOR OYES • AP312 • O ..... NO ...._ _ . Seism*? MeN,Meld INIWC9r•MONefedeinaltiness7 IMJOR ta iis MINOR ONO Ones IS NAM 0 MCA 0 STC (NI STOWILA 1 towns hiss Dap OYES ONO FMAlffl0VIL ION Elms O mo GENERAL IMIINIONSIO RPM I:O~RIvM Waft m RN Emise MitIM (TwINISbaw) esamstueepas 0 YES 0 NO IleSallainras Met PM N541000004 WI 80010 WO. 10S65 I. i ppm! WO. R we amoval). IOOW (R.1 W0) OperiMes Proms Smdketax CA.1015 REWSION sta. tan Iteran1P. NM INaalaa IR 11129/40l$ Mel Prcpaal NM P. Pmbelimoy RI 10/1/2019 UpiSled b remwe wok number DUMP itm dectike. three is mixt and $110.3 N M Meth NYi P. Awhalsnav Acta. w r MN Remade), P. Awhatheav fall/2019 COa0ad By K. Ifenefripi ION/2019 AWInd al , DbakInismd P. Awhelam Pinkhas AYSIIMMOV MII..... , . eve by Mir ION/2019 201t10010•1110 4CW ram No. NT.EOOI IRIPA Pas t 03 This Coconut Is Unconerolf *0 Ono Printed SDNY_GM_02754909 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241831 EFTA01326949

• • • SDNY_GM_02754910 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 I 832 EFTA01326950

• • nextant aerospace Natinuato //NW //WOW I E0 IfT.E0•1118-31 I Title: Engine Inlet Rivet Repair ENGINEERING ORDER PROCEDURES MN INAPUVO4 Fla 1 Veually inspett the trgle Se! Sp and barrel la arty otw damaged, nisang et loose banners. - II ao *Maw! draepandes are deteceet ecetnue MI Well IS C4101100 bib. - II iaS36:444 descepron we rcte canted Nutt,* ABIOGDOCS ingetabIt / 1414 2 VisuallyAmpect ihe arra rotor a deined in Sub T ask 724t-20420401 a/ Inman Inlemelimel LYE MANTENAACE 144NUAL -F.144-34P III poem reaskin) • II no allialel dscrepaxies wa dettete4 COMMA at remints Sinai toot - Indto,. ones:* se MK COMM Nubia Myopia lonfospilica CO 3 Longs dareplilvats MIMI, in Fgt., I and worn ovkanplably dill cal to teak., tamale men'. makog sure not lo Sage, gin OrPIRIZI ile Welt( kit pill it O 4 F'pacee be lidos alio wissirg Winn tor WY/ion albatrAlax Nat PR4CR3212-5.XX in lau of ncortai sold Nees MS2042104:64X - PinPern hobiby ay 444 mop 13 IS nawbed *MO" at NOM. per Chanyt tenni CA.1015 • Disinvie be careel avie lievei Ix tie anus 13 Is int slam Cheaytka cloosrent CA.1015 • Usip Os aianufullenea nasnandad inalahlte WI Intl tin eimi issianes per OweiyMax (band CA-1015 • Inspect the cargaled MIS loyally to bdiro ether hat bum Woad end Ihe stem has Wad Mt ugh Ito Oat head. Reba Carnytter donna CavIOIS ler Impede. raid tartan. AA .4 4 '••tc., lag -80— _ LIMITATIONS Rene INSTRUCTIONS FOR CONTINUING AIRWORTHINESS RCA's) Mow Pt rairisike brredke pylon ii MSS nulnlenence ranuat In pedal .*wis shdl Wein as iniceled in be simnel inanionwics mina °rowan 44444ofilipstkai pommel 42,4044• COMPLIANCE tIMPAR WW1 GP aer 410 A AfOVEMOIMNI)31 N.1,88 7:5 /MOM IOW MAIM itg 2.446/ no OTIAWalsOialla*MOESVR0ea..."0.6•100 ook4 /i• 1 14~' CRS, WC7R346J OAT fo/t/i1 En Ma NT4041 /R. A Paget d3 This Neuman. Uncontrolled Once Printed SDNY_GM_02754911 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241833 EFTA01326951

• • • SDNY_GM_02754912 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241834 EFTA01326952

• • • nextant aerospace II NSMASIID MOW //MORN ENGINEERING ORDER EO k NT-E0-1118-31 Tttle: Ina Inlet Repair I Figure 1: Damaged Rivet Location on RH Engine Inlet Up (Typical Shown) P. 3 cI3 Form No. NT.E0-01 f Roy A Thls Docua*nl Is Unconirollod Once Prmied SDNY_GM_02754913 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241835 EFTA01326953

• • • SDNY_GM_027.914 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241836 EFTA01326954

0 MAJOR REPAIR AND ALTERATION US Oen... Tninportallon Powerplant, Propeller, Appliance) now, 21204020 Es 501/201S Ibeeeee TnadneMetiew MAIM OM/ al (Airframe, or foists, Avilitlaa AdministeSs INSTRUCTIONS: Print or typo all entries. See Title 14 CFR gag. Pet 43 Appends 8, and AC 43.9.1 (or subsequent revision thereon for instructions and disposition or INS form. This repel Is required by law (49 U.S.C. §41701). Failure to report can result in a civil penalty for each such Nankin. (49 U.S.C. §46301(a)) 1. Aircraft Nationally and Registration Mak UNITED STATES / N188TS Serial No. RK-244 !make RAYTHEON AIRCRAFT COMPANY Model 400A Series 2. Owner Name (As shown as registabon caracole) THORAIR LLC Address (As shown on roghbation certificate) Anus PO 80X 22i0 VI SAPOUSXY saw OH 29 14$11 Cony VNITE0 STATES 3. For FAA Use Only 4. 5. Unit Idendfication (Mt Make Model Serial No. Revak Alteration ii pi AIRFRAME MYIIIIECOMIKOVIT CCIONIf (As Omaha in Man :above) RK-2.11 POWERPLANT PROPELLER APPLIANCE Tee Manaiaret 6. Conformity Statement A. Agency's Mane and Address B. KM of Agency Mao WOW, MAYEN U. S. Garaged Mechanic rasnasons, Ado.. 300110•00.1000 Foreign canelcated Mechanic _j C. Certificate No. oar CUEVEI/J0 Ss OH Centres:4 now Stinson CRS# WC7R346J 2* 411411 ow" WNW STATES Z C•finteled Mantionanca Oryanizaton II I codify Met the repair andlet eleretton made to In unigs have been made h =men* with the requirements of furnished Meath tme and eared le the ow et my ko0.04.106. bandied In MITI 5 above and described on the reverse or SttlidifTWES hereto Pad 43 of the U.S. Federal Aviation Regttatkas and that Vie Information ended range bal Ext per 14 CFR Pad 43 App. B K Slonare/DetedAul . r .„,.. #4, Ryan M Landes 10/7/2019 7. proval for Return to Service Pursuant to the authority gNen person speeded below, the wit Wenrtil Adrfilitistr atOr of the Federal ANation Administration and Is j In hem 6 Approved knpected In the mane( presorted by the Relecied BY — FM Fe. Standards Inspector — —. Manufachrer — Maintenance Organization Palmas Apiroved by Calm oepartmeni or Tramped r ......., FM Designee 7 Repair Station Inspection Authorizalion (Spray) Cerlificat or Designation No. CRS# WC7R346J SIgnatur died IndMduai David Kerr 10/7/2019 FAA Form 337 (10/06) Page I SDNYGivi02754915 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241837 EFTA01326955

NOTICE iveighr end balance or operating Nmitafion changes she, be entered In the appropriate aircraft recent M Salon must bbl compatible with aff previous alterations to EISSUM continued conformity will the applicable airworthiness requIreinent*. O. Description of Work ACCOMPlithel pf move sate is Mend. attach 80010701 sheet Wen* hen arced a:steamily and registration met* and date nor* cempreted) UNITEDSTATES/NIWTS 1017/2019 Nalknalltyars3 Raglatelkat Mark Data INSTALLATION OF ADS-B OUT ON PART 25 AIRCRAFT Complied with installation of BHE & Associates, LTD. STC# ST11216DS Installation of Automatic Dependent Surveillance-Broadcast Out on Part 25 Aircraft IAW BHE & Associates,LTD. Master Data List (MDL) number 584-00-0001 Rev.G. Dated 8/29/2019. Reference BHE & Associates, LTD. Aircraft Flight Manual Supplement (AFMS) Installation of ADS-B Out on Part 25 Aircraft. Report number 584-00-0046 Rev.C. Dated 5/4/2019. Reference BHE & Associates, LTD. Electrical Load Analysis (ELA) Installation of ADS-B Out on Part 25 Aircraft. Report number 584-00-0050 Rev.B. Dated 10/9/2018. Reference BHE & Associates, LTD. Instructions for Continued Airworthiness (ICA) Installation of ADS-B Out on Part 25 Aircraft. Report number 584-00-0047 Rev.D. Dated 3/19/2019. Weight and Balance: Reference calculated weight and balance dated 10/7/2019. Equipment List: Updated. Reference Work Order: CCM-R3160. END 1=1Additional Sheets An Method FM Form 337 (10/06) Page 2 SDNY_GM_02754916 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024I838 EFTA01326956

athee.s.tan efistries /Department efrrampottalint I;21,11cationflivithirtrathn Supplemental Type Cergficate Nailer. ST11216DS 7birenafrateivaedterBHE & Associates, Ltd. 12002 Warfield St. Suite 250 San Antonio, TX 78218 real per tbar at clap is the type juiptfintiefaffenag quad an' Me /inniations onaramennas dm:fitter specified Sena sear tie Onntuteineanrganratenis gifint25 itieFederal Aviation Regulations. Original Product - Tape Ct-rlilicate Numlict: Make: See attached AML Model: See attached AML See attached approved model list (AML) Description of 'Fyn Deakin Clamp:: Installation of automatic dependent surveillance-broadcast (ADS-B) out on Part 25 aircraft in accordance with Master Data List 584-00-0001, Revision IR, dated June 29. 2018 or later FAA approved revision. For Instructions for Continued Airworthiness and Airplane Flight Manual Supplement reference the attached AML Limitations and Conditions: I The installer must determine whether this design change is Compatible with previously approved modifications 2. If the holder agrees to permit another person to use this certificate to alter a product. the holder must give the other person written evidence of that pemaission 3. See attached AML for additional limitations and conditions. centfirate and's& supporting data guild is tie earn forappanniderrosoin in Oa unistsurmakrel, suspended snimiafroror a termination fate 4.r allientire andlisitify tendril-mi./Snuffing/tie falinnOnntion indinnairat iota Date of Application: February 9. 2018 Daic or lase:mem Junc 24. 2018 Dam kcissucd: Dow Am-acted: illy /Dina ion tit fidunnistrotar Seraame lit4 VT ORB Aviation Project ODA Administrator ODA-831473-SW My alwaecn of this certecate is eyeshade by a an al nal mewing 51.000. a Iftnicemaril not exceeding 3 yen a torn Pas cormcze may be transfeed or made evadable to third persons by brewing agreements er acepowee with IC CFR 2147. Possession ulna Supplemental Type Ceder-roe (STC) OeCofrenl by persons order than the STC holier does net cortabbste rights to the design data nor to altar an small aroatl signs. of propeller The STC, supporting documented:a (dramoos. Aetna:We speokatons. figM manual supplements. etc) is the property of nit SIC homer An STC holier who least • person buying STC war an arrcraft awes ,none. ce propener must prove that pe so yam tynnen purression accepts* to the FAA. IRS 14 CFR 21.120). FAA Form 5110-2 (914) Page 1 o12 SDNY_GM_02754917 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241839 EFTA01326957

thuitiatatts °amnia apartment 17fransportathn FeafrativiattS/larministration Supplemental 7)Te Cent/lc-ate INSTRUCTIONS The transfer endonernent below may be toed to notify dw appropnne FAA Aixereft Certifieatial Office ache [mien of this Supplernmul Type Cartgkate. The MA will reissue the certificate m the nose of the transfereeand leeward it to him. Transfer'Endorsement Transfer the ownership of Supplemental Type Certificate Number: ST11216DS To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement): eau itraalit *mama Irina: My alleradon e this conthstia 4 punishable by a Me Of flat exceeding 51.000. of Imprisonment not escaertrg 3 yaws. a bath this certificate may be Rfingerred de made AMAMI 30 two Mein by Witernents In accordance with Id CPR 2147. Possession of this Supplemental Type CeMcra (STC) Saturnine by persons at than the STC hart& does not con:A/luta rights 10 the design data nor to stem an stvel, Srget engine. or propeller. The STCh supeoceng eleceneetehen (dnawrtos, ireeeeekee. weeneelehe fight manual supthements, etc) is the property of the STC toblet. M SIC maw wow stows a person lo use the STC b alter an aitheft. shalt engine, a propeller must prova Mt person with erten Permission acceptable to the FM (Ref. II CFR 21.1201. FAA Form 8110.2(5114) Paget Of 2 SDNY_GM_O2754918 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241840 EFTA01326958

DocuSign Envelope a CFB621313.543FE8-4C8D.A4E34461F9B213045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS FOR THE INSTALLATION OF ADS-B OUT ON PART 25 AIRCRAFT REPORT No. 584-00-0047 Revision D Date: 03/19/2019 NOTICE: The contents of this document are proprietary to BHE & Associates. Ltd. and shall not be disclosed, disseminated, copied, or used except for purposes expressly authorized in writing by BHE & Associates, Ltd. BHE & Associates, Ltd. San Antonio, TX 78216 USA CAGE: N/A Pero By VT-DRB. FSCM 47MZ7, Snt 1 o139. 2019fMatf19 SDNY_GM_02754919 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241841 EFTA01326959

DocuSgn Envetope CFS82885-6FES4C8D-A4E3-5461F9820045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS NOTICES AND SIGNATURES Notices: Note: Paragraphs andror figure numbers followed by' i" indicate a change by latest revision. Approval Signatures: NAME SIGNATURE Prepared by: R. Zamora See rev IR Checked by: M. Graham See rev IR Approved by: M. Graham See rev IR REPORT No. 584-00-0047, Rev: D BHE & Associates, Ltd. Page 2 of 36 Red By VT.DRB. FSCM 471127. Sit 2 01 39, 201944.1a/f19 SDNY_GM_02754920 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241842 EFTA01326960

DocuSign Envelope ID: CFI36211185-6FE8-4C8D-A4E3-5461F9820045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS Record of Revisions , . . . Revision Number . . . ... . .. . Description of change - . .s. • .., .. — - . . - • RevislOn . , Date Approved IR Innis] Release 5/9/18 MG A Page 8, Section 1.1 revised transponder and GPS part numbers. Page 10, Section 2 remove 'Flight Hours' horn Table 4 6727/18 MG B Page 4, Revised list of aircraft models in Introduction Pages 9.24-25, 28-29. Revised aircraft models in Tables 3, 7, and 9. Pages 8 and 28, clarified wording for installation. 11/6118 MG C Revised Table 3 on page 9 Revised Table 4 on page 10 Revised Table 5 on page 26 Revised Table 6 on pages 27 & 28 Revised section 6.1.9 on page 31 Revised figures on pages 13 & 20, Added figures on pages 14, 17 & 18 1/18/19 MG D Added STC number on page 4. Added figure on page 24. Revised form form in Appendix C. 3(14lict REPORT No. 584-00-0047, Rev: D SHE & Associates, ltd. Page 3 of 36 Red By VT.DREI. FSCM 47M27. Sht 3 of 39. 2019/Mar/19 SDNY_GM_02754921 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241843 EFTA01326961

DowSign Envelope ID: CF862885-6FE8-4080-a4E3-5481F9620045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS INTRODUCTION These Instructions for Continued Airworthiness (ICA) document have been developed using the guidelines in Appendix 'if of 14 CFR Part 25 as required by §FAR 21.50 and §25.1529. This document is designed to provide avionics and aircraft technicians with sufficient information to inspect, troubleshoot, adjust, repair, test, remove, and install ADS-B on the following Part 25 Aircraft. • Bombardier Inc. - CL-600-1A11, CL-600-2Al2, CL-600.2816 (Challengers) • Gulfstream Aerospace -1125 Westwind Astra. Astra SPX. Gulfstream 100, 0150 • Gulfstream - G-1159, G-1159A, G-1159B, G-IV. GV • Gulfstream - 200 • Sabreliner - NA-265-65, NA-265-70, NA-265-80 • Textron Aviation Inc. — 500. 550, 5550, 560 (Citation) • Textron Aviation - 400, 400A (Beechjet) • Textron Aviation - 650 • Textron Aviation - HS.125 Series 700A, HS.125 Series 700B, BAe.125 Series 800A, BAe.125 Series 800B, Hawker 800XP. Hawker 750, Hawker 850XP. Hawker 900XP • Learjet - 60 (STC Aircraft) • Dassault Aviation - Falcon 10, Mystere-Falcon 50, Mystere-Falcon 20-05/D5/E5/F5, Mystere-Falcon 200. Mystere-Falcon 900 Table 1: Equipment Type Description New CPN I Qty DO-260B ADS-B Out TDR-94 Transponder 622-9352.502 0, 1 or 2* TDR-94D Transponder 622-9210.502 0, 1 or 2* GPS1203C GPS Receiver 84327-50-XXXX 0 or 1 CI 429.200 GPS Antenna CI 429-200 0 or 1 GPS-40005 GPS Receiver 822-2189- 004/005/006/007/010/011/100 0, 1 or 2 *Either TDR-94 or TDR-94D will be Installed. The above equipment is installed in accordance with FM Supplemental Type Certificate No. ST11216DS . See the List of Applicable Publications (LOAP) in Appendix A of this document. The publications listed in the LOAP constitute the required information essential for continued airworthiness for the aircraft. The documents contained in the LOAP are a necessary part of this ICA and the latest revision should be available to maintenance personnel when performing maintenance. The STC holder will continue to monitor changes to the ICA that were the basis of the supplementary ICA and provide revised supplemental ICA as necessary. The information in this document supplements or supersedes the original manufacturer's maintenance manual only in those areas listed. For limitations, procedures and other information not contained in this document, refer to the aircraft manufacturer's maintenance manuals, illustrated parts manuals and wiring diagrams or the vendor manuals as listed in the LOAP. REPORT No. 584-00-0047. Rev: BHE 8 Associates, Ltd. Page 4 of 36 Rye By VT-DRB. FSCM 476.127, SIB 4 a/ 39, 2019/MarD9 SDNY_GM_02754922 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241841 EFTA01326962

DocuSign Envelope ID: CFS62885SFE8-4C8O-A4E3-5461F9B2D045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS RECORD OF REVISIONS For continuous use of this document, this document must be maintained in current revision status. Each time the STC holder finds it necessary to revise this document; a revision will be distributed to all users of the STC. Revisions will be supplied to the customer by: a) E-mail with an attached PDF file, or b) Compact Disc (CD) via mail Changes to this document will be incorporated by an updated revision to the complete document. All pages will indicate the "new revision level. Upon receipt of the new revision, the previous revision should be discarded and replaced with the updated, current, revision. Changes to this document will be listed in the revision block on page 3. It is the responsibility of the person(s) performing maintenance on the installed system to ensure that this document is current prior to performing this maintenance. The current revision number may be verified by contacting the STC holder, BHE & Associates. Report any discrepancies to the installation of this STC using the form in Appendix C of this document. Once filled out the form must be sent to both the ODA and the STC holder. Their addresses are as follows: ODA VT-ORB Aviation Consultants 9800 John Saunders Rd San Antonio, Texas 78216 STC Holder BHE & Associates Ltd. 12002 Warfield Suite 250 San Antonio, Texas 78216 REPORT No. 584-00-0047, Rev: D BHE 8 Associates, Ltd. Page 5 of 36 Rah By VT-DRS. FSC51 47127. Sht 5 of 39. 2019fhtall 9 SDNY_GM_02754923 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241845 EFTA01326963

Dzoof$Ign Envelope ID: CFB628B5-6FE8-4080•A4E3-5461F992D045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS TABLE OF CONTENTS INTRODUCTION 4 RECORD OF REVISIONS 5 1 SYSTEM DESCRIPTION 8 1.1 GENERAL 8 2 AIRWORTHINESS LIMITATIONS 10 2.1 Inspection intervals 10 2.2 Inspection Program 22 2.3 Inspection Method 22 2.4 Eddy Current Inspection 28 3 MAINTENANCE PRACTICES 29 3.1 Removal/Installation 29 3.2 Access Location 29 4 POWER DISTRIBUTION 30 4.1 Circuit Breakers by Bus 30 5 SYSTEM TROUBLESHOOTING 31 6 INSPECTION REQUIREMENTS 31 6.1 Scheduled Inspections and Maintenance Checks 31 6.2 Wiring 34 Appendix A - List of Applicable Publications Al Appendix B - Special Tools and Equipment B1 Appendix C - Discrepancy Reporting Form Cl REPORT No. 584.00.0047, Rev: 0 BHE & Associates, Ltd. Page 6 of 36 fiord By VT-OR13, FSCM 47M27, SIM 6 of 39, 2019/Mar/IS SDNY_GM_02754924 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241846 EFTA01326964

DoteSign Envelope ID: CR3628115,6FE8-4C8ETME3.5461F9432O04S INSTRUCTIONS FOR CONTINUED AIRWORTHINESS LIST OF FIGURES AND TABLES Table 1: Equipment 4 Table 2 Equipment List 8 Table 3 Equipment by Aircraft 9 Table 4 Inspection Intervals 10 Table 5 Manual List 28 Table 6 Access Panel Location 29 Table 7 Equipment Installation Locations by Aircraft 29 Table 8 New and Upgraded Equipment 30 Table 9 Maintenance Manual by Aircraft 33 REPORT No. 584-00-0047, Rev: D BHE 8. Associates, Ltd. Page 7 of 36 Red By VT-ORB, FSCM 47MI7. Sht 7 of 39. 2019thlar/19 SDNY_GM_02754925 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 I 847 EFTA01326965

DozeSon Envelope ID: CF8132885-6FE8-4C80-A4E3-503IFOBADO4S INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 1 SYSTEM DESCRIPTION 1.1 GENERAL This STC will include installations and/or updates to equipment to allow for Automatic dependent surveillance —broadcast Out (ADS-B Out). ADS-B periodically broadcasts information about each aircraft, such as identification, current position, altitude, and velocity, through an onboard transmitter. The equipment list in Table 2 below details the equipment required for this installation. The TDR-94/94D Transponder(s) will be upgraded to part number 622-9352-502 (94) or 622- 9210-502 (94D), if not previously installed. The TDR-94/94D Transponder is an all solid-state, crystal-controlled receiver/transmitter. The transponder(s) will get the GPS information from either a newly installed Freeflight GPS1203C GPS receiver and dedicated GPS antenna; or, a GPS-40005 GPS receiver. Depending on the aircraft configuration, the GP$-4000/A/S may be previously installed. If the previously installed GPS- 4000/NS is not a part number 822-2189-004/005/006/007/010/011/100 it will have to be upgraded to one of these part numbers. (Reference Tables shown on drawing 584-00-0004 for applicable GPS installation based on aircraft model) Wiring is added dependent on the installed or replaced GPS receiver(s). Transponder(s), and annunciator installed. (Reference Tables shown on drawing 584.00.0004 for applicable installations based on aircraft model and subsequent Wire Routing drawing 584-00-0005).See section 6.1.9 for details on inspection. An optional ADS-B Out annunciator can be installed to alert the pilot that the ADS-B function of the active transponder is not properly functioning. The ADS-B Out annunciator is required for all standalone GPS installations. Standalone means the GPS only provides data to the transponders. All 1203C installations and 4000S installations that only connect to the transponders are standalone. It can be installed as an option for installations where the 4000S is used for both ADS-B and FMS navigation. ((Reference Tables shown on drawing 584-00.0004 for applicable ADS-B Out Annunciator installation based on aircraft model) Table 2 E ui ment List Type Description New CPN Qty DO-260B ADS-B Out TDR-94 Transponder 622-9352-502 0, 1 or 2* TDR-94D Transponder 622.9210.502 0, 1 or 2* GPSI203C GPS Receiver 84327-50-XXXX 0 or 1 CI 429.200 GPS Antenna CI 429.200 0 or 1 GPS-40005 GPS Receiver 822.2189- 004/005/006/007/010/011/100 0, 1 or 2 *Either TDR-94 or TDR-94D will be installed. REPORT No. 584-00-0047. Rev: D BHE 8 Associates. Ltd. Page 8 of 36 Rom By VT-ORB. FSCM 47MZ7, SN 8 of 39. 2019N.1419 SDNY_GM_02754926 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241848 EFTA01326966

()cooSign Envelope ID: CF/352885-6FE84C80-A4E3-9461F9820045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS Table 3 below lists the equipment being installed by aircraft. The aircraft will leave with updated TOR- 94$ or 94Ds depending on the what transponder was already existing. Table 3 E ul ment by Aircraft Aircraft Transponder Installed/Retained/Replaced. GPS Installed/Replaced Antenna Installed Learjet 60 TDR-94s or 94Ds GPS-1203C or GPS- 40005 CI 429-200 Gulfstream Aerospace 1125 Westwind Astra, Astra SPX, Gulfstream 100, G150 TOR-94s or 94Ds GPS-4000S N/A Gulfstream G-1159, G-11598, G-IV, GV TOR-94s or 9413s GPS-1203C or GPS- 40005 CI 429.200 Gulfstream G-11594 TDR-94s or 94Ds GPS-4000S N/A Gulfstream 200 TDR-94s or 94Ds GPS-40005 N/A Textron Aviation 500 TDR-94s or 94Ds GPS- 1203C or GPS- 40005 CI 429-200 Textron Aviation 550, 5550, 560 TOR-94s or 94Ds GPS-1203C or GI'S- 40005 CI 429.200 Textron Aviation 400 TOR-94s or 94Ds GPS-1203C or CPS- 4000S CI 429-200 Textron Aviation 400A TOR-94s or 94Ds GPS-4000S N/A Textron Aviation 650 TOR-94s or 94Ds GPS-1203C or GPS- 4000S CI 429-200 Bombardier CL-600- 1411 CL-600-2Al2, CL- 600.2816 TOR-94s or 94Ds CPS-1203C or CPS- 40005 CI 429.200 Sabreliner NA-265- 65, NA-265-70, NA-265- 80 TDR-94s or 94Ds GPS-4000S N/A Textron Aviation HS.125 700A, BAe.125 800A/800B, Hawker 800XP TOR-94s or 94Ds GPS-1203C or GPS- 40005 CI 429-200 Textron Aviation HS.125 7008, Hawker 750/850XP/900XP TOR-94s or 94Ds GPS-40005 N/A Dassault Aviation Falcon 10, Mystere- Falcon 50, Mystere- Falcon 20- C5/D5/E5/F5, Mystere-Falcon 200, Mystere-Falcon 900 TOR-94s or 94DS GPS-40005 N/A REPORT No. 584-00-0047, Rev: D BHE & Associates, Ltd. Page 9 of 36 Red By VT.DRB. FSCP..1 44127. Slit 9 of 39. 2019rtcladi9 SDNY_GM_02754927 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241849 EFTA01326967

DoomSign Enveleft ID: CFB628B5-6FE8-4C8D-ME3-5461F9620005 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 2 AIRWORTHINESS LIMITATIONS The Airworthiness Limitations section is FAA approved and specifies maintenance required under 14 CFR H43.16 and 91.403 of the Federal Aviation Regulations unless an alternative program has been FAA approved. 2.1 Inspection Intervals The following items require high Frequency Eddie Current inspections including 2.0 inch detailed visual inspection around periphery of the installation. Inspections as listed in the table below. Table 4 Ins ion Intervals Inspection requirements are for AML fuselage modification Inspection In ervals (Flight Cycles) Detectable Crack Length (in.) Threshold Recurring Fwd bulkhead penetrations 4,000 4,000 0.200 GPS Antenna Installation 6,700 6,350 0.200 GPS Antenna Installation (See Note 1) 5,650 5,400 0.200 Note1: These intervals are applicable to the Textron Aviation Cessna 650 and all the Gulfstream Models The following images specify antenna installation and bulkhead feedthrough installation locations. REPORT No. 584-00-0047, Rev: D BHE & Associates, Ltd. Page 10 of 36 Rerd By Vf -ORB. FSCM 47MV. Sol 10 of 39: 2019/Marf19 SDNY_GM_02754928 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 I 850 EFTA01326968

I 58 I ti00-V.L.43 cr) C co H H n -O O n H H 3D C 3D -O 3D 3D -O Vf > • 1 OD LD I— cn P 2lc) co -4 CD— L'S I_a r - 1000O3 , I ,41.3 DocuSign Envelope ID: CFB628135-6FEB-4C8D-A4E3-5461F9820045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS BOMBARDIER INC. CL-600-1A11 (CL-600), -2Al2 (CL-601), -2B16 (CL-601-3A VARIANT, CL-601-3R VARIANT, CL-604 VARIANT) ACC DOABLE LOCATION TS CS OM USW 0t 47115 SAO 5300 55 rs mm no O MO r'S na rs 29100 I 1":* IS r'S a AS AS 4513▪ 0 T REPORT No. 584.00.0047, Rev: D SHE & Associates, Ltd. Page 11 01 36 Reid By VT-ORB. FSCM 471427, Shill al 39. 2019;161mM EFTA01326969

c581 ti:00-V.Ld3 cn C co H H ITI -o 3D H H 3D C 3D-O 3D G.) -O 0 LO cn P 'O im O su -4 g DowSion Envelope ID: CF862885-6FE8-4030-41E3-548iF9821)045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 20.20 TEXTRON AVIATION 400 ACCEPTABLE LOCA11ON IS FS 172.24 196.41 FS FS FS FS FS FS FS 124.61 141 14 71.65 FS 203.35 221.46 240.75 26404 FS FS FS 11734 13747 1503.20 266.1 18 S 4 212.40 231. FS 42 250.39 269.69 Ft I I I FS PRESS WOO I F L js is I 80.91 I 99.02 FS FS 88 96 106.07 :0: 0 hrt , litu REPORT No. 584.00.0047, Rev: D BHE & Associates, Ltd. Page 12 of 36 Red By VT-DRB. FSCM 4714Z7, SIR 12 o139. 2019/Man19 • EFTA01326970

V) DocuSign Envelope ID: CFB62885-SFE8-9C8D-A4E3-5461F9B2D045 C INSTRUCTIONS FOR CONTINUED AIRWORTHINESS £ SS I PZOCV.L43 O3 t. O 73 0 0 70 73 73 73 V) SO lO N p ,G) U E Ca ) O.; lea TEXT -PON AVIATION INC. 550, S550, 560 ACCEPTABLE LOCATION ACCEPTABLE LOCATION FS 59.00 FS FS 151.00 179.02 Fs F5 FS Fs 134.00 165.00 94.00 FWD 117.00 PRESS I BLKHD r _I 1 FS 225.23 23 (560) FS 223.40 , id? , FS 216.10 (560 ONLY) REPORT No. 584-00-0047, Rev: D BHE & Associates, Ltd. Page 13 of 36 Redd By VT-ORB, FSCM 47PAZ7, Ste 13 01 39, 2019/Mar/19 EFTA01326971

V't DaceSoon Envelope ID: CF8628854FE/54C8D-A4E3-5461F902D045 C INSTRUCTIONS FOR CONTINUED AIRWORTHINESS tgi? I ti00-V1-13 co n H ITl -0 0 0 C ITl po -0 po -0 : 3/4400 .93 cn P :4 0_ it, FS 58.00 TEXTRON AVIATION INC. 650 FS 94.00 PRESS 8VHD FS FS 172.00 202.00 FS FS 157.00 187.00 ACCEPTABLE LOCATION FS FS 261.00 288.76 I FS 00 272.00 I i C: 1 0 \ 1 I I i M l il I REPORT No. 584-00-0047, Rev: D ha SHE 8 Associates. Ltd. Page 14 of 36 Red By VT-DRB, FSCM 47M27, Snt 14 of 39. 2019/Mer/19 EFTA01326972

558 I ti:00-V.L.43 C rn H H -o 0 H nr" H rn 0 0 rn 70 -o 7s G) ,z) -o 1) cn P 2 ,G) co cp_ I_a DocuSign Envelope ID: CFB6288543FE8AC8D-A4E3-5461F9B20045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS TEXTRON AVIATION HS.125 SERIES 700A, BAe.125 SERIES 800A & 800B, HAWKER 800XP 67.0 1800 2043 224 • ra MA •I0 11; I Ur 241 Sn • 2822 FICIA ;II ET- (71 1.10 10I0I I I i 1) - 1 I irl n I1 14 n 101.0 two own simony O i l I I I rT 6— r - - 1 - - _Cr REPORT No. 584-00-0047, Rev: D BHE & Acanriates, Ltd. Page 15 of 36 Reid By VT-ORB. FSCM 47MZ7. Sht 15 of 39. 2019/Mar/19 EFTA01326973

cn C co rn H H n -o 7o 0 H rn n H rn 0 31 ci rn 73 -o 73 -o to Co L0 Cn P IC) O CU 958 1 ti00-V.Ld3 33491 DocuSign Envelope ID: CF862885-6FE8-4C8D-A4E3-5461F982OO45 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS LEARJ ET 60 110.99 17 124.39 151.19 17549 20 .79 232.1 2 274.51 302.59 323.5 r3.3 9 305.11 137.79 FIO r 2 99 F144 Fl p.59I209 F-21 I ;23 90 .57 r• F. 144.59 till 1210.19 197.59 F1S 2 r19 246.59 T3INS1 341143 F204 1 r23 rt4 20.39 riI REPORT No. 584-00.0047, Rev: D BHE & Associates, Ltd. Page 16 of 36 Reed By VT-ORB. FSCM 47M27. Sol 16 of 39. 2019iMart19 EFTA01326974

L 58 I ti:00-V1.43 cr) C co n H H ITl 0 H n 0 3D -o 6) -o Vf CO . 1n oz lc) SD -4 ca CD_ ,.(f, I_a FRCSs FS FS 145.0 .0 193.0 133.0 rs 1:10 DowSign Envelope ID: CFB62885-6FE8-403D-A4E3-5461F9B2D045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS GULFSTREAM G-1159, G-1 159B, G-IV ACCEPTABLE LOCATION Fs 63.0 BU010 L —P\ - I I I I t _ _ _LS 1 I I I REPORT No. 584.00-0047. Rev: D BHE 8. Associates. Ltd. Page 17 of 36 Ftefd By \MORD FSCM 47MZ7, Shl 17 of 39, 2019IMart19 EFTA01326975

cn C co H H -to 3D n H IT IT 3D C IT 3D -0 3D -0 Ln 2 3 : D cn oz O co NNAy 858I ti:00-V.Ld3 DocuSion Enveboe ID: CFB62885-6FE8-4C8D-A4E3-5481F9132D045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS GULFSTREAM GV ACCEPTABLE LOCATION FS FS FS FS 157.. S 181.0 205.0 229.0 FS 145.0 1.3.1 I 193.0 217I.0 241.0 FS I FS I FS I FS 63.0 FWD 8U1HO - -Jill T1 n PRESS I _ 1 I 1 1 1 1 1 11 1 1 11 i a .• a =II 1 r- ie a 1 l 'P.41 I I i 100 — a_ 1 II I . I. i i i i 1 I i (:( I I I I I I I I I II II —I--i— 1 _i_ p_ _p_ • i i I I I I I REPORT No. 584-00-0047. Rev: D BHE 8 Associates. Ltd. Page 18 of 36 Reid By 1/7-DRB, FSCM 41M17, SIR 18 of 39.201911Am/19 EFTA01326976

6 g2 I VZOCVJ.d3 (r) C co n H rT -0 0 n H rT H 73 ;a -o 73 Gl 73 -0 I O I-' IE E a E.: DoctiSign Envelops I0: CFB628B5GFE8-4C8D-A4E.95461F9B2D045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS r " .- ri- --- - : T -"- -- , I, I II I I I. I I i I I I ll II / (gggli Ott OO III ( ( OOO t I i -ID,- -144- I Itl--=:- 1 ii n ,, I III I 1 \‘'\ II III I III II /: % N I I I I I I I I i I li • N I II i ii / \t i l! III I I I I I 117 / 1 I I I V / H[L J__ __-- ..- LOOKING AFT AT FWD SIDE OF FORWARD PRESSURE BULKHEAD (TEXTRON AVIATION 400) REPORT No. 584-00-0047, Rev: D BRE & Associates, Ltd. Page 19 o136 Reif By VT-DRB, FSCM 471.427, Sht 19 of 39. 20i9ThAv/I9 EFTA01326977

V) DowSipn Envelope ID: CFB628B5-6FE8-4C8D-A4E3-5461F9E2D045 C INSTRUCTIONS FOR CONTINUED AIRWORTHINESS Co .93 to LOOKING AFT AT FWD SIDE OF FORWARD PRESSURE BULKHEAD ZCI (TEXTRON AVIATION INC. 500, 550, S550, 560) O •- 0 1,1 REPORT No. 584-00-0047, Rev: D I-4 IJ 00 O BHE & Associates, Ltd. Page 20 of 36 Raid By VT-DREI, FSCM 47MZ7, SM 20 of 39, 2019/Marit9 EFTA01326978

I9SIKOCV.L.43 in C L1.0:1 0 0 0 73 0 73 70 70 DD ,93 O 2 0.1 CL it GocuSIgn Envelope ID. CFB62885-6FE8-4C8D-A4E3-5461F9B20045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS CAL1191tOOE WAD* , ay.; , .-r4 .17ir ‘" ,t, tit tel l ti: +. tS -it tj.t 41_ • rir si ti I • • rh " I Tteirh rfi • 4. 4 LI • 0 oi pp , I: 0 j j gMET:EfiftlEF ! I I ' I I I I I le l : I It 4 11\ I I:1 II ;T+4 I: rh 1 44 fprim. -*-174-ditrati- +. 4 41 +. ifolCatshig{q- , , I I III I I I I 2: -1-r= - 0 ‘....thrietiz -- r-- fit ii-711 i+ E-- I I I I LOOKIC SIT AT FOB SEC OF TOIFORD NOM MOEN (LEARJET 60) REPORT No. 584.00.0047, Rev: D BHE & Associates, Ltd. Page 21 of 36 Rohl By VT-DRB, FSCM 47MV. Sht 21 o139, 2019A1ail19 EFTA01326979

DocuSIgn Enveope ID. CFB628B5-6FEB-4C8D-A4E3-5461F962D045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 2.2 Inspection Program Perform additional fuselage modification inspections. 2.3 Inspection Method Inspect fuselage skin in the modification area, doubler fastener holes area, using high frequency eddy current inspection techniques, according to the intervals outlined in table 4. The detectable crack length for eddy current inspection techniques Is 0.200'. For the fastener holes, the inspector should look for cracks on the surface of the skin and doubler around the fastener holes. REPORT No. 584-00-0047, Rev: D BHE & Associates, Ltd. Page 22 of 36 Red By VT-ORB. FSCM 47MZ7.Sht 22 of 39.201917.18:119 SDNY_GM_02754940 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241862 EFTA01326980

DocuSIgn Envelope ID: CFB8288543FES4C80.04E3•5461F9B20045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS LNSPECTION AREA & METHOD FWD BULKHEAD PENETRATIONS typical InstaIlation,shtnvg kspcctions applicable to all PadttatilWiiiitailkiiciai: Ni• "19,4 pcction . NefirdSi Eint lldthiS2t11 411Vtigta l l j cry of installation LiNs. tra alit REPORT No. 584-00-0047. Rev: D SHE & Associates. Ltd. Page 23 of 36 Red By VTCRB, FSCM 47M27, Shl 23 of 39. 2019/M91119 SDNYGtv1_02754941 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241863 EFTA01326981

(locoSago Envelope ID: CF862885-43FE8-4C6D-A4E3-5461F91320045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS INSPECTION AREA & METHOD FWD BULKHEAD PENETRATIONS REPORT No. 584-00-0047. Rev: D BHE 8 Associates. Ltd. Page 24 of 36 Reid By VT.DRB. FSCPA 47MZ7. $01 24 o139. 20194Am/19 SDNY_GM_02754942 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241864 EFTA01326982

DocuSign Envelope III CF13628B5-6FE8-4CBD-A4E3-5461F9432D045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS INSPECTION AREA & METHOD GPS Antenna Typical Installation sbown„Inspections are applicable to all antenna installations REPORT No. 584-00-0047, Rev: 0 BHE & Associates, Ltd. Page 25 of 36 ReRI By VT-ORB. FSCM 47M27. SM 25 of 39. 2019iMarti 9 SDNY_GM_02754943 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241865 EFTA01326983

DocuSogn Envelope ID: CFI362895-6PE8-4C6D-ME3-5461F9620045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS INSPECTION AREA & METHOD GPS ANTENNA Typical InstallatiOnshOlit; Inspections arc applicable to all. antenna installations 1111544 ,ta, "fa Learthiz..4 al. i.ioziqnr- r.-:z REPORT No. 584-00-0047, Rev: D BHE 8 Aqsartates, Ltd. Page 26 of 36 Red By VT-DRB, FSCM 47M/7. She 26 of 39. 20150.ierng SDNY_GM_02754944 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241866 EFTA01326984

FInfogign Envelope ID: CFB62/995-6903-4C8D-A4E3-546199820045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS INSPECTION AREA & METHOD GPS ANTENNA Typical. Installation shown. 100;eetions are 4P01FOle !P. 01 WAAPP1Ps101019FIL ifFcz4R#tioxi:Aita,o-ilmer tit '' . • . '. rA 93-7.!,....E94..._ . Nif ts. rotr., ' T -9,:'' 'z realel_.. :9::. " ~ 4 I ..9.4-# -3.143_. Pat atijt lin g tet0 3 F RICWS4 W i Paa t4 CRIW4 S A4 T J .. ‘ 4 4 arcnlnd . kmia tle.il. .. 4-41 4 1.4L,4,1" ajcyjnia*FipeirIdt, • ygSyt ,t<ti . z...4_,.. Tellie, .1:.! . - - zPrr .rpil*:;-: ' - - ' ..As= a'l. REPORT No. 584-00-0047, Rev: D BHE & Associates, Ltd. Page 27 of 36 Reid By VT-DRB, FSCM 479427. SN 27 of 39. 20191.4aill9 SDNY_GM_02754945 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241867 EFTA01326985

DowSIgn Envelops ID: CF1352193.543FES-4C80-A4E3-546 I F9B2D045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 2.4 Eddy Current Inspection For eddy current inspection requirements and procedures, refer to the referenced documents in the table below for the different aircraft types. The following documents describe the various procedures and requirements for HF eddy current inspection including personnel, instrumentation, equipment setup and standardization, probes, special tools and equipment eddy current standards, and eddy current test procedures required by the Cessna Aircraft Company. The defects identified by this method are incipient fatigue or corrosion stress cracks in bores, machining radii, shoulders and countersunk holes, and in the actual skin. The direction of propagation defects are perpendicular to in-flight stresses in the case of fatigue stress cracks, or perpendicular to internal stresses for stress corrosion cracks. This method also detects minor corrosion-induced surface damage. Table 5 Manual List Aircraft Manual Document Number • Learjet 60 Non-Destructive Inspection Manual NDI-2 (Chapter 3) Textron (Citation) 500,550, S550,560 Series 500 Non-Destructive Testing Manual 5056ND (Part 6, Chapter 20) Textron (Citation) 650 Model 650 Non-Destructive Testing Manual 65ND (Part 6, Chapter 20) Textron (Beechjet) 400, 400A Model 400/400N400XP Maintenance Manual 128-590001-9C29 (Chapter 20-80-03) Textron (Beechcraft) HS.125 700A. Bae.125 800A. Bae.125 8008, Hawker 800XP 125 Series 1-800, Hawker 750, 800, 800XP, 850XP. and 900XP Non-Destructive Testing Manual N/A (General Techniques - Part B) Challengers Structural Repair Manual N/A (Chapter 51) Gulfstream G-1159, 6-11598,6- IV, GV Structural Repair Manual N/A (Chapter 51) Oscars' 91, FAA APPROVED: 405,106FIC36743,- Danyl Seow, Project ODA Administrator VT DRB Aviation Consultants A Division of VT San Antonio Aerospace, Inc. 9800 John Saunders Rd, San Antonio, TX 78216 Date 3/21/2019 Vant SW" I REPORT No. 584-00-0047, Rev: D BHE & Associates, Ltd. Page 28 of 36 ROM By VT.C4iS FSCM 47127. SM 28 of 39. 2019/MaTh9 SDNY_GM_02754946 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241868 EFTA01326986

DowSign Envelope ID: CF9628BS6FE8-4C8D-ME3-9461F9132D045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 3 MAINTENANCE PRACTICES 3.1 Removal/Installation The following installation manuals contain complete, detailed instruction for the installation and removal of equipment. Installation locations for the equipment vary by aircraft, reference tables 6, 7 and 9 for more details on equipment locations and respective maintenance manuals. • Equipment Installation Manual for the FreeFlight System Model 1203C GPS/SBAS Sensor, document 86764, Installation Section • Collins GPS-4000( ) Global Positioning System Installation Manual, document 523-0780545, Installation Section. • TDR-94/94D ATC/Mode-S Transponder System (-5XX), document 523-0821492, Installation Section 3.2 Access Location Refer to the Aircraft Maintenance Manuals listed in table 9 (or additional details. Table 6 Access Panel Location Location of Access Access Panels Nose Avionics Bay Forward Nose Access Panels (Right & Left) Cabin EE Racks N/A Instrument Panel & Pedestal N/A Tail Avionics Bay Tail Access Panel Table 7 Equipment Installation Locations by Aircraft Aircraft Transponder Location GPS Location Learjet 60 Nose Nose (GPS-4000S) Cabin (1203C) Gulfstream Aerospace 1125 Westwind Astra, Astra SPX, Gulfstream 100. 6150 Nose Nose Gulfstream 200 Nose Nose Gulfstream G-1159, G- 1159A, G-11598, G-IV RH EE Rack, Cabin RH EE Rack, Cabin Gulfstream GV LH & RH EE Rack, Cabin LH & RH EE Rack, Cabin Textron Aviation 500, 550, S550, 560 Nose Nose REPORT No. 584-00-0047, Rev: D BHE & Associates, Ltd. Page 29 of 36 Reid By VT-DRS. FSCIA 471.427. Sht 29 of 39. 2019Staf/19 SDNY_GM_02754947 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241869 EFTA01326987

DecoSign Envelope ID: CFB628435-6FE8-4C8D-A4E3-5461F9820045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS Aircraft Transponder Location GPS Location Textron Aviation 400/400A Nose Nose Textron Aviation 650 Aft Cabin Nose (GPS-4000S) Cabin (1203C) Bombardier CL-600-1A11 CL-600-2Al2, CL-600-2816 Under Floor, Cabin Under Floor, Cabin Sabreliner NA-265-65, NA-265.70, NA-265-80 Nose Alternate: FWD EE Shelf Nose Alternate: FWD EE Shelf Textron Aviation HS.125 700A/7006, BAe.125 , 800A/800B, Hawker 750/800XP/850XP/900XP Nose Alternate: AFT EE Shelf Under Floor, Cabin Alternate: AFT EE Shelf Dassault Aviation Falcon 10. Mystere-Falcon 20- 05/D5/E5/F5, Mystere- Falcon 200. Mystere-Falcon 900 Nose Nose Dassault Aviation Mystere- Falcon 50 Nose Nose Alternate: Aft Avionics Shelf 4 POWER DISTRIBUTION 4.1 Circuit Breakers by Bus There are multiple options for the installation, the table below shows the possible equipment part numbers that may have changed with this update and the associated electrical load. The following equipment part numbers may have changed with this update. Table 8 New and Upgraded Equipment Equipment/System Model/Part Number • Max Load in Amps TDR-94 622.9352.502 1.79 TDR-94D 622-9210.502 1.79 GPS RECEIVER GPS1203C 84327-50.XXXX 0.179 GPS RECEIVER GPS-40005 822-2189- 004/005/006/007/010/011/100 0.56 REPORT No. 584-00-0047. Rev: D BHE 8 Associates, Ltd. Page 30 of 36 Read By VT-DRB, FSCM 47M27, Set 30 o139. 2019!Mar/19 SDNY_GM_02754948 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241570 EFTA01326988

DocuSgn Envelope ID: CF862885-6FE8-4C80-A4 E3-546 I F9B2D045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 5 SYSTEM TROUBLESHOOTING For troubleshooting information, refer to the following; Equipment Circuit Breaker Document GPS1203c ADS-B GPS Equipment Installation Manual for the FreeFlight System Model 1203C GPS/SBAS Sensor GPS-4000S ADS-B GPS Collins GPS-40005 Global Positioning System Installation Manual, document 523.0780545, Maintenance Section TDR-94D TDR TDR-94194D ATCIMode-S Transponder System (-5XX). Document Number 523-0821492, Maintenance Section 6 INSPECTION REQUIREMENTS 6.1 Scheduled Inspections and Maintenance Checks This section of the document contains information regarding Time Limits — Inspection and Maintenance Checks, Overhaul and Replacement Items and Inspection Requirements. 6.1.1 Time Limits - Inspection and Maintenance Checks Note: Recommended inspection/maintenance intervals do not guarantee that the item will function properly between inspection/maintenance checks. The inspection intervals are based on average usage and environmental conditions. Aircraft operated under extreme conditions, (extreme hot, extreme cold, high humidity, salty air, etc.) may require more frequent maintenance than the intervals specified in this document. The aircraft operator may perform more frequent inspection/maintenance checks based on his usage. 6.1.2 Visual Inspections The equipment necessary for conducting a visual inspection usually consists of a strong flashlight, a mirror with a ball joint, and a 2.5x — 4x magnifying glasses. A 10x magnifying glass is recommended for positive identification of suspected cracks. 6.1.3 Corrosion Treatment Before attempting a close, visual inspection of any selected part or structural area, it should be checked for signs of corrosion. Any corrosion found should be tested to discover its extent and severity. Heavy or severe corrosion requires immediate corrective action. If mild corrosion is present, it should be carefully, but completely, removed before continuing with preparations for the visual inspection. 6.1.4 Structural Failure Determination. The first step in a visual inspection should be an examination of the area for deformed or missing fasteners. These should be identified for subsequent replacement. A close examination for cracks in the surfaces of structural members should then be made with the aid of a flashlight. The majorities of cracks start at, and progress from, points of concentrated stress such as sharp corner cutouts and fastener holes. Cracks may also occur in sheet metal bend radii and similar places that were subjected to severe forming operations during manufacture. REPORT No. 584-00.0047, Rev: D BHE 8 Associates, Ltd. Page 31 of 36 Reid By VT-DREI, FSCIA 47W7. Shl 31 of 39. 2019iMat/19 SDNY_GM_02754949 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241 I EFTA01326989

DocuSign Envelope ID: CFB62885-6FE8-4C80-A4E3-5461F9920045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 6.1.5 Cleaning of Structural Parts All parts of areas from which mild corrosion has been removed should be thoroughly cleaned using an approved solvent. (Metal conditioner should not be applied at this time as it may interfere with subsequent dye penetrant inspection.) 6.1.6 Cleaning Other Areas All other areas to be inspected should also be cleaned of any deposits that might hinder the discovery of existing surface flaws. The protective finish need not be removed. The cleaning should be performed using any approved solvent. For cleaning high heat-treat steel parts, or areas in which a high heat steel part is installed, use only the approved solvents. 6.1.7 Crack Detection Technique When looking for surface cracks, the inspector should point his flashlight towards himself and hold it at an angle of 5° - 45° to the surface. (See Figure 6) The extent of the crack may be traced by directing the beam at right angles to the crack. Never direct the light beam at such an angle that the reflected beam shines directly into the eyes. The proper procedure is to keep the eyes above the reflected beam. FLASHLIGHT INCIDENT - LIGHT BEAM FAYING SURFACES EYE ABOVE REFLECTED LIGHT BEAM REFLECTED LIGHT BEAM CRACK OPEN TO SURFACE Figure 6 — inspection for Cracks 6.1.8 Verification of cracks A 10x magnifying glass may be used to confirm the existence or extent of a suspected crack. REPORT No. 584-00-0047, Rev: D BHE & Associates, Ltd. Page 32 of 36 Rord By VT.098. FSCM 47MZ7. SM 32 of 39. 2019/Maff 19 SDNY_GM_02754950 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241872 EFTA01326990

DocuSign Envelope ID: CFB628B5-6FES4O9O.AcES5461F962O045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 6.1.9 Visual Wiring Inspection Perform visual inspections of the wiring. These visual inspections should be performed as part of the existing applicable inspection cycles, not to exceed 1200 hours. (Reference Tables shown on drawing 584-00-0004 for applicable installations based on aircraft model and subsequent Wire Routing drawing 584-00-0005) Refer to the pertinent Maintenance Document listed below: Table 9 Maintenance Manual by Aircraft Aircraft TCDS Model Maintenance Manual Learjet 60 60 P/N MM-103 Bombardier Inc CL-600- 1A11 CL-600-1A11 PSP 601-2 Bombardier Inc CL- 6002Al2, CL-6002B16 CL-600-2B12, CL-600- 2816 CL 604 AMM Dassault Aviation Falcon 10 Falcon 10 Dassault Falcon 10 Maintenance Manual Dassault Aviation Mystere-Falcon 20- C5/D5/E5/F5, Mystere Falcon 200 Mystere Falcon 20- C5/D5/E5/F5 Dassault Fan Jet Falcon Maintenance Manual Dassault Aviation Mystere-Falcon 50 Mystere Falcon 50 Dassault Falcon 50/50EX Maintenance Manual Dassault Aviation Mystere-Falcon 900 Mystere Falcon 900 Dassault Falcon 900 Maintenance Manual Galaxy/Gulfstream G100/SPX G100/Astra SPX P/N G100-1001-11-1 Galaxy/Gulfstream 1125 Astra 1125 Astra P/N 25W-1001-11-1 Galaxy/Gulfstream 200, Gulfstream G150 Gulfstream 200, G150 -------- Gulfstream G-1159, G- 1159B G-1159, G-1159B Gulfstream II Maintenance Manual Gulfstream G-1159A G-1159A Gulfstream Ill Maintenance Manual Gulfstream G-IV G-IV Gulfstream IV Aircraft Maintenance Manual Gulfstream GV GV Gulfstream V Aircraft Maintenance Manual Textron (Citation) 500/550/S550 500/550/S550 Model 500 Maintenance Manual REPORT No. 584-00-0047, Rev: D BHE & Associates, Ltd. Page 33 of 36 Res By VT-ORB. FSCAI 47M27. Sht 33 of 39. 2019/Mar/I9 SDNY_GM_02754951 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 I 873 EFTA01326991

DowSkr Envelope ID: CFB62841.543FEB-4C80-ME3-5461F96213045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS Textron (Citation) 560 560 Model 560 Maintenance Manual Textron (Citation) 650 650 Model 650 Maintenance Manual Textron (Beechjet) 400, 400A 400/400A P/N 128-590001-9C Textron (Beechcraft) HS.125 700A, 700B 700A, 700B AFMS-125-700 Textron (Beechcraft) BAe 125 800A. 8008 800A. 800B AFMS-800 Textron (Beechcraft) 750 750 AFMS-800XP Textron (Beechcraft) 800XP 800XP AFMS-800XP Textron (Beechcraft) 850XP 850XP AFMS-800XP Textron (Beechcraft) 900XP 900XP AFMS-800XP Sabreliner Aviation NA-265-70, NA-265-80 NA-265-70, NA-265-80 P/N SE 0405 MM Sabreliner Aviation NA-265-65 NA-265-65 P/N SE 0303 MM A "visual nspection" is defined as the process of using the eye, alone or in conjunction with various aids, as the sensing mechanism from which judgments may be made about the condition of a unit to be inspected. This level of inspection is made from within touching distance unless otherwise specified. A mirror may be necessary to enhance visual access to all exposed surfaces in the inspection area. This level of inspection is made under normally available lighting conditions such as daylight, hangar lighting, flashlight, or droplight. A visual inspection may require the removal or opening of access panels or doors. Stands, ladders, or platforms may be required to gain proximity to the area being checked. The inspection criteria provided below is intended as general guidance. Conduct special inspection as deemed appropriate by each operator based on aircraft experience. Any discrepancies found should be repaired. 6.2 Wiring The inspection criteria provided below is intended as general guidance. Special inspection should be conducted as deemed appropriate by each operator. Any discrepancies found should be repaired. a. WireNVire Bundle — Inspect for: • Aluminum drill shavings, lint or dust on or inside wire bundles. Aluminum shavings can, with vibration or other motion, cut through wire insulation and provide a conductive path between wires in a bundle or to adjacent grounded structure. Lint and dust can accumulate on wire bundles and may, if subjected to overheated wires, ignite or possibly feed an electrical fire. REPORT No. 584-00-0047, Rev: D BHE 8 Associates, Ltd. Page 34 of 36 Red By VT-DRB. FSCM 47IAZ7. Shl 34 of 39. 2019:Mar/19 SDNY_GM_02754952 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241x74 EFTA01326992

DowSign Envelope ID: CF882885.8FE8-4C80•ME3.5481F9820045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS • Wire insulation that has become brittle. Wire may be more susceptible to cracking. Damaged insulation and/or exposed conductor material of wires. Cracked, chafed and cut insulation can provide a conductive path between wires in a bundle or to adjacent grounded structure. • Pinched wires can occur at wire clamps, connector backshell clamps, excessively tight cable ties. etc. • Inappropriate/improper wiring repairs such as the use of duct tape, electrical tape, poor crimp splices, etc. • Wire insulation damage due to fluid leaks (i.e. fuel, hydraulic fluid, etc.) • Separation of electrical wires from hydraulic, fuel and oxygen lines. Ensure a minimum of 0.5-inch separation and any wiring routed within 2.0 inches must be clamped to provide separation. • Small bend radii of wire. Wiring subjected to excessively tight bend radii may sustain damage to the wire insulation. • Sagging wire bundles. Ensure bundles are not allowed to droop onto structure, components, cables, hoses, other bundles, etc. • Wire attached to the outside of a wire bundle using plastic ties instead of being installed under existing wire damps. Can cause chafed and cut wire insulation. • Unsupported wires running into conduit or wire supported in such a way as to pull the wire against the side of the conduit entrance instead of into the center. Can cause chafed and cut wire insulation. • Proximity to high temperature equipment. Wiring shall be kept separate from high temperature equipment, such as resistors, exhaust stacks, heating ducts and deicers, to prevent wire insulation deterioration. • Wires with different insulation types should not be routed together, where possible. Certain wire insulations may be easily abraded by other types of wire insulation. b. Wire Harness Clamps — Inspect for • Condition. Ensure any protective material on the wire clamp (i.e. rubber, plastic, etc.) is in serviceable and functional condition. Clamps should be secured to structure and wire bundle should be snug in clamp. • Ensure clamps are not installed over splices. c. Connectors - Inspect for • Condition. Make sure connectors are free of corrosion, moisture, dust and metal shavings. Check for worn environmental seals, loose contact tension, proper contact locking, missing seal plugs, missing dummy contacts. etc. Drip loops should be maintained when connectors are below the level of the harness and tight bends at connectors should be avoided or corrected. d. Backshells — Inspect for: • Condition: Wires may break at connector backshells due to excessive flexing, lack of strain relief or improper buildup. Loss of backshell bonding may also occur due to these and other factors. REPORT No. 584.00-0047, Rev: D BHE & Associates, Ltd. Page 35 of 36 Rem By VT-ORB. FSCM 47M27. Shl 35 0( 39. 2019/Mar/19 SDNY_GM_02754953 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241875 EFTA01326993

DocuSign Enveiooe ID: CFB628B5-6FE8-4C613-A4E3-5461F9432D545 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS e. Electrical Conduits and Sleeving - Inspect for • Susceptibility to water/moisture entrance: Conduits should not be susceptible to the entrance of moisture. If moisture going into conduits and sleeving is unavoidable, provisions should be made in the lower portions of the conduit to drain any moisture and prevent accumulation. • Condition: Damage to sleeving and conduits, if not corrected, will often lead to wire damage. Make sure components are free from corrosion, moisture, dust, and metal shavings. Check that conduit is secured to structure. f. Terminations — Inspect for • Condition: Terminal lugs and splices are susceptible to mechanical damage, corrosion, heat damage and chemical contamination. The buildup and nut torque on wire lugs is critical to their performance. Grounding Points - Inspect for • Condition: Grounding points should be checked for security (i.e. tightness) condition of termination, cleanliness and corrosion. Any grounding points that have corroded or have lost their protective coating should be repaired and checked for proper resistance. CAUTION Use care when disturbing or removing wire harness/bundles to minimize the possibility of wire insulation damage or cracking. Care must be especially used in areas with severe moisture problems. During any repair, modification, or installation work in close proximity to wire bundles, mounts, connectors and systems, ensure that these areas are protected from and/or cleaned of metal shavings and debris. REPORT No. 564-00-0047, Rev: O BHE & Associates, Ltd. Page 36 of 36 R•I'4 8y VLDRB. FSCM 473AZ7, Sht 36 of 39, 20194A8r/19 SDNY_GM_02754954 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241676 EFTA01326994

DocuSign Envelope ID: CFB828B54FE8-4C80.ME3.5461F9820045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS Appendix A — List of Applicable Publications NOTE: The latest released revision of the publications listed in the LOAP constitutes the required information essential for continued airworthiness for the aircraft. Document TM. Document Numbei Airplane Flight Manual Supplement 584-00-0046 Master Data List (includes wiring diagrams, equipment installations and ground test) 584-00-0001 TDR-941940 ATC/Mode-S Transponder System (-SXX) Install Manual 523-0821492 GPS-4000( ) Global Positioning System Installation Manual 523-0780545 Equipment Installation Manual for the FreeFlight System Model 1203C GPS/SBAS Sensor 86764 REPORT No. 584-00.0047, Rev: D BHE & Associates, Ltd. Page Al of Al Re -O Red By VIFtS. FSCM 471/27. Sht 37 ol 39. 2019nNadt 9 SDNY_GM_02754955 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 I 877 EFTA01326995

DocuSign Envelope ID: CF8628B5-6FE8-4C8D-A4E3-5461FSEQ0O45 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS Appendix B — Special Tools and Equipment Transponders - Aeroflex IFR-6000 or equivalent test set. GPS - JCAir 429 or equivalent 429 Bus Reader GPS - Oscilloscope REPORT No. 584.00.0047, Rev: D BHE 8 Associates, Ltd. Page 81 of 81 Red By VT.DIRD FSCM 47M27, Ste 38 ol 39. 20i9iMar/i9 SDNY_GM_02754956 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 I 878 EFTA01326996

DowSign Envelope la CF882/9354FE8-4C8O-A4E3-5461F982O045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS Appendix C — Discrepancy Reporting Form This form to be used by aircraft owner operators and modification centers to report discrepancies with modifications and repairs approved by the ODA. DATE DISCREPANCY DISCOVERED: Self explanatory. DISCREPANCY: Describe the discrepancy in detail. RECOMMENDED CORRECTIVE ACTION: Describe what actions you recommend faking fo correct the discrepancy. REPORTED BY: COMPANY NAME: PERSON TO NUMBER: Sell explanatory. PHONE CONTACT: TITLE: Signature: Sell explanatory. Date: Self explanatory. Please submit the completed form to the following contact: VT DRB ODA Unit 9800 John Saunders Rd San Antonio, TX 78216 USA Phone: (210) 293-3720 Email: service.su000rtevt-drb.com REPORT No. 584-00-0047, Rev: D SHE & Associates, Ltd. Page Cl of Cl Red By VT-DRS FSCM 471427. Ste 39 of as. 2019thlar/19 SDNY_GM_02754957 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241879 EFTA01326997

SDNY_GM_02754958 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 I 880 EFTA01326998

US Deasvrat MAJOR REPAIR AND ALTERATION a. !teants) (Airframe, Powerplant, Propeller, or Appliance) Fel are Avian Adminisizafte tan Ma. 21 X.0320 Fa SWOON E fistrarIc Tenho MSS FAA Usa0alif INSTRUCTIONS Pmt or type all entries. See Title 14 CFR 543.9. Pal 43 Agana B, aid AC 43.9-1 (or subsequent revision thereof) for InStruCtICOS and clam:salon of MIS form. This report Is required by law (49 U.S.C. 444701). Faits° to moon can result In a col penalty for each such violation. (49 U.S.C. 94630101B 1. Aircraft Nato/way and Registration Mark UNITED STATES / N188TS Senal No. RK-244 'make RAYTHEON AIRCRAFT COMPANY Model 400A Series 2. Chimer ITHORAIR Warne (As shoos o n registration owflAsete) LLC Address (As shown on reghtration certlAcats) mars PO BOX 2218 on SANDUSKY Sae OHIO zo 44871-2218 carer UNITED STATES 3, For FAA Use Only 4. Typo S. Unit Identification Repair nitration Unit Stake Make Model Serial No. 7 n AIRFRAME Aeneas co..huff (As described hi Iron I above) RK.244 POWERPLANT O D PROPELLER K ri APPLIANCE type Namotassaw 6. Conformity Statement A. Agency, Name and Address B. Kind of POORCy Tee Cmistant AdatiCli LLC U. S. Cesislcated Mechanic I Macelaclunu mean 355 RICHMOND ROAD r Foreign Ceraficead Mechanic C. Certificate No. cos CLEVELAND Os Gii Catfrated RepeIrStsfee CRS#WC7R346J es 44143 es„,,„ USA Ceteketed Maintenance Oreantteb:o D. I certify Mal INC repair and/cr alteration made to the IAMB Identified in Wen 5 gave and described on the reverse or attachments hereto have been made In accordance Wth the requirements of Pan 43 of the U.S. Federal Aviation Regulatons and that the Wormation furnished herein h true and coned to the bop, my Eden:sec range fuel per 14 CFR Part 43 AP. B Signs I Steven A. Watkins 10/04/2019 7 apron] for Return To 9erVIC. Pursuant to the authority g' a below, the Lott Idengogg Administrator of the a' Adminkstreg and la VIA:droved in nun 5 nspected in the manner presated by the rejected BY FAA Flt. Standards Impeder Manufacturer Maintenance Organization Palma &graved by CaraMen Departmental Teramxt FM Designee  Repair Staten spectionAuthanoton her Cattalo a Designation No. CRS# WC7R346J Signature/0 AtA ' indMdual _...----:- ---------- David Kerr 10/04/2019 FAA Form 337 (10/06) Page I SDNY_GM_02 754959 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241881 EFTA01326999

NOTICE Weight and balance o r operating amliation (tenses shall be entered in The approplefe aircraft record. Melioration must be compatible with ail previous alterations to assure continued conformity **a the applicable ainvorthiness requirements e. Oescriptkei m Work Accomplished (II more space Li ',puha% attach adaborrei sheets. Identity mat &kalif nations* and registration meet and date salt completed) UNITED STATES /PINTS iettordie NOWAY and ROW: Oboe Merit Date Engine Inlet Rivet Repair Installed blind rivets in place of the damaged solid rivets on the lip of the right hand engine inlet forebody assembly part number 541000-004, serial number R0010, In accordance with nextant aerospace engineering order NT-EO-1118-31 rev IR dated 11129/2018 with FM form 8110-3 dated 11/3012018. Instructions for Continued Airworthiness: Follow the maintenance inspection practices in the aircraft maintenance manual. Inspection intervals shall remain as indicated in the aircraft maintenance manual or operators approved inspection program as appropriate. Weight and Balance unaffected. Reference Constant Aviation work order CCM-3160 END C:DAddilional Sheets Pee Attached FAA Form 337 (10/06) Page 2 SDNY_GM_02754960 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241882 EFTA01327000

WI DIPPATTARIT OF TRANSPORTATION FEDERAL AVIATICNACOMPASTPADM STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS I. DATE November 30, 2018 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. WM Textron Aviation S. SOX I. NO. N541000-004 4. TYPE Mint Era MOAK NM Embody Assy a NAME or APPLICMY Florian Aerospace LLC Cleveland, Ohlo LIST OF DATA I. IDENTOCATION 7 TIRE NTE0•1118-31 Rev. IR November 29, 2018 Engine Inlet Envoi Repair. Notes: 1) The structural aspects only of the above listed data are approved herein. This approval is only for the engineering data. It indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and subparagraph listed below as 'Applicable Requirements.' 2) This form constitutes FAA approval of all the engineering data necessary for substantiation of compliance to necessary requirements for the entire repair. t morose or DATA: Engineering data to support repel procedure for Textron 400A Forebody Assy P/N N541000-004, SIN R0010 under Nextant Aerospace Work Order No.10565.1.1. S. APPLICAEUE REOUREMENTS FAI walk acts) CFR Title 14 Part 25.301(25-23), 25.303(25-23), 25.305(eXb)(c)(25-231, 25.307(eX25-231, 25.601[25-04 25.8030104(c)(25-38), 25.605(aX25-00j, 25.807(25-23), 25.609(aXbX25-00I, 25.811[25-24 25.813(aXb)(c)(25-00). 25.819[25.24 and 25.625(a)(bXcX25.231. M CERTIFICATION . Under whyty vamml by drachm of Me AdmInIstrata and Vi accordance WA conclaIons md Rations of appolmmem under 14 CFR PM MI data IMO alma ad en tithed Meets motored _KUL Moe been examined In Kendra siD estotallm1 procedures and kmdbeemply wit, apalicam reourarims a ma Manion. Manderds Wed El Recommend Mown, of Masa data I(1W) TISMON reA Approve dime data It SKINATUREDDCF OESMNATE0 ENCREERING REPRESENTATNEER 12. DESIGNATION NUMBERS(131 13. a ASSFICATOIES) P rae" .9 • /7.7 t Paul Hedding DERT-410115-CE Structures FM Form 8110-3 (03.101 SUPERSEDES PREVIOUS ED(TX)11 File Number: 1118777.01 Pane 1 of 1 SDNY_GM_02754961 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241883 EFTA01327001

SDNY_GM_02754962 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 I 884 EFTA01327002

fi Sy MAJOR REPAIR AND ALTERATION US D•firrintot of rransponstion (Airframe, Powerplant, Propeller, or Appliance) a nista Miele, Administration am i 2,20 0020 Ent Si3t/20.13 Moran Teinkrio N.insoi For ant Ufa Only INSTRUCTIONS: Print or type all entries. See Tele 14 CFR §43.9. Pan 43 Anaemia B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This capon is required by law (49 U.S.C. §44701). Failure to report can result in a civil penalty for each such violation. (49 U.S.C. §46301(a)) 1. Aircraft Nationality and Registration Mark USNN493LX Serial No. RK-244 Make Raytheon Aircraft Company Model 400A Series 2. owner Name (As shiywn on reoisOstion oertificate) Flight Options Address (As shown on regisrfation certificate) Mavis 26100 Cures, Wnsht PKWY Cry RiChniond Ilitighia SLY OH 20 44143.1453 Catty USA 3. For FAA Use Only 4. Type 5. Unit Identification Repair Alteration Unit Make Model Serial No. O El AIRFRAME ii.............wriem (As described in Item I above) "" O . POWERPLANT O . PROPELLER O • APPLIANCE Typo manufacturer 6. Conformity statement A. Agency's Name and Address B. Kind of Agency -- Na. unantAseepar.• U.S. CeMcated Mechanic f klanutacturet Adam HS Rawohli row Foreign Certificated mechanc C. Certificate No. oh pewees Ox x Centicated Repair Staten CRS# 25NR6678 ;to 11113-14S3 Camay USA Certificated Maintenance Organnaion 0. I certify that the repair andior alteration made to the tine( ) identified in item 5 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Extended range fuel per 14 CFR Part 43 App. B Signature/Date of Authonzed Individual 2.- 1 -1 0/--r .4 7. Approval for Numt ervic -In -_..2(7/ Y P rsuant to the authority g yen persons specified below. the unit identified in item 5 was 'nspeded in the manner prescribed by the A minetrator of the Federal Aviation Administration and S InApproved JDRejected BY FAA Fit. Standards Inspector Manufacturer Maintenance Organization PiaraOnS ArCeOveci by Cartbdian Deparallell of Transccet FM Designee X Repair Station Inspection Autheiftabon Other (Specify) Certificate or Designation No. CRS# 25NR667B Signature/Date of Authorized Individual 7 i 7-A1A? FAA Form 337 (10/06) Page I p5f-o/- 20/ p SDNY_GM_02754963 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241885 EFTA01327003

NOTICE Weight and balance or operating limitation changes shall be entered m the appropriate aircraft record An alteration must be compatible with all previous alterations to assure continued conformity with the appltable airworthiness requirements S. Description of Work Accomplished (If nave space is required attach adationat sheets Identify with aircraft nationally and regatta:ran mark and So work completed) /4193LX Nationality and Registration Mark Date It/2912013 This 337 is amended 01APR2019 to correct a Typo in block 8. Installed New Pitot Probes in accordance with STC ST10959SC. Nextant Master Drawing List Document 373-00-0001 Rev CC EO24-11. Removed Pitot Probes Part Number PH1100-MU-R-1 Removed Pitot Probes Part Number PH1100-MU-L-1 Installed Pitot Probes Part Number PH1100-MUR-EN Serial Number 1975803 Installed Pitot Probes Part Number PH1100-MUL-EN Serial Number 1728401 Leak Check carried ouit Beechcraft Aircraft Maintenance Manual Chapter 34-12-00-201 ICA Continue with Normal Hawker Beech Maintenance Practices for this area. END =Additional Sibeets Are Attached FAA Form 337 (10/06) I'aec 2 SONY_GM_02754964 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241886 EFTA01327004

DEPARWENTOFTRANSPORTATION-FEDERALAVIATIONAMAINISTRATION STANDARD AIRWORTHINESS CERTIFICATE I MATIONAUTY AND 2 MARUFACTURER AND 1•30E1 3 aURCRAFT SERIAL 4 CATEGORY REGISTRATION MARKS Raytheon Aircraft NUMBER N188TS Company 400A RK -244 Transport AUTHORITY APO OASIS FOR ISSUANCE Dm incest. tons 19 imed pew* b49 USG MINA Wank. SK &idly 41% cl aunt the moat myna sam3 Ms Won immelid ell bee m <atm ttm tot tinker twece, bbn cerata tette memo% atm We Own13mM be NO•remb d ft icoxits cenrcamm ref *MIS inereres me.4 amok., MM.= gm to Can, to rooked CeelAestexcome 1:44 New fatten -None- I TERMS AND CONDITIONS llim4 WOW IMM01041.11SMO. *MK SAMaIMM b Ante isloMiNd by A. FM 1m srmetmemetkele is dubs by as nailesomi. motel* mailmemt aY Swim re ',etym.) nAmdamm M21,4 91dt% hand AmpamRatin is *ROOM In all BROOM m MUM'S Pitt /ATE OF ISSUANCE FM REPRESEI4TATIVE DESP3MATION NUMBER $3/06/2014 Arnold Wolfeat Ae GL-25 Mry alstake. wed.. if am deo weak mix patella bp be ad est, $1101 ispbeammail ammtkop mos a Mt 14 CERBRWE WM SE MAYER TEMTOUrt BUCCOMMICE turn NPUCAILE CEOBUL MOON MIAOW. A Rem 1100.2 (0441}Sesedis Pesebus Edam COPY rzoN\ P. atackcr SDNY_GM_0275.O65 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241887 EFTA01327005

Y400 SDNY_GM_02754966 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241858 EFTA01327006

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SDNY_GM_02754968 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241890 EFTA01327008

C U.S.Department Cleveland Fight Standards District Office cr latsportoean 25249 Country Club Blvd North Olmsted, OW 44070 Federal Aviation 440-686-2001. Fax, 440,686-2080 Administration October 9, 2018 Aircraft Registration Branch AFS-750 To whom it may concern: During review of AFS-750 records it was found that a discrepancy existed of the Airworthiness Certificate for N188TS, Make: Raytheon Aircraft Company, Model: 400A, Serial Number RK-244, it was noted that the Airworthiness Certificate registration number did not show the required Nationality letter "N". During inspection of the aircraft it was found that the original Airworthiness Certificate did in fact have the required Nationality letter. Made a copy of the original Airworthiness Certificate and forwarded to AFS-750. If you have any questions in this matter, please contact me at 440-686-2053. Sincerely, Athen J. Neuman. FAA PMI CLE FSDO (440) 686-2053 Office [email protected] SDNY_GM_02754969 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241891 EFTA01327009

SDNY_GM_02754970 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 I 892 EFTA01327010

0 MAJOR REPAIR AND ALTERATION US barna 0 00.3001100., (Airframe. Powerplant. Propeller, or Appliance) reel. Aviation Atislaliplratiell DVS Pea 200.0020 bp SOU2On ewer . Troop.; Nee. sera Osten,. INSTRUCTIONS: Print Or type all 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 a owl penalty for each such violation. (49 U.S.C. §46301(a)) 1. Aircraft Nationally and Registration Mark USA/ N188TS Serial No. RK-244 Make RAYTHEON AIRCRAFT COMPANY Model 400A Series 2.owner Name (As shown on sew:ratan terttfreste) THORAIR LLC Address (As shown on registration certrkate) bras PO BOX Me Oty SAflDUS(V Sate OHIO Z. mamma Celery UWTEDSIAMS 3. For FAA Use Only 4. Type 6. Unit Ident/fleadon Unit Make Model Serial No. Repair Alteralion n Fi i. ass" ft mecomowteepava. (As deserted In Item 1 above) AIRFRAME K POWERPLANT X -- PROPELLER APPLIANCE to. Kanuteaurer 6. Conformity Statement A. Agency's Name and Address B. Kind el Agency Nn Newt A010,01K0 U. S. Connoted Mechanic I Macula:as Ado,. sedoarceenteeNv Fenian Cartecetad Iletharsa C. Cerbacate No. Or/ deified Vas x110 7 Cerbkated Raper Station CRS# WC7R346J De 44143 o w „,,,,, UMW SIMS Cerlikatad laMMOMIPS Organ/Wan O. I certify Mat the repair anctior alteration made to the Lait(s identified in item 5 above and described on the reverse or attachments hereto have been made in accordance with the restatements of Pan 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and cared to the best or my knowledge. Extended range fuel per 14 CFR Part 43 Ape. B K Signatur ate of Authonzed ( - C I nOMdual Chad Graham 10/06/2017 7. rovel for Return to Service idenggiag 5 in the by the Pursuant to the authority g yen persons specified below, the and Administrator of the Federal Aviation Administration and is I i IApproved in den nspected manner prescribed Rejected BY .--- — FM Al. Standards inspector — — Manufacturer Maintenance Organization Panora Approved by Canadian Desennentet Tranesen — ,--- FM Designee — L Repair Station E Inspection Authorization Other apoulY) Certiltat or a ...a ., Designation No. (Alba WC7R346J Signahare/Cat On led Indnadu Steven A. Watkins 10/06/2017 w--.....___ FM Form 337 (10/06) Page I SDNY_GM_O2 754971 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241893 EFTA01327011

NOTICE Weight and balance or operating limitation changes shall be entered in the appropnate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (if more space is remirect attach Saban& sheets Man* Nib Mitre nationally and ritgisfration mark and dere sot completed) USA? HINTS Igebonelly and Pei:peahen Mark Date 1008/2017 STC# ST02371LA Wing let Option Installation Installed Nextant Aerospace Winglets IAW Nextant Aerospace STC# ST2371LA amended date 3/10/2017, Master Data List# MDL-NXT-001 Rev J, dated 2/14/2017, and minor deviations IAW EO# NT-EO-0817-09 Rev A and NT-EO-1017-09 Rev IR. Removed Equipment Item Left Wingtip Assembly Left Strobe/Position Light Assembly Wing Tip Lens Right Wingtp Assembly Right Strobe/Position Light Assembly Wing Tip Lens Tail Strobe Light Tail Position Light Strobe Power Supply Installed Equipment Item Left Winglet Assembly Right Winglet Assembly Left Winglet Light Assembly Right Winglet Light Assembly Tail Strobe Cover Plate Tail Position Cover Plate Part Number 45A10552-001 45A88750-22 8888-170000-01 45A10552-002 45A88750-22 8888-170000-02 4588315-121 45A88754-11 01-790080-00 Part Number NEXT-SA15250LA57-10001 NEXT-SA15250LA57-10002 87-03916-001 87-03917-001 NX0047-3340-0101-001 NX0047-3340-0102-001 Serial Number 00575 Serial Number S-NEXT-0001 S-NEXT-0001 00214 00216 ICA Follow the maintenance inspection practices in the Nextant Aerospace Instructions for Continued Airworthiness Document No. NX0047-ICAO-0101 Rev. A, dated 6/20/2016 or later FAA approved revisions. AFMS FAA Approved Airplane Flight Manual Supplement Document No. NX0047-AFMS-0101 Rev. IR, dated 3/10-2017 or later FAA approved revisions have been added to the Airplane Flight Manual Weight and Balance Reference Weight and Balance Report dated 10/06/2017 END (=Additional seems AM Attached FAA Form 337 (10/06) Page 2 SDNY_GM_02754972 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241594 EFTA01327012

viltb Smut OH ekserrir irpzir burnt of Zraltspur felon - ehrral gittriation ithutinistratinu $upplemental `Type Certificate ..fre;,/ohe ST02371LA gra.. a:v4ear.o.,:vaeark Nextant Aerospace, LLC 355 Richmond Road Richmond Heights, Ohio 14143 eencias dretref4afor E4 kJ! 44.104,40. Ie4Aall067,7,40•14%e Mac deP71444,44 efritlea,SAVIal likelier Ca 4400(10(21/4.00a/13.64, ,(h theelivoeltinow etreeaysowtoN eyegatool 25* 6/64. reeteratfAvaileive Array& . *Certification basis is set forth on TCDS Al6SW and continuation sheets 3 and 4. 9.-fraaitAileme agme. -4-(4/ Al6SW Beechcraft Corporation 400A .94,3 cosi I eao; oo talfeys Zr , Alteration of a Beechcraft Corporation 400A airplane, to replace Pratt & Whitney JT15D-5 series engines with Williams International F344-3AP engines (TCDS E3GL) with Full Authority Digital Engine Control (FADEC) and associated systems (Coatis. A) and (/or) the installation of Nextant Wingless (Config. B), in accordance with Nextant Aerospace Master Drawing List No.: MDL-NXT-001, Revision 1R. dated 8/22/2011, or later FAA approved revisions and the appropriate FAA approved Airplane Flight Manual Supplement(s) for the applicable installed configuration(s): Con& A: NXTI-AFMS, Rev IR, dated September IS, 2011 or later FAA approved revisions Contr.. U: NX0047-AFMS-0101, Rev IR, dated March 10, 2017 or later FAA approved revisions Stilleb4494 end KWh:47414d. The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of that aircraft. The approval of this modification applies to the above-noted airplane models only. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give leo. Other person written evidence of that permission. (CONTINUED on page 3) A , a.-444arl4•awmiet4ienoirreas tethi aide /4 ekratA• grattevidentrarmesa air e ice' arta. ottermeeltreaeokanaiset: eotrAfewetko t lasootettwieto actie dee•Tri4), Ita144 64. tgaigotho3tr000koo ol;34 grit iteriorshOw Owe tairecno• March 24, 2008 September 27, 2011 gluaffnie.wile.. March 10, 2017 • 1 1 (Sigirature) Manager, Propulsion Branch Los Angels Aircraft Certification Office Made ,fry attention if this ("Afton* is pmcnis6a64 byelaw of rot cozotorio Wog or ler& meat oat mooting 3 yostre or bosh Ma lion IMO-MO -de rg.r of . 914 mtge.,: ray fie uaufemiia ottordlout with fir 01.47. SDNY_GM_02754973 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241895 EFTA01327013

SDNY_GM_02754974 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 I 896 EFTA01327014

)triitrb Auntie ail America Prpurhurait of transportation - getter:II ithiartirm Abininintration Supplemtntal ¶gpe Certificate (Qlcmtinuatiuu Afite0 ,M;Padeic ST02371LA Siarackener erearard iii.rdiareeta • Nextant Aerospace, LW, "Installation of Rockwell Collins Pro Line 21," Amended STC ST10959SC, dated September 26, 2011 or later FAA approved revisions is required as pan of this alteration. • The new Vmca and Vmcg values are 94 K1AS and 93 KIAS respectively. • The new engine minimum rated thrust is 3,031 lb at sea level, flat rated to an ambient temperature of 77°F. • Approved engine fuels are: Grade Speeifisaties Jet A ASTM-D 1655 Jet A-I ASTM-D 1655 • FAA accepted revisions of the Nextant Aerospace, LLC Instructions for Continued Airworthiness document must be made available to the operator with the installation of the STC configuration(s). o Coat A: NXT1-ICA, Revision IR, or later FAA accepted revisions. o Confin, B: NX0047-ICAO-0101, Revision A, or later FAA accepted revisions. CriValv.iv• JJvrJnJ The certification basis for this modification is as follows: The original certification basis for the Hawker Beechcraft Model 400A airplanes identified on TCDS AI6SW, Revision 26, dated March 17, 2010: Part 25 of the Federal Aviation Regulations effective February 1. 1965. as amended by 25.1 through 25-40. plus §§ 25.1335, 25.1351(d). 25.1353(c)(5), and 25.1447 of Amendment 25-41: §§ 25.29, 25.255, and 25.1353(c)(6) of Amendment 25.42; and §§ 25.361(6) and 25.1329(h) of Amendment 25-46. Part 36 of the Federal Aviation Regulations effective December 1, 1969, as amended by 36.1 through 36.17; SPAR 27 effective February 1. 1974. as amended by 27-1 through 27-5; and Special Conditions No. 25-ANM-32 dated February 22, 1990 (High Altitude Operation at 45.000 feet), and Special Conditions No. 25-ANM-33 dated June 18, 1990 (Lightning and Radio Frequency Energy Protection). (See NOTE 12) Equivalent Safety Items (I) Out-of-trim characteristics FAR 25.255 (2) Pilot compartment view FAR 25.773(b)(2) (3) Passenger compartment door FAR 25.813(e) (4) Emergency ail marking FAR 25.811(d)(1) and 25.811(d)(2) Application for amended Type Certificate dated February 18, 1988. Any oftertaion of Weis orrtiftarto u nutinia64 Cy a fw of not awing $1,004 or ispironatrer sec qtatallS 3 on or born. MA Pas 01.14.30,0.4•11 "op et • ggir cortifirste say 6s tnissformfin mandato via f Aft.21.4 7. SDNY_GM_02754975 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241597 EFTA01327015

SDNY_GM_02754976 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 I 898 EFTA01327016

Xuittlt 'tales P.uterita gleparhneul of trausportatimr - Actual Ablation Abministration Aupytentental alertificatt (Continuation Alizet) Ireednir ST02371LA g;nce.artan.99O.4, 4.-468sco(/ Regulation at a later amendments for components and areas affected by the change (Ref. FAA approved Compliance Check List): Subpart A - General : 44 25.2(25.99) Subpart B — Flight; 4425.207(25-121), 25.255(25-42) Subpart C — Structure. 44 25.571 (25-96) Subpart D — Design and Construction: 44 25.603(25.46), 25.605(25-46), 25.611(25-123), 25.613(25-112), 25.625(25-72), 25.832(25-72), 25.863(25.46), 25.869(25-123), Subpart E — Powerplant: 44 25.901(25-46), 25.903(25-100), 25.951(25-73), 25.961(25-57), 25.981(25-125), 25.994(25-57), 25.997(25-57), 25.1013(25-72), 25.1019(25.57), 25.1021(25.57), 25.1043(25-42), 25.1045(25-57), 25.1091(25-100), 25,1093(25-72), 25.1103(25-46), 25.1141(25-115), 25.1143(25-57), 25.1163(25-57), 25.1165(25-72), 25.1181(25-115), 25.1183(25-101), 25.1185(25-94),25.1189(25-57), 25.1195(25-46), 25.1203(25-123), 25.1207(25-46). Subpart F — Eauipntenn 4425.1301(25-123), 25.1305(25-115), 25.1307(25.72), 25.1309(25-123), 25.1316(25-80), 25.1317(25-122), 25.1321(25-41), 25.1331(25-41),25.1351(25-72), 25.1353(25-123), 254357(25-123), 25.1381(25-72), 25.1431(25.113), 25.1438(25.41), Subpart G — Operating Limitations and Information; 44 25.1501(25-42), 25.1521(25-72), 25.1527(25-105), 25.1529(25-54), 25.1543(25-72), 25.49(2540), 25.1551(25-72), 25.1557(25-72), 25.1581(25-72), 25.1583(25-105). Subpart H - Electrical Wiring interconnection Systems (EWIS); 44 25.1701(25-123), 25.1703(25.123), 25.1705(25-123), 25.1707(25-123), 25.1709(25-123), 25.1711(25-123), 25.1713(25-123), 25.1715(25-123), 25.1717(25-123), 25.1719(25-123), 25.1721(25-123), 25.1723(25-123), 25.1725(25-123), 25.1727(25-123), 25.1729(25-123), 25.1731(25-123), 25.1733(25.123). 14 CFR Part 34(34-3); 3411 14 CFR Part 36 (36.28): 36.1-36.7, 36.101-36.105, 36.15D1, 36.1581. The following Nextant Aerospace Continued Airworthiness Supplements are applicable to airplanes modified in accordance with this STC: • Master Minimum Equipment List document No. MMEL Rev. 8, dated 02/21/2011 or later FAA approved revisions. • EWIS (Electrical Wiring Interconnection Systems) Inspection Procedure/Report No. NXTI-EA-007 Rev A dated 8/24/11 or later FAA approved revisions. lay thorn:ion of this ratifies:a u punishable 6y n foot of not met:fats $1,000, or Imprisonment sot waling 5 yin or boot not. rem 11110-200.40 pogo 4 or • Ili; certificate /1416. tram/erred ocoortfoors nog CAR.21.47. SDNY_GM_02754977 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241899 EFTA01327017

SDNY_GM_02754978 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 1900 EFTA01327018

0 MAJOR REPAIR AND ALTERATION 1S Onsaint to (Airframe, Powerplant, Propeller, or Appliance invirssunin 'KS Aviation Adeaffila,004 ram Append Ow No v20-ccoo Noon= Electroric Tracking NurDer For FAA Use Only INSTRUCTIONS PAM or type al ones. See FAR 43.9, FM 43 Append& 8, and AC 43.9-I (or subsettuent revision thereof) for instructions and disposition ol this form. TNs repot is Waal by taw (49 U.S C 1421) Failure lo report can Molt howl penalty not to maid $1.000 la each such Notation (Section 901 Federal Aviation Ad 1959) I. Aircraft Natonalty and ReDstraton Mark N493LX Serail No. RK 244 Make Raytheon Aircraft Company Model 400A Senn 2. Ovmet Name (As sham on nmsfration comet:de) Flight Options .LLC Address (As sherds on reddration certsfitted Am.,. 26180 Curtiss Wriaht PKWY CO). Richmond Hetanta sate OH La 44143-1453 Coaltv USA 3. For FM Use Only 4. Type S. unn mentification Repair Moreton Unit Make MOON WM Mantel 0 0 AIRFRAME (As dncnbed in Rem I above) 0 O POWERPLANT 0 Ei PROPELLER • O APPLIANCE Type manzeauw & Conformity Statement A. Agency's Name and Address B Kim or Agency Now Constant Aviation Adam 355 Richmond Road can Cleveland ass OH 2p 44143-1453 Canty USA O USCerbficated Mena/Ain O ManutaCturef O Foreign Generated Mechanic C. Ceases No. 0 Certificated Ryas Station CRS # WC7R346J O Certificated MaiMenance Organization 0 Imlay Mat the repair ancitor alteration made to the urn(s) Identified in item 5 atom and detrained on the reverse ot attachments hereto have teen made in accordance ash the requirements of Pan 43 of the U S. Federal Aviation Regulations arid that the information (limn/had herein is the arid correct to the best of my ki Extended range fuel pee 14 CFR Part 43 App. 8 0 SonalureJOMe or Authorized land Waal ISI f OWSep/2017 7. Approval tar Return to Service Pursuant lo the authority given persons specified below. Me unt idensEed in item S was inspected in the manner prescribed by the Admintstrator of to Federal mann Adinamaratan and N 0 Anstovso 0 REJECTED BY FM FR Standen% Inspector Manufacturer Manufacturer Maintenance CrsersizatiOn Person Approved by Canadian of Transport FM De ghee X Ream Swoon inspeceon Aflizabon Other (Smolt/ Cattalo or Designation No WC7R346J Signature/Da aka:1.0,4nd InSvclual • 09/Sep/2017 FAA Form 337 paw SDNY_GM_O2754979 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241901 EFTA01327019

NOTICE Weight and balance a operating halnahOrt changes Shia be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued contomMy with the applicable ainvorthiness requirements. 8. Description of Work Accomplished (It more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed) N493LX Nationality and Registration Mark 12/Sep/2017 Date This is a revised FAA 337 to correct the Serial Numbers of the Engines that were installed by Nextant Aerospace CRS # 25NR667B on FAA 337 Dated 05/30/2013 Nextant Aerospace Completed STC # ST02371LA Removed Pratt and Whitney JT15D-S Series Engines. Installed the Williams International F144-3AP Engines with Full FADEC and Associated Systems in accordance with Nextant Aerospace MDL -NXT-001 Rev IR Dated 08/22/2011 or later FAA approved revisions, and FAA Approved AFM Supplement NXT-1-AFMS Rev IR dated 9/15/2011 of later FAA Approved revisions. Installed Left Engine Part Number. 111000-202 Serial No. 252767 Installed Right Engine Part Number 111000-202 Serial No. 252768 ICA AFM Supplement was installed on Aircraft. Nextant Aerospace Instructions for Continued Airworthiness Document NXT-ICA Rev IR or later FAA accepted revisions are included in the Aircraft Maintenance Records. Carried out Engine Ground Runs and System 0PS checks IAW Ground Test Plan 373-00-0024 Rev F. End Id Additional Sheets Are Attached FAA Form 337 (10-C6) SDNY_GM_02754980 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241902 EFTA01327020

umnovantaMetCA OEPHITMENT OF TRAKSPORT41101.FECEPAl AVIATION 0/010TRATION • • STANDARD AIRWORTHINESS CERTIFICATE liCOWJIV Ye I ...masa( tarn mt.-Val I .a•cwt *My a Canteara 41CISMAIW"..3 Raytheon Aircraft 18813 Canpany 4COA • Aralarrs160.414,4/1Coanal..( Faalaw••••••• ..•••••,...... I' Oa. wry /sin Oa mat aka add MOW •14.1•1•1 ••••• teatlatanallotalfa•la. fa am. f a woo Po allallasalenStaimaliaeok •ffdli II ell COMV•Pli. gr•Pli atom RK-244 Transport I ad MO coronas San , WM.. IMMO. •••••3 man lill•S•0014011•144.10••••••••• ▪ alliMas lamas ._. PIAIMemien Wasilmaroslan. malmadbalnalk 0of tegifliamiSes Calal 00 *WC tilienAlen NASA 0.3/06/2014 Arnold Wolfe carn .......•OnnaleilInntaikaameg inialelmnairgerasSe pilitea INCOITCASIOSIC DOWIT la al SataMa ••= 8:0•Cl Val late! ROM 00.0:5140.4100 hnT c'YIa ,, . ...."..b"" SDNY_GOA 02754981 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00241903 EFTA01327021

SDNY_GM_02754982 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 00241904 EFTA01327022

trCIOMISO. ANIMA CEPIRTVIENT Or MANSPCMATION.F MEWL AVIATON ADIAINISTPATION • STANDARD AIRWORTHINESS CERTIFICATE sedmarnit 4 .....DttnA 0-0 vita I AMOT fa* • CAROM a." 3" .." Raytheon Aircraft re1 11493LX C:ICompany 400A R 44 ransport uNINNA•14.1. ••••pell et it SOOMISISIN. ad Ss. wank •••••Illt • 4 11•••••••••••011011•1•NIMISIMIS Ma••••••• snit wear O110• 4•11nikrOlillaipPkiliamemOmMt••••••••••••••110.1 110.0 4•NnieulaitO•••••••••iimaSin IRS *NOnti• • sa stsiongeet said ...Willie...I invenitataa•••.fra e• Saw MS, gar snag N. Rae. ••••••••• ••••••••••Wel. It ell II ill. lan••• kiln, wil• 03/06/2014 Arthur Ockwell 1 I DARTS 339 4 IG: Pit *A.I.MIL ist Maisallyi %MO IIMIMIPPS • ••••41:4•Vtt „Or= ===r n. SDNY_GM_02 754983 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 00241905 EFTA01327023

SONY_GM_02754984 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 00241906 EFTA01327024

4/10/2014 Flight Standards District Office Great Northern Tech Bldg. II 25249 Country Club Blvd. North Olmstead, Ohio 44070 Cleveland Flight Standards District Office: ThorAir LLC. would like to request a new airworthiness certificate for Serial number RK-244, Raytheon Aircraft Company 400A. The reason for requiring an airworthiness certificate change is a new registration number is being placed on the aircraft. Included with this letter is AC Forum 8050.64 issue date Apr 03, 2014 showing the change in registration number from N493LX to N188TS. Signature of Owner: Title of Owner: President of ThorSport, Inc., ThorAir, LLC. It's Member SDNY_GM_02754985 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241907 EFTA01327025

SIDNY_GM02754986 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241908 EFTA01327026

FAA FORM 8130-6, APPLICATION FOR U.S. AIRWORTHINESS CERTIFICATE FONT AWOMONI OM O. No. 21204015 Fapimian DOW 02228/2013 0 APPLICATION FOR LIS OeNrIMAI U.S. AIRWORTHINESS orNammteben Faleal A.I•Ilon CERTIFICATE A/Mmunlion INSTRUCTOONS • PrAmon)90. DO rat wills In sno0•1 sew t.,. woe FAA mI4 MN SANT, 6•60 40; Oar le oft sulhalle1FAA RACOMAINIrtt N sikklovl Wows mound. msonschAwIl Ftie &pedal Nolv pones Ample, Socha I. N. and VII es ocolcale L AIROtAFT ousoupnow I AMSTRAD:IN MARK N493LX 2 AIRCRAFT BOXERS NAME Rua Raytheon Aircraft Co 3 AIRCRAFT IACJOEL DESIGNATION 400A 4. YR MFR. 1999 FM COD NG S ARCRAFT SERIAL NO. RK-244 6 ENDRE WADERS NAME plow Williams Intemational 7. OGRE /ACOEL DESIGNATION FJ44-3AP 9 KAMER OF INGRES 2 9 PROPELLER WADERS MK me, N/A W. PROPOSER 1100EL OFFIGNATION II. AIRCRAFT 6 rim dowoutt NIA I MAORI P !3 ; g R V t a S ARAM...TON IS HERM MACE VCR p.ss roses* Assl I A I .1 STAIOAROAWACRTHNESS CERT/MATE Omamewmf 1 1 5.55+ i 1.40" I I acsay I (hassle i I eosin' I 1•W0,' I 1 PAD a SPECIAL NRAORGINEES CERTIFICATE Os emwoN 'NW 7 PRIMARY 9 LIGHT I I MS* I 1 PoseAPanchvia I I valp-955Custi I I Sew I I At 2 -SPORT ...mar UNITED ran S PROVISIONAL d I CUS i pms. m/ 2 35 • CUS I MORCIATIAE MOPES! WAWA 2 Nam. SURVEY 1 WEAL AOYERTERNO 3 RESTRICTED eN mops eraufe 4 FCREST amok N3 PATROLU 5 %%RATHER CCHTROL pie RON) 0 fares.; ODER MAW I RESEARCH ANDOEVELOFIENT 2 AMATEUR MALT 3I 6304EITICA4 • AIR RACING 5 DEW MOOG 6 NAFMET SURVEY 0 TO WOW CCMPLIANCE WITH DE CFR 7 OPERATING PIANDOWWN MT SALT AIRCRAFT EXPERIMENTAL M OdolrumnINAT.M an marnows anion 4 Mow me4I 9 I03.1 4 Miss •••••00/ a* co.Scle. 0 OPERATING II3 OvensaNUOIScal Kean LIGHT-SPORT SC OWEN "MOM MA 93W* MAXI IWICIO ROMPPI MO9Ory 9.wworm4 calks& Labe 5 21.' • UNMANNED OA RESIAROI MD CEMELCONIENT I IC i [CREW TRAINING ARCRAFT te MARKET SURVEY 1 FERRY FLIGHT FOR REHIRE N.TERATICNE IMMTENNICE. OR STORAGE SPECIAL FLIGHT PERMIT MONO 2 EVACUATE IRCIA AREA CV RAPEICING DANGER a or04 CO•Mist 11,44 OS a. rano:am S mil 3 OPERAT Cod IN EXCESS OF MAXIMUM CERTIFICATED TAKEOFF WOW! • MARINO OR EXPORTS] i 9 1 . I PRODUCTION NOR TEEMS 6 CUSTOMER 00A3MYRATION FUMES ci 6 WA ME AIRWORTAMESS aRTWICATE tOve SW *bar e °prawn tees tileatalegiaMal M. OMER'S CEA TIT ICATIOM A REOSTERED OWNER 04 ~An mom issammtam IF MAUR POCK NERIS- • I i NAME ThorAir LLC ACCRUE PO Box 2218, Sandusky. OH 448/1 ARCM,' CERTIRCATADN BADS M•P IMAM NNW essmwor ten. b* AIRCRAFT sseCSICANCea CR TYPE CERTIFICATE DATA WEFT town. m I gess./ • i A18SW Rev 26 1 AiRwORTM Ness DRECTNESICANIOMMMIMOI •••••••••••••••••••••••••• ~an 0 !WS° a wawa. Ise •.*** ow • • a II ens tlegialso Bi Weekly 2014 2/10/2014 - 07/23/2014 AIRCRAFT USTM3 Km Pe Im/IPM N/A SUPPLEST& TYPE CERTIACATE me /ewes ems ETC See Attached Sheet C AIRCRAFT OPERATON NO IINNIVAICE RECORDS CHECK IF MOCKS IN 1 U cououracevam 0 M sociwoO 4 TOTAL AIRFRAME MAWS 8816.1 TTAF 3 EXPERIMENTAL CM, itanoa bon Sas I a lainedadDlini ...NM N/A 0. Clanne5n 5NN• I MY, / oar/ 1700 I 4.6 lososans en Thy to e vs I.$5 NNI Seem n-1/MIS cswa nailed DADDOWOROMO NINE Awn° of FR haS eiscrees mow ow ow non Cob NAM Ells Ned Mite* F•Seml AMROI ROMPONI. and OM Do is mond Am VS own man Aemvsnom v. NUM Ms Wm niptoso AMR /MTh RN EOM 92/ DATE OF APPLICADCA: 03/06/2014 NAVE AND mu ••••• MN Anton Kcarivnik Agent SIGNATungtc.. .0.1,z I § I i 1 i A OE ARCRAFT DESCRIBED ABOVE KM OF EN INSPECTED NO FOUND NRW3RMY BY: grump. rm. 5v, a cams P. Pad 1 "cm fr , '?' Conr an racer may CERTOICATEOAIECAMIC RNA UMW, AM 3 i I 6 CERTIFICATED REPAOSTION //vn comm. -I 5 AIRCRAFT MUNI AMMER IN,.. mob.. DATE TILE SIGNATURE V. MA REPRESENTATVE CERMICATION Osamtargasmosi 4 /411 el i NE CERTIFICATE nova Teo A I Ito ow re atm* butted P Swami M Wiesen imams la 4 AMENDMENT CR NOCIFKATICN OF CURRENT MMORIWNESS CERTMCATE B. inglocia, to VINS5VOWNIN ARAM SKIS' NI RN ONONININ FM DEFECTOR FM nourusE CERTIFICATE MIXER LACER m CFR pal 66 I J 14 06401121Cit OS I I 14CFR PIN IM OATS 03/08/2014 AUCOC*300 CFFICE GL-25 4 FM SA =COI A Odovell 3 1 r TYRE REVIEW , OART833943Cal. a k • • E AST FM Fan elan (4/11)A4 Promos Comm Sulermwo EYLMOncF -PDF RECE MAR 1 U 2014 CLE-021. SDNY_GM_02 754987 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 0 0 a EFTA_0024I909 EFTA01327027

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ThorAir March 3, 2014 ThorAir, LLC. PO. Sox 2218 Sandusky, Oh Re: RK 244 - Agent Authorization To whom it may concern: This letter is to confirm that ThorAir, LLC, authorizes Nextant Aerospace, LLC, as ThorAir's agent for a Beechjet 400A, bearing serial number RK-244 and FAA Registration number N493LX, which is owned by ThorAir, liC., and operated by ThorSport, Inc., for any and all authorized FAA actions needed. Sincerely, ThorAir, LC By: Mci\ sZ/N\Y ZS 1-1\\AQ ° A 9 Notary's Official Signature Sworn and subscribed to me this dayaof VC\ ON O\ 2014 btyk -,\NAt -AX:f-C.A) ThorAir • P.O. Box 2218 • Sandusky, Ohio 44870 Phone: (419) 621.8800 • Toll Free: (888) 394.7325 ThorAfr SDNY_GM_02754993 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241915 EFTA01327033

SDNY_GM_02754994 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 19 16 EFTA01327034

R K-244 STC list (03/05/2014) Reference 8130-6: Application for Standard Airworthiness Certificate Transport Category, dated March 6, 2014 Reference section III owners certification ST02371LA: Replacement of Pratt & Whitney JT15D-5 series engine with Williams International FJ44-3AP engine (TCDS E3GL) with Full Authority Digital Engine Control (FADEC) and associated systems. ST10959SC: Installation of Rockwell Collins Pro Line 21 Electronic Flight Instrument System (EFIS) with Rockwell Collins FMS-6100, Localizer Performance with Vertical Guidance (LPV) approach capability and Universal Avionics System Company (UASC) Terrain Awareness Warning System (TAWS) ST03960AT: Installation of Aircell Axxess Cabin II Iridium Phone and High Speed Internet System with Wireless Local Area Network (WLAN), Astronics 115VAC 60Hz Cabin Inverter and Bonner LED Cabin Lighting System. ST01572WI: Installation of four (4) model 400A OEM seats, one (1) three-place divan, one (1) aft toilet, one (1) set of aft pocket door dividers, one (1) set of forward pocket door dividers and LED lighting. STC01794LA: Installation of Hawker 97650W0370 or 9750W0370-8 battery ST000812SE: Group airplane approval for Reduced Vertical Separation Minimum — (RVSM) SDNY_GM_02754995 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241917 EFTA01327035

SDNY GM 02754996 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 19 I 8 EFTA01327036

EFTA01327037

SDNY GM 02754998 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241920 EFTA01327038

SDNY GM 02754999 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241921 EFTA01327039

SDNY GM 02755000 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024I922 EFTA01327040

SDNY_GM_02755001 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241923 EFTA01327041

SDNY GM 02755002 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241924 EFTA01327042