FAA FORM 8130-6, APPLICATION FOR U.S. AIRWORTHINESS CERTIFICATE Form Approved 0 NA B. No. 2120-0018 0 APPLICATION FOR U S Omellial U.S. AIRWORTHINESS of TonsporliNen Festal MISR CERTIFICATE Aassberollon INSTRUCTIONS - PSI or IsTe. Do nce wile on shaded areas: Mow ate W FM woolly. SOW, ofOrill ref 10 en 444hanzed FM Representative II addional VW It MONfed. WO ellachmeN For SPOON MON Wrote 00TOINe Seaon II. A. and NI as applicable. r... § * o. 22 I REGISTRATION MARK N493LX 2 AIRCRAFT (WADERS NAME Wow Raytheon Aircraft Co 3. AIRCRAFT MODEL DESIGNATION 400A 4. YR /OR 1999 FM COOING $ AIRCRAFT SERIAL NO. RK-244 6 EROTIC BUILDERS NAME way Williams International 7 ENGiNE MODEL DESIGNATION FJ44-3AP S MUSSER OF ENGINES 2 9 PROPELLER GUILDERS NAME PAN N/A ICI. PROPELLERMOM GESIGOLATION s I AR CRAFT IS rtme. 4 A i N/A WORT o Vs C Si cc Li 4, APPLICATOR IS HERESY MADE FOR !Chid mitaliki• SU I A I I STAROAR0 AMYARTMNIESS CERTIFICATE passneasown I I I I vni u I Hama ', III `AN., " I I " A ' I I s oom 1 I ..'" (I SPEWS. AMWORTHNESSCERWICATE /0•••••••••• Nan 7 PRITmRY 9 LIGHT-SPORT I I Arran. I I PowrasseNA• I I LWAri-Shill.Conaol I I GOF I 2 E.4....o.. LIIIITE0 art M 5 PROVISIONAL maws SU I CLASS, 2 CLASSY I AORCULTURE AND PEST CONTROL 2 AERIAL SURVEY 3 AZ NAL ADVERTISING 3 A le =nay.. faemsepral140, 4 FOREST M a Rea** $ PATROLLNG 6 MATTER CONTROL 0 OTHER !swam I RESEARCH ANO DEVELOPMENT 2 AMATEUR SUIT 3 OGISITION 4 AR RACING 5 CREW TRANING 6 I MARKET SURVEY 0 TO SACAVGONPUNICE NTH THE CFR 7 OPERATING Mawr Carasor NT CULT NRCRAFT EXPER MENTAL IA &Mho einnAwAho-e en anclitness ortice.e t Oa MAHN $ 1011 . ..........o....ye am oaldtaIO $ OPERATING a Ocersdra LepaSoarl Kilda, ueirr-socat ric OIFIR4V9 IFORCei PWCUSI4 Wild CMS RIVRPOrl Magary ahcoviness ceNleslovieW$ 2t.ITO 9 UNLIAMED 9A RESEARCH MID DEVELOPMENT I 9C I I CREW TRAINING AIRCRAFT 56 WARM' SURVEY I FERRY FLIGHT FOR REPAIRS. ALTERATIONS. MAPRENANCE OR STORAGE SPECIAL FLIGHT PERMIT memo 2 EVACUATE FROM AREA Of IMPENONG RANGER S Apnea* a OA emateld Pon Oarial• FRIORA.4 IR al •404$01. RIR 3 OPERATION IN EXCESS CF IMALIUM CERTIFICATED TAKEOFF MIGHT • DELIVERING OR EXPORT/4G 1 5 I I PRODUCTION FLOW TESTING 6 CUSTOMER DEMONSTRATION FLOGS CI 6 MULTIPLE AIRWORTHINESS CERTIFICATE Kama moon Nmemeceam... Parbovilenre Wet a • WRY.) O 8 14. lcis u a kr A REGISTERED OMAR Ms ewe semnessionna mos, FORAMCHIC% HERE- 0 I NAME F ight Options LLC ADORERS 28180 Curtis Wright Parkway. Richmond Heights .OH 44143 B. AIRCRAFT CFR T IF CAT ION OASIS (ORA •00444.0 14104 .49 MVO* IS 00 ARON* AIRCRAFT SPEGFICATION OR TYPE CERTFCATE DATA SHEET /ow re .0 i Avrenne) A16SW Rev 28 I NAWCRTHINESS DRECTIVES Nr••• vas arker•Aa. on otapar re gon eronentee sem bit AO $VPASIENT neat* At. OWINI WY anions* if appiner. Bi Weekly 2013-25 12/02/2013 - 12/15/2013 AMAMI LISTOIO 0.1.0Salealt N/A I SuPPLEMENIAL TYPE CLAWCATE Am ame s.* srchaemmem) See attached sheet C AIRCRAFT OPERATION AND MAINTENANCE RECORDS CHECK F RECORDS IN WTH I G A OMP CFR LLANC N E ateP AU I I TOTµ MRFRAME HOURS TTAF 8581.43 3 EAPERMENTµ ONLY oror.ors dem snap row NoVoser mon 04444441 , 2.81 0 CERTIFICATION dwelt/ easy ral I 8 403.00. ROI To. 43 44 R4 URI44 SRNS atrevainaleanioao wowed wow Mn Ivo ncsesceol oars (a Ns nem) of re emaek deSCADed to.. MN to *welt CAM 44MI tag ird Sab* Federal AR011ori I4494sbou. moths ma sacra 4 regs•el war Po AFARS Melia, Acenwuraca in Ma porn Anoeded to 4 IkrwrAPry Fa el ode Re she APPLICATION DATE OF APP 12/29/2013 LAME MD TITLE (Ana,...) Anton J. Koprivnik Agent SIGNATURE by )1„, a igi S I 6 A. TIC NRCRAFT ()ESCROW MOVE HASSEEN NSPEGTE0 AND FOUND NRWORTRY BY coma ea semen, yr om awn. Icy "sou 2 HI CFR zt ) 121 CERTIFICATE HOLDER 11, \ • 3 CERTIFCATED TECHNIC ANeas etarlai 5 I CERTIFICATED REPAIR STA Rao Geo. PO) AIRCRAFT MONUFACTURER Chose saw/ DATE TITLE SIGNATURE < i g s Mani aersma oinfraw4 A *MN I THE MITIGATE REOUESTEO A IRO Mel as ANSI booted h Samos i or Vii rads IVIVIVIIWII RR 4 MIENDMENT OR mODFICATION OF CURRENT NRWORTNINESS CERTIFICATE S 916040101 IN • Rhoaal WI Dame Leder SWAN VII an comk40•3 Di. FM INSPECTOR FM DESIGNEE CERTIFCATE MOLDER UNCER RACER No 65 I 'M CFR pal IV OR OS I !IA CFR pen 145 DATE 12/29/2013 16000500 OFFICE CLE-25 F FAA INSPECTORS SIGMA SIGNATURE AND NO Arthur•Ockwell DART83.3943GL • 015 1 t i\ 1 F CTOR TION REVIEW S HA E ED lb 1.• LUW AC- 3/304ru11)AJPhWoi4 ENans SuC*SONNI EleeVorse Fermi -PDF 2 SDNY_GM_02755003 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 n 3 a 0 3 O 0 EFTA_00241925 EFTA01327043

SDNYGM02755004 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241926 EFTA01327044

K 'ROOK-nom FLIGHT itSnNO A MAILIFACTURER NAME ADDRESS 8 PRODUCTION BASIS (CNKS•04•01• AWN PROCUCT KM CERTIFICATE (Gm. peckcata catiftdos twits) TYPE CERTFICATE OTHER C. GNE OUMITITY OF CERTIFICATES REQUIRED FOR CPERATIM NEEDS DATE OF APPLICATION IMAM MO ne PAM a OFF) SIGNATURE H t o i V 5 P i 0 I 1 g I t t I I I A OESCRP TC/N OF AIRCRAFT REGISTERED OMER ADDRESS BULGER MODEL TAMM SERIAL NUMBER REGISTRATION MARK 8 DESCRIPTION OF FLIGHT CUSTOMER DEMONSTRATION FLIGHTS 0 (GINce /appestat) FROM TO MA CEPARTURE DATE DURATION C CREW REQUITED TO OPERATE THE AIRCRAFT NC ITS EOUPMENT I I PROT I I CO-PILOT I I FLIGHT ENGINEER I I OTHER (Stec*) THE AIRCRAFT GOES NOT /MET THE APPLICABLE AIRNORTHINESS REQUIREMENTS AS FOL LONG. E. THE FC4.1.0WIM RESTRICTIONS ARE CONSIDEREDNECESSARY FOR SAFE OPERATION (Use Maammal ihmeisse00 F CERTIFICATION- I herite oewy 'hell in tie regstered yew lot Ns apse) cd 04.resnoca nocooreence wet Tile 49 et the Unto] Dais Cole44101ns are isle teethe/Ire Pleated to oteeiteemileed abHe.the Its matt is registered win OM F•cl•relkvikoct FASO MAMA RegAmene. enrol Ms Om applleatei were the impeded AM ni GATE NAME AND TITLE (Palls ME SIGNATURE z I i e 1 E li ... g ar § i P. Ope• en, LII•Ulare aryl Mariam. n Domonce MN 14 CFR Seam 91 S. As AWLesbie G Stammered Conionney. FM Fan 8133-9 MRCP ofiefONAM0 H. rotor Alownhans Corthaan Ice linpri Altaall WI Sam legume) (# ad El CANON Omen, LeHalsze Mated 1 C DMA ONIRPOIL IFIKNOMM. eta (Mach Moe rented) 1 PreHme Aft*ITW011 Celicilt• loved n Ace:atria Win i4 CFR Realm 21.191 (a) cm IGATMAMICAM 1 0. Camel WADY end gatirce IrtanaboulmeetienAtaeli 1 /Map RES vd Atmekal. FM Fan 33T (MOM Men Amme) 1 J Drool Are:Moen Comma Issued c Moyearce VAT g id cm s law, 21.181 (a) Jeavyannfro 1 F TM niceceol Recerclia HAMM Ftezeds K tgle-SWI Anise 510~ 110 Germaine. FM Font 813045 (Mad% ..San Mtlia0) FAA Finn 130-6 WI 1) AI Previous EdOene Smpenaled Eletlttelie FORM -POE Page 2 d2 SDNY_GM_02755005 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241927 EFTA01327045

SONY_GM_02755006 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241928 EFTA01327046

6Z6 I VZOCVJ..43 n rn 0 70 s moms...um Are Price Truincei N493LX 2 WillJFACTURER APO COIL Raytheon Aircraft Company 400A S SACRA*T SERA. Immo RK -244 FCAMORT ranspor t $ AuNow. MID asiliti ISSUMIC4 M Cn Downes anti. • dead James I tiSC SHIM woods Salae es ifisiaM bee east De termateat manlyo n= Yee ameba M M .I. Me iirelimat lob Ad en low 70 C Yes. Saw Is spa' a *Lipka, copra ea al *WM meas. MM AMT libruisigeM mon ea is sad Wm Wm, 410 to 'V 1O hopenc D3 70 GI ll 4 tOmi 70 US laninniadni Ewa Worm melirlo *sws od mein lamina Of edam isloWid brie Mit SWIMS eta in fddriwa sato M Masa ni > I , note" Minim MINS* ay Mood I OATS OF ASS FM AMESENTAME. r 12/29 013 Arthur Ockwell (S. L E:R:83 '1394 E3RG L NI Ilingek gTelart V no el Ix cede,. onto waning a Ire ni tatIonlIthrryteirori tratibi 1 I'm no V3 IL Ma CtoriWn rep• (AMMO li T. Ulfflft P MIXIMIGICI YAM 00K NU 'ww arimougoamoia : 4 00 WTED STATES COMMA DEPARTMENT Of TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE * None * n qk EFTA01327047

SDNY_GM_027550C6 ECTIVE ORDER PARAGRAPHS 7, 8 EFTA 00241930 EFTA01327048

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RK 244 STC list (12-26-2013) Reference 8130-6: Application for Standard Airworthiness Certificate Transport Category, dated December 26, 2013 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_02755011 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241933 EFTA01327051

SDNYGNI02755012 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241934 EFTA01327052

26180 Colin Weighi Pathway 'Cleveland. Ohio 44143 W.703.2148 www.11ighlopiiontam December 26, 2013 Nextant Aerospace, LLC 355 Richmond Road Cleveland, Ohio 44143 Attention: James Immke Re: RK-244 — Agent Authorization To whom it may concern: aliLOptions This letter is to confirm that Flight Options, LLC ('FO's) authorizes Nextant Aerospace, LLC, as FO's agent, for a Beechjet 400A, bearing serial number RK-244 and FAA Registration Number N493LX (also identified as a "Nextant 400XT'), which is owned by FO, for any and all authorized FAA actions in regards to: Airworthiness Classification Experimental X Airworthiness Classification Standard Sincerely, Flight Options, LLC By: Michael Metera Vice President, Administration & Contracts --777,,46/-det occitted Si Aure Sian and Subsortbez1 4o me 4416 do,/ -z-c,c,c bectenber O.c 2ni h4 C•N‘e.1.-,4246 tAelrere, • SDNY_GM_02755013 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241935 EFTA01327053

SDNYGA0102755014 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024I936 EFTA01327054

SDNY_GM_02755015 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024I937 EFTA01327055

SDNY_GM02755016 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241938 EFTA01327056

0 MAJOR REPAIR AND ALTERATION u S Cupeemni a (Airframe, Powerplant, Propeller, or Appliance) TranneriallOn FokinaInlaillea Aderilalotralca sorra nocrored CMS Pro 21204020 iirsorsoca Stet:Ciente Tracking Number For FAA Us* Only INSTRUCTIONS' Pail Cr Nye am envies. See FAR 43.9. FAR 43 Appendix 8. ant/ AC 43.9.1 (or sut4equent revision thereof) for instrictora and clisposito of this form. This meat is required by bw (49 U S.C. 1421) Failure lo roped can result in a civil penalty not lo exceed 51030 f0r each Such NobiliCel (Section 901 Federal AMIl0n Ad 1958) I. Aircraft etaboraley and Registration Mark N493LJ( Seel No RK-244 Make Raytheon Aircraft Company Model 400A Series 2. Owner Name (As shown on registration certificate) Flight Options .LLC Address (As shown on tegiatrelion certificate) Imes 26180 Curtiss Wright PKWY city Richmond Haightc ea. OH a M14114/3 Caner Sap 3. For FAA Use Only 4. Type 6. Unit Identification Repair Alteration UM tame weal Serial Number 0 CS AIRFRAME (AS desalt:media Rent f above) 0 O POWERPLANT MI O PROPELLER O O APPLIANCE Trap mrecreaser 6. Conformity Statement A Agencys Name and Address B Keg &Agency NOM Nextant Aerospace Meets 355 Richmond Road Cm Cleveland ea. OH Al 44143-1453 cowry USA O U.S Certificated mechanic O IManulacturer O Foreign Centfecared Mechanic C. Caleicale No. Lil Certificated Repair Station CRS # 25NR667B 0 Generated Maintenance Otani/seen 0. I Certify that the repay and/or meraton made to the und(s) Moaned m tern 5 above and described On the reverse or anachrnents hereto have been made in accordance with the requirements 01 Part 43 ol the U.S. Federal AWMkin ReguYekris and that ale MIcanaton furnished herein is true and correct to the best of my knowledge. Extended range hat per I 4 CFR Part 43 Ama. 6 0 Signature/Oa A.Ockwell Signature/Oats of Authorized individual ki.. 05/30/2013 7. Approval for Return to Service Pursuant to the authority given persons penned hams the unn Menhfred Aare:strata of Me Federal Aviabon Adrnmiseatoon and 4 m item 5 was inspected Into manner presented by the AlJeFt0YED 0 REJECTED FM FP Standards Inspector Manufacturer Maintenance Organization Penal APOr0ved by Canadian Department ol Transport BY FM Designee X Repair Staten Inspection Au Other (spew izaton c.a.:hie." Dempster., No CRS # 25NR6678 SignaturetOale of Authorized Mdiddual A.Ockwell 05/30/2013 eeeAL FAA Form 337 (7006) SDNY_GM_02755017 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241939 EFTA01327057

SDNY_GM_02755018 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241940 EFTA01327058

NOTICE Weight and balance or operating Ametation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with ad previous alterations to assure continued conformity with the applicable airworthiness requirements. S. Description of Work Accomplished Of more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) N493LX Nationality and Registration Mark Part I of 3 The Following Equipment was removed along with Associated Hardware. 05/30/2013 EFD-871 622-9345-203 Electronic Flight Display EFD-871 622-9345-203 Electronic Flight Display MFD-871 622.9434-213 Multi Function Display ICU-85 622.6189.002 Internal Compensation Unit ICU-85 622-6189-002 Internal Compensation Unit AHC-85E 622-9336-400 Attitude/Heading Computer AHC-SSE 622.9336-400 Attitude/Heading Computer SDU-6408 622-9735-001 Sensor Display Unit SDU-6408 622.9735-001 Sensor Display Unit DCP-5O0O 822-1028-011 Display Control Panel DCP-5000 822.1028.011 Display Control Panel ARP-851 622-9500-011 Altitude Reference Panel ARP-851 622-9500.011 Altitude Reference Panel AAP-851 822-0328.011 Altitude Awareness Panel AAP-851 822-0328-011 Altitude Awareness Panel CHP-850 622-7397-002 Course Heading Panel D8U-4100 822-0014-002 Data Base Unit DAU-650 622.9344-101 Data Acquisition Unit SOD-640A 622.9347-001 Sensor Display Driver IOC-4000 ( 4) 622-9814.514 Card Assembly MDC-4000 622-9818-751 Maintenance Computer CSU-4000 (2) 822.0049-002 Configuration Strapping Unit FMC-5000 (4) 822-0891-008 Flight Management Computer PWR-4000 (4) 622.9945.021 IAPS Power Card GPS-4000 822-0931-003 GPS Receiver Mounts 622-9430-002 EFD /MFD Mounts EFB Electronic Flight Bag Mounting E Additional Sheets Are Attached Date Form 337 oci-osi SDNY_GM_02755019 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241941 EFTA01327059

SDNY_GM_02755020 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024I942 EFTA01327060

NOTICE Weight and balance or operating linwtation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with ell previous alterations to assure continued conromtity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is metered attach additional sheets. Identity with aircraft nahenalety and registration mark and date work completed) N493LX 5/30/2013 Nationality and Registration Mark Page 2 of 3 Installed the Following Equipment along with Associated Hardware. Date Model Part Number Description Weight Arm CCP-3000 822-1746-002 Cursor Control Panel 2,60 90.0 CCP-3000 822.1746-002 Cursor Control Panel 2.60 90.0 DCU-3001C 822-2362-003 Data Concentrator Unit 5.0 325 DCU-3001C 822-2362-003 Data Concentrator Unit 5.0 325 ECU-3000 822.1200-209 External Compensation Unit 0.40 57.5 ECU-3000 822-1200-209 External Compensation Unit 0.40 57.5 FSU-5010 822-1543-101 File Server Unit (1." IFIS) 6.5 60.83 ECU-3000 822-1200-998 File Server Unit (1st IFIS) 0.40 57.5 AFD.3010E 822-1753.416 Adaptive Flight Display 12.90 89.2 AFD-3010E 822-1753-416 Adaptive Flight Display 12.90 89.2 AFD-3010E 822-1753.416 Adaptive Flight Display 12.90 89.2 AFD-3010E 822-1753.416 Adaptive Flight Display 12.90 89.2 IMT-3010 822-1140-401 AFD Mounting Rack 4.40 85.0 IMT-3010 822.1140-401 AFD Mounting Rack 4.40 85.0 IMT-3010 822-1140-401 AFD Mounting Rack 4.40 85.0 IMT-3010 822.1140-401 AFD Mounting Rack 4.40 85.0 10852801Y00 Fuel Quantity Conditioner 0.90 324 PC920.2A2000PH-2A1 Fuel Flow Conditioner 1.10 325 GPS-40005 822-2189-004 GPS Receiver 6.0 37 Cl 429-410 GPS Antenna 1.0 166.14 Amp Cluster N241100-002 DC Voltmeter 1.5 97.4 373-93-1501-1 Speed Switch (2) 0.25 89.2 DBU-5010E 822-3000.202 Data Base Unit 1.60 134.5 P5-8350 501-1228-004 Power Supply 12.5 52.9 MMT-5000 822.1811.003 File Server Unit Rack 0.30 57.5 MMT-3010 (2) 822-1290-003 AHS Mounting Rack 1.80 57.5 XM WR-1000 822-2031-002 XM Weather 1.5 41.0 CHP-3010 822-1280-003 Course Heading Panel 1.30 92.5 OCM-4100 822-1463-228 Options Configuration Module. WAAS/LPV 0.30 57.5 Options Configuration Module. OCM-4100 822-1463-228 0.30 57.5 WAASAPV Additional Sheets Are Attached Form 337 ('006) SDNY_GM_02755021 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241943 EFTA01327061

SDNY_GM_02755022 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241944 EFTA01327062

NOTICE Weight and balance or operating limitation changes shall be entered M the appropriate eimme record. An alteration must be compatible with all previous alterations to assure continued conformdy with the applicable airworthiness requirements 8. Description of Work Accomplished (II more space is required. attach additional sheets. Identify with aircraft nationably and registration mark and date work completed) N493LX 05/30/2013 Page 3 of 3 Nationality and Registration Mark Date Model Part Number Description Weight Arm CSLI-4100 (2) 822-1364-002 Configuration Strapping Unit 1.60 55.7 MDC-3110 822-1987-006 Maintenance Data Computer 0.80 55.7 FMC-6000 (2) 822.0868-123 Flight Management Computer 1.90 55.7 ADC-850D (2) 822-0389-468 Air Data Computer 5.30 60.83 ANC-3000A (2) 822-1378-001 Attitude Heading Computer 4.80 57.5 DCP-3030 (2) 822.1828-002 Display Control Panel 1.90 89.96 PWR-4000 (4) 622-9945-022 IAPS Power Card 1.3 55.0 IOC-4100 (4) 822.1362.511 Input/output Concentrator 0.8 55.0 LT-4001-010 Master Caution Panel 1.3 87.0 Rev. Panel 373-91-3203-1 Pilot Reversion Panel 0.2 88.0 Rev. Panel 373-91.3203.3 Co-pilot Reversion Panel 0.2 88.0 9-PED 373-91-3203-9 9-Pedestal Panel 1.8 92.89 345-6196 ELT Switch 0.2 88.0 Annunciator Led-42-12-BB-E0Y47 AUX BATT (1/2) Annunciator 0.05 88.0 Annunciator (2) Led-40-18-BB-EOY4S Pull Up/ Terrain Annunciator 0.05 88.0 Annunciator 2-F840231 Terrain Inhibit/ Terrain Fail 0.05 88.0 In Accordance with STC 51109595C. See Attached Copy AFM Supplement, Nextant Aerospace Doc. No. 373-00-0023 Rev IR Dated 09/02/2011 or later FAA approved revision, installed on Aircraft. Equipment Pilot Guides are Installed in the Aircraft as Portable Document Format (.pdf) via supplied I-Pad. NOTE: Portable electronic devices used to store required aircraft records required by Part 91.9 are considered Electronic Flight Bags (EFB) per FAA Advisory Circular AC 120-7613 par 4-g. Commercial operators are required to obtain authorization for their use from their managing Flight Standards District Office. Instructions for Continued Airworthiness (ICA) Ref Nextant Aerospace Document 373-00.0002.Rev C or Later are included in the Aircraft Maintenance Records Carried out System Ground Test Plan IAW Master Drawing List (MDL) 373-00-004 Rev C. Carried out Hawker Beechcraft Service Bulletin 34-3431 Reduced Vertical Separation Minimum (RVSM) Airframe inspection / Modification. Performed FAR 91.411Inspection per Part 43 appendix "E" Pitot Static & FAR 91.413 Inspection per Part 43 appendix "F" Transponder System checks. Additional Sheets Are Attached Form 337 O0-06) SDNY_GM_02755023 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241945 EFTA01327063

SDNY_GM_02755024 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241946 EFTA01327064

*Web 'hats el jlonerica !apartment of transportation -- 311eheral "thintion Pibministration $upplemental 'Type Certificate emteimersettiststeeek A140924" ST10959SC Nextant Aerospace LLC 26180 Curtiss-Wright Pkwy. Richmond Heights, OH 44143 araAidasa46411549th elA *MI iteeithA• ayeereerthnteddelaVa . ‘01•7414M104442.0‘etha.•a01 014•01 lefe fni•en IMMO ka efthreeed(thAV PrIthrneaa IAA( 25 944 Federal Aviation $801w4.64su (Sec Pages 3 and 0 for complete certification basis.) CarraePendant. gon..14:.;,44a,b.Z...14.. A 6SW Hawker Beechcraft Corp. sg,i,z 400A nuorares tsars frArs glair Installation of Rockwell Collins Pro Line 21 Electronic Flight Instrument System (EFTS) with Rockwell Collins FMS-6100, Localizer Performance with Vertical Guidance (LPV) approach capability and Universal Avionics Systems Conically (UASC) Terrain Awareness Warning System (TAWS) in accordance with Nextant Aerospace LLC Master Drawing List Doc. No. 373-00-0001 Revision W, dated March 29, 2012, or later FAA approved version, Snider/ n) cad wasa•us: 1) 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 that person written evidence of that permission. . 3) For aircraft equipped with Pratt & Whitney JT15D Engines FAA approved Airplane Flight Manual Supplement, Nextant Aerospace LLC Doc. No. 373.00.0008 Revision IR, dated 10/19/2009, or later FAA approved version, is required on board the modified aircraft. ow/ ee- an.,.-4," dale Gate <4. ?ewe A- eyfrawrzteOtsenesta‘v .16,c 4 nyydnels, a kanandava dart a ediearaw euknetawled4 ae. ..45dataadak..- ,97niearl. 4veram ./Inteakaatadase. giaernAarioaaaa' ..fune 26, 2008 ff trie nhaenana October 19.2009 .fiteeteeseaned giek cotioneree September 26, 2011; April 05, 2012 n-s e) Steven L Langnois mrrater. Systems and Flight Test Mach Chicago Airenft Certiliestien Office Ink) • Oe or taleettis • • la pi • • try* cane e r. • ncl n ..%e. ar aapt newne nnl no MP • or awn. l'AA Min 11.110.2120.4111 PAU 2 et 4 PULS nal terelliC•10 Sky b• transit vied Je acteraerte• oat. /AR 27.41 SDNY_GM_02755025 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241947 EFTA01327065

SDNY_GM_02755026 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024I948 EFTA01327066

3!Initeb filtehe of cAnterics !epnrhnent of Zgranspurtation - rebernl jthintion Abministration $upplententai Zurre Tertiftrate ((continuation *lee° ifi randee STI0959SC §42.44v5.4.ukynen. October 19, 2009 Date Amended: September 26, 2011; April DS, 2012 -Weedlohivw onaniAndthAw tervskaasei: 4) For aircraft equipped with Williams F344-3AP Engines, those engines must be installed under STC ST02371LA. 5) For aircraft equipped with Williams F144.3AP Engines FAA approved Airplane Flight Manual Supplement, Nextant Aerospace LLC Doc. No. 373-00-0023 Revision IR, dated September 2, 2011, or later FAA approved version, is required on board the modified aircraft. 6) Aircraft must have previously qualified for Operations in Reduced Vertical Airspace via: RK-I thru RX-I 17 and R.K-I 19 thru RK-139, Hawker Bcecheraft Service Bulletin No. 34-3431. RK-I IS, RK-I 40 thru RK-224, Hawker Beechcraft Service Bulletin Nos. 34-3228 and 34-3431. RC-225 thru RK-299, Hawker Beechcraft Service Bulletin No. 34-3431. RK-300 and after as original equipped from Hawker Beeclicraft. 7) For aircraft equipped with Universal Avionics Systems Corporation (UASC) TAWS FAA approved Airplane Flight Manual Supplement, Nextant Aerospace LLC Doc. No. 373.00.0036 Revision IR, approved March 28, 2012, or later FAA approved version, is required on board the modified aircraft. 8) For aircraft with Collins Proline 21 FMS-6100 LPV Approach enabled FAA approved Airplane Flight Manual Supplement, Nextant Aerospace LLC Doc. No. 373.00.0032 Revision IR, approved March 28,2012, or later FAA approved version, is required on board the modified aircraft. V:-.-.4Aeway, Based oil 14 CFR §p I.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Hawker Beechcraft 400A aircraft is as follows: a. The type certification basis for the Hawker Beechcraft 400A aircraft is shown on TCDS A IGSW for parts not changed or not affected by this change. b. The certification basis for the parts changed or affected by this change since the reference date of application, September 29, 2009, is based on TCDS A1GSW and §§ 14 CFR Part 25 as shown on page 4 of 4 of this STC. Any ccccccc Jon of (Ala csitIllen• Is puniseable by I floe of nee •ryncueq si.000. of INICI tamen net eoceetting S years. ar bets. IAA IOU 4110.1.1.10•601 mos I or I Nan MTh C•It4flontip soy b ccccc non, In acre/donne eJ I AS SI.ci. SDNY_GM_02755027 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241949 EFTA01327067

SDNY_GM_02755028 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024I950 EFTA01327068

/AtlikJ $1alco of America pepartment of Zumaportntion - Aeberal Ablation Abministration Supplemental 'Type Tertificate (aantinuation *pet) ,9404 eihwasot October 19.2009 Date Amended: Sep:ember 26, 2011; April 05, 2012 Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the baseline Installation of Rockwell Collins Pro Line 21 Electronic Flight Instrument System (EFTS) with Rockwell Collins EMS-6100 modification was detennined to be TCDS A16SW and the following later regulations: Am& [244) 25.771 (a,c) Amdtl25.23J 25.301:25.303:25.581; 25 607: 25.611. 25.773 (0)(1)(2Xd) Amd1.125-38) 25.1309 (aXti)(c)(6XeX8): 25.1322 Amck.[25.401 25.901 (b)0X1); 25.1549 (a)(9)(e) Amde[25.41) 25.1321 (a)(b)(c)(c): 25.1331:25.1333 Amdi.(25421 Anich. [2546) AnWt[25.541 Amde[25-72) Amdt.(25-80) 25.1501 25.603:25.605: 25.613; 25.1529 25.307; 25.571, 25.1307 25.1316 25.1329(h) (c)(c); 25.1351 (a)(1Xd): 25.1381; 25.1521 (.)(c); 25.1543 (b): 25.1581: 25.1583 (a) Arndt [2546) Andtt25.90) Am01.12541) Amdel25-102) Arm:X(2510g 25.305 25.1303 25.561 25.981 (MXb) 25.1585 (a) Amdi.(25-108] Amt11[25-109) Amdt[25.113) Aindel25-1221 Amdl.(25.123J 25.1325 (d) 25.1323 (a)(1)(g) 25.869 (a)(4); 25.1431 25.1317 (a)(b)(c) 25.1353 (axc) Based on 14 CFR §§ 21 Mend 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Collins Proline 21 FMS-6100 with LPV Approach enabled and UASC TAWS was determined to be TCDS A I6SW and the following later regulations: Arndt (Ckinjnall 25.601. 25.605, 25.609. 25.613.25.1301. 25.1357, 25.1381. 25.1525, 25.1541, 15.1581 Amdi [24-4) 25.771 (a) Amd1.(25-23) 25.301; 25.303; 25.305, 25.307.25.561(c); 25.607; 25.611, 25.1307 Amcti.)25-311) 25.603, 25.1322. 25.1583(0 Amdt.(25-40) 25.1585 (a) Amdt[25-41) Arndt [2542) Amdt(25-46) Amei.D5.54J Amdi 125.72) 25.1309 (aX8)(cXdXe)(8) 25.1501 25.777(aXc) 25.1529 25.869(100) 25.1351 (aXI) Amdl(25.102J Amdt [25-1131 Amdl.[25.123J 25.9111(aX17) 25.1431(a) 25.1353 (axc) -END. Any *Icon el at Rh pia/ ln.alt OY a SO !1.000. w 1ptlfors a. net *scowling 1 yens, o• btn. FAA rom 411.0.1•141.4.44) Plea 4 44 4 Plat mt. cocci OW* .. y be ceenteistd in •ccorame nth IAA 21.0. SDNY_GM_02755029 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 195 1 EFTA01327069

SDNY_GM_02755030 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241952 EFTA01327070

a MAJOR REPAIR AND ALTERATION us twormonter (Airframe, Powerplant, Propeller, or Appliance) nameenown Fowl Worn MOW 2120-0)10 it/WV/COT Electronic Tracking Number For FM Us* Only Fats mutton Arenaunmen INSTRUCTIONS: Print or type all entries. See FAR 439. FAR 43 Appendix B. and AC 439.1 (or subsequent reviler, thereof) for insPucticas and disposalo al tlis Semi This meet is required by law (49 U.S.C. 1421). Failure to report can result Macaw( penalty not lo emend $1.000 for each such riolallon (Section 901 Federal MAMMA Act 1958) 1. Altera Nations* and Recta/aeon Mark N493LX Serial No. RK 244 Make Raytheon Aircraft Company Model 400A Wes t. 0*.,.. Name (As shown on Mentionwocellitere) Flight Options .LLC Address (As shown on rIgiStainOn cernIOSIO) Awns. 26180 Curtiss Wriaht PKWY ON Richmond Height% Ram OH zo 44143-1453 Cann M 3. For FM Use Only 4. Type 5. Unit Idendfleadon Repair Alteration Unit Matte Model Serial Number 0 S AIRFRAME (As 00020 in nem I above) 0 • POWERMANT 1:1 o PROPELLER O O APPLIANCE Tan renreeLre 6. Conformity Statement A. Agency's Name and AddreSS B K nd of Agency tame Nextan1 Aerospace Adenns 355 Richmond Road City Cleveland hare OH zp 44143-1453 ceralay USA 0 us Certificated Mechanic 0 I Maniiacturcr 0 F“epn Certificated Mechanic C Cenacee No Ili) Cenilicared Repair Station CRS it 25NR6678 0 Cenificated Maintenance Organitabon 0. I cenifirilhaf the teen and/or alteration made to the unt(s) dentified in hem 5 above and described on the reverse or allacliments hereto have beam made in accordance with the requirements ei Pan 43 of the V.S. Federal Aviation Regulators and that the information furnished herein is true and correct la the best of my knowledge. ExtendedfR range NM et II p C Pane App. Ei 0 Sitnature/Dale of Authorized Individual (.1‘ 05/30/2013 7. Approval for Return to Service Pursuant to the authority given perscos weaned woe. the unit c'lentate4 in item 5 was inspected n the manner rammed by the Administrator of the Federal Aviation Adnimsbatkin and Is @APPROVED 0 REJEC7E0 BY FM FR Standards Inspector Manufacturer Maintenance Organist= Poser. Approved Of Candi:tan Department of Transport FM Designee X Repair Station Inspect-on Auttorizaeco Other (Specify) Cerblatte Or Designation No. CRS # 25NR6678 Manalure/)ate of Authonzed Mai dual II 05/30/2013 ..ckulk FAA Form 337 pooh SDNY_GM_02755031 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241953 EFTA01327071

SDNY_GM_02755032 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241954 EFTA01327072

NOTICE Weight and balance or operating limitation changes shall be entered in the 8POrnenale olltren record. An alteration must be compatible with a# previous alterations to assure continued conformity with the applicable aitworthineSSreqUireMenit 8. Description of Work Accomplished (If more space is (required attach additional sheets. Identify with aircraft nationality and registrabon mark and date work completed) N493LX Nationality and Registration Mark Nextant Aerospace Completed STC # 5102371LA Removed Pratt and Whitney JT15D-5 Series Engines . 05/30/2013 Date Installed the Williams International 1J44-3AP 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 MM Supplement NXT-1-AFMS Rev IR dated 9/15/2011 of later FAA Approved revisions. Installed Left Engine Part Number. 111000-202 Serial No. 252757 Installed Right Engine Part Number 111000-202 Serial No. 252758 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 K Additional Sheets Are Attached FAA Form 337 06667 SDNY_GM_02755033 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241955 EFTA01327073

SDNY_GM_02755034 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241956 EFTA01327074

e3tniItbfrIolte431,f1intricn Xlepartmcnt of Zrattspartntiatt - gebentI ?britiniatrn lion $upplententat Type Certificate Ata02,e" ST0237ILA Me6lograsatura Nextant Aerospace, LW 26180 Curtiss Wright Folkway Richmond Heights, Ohio 44143 cre4egveathatenti Pie 44(f/fin aniOnAraryiegervivivemotativa de intrZahew endeeteedfaivar //levey4. to- regfecatteea men* arrow/Strew eeyeti3ceetwiCi aunt 25* Var. givaireavaeheva "Berdttiti lea t. *Certification basis is set forth on TCDS A I6SW and continuation sheets 3 and 4. (gril;metarsene col Ifenpfera4vilc A I6SW desed": Hawker BeechcraR ..sgeeles, 400A taVere?-4 1.91". 93kter Virverpt Replacement of Pratt &. Whitney ITI5D-5 series engine with Williams International FI44-3AP engine (TCDS E3GL) with Full Authority Digital Engine Control (FADEC) and associated systems, in accordance with Nextant Aerospace Master Drawing List No.: MDL-NXT-00I, Revision RI. dated 8/22/2011, or later FAA approved revisions and FAA Approved Airplane Flight Manual Supplement, NXTI.AFMS, Rev TR, dated September 15, 2011 or later FAA approved revisions. Nextant Aerospace, LLC Instructions for Continued Airworthiness document NXT I -ICA, Revision IR, or later FAA accepted revisions must be provided with this STC. Smiamwo widie,w424heiv.. 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 the other person written evidence of that permission. (CONTINUED on page 3) eetiOak mniedci strav4ilys dace reditheeli eteyf eyyteeevriatmencvat:s Sid untie swarmed-ma( !keret:1e I erwAireacv• a fentreiraieen th eatereirao adertfAirea ..4dettio0trate, onto rnerettavetheta ..346633theakalleer OitotAr genakit. March 24, 2008 91.4,04:uffeme0.. September 27, 2011 Act )6) erraktoil.. gl""greble#1:. tkiliye/e neriCilevier Pgrowstret Manager, Propulsion Branch Los Angeles Aircraft Certification Office (Title) /toy afreterion of lick cceilicore LI pinia6a6k 6y it fin of mot 'wrote 61,004 or nerfromerar Ira ttnertaitil 3 yen, or &HA VAS riPlIR 6110,2(10.G1) Pogo t el • Oho tenfrtatemay& icearfrtreif aeromOitre il6 file:221.47. SDNY_GM_02755035 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241957 EFTA01327075

SDNY_GM_02755036 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024I958 EFTA01327076

INSTRUCTIONS: The transfer endorsement below may be used to notify the appropriate FAA Regional Office of the transfer of this Supplemental Typc Certificate. The FAA will reissue the certificate in the name of the transferee and forward it to him. TRANSFER ENDORSEMENT Transfer the ownership of the Supplemental Type Certificate Number to (Warne of transferee) (Rana of trantftd 6.484fromfaita) OA Pat, t. roe) from (Aran of grantor)(Tritit or type) Winn °fatalism) (Mager oaf sirte) Ogee.% swanned° Extent of Authority (if licensing agreement): Date of Transfer: Signature of grantor (In Fage2 of SDNY_GM_02755037 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241959 EFTA01327077

SDNY_GM_02755038 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241960 EFTA01327078

guitar Pates OH Sumac.' Pepurtment of ¶rnnaportution - greberal Ablation cAhntittiotrntioxr $upplemental 'Type Tertificate (gatitinuation Sheet) Afe.eei24, ST02371LA Sem%haw atm./Wean/draw loonanataii • Nextant Aerospace, LLC, "Installation of Rockwell Collins Pro Line 21," Amended STC STI0959SC, dated September 26, 2011 or later FAA approved revisions is required as part of this alteration. • The new Vmca and Vmcg values are 94 KIAS 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 Specification Jet A ASTM-D 1655 Jet A-1 ASTM-D 1655 ntlelicandiroaiew.4 The certification basis for this modification is as follows: The original certification basis for the Hawker Becchcraft Model 400A airplanes identified on TCDS A I6SW, Revision 26, dated March 17, 2010: Part 25 of the Federal Aviation Regulations effective February 1, 1965, as amended by 25-1 through 2540, plus §§ 25.1335, 25.1351(d), 25.1353(c)(5), and 25.1447 of Amendment 25-41; §§ 25.29, 25.255, and 25.1353(cX6) of Amendment 25-42; and §§ 25.361(6) and 25.1329(h) of Amendment 25.46. Part 36 of Ihe Federal Aviation Regulations effecliye December 1, 1969, as amended by 36-1 through 36-17; SPAR 27 effective February 1, 1974, as amended by 27-I through 27-5; and Special Conditions No. 25-ANM-32 dated February 22, 1990 (High Altitude Operation at 45,000 feel), and Special Conditions No. 25-ANM-33 dated June I8, 1990 (Lightning and Radio Frequency Energy Protection). (See NOTE 12) Equivalent Safety Hans: (I) Out.ottrim characteristics § 25.255 (2) Pilot compartment view § 25.773(b)(2) (3) Passenger compartment door § 25.813(c) (4) Emergency exit nnrking §¢ 25.81 l(dXI) and 25.811(d)(2) Application for amended Type Certificate dated February 18,1988. Regulation at a later amendments for components and areas affected by the change (Ref. FAA approved Compliance Check List): Subpart A - General : 25.2(25-99) Subpart B— Flight: 25.207(25-121), 25.255(25.42) Subpart C —Structure: 25.571 (25-96) Any damning El 14it rmfreate 4 Janata& by a As of riot earenang Boa or isopttoemini mm tureing J pan, or firll IM ono 020.2110.40 rya 3 Of 4 IfinerrtOrate may de transftrmf acconfanottath CAt21.47. SDNY_GM_02755039 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241961 EFTA01327079

SDNY_GM_02755040 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241962 EFTA01327080

pullet' "Malta (91 Aim Its Peparfaunif of Igrmusporintion - geberni c&bintion cabininistratinit $uppiemental ZUgpe Certificate (Gffontinuation Atet) ireuniee ST02371LA 51,444:.samSas4/conkrae.(1 Subnart D- Design and Construction: 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 — Powernlant: 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). $ubnart F— Equipment; 25.1301(25-123), 25.1305(25-115), 25.1307(25-n), 25.1309(25423), 25.1316(25-80), 25.1317(25-122), 25.1321(25-41), 25.1331(25-41), 25.1351(25.72), 25.1353(25-123), 25.1357(25-123), 25.1381(25-72), 25.1431(25-113), 25.1438(25-41), Subpart G —Oueratina Limitations and Information: 25.1501(25.42), 25.1521(25-72), 25.1527(25- 105), 25.1529(25-54), 25.1543(25-72), 25.1549(25.40), 25.1551(25-72), 25.1557(25-72), 25.1581(25-72), 25.1583(25-105). Subpart R - Electrical Whine interconnection Systems 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(25423), 25.1723(25-123), 25.172.5(25423), 25.1727(25-123), 25.1729(25-123), 25.1731(25-123), 25.1733(25-123). 14 CFR Part 34 (34-3): 34.11 14 CFR Part 36 (36-28): 36.1--36.7, 36.101-.36.105, 36.1501, 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. NXT1-EA-007 Rcv A dated 8/24/11 or later FAA approved revisions. flay diennioo of t44 anifteato is yriatiba6ii 6y a fine ewe twafio, $1300, or hopthoowoot NO4 midi"), 3 part or 6014. FM Piro 1110.2114-GGI n. a 4 Oinatrscotemay6ornouforreintercon4otelooliimnoz SDNY_GM_02755041 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241963 EFTA01327081

SDNY_GM_02755042 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241964 EFTA01327082

0 MAJOR REPAIR AND ALTERATION ki.9 agermentor (Airframe, Powerplant, Propeller, or Appliance) trangalalite Frn APWOMIO cum go 21204:020 Ii, Elected:et Tracking Number For FAA Use Only Fid401 ASPIMM Kedmoriden INSTRUCTIONS: RIM or type as entries See FAR 43.9. FAR 43 Appendix B. and AC 43.9-1 fee subsequent revision thereof) foe instruction and dieddiaCel 0 Mg Rim TM repOrt IS required by taw (49 U.S.C. 1421). Failure to (Open can reseal mauve penally not to exceed SLOCO for eaCC Such MNItkon Minion 901 Federal Aviation Act 1958) i Ad reel Nakinally 80day:43600 ,4am N493LX Sinai No. RK 244 Make Raytheon Aircraft Company Model 4OOA Series 2. owns Nero (As shown on tegisre aeon ceingage) Flight Options .LLC Address (As shown on registration certificate) memos 26180 Curtiss Wrieht PKWY cry Richmond Heiehte sew OH ze, 44143-1453 county LIbia 3. For FAA Use Only 4. Type S. Unit MeMllication Repair Alteration Unt Make Model Serial Number • r AIRFRAME (As descnbed in Item 1 above) O O POWERPLANT 0 O PROPELLER lE1 El APPLIANCE r ype maroaavo. 6. Conformity Statement A. Agency's Name and Address B K nd of Agency 111~ Wotan( Aerospace Adam 355 Richmond Road Coy Cleveland den OH re 44143-1453 Cony USA 0 U S Certificated Mechanc 0 i Manufacturer 0 Foreign Certificated Mechanic C Certificate No El Cogitated Rebate Station CRS # 25NR6678 0 Certificated Maintenance Organization D. I certify that me repair andor aeration made to tne unites) identified In item 5 neve and described on the reverse or attach:roots hereto nave been made h acccedance with the requvements of P ri 43 Of Ito U.S Federal Aviation Rogialicns and that the information furnished herein a true and comely:. the best of my knowledge Air CFR Pan 43 Extended range fur APR B Anton J. Koprivnik 72/292013 Signature:Date of Authorized Ircligdu r ,..„1 7. Approval foe Return Pursuant to the loth:fey given person; Spedtled Wog. the unit idettled Admiritarate Of the Federal Aviation Administration and is O:C in fern 5 was inspected In the manner presets by the APPROVED 0 REJECTED BY FAA Fit Standards IMpeCler tilanklecturer Maintenance Organization Person Approved by Canadian DepartmeM of Transport FAA Designee X Repair Station inspeebon &Swingle° Other Morel CetifiCate co Designs:Om No. CRS* 25NR6678 SignatureiDale of AlAhorived Individual 's Anton J. Koprivnik 12/29/2013 FM Form 337 0040 SONY_Gt4_O2755O43 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241965 EFTA01327083

SDNY_GM_02755044 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241966 EFTA01327084

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous afterabons to assure continued conformity With the applicable airworthiness requirements 8. Description of Work Accomplished (If more space is required. attach additional sheets Identify with aircraft nationably and registration mark and dale work completed) N493LX Nanonality and Registration Mark 12/29/2013 Date Installed the folowing InFlight Entertainment System in accordance with STC # ST03960AT and in accordance with Nextant Aerospace Master Drawing List DB1002067. Revision F.05 Dated: October 9, 2013. Installed Bonner Cabin LED Lighting System without the Venue System in accordance with NX330-1304002. Rev B Dated October 17, 2013. Ref. drawing for parts list. ICA Requirements. Ref FM Order 8100.17 Page 7.5 and 7-6 Use FAA publications such as AC 43.13-1, Acceptable Methods, Techniques, and Practices—Aircraft Inspection and Repair, and AC 43.13-2, Acceptable Methods, Techniques, and Practices—Aircraft Alterations; part 43 appendix 0, or other applicable aviation standards. Installed Iridium Sat Comm (Cockpit Phone only) and Broadband Internet System with Aircell Axxess II and ATG 4000 in Accordance with DB 1001013. Rev E ICA for Aircell System Ref to Nextant Aerospace Document No 081105003. Rev A dated September 22 2011 or later FM Accepted Revisions The following manuals contain complete detailed maintenance instructions and should be consulted for all maintenance activities not covered within this ICA: Aircell Axxess II Installation Manual 012004 Revision E, dated March 2010 or later applicable revision Aircell ATG-4000 Installation Manual 013485 Revision B Dated November 2009 or later applicable revision Aircell Axxess II WLAN AFM Supplement 061002072 Rev IR dated March 22 2012 for the has been Installed in the AFM Installed the Astronics DC•AC 115 VAC Power Supply in Accordance with D81002067 Rev F.04 Dated 10/9/2013 This is Located under the Seat Divan ICA for Astronics 115 VAC Cabin Inverter Ref to Nextant Aerospace Report No DB1108018 Rev IR Date 9/22/2011 or later FAA Accepted Revision. Aircraft Flight Supplement DB1109012 has been installed on the Aircraft See Current Weight and Balance Dated: December 29, 2013 End K Ado it anal Sheets Are Attached FAA Form 337 peoc, S ON Y_GM_02755045 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241967 EFTA01327085

A. SDNY_GM_02755046 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 1 EFTA 0024196% EFTA01327086

Uniith Slates of cRourica pepariment of ffiranoportation geberal (Ablation Pministration $upplemental Egpe Tertificate at) nr/Oivele impale ST03960AT Nextant Aerospace LW 3800 Southern Blvd. West Palm Beach, FL 33406 err//4' aline/:4 nivasse Or 4n touroer Aleve4entrekt/ tr•dr /4 ttro44/4ved nanfernalhirn den/te +neeArtienen at r/.' rtn;WellitineJJ nrithontnal r/ fikne25 r//4 Federal Aviation :iayskaivna. 65,-,frewnegAnket. jen rievolva, Aantrew Al6SW .414.9,4 Hawker Beechcraft Corporation ...eeevr-ae, 400A lotunfo/Arn r/rvfie lawiter War.. Installation of Rockwell Collins Venue In-Flight Entertainment(IFE), Airccll Axxess Cabin II Iridium Phone and High Speed Internet System with Wireless Local Area Network (WLAN) Astronics 1 I SVAC 60HZ Cabin Inverter, and Emteq LED Cabin Lighting System in accordance with Nextant Aerospace LW, Master Drawing List D131002067, Revision E, dated January 26, 2012, or later FAA approved revision. envana4M-en.. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determine by the installer that the interrelationship between this change and any other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. at) en-44, t4P wain!, Jerneelekp dant fritiMetz; f:va)Aertaternts/VW/ernefftio 44/ win/ ,intweetteerri Jenierrornevi reve‘neere re kniniverhivit eler* elienrae Nien(Avieelify .4.4e4reWerekt- V/4 '.7v/ /Al • / • /te/ • )/ /' 26.74. r/I:v/re;:vileew July 28,2012 t':Gt/e tyle).iteortm• March 22, 2012 fay* erniareene.• a' rle tante/hien, tfteet.)/erf4-,- nl Melvin D. Tay Manager Atlanta Aircraft Certification Office Any alteration of all. cortsticipt• it pwatado es/ • tins of not annd.frq 31.000. or norlsom•ot ror ....my 3 ye•rs. or Dorn. OA Oa 0110-2110.44i Mt I of . eMdt lAL certalfet• ray et unarmed is eccoll•N• with PAR 11. • SDNY_GM_02755047 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241969 EFTA01327087

SDNY_GM_02755048 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241970 EFTA01327088

Pniltb Stotts of Amccica gieparhnint of transportation - Athena cl‘ biation ADministration $uppietturrtal Zug Tertificate (Tantinuntion *Fel) tfriendese ST03960AT When the Rockwell Collins Venue system is installed Airplane Flight Manual Supplement, DB1106015, Revision A, dated March 22, 2012, or later FAA approved revision, is required. When the Aircell Axxess II system is installed Airplane Flight Manual Supplement, DB1002072, Revision IR, dated March 22,2012, or later FAA approved revision, is required. When the Astronics Cabin Inverter system is installed Airplane Flight Manual Supplement, 0811090I2, Revision IR, dated March 22, 2012, or later FAA approved revision, is required. This system is intended to provide Internet connection and email services to the airplane's cabin using portable electronic devices (PEDs). Any other intended function of this equipment will require a re- examination of the certification basis. When the Rockwell Collins Venue system is installed Instructions for Continued Airworthiness (ICA), Nextant Aerospace Document No. DB1002068, Rev IR, dated September 22, 2011, or later FAA accepted revisions must be made available to the operator at the time of installation. When the Aircell Axxess II system is installed Instructions for Continued Airworthiness (ICA), Nextant Aerospace Document No. DB1105003, Rev A, dated September 22, 2011, or later FAA accepted revisions must be made available to the operator at the time of installation. When the Astronics Cabin Inverter system is installed Instructions for Continued Airworthiness (ICA), Nextant Aerospace Document No. DBI 103018, Rev IR, dated September 22, 2011, or later FAA accepted revisions must be made available to the operator at the time of installation. When the Emteq LED Cabin Lighting system is installed Instructions for Continued Airworthiness (ICA), Nextant Aerospace Document No. DB1108019, Rev IR, dated September 22, 2011, or later FAA accepted revisions must be made available to the operator at the time of installation. My tlt•ncIOn or tAlt ttttt 11C•C• It SSUSA•ble by • Ube of not txf•MLIng $1.040. at lapilsosent not oKIM i ynrs, or bac, in now 5110-2.100.0) ma 2 .4 1 flat MIS ***** fICM• Yy be Monter 5. mtbriSSIK• Ida YAK ILO'. SDNY_GM_02755049 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241971 EFTA01327089

SDNY_GM_02755050 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241972 EFTA01327090

!Nitta Shahs of Anttrifit pepartment of raransportation - *bend Ablation elbministratioo $upplemental `Type Tertificate ((llontinuntian *lett) Aa/IdeleST03960AT 444/.;mg The Certification Basis for this installation is per Type Certificate Data Sheet A I6SW original Certification Basis, Federal Aviation Regulation (FAR), Part 25 as amended by Amendment 25-I through 25.40 plus FAR 25.1335, 25.1351(d), 25.1353(cX5), and 25.1447 of Amendment 25-41; FAR 25.29, FAR 25.255, and FAR 25.1353(cX6) of Amendment 25.42; and FAR 25.361(b) and 25.1329(h) of Amendment 25-46. In addition the following specified rules amendment levels were used for this installation. 25.571 25.1353(aXc) 25.1357 25.1431 25.1529 125.541 (25.1231 (25-123] 125-1131 125-541 (-) Indicates amendmen level Any Ncsrstlon of tAl• Corti tttttt Is puitl•habl• by s firm of sot esc•eding /Ltd; or 'enlacement net exceeding l deers. or both. • of • Any strop:Onto with IM 11.17. SDNY_GM_02755051 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241973 EFTA01327091

SDNY_GM_02755052 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241974 EFTA01327092

e MAJOR REPAIR AND ALTERATION cI .. 5. Can p aw. ,: d (Airframe, Powerplant, Propeller, or Appliance) rift...U.00m Aemerndon rem Seam OMB the 21204020 ludato? Elect/Oak Mocking Nwtot For FM Use Only INSTRUCTIONS: Prd or type al ands Ste FAR 43.9, FAR 43 Appendw S. end AS 431-1 (or 44014quen resllkn Theo() for insauclions and esoodaton of iris rant Iles walls Nene team (4911.S.C. 1421) Fabare to raped an mull Placid penally not to exceed 31.000 tor *en such skidon (Secan 901 Were, Adam Ad 1956) Nadonalty and Rogledraem PARR N493UX Seed No. RK244 Masa Raytheon Akaaft Company Mode 400A Sales 2. Owner Name f As sham, on regthrfarlon netttale) Flight Options, LLC Aetna (As shown on rodstratten cerdtedd 463.46180 Curtin Wright PKWY carRichmond Heiohts sw,i0hio 4,44143-14U cealn4)- 3. For FM Use Only 4. Type 6. Untl IdentMcallon Repair Abatedn Unit Mew Mo0&t Sad Number CI e AIRFRAME (As deSnitted I Gem / Steve) ID O POWERPLANT O O PROPELLER O O APPLIANCE Type Mattilaste 6. ContonnRy Statement A Agencys Name and Added B Redd Avert/ •,,,,sConstant Aviation 0 U.S. Cerlincated lisschink 0 IManutaduret nass,5211 Secondary Road 0 roman Centlealer methane C. CaNfaa No. ratCleveland StawOhi0 0 c.nkakd Repair Salon CRSOVC7R345J zp44135 eornerUnited 5jame 0 CerldcMed Mantensece Orgendiron 0. I web Walesa repair actor aaaallen made to the wil(s) kienelled In Ilan 5. Abeva and dosolDed on Inc raVelle a alladienCrila hereto have been male h SCCOnlanee wed the requrementi of Pad 43 dem U.S. Federal Aviation Rag-J.1:cm and that Ino neotiyelen turnewid wen Isms aM moo to the best <Amy Emmett*. &ladled arcs Fad per 14 CFR Pan 43 APP. B O SIgnalurSale Authorized lelvIdual .../ Date: December 30, 2013 T. Pro &turn to Sento Pursuant to MOMAWItyaben MOWS IC•Xted below. Ih0 uftt toenw In iron 5,W5 impeded to the manner presabial by tied wow:side d lie FOSeral Aviation Adeninittabco and is @APPROVED O REACTED AY FM Fa Slarearda 'Weds( Manubcturet Malnionerce Organtairn POW APPIted by Cansden ospartmerdoiTtareprt FM Designee X Repair Elam Impeden Aumorization °uncaps(*) calked or Dcsignallon Na CRSIA/VC7R346J Signature/Oale 44 Au0716 indivifraki i 4 _pi C....--_. Date: December 30 . 2013 FAA Form 337 mote SDNY_GM_02755053 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241975 EFTA01327093

SDNY_GM_02755054 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241976 EFTA01327094

NOTICE Weight and balance or operating ACPtalon changes shall be entered In Ina epprOpriale aircraft record An aftentliOn MSS be compatible with ell previous afterations to assure continued conformity WA Ina applenbie eirworterness fl at 1107010. 8. Description 01 Work Accra/nen/lad (17 more apace is reradred. aback addreonal sheets. Idenlity will aircraft nalionekly and regislabon mark end dale work completed) N493LX 12/30/2013 Nationality and ROgnretIon Mark OMB ACCOMPLISHED INTERIOR REFURBISHMENT/MODIFICATION AND 3 PLACE DIVAN INSTALLATION 111E FOLLOWING AIRCRAFT WTERICIR ITEMS HAVE BEEN FIEFURRISHETT Repoli-tea rtmosemd carnal columnsen Mane Nan Leather Accordance. mm, Betenlel 400A AMM 2970:07401, 73470-0d431 Removed and /Inland Glare weal and Eyebrow panel rrzeetia min Mac Black Leatner n AmotOonCe byth kettle 400A AMFA 20-60-00.201. Removed and Rcptaoed CoMpl &dawn maieral YAM Male Nark Leather n Accor0.1100 WIT' Regan( 400A AMM 20 so 00.701. Removed end stewed Pilot Seal Pan Mann TAOHIOOPIS0001 Serial Numb, 62. Foam and recovered rim Garret Steenkin Oak and Excel CaPPOCCIne Leather. Removed end laplixibil Conn Seal Pan Number TAOHIOOCIA00-01 Soul Number 240. Foam and mooned win Care% Sheennt Oak and Exton Cappuccino Leann Honnyed end Replaced Let Hand ea Passenger Seal Pal Number 2524414(430A) Serial Writer 9907194 Foam and recovered with Townsend Lester (1, tag Been) Removed and replaced RDA Hand N5 Passenger Seal Pan Inner 7524.014(4308) Sabi Number 000428.7 Foam and recovered wen Townsend Leather(reisago (Veen) Removed and Replaced Let Hand Se Passenger Seal PM Number 7574-014(5308)Serlal Number 0303484 foam and meowed wet TonnSend Learner Mentage r340^^) Removed and replaced ROM Hand sir Passenger Seal Pad Number 2524014(530A) Serial Number 030708-2 FOAM and ItCovered with Townsend lea:her (Ileolape Brown) THE FOLLOWING MANUALS ANDAPPROVED DATA HAVE BEEN UTILIZED FOR OASIS OF REFURBISHMENT: Skande Flamm/RAIN TOM 5254078 as approved by FM DER lane elberveln (DERV 832780-CE) en FM fain 5110-3 doled 4/23/2013 Fenn Cut 1 ammabely Teal 4311 19 e*eved by FM DER limb Reed II (OERT.230293-CE) on FM Finn II 10-3 doled 17/23/2013. Skanda I anrnablN UM Report TP 22081 Rey A as approved by FM DER Jane Eliterslen CERY432780-CE) on FAA term 8110-3 Men 05/02/2013. Tine Place Divan installation 'twined (3) Pacenon par Number 3743390(450131)T123.K02 SIN 003702k. Ancrdante wan Aviation Fannin STC4 ST0157204 and Marna Hannan* toy. retnn 5754078 per Jane Bibersleln FM GER (DERY4132753-CE) dated 4/73.2013 THE FOLICAMNO INTERIOR ITEMS HAVE BEEN MOOIFIED. UPI GsAy Any, RAI Gnaw Ndy. Man Any. UN Gat/ Asey and Irmiall per Della G drawing DGOCA01.101 Rev D. OdA CA01.101 EO E.I. Lai Galey 'Waft Da/D.409501 Roy BOA-I. 000-CAOI.501 Rev IR as EipprOeid on FAA lam 81104 pet FAA DER Donald Genre (DERT-790135-SW) doled Meryl 25 2013. 511 Gain Assy and Instil per Dna G drnengs DOD-CAW-101 Rev B. CGGCA02401 Rev IR as approved on FM form 81103 by FAA DER Donald tDERT-750135SW) dated Mardi 23. 2013 Divan May per Dab 0 Manage OGLIDA00401 Rev C rid DOODADS-101 CO DI as approved of FAA loon 5110.3 per FAA DER Own Gilasple (DERT 750135414) dated march 75 7013. Berner IN Wesel assy Many 7553-0038 Rev C. Inner Scieledge any drawing 2537.0037 Rev C. Bonner KII Foldout Tette assy drawings 25530041 Rev C and 2559-0040 Rev B. Scam XTI Ivies Ka Inn Penn 2553-0037 Rey C Appioved on FAA torn 81 £0.3 pia Stesmen Forman DERT.230238-CE dein Dec 20. 209 INSTRUCTIONS FOR CONTINUED mRwOrtalitts$ THE REMOVAL OF THE INTERIOR IS OH THE CONDITION OF FAILURE. THERE ARE NO ADOITIOWIL INSPECTIONS REQUIRED. CONTINUE TO INSPECT LAW MANUFACTURERS NAM. SRN. OR CMM AS AfinLICMILE AIRCMFT EQUIPMENT LIST AND WEIGHT AND BAUVICE WERE UPDATED BY THE CUSTOMER END- O Additional Shoots No Attached FAA Form 137 (tocs) SON Y_GM_02755055 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241977 EFTA01327095

SDNY_GM_02755056 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024I978 EFTA01327096

US DEPARTMENT OF TRANSPORTATION EDERAL AVIATION ADMINISTRATION STATEMENT OF CONIPI IANCE WITH THE FEDERAL AVIATION REGULATIONS DATE Dec 26, 2013 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Beechcraft Corporation MODEL 400A TYPE (Airpione. Radio. Helicopter. etc.) AIRPLANE NAME 0 'APPLICANT NEXTANT Aerospace Cleveland_OH. LIST OF DATA IDENTIFICAITON TITLE REPORT: BEECHJET 400A INTERIOR STRUCTURAL SUBSTANTIATION BEECHJET 400A XTI LINER KIT INSTL. Beech Jet 400A, Aircraft Serial No. RK-244 Certification Bases for this aircraft modification is per Type Cenificate Number A I 6SW Revision 28 dated April 12,2013 RKG3282 Rev. IR, 8.28.2013 2553-0037 Rev C, dated 8.30.2013 PURPOSEOF DATA DESCRIBE AND SHOW VERIFICATIONS FOR NEXTANT INTERIOR INSTALLATION ON BEECHJET 400A, AIRCRAFT SERIAL NO. RK-244 APPLICABLE REQUIREMENTS ( List specific sectoom) 14 CFR Pan 25 §.301, 303, 305, 307a), 365, 561, 571, 601, 603, 605, 609, 613 CERTIFICATION - Under authority of appointment under Pan 183 Mille have been vested by direction of the Administrator and in accordance with conditions Federal Aviation Regulations, data listed above and on attached sheets examined in accordance with established procedures and found to comply Regulations approval of these data Approve thew data and limitations numbered with applicable requirements of the Federal Aviation I04 Therefore 0 Recommend ,ii SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATIONS) . Suphai Fames DEBT-210238-CE STRUCTURES AND DAMAGE TO1ERANCE .13 2 . FAA Form 8110-3 wit) SIDUEDS unmans amen 00 WI -41) SDNY_GM_02755057 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241979 EFTA01327097

SONY_GM 02755058 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241980 EFTA01327098

FAA FORM 8130-6, APPLICATION FOR U.S. AIRWORTHINESS CERTIFICATE Form Approved O.M.B. No. 2120-0018 Ex irahon Dec 02/2602013 la APPLICATION FOR U S aim U.S. AIRWORTHINESS 0 T,Insoce.wat Federal A awn CERTIFICATE 4.4nenstrica. INSTRUCTIONS • PAN a We Co AM Ante A shmImi meas. Ira re Ice FM '44 onry Soter4 pig nal only AA On OATonnsl FM Rimesorisugo I oddmovi ram m tecsanog use etschment For sow/ ilosi pennals compbm Sealant IL VI. rod VI As ecolcablo ,T. € 2 : V5 :g i REGIS !RATON MARK N493LX 2 AIRCRAFT TMUTETTS NAME 4.•4•6 Raytheon Aircraft Co 3 NRCRAFT ROCS DESIGNATION 4OOA I YR. MFR 1999 FM COOING 5 ARCRA77 SEAM. 143 RK-244 6 DOPE Ka DERS MME Mow Williams International 7 OGRE MOOR CESKIMATION F444-3AP It RIMIER CF DORIS 2 9 Amapa]. ER LANCERS RAW Amy N/A XI PROPELLER MOOSE CES044T04 II NRCRAFT IS /Coss nmemmi N/A I &PORT 0 i S V A 4 g APPUCATON IS HEREBY MADE FOR Mow mAltRom•I I A I STAICAPONRYC.RTKNESS CERTFCATE Oramos pro I I •mm't I I T"`"` I ram 44 I I •••••••41 I I "way' I I 1414414 Home 6 .4 SPEOAL AiRAORDI NESS CERTIPICATE Om remmesisso PROURY 9 UGNTSPORT I I Arlan I I Pommarscru. I I WilisflEtsflOATIM Helder I I 2 Ara.. UNTIED Wm Man Of I CUSS I 3 PRORSIONAL nAme• env 2 CUSS I 1 ACIRCIARITE NO PEST CORROL 2 AERIAL SURVEY 3 AERIAL ADVERTISING 3 RESTI A ECTED poss. meal 4 CREST S PATROL/4 6 HOTPOT CONTROL to ems** 0 OTHER Norm I i IIMMROI AND CEVELOPMENT 2 AMATEUR Out 1 3 ONEITIOI 4 NRsRAON3 S CREW TRAINIC 6 MARKET SURVEY 0 TOHav compuencE %%mum am 7 OPERAnNG Pam* 649 ..NITK CAT AIRCRAFT i EXPEFtMENTAL IA Emir! MOMMA an racrIhress orettical• 199 nal awl EMI 4 OMAN meal seniassie I OtiERATAG w onto/ Etnspa• oar LIONTOORT EC Orsuna banal oieeuse sued spew. erlispon emery avezononi agleam wet $ 21 193 OMMORD IA RESEARCH ANCIOEVELOVERT ICI RAW/ TRAI/61/3 NRCRAFT IS AWNS SURVEY 1 FERRY RIGHT FOR REPAIRS. ALTERATIONS. TINARENTACE. OR STORAGE SPECIALEDGAR PEROT RAMS 2 EVACUATE NOM MO OF IMPOONG OA/43ER I coln••••••••••ANA Ono.* 2...., w. w... ~2 ,...... 0. 4 3 OPERATOR IN MESS OF MAXIMUM CERTORCATEDTAKE4)FF REIGN 4 CeuvetwooR EXPORTING I S I I mooucnotiFUOIT TOMO 6 CUSTOMER DEMONSTRATOR FLOWS CI 6 MULTIPLE AiRWORTHAIE3SCERTIFCATE CosnalCatibeerwOrosive in elSow a bar a wolge/ 2 c • A REGISTERED WATER IA TiencaeaslossienmenigaNITTO IF 00116. CTICCX REFS--. I muff F igh Options LLC ADDRESS 26180 Curtis Wright Parkway, Richmond Heights .OH 44143 B ARCRAFT CERIFICATICAI BASIS tom falkSiill t Oa in (p.m. row ea vowed AMC:RAFT SPEOFICADCR OR TYPE CERTIFKATE DATA SHEET 0.06.4 Ammm.vAl N/A I atimcarmaEss onscnvEs Kan. nia...sas......a................... now A sumfmOrwsom As wmoy Ara a /oar emmesso Bi Weekly 2013.22 10121/2013 -11/032013 APOIAFT UST46(0.•••••^01•414.7 N/A SUPPLEMENTAL TYPE CERTIMATIE ase A....../..6.3762.6Amnso N/A C AIRCRAFT OPERATION AND MAINTENANCE RECORDS ORCX F REcfl IN I COUPWACE 551714 14 CFR sec6591 417 TOTAL AIRFRAME TOPS TTAF 85M.82 3 EXPENMERTAL ONLY Me mos Am. mm Assam se A AA A 4 0 14.82 0 CERT F CATION .1746•16. ON* tel 1 114404•551•415 *al 49 Ors VIM 747110 sesonnress marcme mammal wn ire mcpmna ma (or In PPM / to PIMIII 4444454.7 SAL Maim 640415 6674 44101 66666 AM Makatle F•dere MAMA Accisfons. And MN ITO IS 1‘1011•0 6111 FM Fail AAleknAOTITesirsIa,15 *MA 666 Wen jowled o'd 17 apt" and SOO 174 to DATE 07 APPUCATOI 11/18/2013 NAME ANO TITLE Sem Owl Antony. J. KoPrhtra Agent SOJATURE ‘ e / 4 11.2.‘„.. 1 I i i I A THE NRCRAFT DESCRINO MOVE HAS BEEN Ir4PECTECIMO FOUND AMORIST EIY:e0esIseim mem cay 14111Asee 171•••••••1 r 2 NUR ,prj 121 CERTIFICATE scam*. 3 CEFITIFICATED ARCHAIC Oa ColOw• mo I 6 CERIVICATE0 REPAIR STATION Au, Ceske Ts/ 5 AIRCRAFT MAIRVACTURER SIM.° An/ OM 1111E SIGNATURE v. FM RtPRISINTAffill CCRIVIWION itaTe1•Ltemitainx•••••••411, I DM CERTIFICATE REQUESTED A I MOM Ito oat Ammo 04400, I.. vil mwasmonons b • maws ON LICX4FICATICITI OP CURRENT ASTACRTHINESS CERT1FCATE a awastn kr • NOM AV4 pan. retlerSocion VII esIn— Or FMINSPECTOR FM DESIGNEE CERT/CATE POWER DEER 14 CIR Asia I I I4 CFR Pal 121 OR OS 1 114 ma/inns DATE 11/18/2013 1600.300 CC ACE CLE-25 4 FM INSPECTORS SIGNATUR CESGNEES SIGNATURE MCC. Arthur Ockwell DART833943GL Q. 1 FM CRS Celtic M UNE • bp., J...‘,...tisr--., FM Fan 013041"I II AA Pa AGA 601110413 Super$17104 Eseaseve FoXISOI -POF Et. vvED DEC 1 9 2013 CLE Otr SDNY_GM_O2755O59 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 • ffi O • a EFTA_00241981 EFTA01327099

t I SDNY_GM_02755060 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241982 EFTA01327100

P E t i PROOJCTION g a A. IIVARIACTURER NAME *OGRESS P R O P / M e i I A S I S (CAW o a r A c o N o on CERTIFICATE (Give prtelleivi O.t10 Nat% .. WOE CERTIFICATE OTHER C. GIVE OUANTITY OF aRTECATES REWIRED f OR CREAMING NEEDS DATE OF APFIJCATION NAME ANOMIE IAN Of WE SIGNATLRE i I I O 1 5 S i 2 i 0 0 A DESCRIPTION OF AIRCRAFT REGISTERED OMER AGGRESS BIALCER (WV ACM SERIAL RIMIER REGIST RATER IMRE a DESCRIPTEN OF RIGHT DETOSER DEMONSTRATION EMIRS O (Cwt itmalcitau FR011 TO VIA DEPARTLRE DATE DURATION C. CREW REOLIRED TO OPERATE TIE NRCRAFT ANO ITS EOLEVENT I I PILOT [ I COPILOT I I RIGOR ENGPEER I I OMER (SPORN D TIE PERCRAFT OCES /CT MEET TrE APPUCAFAE MANGROVE% RECNAREMENTS AS FOLLOWS. E TIE FOU.OAING RESTRICTIONS ME CONSIDERED NECESSARY FOR SAFE OPERATION (On Firechworl It nO0Fsmy1 F CEATIFEATION - I MEN panty Ms I an M WOES owe (of lw POEM of Fe Rola *noted sews. WE Pe Mein is nose*, NM H FENS Avalon All•Oltteka In =Wave Mn Tao re DA N Wed %An GNP 400' iLma as Eclat* Fan Mom Rpoinora n ON re WMPm tem reseed Rd es We ler Ur VI Sweat DATE IMRE AM TIRE JAW 0/ Fa) SORT UK . 1 1 IE i 1 g I J A 2proVE UMW.* Ird Vedni, In CamIrc•IMP II CIR Slate 91.1 D. Stiewnve al Carta/MN. FM Form 6130. fAciaot Vim stoat° II Foy,. Mrecettris CASIsion tor Awl AMA Dawn MAT AMERI) R. Cornet CESARE LRAItons Altana C. DM Dote. MVP" Pc WEN PAM *MOE i RvIRa Anhannvo OMAR. NERO nApartlenco NM IA CFR Sicson 21.19 1 (a) am (Onanagnaao 1 at Waft Waft Fla Bain:* INN*._ Avairas Marva I Valor REpOrird ~MA FM Fain 337 CAPRA seen AMINE 1 . . Omni Ancennics CrVica Awed /*Am:Nino NM I d ("fa no , 21.191(a) toanotama) F TM Ricceten REWIRE hAiv•II ReComb I( Liyagn Ana %int of COVIact EM Ewa PINY'S 0.11•01 PISA APOREE FM Form 1304 I 4/10 Al PilhiCta UPON Supine:Rd Electronic Fond -PDF Pop 2 ol 2 SDNY_GM_02755061 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241983 EFTA01327101

SDNY_GM_02755062 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241984 EFTA01327102

%sierra STATIc Ce MOW. OMATIIIINT Or TRAMPORTare. • SIC€RM "WOW ACildwaTRA11O.4 SPECIAL AIRWORTHINESS CERTFICATE A CATEGORYRICSIGNATCHI =WEAL PURPOSE MEWS 6 DM n R. ILFAXU- IIACRFREA NAME ,i1/ ; .., 'DURESS e C FLIGHT F u \ L . TO T O 4A•• I . D " Milt SER NO w -≥44 o. EARLISER nFIGRETRI A REACio ry ),...i f UO L AIM E OATE CR LSSUARICE I e V E $n 12.X114 OPERAUNG um T Ns tEo -- ku FE:2013 ,. . RAPTOR DRSGERTRCATE socase of trantr•cs9+ . , . Pithy °Wel 1 1. . SConliceiNt0FAC400) OFT831063al. AFF sewn ilpalanotrusairofna tomato wry. Nana* by • Ire cm seeding PACO cv iftrionraer4r0i isondrq >pen*. ton NIG COHOICATEWST OE DORLArti) ON 1)t W1 IN ACCORPOCE WITH mw le-astral CODE 0 'MAN ROMA7014 (CM YNrNymAnMLu SDNY_GM_02755063 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00241985 EFTA01327103

A TM anioRass aortic:me turas inn art** a' Rat la $04-6. 0 VS/ gin** 00 44701 an! /IV Ilea d Semi Peinincea KM ip B The sewaikins coldest aura. 1%. ,ndnAaSur In0tn Sworn oh* 0 ordO Podscro, :We al fat cgOi "Sabi OW Mat 01 Mc n tegarved Alb meg Wandcoy ontxtpolckm Site um Leder*. anemia' pso Re consvaol or Pat sib (2)Cengporws rd ecorctilto Pawpaw (le 174 C no analw'bucetkab Ontalin be aftl wan*, PO TOW IS ke te pomp awn 11b, A O Di invihnns cot SR calks nita One SW claret IN nth sMI coved,. Ka royale,/ ttM i 0~ hi 'snits till* Metal* OR 7b not OM Ni MO anepatirMett al Wadi conwheets sod ducial advalhem (Of r a posa4 be /mix 1b RN Croon°, On bitIMICOVICalASIo• ?Wow gurs mato Stead Onutelco int yen. MY (I) meal n moils= td. to ;plat* Ofianin =minx ofeandecne •-0 Invaots .0.0, est* posm10 by theAtanisrece at pd Otis wits" al army bap =myvita:Pe spear masa, dab °sorry E Wris NOW unnIncl worded nolo/ Res olingroteis conkier • 'MAW *SR etralat aid wolef Ps onto+, Pearlte.10 It CIA Pm V. Seam 21 1St of 11.21t SONY_GM_02 755064 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 00241986 EFTA01327104

• tILITIO ELATES," MIKE • : DIEVRITADCT CP lIVMEOMALKPI• TOLOW , IALTEINVIAIIIIMILTIN SPECIAL AIRWORTHINESS CERTIFICATE A CATtOORTUNGNAIKa EXPERIMENTAL PURPOSE * andbankipeal El two FACTURER RAW ti Ammo D FLOW FROIA TO t- D TA MT1E X BUILDER Mutate UCCIEL ARRA E RATED, CRUM idui yrjanen A MEE annum. T Midi T. Rey/KEPI ME PART Of THS MIME( INSITITATION CR DEE a PC OARFJOOI4SCE T. kty imapRovert INACO3RONECE eirmot reventita g d Ds aM6Y way bit Weltle tE II MO a ELOIEOLE SI COO W rot oottoug 3 row Teton TAG CERTIFICATE KIST OE OISELAYED -NNE MIME, AIN APPOCES.E TITLE It COCE OF Eta IILL REOULAII0'4 OE I SDNY_GM_027S5C6S T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00241987 EFTA01327105

A n na weesheas colleen Masi Well. airety al Pat Us 10140/0010 SIM MM MP 44/04 and la Ti Cali cl WO, 419 002'0010 D ' Thorootwessanksinseera ite marbant rarelathl *WOOS* bareict froAcks Wit but PI cek "Ada. Or INK al liCall 1St* 0 Wen NO pirK0 ft* C a* a co:Wool quest. we r rs antra (1)Carn pews open • r a na sakn ce Imo sae 0ICerag pml el tenitil I, Or i0014 cite NW C Do •••••••••• conks* lairs to nita 40.041 0 IM twa Wag be mon twin lbs.& D Ths anagram nintlet t ad Iv la d earat Iv mat b Midi mold ta ton ended ward Wiwi Iv an west. eft* *Oa CM U. Snit ea. td Nos Ito name. dr* scratecevonwo M. OWN ~Inn ODOM padof by MM. 50 be tametcn as arra:al OS MO a. No ciao nry opts bs scat aorta cm to nre•I Se (I I earn a Main MM.. COMA! CPR ard n IKKOdInCe at wanes. lantlikes./0 rep 01 CUSS CI to FM at pi elINOP11011. MOS Mg Sir Why Eitel to wail Rana d hi earn E'• stagnant suceacc a racied. M scents ohms is °MON b Re Salem MI tre IN Mare {retorted .• 14 CR. Pan 21. Sesks11 Mail 217. SDNY_GM_02755OS6 1" TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 00241988 EFTA01327106

O.S.Oapartment of Transportation Federal Aviation Administration REG. NO. N493LX EXPERIMENTAL OPERATING LIMITATIONS For Research and Development (R&D) MAKE: Raytheon Aircraft Co MODEL 400A FAA Cleveland FSDO Great taxihem Yamada,/ Park II 25249 Courily Club 0940. NOM amulet,. Ohio 44070 (440 6803-7000 SERIAL NO: RX - 244 THESE OPERATING LIMITATIONS SHAH. BE ACCESSIBLE TO THE PILOT 1. No person may operate this aircraft unless the FAA Form 8130.7, Special Airworthiness Certificate. is displayed at the cabin or cockpit entrance and visible to passengers or flight crew members. 2. No person may operate this aircraft for other than the purpose of Research and Development to accomplish the flight operation outlined in the applicant's program letter Dated November 13.2013, which describes compliance withl4 CFR 21.193 (d) and made avadatte to the pilot in command of the aircraft In addition, this aircraft shall be operated in accordance wah applicable air traffic and general operating rules of 14 CFR part 91,and all additional limitafonsherein prescribed under tho provisions of 14 CFR 91.319 W. 3. R&D flights must be conducted lAW Nextant Aerospace's Program Letter Dated November 13. 2013, within the geographical area described In the program letter. R&D Akins will be conducteiln North America 4. Except for takeoffs and landings, this aircraft must not be operated over densely populated areas or in congested airways. 5. This aircraft must not bo operated unless it is maintained and inspected in accordance with the appropriate military technical publications and/or manufacturer's recommendation. The ownerioperator must select, establish, identify, and use an inspection program set forth in 14 CFR 91.409 (e), fib (g), and 04. This inspection program must be recorded in the aircraft maintenance records. 6. The Pilot In Command of this aircraft must hold an appropriate category/class rating. If required for the type of aircraft to be flown, the Pilot In Command also must hold either an appropriate type rating or a Letter of Authorization issued by an FAA Flight Standards Operations Inspector. 7. This aircraft may bo operated under VFR, day and/or night. 8. Thb Aircraft may be operated under IFR, and must be properly equipped for instrument flight in accordance with 14 CFR 91.205. 9. No person may operate this aircraft for carrying persons or property for compensation or hire. 10. No person may be carried in this aircraft during flight unless that person is essential to the purpose of the flight 11. The Pilot In Command of this aircraft must advise each passenger of the experimental nature of this aircraft. And explain that It does not meet the certification requirements of a standard certified aircraft. 12. This Alrcraftmust containthe Beech Model 409A Flloht Manual with Nextant 400XT AFM Section lnsert, Placards, markings, etc. (or other operating instructions developed loran STC modification), as required by14 CFR 91.9. 13. This Aircraft is Prohibited from Aerobatic Flight, that is an intentional Maneuver involving an Abrupt change in the Aircrafts attitude, an abnormal attitude, or abnormal acceleration not necessary for normal flight, unless part of show compliance flight testing 14. This aircraft shall rot be used for glider towing, banner towing, or intentionalparachutejum 9 Page I al 2 SONY_Glil_02755067 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241989 EFTA01327107

SDNY_GM_02755068 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241990 EFTA01327108

U.S. Department of Transportation Federal Aviation Administration FM Cleveland FSDO Ghat Atntlern TOckly0109Y Park II 25249 Country Ovo Blvd Nom COnstead (440)44154000 15. No person shall operate this aircraft unless within the preceding 12 Calendar months it has had a condition inspection performed in accordance with 14 CFR Part 43, appendix D,or other FM approved programs, and was found to be in a condition for safe Operation. This inspection will be recorded in the aircraft maintenance records. to. FAA-certificated Repair Stations and FM - Certified mechanics with appropriate ratings, as authorked by 14 CFR 43.3 may perform inspections required by these limitations. 17. Inspections shall be recorded in the aircraft maintenance records showing the following or a similarly worded statement: "I certify that this aircraft has been inspected on (insert data) in accordancewith the scope and detail of 14 CFR part 43, appendix 0,or other FAA approved programs and found to be in a condition for safe operation." The entry will Include the aircraft's totaltime-in-service, and the name, signature, certificate number, and type of certificate held by the person performing the inspection. 18. If the aircraft, engine, or propellor operating limitations are exceeded, an appropriate entry will be made in the aircraft records. 19. 11% aircraft must not be operated unless it is maintained and inspected in accordance with the requirements of 14 CFR Part 43. 20. This aircraft must display the word "EXPERIMENTAL"in accordance with 14 CFR 4523lb). 21. The Pilot In Command of this aircraft must notify air traffic control of the experimental nature of this aircraft when operating into or out of airports with operating control bees The Pilot In Command must plan routing that will avoid densely populated areas and congested airways when operating VF R. 22. This aircraft does not meet the requirements of the applicable, comprehensive. and detailed Airworthiness code as provided by Annex 8 of the International Convention of Civil Aviation. The Owner/Operator of this aircraft must obtain written permission from another country's Civil Airworthiness Authority (CM) prior to operating this aircraft in or over that country. That written permission must be canted aboard the aircraft together with the U.S. airworthiness certificate and, upon request be made available to an FAA Inspector or the CAA In the country of operation. 23. Arcraft instruments and equipment installed and used under 14 CFR 91205 must be inspected and maintained in accordance with the requirements of 14 CFR parts 43 and 91. Any maintenance or Inspection of this equipment must be recorded in the Aircraft Maintenance records. 24. Application must be made to the geographically responsible FSDO or MIDO for any revlsicn to these operating 25. 14 CFR 47.45 requires that the FM Aircraft Registry must be notified within 30 days of any change it the aircraft registrant's address. Such notification Is to be made by submitting Aeronautical Center Form 8050-1, Aircraft Registration Application, to MS-750 in Oklahoma City, OK. 26. Condition Inspections must be performed in Accordance with 14 CFR Part 43 Appendix D at least every WO Hrs Flight Hours. This Inspection must be performed by an FM Certified Mechanic with the Appropriate Ratings as deemed in 14 CFR. 43.3 27. The Special Airworthiness Certificate and Operation Limitations will copke on. Jan 12.2014 Arthur Ockwell Designated Airworthiness Representative DART833943GL Issued at Cuyahoga Airport Date Issued: Nose-nter IS 2013 Page 20(2 SDNY_GM_02755069 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241991 EFTA01327109

I SONY GM 02755070 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024I992 EFTA01327110

nextant aerospace Quality Assurance Department To: Federal Aviation Administration Flight Standards District Office Great Northern Technology Park II 25249 Country Club Blvd North Olmsted, Ohio 44070 Date: November 13, 2013 From: Anton J. Koprivnik Chief Inspector Nextant Aerospace $ubiect; FAA Program letter for Beech let 400A, Serial number RK-244, Registration Number N4931.X. Ref: FAA order 8130.2G 1. Registered Owner: Flight Options LLC. Address: 26180 Curtiss Wright PKWY, Richmond Heights, Ohio 44143 2. Aircraft Description: Twin Engine Light let a. Registration: N493LX b. Aircraft Builder Raytheon Aircraft Co c. Year mfg.: 1999 d. Aircraft Serial Number: RK-244 e. Aircraft Model Designation: Beech let 400A 3. The program purpose for the aircraft will be used To complete the flight performance profile in Research & Development Category in support of FAA Project SA 152S0LA•T (Replacement of Wingtips) 4. Program Duration a. List the estimated flight hours required for program: 20 Hrs b. Number of flights: 20 c. Number of days: 60 5. Describe the areas over which the flights to be conducted and address of base operation: The base of operation is Cuyahoga County Airport, 355 Richmond, Cleveland, Ohio. Flights will be conducted in North America. 6. Describe the aircraft configuration: This Aircraft is a standard Beech set 400A with new Williams F144-3AP engines and upgraded avionics with full authority digital engine controls (FADEC) a. Maintenance Program 1. Hawker Beechcraft Maintenance Manual Chapter 5 Rev C22 or later with the exception of the 1115D Engines. 2. Williams International recommended El44 3A Maintenance manual (FADEC maintenance is covered in 71-00-00 of this manual) 3. Maintenance Requirements for the Throttle Quadrant is addressed in the Instructions for Continued Airworthiness on the F144-3AP STC. Anton J. Koprivnik Chief Insdfct r Nextant Aerospace Tel Work 216-797-8257 Cell 216.225.8645 SDNY_GM_02755071 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241993 EFTA01327111

i SDNY_GM_02755072 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241994 EFTA01327112

16180 Curbs, Woght Pathway Cleveland. Oluo14143 877.703.2348 www.11ightoptions.com November 13, 2013 Nextant Aerospace, LLC 355 Richmond Road Cleveland, Ohio 44143 Attention: James Immke Re: RK-244 — Agent Authorization To whom it may concern: Options This letter is to confirm that Flight Options, LLC ("FO") authorizes Nextant Aerospace, LLC, as FO's agent, for a Beechjet 400A, bearing serial number RK-244 and FAA Registration Number N493LX (also identified as a "Nextant 400XT), which is owned by FO, for any and all authorized FAA actions in regards to: X Airworthiness Classification Experimental SDNY_GM_02755073 Airworthiness Classification Standard Sincerely, Flight Options, LLC By: MOLLY KEANE NOTARY PUEIUC STATE OF ONK) My Corm upen Am 24.2016 Michael Metera Vice President, Administration & Contracts -1-eccick, SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241995 EFTA01327113

SDNY_GM_02755074 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241996 EFTA01327114

MAJOR REPAIR AND ALTERATION u s oupwwirt a (Airframe, Powerplant, Propeller, or Appliance) reesrAirlan (torsi kola', A4mIrist,KOCI Fan frowww Ore Ns 21200O20 I I Ns Elsdrenk Tracking Number For FAA USG Only INSTRUCTIONS: Print or type as snarled See FAR 43.9. FAR 43 Appendix B. and AC 43.9.1 (0 subsequent revision thereof) for instruCtiOns and disposition Cl this form The report is required by Inv (49 U.S.C. 1121). Failure lorePart Cal Mater in a civil Pena), not re IMMOST.0W for each such vialation (Section 901 Federal Actaeon Ad 1955) I. Aircraft Natrona* and Regisbatian Mark N493LX Serial No. RK 244 Make Raytheon Aircraft Company Model 400A Series 2. Owner Name (At snOirm on registration candCON) Rig ht Options .LLC Address (As shown on registration cerriscrreel Athirst 7.6180 Curtiss WrIcht PKWY coy Richmond Height slake. OH ao 44143-1453 cover? OA 1. For FAA Use Only 4. Typo 5. Unit Identification Repair ikaarebon UM Make Model Serial Number O El AIRFRAME (As dunned, M nem I above) 0 O POWERPLANT O O PROPELLER O O APPLONCE ;le !Jar:ix-Low 8. Conformity Statement A. Agency, Name and Addren B. Kind o4 Agency Nam Nextant Aerospace Mows 355 Richmond Road Car Cleveland sure. OH co 44143.1453 coney USA 0 U.S. Certificated Mechanic 0 Manufacturer 0 Foreign Certificated *anon C. Certificate No. Ell Certificated Repair Station CRS # 25NR667B O Certificated Mahlenance organization D. Inertly that the repair andror allerabon made to the 'mills) ides ed in Item 5 above and described on the reverse or attachments hereto have been made k accordance with the retedrements of P rl 43 of Ste U.S. FederalAviation Ragulabans and that the information furnished herein neve andconed to the best of my enornedge. Extended range fist per I4 CFR Part 43 App B O Signahrtan)me of Aug-coked Individual , Anton J. Koprivnik 12/29/2013 7. Approval for Return Pursuant lo the authority given persons peofied bekvr. the un I Mangled In item 5 was inspecsed 0 mo manner retuned by the Administrator or the Federal AnalionAdministralion and is 0 44PROvso O Rt./Mt:EP FAA FR Inspect sunwards or Manufacturer Mantenance Organization !Perso Approved by Canadian Depa el Pansport renent BY FAA Designee X Repair Station Instal:moan Authorization Dew (Spear) Cartiaimre or Design # 25NR6676 don No. CRS SianalureiDate of Armoczed menden Anton J. Koprivnik ' ••• 12/29/2013 FAA Form 337 (10-06) SDNY_GM_02755075 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241997 EFTA01327115

SDNY_GM_02755076 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241998 EFTA01327116

NOTICE Weight and balance or operating Mutation changes shall be entered in the appropriate &Mae record. An alteration must be corvette,* mill all previous alterations fo assure Continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nations/fly and registration mark and date work completed.) N493LX Nationality and Registration Mark 12/29/2013 Date Installed the following In-Flight Entertainment System in accordance with STC U ST03960AT and in accordance with Nextant Aerospace Master Drawing List DB1002067. Revision F.05 Dated: October 9, 2013. Installed Bonner Cabin LED Lighting System without the Venue System in accordance with NX330-1304002. Rev B Dated October 17, 2013. Ref. drawing for parts list. ICA Requirements. Ref FAA Order 8100.17 Page 7-5 and 7-6 Use FM publications such as AC 43.13-1, Acceptable Methods, Techniques, and Practices—Aircraft Inspection and Repair, and AC 43.13-2, Acceptable Methods, Techniques, and Practices—Aircraft Alterations: part 43 appendix D: or other applicable aviation standards. Installed Iridium Sat Comm (Cockpit Phone only) and Broadband Internet System with Aircell Axxess II and ATG 4000 in Accordance with 08 1001013. Rev E ICA for Aircell System Ref to Nextant Aerospace Document No DB1105003. Rev A dated September 22 2011 or later FM Accepted Revisions The following manuals contain complete detailed maintenance instructions and should be consulted for all maintenance activities not covered within this ICA: Aircell Axxess II Installation Manual D12004 Revision E, dated March 2010 or later applicable revision Aimed ATG-4000 Installation Manual D13485 Revision B Dated November 2009 or later applicable revision Aircell Axxess II WLAN AFM Supplement DB1002072 Rev IR dated March 22 2012 for the has been Installed in the AFM Installed the Astronics DC-AC 115 VAC Power Supply in Accordance with DB1002067 Rev F.04 Dated 10/912013 This is Located under the Seat Divan ICA for Astronics 115 VAC Cabin Inverter Ref to Nextant Aerospace Report No DB1108018 Rev IR Date 9/22/2011 or later FM Accepted Revision. Aircraft Flight Supplement DB1109012 has been installed on the Aircraft See Current Weight and Balance Dated: December 29 2013 End K Additional Sheets Are Attached FAA Form 337 0046) SDNY_GM_02755077 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241999 EFTA01327117

SDNY_GM_02755078 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 002420((1 EFTA01327118

pilteb $Iatta of Atrorica !apartment of Crannporfation —31reberal jkbiation jthtnittistr anon (Supplemental Type (Certificate ,fl) tee/Arte eietnnfle, ..4‘984 0 ST03960AT Nextant Aerospace LLC 3800 Southern Blvd. West Palm Beach, FL 33406 tre-fOu //et I de neer &re elevrei‘o deAtetbreiptonvArinvAf /de etettrectehte trzenientStre efeereAr eta reelleekterronmee4 de erkeecava At/weirs:rah eye fikei 25 Va. Federal Aviation Siter ikai•••• , 6:-#thalOrdemot sfrow4.-44ntte,.- develd.• gliverfrika Our* Mr Al6SW Hawker Beechcraft Corporation 400A Installation of Rockwell Collins Venue In-Flight Entertainment(IFE), Aircell Axxess Cabin 11 Iridium Phone and High Speed Internet System with Wireless Local Area Network (WLAN) Astronics 115VAC 60HZ Cabin Inverter, and Emteq LED Cabin Lighting System in accordance with Nextant Aerospace LLC, Master Drawing List DB1002067, Revision E, dated January 26,2012, or later FAA approved revision. ..95;;wezthew., ffaiftwafmt• This approval should not be extended to other aircraft of this model on which other previously approved modifications arc incorporated, unless it is determine by the installer that the interrelationship between this change and any other previously approved modifications will produce no adverse effect Upon the airworthiness of that airplane. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. ..974 tw/92674 reed/4 .myyrethity wale t;i de 4J6 erierreteet.4eKetrowettiv tio *Or/t nit ••••••warryrd. •flyinenteed erg:drier re &teenier/4w toile b aftere4e sutatfeweenf err de .4.4,47,i4revr.. ty(de 9reitnedect;r/tete ...thetisti/tethive, Owe r.Artie.vmw July 28,2012 Oat r/Atetetwer March 22,2012 /e nva•••ed.• "Gilt mwenelevoC. ..V,•• en' ntitidevtlet• Melvin D. Tay Manager Atlanta Aircraft Certification Office Ity am/scion of can cortilleac• 4 puninad• kr a Imo et net atcoetin shoot, or is inners: nee azenolni 1 rests, et bath. * ttlf0fat• / to aYUbr SDNY_GM_02755079 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024200I EFTA01327119

SDNY_GM02755080 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242002 EFTA01327120

Limo Preis of America Xleparhnent of transportation - Atberal Ablation gthministration Supplemental Zgrie Certificate (C[cmtinuatiort *get) tirttathieST03960AT When the Rockwell Collins Venue system is installed Airplane Flight Manual Supplement, DB1106015, Revision A, dated March 22, 2012, or later FAA approved revision, is required. When the Aircell Axxess II system is installed Airplane Flight Manual Supplement, DB (002072, Revision IR, dated March 22,2012, or later FAA approved revision, is required. When the Astronics Cabin Inverter system is installed Airplane Flight Manual Supplement, DB1109012, Revision IR, dated March 22, 2012, or later FAA approved revision, is required. This system is intended to provide internet connection and email services to the airplane's cabin using portable electronic devices (PEDs). Any other intended function of this equipment will require a re- examination of the certification basis. When the Rockwell Collins Venue system is installed Instructions for Continued Airworthiness (WAX Nextant Aerospace Document No. DB1002068, Rev IR, dated September 22, 2011, or later FAA accepted revisions must be made available to the operator at the time of installation. When the Aircell Axxess II system is installed Instructions for Continued Airworthiness (ICA), Nextant Aerospace Document No. DB 1105003, Rev A, dated September 22,2011, or later FAA accepted revisions must be made available to the operator at the time of installation. When the Astronics Cabin Inverter system is installed Instructions for Continued Airworthiness (ICA), Nextant Aerospace Document No. DB 1108018, Rev IR, dated September 22,2011, or later FAA accepted revisions must be made available to the operator at the time of installation. When the Enneq LED Cabin Lighting system is installed Instructions for Continued Airworthiness (ICA), Nextant Aerospace Document No. DB11080I9, Rev IR, dated September 22, 2011, or later FAA accepted revisions must be made available to the operator at the time of installation. My elrrnUwn or L1L wrUtlnN L pnbneplr by • bar et net rnerOlnp 11,04 • er lyrbawnr rx oxen so l non, Or bin. TM rose 8110-2 -1110-1,) ?WI 2 of 3 'ACM nilw soy b tranaterml In oiccoto4Ace vI lb FAR 11.17. SDNY_GM_02755081 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242003 EFTA01327121

SDNY_GM02755082 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242004 EFTA01327122

Putteb Ateles of .Avarice !tom:fount of litransportation - Aeberal j16izif ion ciA bininisl ration Supplemental 'Type Certificate (Enntinuation Sheet) Jirtt/2Am ST03960AT fraPojieles/eiv..36144/).. The Certification Basis for this installation is per Type Certificate Data Sheet AI6SW original Certification Basis, Federal Aviation Regulation (FAR), Part 25 as amended by Amendment 25-1 through 25-40 plus FAR 25.1335, 25.1351(d), 25.1353(c)(5), and 25.1447 of Amendment 25-41; FAR 25.29, FAR 25.255, and FAR 25.1353(eX6) of Amendment 2542; and FAR 25.361(6) and 25.1329(h) of Amendment 25-46. In addition the following specified rules amendment levels were used for this installation. 25.571 1 25.1353(a)(c) [25-541 [25-1231 [-] Indicates amendment level 25.1357 [25-1231 25.1431 [25-1131 25.1529 (25-541 AAy alcerstfon of chip cnititicoco Is putiShataf by a hi* of MC excreting 12410, or loprisonseat not •nendleg I rya/s. or lea. rM Rom 1110-2-1410-tfl Hat 3 of 3 h.413 This certificate may be tea ***** rod Is sccoreosce WU, I1.0). SDNY_GM_02755083 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242005 EFTA01327123

SDNY_GM02755084 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242006 EFTA01327124

Nextant Aerospace LLC 3800 Southern Blvd Bldg. 1625, Suite 307 West Palm Beach FL 33406 Approved By Report No: DB1002067 Revision F.05 Master Drawing List Document Number: DB1002067 Revision: F.05 10/18/2013 in-Flight Entertainment HAWKER BEECHCRAFT 400A Aircraft FAA STC ST03960AT Date 1-4-2013 Page 1 of 7 SDNY_GM_02755085 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242007 EFTA01327125

SDNY_GM_02755086 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242008 EFTA01327126

MAJOR REPAIR AND ALTERATION US D4WInael a (Airframe, Powerplant, Propeller, or Appliance) Treopmation Eutaw Aviation mminermon ram Ow coed ova Ho. 2120{020 I I/302007 Electronic Tracking Number For FAA Use Only INSTRUCTIONS: Print or type all entries. Sat FAR 439. FAR 43 Appendix B. and AC 439.1 (Or subSequont reviponthereol) for -nsisuctons are disposition of this form. Tins report is required by bw (49 U.S.C. 1421). Failure to report can result on a civil penate not to elMCCI $1.000 for each suannolation (Section MD Federal Aviation Ad 1950 I. Aircraft Nahonally and posistraion Mark N493LX sena No. RK 244 Make Raytheon Aircraft Company model 40OA Smes 2. Owner Nwne (As show° on reg#fraton eettakele) Flight Options .LLC Address (AS 51101vit on legilltatiOn cerbkafel Manes 26180 Curtiss Wriohl PKWY cb,. Richmond Heights Mete OH zit 44143-1453 Cooney 06 3. rif FAA Use Only a. Type 5. Und Identification Repair Alteration Urst Make Model Serial Number 0 it AIRFRAME (As anent.; on Rem I above) ill ID POWERPLANT El El PROPELLER El el APPLVWCE Tyne lAnteciwig 6. Conformity Statement A. Agency, Name and Address B. Kind of Agency Mere Nextant Aerospace mow 355 Richmond Road cry Cleveland snare OH ao 44143-1453 Corny USA 0 LI.S. Cenrcatea mecnark 0 Ilearniactund 0 Foreign C•rorcairo mechanic C. Cortikab) No. ea Ceet•catied Repair Stabil CRS # 25NR6678 0 Cerkficaled Maintenance Organization 0. I teitfy that the repair bildlee allerabon made to liw unit(s) identified in item 5 above and described on the reverse Or attachments hereto have been made in accordance won the requIrements OW 11 43 of !M U.S. Federal McMinn Rev:eh°, s and that the -nrocfiatied furnished harem is true and 03Crea to the best of my knoorledge. Emended range fuel eel de CFR Part 43 Apo 9 0 SignalureDale of Authorized Individual Anton J. Koons/Mk 12/29/2013 7. Approval toe Return to rustic Pusuanl to the aulhonty given persons Wended berms the unit identified in item 5 was inspected in the manner preScnbed by the Administrator of the Federal AwananAdmineadeen and M El APPROVED 0 REJECTED BY FM Fit Standards Inspector Manufacturer M aintenance Orgarmation Parson Approved by Canadian Department of Transport FAA Designee X Repair Station InSP4010n AufiVrilabon Omer Specify) Cents*, Delbration No. CRS N 25NR667B S rature/Date of AuMortzed Mcbcdual de 7 7 , t Anton J. Koprivnik 12/29/2013 err .-' d FAA Form 337 poem SDNY_GM_02755087 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242009 EFTA01327127

SDNY_GM_02755088 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242010 EFTA01327128

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record An alteration must be Compatible with aft previous alterations to assure continued conformity with the applicable northiness requirements 8. Description of Work Accomplished (If more space is required, attach additional sheets identify with aircraft nationally and registration mark and date work completed.) N493LX Nationality and Registration Mark 12/29/2013 Date Upper Aft Baggage Panel Mod Modified Baggage Ceiling Panel to Accommodate the Engine FADEC wire harness. 1. Fabricated two panel pieces, N251103-001 and N251103-002. 2. Installed N251103-001 to existing baggage compartment structure 128.440095-1 using two screws and install N251103-002 as shown with a trim to fit honeycomb piece fabricated from interiors using potted inserts. 3. Attached honeycomb baggage panel to N251103-001 in upper aft baggage area using three 40S5-21 Camloc quarter- turn fasteners and 214-16D receptacles. Secured N251203-002 to existing upper aft baggage panel with two Camloc 4055-21 quarter - turn fasteners and 214-16D receptacles. See attached FM Form 8110-3 Signed by DERT-410115-CE Paul Hedding on February 12. 2013 using Nexlant Aerospace Engineering Order EO 029. Rev E Dated February 8.2013 ICA Weight change is Negligible. Continue with Beechjet 400/400A Maintenance Manual Inspection Procedures for this Area End K Additional Sheets Are Attached FAA Form 337 (ckos) SONY_GM_027550139 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024201 I EFTA01327129

SDNY_GM_02755090 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002420 I 2 EFTA01327130

U.S. DEPARTMENT OF TRANSPORTATION FEOERAL AVIATION AOMINISTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS 1 DATE February 12, 2013 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MAKE Hawker Beechcraft Corporation 3. MODEL NO. 400A 4. TYPE (Aircraft ErKene. nrOneder. eSc.) Aircraft 5. NAME OF APPLICANT Nextant Aerospace LLC Richmond Heights, Ohio LIST OF DATA 6 IDENTIFICATION 7 TITLE EO 029 Rev. E February 8, 2013 Upper Aft Baggage Panel Mod. END 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 FM approval of all the engineering data necessary for substantiation of compliance to necessary requirements for the entire alteration. S. PURPOSE OF DATA Engineering data in support of major alteration to Hawker Beechcraft 400A, SIN RK-244. 9. APPLICABLE REQUIREMENTS (List Weak WS4) CFR Title 14 Part 25.301[25-23], 25.303(25-23], 25.305(a)(b)(c)(25.23J, 25.307(a)(25-23], 25.562(c)(25-23], 25.601[25.00], 25.603(a)(b)(c)(25-38), 25.605(a)(25-00), 25.607{25-23], 25.609(a)(b)(25.00), 25.611(25.23], 25.613(a)(b)(c)(25-00], 25.619(25-23], 25.625(a)(b)(c)(25-23], and 25.789(25-32]. 10. CERTIFICATION • Under authority Part IB3, data Wed above and on apcimble requirements of Ito AinCettaleSS vested by deecton 01 the Administrator and I, accordance vsth condsons and nmsa5cns of appcintrneM under 14 CFR Washed sheets numbered WA have been examined in accordance wee establ.wed procedures and Found to comply with Standards Listed. approval of New data these data . Recommend I (We) Therefore 0 Approve I1. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(5) 12. DESIGNATION NUMIERS($) 13. CLASSIFICATION'S) •sr ---"407— Paul Hedding DERT-410115-CE Structures FAA Form 81103 (0110) SUPERSEDES PREVIOUS EDITION We Number H13107-06 Page 1 of I SDNY_GM_02755091 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242013 EFTA01327131

SDNY_GM_02755092 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242014 EFTA01327132

e MAJOR REPAIR AND ALTERATION uSOirawmort or (Airframe, Powerplant, Propeller, or Appliance) cirsoontoot reword Arbon 4.4minsireim Fenn Aerate OW. 212043320 CCM Eltchonn Tracking Number For FAA Ufa Only INSTRUCTIONS: PrM1 or type a alai. See FAR 4&9. FAR 43 Appendix & and AC 43.9-1 (or subsequent revision Memo° for instruckas and diSposilion of this form. This report Is required by law (49 U.S.C. 1421). Failure le report can result In a call penalty not to exceed 31.030 for each such ligation (Section 901 Federal AUabal Ad 1953) 1. Aircraft NeleAlidy and Reczalraben Mark N493U( Serial No. RK 244 Make Raytheon Aircraft Company Model 400A Series t. Owner Perna (As skim on rflistrafron CerhOCOM Flight Options .I.LC Address (As shown on rep/save% centekafe) Peeress 26180 Curtiss Wright PKWY ciiy Richmond Heights sum OH Z9 44143-1453 So-ant Oa 3. For FAA Use Only 4. Type S. Unit Identification Repay Metalled Unit Make Model Serial Number O 0 AIRFRAME (As described in nem f above) . O POWERPLANT El O PROPELLER O O APPLIANCE Type NtrivJaeder 0. Conformity Stet mom A. Agency's Name and Address B. lard of Agency Nam Nextant Aerospace Addroris 355 Richmond Road coy Cleveland sink OH za 44143.4453 Cony USA 0 lie °MACAW Mechanic 0I Mankfacturer 0 Ferias Camas's rarrthanic c. cerebra No. i i i Cildideated Repair Station CRS # 25NR687B 0 castrated Maintenance organizawa 0. I anbly that the repair &Wry alteration made tome una(s) denlifieti in ilem S above and described on Me serene or attachments hereto have been made in accordance Nile the requirements of P rl 43 Of the U.S. Federal AviabOn Regulations a nen a: the ink:mar:ton furnished heron is Irue and arrecl 10 the beg Of my knowledge. Extended range fuel per 14 CFR Pan 43 Pep. e - • Signaturetele c4Autixtrilet InOsidual Anton J. Koprivnik 12/29/2013 l 7. Approval for Return to ce sa Pursuant lo the authority given persons peened below, the unit dangled in item 5 was inftpeeled in the manner prescribed by the Administrator of the Federal Aviation Administration are is 121 APPROve0 O REJECTED FM Flt Standards Inspect*: Manufacturer Maintenance Oramizalion Person Approved by Canadian Department of Transport BY FM Ochres X Recast Sleben Other ) InspecionAulhorizabon ceteraOr Desiginalian No. CRS ft 25NR66713 Scraturntale of Amhonzed Indrddual Anton J. Koprivnik 4 ....L......./ 1229/2013 FAA Foam 337 (loam SDNY_GM_02755093 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002420 I 5 EFTA01327133

SDNY_GM_02755094 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242016 EFTA01327134

NOTICE Weight and balance or operating limitation changes shalt be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations fo assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft natkaulley and registration mark and date work completed) N493LX Nationality and Registration Mark 12/29/2013 Date Installed New Pitot Probes in accordance with SIC ST10159SC. Nextant Aerospace Master Drawing List Document 373-00-0001 Rev CC E024-11 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 Probe Part Number PH1100-MUL-EN Serial Number 1728401 Leak Check carried out IAW Beechcraft Aircraft Maintenance Manual Chapter 34-12-00-201. ICA Continue with Normal Hawker Beech Maintenance Practices for this Area End K Addilional Sheets Are Attached FAA Form 337 (mob) SDNY_GM_02755095 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242017 EFTA01327135

SDNY_GM_02755096 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002420 I 8 EFTA01327136

MAJOR REPAIR AND ALTERATION a U.ElDeementrace (Airframe, Powerplant, Propeller, or Appliance) teeepeetplee areas AViabla mairastre.on Fab cov anonco7 ea ONO Ne. moo= Elects* Tracking Number For FAA Use Only INSTRUCTIONS: Print ce type all envies. See FAR 43.9. FAR 43 Appendix B. and AC 43.94 (or subsequent revision thereol) for astrumans and atbeatiOn Of thiS Rum. This Meal iS required by law (49 U.S.C.1421). Failure tie tat can result in a civil penalty not to exceed $1.000 for each such violation (Section 901 Federal Aviation Act 1958) I.Aircraft Nabonalty and Regestraton Mart N493LX Serial No. RK 244 Make Raytheon Aircraft Company Model 400A Series Owner Name (As show, on registration cortthcata) Flight Options .LLC Address (As shown on registration oerhficate) meow, 26180 Curliss Might PKWY 2. any Richmond Heights sin OH zo 4±11,4a4.53 country USA 3. For FAA Use Only 4. Type S. Unit Identification Repair Menem lJed Make Model Serial Number El 0 AIRFRAME (As discrete in item I awe.) 0 O POWERP1ANT CI O PROPELLER s O APPLIANCE Typo Menulackeer II. Conformity Statement A. Arrays Name and Acmes: a Kind of Agency Novi Nextant Aerospace Adam 355 Richmond Road ant Cleveland Pam OH at 44143-1453 Carey USA 0 0 S. Cenncated arecAanic 0 Man Vacever CI Foreign Cortical Mechanic C Ceti riCale No 0 Cendicated Repair Station CRS # 25NR6678 0 Cerbficated Maintersarbe Organized*, D. I tatty that the repair (index alteration made to the Lobs) identified in item 5 above and described on the reverse a attachments hereto have been made in accordance tirrh the requirements of P rl 43 el ,,c U S Federal Aviation Republica. and Mal the informanm furnished herein *lrue and correct ID the beet 01 my knowledge edended range fuel per 14 CFR Pan 43 APP. B O Signature/Date of Autheilted Individual Anton J. Koprivnik 12)29/2013 2i • :....../ 7. Approval for Return Ma Pursuant lode authority given persons pecited below. the unit identified Administrator of the Federal Aviation Administratim and is rb in Om APPROVED 5 was • in:peeled in Me manner prescribed by the REJECTED By FM Fe Standards Inspector Manvlacurer Makeenance ClightliZZAka Person Approved by Canadian Department of Transport FAA Designee X Regale Station impectonAuthoozetion Other (Sce00) Certificate or Desapraton nib. CRS # 25NR6679 Manature/Date of Authaized Individual J. Koprivnik . 12129.'2013 at .; FAA Form 337 DOOM SDNY_GM_02755097 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242019 EFTA01327137

SDNY_GM_02755098 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242020 EFTA01327138

NOTICE Weight and balance or operating limitation changes shall be entered in the Appropriate airaaft record. An alteration must be compatible with at previous aerations to assure continued conformity mth the appaable airworthiness requirements 8. Description of Work Accomplished (If more space is required. attach additional sheets. Identify with aircraft nationality and registration mark and date work completed) N493LX NationaMy and Registration Mark Provisions for 19107 in Cockpit Sidewall at F5122.735 12/29/2013 Date Added Mount provisions for19107 in bracket assy. 45A88588-3 at Flight Station 122.735 provided in Structure Repair Manual Document 53.20.05-001. Use receptacle MS3470W18. See attached FAA Form 8110-3 Signed By DERT-410115-CE Paul Hedding. Dated December 28, 2012 using Nextant Aerospace Engineering Order 115-12 Rev C, Dated November 27, 2012 for details. ICA Weight change is Negligible. Continue with Beechjet 400/400A Maintenance Manual Inspection Procedures. End K Additional Sheets Are Attached FAA Form 337 (I 046) SDNY_GM_02755099 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242021 EFTA01327139

SDNY_GM_02755100 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242022 EFTA01327140

U S. DEPARTMENT Of TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS 1. DATE December 28, 2012 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2 MAKE Hawker Beechcraft Corporation 3. MOOEL NO 400A 4. TYPE (AVCratt Enpne. Propeller. eta) Aircraft 5 NAME OF APPLICANT Nextant Aerospace LW Richmond Heights, Ohio LIST OF DATA 8 IDENTIFICATION 7 TITLE EO 115-12 Rev. C November 27, 2012 — ----- ----- Mount Provisions for J9107. — ------ END -------------- — 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 FM approval of all the engineering data necessary for substantiation of compliance to necessary requirements for the entire alteration. a. PURPOSE OF DATA: Engineering data in support of major alteration to Hawker Beechcraft 400A, S/N RK-244. 9 APPLICABLE REQUIREMENTS Gist spear stollens/ CFR Title 14 Part 25.301(25.23), 25.303(25-233, 25.305(a)(b)(c)(25-23), 25.307(a)(25-23), 25.601[25-00], 25.603(a)(b)(c)(25-381, 25.605(a)(25.00], 25.607[25-23E 25.609(a)(b)125-001, 25.611(25-231 25.613(a)(b)(c)(25- 00j, 25.619[25-23], and 25.625(a)(b)(c)(25-231. ID. CERTIFICATION • Under autos* vested by direclico of the Admire:Oak( and in accordance with ccarlibons and limitations of app9mment Lamer 14 CFR Pad 113. data toned above and on adached sheets numbered _NM have tern twined in accordance vai established procedures and found to comply with appaceble requirements of the Ainverthioess Standards Listed. 0 Recommend approval of these data I (We) Therefore 0 Approve those data it $iGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATNE($) 12 DESIGNAGON NUMBERS(S) 13. CLASSIFICATION(S) Igtg ' 2- Paul Hedding DERT-410115-CE Structures FAA Form 8110-3 (03.10) SUPERSEDES PREVIOUS EDITION Fee Number H1274043 Page 10(1 SDNY_GM_02755101 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242023 EFTA01327141

SDNY_GM_02755102 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242024 EFTA01327142