A. MANUFACTURER IR SGG NAME ADDRESS B. PRODUCTION BASIS (Chick appitsbis Mm) PRODUCTION CERTIFICATE (Give proxkottim Akar° number) TYPE CERTIFICATE OTHER ft C GNE QUANTITY OF CERTIFICATES REQUIRED f OR OPERATING NEEDS DATE OF APPLICATION NAME AND TITLE (Prini of RPM SIGNATURE A DESCRIPTION OF AIRCRAFT REGISTERED OWNER ADDRESS BUILDER (Make) MODEL SERIAL NUMBER REGISTRATION MARK B. DESCRIPTION OF FIGHT CUSTOMER DEMONSTRATION FLIGHTS 0 (Check 11 morat4) FROM TO VIA DEPARTURE OATE DURATION C. CREW REQUIRED TO OPERATE THE AIRCRAFT AND ITS EOUIPME NT I PILOT I I CO-PILOT I I FLIGHT ENGINEER I I OTHER (Specify) D THE AIRCRAFT DOES NOT MEET THE APPLICABLE AIRWORTHINESS REQUIREMENTS AS FOLLOWS. E. THE FOLLOWING RESTRICTIONS ARE CONSIDERED NECESSARY FOR SAFE OPERATION eltadmmni dnecessory) F. CERTIFICATION - I Namby =try Meilen the recoteted =nor for his ageed)of Me aircraft described them: that the aiwah is mcistered math the Federal Atielign Adniftisvation in smorcteme mt. Tills 49 of the LISS Sates Code 44101 gun and applicable Federal Mallon Regattas. end that IM aircraft hes Wen =peeled end s safe for the NOV desated DATE NAME AND TITLE (NW Of RPM SIGNATURE A. Operating Limitations and MaikessnOmnpharce Wan 14 CFR Section 919. f4 APPlicable G. Steinman( of Colonnity. FAA Form 8130-9 (Mach when mugs* B. Cat Opening LerMations Attached 14 Foreign Almmtniness Gerthcaban for Import Airat (Attach when spired) C. bete Drarwma Phoiographa etc (Alfa, whin 0.9a0NO I D. Caren) Segni and BNence Wormalion Available In Aircraft I I. Previous Arworehmen Cantata Issued in Accordance With 14 CFR Section 21.191 (a) CAR (Onginet MaCNKO I I E Major Rest and Maralion. FAA Form 337 (Minh when inured) F. This inspecbon Recorded n Aumaft Records J Current Airworthiness Cenfcate Issued n Accordance Wen 14 CFR Seelien 21.181 (a) (Copy egeeMNO K Ufett-Spcs AraM Stmement of Compiarce. FAA Fran 8130-1S (AEW, when =NYS) FM Form 81304 (4111) Ap Previous Edabm Superseded Demonic Forms -PDF Page 2 Of 2 EFTA00011769

EFTA00011770

UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE 1 NATIONALITY AND REGISTRATION MARKS N493LX 2 MANUFACTURER AND MODEL Raytheon Aircraft Company 400A 3 AIRCRAFT SERIAL NUMBER RK-244 4 CATEGORY Transport 5 AUTHORITY AND BASIS FOR ISSUANCE This airworthiness certificate is issued pursuant to 49 U.S.C. § 44704 and certifies that, as of the date of issuance, ircraft to which issued has been inspected and found to conform to the type certificate therefor, to be in condon for safe o 'on, and has been shown to meet the requirements of the applicable comprehensive and detailed airworthiness code as sided by Annex 8 to the Convention on International Civil Aviation, except as noted herein. Exceptions: *None* 6 TERMS AND CONDITIONS Unless sooner surrendered, sus is effective as long a 91 of the Federal A DATE OF ISSUANC 12/29/2013 /d, revoked, or a termination date is otherwise established by the FAA, this ainvottiness certificate rts 21, 43, and DESIGNATION NUMBER DART833943GL Any alteration, reproduction, or misuse of this certificate may be punishable by a fine not exceeding $1,000 or imprisonment not exceeding 3 years or both. THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. EFTA00011771

S EFTA00011772

UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION • FEDERAL AVIATION ADMINISTRATION SPECIAL AIRWORTHINESS CERTIFICATE A CATEGORY/DESIGNATION EXPERIMENTAL I' - PURPOSE RESEADIAJELOPOKX i 0B MANU. NAME //b, A .,:`, il4,,1,/ - ADDRESS III OWAI)Vd1 FLIGHT FROM N j AY i,kiA / - 1`, TO il r`4, I , D N• 493L4 11;1 t ', , StRIALNO. RK- 244 BUILDER RaythemAihrifikpany 1.4 MODEL 4C0A E DATE OF ISSUANCE K..8) '&31 1 /0 .€XPIRY Jan 12.2014 OPERATING LIMITATIO,i' At,' 08';20B,igE PART OF THIS CERTIFICATE "D'ESIGNATION OR OFFICE NO. DART833943a Any alteratio •production or misuse of this cetficale may be punishable by a fine not exceeding $1,000 or imprison • 1 not exceeding 3 years, or both, THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT IN A9 i 'DANCE WITH APPLICABLE TITLE 14, CODE OF FEDERAL REGULATIONS (CFR). FAA FORM 8130.7 (07(041 SEE REVERSE SIDE NSW. 005240.6914000 EFTA00011773

A This airworthiness certificate is issued under the authority of Public Law 104.6, 49 United States Code (USC) 44704 and Title 14 Code of Federal Regulations (CFR). B The airworthiness certificate authorizes the manufacturer named on the reverse side to conduct production flight tests, and only production flight tests, of aircraft registered in his name, No person may conduct production :light tests under this certificate: (1) Carrying persons or properly for compensation or hire: and/or (2) Crying persons not essential to the purpose of the flight. This airworthiness certificate authorizes the flight specified on the reverse side for the purpose shown in Block A. This airworthiness certificate ceitifies that as of the date of issuance, the aircraft to which issued has been inspected and found to meet the requirements of the applicable CFR, The aircraft does not meet the requirements of the applicable comprehensive and detailed airworthiness code as provided by Annex 9 to the Convention On international Civil Aviation. No person may operate the aircraft described on the reverse side (1) except in accordance with the applicable CFR and in accordance with conditions and limitations which may be prescribed by the Administrator as part of this certificate; (2) over any foreign county without the special permission of that country. E Unless sooner surrendered, suspended, or revoked, this airworthiness certificate is effective for the duration and under the conditions prescribed in 14 CFR, Part 21, Section 21.181 or 21.217. EFTA00011774

RK 244 STC list (12-26-2013) Reference 8130-6: Application for Standard Airworthiness Certificate Transport Category, dated December 26, 2013 Reference section ill 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) EFTA00011775

EFTA00011776

Cleveland. Ohio 44143 December 26, 2013 Nextant Aeros ace, LLC Cleveland, Ohio 44143 Attention: Re: RK-244 — Agent Authorization To whom it may concern: aLti 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 FM 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: Ma_ Vice President, Administration & Contracts Notary's Officio" &Ina-Cure Siam ana subscx tbez1 4-o Pt -141 do. 2 G, ckC bef-,e.,nt•er O4 2_01 3 bl EFTA00011777

EFTA00011778

EFTA00011779

I EFTA00011780

0 MAJOR REPAIR AND ALTERATION US Mammon a Riff', Apotral ovs Ne 2l mono itt3orzoci7 Electronic Trackin Number 9 Trarapanalkin (Airframe, Powerplant,Propeller, or Appliance) For FAA Use Only Fedni Aviation AchninIstratreri INSTRUCTIONS: Pant or type all entries. See FAR 43.9. FAR 43 Appendix 8. and AC 429-1 (or subsequent revision thereof) for instructors and disposition of this form. This report is required by law (49 U.S.C. 1421). Faiture to report can result in a civil penalty not to exceed 51.000 for each such violation (Section 901 Federal Aviation Act 1955) 1. Aircraft Nationality and Registration Mark N493LX Serial No RK-244 Make Raytheon Aircraft Company Model 400A Soles 2. Owner Name (As shown on registration certificate) Flight Options .LLC Address (As shown on registration certificate) Address Cry Richmond Heights state. OH Zip 44143-1453 co.ty USA 3. For FAA Use Only 4. Typo 5. Unit Identification Repair Alteration Unit Make Model Senal Number 0 ►1 AIRFRAME (As descnbect in gem 1 above) III a P0WERPLANT K a PROPELLER K O APPLIANCE Type lilanyfanser 6. Conformity Statement A. Agency's Name and Address 8 Knd of Agency Nerve Nextant Aerospace Address City Cleveland stn. OH Zip 44143-1453 cony USA O u.S. Certificated Mechanic O 'Manufacturer O Foreign Centticated Mechanic C. Certificate No. 0 Certificated Repair Station CRS # 25NR667B O Certificated Maintenance Organization D. I candy that the repair smiler alteration made to the unit(s) Identiaed in item 5 above and described on the reverse or attachments hereto have been made n accordance with the requiements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of ray knowledge. Extended range fuel per 14 CFR Part 43 Apo. Et 11 05/30/2013 7. Approval for Return to Service Pursuant to the authority given persons speared ['Sow, the unit identified in item 5 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is El APPROVED K REJECTED BY FAA Fit Standards Inspector Manufacturer Maintenance Organization [Person Approved by Canadian Department of Transport FAA Designee X Repair Station Inspection Au •rization i other (SPearY) Certificate or Designation No. CRS it 25NR667B 05/30/2013 FAA Form 337 (1006) EFTA00011781

EFTA00011782

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations fo assure continued conformity with the applicable airworthiness requirements 8. Description of Work Accomplished (If more space is required, attach additional sheets. !den* with aircraft nationality and registration mark and date work completed) N493LX 05/30/2013 Nationality and Registration Mark Date Part I of 3 The Following Equipment was removed along with Associated Hardware. 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-SSE 622-9336-400 Attitude/Heading Computer AHC-85E 622-9336-400 Attitude/Heading Computer SDU-6408 622-9735-001 Sensor Display Unit SDU-6408 622-9735-001 Sensor Display Unit DCP-5000 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 DBU-4100 822-0014-002 Data Base Unit DAU-650 622-9344-101 Data Acquisition Unit SDD-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 !APS Power Card GPS•4000 822-0931-003 GPS Receiver Mounts 622-9430-002 EFD /MFD Mounts EFB Electronic Flight Bag Mounting El Additional Sheets Are Attached Form 337 (10-06) EFTA00011783

EFTA00011784

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality 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" ins) 6.5 60.83 ECU-3000 822-1200.998 File Server Unit (1st IRS) 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 AF0-3010E 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 PS-835D 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 Options Configuration Module. OCM-4100 822-1463-228 0.30 57.5 WAAS/LPV Options Configuration Module. OCM-4100 822-1463.228 WAASAPV 0.30 57.5 Additional Sheets Are Attached Form 337 (10.06) EFTA00011785

EFTA00011786

NOTICE Weight and balance or operating limitation changes shell be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality 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 CSU-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 AHC-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-42-12-8B-E0Y47 AUX BATT (1/2) Annunciator 0.05 88.0 Annunciator (2) Led-40-18-88-E0Y4S Pull Up/ Terrain Annunciator 0.05 88.0 Annunciator 2-F840231 Terrain Inhibit/ Terrain Fail 0.05 88.0 In Accordance with SIC ST10959SC. 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 120-768 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 PAW 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. K Additional Sheets Are Attached Form 337 (10.06) EFTA00011787

EFTA00011788

*atm of 4\ nterica department of eafrartsportation Ifeberal (Ablation glibministration $upplerttental Type Certificate .121, an.1.456%4 ACIalate ST10959SC Nextant Aeros ace LLC Richmond Heights, OH 44143 arA4A 44,a; donjs414,A 4ye diainfr44 /40avnneediclavle /.4 dovialani azulawelaivo rRJ rataSewitereen nwv/4i airnaam trytabetneaht marl 25 944 Federal Aviation Jigewana.J. (See Pages 3 and 4 for complete certification basis.) eini‘sezeilierka• 4,eg;n4jetatin./YimaGe Al 6SW ../44. Hawker Beechcraft Corp. ,.#r61. 400A gieW.)7/w tyriffifs 91474 KZ/7r Installation of Rockwell Collins Pro Line 21 Electronic Flight Instrument System (EMS) with Rockwell Collins FMS-6100, Localizer Performance with Vertical Guidance (LPV) approach capability and Universal Avionics Systems Company (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. Sintelalsiinss andriaisiast: 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 al 5D 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. cete94'eare and 4 invites? a/a 0444' Ai a Au) wiaatvs,.....4.4 S'ent t...41..vtentseired wt.itar.a.‘ei vvend re a keetaisaloin cotto tweserwe:m ma < 4. 4A .4144,4x4,47 4v r724 .9;eArat lenearaectleM gia.4./yrrearairen June 26, 2008 g4.4. elt;vacar..t October 19.2009 glao freV.1.31/..1 afflealb2(' September 26, 2011; April 05, 2012 Manager, Systems and Flight Test Branch Chicago Aircraft Cenitication Office (Tirle) Any .notation or (big JS poroshata., OY . floe of not ovcoodino .1.J.O. or Joprison.0.1 .0C •mcoOdinq 1 year., or Opt.. Fmk rot.. 4110-2110.641 PAGE I of 4 P&G'S This NY be trans:oared Ja accorderce .Jco fa 21.42. EFTA00011789

EFTA00011790

jfintieb Stales of ,Aintrita !el:ointment of 2granisportation - ebernt Ablation ,2\ botinisfration Supplemental `Type Tertifirate (Cartiinuation $ijeet) Aa,724/e ST I 0959SC Pak o>44.saonoo• October 19, 2009 Date Amended: September 26, 2011; April 05, 2012 gleadeal OesetWAISAYIJ 7ISVialeAr k 4) For aircraft equipped with Williams FJ44-3AP Engines, those engines must be installed under STC ST0237ILA. 5) For aircraft equipped with Williams FJ44-3AP 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 RK-I 17 and RK-I 19 thru RK-I39, Hawker Beechcraft Service Bulletin No. 34-3431. RK-118, RIC-140 thru RK-224, Hawker Beechcraft Service Bulletin Nos. 34-3228 and 34-3431. RK-225 thru RK-299, Hawker Beechcraft Service Bulletin No. 34-3431. RK-300 and after as original equipped from Hawker Beechcraft. 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. tifeaeAaten Suit: Based on 14 CFR §p 1.115 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 Al 6SW 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 A I6SW and §§ 14 CFR Part 25 as shown on page 4 of 4 of this STC. • Any alser [son of chis cerCIfjcace is pvnishable 0y 4 Zito or hot eeeoedin0 01.000. or inpeJsohosoc not extooding J years. or both. FAA ram IIIO-0.1110-PII PACE 3 of 4 PAGES This ces(iIi4Ate *my be Cron ***** SO' An sccordance .lth FAA L.U. EFTA00011791

I EFTA00011792

!lulled *alto of /mtrica pepartment of Eransportatiott - geberal jAbiation cAbministration Supplemental Igp Tertificate ((Continuation Ace° Paie4 rAvacteres October 19. 2009 Date Amended: September 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 (EFIS) with Rockwell Collins FMS-6100 modification was determined to be TCDS A I6SW and the following later regulations: Amdt.[24-4) 25.771 (Le) Amdt(25.23) 25.301; 25.303: 25.581; 25.607: 25.611. 25.773 (a)(1)(1)(d) Amdt.(25.38J 25.1309 (eXtiXe)(cXeNn: 25.1322 Amdi.)25-401 25.901 (b)(1Xi); 25.1549 (1)(bXe) Amdt.I25-41) 25.1321 (aX6)(e)(e): 25.1131;25.1333 Amdt.[25-421 Amdt.125-46) Amdt.(25.54) Amdl.(25.72J Amdt.125.801 25.1501 25.603; 25.605: 25.613; 25.1529 25.307;25.571, 25.1307 25.1316 25.1329(N (OK): 25.1351 (a)(1)(d): 25.1381; 25.1521 (a)(c); 25.1543(6); 25.1581: 25.1563 (a) Am& (25-86) Andt[25.90J Amdt.12541) Amdl.125-1021 Amdt.(25-105) 25.305 25.1303 25.561 25.981 (a)(b) 25.1585(a) Amdt.(25.108J Arndt 125-1091 Amdi.(25-1 131 Amdt (25-122) Amdl.(25.123J 25.1325 (d) 25.1323 (aX060 25.869 ('X4):25.1431 25.1317 (a)(bXe) 25.1353 (aXc) 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 Collins Proline 21 FMS-6100 with LPV Approach enabled and UASC TAWS was determined to be TCDS A I6SW and the following later regulations: Amdt (Original) 25.601, 25.605, 25.609, 25.613. 25.1301, 25.1357, 25.1381. 25.1525, 25.1541, 15.1581 Amdt.(24-4) 25.771 (a) Amdt.(2S-23) 25.301; 25.303; 25.305, 25.307, 25.561(c); 25.607; 25.611, 25.1307 Amdi.(25.38) 25.603, 25.1322, 25.1583(e) Amdl [25.40) 25.1585 (a) Amdt.(25•41) Amdt.(25-42) Amdt.(25-46) Amdt(25.54) Amdt.(25-72) 25.1309 (a)(b)(c)(6)(eXg) 25.1501 25.777(a0(c) 25.1529 25.869(a)(1) 25.1351 (a)(1) Amdt.(25-102) Amdt.[25-1 13) Amdt.[25.123] 25.98 1(a)(b) 25.1431(a) 25.1153 (aXe) - END - A y elu at on of C J* cort• Mktg is pimp& 'DM by s fine at not *Ambling $1.000, or Jowlsoewnt tun •xcentiao 3 yens, or Ugh. !AA 400.4 $110.1-1110.0!1 IPla 4 of 0 MASS This c•rt4 ('care 'Ay be transferred in ACCOt011AC• with FAA 21.4/. EFTA00011793

EFTA00011794

0 MAJOR REPAIR AND ALTERATION u.SOccrartment or (Airframe, Powerplant, Propeller, or Appliance) Tcansporodon ROHR Aviation A/mnions:in Form Approved OMB No. 21200720 itranwr Electronic Tracking Number For FAA Use Only INSTRUCTIONS: Pnnt or type all entries. See FAR 43.9, FAR 43 Appendix B. and AC 43.91 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not 10 exceed 51.000 for each such violation (Section 901 Federal Aviation Act 1958) 1. Alrcraft Nationality and Registration Mark N493LX Serial No. RK 244 Make Raytheon Aircraft Company Model 400A Series 2. Owner Name (As shown on registration cemecate) Flight Options .LLC Address (As shown on registration certificate) mo ss ra city Richmond Heights slew OH zip 44143-1453 canny USA 3. For FAA Use Only 4. Type 5. Unit Identification Repair Alteration Unit Make Model Serial Number El El AIRFRAME (As descnbed in Item I ahove) K O POWERPLANT 0 K PROPELLER 0 K APPLIANCE Typo manitock_tor G. Conformity Statement A. Agency's Name and Address B. Kind of Agency name Nextant Aerospace AROMA city Cleveland slaw. OH Zip 44143-1453 campy USA O U.S. Certificated Mechanic O1 Manufacturer O Foreign Certificated Mechanic C. Certificate No C Certificated Repair Station CRS # 25NR667B O Certificated Maintenance organization O. I certify that the repair and/or alteration made to the unit(s) identified in tern 5 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Extended range fuel per 10 CFR Part 43 App. B 0 Signature/Date of Authorized Individ 05/30/2013 7. Approval for Return to Service Pursuant to the authority given persons speofied below, the unit identified in item 5 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is El APPROVED El REJECTED BY FAA Flt standards inspector Manufacturer Maintenance Organization I Person Approved by Canadian Department of Transport FAA Designee X Repair Station Inspection Autftrization Other Specify) Certificate or Designation No. CRS # 25NR667B Signature/Date of Authorized Individual 05/30/2013 FAA Form 337 (10.06) EFTA00011795

EFTA00011796

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) N493LX Nationality and Registration Mack Nextant Aerospace Completed STC tt ST02371LA Removed Pratt and Whitney JT15D-5 Series Engines . 05/30/2013 Date Installed the Williams International FJ44-3AP Engines with Full FADEC and Associated Systems in accordance with Nextant Aerospace MDL -NXT-001 Rev IR Dated 08/22/2011 or later FAA approved revisions, and FAA Approved AFM Supplement NXT-1-AFMS Rev IR dated 9/15/2011 of later FAA Approved revisions. Installed Left Engine Part Number. 111000-202 Serial No. 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 OPS checks IAW Ground Test Plan 373-00-0024 Rev F. End K Additional Sheets Are Attached FAA Form 337 (ro.os) EFTA00011797

EFTA00011798

}lidkit Alnico erAciericii Pepin. Intent of ZIrmispectrdinit - jliederid cAbintion i*ittriiriotration $upplemental Tuve Certifiaxte ACeenz4/, ST02371LA Yt, rfiriVcale 'Akira Nextant Ados ace LLC Richmond Heights, Ohio 44143 cre3/4 ) /Lair liar a. /4 Ow devrAfr alfriSearndastenal dowlakiw cerrelconait4J. erreArei reet9freheemorniter4 riecemitarthew rwatimervai tegnarl 25 * teen ..greverea47.4iw -94,144*."0. *Certification basis is set forth on TCDS A l6SW and continuation sheets 3 and 4. ifgviriteaordra' *to WreiViartrivi‘rcero.• A 1 GSW Hawker Beechcraft 400A Nvo*afeiis ifira Our Meir Replacement of Pratt &, Whitney 5D-5 series engine with Williams International FJ44-3AP engine (TCDS E3GL) with Full Authority Digital Engine Control (FADEC) and associated systems, in accordance with Nextant Aerospace Master Drawing List No.: MDL-NXT-001, Revision 1R dated 8/22/2011, or later FAA approved revisions and FAA Approved Airplane Flight Manual Supplement, NXTI-AFMS, Rev IR, dated September 15, 2011 or later FAA approved revisions. Nextant Aerospace, LLC Instructions for Continued Airworthiness document NXT1-ICA, Revision IR, or later FAA accepted revisions must be provided with this STC. ..Weetheaivto rriorteewrieliw.i: 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) gai ereVetakt ecoriall.irwrevar ata ele.it;aA onewoorararre-evnertia At Oat/the JItneerteleredJaOrneed retwevie.v. a. knieririzaiva Abe Ai careciari evireteddevel. ./Mteire:OrrIcv, eyeafei Rielerrat6thierleiva ..egedieritealredicva fkia,/eryacre4;v:. March 24, 2008 ame/kwavien.. September 27, 2011 14. raterneleil.- &itroit Manager, Propulsion Branch Los Angeles Aircraft Certification Office (Time) Any alteration of this atiffrate it panisfiable by a fine of no: excetelloyi $1,004 or iiniultonment not taccediv 3 years, or Gotta YM rem 0110.2(10.4i) Pegs r of 4 Vic certificate nay de trainfeired moat:met n1(0)1(.4.21.47 EFTA00011799

EFTA00011800

INSTRUCTIONS: The transfer endorsement below may be used to notify the appropriate FAA Regional Office of the transfer of this Supplemental Type 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 Paine of transferee) Oteritrss of transfer) tecum(vr an! itrrei) (ail Sr•14 da Zip rile) from (name ofgrantor)(Pr(nt or we), (fiffiress of grantot) OrlimbentnIscrert) tic% Seal an d Zip roe) Extent of Authority (if licensing agreement): Date of Transfer: Signature of grantor an MO Pagc2 or 4 EFTA00011801

EFTA00011802

puttee Plates WI Anterior .Bcpairtnient of Zikantepartation - lfebernt Abintiou Pt bmirtistrtttiorr $upplartentai Zgin Tertifirate (ffinutinuntion $11291) Afeeenie/< ST02371LA -2reintrakiinr analifoncerdeanix (conitnan(1 • Nextant Aerospace, LLC, "Installation of Rockwell Collins Pro Line 21," Amended STC ST10959SC, dated September 26, 2011 or later FAA approved revisions is required as part of this alteration. • The new Vince and Vmcg values arc 94 KIAS and 93 K1AS 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 Wee49catkew,....fiani The certification basis for this modification is as follows: The original certification basis for the Hawker Beecheraft Model 400A airplanes identified on TCDS AI6SW, Revision 26, dated March 17, 2010: Part 25 of the Federal Aviation Regulations effective February 1, 1965, as amended by 25.1 through 25.40, plus §§ 25.1335, 25.135I(d), 25.1353(c)(5), and 25.1447 of Amendment 25.41; §§ 25.29, 25.255, and 25.1353(0(6) of Amendment 25.42; and §§ 25.361(b) and 25.132900 of Amendment 25.46. Part 36 of the Federal Aviation Regulations effective December 1, 1969, as amended by 36-1 through 36-17; SPAR 27 effective February 1, 1974, as amended by 27-I through 27-5: and Special Conditions No. 25-ANM-32 dated February 22, 1990 (High Altitude Operation at 45,000 feet), and Special Conditions No. 25-ANM-33 dated June 18, 1990 (Lightning and Radio Frequency Energy Protection). (See NOTE 12) Equivalent Safety Items: (I) Out.of-trim characteristics § 25.255 (2) Pilot compartment view § 25.773(b)(2) (3) Passenger compartment door § 25.813(c) (4) Emergency exit marking §§25.811(d)(1) 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 11— Flight: 25.207(25-121), 25.255(25.42) Subpart C Structure: 25.571 (25-96) pay dimwit of the attfwan is pialisha64 by a fine of not cowling $1,000, or neprinament not aim% 3 pan, or boa PM Pons 0310.2110-6I) sego ) of 4 ?hit certificate nay ds traurfirra f in anonfann with TRIL21.47. EFTA00011803

EFTA00011804

palish Stoles 01 A tunics Peparfutent of Zrattoporintion - jliehertti cAbintiott Jtlbritittistrrttirm $upplartental Zglat Tertifiatte (clantinuation $beet) ./rande.# ST02371LA WeriaAniaimegade:s iconloaraesed Subpart 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(25400), 25.1093(25-72, 25.1103(25.46), 25.1141(25-115), 25.1143(25-57), 25.1163(25-57), 25.1165(25-72), 25.1181(25-115), 25.1183(25-101), 25.1185(25-94), 25.1189(25-57), 25.1195(25.46), 25.1203(25-123), 25.1207(25.46). Subpart F —Equipment: 25.1301(25-123), 25.1305(25-115), 25.1307(25-72), 25.1309(25-123), 25.1316(25-80), 25.1317(25-122), 25.1321(25-41), 25.1331(25-41), 25.1351(25-72), 25.1353(25-123), 25.1357(25-123), 25.1381(25-72), 25.1431(25-113), 25.1438(25-41), Subpart G— Operating 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 H- Electrical Wiring interconnection Systems (EWIS): 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(25423), 25.1717(25-123), 25.1719(25-123), 25.1721(25-123), 25.1723(25423), 25.1725(25-123), 25.1727(25-123), 25.1729(25-123), 25.1731(25-123), 25.1733(25-123). 14 CFR Part 34 (34-3): 34.11 14 CFR Part 36 (36-28): 36.1-36.7, 36.101--36105, 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. NXTI-EA-007 Rcv A dated 8/24/11 or later FAA approved revisions. -END- Any iteration of this artyieate is punishable by a fine of not evettfing ii,00cs or implisonntent not mere% 3 years, or both PM Pons 1110-2(10-40 Pogo 4 at 4 This syndicate may be transtetriin acrodance nib TAR,21.47. EFTA00011805

EFTA00011806

0 MAJOR REPAIR AND ALTERATION u S oessani or (Airframe, Powerplant,Propeller, or Appliance) Tissoananon Paws minion ministration Font amens 0m8 No 2t204:020 it nor2037 Electronic Tracking Number For FAA Um Only INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B. and AC 43 9.1 (or subsequent revision thereof) for instructions and dispositio of this form This report is required by law (49 V.S.C. 1421). Failure to report can result in a civil penalty not to exceed 51.000 for each such 'elation (Section 901 Federal Aviation Ad 1958) 1. Aircraft Nationality and Registration Mark N493LX Serial No. RK 244 Make Raytheon Aircraft Company Model 400A Senes 2. Owner Name (As ShOwn on tegistrabOn certificate) Flight Options .LLC Address (As shown on registration certificate) Metes, City Richmond Heinfits swe.OH zip 44143-1453 coulee USA 3. For FAA Use Only 4. Type S. Unit Identification Repair PAeratiOn Unit Make Mood Serial Number El El AIRFRAME (As described in Item I above) • O POWERPLANT ID O PROPELLER O O APPLIANCE Typo Manufacturer 6. Conformity Statement A. Agency's Name and Address B K no of Agency Nara Nextant Aerospace moms cry Cleveland slate OH zo 44143-1453 Country USA 0 U.S. Certificated Mechanic 0 Manufacturer 0 Foreign Certificated Mechanic C. Certificate No. El Certificated Repair Station CRS # 25NR667B 0 Certificated Maintenance Organization D. I certify that Ihe repair and/or allerabon made to the unit(s) identified in item 5 above and described on the reverse or attachments hereto have been made In accordance with the requirements of Part 43 of the U S Federal Aviation Regalabons and that the information furnished herein is true and correct to the best of my knowledge - Extended range fuel Per 14 CFR Part 43 App. B MI 2/29/2013 7. Approval for Return t lett / Pursuant to the authority given persons specified below, the unit identified Administrator of the Federal Aviation Administration and is .. in item 5 was inspected in the manner prescribed by the APPROVED El REJECTED FAA Flt Standards Inspector Manufacturer Maintenance Organization i Person ApprOved by Canadian Department of Transport BY Certificate Designation CRS or # 25NR667B FAA Designee No. X Repair Station Inspection Authorization Other (SPecif0 /29/2013 FAA Form 337 (teat) EFTA00011807

EFTA00011808

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed N493LX Nationality and Registration Math 12/29/2013 Date Installed the following In-Flight 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 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 DB 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 012004 Revision E, dated March 2010 or later applicable revision Aircell 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 10/9/2013 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 Additional Sheets Are Attached FAA Form 337 (io.os) EFTA00011809

• EFTA00011810

Vniteb 'take of ;America gleporiment of ligrattoportation geberal cMialion cabrninistration $upplementat Type Tertificate Actinetede4 ST03960AT .71;5 fernAvA' 44"a Nextant Aerospace LLC West Palm Beach, FL 33406 reehAm ten/ee rieenfe 4, Or /me eAlikes/9- dravethyyreetafe/ end at, etw'rerhiw4 Awe/ erna>;v7J acyrise se4 VerseAtif "wen ineet zee felivideiVtinkl esyntinview/3 r/ !Arne 25 Vier Federal Aviation .92,1”42vawa. Sfironetrity4n1- • , ;fie KvOrrelo •AC0,6- AI 6SW ..4160A Hawker Beechcraft Corporation Sea: 400A fiskle.s0/eisss el .gs>ir iiSlsises War.' Installation of Rockwell Collins Venue In-Flight Entertainment(1FE), Aircell Axxess Cabin II Iridium Phone and High Speed Internet System with Wireless Local Area Network (W LAN) 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. ,9ramArhiv., 4welfenaiv,J.• 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. ..We3 ovietrain twee 'Or ay/Are/49 44/et avtii nt; etzyteretet.Ateeentteas 4. *Or/ foyhl Jitemfeeireet. Jeninena e n rime re re beziniiseekvs etr* hl reeete,:le estireifiVergy /4 .4 1,4,,,:viderv/re r//6 ....XsArset fleas/4w 0.4 July 28, 2012 -eget rAwerewee March 22, 2012 fate re/:waved: ewe sowitiveAv6.- Atlanta Aircraft Certification Office My sitoraclon of this corcilicsfe is ounissablo Dye lino of hoc osensitno 12,000, or Imprisonment not excee0ing J ye***, or moth. VAL fwm 8110-2(10-fel MGt I of 1 YMCAS This cora/leaf* se/ N csonstfrzoii In se,ezdan.• mach PAR 21.4.. EFTA00011811

EFTA00011812

VolItb *tato of America pepartnunt of transportation - Xeherni Pkbintion ptbministrntion $upptententnl Zype Certificate (Tantinuation $beet) tfriteregett 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, 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 (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. DBII05003, 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 I 108018, 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. Any alteration of this ooze ion* purdahs)) • by • flea at net trend nq 11,000, or ltprlsonwent not arcabffir4 l years, or both. MA it 1110-2-1(10-49) PAGE 2 or 3 PAGES This entificat• way b transforrect in •ccoraanc• with PAR 22.17. EFTA00011813

EFTA00011814

Alates of ,America peoartment of grzinsportation - geberat Ablation Administration $upplemental `Type Tertificate (Tantirtuation Sheet) A rtaidede ST03960AT enr/Veleedava The Certification Basis for this installation is per Type Certificate Data Sheet Al6SW 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(e)(6) 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 [25.541 _ [25.123] [25-1231 [25-113] [25-541 (1 Indicates amendmen level Any alt aaaaa on or this corellicett is punishable by • Tins of not enabling 53,000, Or laprisonnent not intending 1 years, or both. FAA EOM 0110-2-2(20-01 AWL 3 of 3 PAGES This certificate nay be transfersest in accordance with FAR 11.4r. EFTA00011815

MS EFTA00011816

0 MAJOR REPAIR AND ALTERATION u s orsemieni al (Airframe, Powerplant, Propeller, or Appliance) hasp:dam F000.11 AARIOA AdwANtratlen ram Append ore tie 21204020 11/30,2t03 Elect/oat Trackirg Number For FAA Use Only INSTRUCTIONS: RIM of type all entries. See FAR 43.9, FAR 43 Appendix B. and AC 43.9.1 (or subsequent revision thereof) for Instructions and disposition of this form. This report is required by law (40 U.S.C. 1424 Failure to report can result Mach& penalty not to exceed 61800 for each such violation (Section 901 Federal Aviation Act 1958) I. Aircraft NationaRy and Registration Mark N493LX Serial No. RK244 Make Raytheon Aircraft Company Model 400A Series 2. Owner Name (As shown on registration certificate) Flight Options, LLC Address (As shown on registration cerfifiCate) cityHichmOnd Heights sue:Ohio 4944143-1453 ciairoa.8 3. For FAA Use Only 4. Type 6. Unit IdeMlfic alien Repel/ Alteration Und Make Model Serial Number El el AIRFRAME (As describer:1ln ken l above) 0 ii POWERPLANT 0 El PROPELLER O D APPLIANCE rye. Nara ...over 6. Conformity Statement A. Agency's Name and Address B. KIM of Agency Na Avi _ i n Aa&es cityCleveland swoOhio CI U.S. Certificated Mechanic 0 IManufacturer 0 Foreign Certificated Mechanic C. Certificate No. 0 Certificated Repair Station CRS#WC7R34OJ zo44135 courevOnited States CI Certificated Maintenance Organization D. I certify that the repak andiOI alteration made to the unit(s) Identified in item 5 above and described on the rover c or Mtn:laments hereto have been made In accordance with the requirements of Pen 43 of the U.S. Federal Aviation Regulations and that the information furnished heroin Is true and correct to the best of my knowledge. Extended range fuel per 14 CFR Part 43 App. 8 ill Date: December 30, 2013 Service Pursuant to the authority given persons spooned below, the unit Idea tn item 6 W3S inspected In the manner presorted by the Administrator of the Federal Aviation Administration end is El APPROVED II REJECTED BY FM Fa Standards Inspector Manufacturer IAMMenance Organization I Person Approved by Canadian Department of Transport FM Designee X Repair Station Inspection Authorization other moon CerOlicate or CRSHWC7R346J Onlonolion No. SignauxerDate el Date: December 30 , 2013 FAA Form 337 node EFTA00011817

EFTA00011818

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft reCOM. An alteration must be compatible will, all previous alterations to assure continued conlomety with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. identify with eircrak nationality and registration mark and dale work completed) N493LX Nationality and Registration Mark 12/30/2013 Dale ACCOMPLISHED INTERIOR REFURBISHMENT/MODIFICATION AND 3 PLACE DIVAN INSTALLATION THE FOLLOWING AIRCRAFT INTERIOR ITEMS HAVE BEEN REFURBISHED: RepalMed, recovered control columns with Mane Bed( Leather Accordance with BeedVel 400A AMM 20-70.00-701. 25.0040-001 Removed and Replaced Glare shield and Eyebrow panel material with Matte Sack Leather In Accordance with Becch)et 400A AMM 20-60-00.201. Removed and Replaced Cockpit Sidewal malarial MU Mane Black Leather In Accordance with Beet:lel 400A AMM 20.80-00.201. Removed and replaced Pitc1 Seal Pad Number TA W II00PM000I Serial Number 82. Foam and recovered with Garen Sheepskin Oak and Excel Cappucdno Leather. Removed and replaced Co-Pilot Seat Part Number TABH100CM00.01 Serial Number 248, Foam and recovered w.thCarrell Sheepskin Oak and Excell Cappuccino Leather. Removed and Replaced Loll Hand #4 Passenger Seal Pad Number 2524.014(-530A) Serial Number 990719.4 Foam and recovered with Townsend Leather (Heritage Brown) Removed and replaced Right Hand #5 Passenger Seal Part Number 2524.014(-530B) Serial Number 990426-7 Foam and recovered with Townsend Leatherpleriinge Brown) Removed arid Replaced Left Hand 03 Passenger Seal Pan Number 2524.014(5306)Sedal Number 03061845 Foam and recovered with Townsend Leather (Heritage Brown) Removed and replaced Right Hand S7 Passenger Seat Pan Number 2524-014(530A) Serial Number 030708.2 Foam and recovered with Townsend Leather (Heritage Brown) DIE FOLLOWING MANUALS AND APPROVED DATA HAVE OLEN UTILIZED FOR OASIS OF REFURBISHMENT. Skendla Flammability Test S254978 as approved by FM t)EIT Jane Mersa* (DERY 832780-CE) on FM form 8110-3 dated 4/23/2013 Flame Out Elam/1180'4y Test 4351 as approved by FM DER Herb Reed II (DERT-230293.CE) on FM Form 8110-3 dated 12/23/2013. Skandla Flammability Test Report IP 22081 Rev A as approved by FM DER and Faberslein( DERY-832780-CE) on FM Form 8110-3 dated 05/02/2013. Three Place Divan installation: Installed (3) ptace divan part Number 32.03913(MOVOT123.K02 S/N 003702 In Accordance Men Aviation Fabricators SIC/ STOI572W1 and Skandia Rammila test report 5254978 per Jane Bibeisleln FM DER (DERV-832780-CE) dated 4/23.2013 THE FOLLOWING INTERIOR ITEMS HAVE BEEN MODIFIED: UR Golly Assy, RM Galley May, Divan Amy. LM Galley Assy and install per Deka G drawing DGD-GW1.101 Rev 0, DGD-CAOI -101 E0 E- t. LfH Galley Install DGO-CA01-501 Rev EO A-1. DGOCA0t-501 Rev IR as approved on FAA formal 10-3 pm FAA DER Donald Geese* (DERT-750135-SW) dated March 25 2013. RA4 Galley Assy and Install per Della G drawings DGD-CA02-101 Rev B. OGLICA02-501 Rev IR as approved on FM /OM 8110-3 by FM DER Donald Geese* (DERT-750135-SW) dated March 25. 2013 Divan Assy per Delta G drawings OCID-CA09-101 Rev C and DGD-CA09-101 E0 0-1 as approved on FM form 8110.3 per FM DER Donald Giuospk (DERT 750135-SW) dated March 25. 2013, Month Kit Sfdewa0 esay &arena 2553-0038 RCN C. Bonner sldeledge any *away 25324)032 Rev C Bonner Ka Foldout Table assy drawings 2553.0041 Rev C and 2553-0040 Rev EL Bonner XTI finer Kit Ina drawing 2553-0037 Rev C as approved on FAA form 8110.3 per Stephen Formes DERT-230238-CE dated Dec 20, 2013. INSTRUCTIONS FOR CONTINUEDAIRWORTHINESS. THE REMOVAL OF THE INTERIOR IS ON THE CONDITION OF FAILURE. THERE ARE NO ADDITIONAL INSPECTIONS REQUIRED. CONTINUE TO INSPECT JAW MANUFACTURERS MBA, SRIL OR CMM AS APPLICABLE AIRCRAFT EQUIPMENT LIST AND WEIGHT AND BALANCE WERE UPDATED BY THE CUSTOMER -END--- O Additional Sheets Are Attached FAA Form 337 (1008) EFTA00011819

EFTA00011820

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE Dec 26, 2013 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Beeehcraft Corporation MODEL 400A TYPE (Airplane. Radio. Helicopter, eta) AIRPLANE NAME O APPLICANT NEXTANT Aerospace Cleveland OH. LIST OF DATA IDENTIFICAITON TITLE REPORT: BEECHJET 400A INTERIOR STRUCTURAL SUBSTANTIATION BEECHJET 400A XTI LINER KIT INSTL. Beechjet 400A, Aircraft Serial No. RK-244 Certification Bases for this aircraft modification is per Type Certificate Number A I GSW Revision 28 dated April 12,2013 RKG3282 Rev. IR, 8-28-2013 2553-0037 Rev C, dated 8-30-2013 PURPOSE OF DATA DESCRIBE AND SHOW VERIFICATIONS FOR NEXTANT INTERIOR INSTALLATION ON BEECHJET 400A, AIRCRAFT SERIAL NO. RK-244 APPLICABLE REQUIREMENTS ( List spec* sections) 14 CFR Part 25 §.301, 303, 305, 307a), 365, 561, 571,601, 603, 605, 609, 613 CERTIFICATION - Under authority of appointment under Pan 183 of have been vested by direction of the Administrator and in accordance with conditions the 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 these data and limitations numbered with applicable requirements of the Federal Aviation I 01413 Therefore O Recommend 0 SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) DERT-230238-CE STRUCTURES AND DAMAGE TOLERANCE FAA Form 8110-3 OO0) SUPERSEDES PREVIOUS EDITOR CPO 961.613 EFTA00011821

EFTA00011822

le MAJOR REPAIR AND ALTERATION NS Droorintro of (Airframe, Powerplant,Propeller, or Appliance) Trampoutto Fees Aviation Administraton FamAprons:1 OMB No. 2120-0020 11/30/8:07 Electronic Tracking Number For FAA Use Only INSTRUCTIONS: Prialor type all entries. See FAR 43.9. FAR 43 Appendix 8. and AC 43.9-1 (or subsequent revision (recto') for instructions and disposition of this form. This report is required Dy taw (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed 91,000 for each such violation (Section 901 Federal Aviation Act 1958) 1. Aircraft Nationality and Registration Ma* N493LX Serial 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 registration certificate) 00°t°'° coy Richmond Heights sets OH re 44143-145 cater USA 3. For FAA Use Only 4. Type 5. U it Identification Repair Minden Unit Make Model Serial Number I gii AIRFRAME (As described in Item 1 above) o POVVERPIANT 0 PROPELLER n ii APPLIANCE ;pit MonufrOuree 6. Conformity Statement A. Agencys Name and Address B. Knd of Agency Norte Nextant Aerospace Andrea City Cleveland see. OH Ze 44143-1453 country USA O U.S. Certificated Mechanic Cl /Manufacturer O Foreign Certificated Mechanic C. Certificate No. SI Certificated Repair Station CRS # 25NR667B O Certificated Maintenance Organization D. I certify that the repair have been made in accordance furnished herein is true Extended range fuel per 10 CFR Part 43 App. B anclior and MI alteration made to the unit(s) identi ed in item 5 above and described on the reverse or attachments hereto with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the Information correct to the best of my knowledge. 12/29/2013 prove or'eum o / Pursuant to the authority given persons specified below, the unit Administrator of the Federal Aviation Administration and is idenUSed r j in dem 5 was inspected in the manner presort ed by the APPROVED K REJECTED FAA Flt Standards Inspector Manufacturer Maintenance Or I Person Approved by Canadian oepanment of Transposed BY FAA Designee X Repair Station Inspection Authorization Other (Specify) Certificate or Designation No. 2129/2013 CRS # 25NR667B FAA Form 337 (10.06) EFTA00011823

EFTA00011824

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations fo assure continued conformity with the applicable airworthiness requirements. 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 Nationality and Registration Mark 12/29/2013 Date Installed the following In-Flight Entertainment System in accordance with STC # ST03960AT and in accordance with Nextant Aerospace Master Drawing List D81002067. 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 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 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 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 It Installation Manual D12004 Revision E, dated March 2010 or later applicable revision Aircell ATG-4000 Installation Manual D13485 Revision B Dated November 2009 or later applicable revision Aircell Axxess II WLAN AFM Supplement D61002072 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 10/9/2013 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 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 (10-06) EFTA00011825

EFTA00011826

Vniteb *oho of L•ttrica !epartment of Zranzportation geberal crtbiation Abministratian $uppietrtental Mgpe Certificate 0 1.4) tree/nia• Ammo/4 Afarland ST03960AT Nextant Aerospace LLC 3800 Southern Blvd. West Palm Beach, FL 33406 ere/Au ea* nefeente la dr fir s eieureArze anvivivertnee/ Arhi /.4^ elnerAtteeveht eseVite arrAr rlJ 4fierVetareprea meet* hie tretoevareaJ erree:rementi ri e 044'25 Ver Federal Aviation ifoyereekaMJ. Cseritenreivat A6:Matee t 6sw SAC -* Hawker Beechcraft Corporation sea. 400A cZetierffr/Ova r/Fp://r Fyn cellar Installation of Rockwell Collins Venue In-Flight Entertainment(IFE), AffCel I Axxess Cabin II Iridium Phone and High Speed Internet System with Wireless Local Area Network (W LAN) Astronics I I 5VAC 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. 2::rnzahma nwawaivr.i.• 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. terhAYEAT envne.g. ,sewterfaye reitik erAhie evrerreveAt4entzereas a.. *Irv/ tea/e, Jetterseiregi Jatonexted AN:rine/re to 4vrtifiver/eivA o&* rJ et4reelm eV/Ma:an • ery de r/66. .rnOnse,/tedrireivs ,./UneiltifeakivA. Over etwAve44-4. July 28, 2012 Ode rAuftern re March 22, 2012 Ode erAsJoreott.- 0404* at/tenni- Manager Atlanta Aircraft Certification Office Any Alcoration of tbla CerellIcare Is poninablt by a Ilo et net exceeding 13,000. or imprisonment nee stcnOlzq J )sirs, or Sorb. TAS. Iran MG— 1 of 2 PAGta This costa:Scare sky 000 n o ferrod In acCergen,e wIcA IAR 14.4,. EFTA00011827

EFTA00011828

3.ilnilebStafeo of America !epartment of granepartation - Ofeberal Abiatiart Abministration Supplemental. 'Tut Tertifirate ( cintinuation *feet) A1/402,60ST03960AT 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 A ircell 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, 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 (ICA), Nextant Aerospace Document No. DB1002068, Rev III, 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. DB1108018, Rev lit, 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 alteration of this coiCitiCOM is ponishible by a rine of not •XMMISM r1.000. or SePrisorrtent not exceeding l press, or both. tilt row 1110-2-1110-0i Mt 2 of 3 outs This certificatebey be transferred In ICCOrdlnef rich FM 2l.47. EFTA00011829

EFTA00011830

giliien Atated of ?merlon pepartment of ' :transpartation - Offeberal cAbiation cataninistration Supplemental Type Certificate (Continuation Ant) A/14022,4 4ST03960AT % ,4:1oteleiva .954re,i4.• The Certification Basis for this installation is per Type Certificate Data Sheet Al 6SW 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(c)(6) of Amendment 2542; 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(We) 25.1357 25.1431 25.1529 125-541 [25-1231 [25-1231 [25-1131 125.541 [..] Indicates amendmcn level END— Any alteration of this certificate is punishable by a fins of not exceeding 41.000, or Itearlsonnant not exceeding A years, or both. FAA Fon. 0110-Z-1110-6U ME 3 of 3 PAGES This Certificate may ae transferred in teceordence with FAR 22.17. EFTA00011831

EFTA00011832

Nextant Aeros ace LLC est Palm Beach FL 33406 Master Drawing List Report No: DB1002067 Revision F.05 Document Number: DB1002067 Revision: F.0510/1812013 In-Flight Entertainment HAWKER BEECHCRAFT 400A Aircraft FAA STC ST03960AT Approved By Date 1-4-2013 Page 1 of 7 EFTA00011833

EFTA00011834

O MAJOR REPAIR AND ALTERATION u.5 Onsarymor or (Airframe, Powerplant, Propeller, or Appliance) rrompxv,43n Fedni Aviation Adralniftrittlen Fttri ',waved OMB No 2120.0020 11/1C/2007 Etecironic Tracking Number For FAA Use Only INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B. and AC 43.91 (or subsequent revision thereof) (Or instructions and disposition of this form. This report is required by law (49 U.S C. 1421). Failure to report can result in a civil penally not to exceed 51,000 for each such violation (Section 901 Federal Aviation Act 1958) 1. Aircraft Nationality and Registration Mark N493LX Serial No. RK 244 Make Raytheon Aircraft Company Model 400A Ser,es 2. owner Name (As shown on registrabon cera ate) Flight Options .LLC Address (As shown on registration centhcate) Add"" c ty Richmond Heigbts slaw. OH 7.,9 44143-1453 county USA 3. For FAA Use Only 4. Type 5. Unit Identification Repair Alteration lint Make Model Serial Number 0 :I AIRFRAME . (As descnbed in (tern 1 above) K O POWERPLANT Ell K PROPELLER • ID APPLIANCE Type manatee( 6. Conformity Statement A. Agency's Name and Address 8 Kind of Agency tin Nextant Aerospace Address Coy Cleveland sum OH zip 44143-1453 duality USA O U.S. certificated Mechanic O Manufacturer O Foreign Certificated Mechanic C. Cendicate No. 0 Certificated Repair Station CRS # 25NR6678 O Certificated Maintenance Organization 0. I certify that the repair and/or alteration made to the unit(s) identified in item 5 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 or the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best o(m knowled•0 Extended range fuel per 14 CFR Pan 43 APP. B 1:3 12/29/2013 7. Approval for Return to rvtce Pursuant to the authOnly given persons specified below, the unit identified in item 5 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is El APPROVED K REJECTED FAA FR Standards Inspector Manufacturer Maintenance Organization I Person Approved by Canadian Department of TranSperl BY Certificate Designation CRS or # 25NR6678 FAA Designee No X Repair Station Inspection Authorization Otner (Specify) „iv 12129/2013 FAA Form 337 (10-06) EFTA00011835

EFTA00011836

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) N493LX Nationality and Registration Mark Upper Aft Baggage Panel od 12/29/2013 Date 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 4055-21 Camloc quarter- turn fasteners and 214.16D receptacles. Secured N251203-002 to existing upper aft baggage panel with two Camloc 40S5-21 quarter - turn fasteners and 214-16D receptacles. See attached FAA Form 8110-3 Signed by DERT-410115-CE on February 12, 2013 using Nextant 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 (10.06) EFTA00011837

EFTA00011838

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 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 Engine. Propeller, etc ) Aircraft 5. NAME OF APPLICANT Nextant Aerospace LLC Richmond Heights, Ohio LIST OF DATA 8 IDENTIFICATION 7 TITLE EO 029 Rev. E February 8, 2013 ----- Upper Aft Baggage Panel Mod. --------------------------------- Notes: 1) The structural aspects approval is only for the demonstrates compliance subparagraph listed below 2) This form constitutes FAA substantiation of compliance END------------ ------ --------- --- data are approved herein. This the data listed above specified by paragraph and engineering data necessary for for the entire alteration. only of the above listed engineering data. It indicates only with the regulations as "Applicable Requirements." approval of all the to necessary requirements e. PURPOSE OF DATA: Engineering data in support of major alteration to Hawker Beechcraft 400A, SIN RK-244. 9. APPLICABLE REQUIREMENTS (List SpeCiat sections) CFR Title 14 Part 25.301[25-23], 25.303[25-23], 25.305(a)(b)(c)[25-23), 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 183. data listed above and on applicable requirements of the Airworthiness K Recommend vested by direction of the Administrator and attached sheets numbered NIA_ have been examined in accordance with conditions and limitations of appointment under 14 CFR In accordance with established procedures and found to comply with Standards Listed. approval of these data these data I (We) Therefore a Approve DESIGNATED ENGINEERING REPRESENTATIVE(S) 12. DESIGNATION NUMBERS(S) 13. CLASSIFICATION(S) in DERT-410115-CE Structures FAA Form 8110-3 (03-10) SUPERSEDES PREVIOUS EDITION FsIe Number. H13107-O6 Page 1 of 1 EFTA00011839

EFTA00011840

MAJOR REPAIR AND ALTERATION U.S Onedrrentol (Airframe, Powerplant,Propeller, or Appliance) Transponason Federal Aviation darndinrstion Form Apprcacd OMB no 2120-0O20 limoacor Electronic Tracking Number For FAA Use Only INSTRUCTIONS: Pont or type an entries. See FAR 43.9, FAR 43 Appendix B. and AC 43.9.1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a cave penalty not to exceed 61,000 for each such violation (Section 901 Federal Aviation Act 1958) 1. Aircraft Nationality and Regstration Mark N493LX Serial No. RK 244 Make Raytheon Aircraft Company Model 400A Series 2. Owner Name (As shown on registration cerbticate) Flight Options .LLC Address (As shown on r ;strewn cerbtkate Armen car Richmond Heieht§ State OH to 94143-1453 county OA 3. For FAA Use Only 4. Type S. Unit Identification Repair Alteration Unit Make Model Serial Number K 0 AIRFRAME (As described in item I above) El O POWERPLANT K O PROPELLER K 0 APPLIANCE Typo Mandacttser 6. Conformity Statement A. Agency's Name and Address B Kind of Agency Name Nextant Aerospace Address City Cleveland Suite. OH zp 44143-1453 county USA El U.S. Certificated Mechanic a Manufacturer Cl Foreign Certificated MechaniC C. Certificate No. 0 Certificated Repair Station CRS # 25N R667B ID Certificated Maintenance Organization D. I Certify that the repair andror alteration made to the und(s) identified in item 5 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Pad 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Extended range fuel per 14 CFR Part 43 APP. CI 0 12/29/2013 7. Approval for Return to S ice Pursuant to the authority given persons specified below, the unit identified Administrator of the Federal Aviation Administration and is ii..2 in item 5 was inspected in the manner prescnbed by the APPROVED 0 REJECTED FAA Flt Standards inspector Manufacturer Maintenance Organization I Person Approved by Canadian Department of Transport BY Certificate Designation CRS or # 25NR6678 FM Designee • NO. X Repair Station Inspection Authorization Other (Specify) 12/29/2013 FAA Form 337 (1ODO) EFTA00011841

EFTA00011842

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and dale work completed.) N493LX Nationality and Registration Mark 12/29/2013 Date Installed New Pitot Probes in accordance with STC ST10159SC. Nextant Aerospace Master Drawing List Document 373-00.0001 Rev CC EO24-11 Removed Pitot Probes Part Number PH1100-MU-R-1 Removed Pitot Probes Part Number PH1100-MU-L-1 Installed Pitot Probes Part Number PH1100-MUR-EN Serial Number 1975803 Installed Pitot 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 Additional Sheets Are Attached FAA Form 337 pace) EFTA00011843

EFTA00011844

0 MAJOR REPAIR AND ALTERATION v s owinnint ot (Air(rame, Powerplant, Propeller, or Appliance) Transatmen Federal Aviation Administration Form /owned 06,18 N. 2i204020 ii3Or2 C07 Electronic Tracking Number For FAA Use Only INSTRUCTIONS Print or type all entries. See FAR 43 9, FAR 43 Appendix B. and AC 43.9.1 (or subsequ nt revision there* fOr InStruetiOnS and disposition of this form. This report is required by law (49 U.S.C. 1421) Failure to report can result in a civil penally not O exceed $1,000 for each such violation (Section 901 Federal Aviation Act 1958) I. Aircraft Nationality and Registration Mark N493LX Serial 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 registration certificate) AdCMCS2 City Richmond Heights sta. OH zc 44143-1453 comity Na 3. For FAA Use Only 4. Type 5. Unit Identification Repair Alteration Unit Make Model Senal Number ili K AIRFRAME (As desciibed in item 1 above) 0 O POWERPLANT . O PROPELLER K O APPLIANCE Type Man& Dela, 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency Name Nextant Aerospace Address City Cleveland sup.. OH zip 44143-1453 Cutory USA ID U.S. Certificated Mechanic 0 I Manufacturer 0 Foreign Certificated Mechanic C. Certificate No. 0 Certificated Repair Station CRS # 25NR6676 El Ceti/leafed Maintenance Organization O. I certify that the repair and/or alteration made to the unit(s) identified in item 5 above and described on the 'Over e or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and trat the information furnished herein is true and correct to the best of my knowledge. Extended range fuel per 14 CFR Part 43 App. B 0 12/29/2013 7. Approval for Return t 'ervice Pursuant to the authority given persons specified below, the unit identified Administrator of the Federal Aviation Administration and is 0 in item 5 was inspected in the manner prescn bed by the APPROVED 0 REJECTED BY FAA Flt Standards Inspector Manufacturer Maintenance Organization I Person Approved by Canadian Department of Transport FM Designee X Repair Station Inspection Authorization Other (Specify) Certificate or Design lion No. 12129/2013 CRS # 25NR6676 FAA Form 337 (10.06) EFTA00011845

EFTA00011846

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and dale work completed) N493LX Nationality and Registration Mark Provisions for 19107 in Cockpit Sidewall at FS122.735 12/29/2013 Date Added Mount provisions for J9107 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 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 (to-067 EFTA00011847

EFTA00011848

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. MODEL NO. 400A 4. TYPE (Aircraft. Engine, Propeller, etc.) Aircraft 5. NAME OF APPLICANT Nextant Aerospace LLC Richmond Heights, Ohio LIST OF DATA 0 IDENTIFICATION 7 DILE EO 115-12 Rev. C November 27, 2012 --------------- Mount Provisions for J9107. -------- 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, S/N RK-244. 9. APPLICABLE REQUIREMENTS (List specific sections) CFR Title 14 Part 25.301[25-23], 25.303[25-23), 25.305(a)(b)(c)[25-23), 25.307(a)125-231, 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), and 25.625(a)(b)(c)[25-23]. 10. CERTIFICATION - Under authority vested by drectica of the Administrator and in accordance with conditions and limitations of appointment under 14 CFR Pad 183, data listed above and on attached sheets numbered N/A have been examined in accordance with established procedures and (cord to comply with applicable requirements of the Airworthiness Standards Listed. 0 Recommend approval of these data I (we) Therefore El ApprOvatheSe data . .. it. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVEIS) 12. DESIGNATION NUMBERS(S) 13. CLASSiFICATiONIS) DERT-410115-CE Structures FAA Form 8110-3 (03-10) SUPERSEDES PREVIOUS EDITION File Number. H12740.03 Page 1 01 EFTA00011849

EFTA00011850

0 MAJOR REPAIR AND ALTERATION u s ceprvurenter (Airframe, Powerplant, Propeller, or Appliance) Tiensevuoce Fodonl Aviation Anniniornion Form APPrOvatl OMB No. 212043020 11 nolcor Elect(WIC Tracking Number For FAA Use Only INSTRUCTIONS: Print or lype all entries. See FAR 43.9, FAR 43 Appendix 8, and AC 43 9.1 (or subsequent revision thereof) for instructions and disposition of this loan. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed 31000 for each such violation (Section 901 Federal Aviation Act 1958) 1. Aircraft Nationality and Registration Mark N493LX Serial 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 re istration certificate Addf05f City Richmond Heights site. OH zp 44143-1453 Cony USA 3. For FAA Use Only 4. Type 6. Unit Identification Repair Alteration Unit Make Model Serial Number 0 0 AIRFRAME (As described in pem 1 above) li O POWERPLANT 0 Ill PROPELLER El O APPLIANCE Typt Manigactortv 6. Conformity Statement A Agency's Name and Address B. K nd of Agency wens Nextant Aerospace Address Cali Cleveland sin. OH zip 44143-1453 cairn USA 0 U.S. Certificated Mechanic a IManufacturer 0 Foreign Certificated Mechanic C. Cenificate No. 0 Certificated Repair Station CRS # 25NR667B 0 Certificated Maintenance Organization D. I certify that the repair and/or alteration made to the wigs) identified in item 5 above and described on Ihe reverse or attachments hereto have been made in accordance vith the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Extended range fuel per 14 CFR Part 43 K App. 8 12/29/2013 Pursuant to the authority given persons pecifed below, the unit Administrator of the Federal Aviation Administration and Is identified CI. in item 5 was inspected In the manner prescribed by the APPROVED K REJECTED FAA Flt Standards Inspector Manufacturer Maintenance Organization I Person Approved by Canadian Department of Transport BY FAA Designee X Repair Station Inspection Authorization Oder (Specify) Certificate or Designation No. CRS # 25NR6676 12/29/2013 FAA Form 337 (10.06) EFTA00011851

EFTA00011852

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. lden ify with aircraft nationality and registration ma* and date work completed.) N493LX Nationality and Registration Mark Title: Ice Detector Master Caution / Master Warning Light on Constantly Re-Installed the previously removed components ( Ref S/B 30-2600, Rev 2) 12/29/2013 Date 1.) Isolation Relay 1(255 P/N: 50-380048-1 2.) Diode CR654, P/N: 132408-22 3.) Ground stud GS151A P/N: M535206-246 (Stud may be marked GS152) As shown in chapter 30-01-01-01 of AMM. 4.) Wire number corrections on wiring diagram 30-01-01-01 Page 1 correct drawing errors on original drawing. Inspect, verify and correct wiring per EO corrections on EO page 2 See attached FAA Form 8110-3 signed by Daniel Buzz DERT-230019-CE. Dated 8/13/2012 using Nextant Aerospace Engineering Order EO 0130 Rev D. Dated 7/18/2012 ICA Weight and Balance Changes are Negligible Continue to Use Existing Beechjet 400/400A Maintenance Manuals Inspection Procedure for this Area END K Additional Sheets Are Attached FAA Form 337 (r0-06) EFTA00011853

I EFTA00011854

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS . 1. DATE 8.13.2012 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MAKE — liwker Eleechcraft 3. MOOEL NO. 400A S/N RK-244 Only 4. TYPE (Airplane. Radio. Heecopter. etc) Airplane S. NAME OF APPLICANT Nextant Aerospace LLC LIST OF DATA B. IDENTIFICATION 7. TITLE Nextant Aerospace Document 130-12 dated 7-18-12 Rev. D ------------- Engineering Order Ice Detector MCiVIW Light On Constantly ......________ aspects only. ------------ This approval is for the electrical systems ----- ----- B. PURPOSE OF DATA Support major alteration to a Ire aft Hawker Eleechcraft 400A RK-244 Only. 9. APPLICABLE REQUIREMENTS (flu SPeriCC stations) 14 CFR 25.1301(a) (Dire] Note: Comphance has been found to the amendment levels indicated on Hawker Beechczaft TCOS Revision 26 Part 25 Amendment 25.1 through 25-40 to the above applicable requirements. 10. CERTIFICATION - Linder aulh why vested by direction of Ilia Administrator and in accordance vMhconditions and limitations of appointment under 14 CFR Pat1183 of the Federal Aviation Regulations. data listed above and on attached sheets numbered &a have bawl examined in accordance with established procedures and round to comply with applicable requirements of the Airworthiness Standards listed. I (We) Therefore approve these date. . It. SIUNATUR 4GNATE E I E RI REPRESENTATNE(S) 12. DESIGNATION NUMBERS(S) 13. CLASSIRCATILMIS) Systems and Equipment CERT-230019-CE ..'AA Form 81104 (03710) SUPERSEDES PREVIOUS EDITION GPO 901.813 EFTA00011855

EFTA00011856

MAJOR REPAIR AND ALTERATION u.S oreartivent or (Airframe, Powerplant, Propeller, or Appliance) TIIIMPC41•11}1 Federal Aviation reaveritration Form Approved ORS No. N20-0020 timOr2tW Electronic Tracking Number For FAA Use Only INSTRUCTIONS: Print or type all entries. See FAR 43.9. FAR 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition Of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not 10 exceed 51.000 for eaCh such icilabon (Section 901 Federal Aviation Act 1958) I. Aircraft Nationality and Registration Mark N493LX Serial No. RK 244 Make Raytheon Aircraft Company Model 400A Series 2. owner Name (As shown on regishation oendicafe) Flight Options .LLC Address (As shown on registration certificate) A6Sress City Richmond Heiaht state. OH zip 44143-1453 country USA 3. For FAA Use Only 4. Typo 5. Unit Identification Repair Mention Unit Make Model Serial Number h.e. K AIRFRAME (As descnbed in (ern t above) K O POWERPLANT 0 O PROPELLER 0 . APPLIANCE Typo Man./acts,: G. Conformity Stat moat A. Agency's Name and Address B. Kind of Agency Nanie Nextant Aerospace Meese city Cleveland State OH zo 44143-1453 Courtry USA O U.S. Certificated Mechanic 0 Manufacturer O Foreign Certificated Mechanic C. Certificate No. ISI Certificated Repair Station CRS # 25NR6678 CI Certificated Maintenance Organization D. I certify that the repair anchor alteration made to the unit(s) Identified in item 5 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Extended range fuel per 14 CFR Part 43 App. II 0 12/29/2013 prove or tum l': crir ce Pursuant to the authority given persons specified below, the unit Identified Admi ist,ator of the Federal Aviation Administration and is 0 in item APPROVED 5 was 0 inspected in the manner prescribed by the REJECTED FM Fit Standards Inspector Manufacturer Maintenance Organization I Person Approved by Canadian Department of Transport BY Certificate Designation CRS or # 25NR667B FM Designee No. X Repair Station inspection Authorize% on Other Specify) 12/29/2013 FAA Form 337 00-00 EFTA00011857

EFTA00011858

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) N493LX Nationality and Registration Mark Antenna Repair Patch 12/29/2013 Date After removing the forward lower "L" Band Antenna, Instead of removing the Antenna doubler and filling the connector hole with a coin patch and installing nut plate plugs P/N. DB1105020-189-25, the antenna repair doubler P/N. DB104042.001 was installed on the existing antenna doubler and two coin repair patches P/n. DB1104042-002 were installed, one on top of the other to allow for a flush skin repair. The existing nut plate holes were filled with 4 screws P/N. AN525-10R7. See Attached FAA Form 8110-3 signed by DERT-410115-CE dated August 15, 2012 using Nextant Aerospace Engineering Order 139-12 Rev C Dated August 03,1111Mails. ICA Weight and Balance change is Negligible. Continue with Beechjet 400/400A Maintenance Manual Inspection Procedures. End K Additional Sheets Are Attached FAA Form 337 po-orn EFTA00011859

EFTA00011860

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS 1. DATE August 15, 2012 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MAKE Hawker Beechcraft Corporation 3. MODEL NO. 400A 4. TYPE (Aircraft. Engine. Propeller, etc) Aircraft 5. NAME OF APPLICANT Nextant Aerospace LLC Richmond Heights, Ohio LIST OF DATA 8 IDENTIFICATION 7 TITLE EO 139-12 Rev. C August 3, 2012 --------- Antenna Repair Patch (L-Band Antenna Moved). ' ----------------- 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 does not constitute FAA approval of all the engineering data necessary for substantiation of compliance to necessary requirements for the entire alteration. The electrical requirements are not included in this approval and require separate approval. B. PURPOSE OF DATA: Engineering data in support of FAA STC ST03960AT. 9. APPLICABLE REQUIREMENTS (List specific sections) CFR Title 14 Part 25.301[25-23], 25.303[25-23], 25.305(a)(b)(c)[25-23), 25.307(a)[25-231, 25.365(a)(b)(c)(d)(f)(g)[25-00], 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)125-00), 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 Pan 183. data listed above and on applicable requirements of the Airworthiness K Recommend I (We) Therefore El Approve vested by direction of the Administrator and attached sheets numbered N/A have been examined in accordance with cor.011ons and limitations of appointment under 14 CFR in accordance with established procedures and found to comply with . Standards Listed. approval of these data these data II. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATNE(S) 12. DESIGNATION NUMBERS(S) 13. CLASSIFICATIONS) DERT-410115-CE Structures FAA Form 8110.3 (03-10) SUPERSEDES PREVIOUS EDITION Fite Number. H12418.02 Page 1 of 1 EFTA00011861

EFTA00011862

le MAJOR REPAIR AND ALTERATION vs oriparinem or (Airframe, Powerplant,Propeller, or Appliance) Tamperiewn Fulmer Aviation noeniseetion ram AProved OMB No. 21204020 11/302007 Electronic Tracking Number For FAA Use Only INSTRUCTIONS: Print or type all entries. See FAR 43.9. FAR 43 Apperdx B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (40 U.S.C. 1421). Failure tO report can result in a cinf penalty net to exceed 81.000 for each such violation (Section 901 Federal Aviation Act 1958) 1. Aircraft Nationality and Registration Mark N493LX Serial No. RK 244 Make Raytheon Aircraft Company Model 400A Series 2. Owner Name (As shown on reels:tattoo certificate) Flight Options .LLC Address (As shown on tegisfration certificate) neoresi City Richmond Heights sure. OH zo 44143-1453 cumin USA 3. For FAA Use Only 4. Type 5. Unit Identification Repair Alteration Unit Make Model Serial Number K E4 AIRFRAME (Asdescribed in MOM I Mon) K D PONIERPLANT • O PROPELLER El • APPLIANCE Type meoracmar 6. Conformity Statement A. Agency's Name and Address 8. Kind of Agency Rae Nextant Aerospace Address City Cleveland slaw OH zip 44143-1453 Country USA O U.S. Cenincated Mechanic CI IManufacturer O Foreign Certificated Mechanic C. Coruscate No. 0 Certificated Repair Station CRS # 25NR667B O Certificated Maintenance Organization 0. i certify that the repair and/or alteration made to the unit(S) Identified in Kern 5 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Extended range fuel per 14 CFR Part 43 APP. B 0 12/29/2013 Pursuant to the authority given persons pecified below. The unit identified Administrator of the Federal Aviation Admnistration and is 111 in Item 5 was inspected in the manner prescribed by the APPROVED 0 REJECTED FAA Fit Standards Inspector Manufacturer Maintenance Organization i Person Approved by Canadian Department of Transport BY FM Designee X Repair Station Inspection Authorization Other (Specify) CedifiCete or Designation No. 12/29/2013 CRS # 25NR667B FAA Form 331 (10-os) er' EFTA00011863

EFTA00011864

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) N493LX Nationality and Registration Mark Title: Pedestal cover extension Modification 12/29/2013 Date After STC modification of pedestal per 373-94-1000_B, existing pedestal close out tray needs to be extended to cover appropriate areas. Modification of the close out tray is required. Modify the pedestal close out tray per drawing NX25 - 10002. See attached FAA Form 8110-3 signed by DERT - 410115-CE. Dated 11/8/2013 using Nextant Aerospace Engineering Order EO 1018 Rev F. Dated 10/9/2013 ICA Weight and Balance Changes are Negligible Continue to Use Existing Beechjet 400/400AMaintenance Manuals Inspection Procedure for this Area END K Additional Sheets Are Attached FAA Form 337 (10-06) EFTA00011865

EFTA00011866

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS 1. DATE November 8, 2013 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MAKE Hawker Beechcraft Corporation 3. MODEL NO. 400A 4. TYPE (Aimsft. Engine, Properler, eft) Aircraft 5. NAME Of APPLICANT Nextant Aerospace LLC Cleveland, Ohio LIST OF DATA 8 IDENTIFICATION 7 TIP E EO 1018 Rev. F October 9, 2013 — -------------- Pedestal Cover Extension Modification. --- - — 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. B. PURPOSE OF DATA: Engineering data in support of major alteration to Hawker Beechcraft 400A, SIN RK-244. 9. APPLICABLE REQUIREMENTS (List specilic sections) CFR Title 14 Part 25.301(25.23), 25.303[25-23), 25.305(a)(b)(c)(25-23], 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)125-23), and 25.789[25-32). 10. CERTIFICATION - Under authority Part 183, data listed above and on applicable requirements of the ArnvonhMess K Recommend vested by direction of the Administrate( and attached sheets numbered Nth have teen examined In accordance with conditions and lirnotati5ns of appointment under 14 CFR in accordance with established procedures and found to comply with Standards Listed. approval of these data these data I (We) Therefore 0 Approve 11. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) 12. DESIGNATION NUMBERS(S) 13. CLASSIFICATION(S) DERT-410115-CE Structures FAA Form 8110-3 (03-10) SUPERSEDES PREVIOUS EDITION File Number H13817.04 Page 1 of 1 EFTA00011867

I EFTA00011868