0 MAJOR REPAIR AND ALTERATION U S Desennial ce (Airframe, Powerplant, Propeller, or Appliance) haiseaseat Feeeni Aviation Adoinhintien Form Apprma O1AS Ho. 21204020 in-8mo/ Elector Tre:f.0ng Number For FAA Use Only INSTRUCTIONS Prim co type all entiles See FAR 43 P FAR 43 Appendix 0. and AC 43 9.1 (or sarsequem caws on thereof) for mStruCcres are disp0sinon of MIS rpm. ThiS rennet is required by law (49 U S.C. t421) Failure b report can renal in a civil penny nol lo acted 51.000 kw iaacA sodi iolation (Section 901 Federal Aviation Act 1955) 1. Aircraft Natananty and Registration Mark N493LX Serial No. RK 244 Make Raytheon Aircraft Company Model 400A Series 2. Owner Name (As skean on regaltabon cookers, Flight Options .LLC Address (As shown on registration arbficate) Aosess 26180 Curtiss Wright PKWY CA, Richmond Neigh% Nem OH 20 4A14344)51 canry USA 3. For FAA Use Only 4. T pe 5. U It Identification Repair menden um Mao Model Serial Number El 0 AIRFRAME (As descasel in Item I above) 0 O POWERPLANT 0 O PROPELLER IN 0 APPLIANCE Ty", "wawa 6. conteemity Statement A. Ageneys Nana and Address 8. Kind a Agency Name Nextant Aerospace Mott 355 Richmond Road cat Cleveland slaw OH Ely 44143-1453 corer USA 0 U.B. Cenidcated Mechanic 0 IManufaceser 0 Foreign cenNeatee Memaic C Cerbficabn No. a Certificated Repay Slam CRS it 25NR6678 0 Carbecateg Manlenance Organization 0. I certify that the repair ander alteration made to the trid(s) emirs in item 5 above and dilated on the reverse Of attachments WOW have been made in accordance wen the requiter/ferns ciParl 43 of the U.$ FederalAviation Regulations and that the Oformation Wished herein is true and correa to the beet of my knowledge. Exergea range fuel per Ade0 14CFR Partin O SignetUrealate omuthonzeo Indio Anton J. Koprivnik . 12/29/2013 7. Approval for Return to Se Pursuant to the autInor3y green persons Spected bebet, the un lidentifild Admirestiala or the Federal ARKIN' Administraeon end Is 0 In dem APPROWO 5 was . inspeced In the manner Faulted by the Attctto BY FAA Fit standar/Is inspector Manufacturer Maintenance Organization Persia) b ian Department of ransom FAA Designee X Repel Simon Inspected Authorization Other (Speedy) Certificate or Desitastion No. CRS # 25NR6676 SigneuraVale or Authorized Individual Anton J. Koprivnik 7C 12/29(2013 FAA Form 337 (loos) SDNY_GM_02755103 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242025 EFTA01327143

SDNY_GM_02755104 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242026 EFTA01327144

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous arerations to assure continued conformity with the apPbCable aiworthinesS requirements 8. Description of Work Accomplished (tenure space is required attach additional sheets Idenbly with aircraft nation's* and registration mark amidst* work completed.) N493LX Nationany 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 K255 P/N: 50-380048-1 2.) Diode CR654, P/N: 132408-22 3.) Ground stud GS151A P/N: MS35206-246 (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 papa) SDNY_GM_02755105 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242027 EFTA01327145

SDNY_GM_02755106 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242028 EFTA01327146

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 '.. 'Iwker Eleechceatt 3. MOOEL NO 400A SIN RK-244 Only 4. TYPE (Airplane. Radio. Herospfer. etc) Airplane 5. NAME OF APPLICANT Nexcent Aerospace. LLC LIST OF DATA 8.IDENTIF/CATION 7. TITLE Revive Aerospace Document 130-12 dated 7.18-12 Rev. D Engineering Order Ice Detector WNW Light On Constantly END --- ThiS approval is for the actrical systems aspects only. S. PURPOSE OF DATA Support major elleiragen to Micron Hawker Ecerchcrall 400A RK.244 Only. 9. APPlICASLE REOUIREtJeNTS (L:Nwedge Su) 14 CFR 25.1301(a) (O.1g1 Note: Compliance has been found to the amendment levels inckaled on Homes Beechcrefl TCDS Revision 26 Pad 25 Amendment 25-1 through 25-40 to the above applicable reoutremeMs. 10. CERTIFICATION - Under math why vested DV direct«. of he AcInkcestralor and in aTandanat Milli POIXD10n5 and limitations of appointment under 14 CFR Pan 183 of the Federal Aviation Regularlons. data Crated Mho and on mired sheets neurtnoil M:8 have been MarTIMMil et accordance with established procedures and round to comply with applicable requirements of the Airworthiness Standards listed. I (We) Therefore approve these data. - it SIGNATURE( NATE E NE RINQ REPRESENTATNE(S1 it DESIGNATION NUMBERMS) 13. DtAssiFicATI0NtS) - Dade] i.. Bunt DERT.230019-CE Systems and Equipment ..AA Form 8110-3 (03110) SUPERSEDES PRENK0US EDITION GPO 9014113 SDNY_GM_02755107 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242029 EFTA01327147

SDNY_GM_02755108 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242030 EFTA01327148

0 MAJOR REPAIR AND ALTERATION i)a S arms a (Airframe, Powerplant, Propeller, or Appliance) T pas Fedenol 444404 Adolnistraben Fran ammo Maw N20-0320 II/307007 Electronic Tracking Number For FAA Uso OalT INSTRUCTIONS Print or type an mines See FAR 43.9. FAR 43 Appendix B. and AC 43 9-1 (or subsequent rata thereof) la instruCbCns and disposeion a This form. This tenon is required by law (49 U.S C. 1421) Fare to sepal can result in crid penalty not to exceed $1000 Ion each such votatcin (Sean 901 Federal Aviation Act 1958) I. Aircraft Nationality and Registration Mark N493LX Sail No. Rt< 244 Make Raytheon Aircraft Company Model 400A Sees 2. Owner Name (As Moen on reeistraboo Certarcate) Flight Options .LLC Adckess (As shown on reg#Irabon awfikate) Moan Curtiss Wright PKWY car Richmond Heights slat OH to 44143-1453 COL443 ai 3. For FAA Use Only 4. Type 5. UMW'S:Mention Reps Alerabon Veit Make Model Serial Number El O AIRFRAME (As desonbed In ffem 1 above) 0 El POWERPLANT O O PROPELLER O O APPLIANCE Tyne mar asoa ll Conformity Statement A Agency's Name and Address B. KM of Agency 1411441 Nextant Aerospace Asa 355 Richmond Road citi Cleveland smut. OH zo 44143-1453 cony USA 0 U.S. Cerlificaled Mechanic 0 IManufsdorer 0 Foreign CerIfical Mechanic c. cantata. No 0 Certificated Repair Sieben CRS # 25NR667B 0 Cartricaim maintenance °roam/aeon O. I ably that the repair anovot aaaratian made to the unt(s) Mead in item 5 above and descnbed on the reverse or Naval, hereto have been made in accordance with the requirements a PM 43 of ton U.S. Federal Aviation Rep/taws and that the information furnished herein is Ma and coned to the al of my knowledge. Extended range fuel pe 14 CFR Pan 43 As 8 O SignaharM0ste OASIS:cid Individual Anton J. Komivnik a 720.._ cii t y 12/29/2013 7. Approval for Return nice Pursuant to the avirtority awl persons waited below. the un Identeled in nem 5 was impeded in the manner prescribed by the Adrithistrakx of the Federal Aviation Administration and is @APPROVED O REJECTED FM Fit Standards inspector Mani/Kam Maintenance Organization Person Approved by Canadian Departrnent or Transport BY FM Designee X Raper station Oktra (Spearly) inspeCl/On AuthorizMion Comical° or Designation No. CRS it 25NR667E1 Signature/Dale c4 Authorized IndMdual d e,,t‘ y Anton J. Koprivnik 12/29/2013 a e< ate FAA Form 317 tto-cist SDNY_GM_02755109 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242031 EFTA01327149

SDNY GM 02755110 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242032 EFTA01327150

NOTICE Weight and balance 0, operating limitation changes shall be entered in the appropriate °Wren record. An alteration must be compatible with alt previous alterations fo assure continued conformity with the applicable einvorthiness requirements. 8. Description of Work Accomplished (If more spec* is requited. attach additional sheets. Wen ify with aircraft nationality and registration math and date work completed.) N493LX Nationality and Registration Mark Antenna Repair Patch 12/29/2013 Date After removing the forward lower "I? 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 Pin. 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 Paul Hedding dated August 15, 2012 using Nextant Aerospace Engineering Order 139.12 Rev C Dated August 03, 2012 for details. ICA Weight and Balance change is Negligible. Continue with Beechjet 400/400A Maintenance Manual Inspection Procedures. End K Ackhlional Sheets Are Attached FM Form 337 (10.06) SDNY_GM_02755111 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242033 EFTA01327151

SDNY_GM_02755112 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242034 EFTA01327152

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL stAllATION 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 a. TYPE (Airaart End** Prope*r. etc) Aircraft 5 NAME OF APPLICANT Nextant Aerospace LLC Richmond Heights. Ohio LIST OF DATA 6 IDENTIFICATION 7 TITLE EO 139-12 Rev. C August 3. 2012 -------------- Antenna Repair Patch (L-Band . -------- Notes: 1) The structural aspects only is only for the engineering compliance only with the below as 'Applicable Requirements: 2) This form does not constitute necessary for substantiation entire alteration. The electrical and require separate approval. Antenna Moved). --------------- of the above listed data are approved herein. This approval data. It indicates the data listed above demonstrates regulations specified by paragraph and subparagraph listed FM approval of all the engineering data of compliance to necessary requirements for the requirements are not included in this approval s PURPOSE OF DATA: Engineering data in support of FM STC ST03960AT. 9. APPLICABLE REQUIREMENTS (Lel setae wows) CFR Title 14 Part 25.301(25-23], 25.303(25-23), 25.305(a)(b)(c)[25-23], 25.307(a)(25.23], 25.365(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)[25-00], 25.611(25.23). 25.613(a)(b)(c)(25-00), 25.619125-231, 25.625(a)(b)(c)(25.23), and 25.789(25-32]. 10. CERTIFICATION - Under autbety Part 183. data Wed above as on apecatto requirements of Me Atmerteness vetted by Cfneetage of Me Mreistralor and e accedence we, condemn and Neatens of appelment under to CFR attached sheets numbered N/A have been teamed in accordance MN estatened procedures and Iced to cane we &Wards Listed. approval of these data thee data ■ Recommend I (W) Therefore tg Approve II. SIGNATURE'S) OF DESIGNATED ENGINEERING REPRESENTATMEIS) 12. DESIGNATION NUMBERS'S) 13. CLASSIFICATION(S) c'e'a"-- Paul Hedding DERT-410115-CE Structures FAA Form 81104 (03.10) SUPERSEDES MUMS EDITION File tenter. H12418-02 Page 1 of 1 SDNY_GM_02755113 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242035 EFTA01327153

SDNY_GM_02755114 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242036 EFTA01327154

e MAJOR REPAIR AND ALTERATION US Oapatmeni el (Airtrame, Powerplant, Propeller, or Applianco) nusatwen lama Adatlen Marnistneen reinsame 0618No. 2120.0320 1.1=07 ElectrooRTrackng Runt« Fm FAA Us* On& INSTRUCTXWS: Pantar type an tablett. See FAR 43.9, FAR 43 Appendix B. and AC 43.9-1 (or subseguenl Maisen ~ei) for instrwlions and 66006666 end form. 1TR nidorl is requirecl by latv (49 U.S.C. 1421). raken »repp:tam endt in a cml gray not to exeeed $1,000 Mr esch suck oblaten (Selvion 901 Federal Realitet Ad 1958) 1. AlreraR Naroonalay and Registra-1N Man N493LX Serai no. RK 244 Mane Raytheon Aircraft Company MOdel 400A Settes 2. Ormer Naine (fl shOmi on reoistagon ~Son) Flight Options .LLC Meien (As shows on (s~ation "ne) Øs CurtissWriaht PKWY os Richmond Heights sta OH u 44143-1453 venn Q8 3. For FAA Un Onty 4. Type 5. U It Wentification Repair Atleraten Unn Make Model Sedd Runder D s AIRFRAME (As aescntel pn (km I *bose) D O POWERPLANT 0 O PROPELLER O O APPLLANCE Type Manuiedvet 6. ConformNy Statoment A ~dis Norne and Addtess B. knea Agency Nyre Nextant Aerospace rams 355 Richmond Road on Cleveland sua OH vo 44143-1453 Gule USA a U.S. Ceitidealed hiechand o I Manufseturer 0 Foreign emnes:dl Mechanie C Gen/kote No. Ø Cefl&aled Repet Motion CRS It 25N R662B a Cenincated Mainlenance Organizahon D. I cenify dial the repet ania)0, ~i made to the tinde) identified in Hein 5 aten« and clescnbecl on the (Nede ot allachments hegle neve ban made in accareanca un the requiremenIS of P n 43 of the U.S. FeelnalAviatinn Regulator: and Nat the informabon luntende hereln is Na ard atirrict lo the best of my iironeedge. Extended range lidi per 14 CFR Pan 43 APP. B D Signaturallate ol AulhOrneel Indiviebal Anton J. Koptivnik 12/29/2013 f .....,fle f 1. Ap val til to Servl Insinuant lo the mitimmy given persons emne) belma, am un I iderilMed in den 5 was inspecied in Ne manne veoxibtrl by gle Adilinelreke Cd the Federal Mima MministratOn and is Ø APPROVED Cl ROECTED FM Fl Siantlads Inspector idanufactufer Maintenanco Organization Person Approvecl by Canaoian Departrrmintof Transport BY FM Designe. X Ropa« Stausn inspection Authorizahsn ONN (SP•Fdd Naticale or ougneten aa CRS S 25NR6678 s s SpnattrelDale N AuSionzed Individvaair Anton J. Koprivnik 12/29/2013 in FAA Forn 337 (10-06) SONY_GM_02755115 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242037 EFTA01327155

SDNY_GM_02755116 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242038 EFTA01327156

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all prewoos alterations to assure continued conformity with the applicable ainvorthiness requirements. 8. Description of Work Accomplished Of more space is required attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) N493LX Nationality and Registtation Mark Title: Pedestal cover extension Modification 12/29/2013 Date After STC modification of pedestal per 373-94-I 000)3, 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 I - I 0002. See attached FAA Form 8110-3 signed by Paul Hedding DERT - 410115-CE. Dated 11/8/2013 using Nextant Aerospace Engineering Order EO1018 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 (1046) SDNY_GM_02755117 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242039 EFTA01327157

SDNY_GM_02755118 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242040 EFTA01327158

V.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ACAIIMSTRATK)N STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS 1. OATE November 8, 2013 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MAKE Hawker Beechcraft Corporation 1. 1.010EL NO 400A 0 TYPE (Aircraft Enpne, PeopeNtr. Et) Aircraft 5 NAME OF APPLICANT Nextant Aerospace LLC L Cleveland, Ohio LIST OF DATA 8 IDENTIFICATION 7 TITLE 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. a. PURPOSE OF DATA Engineering data in support of major alteration to Hawker Beechcraft 400A, SIN RK-244. 9. APPLICABLE REQUIREMENTS (UM speak womb CFR Title 14 Part 25.301[25-23j, 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 autheriN vested by Orman of the Administrator and In ace dance with earthen; and limitatbres et appoiMmem 'Ada 14 CFR Partin. data stied above and on attached sheets numbered NIA_ have been examinee in mconlance nith estabished procedures and found to ecniptivith applcaoh requirements of the kiwortrtirms Standards Listed. 0 Recommend approval of these data I (We) Therefore (23 Approve these data II. SIGNATURE1S) OF DESIGNATED ENGINEERING REPRESENTATIVES) 12. DESIGNATION NUMBER$($) 13. CLASSIRCATION0a Olt 5.', --> 17 Paul Hedding DERT-410115-CE Structures FAA Form 81104 (03-10) SUPERSEDES PREVIOUS EDITION Fie Number H13817-04 Page 1011 SDNY_GM_02755119 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242041 EFTA01327159

SDNY_GM_02755120 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242042 EFTA01327160

0 MAJOR REPAIR AND ALTERATION u S Deerninl el (Airframe, Powerplant, Propeller, or Appliance) Tv mlioxtake. Nano Aria*. Modrisliallon folnAwckad O M No 21204020 I ifXv2C07 Eiectionic Tracking Number For FAA Use Only INSTRUCTIONS: Print or tweet enbies. See FAR 43.9. FAR 43 Appendix B. and AC 43.9-1 (or sub's:pent revision memo for instructions and cesposigcn of Ins form That report a required by law (49 U.S.C. 1421). Failure to rePerf oan result in • c)if Penal not to need $I.= kat eath SuCh *talon (SeCkie 901 Federal Aviation Act ISM) I. aroMl Nabortaidy and Repatriation WA N493LX Serial No. RK 244 Make Raytheon Aircraft Company more 400A Sates 2. Owner Name (As shown on registration confined Flight Options .LLC Address (As shown on registration ortificar4) Address 26180 Curtiss Wright PKWY cry Richmond Heights sw, OH zo 44143-145_3_ Carry USA 3. For FAA Use Only 4. ype 5. Unit Identification Repay Allerebon Unit Make model Serial Number • CI AIRFRAME (AS descnatain Hem I above) 0 O POWERPLANT ID O PROPELLER ID MI APPLIANCE TOO IMMULICIartit 6. Conformity Slat mont A. AgeMYe Name and Address B K nd of Agency Pa Neaten( Aerospace *anis 355 Richmond Road Cory Cleveland sue. OH ip 44143.1453 aunty USA _0 0 u S. Certificated Methane 0 ManufaCturer 0 FOreqn Cenficaled *chant C CetifIcate No. 0 Seitlitated Repair Station CRS # 25NR667B Caroficaled Mentionsme Organization O. lc:edify that the leper artier attention made to the unit(s) identified in item S above and descnbed on the reverse or anennents hereto RUG been made in accordance with the requirements of P rt 430f the U.S. Federal Maiden Regulations and OW tie INCX11134011 furnished beret, is hue and correct to tie beat of my knowledge. &ended farce rue 14 per CFR Part 43 App. B El Signalure/Vate of Authorized individual Anton J. Koprivnik tape7, . 12/29,2013 7. Approval for Return to Settee Pursuant to the adhoilty given pe sons molted below. Me unit Adminisbanc of the Federal AMMIC41 Admonition and is in den led in men 5 was inspected In the manner deserted by the APPROvE0 0 REJECTED ay FAA FS Standards inspector Manursolurer Maintenance Organization Person Approved by Canadian Oeparuners of Transport FAA Designee X Repay Station Inspection Autheetnace Omer (Spicer) Certificate or Desi NO. ton 25NR6676 CRSgn rt SidnalwerDatio of Authorized Individual Anton J. Koprivnik ....94::> 12/29/2013 4 „ FAA Form 337 (10-00) SDNY_GM_02755121 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242043 EFTA01327161

. SDNY_GM_02 755122 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242044 EFTA01327162

NOTICE Weight and balance or operating /imitation changes shall be entered in the appropriate aircraft mead. An alteration must be compabble with all previous alterations to assure continued conformity with the applicable airworthiness requirements 8. Description of Work Accomplished al more space is required attach additional sheets. Identify with aircraft nationality and registration mark and dale work completed.) N493LX Nationality and Registration Mark DEACTIVATE CLOCKS 12/29/2013 Date For Pilots Clock Deactivation: I.) Removed PLT CLOCK circuit breakers from LH FWD CB Panel. Spliced feed wires together. Cap and Stowed Load side wires. 2.) At Radio Junction Box: a.) disconnected wire W78-I9 from 3931125 PIN R & S. b.) Spliced wire W78-19 from pin R with 3931122 wire W7I-3 (20) pin D•. For Co-Pilots Clock Deactivation: 4.) Removed COPLT CLOCK circuit breakers from LH FWD CB Panel. Spliced feed wires together. Cap and Stowed Load side wires. 5.) At Radio Junction Box: a.) disconnected wire W78-45 from 393 ITBI 3931R3 pin 3. b.) cap and stowed wire. c.) Installed jumper from pin 3 to 3931322 pin P (splice with wire W7I-4 (20)) 6.) Tcstcd all WOW interface circuits at HI & #2 DCU, # 1 & #2 DCP,41 & #2 PEWS' & #2 MFD, DAU, 41 &#2 ADC, 4 I & 42 GPS, 41 & 42 FEU, #I & 42 TDR. 7.) Changed power wiring for ELT from 42 Clock to #2 Audio panel. Disconnected wire from inline fuse ELTFI feed side and connected to Audio power input 2350P4 pin 8 (spliced with wire W965.019 (20)). Tested ELT. This removal was electrically approved by Daniel L. Bun FAA DERT-230019-CE using a FAA 8110-3 Dated November 15, 2013 Using Nextant Engineering order 1165 Rev B Dated 11/13/2013 End K Additional Sheets Are Attached FAA Form 337 00-00 SDNY_GM_02755123 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242045 EFTA01327163

SDNY_GM_02755124 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242046 EFTA01327164

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS 1 DATE 11-15-2013 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MAKE - Hawker Beechcraft . • 3 MODEL NO. 400A Stal RIC-244 Only 4. TYPE (Airplane. Raft AMMOMm; eft.) Airplane 5. NAME OF APPLICANT Nextant Aerospace LLC LIST OF DATA &IDENTIFICATION 7. TITLE Nextant Aerospace Document EO 1185 dated 11.13.13 Rev. B —.- Engineering Order Deactivate Clocks elecb-ical systems — --- — This approval is For the END-- aspects only. 8. PURPOSE OF DATA Support mayor alteration to aircraft Hawker Beechcraft 400A RK-244 Only. 9. APPLICABLE REQUIREMENTS (List sneak sections) UT CFR 25.1301(8)(0dg] Note: Compliance has been kund to the amendment levels indicated on Hawker BeeChtraft 400A TCOS Revision 28 Part 25 Amendment 25- 1 through 25-40 to the above applicable requirements. 10. CERTIFICATION - Under authority vested by direction of the Administrator and in accordance Min conditions and imitations of appointment under 14 CFR Part 183 of the Federal Aviation Regulations. data listed above end an altsched sheets numbered TE5 have been examined In accordance with established procedures and found to comply with ape/male requirements of the Airworthiness Standards lived. I (We) Therefore approve these data. ii. SIGNATDRE(S a, ESIGNA, D ENGINEERING REPRESENTATNE(S) 12. DESIGNATION NUMBERS4S) 13. CLASSMCATIONISI / i DERT-230019-CE Systems and ErnftorneM Daniel L. 9. • • .r AA Form 8110-3 (03410) SUPERSEDES PREVIOUS EDMON GPO 901413 SDNY_GM_02755125 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242047 EFTA01327165

SDNY_GM_02755126 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242048 EFTA01327166

0 MAJOR REPAIR AND ALTERATION u soshienme, (Airframe, Powerplant, Propeller, or Appliance) Transports* rest Ass mareasaron roan Approved OMB NO. 2120.0020 or3D2337 Etectionlc Tartan Number Foe FAA UM Only INSTRUCTIONS: Print or type an wan. See FAR 43.9. FAR 43 Appendix 9. aid AC 43.9-1 (or subsequent revision Smog for instrucarrt and t1SpOsilion of this form This report is required by law (49 U.S.C.1421), Faire to report can result In a Call penalty not lo exceed $1.000 for each such violets (Saba 901 Federal Aviation Act 1958) 1. Aircraft Mahwah'', and Registracer Mark N493LX Serial No. RK 244 Make Raytheon Aircraft Company Model 400A Series 2. Owner Name (As snows on registrar ron cerhfictrM) Flight Options .(SC Address (As snows On reparation centre/Cafe) Moots 26180 Curtiss Wright PKWY cry Richmond Heights sirs OH zo 44143-1453 cony UM 3. For FAA Use Only 4. Type 5. Unit Identification Repair Alteration Unit Make Model Seas Number C III AIRFRAME (As deserted in /em I aborts) D O POWERPLANT 0 O PROPELLER O O APPLIANCE Two orandactwor 6. Conformity Stat mont A Agency, Name and Meese 8. K nd ciAgenCy Name Nextant Aerospace Adam 355 Richmond Road CM Cleveland swh OH ao 44143-1453 cony USA 0 u.s.cerbothied Mechanic 0 Manufacturer O rotor cenacated Mechanic C Certificate No 0 Certificated Repair Sias CRS it 25NR6678 0 Cerbficatro Maintenance OrgaMarton D. I certify that the reps; andarx alteration made to the alga) Wearied in item 5 above and desabed on the reverse or attachments hereto have ban made in accordance will the requiononts of Part 43 Of the U.S. Federal Aviation Regratoris and that the rocernafion furniihed herein is true and anneals, the best of my knOwledge. Extended range fuel per 14 CFR Part 43 APP. 9 D Signature/ale Of Autry:aired Individual Anton J. Koprivnik :117 —. ' 12/29/2013 7. Approval for Return to Ice Pursuant Io the authority given persons specified below, the umt den IMO in Rem 5 was inspected in the manner prescribed by the Administrator of the Federal Matron AdmOisabOn and is el APPROVED 0 REJECTED BY FAA al StarKlards Inspector Department Manufacturer Mantenance Organization Person Approved by Canadian et Transport FM Designee X Repair Station InsPeCan Authorization Other Specfird Certificate a Deagnallon NO. CRS ft 25NR6678 SigruturelOate of Authorized IndiScar Anton J. Koprivnik 12/29/2013 <9Z . Cea ti ./. FAA Form 337 room .7 SDNY_GM_02755127 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242049 EFTA01327167

SDNY_GM_02755128 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242050 EFTA01327168

NOTICE Weight and balanCe or operating Limitation changes shah be entered in the apIxopliste 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 flf more space is required. attach additional sheets Identify with aircraft nationality and registration mark and date work completed.) N493LX Nation** and Registration Mark 12/29/2013 Date TITLE: Aircraft Windshield Sealing Process Deviation: Mow Deviation from AMM 56-10-00-201 for the sealing of the aircraft windshield process. Temporary fasteners are not necessary during the sealing of the windshield. Original 8 typical bolts for installation may be used during the process, to keep retainers and shims in place during the entire sealing & installation of the windshield. After proper sealing time had elapsed. torqued bolts for installation of windshield per AMM. See attached FAA Form 8110-3 Signed By DERT-410115-CE Paul Hedding. Dated June 12, 2013 using Nextant Aerospace Engineering Order 1257, Rev. A, Dated May 21, 2013 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 gots) SDNY_GM_02755129 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024205I EFTA01327169

SDNY_GM_02755130 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242052 EFTA01327170

O.S. DEPARTMENT Of TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS I. DATE June 12, 2013 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MAKE Hawker Beechcraft Corporation 3. MODEL NO. 400A 4 TYPE (Amok Ear.. Axe*. etc) Aircraft 5. NAME OF APPLICANT Nextant Aerospace LLC Richmond Heights, Ohio LIST OF DATA JJAENTIFICATION 7. TITLE EC) 1257 Rev. A May 21, 2013 ---------------- Aircraft Windshield Sealing Process Deviation. ------ 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 repair. is PURPOSE OF DATA Engineering data in support of major repair to Hawker Beechcraft 400A, S/N RK-244. 9. APPVCABLE REOUIREMENTS (Lin specific sectOns) CFR Title 14 Part 25.301(25-23), 25.303[25.23), 25.305(a)(b)(c)(25-23), 25.307(a)(25-23), 25.601[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 audiority Pan Mt data listed above and On applicable requirements of the Airworthiness vested by direction of the Adrrireara1Or and in accordance with Ca ns and mnitalkns of ameontment ureter li CFR attached Vita numbened _DIA_ have been examined In accordance with estaUtshed procedures and found lo comfy with Standards Listed. approval of these data these data • Recommend I (We) Therefore Approve II. SiGNATUREIS) OF DESIGNATED ENGINEERING REPRESENTATNE(S) 12. DESIGNATION NUMBERS(S) 13. CLASSIFICATIONISI tat Paul Hedding DERT-410115-CE Structures FAA Form 81104 (03-10) SUPERSEDES PREVIOUS Eamon Eft Number. H13357.01 Page 1 ell SDNY_GM_02755131 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242053 EFTA01327171

SDNY_GM_02755132 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242054 EFTA01327172

MAJOR REPAIR AND ALTERATION u.Sovaineereer (Airframe, Powerplant, Propeller, or Appliance) Trangswien reeenceviatim Aik•Milstale. rorm Amami( cub NP. 2t204020 tioadeOf Electronic Tracking Number For FAA Use Only INSTRUCTIONS: Print or type all entries. See FAR 43.9. FAR 43 Appendix B. and AC 43.94 (or subsequent revision theme° for instructions and disposition or des Icon. This report is required bylaw (49 U.S.C. 1421). Failure le MPW1can result m *chi Penal nee to raced 31.1:00 for each such violation (Section 901 Federal Awalkm Act 19513) I. Aircraft Nation:My and Registration Mark N493LX Serial No. RK 244 Make Raytheon Aircraft Company Model 400A Series 2. Owner Nome (As shown on registration cetldicate) Flight Options .LLC Address (As shown an registration certificate) access 26160 Curtiss Might PKWY Ca Richmond Heights sw. OH zit 44103-1453 Corny OA 3. For FAA Use Only 4. Type S. Unit Identification Repel( AllerabOn Veit make model Serial Number MI P. AIRFRAME (As descnted in Nem i above) 0 El POWERPLANT El O PROPELLER 0 MI APPLIANCE ace rem.rectme 6. Conformity Sul moot A. Agency. Name and Address B. K nd of Agency Nene Nextant Aerospace Parma 355 Richmond Road Cm Cleveland sloe. OH Ze 44143-1453 Cowley USA 0 u S. Cenrcated Methane 0 Manufacturer 0 Foreign Gen/loved methane C Certificate No. 0 Cerlfcaied Repair &non CRS # 25NR667B 0 Cenificated Mai nienance Organize: on D. I certify that the repair anctioc al enition made to the unit(s) identified in sem 5 abort and deserted on the reverse or attachments hereto have been made in aCCOlanceml the requirements of Part 43 of the U.S Federal Aviat on Regtiat ons and nal me intonation furnished herein Is true and correct to the best of my kevAleace Edencled range fuel per 14 CFR Part 43 APP. B El Signahre/Dete of Authorized Individual Anton J. Koprivnik ' , 12292013 7. Approval for Return Service PuntuaM to the authorityOen persons speafied below. the unit identMed in item 5 was inspected n the manner presaged by the Administrator 04 the Federal Avutice Administration and is @APPROVED 0 MUTE° BY FAA FPI Standards inspector Manufacturer Mantenance Organization Person Approved by Canadian DepartmeM ol Transport FAA Designee X ReaviSta50(1 Inspection Authorization Other (AMA') CertiScate or Designation No. CRS IS 25NR6678 SigneturelDate of &Merited individual Anton J. Koprivnik 2 ., 12/292013 CA.,44 FAA Form 337 Dam SDNY_GM_02755133 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242055 EFTA01327173

SDNY_GM_02755134 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242056 EFTA01327174

NOTICE Weight and balance or operating limitation changes shall be entered in the appropnate aircraft record. An alteration must be compatible with all previous alterations fo assure continued conformity with fhe applicable ainvorthiness requirements. 8. Description of Work Accomplished Of more space is required. attach adotional sheets. Identify with aircraft nationahly and registrabbn mark and date work completed) N493LX Nationality and Registration Mark 12/29/2013 Date Requested for use of new processes & materials for the removal and installation of Main & Side Windscreen, deviation from HBC AMM When performing the removal and installation of the windscreen and/or cockpit side windows, the following deviations from the HBC AMM are allowed & recommended: 1. During the removal & installation of the main windscreen, reference FO-AMMS document, chapter 56-10-01 for the main windscreen installation using AVDEC materials. This document correctly defines the processes and materials to be used for the removal and installation of the main windscreen. 2. During the removal and installation of the cockpit side windows, reference Flight Options FO-AMMS Document, chapter 56-10-10 & 56-10-11 for the replacement of the side window inner rubber gasket. This document correctly defines the processes and materials to be used for the replacement of the cockpit side windows inner rubber gasket. NOTE: TG8498 & HT3935-7 may not be used on exterior surfaces unless sealant is to be painted after curing for protection against UV light. PERMISSIBLE TO PAINT OUTER WINDSHIELD RETAINER WITH Chevron White JET GLO, CMOS70513 (Sherwin-Williams) This Alteration was FAA Approved by Paul Hedding FAA DERT-410115-CE using an FAA Form 8110-3 dated December 28, 2013. Using Nextant Aerospace Engineering Order 1303 Rev B Dated November 13, 2013 ICA Continue with Normal Hawker Beech Maintenance manual Inspection Requirements for this Area End K Additional Sheets Are Attached FAA Form 337 (loos) SDNY_GM_02755135 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242057 EFTA01327175

SDNY_GM_02755136 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242058 EFTA01327176

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADAtNISTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS 1. DATE December 28. 2013 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2 MAKE Hawker Beechcraft Corporation 3. MOOEL NO. 400A 4. TYPE (Mott EnPne. PrOPeag etc) Aircraft 5 NAME OF APPLICANT Nextant Aerospace LLC Richmond Heights. Ohio LIST OF DATA A IDENTIFICATION 7 IptE EO 1303 Rev. B November 13, 2013 Process & Material Deviation for the Removal and Installation of the Main & Side Windscreens. — Notes: 1) The structural aspects only of the above listed data are approved herein. This approval is only for the engineering data. It indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and subparagraph listed below as -Applicable Requirements! 2) This form constitutes FAA approval of all the engineering data necessary for substantiation of compliance to necessary requirements for the entire alteration. ---------- — 8. PURPOSE Of DATA: Engineering data in support of major alteration to Hawker Beechcraft 400A. SIN RK-244. 9. APPLICABLE REOUIREMENTS pal Wed& eneltens) CFR Title 14 Part 25.301(25-23), 25.303[25-23], 25.305(a)(b)(c)[25.231, 25.307(a)(25-23), 25.562(c)(25-23). 25.601[25-00), 25.603(aXb)(c)(25-38). 25.605(a)(25-00i, 25.607[25.23J, 25.609(a)(b)[25.00), 25.611[25.23]. 25.613(a)(b)(c)125-00), 25.619[25-24 25.625(a)(b)(c)(25.23), and 25.789[25-32). ID. CERTIFICATION • Under atilt.* Pad 183. dale Wed above and on optical)* requkernents of Ihe AinvortNneSS 0 Recommend vested by direction of the Administratex and in accordance vet conditions and linstabonis of appointinatt under 14 CFR attached sheets numbered NM have been examined in acwdance wIth ettabaShed ptocedwes and Sound to campy with Slandeds Oiled. approval of these data these data I Me) IlterefOre Approve It SIGNATURE(S) OF DESIGNATED ENGINEERING REPRE$ENTAT1VE(S) 12 DESIGNATION NUMBERS(S) 13. CLASSIFICATION(SI r -r--1 — Paul Redding DERT-410115-CE Structures FAA Form 81104 (03.10) SUPERSEDES PREVIOUS EDITION File Number 1113949-01 Page Tot I SDNY_GM_02755137 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242059 EFTA01327177

SDNY_GM_02755138 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242060 EFTA01327178

0 MAJOR REPAIR AND ALTERATION S eastanice (Airframe, Powerplant, Propeller, or Appliance) Tarnorao, ask' enema amasineen Fan, Panned Os. No. 212oco2o i inor2C07 Etat:coca Tracking Number For FAA Use Only INSTRUCTIONS. Print or ape all entries. See FAR 43.9 FAR 43 Appendix B. and AC 4314 (or subsequent redskin thereof) for in true and ciatoskon a tit's form. This report is required by law (49 U S.C. 1421). Failure to report can rest on a Cava penatly rot to exceed 31.400 for each such nation (Section 901 Federal Analion Act 1958) I. Mrcraft Nationality and Registrant' Mack N493LX Siorial No. RK 244 Make Raytheon Aircraft Company Model 400A Sines 2. Owner mime (As show, or, regnittsensn cerbicaSit) Flight Options .LLC Address (As shown on regisbation certificate) mans 26180 Curtiss Wright PKWY ely Richmond Heiohts Ps. OH zo 44143-145I carih. USA 3. For FAA Use Only A Type 5. Unit identification Repair Altenatean Lint Matte Model Serial Number 0 lE) AIRFRAME (AS daunted In Sat f above) 0 O POWERPLANT 0 • PROPELLER -. • 0 APPLIANCE Type mentoant 5. Conformity Statement A. Agency's Nara and Address B. KIM of Agency we. Nextant Aerospace mom 355 Richmond Road city Cleveland slay OH ze 44143.1453 cony USA 0 V.S. Cedlliated Mechanic 0 !manufacturer O Foreign Cenocated Mechanic C. Certificate No. El cerusared Repair Sudan CRS # 25NR667B 0 Certificated maintenance oromirehon O. lanky that the Ma ander aeration made lo the itt(s) identified in nem 5 above and described on the reverse or attachrents hereto have been male in accordance with the rerrurrernent5 of Pan 43 of the U.S. Federal Aviaan RegutaNans and that the intamanon furnished herein is Ina and correct to the best of my knowledge. Enacted range fuel Per 14 CFR Part 43 App. El 0 SignatureiDate of Aul Anton J. Koprivnik 11Oreer3 Inclrec j r.7 12/29/2013 7. APPrOval for Raunseervice Pursuant to the authOnly given persons petalled beast the unit Wen fled in item 5 was inspected in to manner prescribed by the Ackniriseettor dine Federal Aviation Arkninislealon and Is Egji APPROTED 0 REJECTED FAA FR Standards Inspecla Department ManufaCturer Maintenance Organization DetranAPPrOved by Canadian of Transport BY FAA Designee X Read Sueon Ogler (SPSalY) Inspection Attexcization conics°, Designated No. CRS St 25NR667B soneummeleorAumenzeo tnewsus a , Anton J. Koprivnik 74 ....), " 12/29/2013 FAA Form 337 it ooN SDNY_GM_02755139 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242061 EFTA01327179

SDNY_GM_02755140 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242062 EFTA01327180

NOTICE Weight and belenCe a, operating limitation changes shall be entered in the aPPropriare aircraft record. An alteration must be compatible wrth all previous alterations to assure continued conformity with the applable airworthiness requirements. 8. Description of Work Accomplished Of more space is required, attach additional sheets. Went,* with aircraft nationality and registration mark and date work completed) N493LX Nationality and Registration Mark Title : Replace MD-302 with Round Style Standby Gauges 12/29/2013 Date Aircraft with MD302 digit SAM instruments must be reverted back to using round standby gauges until issues are resolved. Modified Instrument Panel (373.92.4110-14) to allow the installation of the original round standby gauges per drawing NX311-10007.03 Rev A Fabricated round indictor subpanel per drawing NX311-10007-01 Rev B Installed instruments into subpanel and install subpanel into main instrument panel per drawing NX311-10007. See Attached 8110-3 DERT 410115-CE Paul Redding dated November 8, 2013 per Nextant Aerospace EO 1543 Rev D dated October 23, 2013 End K Additional Sheets Are Attached FAA Form 337 (loos) SDNY_GM_02755141 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242063 EFTA01327181

SDNY_GM_02755142 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242064 EFTA01327182

U.S. DEPARTMENT Of TRANSPORTATION FEDERAL AVIATION ADMINISTRAMON STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS I. DATE November 8, 2013 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MAKE Hawker Beechcraft Corporation 1 MODEL NO. 400A 4. TYPE (Ahvn& Engine. PropeNer. oft) Aircraft 5. NAME OF APPLICANT Nextant Aerospace LLC Cleveland, Ohio LIST OF DATA 6 IDENTIFICATION 7 TITLE EO 1543 Rev. D October 23, 2013 ------------------ Replace MD-302 With Round Style aspects only engineering only with the Requirements." not constitute substantiation The electrical separate approval. Gauges. -- Notes: 1) The structural is only for the compliance below as "Applicable 2) This form does necessary for entire alteration. and require — of the above listed data are approved herein. This approval data. It indicates the data listed above demonstrates regulations specified by paragraph and subparagraph listed FAA approval of all the engineering data of compliance to necessary requirements for the requirements are not included in this approval 8. PURPOSE OF DATA: Engineering data in support of major alteration to Hawker Beechcraft 400A, SIN RK-244. 9 APPLICABLE REQUIREMENTS 0.1s1 specific sections) CFR Title 14 Part 25.301[25-23), 25.303[25-23], 25.305(a)(b)(c)[25.23J, 25.307(a)(25-23), 25.582(c)(25-23), 25.601[25-00), 25.603(a)(b)(c)[25-38), 25.605(a)125.00). 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 audio* vested by drec*cn d toe Adrrirestrator and in accordance rah cord:bans and imitator* of appointment ulcer 14 CFR Pan 183. data listed above and on attached sheets numbered Nth have been examined in accordance with eStatilithed prOCedunis and found to comply with applicable requirements of The airstetheinS Standards Listed. 0 Recommend approval of these data I (We) Therefore El Approve these data II. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESEWMTNE(S) 12 OESIGNATION NUMBERSIS) 13 CLASSIFICATIONS) ratVlae— Paul Hedding DERT-410115-CE Structures FM Form 8110-3 (0340) SUPERSEDES PREVIOUS EDITION File Number. H1351841 Page I off SDNY_GM_02755143 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242065 EFTA01327183

SDNY_GM_02755144 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242066 EFTA01327184

t il e/ MAJOR REPAIR AND ALTERATION u 5 zal.eit of (Airframe, Powerplant, Propeller, or Appliance) nssewwnston 0 eon, Munion ReninIstraisca 70nencennes Owe No Woman togas:col Electronk Tradurg Number For FAA Use Only INSTRUCTIONS: Print a type MI entries. See FAR 43.9, FAR 43Apperdix EL and AC 43.9.1 (cc subsequent revition thereonfor insIntiorn and d.sposnion of this tomm. Misreport is required by law fag U.S.C. 1421). Pal...Nolo report can result in acres penalty not lo exceed S1.000 IN each such iolation (Section 901 Federal Ayiaton Act 1958) 1. Aircraft Nationality and Registration Mark N4931.J( Serial No. RK 244 Make Raytheon Aircraft Company Model 400A Series 2. Owner Name (As sbonn on rep)stranion ca ticate) Flight Options .LLC Address (As shown on resibearbn COROD/f0) ORDIRss 26180 Curtiss Wright PKWY eel Richmond Heights sale. OH to 44143-1453 Corso USA 3. For FAA Use Only 4. Typo 5. Unit Identification Repair Alteration UM Make Model Serial timber O El AIRFRAME (As (Jason:v.1m (tern I above) O D POWERPLANT I0 O PROPELLER O O APPLIANCE Type manutenurer 6. Conformity Statement A. Agency's Name and Address 0 'Ord of Agency one Nerlant Aerospace Perin 355 Richmond Road car Cleveland sung. OH 20 44143-1453 CCouvry USA 0 U.S. tearless seeossne kends:lure/ 0 Foreign Cersccaied Mechanic I rtificate No. C. Certificate 0 Certificalpi Repair Station , rcRs# 0 Cerlikated Maintenance Organization 25NR667B 0. I certify that the repair vitior alteration made to me unit(s) klenbeed in deco 5 above and described on Me reverse or tot:tro/Ns here:o have Coen made in itC4:013r.00 with the requrnmonts of Parl 43 of the U.S. Federal Aviation Regulaoons and that the nfornEon furnished herein is true and correct to the DOD of my knowledge. Extended range fuel 14 CFRPart43 APP. Ill O Signaturethate ol Authorized Individual pp Anton J. Koprivnik a ./C . 12/29/2013 7. Approval for Ret Servl Pursuant ba the authority even persons specified belmv, the twit denbfied in hem Admiristrotor el the Federal Aviation Administration and is la APPROVED 5 was II inspected in the manner resorbed by the REJECTED FAA Fe Standards Inspector PAartultxture Maintenance Organization Person Approved by Canadian °enactment of Transport FM Designee X Repair Station ineeedionntenonzabon Other MOW Crick. or Desenabon No. CRS N 25NR667B $itrattestate of Authorized Individua2..7 x54_ i 9 12/29/2013 Anton J. Koprivnik i A i FAA Form 337 (1046) SONY_GM_02755145 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 110242067 EFTA01327185

SDNY_GM_02755146 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024206% EFTA01327186

NOTICE Weight and balance or operating limitation changes shah 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 math and dale work completed) N493LX Nationality and Registration Mark Spoiler Linkage Closeout Modification 12/29/2013 Date Modified the Cockpit Floor Close out Panels Part Number: LH 45A30839.7 (Pilots) and Part Number: RH 45A30839-7 ( Co-Pilots) . Installed Nextant Aerospace Closeout Panel Part Number NX532- 1004-1 between these Panels to allow room for the New Throttle Quadrant to fit under the Center Pedestal This Alteration was FAA Approved by Paul Hedding FAA DERT-410114-CE using a FAA 8110-3 Dated December 28, 2013 using Nextant Aerospace Engineering Order 1563 Rev. 8 Dated December 24, 2013 ICA Continue with Normal Hawker Beech Maintenance Manual Inspection Requirements for this Area End K Additional Sheets Are Attached FAA Form 337 time) SDNY_GM_02755147 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242069 EFTA01327187

SDNY_GM_02755148 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242070 EFTA01327188

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS i. OATE December 28, 2013 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MAKE Hawker Beechcraft Corporation 3. MODEL NO. 400A 4 TYPE (Arcralt Engine. Propeller. ek) Aircraft S. NAME OF APPLICANT Nextant Aerospace LLC Cleveland. Ohio LIST OF DATA 6 IDENTIFICATION 7 TITLE EO 1563 Rev. B December 24, 2013 ..--.--- Spoiteron Linkage Closeout Modification. END Notes: 1) The structural aspects only of the above listed data are approved is only for the engineering data. It indicates the data listed above compliance only with the regulations specified by paragraph below as 'Applicable Requirements." 2) This constitutes FM approval of all the engineering data substantiation of compliance to necessary requirements --------- herein. This approval demonstrates and subparagraph listed necessary for for the entire alteration. a. PURPOSE OF DATA. Engineering data in support of major alteration to Hawker Beechcraft 400A, SIN RK-244. 9. APPLICABLE REQUIREMENTS (UM ipecac 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), 25.601[25-00], 25.603(a)(b)(c)[25.38), 25.605(a)[25-00j, 25.607[25-23], 25.609(a)(b)[25-00), 25.611[25.23), 25.613(a)(b)(c)[25- 00]. 25.619[25-2n and 25.625(a)(b)(c)(25.23). 10 CERTIFICATION • Under authority Part 163, dela listed above and en ac liable requirements of We Airtatberess veiled by Brecon of Ire Adminielrefor and In accordance with cordnorts and Invlatons ot appointrnere under 14 CFR attached sheets numbered NIA have been inarnhed In accordance web established procethees and Mond to comely wan Standards Listed. approval of these data these data . Recommend I (We) TherelOre C Approve I I. SiGNATUREIS) OF DESIGNATED ENGINEERING REPRESENTATNE(S) 12 DESIGNATION NUMBERS(S) 13. CLASSIFICATIONIS) 1.19. /— Paul Hedding DERT-410115-CE Structures FAA Form 81104 (03-10) SUPERSEDES PREVIOUS EDITION Fite Number 1413950.01 Papa 1 el I SDNY_GM_02755149 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024207 I EFTA01327189

SDNY_GM_02755150 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242072 EFTA01327190

S Dapaterital Of Ten/Plealeel News *sawn Adifttelleekte MAJOR REPAIR AND ALTERATION (Airframe, Powerplant, Propeller, or Appliance) rem Approroci OMB the 21204020 IfielY2C07 EtectraticTraclerg Ambit For FAA Use Only INSTRUCTIONS: Print Cr type all entries See FAR 43.9. FAR 43 Appendix 8. and AC 43 94 (or subsequent revson thereof) Ice indruCikass and disposition of (Ns !sm. This report is required by law (49 U.S.C. 1421). Failure lo report can rcsub in a cvs penalty not to exceed 11.000 for each such violate:ft (section 901 Federal Reseal Act 1956) 1. Aircraft 2. Owner Nabonairy aid Registration Mark N493LX Serial No. RK 244 Make Raytheon Aircraft Company Name (AS sham on rag:oath:on certithafe) Flight Options .LLC Model 400A Senn Address (As shown on rathafrabon carbficare) moths 26180 Curtiss Wright PKWY Cey Richmond Heights suit OH iv 44143-1453 co,riry USA 3. For FAA Use Only 4. Type 5. Unll Identification Repair ',Aeration Una Make Model Serial Number AIRFRAME (As deserted in nem r above) POWERPLANT PROPELLER APPLIANCE thew manischew 6. Conformity Slat ment A. Agency's Name and Address Nextant Aerospace U.S. Celli tmed Mechanic 0 I Manufacturer mth. mo.th 355 Richmond Road 0 Foreign Certificated Mechanic C. teacart No. cey Cleveland yr. OH St Certificated Repair Szabon zc 44143.1453 Cony USA 0 Certificated Maintenance Organizatice, CRS # 25NR6678 B. Kind of Agency D. I ceney that the repair ardor alteration made to the uNt(s) iderilifed in den 5 above and devAbed on the revere. Cr allachmenls hereto have been made In accordance with the requirements of Part 43 of the U.S. Federal AMIN, Regulabors and that the thIcemalion furnished herein is true and correct to the best of my knowledge. Extended range fuel per 14 CFR Part 43 App.B Anton J. Koprivnik Signature/Date of Asti:deed Indwidua ic; sI trrie, 7. Approval for Return to Service 12129/2013 Pursuant to the authority given peruse specified blow. the unit identSed in item 5 was Inspected in the mime( prescribed by the Administrator of the Federal Adaiken Administration and is 0 'AVOWED 0 REACTED 8Y FM FR Standards InspeClOr Manufacturer Maintenance Organization Person Approved by Canadian Department ci Transport FM Designee X Reps Station Inspect:an Aufitheization Other (SWAY) Certificate or Designation NO. CRS ft 25NR6678 FAA Form 337 BOOB Sign %regale &Authorized I nainsiagsp Anton J. Koptivnik 12/292013 SDNY_OM_02755151 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242073 EFTA01327191

SDNY_GM_02755152 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242074 EFTA01327192

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 enure continued conformity with the applicable almortflineSa requirements- 8. Description of Work Accomplished (If more space is requited, attach additional sheets. Identify with aircraft nationality and registration mark and dale work completed.) N493LX Nationality and Registration Mark Nextant Aerospace Carried out a Repair to the Horizontal Stabilizer Ribs 12/29/2013 Using Nextant Aerospace Kit Part Number NXK-128-6200 Rev B. Dated July16. 2012. The following Ribs were replaced. NXR-45A21112-007 NXR-45A21113-007 NXR-45A21101.021 NXI1-45A21116-007 NXR-45A21117-007 Rib — H Stab Cant STA 13.779. Rib — H Stab Cant STA 29.921. Rib — H Stab Cant STA 46.063. Rib — H Stab Cant STA 62.205 Rib — H Stab Cant STA 78.346 The following Ribs were not Replaced as there was not Damaged. NXR128-620020-001 NXR128.620020.002 Date This Kit was FAA Approved by Paul Hedding DER-T 410115-CE Structures on an FAA 8110-3. Dated June 12, 2013. Using Nextant Aerospace Engineering Drawing NXR-128-6200 Rev B Dated July 16.2012 END K Additional Sheets Ate Attached FAA Form 337 ham SDNY_GM_02755153 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242075 EFTA01327193

SDNY_GM_02755154 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242076 EFTA01327194

U S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS 1. DATE June 12, 2013 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MAKE Hawker Beechcraft Corporation 3 MODEL NO 400A 4. TYPE (alectalt. Enprna Propene,. etc) Aircraft S. NAME OF APPLICANT Nextant Aerospace LLC Richmond Heights, Ohio LIST OF DATA 8 IDENTIFICATION 7. TITLE NXR-128-6200 Rev. B July 18, 2012 NXR-45A21112-007 Rev. C July 13, 2012 NXR-45A21113.007 Rev. B July 13, 2012 NXR-45A21114-007 Rev. El July 13. 2012 NXR-45A21115-007 Rev. C July 13, 2012 NXR-45A21101-021 Rev. A July 19, 2012 NXR-45A21116-007 Rev. B July 13.2012 NXR-45A21117-007 Rev. B July 13. 2012 Kit — Horizontal Stabilizer Rib Replacement Installation Instmclions. Rib — H Stab Cant STA 13.779. Rib — H Stab Cant STA 29.921. Rib — H Stab Cant STA 46.063. Rib — H Stab Cant STA 46.063. Rib Assy — H Stab Cant STA 46.083. Rib — H Stab Cant STA 62.205. Rib — H Stab Cant STA 78.348. a. PURPOSE OF OATA. Engineering data to support repair procedure for Horizontal Stabilizer PIN 45A21002.0121 on Hawker Beechcraft 400A SIN RK-244. 9. APPLICABLE REQUIREMENTS Oast specific seams) CFR Title 14 Part 25.301[25-231, 25.303[25-23I, 25.305(a)(bftc)[25-23), 25.307(a)(25.23J, 25.601[25-00]. 25.603(a)(bftc1125-381, 25.605(a)(25-00), 25.607[25-2n 25.609(a)(bft25-00], 25.611[25-23], 25.613(a)(b)(c)(25- 00], 25.619(25-23J, and 25.625(a)(b)(c)(25-231. I0. CERTIFICATION - Under authority Pen in data seed above and on apPlicable requirements of the Favronaineas veiled by &ec%on or tie Admire:W*1er and in at-cadence watt ccadltions and liermatons of appointment un0er 14 CFR attached sheets marcane 2_ have been examined in accordance YAM estaNished prorAdures and found to comply rah Standards Listed. approval of dine data these data • Recommend I (We) Therefore E Approve I I. SIGNATLIRE($) OF OESIGNATED ENGINEERING REPRESENTATNE(S) 12. OESIGNATION NUMBERS(S) 13. CIASSIFICATION(S) teacP4L Paul Redding DERT-410115-CE Structures FAA Form 8110-3 (OS WI SUPERSEDES PREVIOUS EDITION Fie /lumber H13370.01 Page 1 of 2 SDNY_GM_02755155 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242077 EFTA01327195

SDNY_GM_02755156 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242078 EFTA01327196

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION AOMNiSTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS 1. 0.47E June 12, 2013 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2 MAKE Hawker Beechcraft Corporation 3. MOOEL NO. 4OOA 4. TYPE (Aerie. Engine. Propeller. efc.) Aircraft S. NAME OF APPLICANT Nextant Aerospace LLC Richmond Heights. Ohio LIST OF DATA 6 IDENTIFICATION 7 TM E END Notes: 1) The structural aspects only of the above listed data are approved herein. This approval is only for the engineering data. It indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and subparagraph listed below as 'Applicable Requirements.' 2) This form constitutes FAA approval of all the engineering data necessary for substantiation of compliance to necessary requirements for the entire repair. e. PURPOSE OF DATA. Engineering data to support repair procedure for Horizontal Stabilizer PIN 45A21002-0121 on Hawker Beechcraft 400A, S/N RK-244. 9. APPLICABLE REQUIREMENTS (list swank sectOns) CFR Title 14 Part 25.301[25-23), 25.303)25-23], 25.305(a)(bftc))25-23], 25.307(a)[25-231, 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)(bftc)(25-23). 10. CERTIFICATION • Under autftnly Pad 113, data wed above and on applicable requirements 04 the Avwxtnaress vested by eirecdee ca the Administrator and in accordance with conditions and smarms of appetranwnt under la CFR attached sheets numbered _z_ have been Ozirrined 01 ac dance with eStatiithed protectors and round to corn* v401 Standards limes approval of these data these data • Recommend I (We) Therefore 0 Approve II SIGNATURE($) OF DESIGNATED ENGINEERING REPRESENTADVE(S) 12. DESIGNATION NVIABERS(S) 13 ClASSIFICATION(S) ' If-V.9-- Paul Hedding DERT-410115-CE Structures FM Form 131104 (03-10) SUPERSEDES PREVIOUS EornoN Hie Winter. H13370.01 Page 2 of 2 SDNY_GM_02755157 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242079 EFTA01327197

SDNY GM 02755158 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242080 EFTA01327198

0 3 1 MAJOR REPAIR AND ALTERATION 9.5 Omannwor a tam Apremea OM No.21204020 ii/30rXIM Electronic Tracklna Matter trinsemiem (Airframe, Powerplant, Propeller, or Appliance) For FAA Use Only Federflerliefra• Afinktiereke INSTRUCTIONS: Print:4'09e all fl ier Set FAR 43.9, FAR 42 Appendix B, and AC 43.9.1 (cc subsequent revision thereof) for Inatnxborts and Oepoelon of Das Wm. This report is rewire] by law (49 U.S.C. 1421). Failure to sport can result In crinl penalty not to exceed V .000 b each such rialtos (Section 901 Federal Aviation AMISS") 1. Aircraft Natkonality and Reg:snow Mark f4493LX Serial No. RK244 Make Raytheon Aircraft Company Model 400A Series 2. Owns NOT* (As Mown on inarab0n mace*, Flight Options, LI: Address (AS Siam on registration Migrate) Arness26180 Curtiss Wrioht PINNY enRichrnond Heights stat42997 ip44143-1453 ediar04118 3. For FAA Use Orly 4. Type 5. Unit Identification Repair Alteration Um, mese model Serial Number El .4 AIRFRAME (As deserted in hem t atom) 0 O POWERPLANT 0 • PROPELLER . II APPLIANCE Type sorwtariurer 6. Conformity Statement k Agency's Name and Address B. K rd OlAgenCY Har•Constant Aviation 0 U.S. cenecateo mechanic 0 MwiAacturer reeys4211 Secondary Road 0 Foreign Certificated Mechanic C. Cortical', No. core Invelancl sweOhio SI centr•catee Repair Station CRSINVC7R346J se44135 owswUnited State; 0 Certificated uweeseanse Organization 0. I certify that me repair arclior alteration made to the urt4(s) identified in e.ern 3 above and described on the reverie et attachments hereto have been nude in accordance win the requiem/nu. ci Pan 43 ol the U S Federal Aviation Reptilian and that the informal= furnished herein is true and correct to the best 01 my knowiedge. Extended raro$ NM per 14 CFR Pert 47 APO. B Sitnalurt(Dala Authorized Individual Date: December 30. 2013 7.47ro ,tum to Service Putsuam to me aulhomy even persons speared below. the und ideOb CO in dent AdelettfelOt of the FederalAnal= Adrrirestralion and is 0 APPROWD 5 was U inspected is the manner prescribed by the REACTED FM Fe Standards IASOCCIOI folaftleICIOref Maintenance Organization Person Approved by Canadian Departnent ci Trust= BY FM Designee X Repair Station Inspection Authonzatron Ogler (spear) Ceillkele Of Desgriabon No CRSFANC7R346J SiOntlfUfel0 or A Inc r. Date: December 30. 2013 4: `9 / efla----- FAA Form 337 tuna) SDNY_GM_02755159 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024208 I EFTA01327199

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alterabbn must be compatible with all previous alterations to assure continued conformity with the Baehr...able airworthiness RIQUIRNNINNS. 8. Description of Work Accomplished (f more space is required, attach additional sheets. Identify with aimmft nano:teary and registration mark and date work completed) N493LX Nationality and Registration Mark 12/30/2013 Date ACCOMPLISHED INTERIOR REFURBISHMENT/MODIFICATION AND 3 PLACE DIVAN INSTALLATION THE FOLLOWING AIRCRAFT INTERIOR ITEMS HAVE BEEN REFURBISHED' Repainted. recovered control °Arms MA Matte Black Leather Accordance wish Beath« 400A MIM 207040.701. 25-00-C43-001 Removed and Retraced Glare shied and Eyebrow panel materiel with Matte Black Leather ri Accordance with Beeehjet 400A Mid 204041201 Removed and Rep:aced COPPS Sidewell material with Matte Meta Leather m Accordance with Beecher 400A MAI 216100.201 Removed and replaced Pilot Seal Pan Number TABH100P1.40001 Serial Number 62. Foam and recovered with Garrett Shrepskn Oak and Excel Cappuccino Lanier. Removed and replaced Co -Pilot Seal Pan Number TABH100CM00-01 Serial Number 246. Foam and recovered with Garrett Sheepskin Oak and Excel Cappuccino Leallier. Removed and Ref/Laced Left Hard II Passenger Seal Part Number 2524.014(-530A) Serial Number 9907114 Foam and recovered with Towncend Leather (Heritage Brown) Removed and replaced Right Hard re5 Passenger Seal Pan Number 252443148130W Serial Number 990426-7 Foam and recovered with Townsend Lealner(ientape Brown) Removed and Replaced left Hard /A5 Passenger Seat Pan Number 2524-0i4(53CE)Senal Number 03%18-5 Foam and recovered with Townsend Leather (Flerrage &trim) Removed and replaced R.ghl Hand #7 Passenger Seat Part Number 2524.014(530A) Serial Number 030706.2 Rani and recovered weth Townsend Leather (Henlage &own) THE FOLLOWING MANUALS AND APPROVED DATA HAVE BEEN UTILIZED FOR BASIS OF REFURBISHMENT Skandia Flammabaty Test S254978 as approved by FM DER Jane Biterssein (DERY 532780-CE) on FM form 8110-3 dated 4/23/2013 Flame Out Flammability Test 4311 as approved by FM DER Herb Reed II (DERT-230293GE) on FM Form 8110.3 dared 12)2312013 Skandia FlarnmahPlY Test Report TP 22681 Rev A as approved by FM OER Jane Biberstein( DERV-032780-CE) on FM Form 81101 dated 05/022013. Thee Place Divan insueltabos Installed (3) Papa delan pan Number 32-0396(ASOPT)T123 KO2 SM 003702 In Accordance vote Aviation rabncaton STC# 5701572Mo/id Skandia Frannie/my teal report 5254978 per Jane Biterstein FM DER (DERV-832760CE) dated 4r23-2013 THE FOLLOWING INTERIOR I uts HAVE BEEN MODIFIED UR Gaily Any. Ml Galley Any. Divan Any. 1M Galley Ash and InsINI per Delta G drawing OGD-CA01.101 Rev 0. 060-CA01-101 CO E-I. UK Gale)/ Install DGD-CA01-501 Rev LO A-1. OGO-CA01-501 Rev IR as approved on FM Ohm 8110-3 per FM DER Donald Glesple (DERT•T50135SW) dated Minh 25 2013 Ml Casey Assy and Instal per Della G drawings 000-CA02-10i Rev B. OGD-CA02-501 Rev IR as approved on FM tam 81104 by FM DER Donald Galion (DERT.750155•SW) Mad March 25, 2013. Divan Any pet Della G drawings OGITCA09-10I Rev C and DGD-CA09-101 ED 0-1 as approved on FM town 5110.3 per PM DER Donald Gas» (DERT 750135•SW) dated Mardi 25, 2013. Benner KB Sidewal any drawing 25510038 Rev C. Benner Sidetedge any draWng 2592-0002 Rev C. Banner Kit Foldout Table any drawings 2553-0041 Rev C and 25510040 Rev B. Bonner /CT liner K4 Ina drawing 2553.0037 Rev C as approved on FM kern 81113 per Stephen Kenna DERT-230238-CE dated Dec 28. 2013 INSTRUCTIONS FOR CONTINUEDAIRWORTHINESS' THE REMOVAL OF THE INTERIOR IS ON THE CONDITION OF FAILURE THERE ARE NO ADDITIONAL INSPECTIONS REQUIRED. CONTINUE TO INSPECT WW MANUFACTURERS ANAL SRM. OR CAVA AS APPLICABLE AIRCRAFT EOUa4ENT LIST AND WEIGHT AND BALANCE WERE UPDATED 8Y THE CUSTOMER -END- O Additional Sheets Are Attached FM Form 337 (1006) SDNY_GM_02795930 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242082 EFTA01327200

U S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WIlli THE FEDERAL AVIATION REGULATIONS DATE Dee 26, 2013 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Beechcrali Corporation MODEL 400A TYPE (Airplane. Ratio. Ile)leopyr. etc) AIRPLANE NAME OF APPLICANT NEXTANT Aerospace Cleveland OH. LIST OF DATA IDENTIFICAITON TITLE REPORT: BEECHJ ET 400A INTERIOR STRUCTURAL SUBSTANTIATION BEECHJET 400A XTI LINER KIT INSTL. Beech jet 400A, Aircraft Serial No. RK-244 Certification Bases for this aircraft modification is per Type Certificate Number A I6SW 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 ( bit specific section.p) 14 CFR Pan 25 §.301, 303, 305, 307a), 365, 561, 571, 601, 603, 605, 609, 613 CERTIFICATION - Under authority of appointment under Pan 183 oldie have been vesled by direction of the Administrator and in accordance with conditions rodent' Aviation Regulations, data listed above and on attached sheets examined in accordance with established procedures and found to con* Regulations. approval of these data Approve these data and limitation numbered with applicable requirements of ihe Federal Aviation I (PK) Therefore 0 Recommend SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) Stephen Farness DERT-230238-CE STRUCTURES AND DAMAGE TO ' • FAA Farm 8110-3 in.zl surnsrm.s ptivicos minow GPO 901 SDNY_GM_02755161 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242083 EFTA01327201

SDNY_GM_02755162 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242084 EFTA01327202

LYE products engineering services. inc. 2946 S. Hvd rook Wilita, Kansas 67216 TI: 316.524.4466 FAX: 316.524 4455 STRUCTURAL ANALYSIS REPORT Forward Calley Cabinet Modifications - Beechcraft Model 400A, RK-244 & RK-305 Document No: 313-ST-001 Revision IR PREPARED BY: Robert F. Clossin Date: December 24, 2013 APPROVED BY: APPROVED BY: Chris Cocklin Robert F. Clossin Manager - Design Engineering President THIS DOCUMENT CONTAINS INFORMATION OF A PROPRIETARY NATURE AND SHALL NOT BE TRANSMITTED, REVEALED, OR DISCLOSED TO ANYONE WITHOUT THE EXPRESS WRITTEN PERMISSION OF LEE PRODUCTS ENGINEERING SERVICES, INC. ADDITIONALLY, USE OF THE INFORMATION IS PROHIBITED EXCEPT WHEN EXPRESSLY AUTHORIZED BY LEE PRODUCTS ENGINEERING SERVICES, INC. SDNY_GM_02755163 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242085 EFTA01327203

Lee Products Engineering Services, Inc. STPIICTUPAI ANAI YSIS REPORT 313-ST-001 REV. IR PAr;F ii REVISION RECORD Revision Date Description Approval IR 12/24/13 Initial Release See Cover Sheet SDNY_GM_02755164 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242086 EFTA01327204

Lee Products Engineering Services, Inc. STRUCTURAL ANALYSIS REPORT 313-ST-001 REV. IR PAGE iii TABLE OF CONTENTS 1. INTRODUCTION 1 2. REFERENCES 2 2.1 CONSTANT AVIATION DRAWINGS 2 2.2 APPLICABLE SUPPLIER DRAWINGS (AVIATION FABRICATORS) 2 2.3 APPLICABLE LPESI REPORTS 2 2.4 APPLICABLE GOVERNMENT DOCUMENTS 2 3. CERTIFICATION BASIS 2 4. DESCRIPTION 3 4.1 GENERAL 3 4.2 RH FORWARD GALLEY ASSY & INSTL 3 4.3 RH FORWARD DIVAN MODIFICATION 4 4.4 LH FORWARD GALLEY ASSY & INSTL 5 4.5 LH AFT LAVATORY EXTENSION 7 5. STRUCTURAL SUBSTANTIATION 7 5.1 LH FORWARD GALLEY ASSY & INSTL 7 6. CONCLUSION 8 APPENDIX A A.1 SDNY_GM_02755165 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242087 EFTA01327205

Lee Products Engineering Services, Inc. STRUCTURAL ANALYSIS REPORT 313-5T-001 REV. IR PAGE 1 1. INTRODUCTION The purpose of this report is to demonstrate the structural substantiation to applicable 14 CFR Part 25 regulations as they relate to the installation and modification of various interior cabinets on Beechcraft Model 400A, S/N's RK- 244 and RK-305, for a FM Form 337 major alteration, performed by Constant Aviation at their Cleveland, OH facility. The installations consist of the replacement of new RH and LH forward galleys, and modification to the existing closet frame, an extension of the aft lavatory, and a modification to the side-facing divan with the manufacturer's approval. Everything except the new LH forward galley has been accomplished on a previous modification as documented in LPESI Report 222-5T-001. Therefore, only the new galley will be discussed and analyzed in this report. The floorplan for the two (2) Beechcraft Model 400A aircraft is as shown below. Figure 1-1 — Floorplan SDNY_GM_02755166 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242088 EFTA01327206

Lee Products Engineering Services, Inc. STRUCTURAL ANALYSIS REPORT 313-ST-001 REV. IR PAGE 2 I 11 2. REFERENCES 2.1 Constant Aviation Drawings Drawing No. Rev. Title • NXT0213-01 IR LH Galley Assembly NXT0213-02 IR LH Galley Installation NXT0213-05 IR Weight Placard Installation NXT0313-01 IR RH Galley Assembly NXT0313-02 IR RH Galley Installation NXT0313-03 IR Divan Assembly NXT0313-07 IR 4" Lay Ext 2.2 Applicable Supplier Drawings (Aviation Fabricators) Drawing Ni. " Rev. 1 • Title " D-10666 A 3 Place Divan Installation (STC ST01572WI) 2.3 Applicable LPESI Reports Drawic•ig 14.1). . . ilvi 4 Title 222-ST-001 B Miscellaneous Cabinet Modifications - Beechcraft Model 400A 2.4 Applicable Government Documents Dotu nit Document ?Re‘i::: ; TitIO, , 14 CFR Part 25 See Sect. 3 Airworthiness Standards: Transport Category Airplanes ANM-115-09-017 1/28/10 Interaction of Interior Structures, Including Seats 3. CERTIFICATION BASIS The Beechcraft Model 400A certification basis is defined Type Certificate Data Sheet (TCDS) Al6SW, Rev. 28, the Certification Basis is 14 CFR Part 25 dated February 1, 1965, including Amendments 25-1 through 25-40. The individual 14 CFR Part 25 subparagraphs that will be discussed herein are: 25.301(a)(b)(c) 25.303 25.305(a)(b) 25.307(a) Loads (Amdt. 25-23) Factors of Safety (Amdt. 25-23) Strength and Deformation (25-23) Proof of Structure (Amdt. 25-23) SDNY_GM_02755167 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242089 EFTA01327207

Lee Products Engineering Services, Inc. STRUCTURAL ANALYSIS REPORT 25.341(c) 25.561(a)(b)(c) 25.601 25.603(a)(b) 25.605 25.607(a)(b) 25.609(a)(b) 25.613(a-e) 25.625(a)(b)(c) 25.787(a)(b) 25.789 4. DESCRIPTION 313-ST-001 REV. IR PAGE 3 Gust Loads (No Amdt.) Emergency Landing Loads - General (Amdt 25-23) Design and Construction - General (No Amdt.) Materials and Workmanship (Amdt. 25-38) Fabrication Methods (No Amdt.) Fasteners (Amdt. 25-23) Protection of Structure (No Amdt.) Materials Strength Properties ... (No Amdt.) Fitting Factors (Amdt. 25-23) Stowage Compartments (Amdt. 25-38) Retention of Items of Mass ... (Amdt. 25-32) 4.1 General The modification of the Model 400A aircraft consists of replacing the existing RH and LH forward cabinets with new assemblies, modifying the RH forward 3- place side-facing divan by refurbing the divan, and modifying the existing LH aft lavatory cabinet by extending its cabinet structure to close out the area around it. All but the new LH galley are previously installed and certified on previous 400A aircraft, and analyzed in LPESI Report 222-ST-001. 4.2 RH Forward Galley Assy & Instl The NXT0313-01 RH forward galley assembly (installed per NXT0313-02) is the same as that previously installed on other Model 400A aircraft. An illustration of the galley in Figure 4-1. SDNY_GM_02755168 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242090 EFTA01327208

Lee Products Engineering Services, Inc. STRUCTURAL ANALYSIS REPORT 313-ST-001 REV. IR PAGE 4 Figure 4-1 - RH Forward GalleyAssy (Contact Pad on Upper Area Not Shown) The galley is manufactured from strong lightweight 0.50-inch thick ATR-FP- 501F2 Nomex/fiberglass composite panels from AAR Composites, and fabricated using ATR panel pin construction. The RH forward galley is installed between the existing RH forward structural partition (which separates the flight deck with the cabin) forward of it and the 3-place side-facing divan immediately aft of it. The lower wider section of the cabinet also encloses the aircraft's air conditioning evaporator mounted separately to the floor structure underneath. 4.3 RH Forward Divan Modification The NXT0313-03 3-place side-facing divan assembly consists of new drawer and fascia door panels onto the existing structural divan frame (Aviation Fabricators D-10666 STC'd Installation Kit - STC ST01572W1). It has also been installed in previous Model 400A aircraft, and analyzed in LPESI Report 222-ST-001. An illustration of the divan assembly is provided in Figure 4-2. SDNY_GM_02755169 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242091 EFTA01327209

Lee Products Engineering Services, Inc. STRUCTURAL ANALYSIS REPORT 313-5T-001 REV. IR PAGE 5 Figure 4-2 - RH Forward Divan Mod The divan closeout panels are manufactured from strong lightweight 0.50- inch thick ATR-FP-501F2 Nomex/fiberglass composite panels from MR Composites, and fabricated using ATR panel pin construction. The STC'd divan frame installation consists of a structural frame (bottom only - no seat backs, cushions form the divan backs), restraint systems consisting of lap belts and shoulder harnesses for all three (3) seated positions, and a D-106699 floorboard modification installation underneath the divan. The frame installed in eight (8) places into the existing cabinet "Brownline" seat track extrusions (inboard and outboard). 4.4 LH Forward Galley Assy & instl The NXT0213-01 LH forward galley assembly is a traditional aircraft galley and is located between the flight deck and the entry door, directly aft of the existing LH forward structural partition (bulkhead). The new galley replaces an existing galley of similar design and the same size. In fact, this new galley assembly is the same as previously installed in other Model 400A aircraft, and analyzed in LPESI Report 222-ST-001, except for a minor change to the upper forward portion of the cabinet. As can be seen in a comparison of the galley illustrations below and Fig. 4-3 of 222-ST- 001, the change consists of eliminating the small recessed condiment tray drawer and extending (down) the existing compartment to compensate. The galley is manufactured from strong lightweight 0.50-inch thick ATR-FP- 501F2 Nomex/fiberglass composite panels from AAR Composites, and fabricated using ATR panel pin construction. An illustration of the LH forward galley is provided in Figure 4-3. SDNY_GM_02755170 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242092 EFTA01327210

Lee Products Engineering Services, Inc. STRUCTURAL ANALYSIS REPORT Figure 4-3 - LH Forward Galley Assy 313-ST-001 REV. IR PAGE 6 The LH forward galley is installed per NXT0213-02 and is installed utilizing the same existing installation attachments - five (5) screw/insert attachments into the existing partition and four (4) floor attachments (2 into the existing seat track and 2 into existing floorboard mounts, and is the same as the previous NXT0313-05 installation analyzed in LPESI Report 222-ST-001. The empty cabinet weights 86.15 pounds (less than the 90.61 pound galley analyzed in LPESI Report 222-ST-001) and the total placarded content weight (Ref. NXT0213-05) of 141.0 pounds (only 1.0 pound more than the 222-ST-001 analyzed galley). Therefore, the total installation weight of the NXT0213-02 galley is 3.46 pounds lighter than that analyzed in LPESI Report 222-ST-001, and is therefore structurally substantiated by comparison. SDNY_GM_02755171 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242093 EFTA01327211

Lee Products Engineering Services, Inc. STRUCTURAL ANALYSIS REPORT 313-ST-001 REV. IR PAGE 7 4.5 LH Aft Lavatory Extension The NXT0313-07 LH aft lavatory modification consists of augmenting the toilet cabinet with new panels and compartments between the existing cabinet and the RH aft partition. An illustration of the modification to the aft lavatory is shown in Figure 4-4 (new components in gray). Figure 4-4 - LH Aft Lavatory Extension This is the same as previously analyzed in LPESI Report 222-ST-001. 5. STRUCTURAL SUBSTANTIATION The structural analysis will be generated using traditional means based on conservative assumptions. In determining the Margin of Safety (MS), the resulting analytical result will be subtracted from 1.0 so that any MS greater than 0.0 is considered a positive margin. Also, MS's greater than 3.0 will be listed as "+Ample". 5.1 LH Forward Galley Assy & Intl The critical loadings for the LH forward galley are the 9.0g forward and 3.5g side load conditions. However, since the new galley weighs 3.5 pounds less than the previously analyzed galley, is of similar shape and design, includes that same installed equipment, and utilizing the same aircraft attachment points, the new galley assembly and installation is therefore structural substantiated by comparison. SDNY_GM_02755172 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242094 EFTA01327212

STRUCTURAL ANALYSIS REPORT Lee Products Engineering Services, Inc. 313-ST-001 REV. IR PAGE 8 The largest placarded drawer is the top, center drawer in the lower section of the galley, which is placarded for 45.0 pounds. The drawer is restrained by a standard Actron paddle latch, P/N A23511-1S. The applied load to the latch is (the drawer itself + hardware is 5.0 pounds): Applied Load = (5.0 lbs + 45.0 Ibs) x 3.5g x 1.15ff = 201.3 pounds The minimum load rating for the A23511 paddle latch by its manufacturer is 225.0 pounds. The resulting margin of safety is: M.S. = 225.0 Ibs / 201.3 Ibs) - 1.0 = +0.12 6. CONCLUSION Based on the above structural analysis, the new cabinets and modification and their installations, listed in Sect. 2.1, into the aircraft have been shown to be compliant with the applicable 14 CFR Part 25 regulations, as defined in Sect. 3 with positive margins of safety. SDNY_GM_02755173 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242095 EFTA01327213

Lee Products Engineering Services, Inc. STRUCTURAL ANALYSIS REPORT APPENDIX A 313-ST-001 REV. IR PAGE A.1 O el olwratuttre L I N 0 n h e i - 'I ivqg I 1 2 • O hh t II I lit AEI y4yto 5 I I N 4- n I O SDNY_GM_02755174 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242096 EFTA01327214

U. S. DEPARTMENT OF TRANSPORTATION - MATE 412312013 FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION , 2.MAKE Raytheon 3.MODEL NO. 400A 4,TTPEMITFIme. Ent** PeOptite. NO Airplane SRAM 0F APPLICANT Constant Aviation-CLM . . LIST Or DATA 6 IDENTIFICATION— tint E Design Data S254976 Rev NC Skandia, Inc. Flammability Test desalts Bunsen Burner Testing Test Specimen P/N's Cont 25 (represents main entry door trim) 27 (represents upper med surround) 28 (represents lower med, lowerMed surround, lh aft blIchcl) 29 (represents pax seat back shrouds, arms, crash pad) 30 (representsseat shrouds) 31 (represents entry Steps, cockpit ped step) 33 (represents cntri coiumn boots, rudder boots) 34 (regreSentsckpt defog Vent closeout) 35 (represents table shrouds) 36 (represents dada and street' closeout) 39 (represents crew seats) Notes: 1) Work accomplished under Skandia Inc. WO *254976-13, Ref Document ID 93650. 2) flammability lestwitnessing only, does not constitute installation approval of materials. 3) IAW Skandia Flammability Streamline Testing Test Plan 21306, Rev IR, Dated 11(03111 Page 2 8,PURPOSE OF DATA Demonstration of compliance with material flammability regtilrements for S/N TUC-244 gAPPLICPtSLE REQUIREMENTS (List sP44lEctleettbm) 14 CFR Part 25:853 (e) Arndt 25416 Appendix F Pant MO) Arndt 25.111 14 CFR P0425.853 (a) Amdt 25.116 AppeDda F Pan I (p)(1Xii) 14 CFR Part 25.855 (d).Amdt 25.116 Appendbc F Pert I (6) . . 1 °CERTIFICATION.- Under authority veiled by direction of the of appointment under 14 CFR Part 153, data listed above and examined in accordance with established probedures endfound Standards listed. O Recommend approval of these data I (We) Therefore .—.) (Approve these data Administratorand In accordance withikondkiona and limitations on attached sheets numbered i — ..)-- have been to comply with applicable requirements of the Airworthiness • 11.SIONATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE NUMBER(S) ia.GLASSIFICATION(S) (:V V1Q /lt) . (_50a0,2,19±14A - Jane Bibers in -FM DER DERY-032780-CE' Structural Special FAA Form 8110-3 (0M0)SUPERSEDES PREVIOUS EDITION SDNY_GM_02755175 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242097 EFTA01327215

SDNY_GM_02755176 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA _00242098 EFTA01327216

3OLG-CON)3231)____ US. DEPARTMENT OF TRANSPORTAtiON FEDERAL AVIATION AOMMISTRATON STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS 1. DATE March 25, 2013 AWCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MAKE Beechlet 3 MODEL NO. 400A t TYPE peipieni I. Reek N06:teree eft) AIRPLANE 6. NAME OF APPLICANT Constant Aviation Cleveland, Ohio UST OF DATA e IDEISTINCATION 7 TILE Document No. DGD-CA08-501 REV: IR Dated: 8/13/12 DOD-CAN-101 REV; C Dated: 1125113 OGD-CA09-101 EO: 0-1 Dated: 2/28/13 CIGD-CA13-101 REV: IR Dated: 2/28/13 DGD-CA14-101 REV: IR Dated: 1131113 ARMREST RI-I INSTL DIVAN ASSY DIVAN ASSY CARD TABLE ASSY LAV CLOSET FRAME ---------• End of Data NOTES' MOD is for Beechlet model 400A (Nextant 400XT variant) S/N RK-244 only. Is for the structural design aspects only on the above listed data and an Installation approval. only for regulations specified In the "Applicable Requirements" block. with additional regulations not listed herein may be required. This form FAA approval of all engineering design data for the entire Additional 8110-3 approvals may be necessary for Damage Tolerance, Mechanical Systems, Electrical, Weight & Balance, as well as other basis, refer to TC data sheet No. A16SW Approvals are provided separately. 1. This approval 2. This approval does not constitute 3. Approval Is Compliance does not constitute alteration. Flammability, disciplines. 4. For certification 5. Structural 5. PURPOSE OF DATA To provide type data fo FAA approval of structure In support of a return to service on SIN RK-244. This approval Is for design data only on a major alteration and is not an Installation approval. _ 9. APPI.CAME REQUIREMENTS (Ust specific &soon) 14 CFR Part 25.601 Arndt 25-0, 23.60300(b). Amdt 25-3S, 25.605 Arndt 25-0, 25.609 Arndt 25-0,25.611, Arndt 25-23,25.613 (eXti)(r) Arndt 25-0, 25.619 Arndt 25-23, 25.625 Arndt 25-23, 25.785 000/XeXdXIXO Moth 25-32, 25,789 Amdt 25-32 10. CERTIFICATION - Under authOrIty Rai 163. data )sled above and rah epplcabk rearmaments of are 0 Recommend vested by Orectren of the Aeminisveicir one in eccordenCe meth condition and limitations cl apoantment tinder 14 CFR on aached sheets membered NM have been examined In accordant* WO astable/led procedure: and found M Camay AiwOrthlresa Starderds La: d. *Won, IR 1"16 data these data I NAM Therettve CI Approve II SIGTUREISI OF DESIGNATED ENGINEERING REPRESENTATIVE($) 12. EM-DONATIDel NUUSERS(S) 13. DASS/FICATIONS1 : • DEPT-7501354W STRUCTURAL Donald las& FAA Form 8110-3 (0Y10)SUPERSEDES PRDROUS ED ION SONY_GM_02755117 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242099 EFTA01327217

SDNY_GM_02755178 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242100 EFTA01327218

13DLG-CON-0325E U.S. DEPARIMNT Of 111ANSPORTATICal FEDERAL VINTON ADWreSTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS 1. DATE March 25.2013 ANCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2 IMRE Beechjet 3. MODEL NO. 400A 4. TYPE (Asps, Aid.. Norco/mt. arc j AIRPLANE 5. NAME Or APPLCAta Constant Aviation Cleveland, Ohio LiSTOF DATA a InENTIFICAININ 7 TRIP Document No. DGD-CA01-SS-O7 REV: IR Dated: 3/6/13 SUBSTANTIATION ANALYSIS --- End of Data NOTES• of the !Manor on en Hasler Beeetteraft 400A Aria --- Is for Beechjet model 400A (Nextant 400XT variant) SIN RK-244 only. is for the structural design aspects only on the above listed data and an installation approval. only for regulations specified In the "Applicable Requirements" dock. with additional regulations not listed herein may be required. This form FAA approval of all engineering design data for the entire Additional 8110.3 approvals may be necessary for Damage Tolerance, Mechanical Systems, Electrical, Weight & Balance, as well as other basis, refer to TC data sheet No. At 6SW 1. This approval 2. This approval does not constitute 3. Approval Is Compliance does not constitute alteration. Flammability, disciplines. 4. For certification B. PURPOSE OF DATA Structural substantiation In support of FM Form 337 for aircraft SIN RK-244. This approval is for design data only on a major alteration and is not an Installation approval. 9. APPLICABLE REOUIRENERTS (List werk aware) 14 CFR Part 25.301( Arndt. 25-23), 303lAmdt. I5-23), ..305(1)(b))Amtll 25-24 -3071Anidt 25.23I. -341]Amdt. 25-0],.561lAmdt. 25-231. .601[Ama. 25-0), 403(aXt)lAradt. 25-331, .6051Aradt. 25-0),.6091Amdt.25-0],.6111Amdt.25.231,.613(e)(bXc)(Aindl.25-0), .625 [Arndt. 25- 23), .7850IXbXsX11XeXplAindt 25-32), .787(allAmdt 2S-32),.789]Aindt. 25-32) 10. CERTIFICATION - Under authority vested by direction of me Administrate.. and In accordance dm conditions end irmations of appointment under (4 CFR Pan In data Isled tow and on attached vines numbered WA nave boon examines n accordance wail eget:race PeoCeOures and loins to trompb, rAt applicable requirements d the AlmultilneSS Standards Listed K Recommend approval of these data I (We) Therefore ts) Approve blew data 4004TURGEs)0F OESIONA 049INEERINDREPRESENTAINE(S) 12. OESIGNAIION nulaeRs(S) C. ORSSWICATII:70) c illi—etg-9 ( 1 tlf --4:0 -- CERT-750135-SW STRUCTURAL nald Gilles,: FAA Form 8110-3 (oma) SUPERSEDES PREVCVS EDITION SDNY_GM_02755179 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242101 EFTA01327219

SDNY_GM_02755180 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I 02 EFTA01327220

13DLG-CON-03258 U.S. DEPARTMENT OF TRANSPCRTMCN FEDERAL AVIATION ADIANISTRAMN STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS 1. DATE March 25, 2013 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MAKE Beechjet 3. MODEL NO. 400A 4. TYPE (Mptine. Raft. IIIM:Opler, efej AIRPLANE & NAME OF APPUCANY Constant Aviation Cleveland, Ohio LIST OF DATA 6 10EIGT1GAllOal 7 TITLE Document No. DGD-CA02-101 REV: B Dated: 1125113 DGO-CA02-501 REV: IR Dated: 6/13/12 DGD-CA13-501 REV: IR Dated: 12/21/12 DGD-CA13-501 EO: A•1 baled: 2/28/12 DGD-CA04-101 REV: IR Dated: 6/13112 RH GALLEY ASSY RH GALLEY INSTL CARD TABLE INSTL CARD TABLE INSTL SIDE LEDGE ASSY -------- End of Data NOTES' ------ is for BseeNet model 400A (Nextant 400XT variant) SRI RIC•264 only. is for the structural design aspects only on the above listed data and an Installation approval. only for regulations specified in the "Applicable Requirements" block. with additional regulations not listed herein may be required. This form FM approval of all engineering design data for the entire Additional 8110-3 approvals may be necessary for Damage Tolerance, Mechanical Systems, Electrical, Weight & Balance, as well es other basis, refer to TC data sheet No. Al flSW Approvals are provided separably. 1. This approval 2. This approval does not constitute 3. Approval Is Compliance does not constitute alteration. Flammability, disciplines. 4. For certification S. Structural & PURPOSE OF DATA To provide type data for FM approval of structure in support of a return to service on SIN RK-244. This approval is for design data only on a major alteration and Is not an Installation approval. 9. APPIXATLE REOUPEMENTS (Ust specie me m) 14 CFR Part 25.601 Arndt 25-0,25.60;(mXb), Arndt 25-38, 25.605 Audi 25-0,25.609 Arndt 25-0.25.611, Arndt 25-23, 25.613 (e)(b)(c) Arndt 25-0, 25.619 Arndt 25-23, 25.625 Arndt 2S-23, 25.785 (e)(bficfidfiefif) Arndt 25.32, 25.719 Arndt 25.32 10 CERTIFICATION • Undo, authonty PM 169. dale aped above and on van eteilmbia recementems of me vested by direction of the Administrator and In accordance Win condi:boos and 4n alerts of appoinienent under t4 CFR Daubed sheets numbered N/A have boon examined In accordance Wm eatables! premiums and found to corn* Ainvoliiness Slandada UMW. approval Of Mese data these eats . Recommend I WO Therrave CO Approve 11. SIGNATUREIS)OF DESIGNATED ENGINEERING REPRESENTATIVE(SI 12 DESIGNATION NUMI5ERSIS) 11 CLASSW1CATICNIS) ," i ) . CA/ fe d/ <24 n.4 0 DERT-750135-SW STRUCTURAL Donald Ggiespie FM Form 6110-3 (OLIO) SUPERSEDES PREVIOUS EDITION SDNY_GM_02755181 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I 03 EFTA01327221

SDNY_GM_02755182 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242104 EFTA01327222

13DLG-CON-0325A U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS 1. DATE March 25, 2013 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2 MAKE Beechjet 3. 1AOCEI. NO 400A 4. TYPE (maw*, Redo, Hatcaot atl AIRPLANE s NAN8 OF APPLICANT Constant Aviation Cleveland, Ohio LIST OF DATA ti tcPtiTICCAT1ON 7 7MP Document No. DOD-CA01.101 REV: D Dated: 3/5/13 DGD-CADI.101 EO: E-1 Dated: 3/6/13 DGD-CA01.501 REV: IR Dated: 6/13/12 OG0-CA01.501 EO: A-1 Dated: 1/29/13 000-CA01.5O1 EO: A-2 Dated: 3/5/13 LH GALLEY ASSY LH GALLEY ASSY LH GALLEY INSTL LH GALLEY INSTL LH GALLEY INSTL ------ Fad of Data Nons • ------ ---- Is for Beecidet model 400A (Nextant 400XT variant) SIN RK-244 only. Is for the structural design aspects only on the above listed data and an Installation approval. only for regulations specified in the "Applicable Requirements" block. with additional regulations not listed herein may be required. This form FAA approval of all engineering design data for the entire Additional 8110-3 approvals may be necessary for Damage Tolerance, Mechanical Systems, Electrical, Weight & Balance, as well as other basis, refer to TC data sheet No. Al 6SW Approvals are provided separately. 1. ThIs approval 2. ThIs approval does not constitute 3. Approval Is Compliance does not constitute alteration. Flammability, disciplines. 4. For certification 5. Structural e. PURPOSE OF DATA To provide type data fo FAA approval of structure in support of a return to service on SIN RK-244. This approval Is for design data only on a major alteration and is not an installation approval. (*.APPLICABLE REOUIREMENTS 11511000* swore) 14 CFR Pare 25.601 Made 25-0,26.6•3(a0(b),Anuft 25-31, 25.605 Arndt 25-0, 25.609 Arndt 25-0, 25.611, Amdt 25.23, 25.613 (s)(b)(e) Arndt 25-0,25.619 Ankle 25-23, 25.625 Arndt 25-23, 25.715 (aNbNeNdNeN0 Amdt 35-32, 25.789 Arndt 25-32 SO. CERTIFICATION Pan 183, data ISIS with applicable recpslrornents I tWe)Therefors - Under aulradly above and of the 0 Recommend wedded by direction on attached shags numbered AlnAorIttness Standards approver of these more data al the AdrrinIstretor WA have end b eccortlance wilh conditions and Invtainorn of appointment under 14 CFR been wurrined in accordance with established procedures and toted to comply Usted. dam e Approve II AlitlE(S)OF OCSIONA °ENGINEERING REPRESENTATIVE/S1 N 12 OESIONANCel lalluRERS(S) 13 CA.ASSIFCATICH(S) r., 1 5.47, i 1 DERT-750135-SW STRUCTURAL nald Gil pla FAA Form 81104 (03 re) SUPERSEDES PREVIOUS EDITION SDNY_GM_02755183 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242105 EFTA01327223

SDNY_GM 02755184 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I 06 EFTA01327224

Aviation Fabricators, Inc. 805 North Fourth Street. Clinton, Missouri 64735 Report # AF-475FTP August 09, 2010 Rev (A) Functional Test Procedure for STC # ST01572WI Hawker Beechcraft Cabin Configuration Applicable Aircraft Model: Hawker Beechcraft 400, 400A SDNY_GM_02755185 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I 07 EFTA01327225

Aviation Fabricators, Inc. AF-475FTP 805 North Fourth Street 08-09-10 Clinton, Missouri 64735 Rev (A) Page 2 014 Revision Log Date Rev Pages Description Approved by 08.09-10 A 1 -Added model 400A G.R. Lowe W -Changed data list # to AF-475MDL SDNY_GM_02755186 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I 08 EFTA01327226

Aviation Fabricators Inc. 805 North Fourth Street Clinton, MO. 64735 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS For Interior Cabin Configurations Document No.: AF-528 Revision "IR" Revision Date: 11121/11 Applicable to: Hawker Beechcraft model 400A Modified by FAA STC ST01572INI The Information in the Instructions for Continued Airworthiness is FM accepted material and complies with 14 CFR 25.1529, instructions for Continued Airworthiness. It supersedes or adds to that provided in the Maintenance Manual for the Hawker Seechcraf I 400A Aircraft, only where covered in the items contained herein. For limitations and procedures not contained in the Supplement, consult the Component Maintenance Manual, or other approved airplane data. Page 1 of 15 SDNY_GM_02755187 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242109 EFTA01327227

ammo (660) 8858317 (660) 885-3743 Fax www.avfab.corn e-mail: saleseavlab.com Nov 7, 2012 'gy-?,9H 5-A fi. OO3 70a CERTIFICATE OF 0NF0RMANCE l A AVIATION FABRICATORS This certifies that vlation Fabricators, Divan, 3 Place with stowage provisions, Beechjet, part number, 32-0396(A60P)T1i3.K-02, serial number, 003702, was manufactured in, or determined to be in conformity to an with approved design data and is iu a condition for safe operation for Installation on aircraft. Jeffrey Lowe Vice-President Aviation Fabricators • Central Airmotive SDNY_GM_02755188 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I 10 EFTA01327228

1 REVISION PAGE Document Title: Instructions for Continued Airworthiness Prepared By: Todd Pogue Reviewed By: Jeffrey R. Lowe Updates to the ICA will be made by Aviation Fabricators Inc. Updates will be listed in the log of revisions and the effective pages will be listed below. Log of Revisions REV. NO. EFFECTED PAGE(S) DESCRIPTION DATE APPROVED BY IR All Initial Release 11/21/11 JRL Per the requirement of Appendix H of 14 CFR Part 25 paragraph H25.1 (c), the changes made to the ICA by the applicant will be distributed via mail by means of paper copy Page 2 of 15 SDNY_GM_02755189 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I I I EFTA01327229

Aviation Fabricators Inc. ICA Document No.: AF-528 805 North Fourth Street Revision (IR) Clinton, MO. 64735 Dale: November 21, 2011 TABLE OF CONTENTS DESCRIPTION PAGE REVISION PAGE 2 TABLE OF CONTENTS 3 ABBREVIATIONS AND DEFINITIONS 4 1.0 INTRODUCTION 5 2.0 INSPECTION REQUIREMENTS AND OVERHAUL SCHEDULE 9 3.0 DIMENSION AND ACCESS' 11 4.0 LIFTING AND SHORING 11 5.0 LEVELING AND WEIGHING 11 6.0 TOWING AND TAXIING 11 7.0 PARKING AND MOORING 11 8.0 PLACARDS AND MARKINGS 12 9.0 SERVICE INFORMATION 13 10.0 AIRWORTHINESS LIMITATIONS 15 11.0 TROUBLESHOOTING INFORMATION 15 Page 3 of 15 SDNY_GM_02755190 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I 12 EFTA01327230

I REVISION PAGE Document Title: Instructions for Continued Airworthiness Prepared By: Todd Ponue Reviewed By: Jeffrey R. Lowe Updates to the ICA will be made by Aviation Fabricators Inc. Updates will be listed In the log of revisions and the effective pages will be listed below. Log of Revisions REV. NO. EFFECTED PAGE(S) DESCRIPTION DATE APPROVED BY IR All Initial Release 11/21/11 JRL Per the requirement of Appendix H of 14 CFR Part 25 paragraph H25.1 (c). the changes I made to the ICA by the applicant will be distributed via mail by means of paper copy 1 Page 2 of 15 SDNY_GM_02755191 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I 13 EFTA01327231

Aviation Fabricators Inc. ICA Document No.: AF-528 805 North Fourth Street Revision (IR) Clinton, MO. 84735 Date: November 21, 2011 TABLE OF CONTENTS DESCRIPTION PAGE REVISION PAGE 2 TABLE OF CONTENTS 3 ABBREVIATIONS AND DEFINITIONS 4 1.0 INTRODUCTION 5 2.0 INSPECTION REQUIREMENTS AND OVERHAUL SCHEDULE 9 3.0 DIMENSION AND ACCESS• 11 4.0 LIFTING AND SHORING 11 5.0 LEVELING AND WEIGHING 11 6.0 TOWING AND TAXIING 11 7.0 PARKING AND MOORING 11 8.0 PLACARDS AND MARKINGS 12 9.0 SERVICE INFORMATION 13 10.0 AIRWORTHINESS LIMITATIONS 15 11.0 TROUBLESHOOTING INFORMATION 15 Page 3 of 15 SDNY_GM_02755192 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242114 EFTA01327232

Aviation Fabricators Inc. 806 North Fourth Street Clinton, MO. 84735 ABBREVIATIONS AND DEFINITIONS ICA Document No.: AF-528 Revision (PR) Dale: November21, 2011 Abbreviations Definitions AML FAA Approved Model List (AML) Detailed Inspection (DET) An intensive examination of a specific Item, installation or assembly to detect damage, failure or irregularity. Available lighting is normally supplemented with a direct source of good lighting at an intensity deemed appropriate. Inspection aids such as mirrors, magnifying lenses, etc. may be necessary. Surface cleaning and elaborate access procedures may be required. FM Federal Aviation Administration FM MIDO FM Manufacturing Inspection District Office General Visual Inspection (GVI) A visual examination of an interior or exterior area, installation or assembly to detect obvious damage, failure or irregularity. This level of inspection is made from within touching distance unless otherwise specified. A mirror may be necessary to enhance visual access to all exposed surfaces in the Inspection area. This level of inspection is made under normally available lighting conditions such as daylight, hangar lighting, flashlight or droplight and may require removal or opening of access panels or doors. Stands, ladders or platforms may be required to gain proemity to the area being checked. ICA Instructions for Continued Airworthiness Special Detailed Inspection (SDI) An Intensive examination of a specific item, installation , or assembly to detect damage, failure or Irregularity. The examination is likely to make extensive use of specialized Inspection Techniques and/or equipment. Intricate cleaning and substantial access or disassembly procedure may be required. STC Supplemental Type Certificate Page e of 15 SDNY_GIvl_02755193 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242115 EFTA01327233

Aviation Fabricators Inc. 805 North Fourth Street Clinton, MO. 64735 1.0 INTRODUCTION ICA Document No.: AF-528 Revision (IR) Date: November 21, 2011 The purpose of this Maintenance Manual Supplement and Instructions for Continued Airworthiness (ICA) is to provide the maintenance technician with the information necessary to ensure the continued airworthiness of the Aviation Fabricators cabin configuration, per installation number 400-3, when installed in the aircraft passenger cabin in accordance with Aviation Fabricators design data included on Master Data List AF-475MDL and per Supplement Type Certificate (STC) No. ST01572W1 Modifications to an aircraft obligates the operator to include the maintenance Information provided by this document into the operators aircraft Maintenance Manual and operator's aircraft scheduled maintenance program. This document defines supplementary maintenance operations and frequencies recommended by Aviation Fabricators Inc., to ensure the aircraft's airworthiness. The information contained herein addresses the requirements specified in 14 CFR 25.1529, Instructions for Continues Airworthiness and supplements the basic Airplane Maintenance Manual only in those areas listed as pertains to the installation of divan assemblies, as installed per the Aviation Fabricator Master Data List AF-475MDL. For limitations and procedures not contained in this supplement, consult the basic Airplane Maintenance Manual. DATA All information to support the continued airworthiness of this modification is contained in: STC ST01572WI. Master Data List: AF-475MDL. Installation: 3 Place Divan (Ref. Installation number 400-3), Installation Instructions D-10666 for P/N 32-0396K-X Parts: P/N 32-0396K-X, 3 Place Divan Installation The new divan assembly (with restraint system) is a self contained complete assembly that mounts to the existing seat track, using standard fittings, in accordance with FAA approved floor plans. The (restraint system) seat belts are attached to the seat track with typical tie down fittings and the inertia reel shoulder harness is bolted to the divan frame on the outboard side using standard aircraft hardware. Design Change Control All data and changes to the parts and assemblies will be tracked per Master Data List AF- 475MDL Rev C or later FAA approved revision. Applicable Aircraft Beechjet 400A Page 5 of 15 SDNY_GM_02755194 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242I 16 EFTA01327234

Aviation Fabricators Inc. 805 North Fourth Street Clinton, MO. 64735 ABBREVIATIONS AND DEFINITIONS ICA Document No.: AF-628 Revision (IR) Dale: November 21, 2011 Abbreviations Definitions AML FAA Approved Model List (AML) Detailed Inspection (DET) An intensive examination of a specific Item, Installation or assembly to detect damage, faiure or irregularity. Available lighting is normally supplemented with a direct source of good lighting at an Intensity deemed appropriate. Inspection aids such as mirrors, magnifying lenses, etc. may be necessary. Surface cleaning and elaborate access procedures may be required. FAA Federal Aviation Administration FM MIDO FM Manufacturing Inspection District Office General Visual Inspection (GVI) A visual examination of an interior or exterior area, installation or assembly to detect obvious damage, failure or irregularity. This level of inspection Is made from within touching distance unless otherwise specified. A mirror may be necessary to enhance visual access to all exposed surfaces in the Inspection area This level of inspection Is made under normally available lighting conditions such as daylight, hangar lighting, flashlight or droplight and may require removal or opening of access panels or doors. Stands, ladders or platforms may be required to gain proximity to the area being checked. ICA Instructions for Continued Airworthiness Special Detailed Inspection (SDI) An Intensive examination of a specific item, Installation , or assembly to detect damage, failure or irregularity. The examination is likely to make extensive use of specialized Inspection Techniques and/or equipment. Intricate cleaning and substantial access or disassembly procedure may be required. STC Supplemental Type Certificate Page 4 of 16 SDNY_GM_02755195 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242117 EFTA01327235

Aviation Fabricators Inc. 805 North Fourth Street Clinton, MO. 64736 ICA Document No.: AF-528 Revision (IR) Date: November 21, 2011 1.0 INTRODUCTION The purpose of this Maintenance Manual Supplement and instructions for Continued Airworthiness (ICA) is to provide the maintenance technician with the information necessary to ensure the continued airworthiness of the Aviation Fabricators cabin configuration, per installation number 400-3, when installed in the aircraft passenger cabin in accordance with Aviation Fabricators design data included on Master Data List AF-475MDL and per Supplement Type Certificate (STC) No. ST01572WI. Modifications to an aircraft obligates the operator to include the maintenance Information provided by this document into the operators aircraft Maintenance Manual and operator's aircraft scheduled maintenance program. This document defines supplementary maintenance operations and frequencies recommended by Aviation Fabricators Inc., to ensure the aircraft's airworthiness. The Information contained herein addresses the requirements specified in 14 CFR 25.1529, Instructions for Continues Airworthiness and supplements the basic Airplane Maintenance Manual only in those areas listed as pertains to the installation of divan assemblies, as installed per the Aviation Fabricator Master Data List AF-475MDL. For limitations and procedures not contained in this supplement, consult the basic Airplane Maintenance Manual. DATA All information to support the continued airworthiness of this modification is contained in: STC ST01572W1 Master Data List: AF-475MDL. Installation: 3 Place Divan (Ref. installation number 400-3), Installation Instructions D-10668 for P/N 32-0396K-X Parts: P/N 32-0396K-X, 3 Place Divan Installation The new divan assembly (with restraint system) is a self contained complete assembly that mounts to the existing seat track, using standard fittings, in accordance with FAA approved floor plans. The (restraint system) seat belts are attached to the seat track with typical tie down fittings and the inertia reel shoulder harness Is bolted to the divan frame on the outboard side using standard aircraft hardware. Design Change Control All data and changes to the parts and assemblies will be tracked per Master Data List AF- 475M0L Rev C or later FAA approved revision. Applicable Aircraft Beechjet 400A Rage 6 of 16 SDNY_GM_02755196 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I IS EFTA01327236

Aviation Fabricators Inc. 806 North Fourth Street Clinton, MO. 84735 3 Place Divan P/N 32-0396K-X (Top not shown for clarity) FOOT ATTCHMENT TO OWN F OOTA1TA?:/lE210 TRACK Figure 1.0A ICA Document No.: AF-528 Revision (IR) Date: November 21, 2011 "ttsurno FOOT ATIACMIT TO /TOMO' GIP Page 8 of 16 SDNY_GM_02755197 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA (X1242119 EFTA01327237

Aviation Fabricators Inc. 805 North Fourth Street Clinton, MO. 64736 Inertia Reel Attachment DIVAN FRAME WASHER INERTIA REEL Figure 1.0B Seat Belt Attachment Figure 1.0C ICA Document No.: AF-528 Revision (IR) Date: November 21. 2011 BOLT Page 7 of 15 SDNY_GM_02755198 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I 20 EFTA01327238

Aviation Fabricators Inc. 806 North Fourth Street Clinton, MO. 64736 3 Place Divan P/N 32-0396K-X (Top not shown for clarity) coat TOWN/01 K•011.60.0 resoisenaision tale. tiaricr4.-.. roar ATT,CHMIBIT TOT RACK Figure 1.0A ICA Document No.: AF-528 Revision (IR) Date: November 21, 2011 "far' FOOT ATTACIVSIT TO TRACKWTH COP reel— Page 6 of 16 SDNY_GM_02755199 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242121 EFTA01327239

Aviation Fabricators Inc. 805 North Fourth Street Clinton, MO. 64736 Inertia Reel Attachment Figure 1.08 Seat Belt Attachment Figure 1.0C ICA Document No.: AF•528 Revision (IR) Dale: November 21, 2011 Page 7 of 15 SDNY_GM_02755200 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242I 22 EFTA01327240

Aviation Fabricators Inc. 805 North Fourth Street Clinton, MO. 64736 SEAT BLACK ASSEMBLY SEAT BOTTOM ASSEMBLY oM CUSHION AAKFMAI V OrBOOBBY0 AMMON Figure 1.0D gam ICA Document No.: AF•526 Revision (IR) Date: November 21, 2011 Vrtat0110C. Lou:Rower VELCROHOOK Page 8 of 16 SDNY_GM_02755201 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242123 EFTA01327241

Aviation Fabricators Inc. 805 North Fourth Street Clinton, MO. 64735 ICA Document No.: AF-528 Revision (IR) Date: November 21, 2011 2.0 INSPECTION REQUIREMENTS AND OVERHAUL SCHEDULE 1. To comply with14 CFR 25.1529, continue the new divan assembly (with restraint system) on the same inspection and maintenance schedule used per the Hawker Beechcraft Maintenance Manual for cabin section inspections. a. The new cabin configuration components require no service other than inspection at normal inspection interval of 200 hours. b. The safety belts require no service other than inspection at normal inspection interval of every 200 hours. c. Perform a detailed visual inspection of each passenger seat bottom and back cushions and covering of all cabin interior components to detect apparent or obvious defects or irregularities. On the cushion assembly, check for cracks and punctures within a 4" diameter circle. The cushion assembly can have no more than three defects found within the 4" diameter circle. If a cushion develops a lump", check to see if there are no more than two lumps within a 4" diameter circle. Any damage to the cushions outside of the described limits will require them to be replaced. Visually inspect the covering assemblies for holes, punctures, and tears. If the damage to the covering is holes smaller than''/? in diameter or a cut at a maximum of 2" in length then the covering is satisfactory. The sewing of the cover assemblies is not to exceed 1" tearing. Any damage to the covering assemblies outside of the described limits will require them to be replaced. d. Visually inspect the divan and seat assembly tubes and diaphragm for cracks and deformation. Damaged conditions could be detected as a crack at the edge of the tube or along the length of the tubes or as a crack, tear or cut found on the seat bottom or back diaphragm. Visually inspect all hardware for excessive wear before and after installation. Replace the seat back and bottom diaphragm if two cracks or deformations are found with a 4" diameter circle. If a tear or cut is found with a maximum of 6", replace the diaphragm. There shall be no broken tubes. There shall be no sharp corners, edges, or protrusions that may Injure passengers. Replace the tubes if they are bent in such a way that they are more than 2" off center. Replace the seat tubes if crack length is found to be .125" or greater. Replace the tube if a dent is found running longer than 3". Replace the seat tubes if deformation is greater than .25" the overall thickness of the tube diameter. Cracked or broken fasteners or fittings are to be replaced with new immediately. Page 9 of 16 SDNY_GM_02755202 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242124 EFTA01327242