au i 9. 8 t )1 9 C A. MAMJFACTURER NAME *OGRESS PRODUCTION SASS (C.hecR makes (MN PRODUCTION CERTS1CATE (Caro induCann can/tka nprnaO TYPE CERTIFICATE OTHER C. GM QUANTITY OF CERTIFICATES REQUIRED FOR OFERATIM3 NEEDS DATE OF APPLICATION NAME ANC% TILE (AM or WM SIGNATURE H k VIA • 2 1 O I 2 i E. Z I g g A DESCRIPTION OF AIRCRAFT REGISTERED OANER ADDRESS EIULCIER NON MODEL SERIAL NUMBER REGSTRATION MARK E. DESCRIPTION OF FLIGHT CuS7CatFR DEMONSTRATION FLIGHTS C) act I I ar~e) FROM 70 DEPARTURE DATE DURATION C. CREW REQUIRED TO OPERATE THE AIRCRAFT AHD ITS EOUPMENT I I PILOT I I COPILOT I ll FUGHT ENGINEER I I O71-IER(Sact/H D. THE AIRCRAFT DOES NOT MEET THE APPUCABLE NRWORTHNESS REQUIREMENTS AS FOLLOWS: THE FOLLOWING RESTRICTK)NS ARE CONSIDERED NECESSARY FOR SAFE OPERATION-. (Use onacnrneni a necessary) F. CERTIFICATION • i hereby unly ow $ an roe nagmenal wince Mr his gat 44 the ~all ~abed Moat OW 1119 Wain li tasleffee mil Me Federal Ayaldin ~eleance, In acmrclance rain Tale 49 of me Unted Swiss Code 44101 mag erd applKetae Federal Anegan Resat" and mat roe awal has can ins:main arc s saM by Me MN detwited. DATE tom4E AM) TITLE (Peal a lyta) SIGNATURE VII. AIRWORTHINESS 0CCUMENTATION I FAAltaGNEE us* or*) ir A OPelead Written. nO Mallngs In Cotriplancie Ma 14 CPR anion 919. AeNtolatile G. Seamen ol Conaway. FAA Form 81309 (Mach .tenrequWo It Foreign Anvorthiness Centation Tor Irian Mend (Meta when recl~) a ^Mane Maclied C. DMA Ortharga ~cgs" em. One& when ~era i I. PnaMme ~eau Cartkam issued a Abadan. WM le cat agago 21.191 (a) cm conrai attach:di l D. Carat ~IF« aid Enna Wormann Mama in Mcrae E Marx RONK imil Mermen FM Form337 (Meal when ragweed) 1 J. Cunard Pirercaemes Graeae leased in Aacrilence WM la caR sock", 21.191 (a) tconschm / F. Trn inseam« Recorder, n Aircraft Records K. ØØ Alma awns% ol Ccerørecte. FAA Form 60015 (Mach when MON« FM Form 91304 VIII 1 ) All Previous Eagle SuNKII40400 Electronic Format -PDF Poii• 2 2 EFTA00011969

EFTA00011970

UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION . FEDERAL AVIATION ADMINISTRATION SPECIAL AIRWORTHINESS CERTIFICATE A CATEGORYIDESIGNATION EVERIEITA. PURPOSE RESEW & COMMENT ,,,:A‘ B . MANU- FACTURER NAME /f/VA.J;-,(-1--1;11\ ADDRESS 8d,Nti(Al \'4, ‘ c FLIGHT FROM II/AVM* AI`A TO Iii '11,0 I r,) \ E' ',.!,! n u N. 4.91I X ' III '')-,; v,-- - --n--) ., L NO. SERIAL R-241 BUILDER Raytheon Ater4facip* IA MODEL OA E DATE OF ISSUANCE tiorO\ \ Ili /0 ;E:X,FAY Jan 12. 2014 OPERATING LIMITKONNIPIi1820134t PART OF THIS CERTIFICATE ' ' li ' DESIGNATION OR OFFICE NO. DART833943GL Any alteration, reproduction or misuse of this certificate may be punishable by a fine not exceeding $1,000 or imprisonment not exceeding 3 years, or both. THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE TITLE 14, CODE OF FEDERAL REGULATIONS (CFR). FAA FORM 5130.7 (MN} SEE REVERSE SIDE NSN. 0052.004914000 EFTA00011971

A A This airworthiness certificate is issued under the authority of Public Law 104.6, 49 United Stales Code (USC) 44704 and Title 14 Code of Federal Regulations (CFR). 0 w The airworthiness certificate authorizes the manufacturer named on the reverse side 0 conduct production flight !et, and only production flight tests, of aircraft registered in his name. No person may conduct production flight tests under this certificate: (1) Caging persons or property for compensation or hire: and/or 0 Carrying persons not essential to the purpose of the flight r v This airworthiness certificate authorizes the flight specified.on the reverse side for the purpose shown in Block A, D This airworthiness certificate certifies that as of the date of issuance, the aircraft to which issued has been inspected and found to meet the requirements °title applicable CFR. The aircraft does not meet the requirements of the applicable comprehensive and detailed airworthiness code as provided by Annex 6 to the Convention On International CivilAvialion. No person may operate the aircraft described on the reverse side: (1) except in accordance with the applicable CFR and in accordance with conditions and limitations which may be prescribed by the Administrator as part of this certificate; (2) over any foreign country without the special permission of that country. E Unless sooner surrendered, suspended, or revoked, this airworthiness certificate is effective for the duration and under the conditions prescribed in 14 CFR, Part 21, Section 21,161 or 21.217. EFTA00011972

' UNITED STATES OF AMERICA ' DEPARTMENT OF TRANSPORTATION . FEDERAL AVIATION ADMINISTRATION SPECIAL AIRWORTHINESS CERTIFICATE A CATEGORY/DESIGNATION ' EXPERIMENTAL PURPOSE Research and Development B MANU• FACTURER NAME NIA • ADDRESS NIA p C FLIGHT FROM ON:A \ TO 0\ D N• 493LX 4\\ SERIAL NO, RK2 44 BUILDER Raytheon Aircraft Company MODEL 400A DATE OF ISSUANC MAY12012013 EXPIRY Nom Ri2013 OPERATING U ATIONS DATE 1 1. ARE PART OF THIS CERT E DESIGNATIO OR OFFICE NO, DARF-400148•CE Any alteration, reproduction o misuse of this certi ie may be punishable by a fine not exceeding $1,000 or imprisonment not exceeding 3 years, or both, THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE TITLE 14, CODE OF FEDERAL REGULATIONS (CFR), FAA Form 813P 04120111 Nous Edition 01104 May be Used until Depleted SEE REVERSE SIDE NSN: 00524493400 EFTA00011973

c A n This airworthiness certificate is issued under the authority of Public Law 104.6, 49 United Slates Code (USC) 44704 and Title 14 Code of Federal Regulations (CFR). B The airworthiness certificate authorizes the manufacturer named on the reverse side to conduct production fight tests, and only production flight tests, of aircraft registered in his name, No person may conduct production flight tests under this certificate (1) Carrying persons or property for compensation or hire: andlor (2) Carrying persons not essential to the purpose of the flight. ft v This airworthiness certificate authorizes the flight specified on the reverse side for the purpose shown in Block A. D This airworthiness certificate codifies that as of the date of issuance, the aircraft to which issued has been inspected and found to meet the requirements of the applicable CFR. The aircraft does not meet the requirements of the applicable comprehensive and detailed airworthiness code as provided by Annex 8 to the Convention On International Civil Aviation, No person may operate the aircraft described on the reverse side (1) except in accordance with the applicable CFR and in accordance with conditions and limitations which may be prescribed by the FM as part of this certificate; (2) over any foreign country without the special permission of that country. E Unless sooner surrendered, suspended, or revoked, this airworthiness certificate is effective for the duration and under the condnions prescribed in 14 CFR, Pad 21, Section 21.181 or 21.211. EFTA00011974

U.S.Oepartment of Transportation Federal Aviation Administration REG. NO. N4931X EXPERIMENTAL OPERATING LIMITATIONS For Research and Development (R&D) MAKE: Raytheon Aircraft Co MODEL 400A WM 0404140MO Ohio 44070 SERIAL NO: RK - 244 THESE OPERATING LIMITATIONS SHALL BE ACCESSIBLE TO THE PILOT 1. No person may operate this aircraft unless the FAA Form 8130-7, Special Airworthiness Certificate. is displayed at the cabin or cockpit entrance and visible to passengers or flight crew members. 2. No person may operate this aircraft for other than the purpose of Research and Development to accomplish the flight operation outlined in the applicant's program letter Dated November 13.2013, which describes compliance withl4 CFR 21.193 (d) and made available to the pilot in command of the aircraft In addition, this aircraft shall be operated in accordance with applicable.air traffic and general operating rules of 14 CFR part 91,and all additional limitalionsherein prescribed under the provisions of 14 CFR 91.319 (i). 3. R&D flights must be conducted IAW Nextant Aerospace's Program Letter Dated November 13. 2013, within the geographical area described In the program letter. R&D Rights will be conducted In North America 4. Except for takeoffs and landings, this arcraft must not be operated over densely populated areas or in congested airways. 5. This aircraft must not be operated unless it is maintained and Inspected in accordance with the appropriate military technicalpublIcations and/a manufacturer's recommendation. The owner/operator must select, establish, identify, and use an inspection program set forth in 14 CFR 91.409 (e), (f),(g), and (h). This inspection program must be recorded in the aircraft maintenance records. 6. The Pilot In Command of this aircraft must hold an appropriate category/Gass rating. If required for the type of aircraft to be flown, the Pilot In Command also must hold either an appropriate type rating or a Letter of Authorization issued by an FM Flight Standards Operations Inspector. 7. This aircraft may be operated under VFR, day and/or night. 8. The Aircraft may be operated under IFR, and must be properly equipped for instrument flight in accordance with 14 CFR 91.205. 9. No person may operate this aircraft for carrying persons or property for compensation or hire. 10. No person may be carried in this aircraft during flight unless that person is essential to the purpose of the flight. 11. The Pilot In Command of this aircraft must advise each passenger of the experimentalnature of this arcraft, • And explain that It does not meet the certification requirements of a standard certified aircraft. 12. This Aircraft must contain the Beech Model 400A Flight Manual with Nextant 400XT AFM Section Insert, Placards, markings, etc. (or other operating instructions developed for an STC modification), as required by14 CFR 91.9. 13. This Aircraft is Prohibited from Aerobatic Flight , that is an Intentional Maneuver involving an Abrupt change in the Aircrafts attitude, an abnormal attitude, or abnormal acceleration not necessary for normal flight, unless part of show compliance flight testing 14. This aircraft shall not be used for glider towing, banner towing, or intentionalparachute jumping. Page 102 EFTA00011975

EFTA00011976

of Transportation Federal Aviation Administration 15. No person shall operate this aircraft unless within the preceding 12 Calendar months it has had a condition inspection performed in accordance with 14 CFR Part 43, appendix D,or other FAA approved programs, and was found to be in a condition for safe Operation. This inspection will be recorded in the aircraft maintenance records. 18. FAA•certificated Repair Stations and FM - Certified mechanics with appropriate ratings, as authorized by 14 CFR 43.3 may perform inspections required by these limitations. 17. Inspections shall be recorded in the aircraft maintenance records showing the following or a similarly worded statement: "I certify that this aircraft has been inspected on (insert date) in accordance with the scope and detail of 14 CFR part 43, appendix D,or other FAA approved programs and found to be In a condition for safe operation." The entry will Include the aircraft's totaltime-in-service, and the name, signature, certificate number, and type of certificate held by the person performing the inspection. 18. If the aircraft, engine, or propeller operating limitations are exceeded, an appropriate entry will be made In the aircraft records. 19. This aircraft must not be operated unless it is maintained and inspected in accordance with the requirements of 14 CFR Part 43. 20. This aircraft must display the word `EXPERIMENTAL" In accordance with 14 CFR 45.23(b). 21. The Pilot In Command of this aircraft must notify air traffic control of the experimental nature of this aircraft when operating into or out of airports with operating control bra The Pilot In Command must plan routing that will avoid densely populated areas and congested airways when operating VER. 22. This aircraft does not meet the requirements of the applicable, comprehensive, and detailed AInvorthIness code as provided by Annex 8 of the International Convention of Civil Aviation. The Owner/Operator of this aircraft must obtain written permission from another country's Civil Airworthiness Authority (CAA) prior to operating this aircraft in or over that country. That written permission must be carried aboard the aircraft together with the U.S. airworthiness certificate and, upon request, be made available to an FAA inspector or the CAA in the country of operation. 23. Aicraft instruments and equipment installed and used under 14 CFR 91205 must be inspected and maintained in accordance with the requirements of 14 CFR parts 43 and 91. Any maintenance or inspection of this equipment must be recorded in the Aircraft Maintenance records. 24. Application must be made to the geographically responsible FSDO or MO for any revision to these operating limitations. 25. 14 CFR 47.45 requires that the FM Aircraft Registry must be notified within 30 days of any change it the aircraft registrant's address. Such notification Is to be made by submitting Aeronautical Center Form 8050-1, Aircraft Registration Application, to AFS•750 in Oklahoma City, OK. 26. Condition Inspections must be performed in Accordance with 14 CFR Part 43 Appendix D at least every 100 Hrs Flight Hours. This Inspection must be performed by an FM Certified Mechanic with the Appropriate Ratings as deemed in 14 CFR. 43.3 27. The Special Airworthiness Certificate and Operation Limitations will eerie on. Jan 12.2014 Designated Airworthiness Representative DART833943GL Issued at Cuyahoga Airport Date Issued: November18 2013 Page 2 c42 EFTA00011977

EFTA00011978

nextant aerospace Quality Assurance Department To: Federal Aviation Administration Flight Standards District Office North Olmsted, Ohio 44070 From: Date: November 13, 2013 Chief Inspector Nextant Aerospace Subject: FAA Program letter for Beech let 400A, Serial number RK-244, Registration Number N493LX. Ref: FAA order 8130.2G 1. Registered Owner: Flight Options LLC. Address: 2. Aircraft Description: Twin Engine Light let a. Registration: N493LX b. Aircraft Builder Raytheon Aircraft Co c. Year mfg.: 1999 d. Aircraft Serial Number: RK-244 e. Aircraft Model Designation: Beech Jet 400A Richmond Heights, Ohio 44143 3. The program purpose for the aircraft will be used To complete the flight performance profile in Research & Development Category in support of FAA Project SA 152501A-7 (Replacement of Wingtips) 4. Program Duration a. List the estimated flight hours required for program: 20 Hrs b. Number of flights: 20 c. Number of days: 60 S. Describe the areas over which the flights to be conducted and address of base operation: The base of operation is Cuyahoga County Airport, 355 Richmond, Cleveland, Ohio. Flights will be conducted in North America. 6. Describe the aircraft configuration: This Aircraft is a standard Beech let 400A with new Williams F144-3AP engines and upgraded avionics with full authority digital engine controls (FADEC) a. Maintenance Program 1. Hawker Beechcraft Maintenance Manual Chapter 5 Rev C22 or later with the exception of the .1115D Engines. 2. Williams International recommended FJ44 3A Maintenance manual (FADEC maintenance is covered in 71.00.00 of this manual) 3. Maintenance Requirements for the Throttle Quadrant is addressed in the Instructions for Continued Airworthiness on the FJ44-3AP STC. Nextant Aerospace 202 A Tel Work Cell '4'Spt& EFTA00011979

EFTA00011980

Cleveland. Ohio 44143 November 13, 2013 Nextant Aerospace, LLC Cleveland, Ohio 44143 Attention: Re: RK-244 — Agent Authorization To whom it may concern: aLitOptions This letter is to confirm that Flight Options, LLC (TO") authorizes Nextant Aerospace, LLC, as FO's agent, for a Beechjet 400A, bearing serial number RK-244 and FAA Registration Number N493LX (also identified as a "Nextant 400XT'), which is owned by FO, for any and all authorized FAA actions in regards to: X Airworthiness Classification Experimental Airworthiness Classification Standard Sincerely, Flight Options, LLC By: Vice President, Administration & Contracts EFTA00011981

:I•1A1 1: • EFTA00011982

FAA FORM 1030-6, APPLICATION FOR U.S. AIRWORTHINESS CERTIFICATE Fpm Approved O.M.O. No. 2120-0018 Expiration Date 02/28/2013 a APPLICATION FOR U.S. Cepartmem U.S. AIRWORTHINESS a Transponaton Federal Aviation CERTIFICATE Adirealsrratioe INSTRUCTIONS • Prim or Iwo Do nol rote in shaded arms; Mese are for FAA molly. Sutom cripnal otmr a en eufacrized FM Repfeientatne. If edclOomil Space is motive& use ailachnent. For special IIHM permits complete Sections H. A. and Alas applicable e t 0 * r • gi I REGISTRATION MARK N493LX 2. AIRCRAFT MOLDERS NAME mum Raytheon Aircraft Co 3. AIRCRAFT MOOELDESGNATION 400A 4. YR MFR. 1999 FM COOING 5 AIRCRAFT SERIAL NO. RK244 S ENGINE BUILDER'S NAME Ago.) Williams International 7. ENGINE MODEL OESIGNATION FJ44.3AP 8. NUMBER OF ENGINES 2 9 PROPELLER BUILDERS NAME MAN N/A ID PROPELLER MOO EL DESIGNATION II. AIRCRAFT IS farm moomsam N/A IMPORT gi burr g g et u a APPUCATION IS HEREBY MACE FOR. Momoorrim on) I A l STANDARD NROORTIMIESS CERTIFICATE roses *wpm Hama Honor, I I I I roarrem I [morn. Hamm. I lona 8 re SPECIAL MFMORTICESS CERTINCATE Moo refierme Arm/ 7 PRIAMM 9 UGHT-SPCRT limas Caw I IN/Hanel I loompParadue I I WeIgHtellarotrc4 I 1 Cider I I Utter Mari M 2 UNITED 1 LASS C 2 5 PROVISIONAL Room oleo CLASS II 1 AGRICULTURE AND PEST CONTROL 2 AEFOAL SURVEY 3 AERIM.A0VERMING 3 RESTRICTED Mcrae to 44 <40:1•000) 4 FOREST 0$0.4 ten."4"; 5 PATROLLING 6 HEATHER CONTROL 0 OTHER (40/4240 I I RESEARCH AND CEVELCPMENT 2 AMATEUR BUILT 3 EXHH/TION 4 AIR RACING S CREW BINNING 6 MARKET SURVEY 0 TO SHOW COMPLIANCE VAN THE CFR 7 OPERATING Morro Crown KIT MKT AIRCRAFT I OA EMOTE aMmill*Mota an armorinns cortfale II 00 nol noel 6103.1 4 EXPERIMENTµ nmcompramoN rem romum e OPERATIC 58 OPROUBUDIGpoil Kt-tun UGHT4PC111 ec OPTION 1911-sped HICAPIT *PAP WOO 5911-spat allegory almannona cerMeate untie 621.190 9 UMMNMED 9A RESEARCH AND DEVELOPMENT ICI I CREW TRAINING AIRCRAFT 96 MARKET SURVEY I FERRY FLIGHT FOR REP...MS.ALTERATION& MAINTENANCE CR STORAGE SPEOAL FLIGHT PERMIT mops 2 EVACUATE FROM AREA OF IMPENDING DANGER 8 wersoo re re mower oaf ammo mom me. oval motes* inform HIN 3 OPERATION IN EXCESS OF MAXJMUM CERTIFICATED TAKEOFF WEIGHT 4 DEUVERING OR EXPORTING I 5 I I PROCUCTIONCL4HT TESTING 6 CUSTOMER CEMONSTRATIONFUGHTS CI 6 MULTIPLE AIRWORTHINESS CERTIFICATE KAM MOM Moron Oiwatim on lanOwe a bile•raniffitaal i § is i A REGISTEREDCOTNER Hs was , mita a rose nommor IF DEALER. CHECK HERE o I NM* F ight Options.LLC Flight Options LLC , Richmond Heights .OH 44143 B AIRCRAFT CERTIFICATION 8ABG rtmempoommuar mamma Sr, n **gat AIRCRAFT SPECIFICATION CR TYPE CERTIFICATE DATA SHEET rom rie ma A•VOiLl ion N/A 1 ACVORTMNESS ORECTIVES (Owl delloWeormOs ii• erreraloomeerwmormeree AD Si,. -Van. 'VW miss If or mmymno ordinee as itooleeerf W O o Bi-Weeky 2013-09, 04/22/2013 - 05/05/2013 NRCRAFT LISTING (G.........e.nw N/A SUPPLEMENTAL TYPE CERTIFICATE ON east el nen Sit N/A C. NRCRAFT OPERATION MID MAINTENANCE RECORDS CAECK IF RECORDS IN COMPLIANCE WIN 14 CFR maion 91.417 TOTAL AIRFRAME CURS 8563.80 3 EXPERIAMMTAL ONLY oa gmmeem sa f me resima im moray Pommel D. accordant* MoKorinests DATE A CERTIRCATION - Mersey wiry Minim Me regtsond maw (of Pis mere) of fl ame deemed atom out me a cart is roomers wfl um Femme miafion Auffirientlen In am Title 49 of to vow Stain Coo:lan), rt)aa and swears Feciend Amato Regutataro and mat lie wenn has Wen is eimilby WV* aP* cenlftele OF APPLICATION 05/13/2013 THE AIRCRAFT OESCREIEDMIOVE § § u i 5 qe a 2 Iii CFR =121 CERTIFICATE HOLDEROm I a l 'CERTIFICATED MECRANICIG•• Gesture no, I 0 I I CERTIFICATED REPAIR STATION min comm. 5 AIRCRAFT MANUFACTURER (ava nava weary DATE I WILE I SIGNATURE ; (I A I A," 5 OFFICE fl u rt ttatax Awns taco HMO A Mee) 14 THE CERTIFICATE REQUESTED A. I lino Mal ins Wine dilated In Salon Ice VII meets refoiterrors to MIENINENT OR MODIFICATION OF CURRENT NRW3RTHWESS CERTIFICATE B. IrdPr-Sen Tor a Medial WY pWT1 Lwow Sprain VII was conducted by. FM INSPECTOR FM DESIGNEE DATE /1400/40 MICOSSOO ct-91T 4 FAA Fern 81304 (4/11) Al Preview Etna Superseded Msdronic Tama -POF Page 1 o12 EFTA00011983

r EFTA00011984

VI. PRODUCTION FLIGHT TESTING A. MANUFACTURER NAME ADDRESS Et PRODUCTION BASIS (CAM M0MS* amp PRODUCTION CERTIFICATE 1Gw Skis cetelicettinai) .. TYPE CERTIFICATE OTHER C. GIVE OLLANNTY OF CERTIFICATES REWIRED FOR OPERATING NEEDS DATE OF APPLICATOR I NAME ANO TITLE (PAM MK*) SIGNATURE VLL SPECIAL. ruGHT PERMIT PURPOSES OTHER THAN PRODUCTION WONT TEST A DESCRIPTION OF MRCRAFT REGISTERED OWNER ADDRESS BUIDER (444/g) MODEL SERIAL NUMBER REGISTRATION MARK B. DESCRIPTION OF RIGHT CUSTOMER DEMONSTRATION FLIGHTS CI COMM arpiest, FROM TO VIA OEPARTURE DATE DURATION G CREW REWIRED TO OPERATE THE MRCRAFT AND ITS EOUIPMENT I I PILOT I i COPILOT I I FLIGHT ENGINEER I I oTHERmixtoM O. THE AIRCRAFT DOES NOT MEET THE APPLICABLE ARWORTHWESS REOUREMENTS AS FOLLOWS: E TIE FOU.OWNO RESTRICTIONS ARE CONSIDERED NECESSARY FOR SAFE OPERATOR Ma artaconenr.r moues) F. CERTIFICATION • 1 nints own& ita I inn ronmerse comer (or PM onov) ol to ICS emoted sten TM et glen A Is recitietedweh re Feces& Aeatt:c AOrtmusilon In KC0nlarball MI. TIN 49 d Me UMW gabs Cods 44101 AM Old Opplane F.dfl ANSI Regal** anent Os eaten ras omen (Assam AN o d. b. so fir easerisol DATE NAME AND TITLE (HMI Or Wee SIGNATURE a 3 4.4 ..4 g 3_ E tf ll At i z V "°°"" cam Unallons end Morkims In Complisnes W0114 CFR Seclion 919. m Apro . EL Stammers of CoMonons, FAA Fpm 8,30.9 (Attach twee i 'Quince )t Forolr Akoortinom Owilkslon fix loom Nana man Atm' rogue') Y El Curia Camel° Lieritef ens Aliened c oga. Dr. &Arcs. 12744O3rXim. etc lath rinuiroal X I Ewa* Mvoltenrs 14 CFR SICEcti hi. 3 a) semen Ai Accordsnas Win CAR (EloGolM (mown 1 D. Omen: weiM re4 BOOM Ink/motion Awilatle in Aktran E. Majot Eepal and Minton. FAA Form 337 (ARM Men IMMO ..%). Iv J Carp' ANAIEhnenCe. MSIved in AtEcedanCe Wm Id CFR Swim 2 S .I. Fit (of 1 (Cary Onto* ic F. Ms iromraon Ftscanol In Moan Recant N. UV-Sport Alrcret SUOMMI ciCarolarcoo. FM Form 813013 Mach Men nequeed) FAA Form 61304 (4111) MI Pnwians Edlli0ni gnomons(' Eiscimoic Formal -POF Page 2 of 2 EFTA00011985

EFTA00011986

UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION • FEDERAL AVIATION ADMINISTRATION SPECIAL AIRWORTHINESS CERTIFICATE A CATEGORY/DESIGNATION EXPERIMENTAL PURPOSE Research and Development a MK. FACTURER NAME NIA ADDRESS NIA st C FLIGHT FROM et TO , , D N. 4931,X SERIAL NO. RK244 BUILDER Raytheon Company MODEL OA E Any imprisonment IN ACCORDANCE DATE OF ISSUANCE mAymoi3 EXPIRY NOV11612013 OPERATING LIMITATIONS DATE ARE PART OF THIS CERTIFICATE DESIGNATION OR OFFICE NO. DARF-400148•CE alteration, reproduction or misuse of this cerii cafe may be perishable by a fine not exceeding $1,000 or not exceeding 3 years, or both. THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT WITH APPLICABLE TITLE 14, CODE OF FEDERAL REGULATIONS {CFR), FAA Form 8130.1 (4412011) Previous Edition 01104 May be Used old Depleted SEE REVERSE SIDE NSM 0052.00.693.4000 EFTA00011987

A PI This airworthiness certificate is issued under the authoriry of Public Law 104.5, 49 United Slates Code (USC) 44184 and Tile 14 Code of Federal Regulations (CFR). D w The airworthiness certificate authorizes the manufacturer named on the reverse side to conduct production fight tests, and only production light tests, of aircraft registered in his name. No person may conduct production flight tests under this certificate (1) Carrying persons or property for compensation or hire: andfor (2) Carrying persons not essential to the purpose of the night. r v This airworthiness certificate authorizes the light specified on the reverse side for the purpose shown in Block A, D This airworthiness certificate certifies that as of the dale of issuance, the aircraft to which issued has been inspected and found to meet the requirements of the applicable CFR. The aircraft does not meet the requirements of the applicable comprehensive and detailed airworthiness code as provided by Annex 8 to the Convention On International Civil Aviation. No person may operate the aircraft described on the reverse side (1) except in accordance with the applicable CFR and in accordance with condons and limitations which may be prescribed by the FM as pad of this certificate; (2) over any foreign country without the special permission of that country, in c Unless sooner surrendered, suspended, of revoked, this airworthiness certificate is effective for the duration and under the conditions prescribed in 14 CFR, Part 21, Section 21.181 or 21.217. EFTA00011988

mato STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE 1 NATIONALITY NC 2 MANUFACTURER AND MODEL 3 AIRCRAFT SERIAL 4 CATEGORY REGISTRATION MARKS Raytheon Aircraft Co. NUMBER N493LX 400A RK-244 Transport 5 AUTHORITY AND BASIS FOR ISSUANCE This eawonhasess cenAcate is issued pagan to the Federal Avtation Ad of 19SI) and cents, the, es a the date of deemd& the simnel to shish weed Ms been inspected and found to conleem to the type corshcato Monitor, to be In condbon to safe operation and has been enhan to rneel the re:we-rents of the applicable comprehensive and detailed einvonNness code as prove:kid by Anneal° the Convention on Intemallenal CM AWtbn• except as noted lea Escepbons: None TEWASANO CONDITIONS Unless sooner stnendered. suspended. teroked. at a terrnInahcn data N othanvise establoshect by the Adadnistrelor. this einirenhiness Cette:000 b elleCIMI BO Bee es the maintenance. preventatse men•Mend. and alterations are Paired In adadane *RI Fans 2I. 43. and 91 of Me Fathom, A registered Yl Sr UMW States. DATE OF ISSUANCE R 10/01/1999 DESIGNATION NUMBER AEA -FSCO -23 My Menlo% repoduceon. a Meese of Ithoelitcate may be paetheble Menne not exceeding SIAM et lepreonmeini not 11$014.910 3 semisweet. THIS CERTIFICATE MUST BE DISPLAYED M THE SAGAMI IN ACCORDANCE tMTH AMICABLE FEDERAL AVIATION REGULATIONS. FAA Farm 4100-2 (108) EFTA00011989

- EFTA00011990

Cleveland, Gala 44143 May 8.2013 VIA HAND DELIVERY Nextant Aerospace, LLC Cleveland, Ohio 44143 Attention: Re: RK-244 — Agent Authorization Ladies and Gentlemen: eit Options This letter is to confirm that Flight Options. LLC ("Flight Options") authorizes Nextant Aerospace, LLC, as Flight Options' agent, for a Beechjet 400A, bearing serial number RK-244 and FAA Registration Number N493LX, which is owned by Flight Options, for any and all authorized FAA actions. Sincerely. FLIGHT OPTIONS LLC Vice President of Whole Aircraft Acquisitions and Sales STATE OF OHIO tty Camm. ExpteS APIS a 2016 511-41.3 EFTA00011991

EFTA00011992

U.S. Department of Transportation Federal Aviation Administration EXPERIMENTAL OPERATING LIMITATIONS PURPOSE Research and Development MAKE Raytheon Aircraft Company MODEL 400A REGISTRATION N493LX SERIAL NUMBER RK244 I ) No person may operate this aircraft unless FAA Form 8130-7 is displayed at the cabin or cockpit entrance and is visible to passengers or flightcrew members. 2) No person may operate this aircraft for other than the purpose of RESEARCH AND DEVELOPMENT to accomplish the flight operation outlined in the program letter, dated May 13, 2013, which describes compliance with 14 CFR §21.193(d) and has been made available to the pilot-in-command of the aircraft. In addition, this aircraft must be operated in accordance with applicable air traffic and general operating rules of 14 CFR Part 91, and all additional limitations herein prescribed under the provisions of 14 CFR § 9I.319(i). 3) All flights must be conducted within the 48 contiguous United States of America, except for takeoffs and landings, this aircraft must not be operated over densely populated areas or in congested airways except when otherwise directed by Air Traffic Control or in an emergency situation. 4) N/A 5) N/A 6) N/A 7) This aircraft must not be operated unless it is inspected and maintained in accordance with appropriate military technical publications and/or manufacturer's recommendations. The owner/operator must select, establish, identify, and use an inspection program as set forth in 14 CFR §91.409(e), (0, (g) and (h). This inspection program must be recorded in the aircraft maintenance records. 8) The Pilot in Command of this aircraft must hold an appropriate category/class rating. If required for the type of aircraft to be flown, the Pilot in Command must also hold either an appropriate type rating or a letter of authorization issued by an FAA Flight Standards Operations Inspector. 9) N/A 10) N/A II) This aircraft may be operated under IFR, and must be properly equipped for instrument flight in accordance with 14 CFR § 91.205. All test maneuvers must be conducted during day Visual Meteorological Conditions (VFR). 12) No person may operate this aircraft for carrying persons or property for compensation or hire. 13) No person may be carried in this aircraft during flight unless that person is essential to the purpose of the flight. 14) N/A 15) The pilot in command of this aircraft must advise each passenger of the experimental nature of this aircraft, and explain that it does not meet the certification requirements of a standard certificated aircraft. 16) This aircraft must contain the placards, markings, etc., (or other operating instructions developed for an STC modification) as required by 14 CFR §91.9. Total Pages: 3 EFTA00011993

EFTA00011994

EXPERIMENTAL OPERATING LIMITATIONS PURPOSE Research and Development MAKE Raytheon Aircraft Company MODEL 400A REGISTRATION N493LX SERIAL NUMBER RK244 Page 2 of 3 17) This aircraft is prohibited from aerobatic flight; that is, an intentional maneuver involving an abrupt change in the aircraft's attitude, an abnormal attitude, or abnormal acceleration not nectssary for normal flight. I 8) This aircraft may conduct acrobatic flight in accordance with 14 CFR § 91.303. Aerobatics must not be attempted until sufficient flight experience has been gained to establish that the aircraft is satisfactorily controllable and in compliance with 14 CFR § 91.319(b). Acrobatic maneuvers intended to be performed must be satisfactorily accomplished and recorded in the aircraft records during the flight test period. I 9) N/A 20) This aircraft must not be used for glider towing, banner towing, or intentional parachute jumping. 21) No person must operate this aircraft unless within the preceding 12 calendar months it has had a condition inspection performed in accordance with the scope and detail of 14 CFR part 43 appendix D, or other FAA- approved programs and was found to be in a condition for safe operation. This inspection will be recorded in the aircraft maintenance records. 22) FAA-certificated repair stations and FAA-certificated mechanics with appropriate ratings as authorized by 14 CFR §43.3 may perform inspections required by these operating limitations. 23) Inspections must be recorded in the aircraft maintenance records showing the following or a similarly worded statement: "I certify that this aircraft has been inspected on (insert date) in accordance with the scope and detail of 14 CFR part 43, appendix D, or other FAA-approved programs, and was found to be in a condition for safe operation." The entry will include the aircraft total time-in-service, and the name, signature, certificate number and type of certificate held by the person performing the inspection. 24) If aircraft, engine, or propeller operating limitations are exceeded, an appropriate entry will be made in the aircraft records. 25) This aircraft must not be operated unless it is maintained and inspected in accordance with the requirements of 14 CFR Part 43. 26) This aircraft must display the word EXPERIMENTAL in accordance with 14 CFR §45.23(b). 27) The pilot-in-command of this aircraft must notify Air Traffic Control of the experimental nature of this aircraft when operating into or out of airports with operating control towers. The pilot in command must plan routing that will avoid densely populated areas and congested airways when operating VFR. 28) This aircraft does not meet the requirements of the applicable, comprehensive and detailed airworthiness code as provided by Annex 8 to the Convention on International Civil Aviation (ICAO). The owner/operator of this aircraft must obtain written permission from another country's Civil Airworthiness Authority (CAA) prior to operating this aircraft in or over that country. That written permission must be carried aboard the aircraft together with the U. S. airworthiness certificate, and upon request, be made available to an FAA inspector or the CAA in the country of operation. 29) Aircraft instruments and equipment installed and used under 14 CFR §91.205 must be inspected and maintained in accordance with the requirement!: of parts 14 CFR parts 43 and 91. Any maintenance or inspection of this equipment must be recorded in the aircraft maintenance records. 30) Application must be made to the geographically responsible MIDO (Cleveland, OH MIDO) for any revision to these operating limitations. 31) 14 CFR § 47.45 requires that the FAA Aircraft Registry must be notified within 30 days of any change in the aircraft registrant's address. Such notification is to be made by submitting Aeronautical Center Form 8050-I to AFS-750 in Oklahoma City, Oklahoma. 32) Condition inspections must be performed in accordance with 14 CFR part 43, appendix D at least every 100 flight hours. The inspections must he performed by an FAA-certificated mechanic with appropriate ratings as definntl in 14 r.pp x dl EFTA00011995

EFTA00011996

EXPERIMENTAL OPERATING LIMITATIONS PURPOSE Research and Development MAKE Raytheon Aircraft Corn . any MODEL 400A REGISTRATION N493LX SERIAL NUMBER RK244 Page 3 of 3 33) Familiarization flights must be conducted only over sparsely populated areas. If aerobatics are involved, the applicant must inform the local FAA office and additional limitations may be imposed as necessary. III. DARF-400148-CE May 20.2013 igna u e EFTA00011997

. EFTA00011998

nextant aerospace Quality Assurance Department To: Federal Aviation Administration Flight Standards District Office North Olmsted, Ohio 44070 From: Date: May 13, 2013 Director of Quality Assurance Nextant Aerospace Subject: FAA Program letter for Beech Jet 400A, Serial number RK244, Registration Number N493LX Ref: FAA order 8130.2G 1. Registered Owner: Flight Options RC . Address: 2. Aircraft Description: Twin Engine Light Jet a. Registration: N493LX b. Aircraft Builder Raytheon Aircraft Co c. Year mfg.: 1999 d. Aircraft Serial Number: RK244 e. Aircraft Model Designation: Beech let 400A Richmond Heights, Ohio 44143 3. The program purpose for the aircraft will be used To complete the flight performance profile in Research & Development Category in support of FAA Project SA 15250LA-T (Replacement of Wingtips) 4. Program Duration a. List the estimated flight hours required for program: 300 Hrs b. Number of flights: 100 c. Number of days: 180 S. Describe the areas over which the flights to be conducted and address of base operation: The base of operation is Cuyahoga County Airport, 355 Richmond, Cleveland, Ohio. Flights will be conducted in North America. 6. Describe the aircraft configuration: This Aircraft is a standard Beech Jet 400A with new Williams F144-3AP engines and upgraded avionics with full authority digital engine controls (FADEC) a. Maintenance Program 1. Hawker Beechcraft Maintenance Manual Chapter S Rev C22 or later with the exception of the 1T150 Engines. 2. Williams International recommended F144 3A Maintenance manual (FADEC maintenance is covered in 71-00-00 of this manual) 3. Maintenance Requirements for the Throttle Quadrant is addressed in the instructions for Continued Airworthiness on the F144-3AP STC. enior Inspector Nextant Aerospace EFTA00011999

. . • • EFTA00012000

LOG BOOK ENTRY from Designated Airworthiness Representative (DAR) REGISTRATION NUMBER AIRCRAFT MAKE/MODEL SERIAL No. TT/TSN LANDINGS/CYCLES N493LX Raytheon Aircraft Company 400A • RK244 8563.8 7115 I find that the aircraft meets the requirements for the certification requested and have issued a Special Airworthiness Certificate dated May 20, 2013 for the purpose of Research and Development. Limitations dated May 20. 2013 and issued with this certificate must be complied with. The aircraft must be maintained in accordance with manufacturers requirements unless another FAA approved maintenance program is utilized. Issuance of this certificate does not eliminate or replace any required maintenance requirements. The Special Airworthiness Certificate has been issued as required to support Research and Development flight-testing as defined in th app icant's program letter. The Standard Airworthiness Certificate dated R 19p111999 has been superseded. / 4/5/ 20 2.013 Date EFTA00012001

EFTA00012002

• • le MAJOR REPAIR AND ALTERATION u 5 Oesenrnont or (Airframe, Powerplant,Propeller, or Appliance) Trantpeeltavan lAcINal Aviation Achninilanakai Foon Soo/own OW) No 2120-0O20 itsodusi Electronic Tracking Number For FAA Use Only INSTRUCTIONS: Print or type all entries. See FAR 43.9. FAR 43 Appendix B, and AC 43.91 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty nor to exceed 51.000 for each such violation (Section 901 Federal Aviation Act 1958) 1. Aircraft NatiOnality and Registration Mark N493LX Serial No RK-244 Make Raytheon Aircraft Company model 400A Series 2. Owner Name (As Shown on registration certificate) Flight Options .11O Address (As shown on registration certificate) Ancireas cry Richmond Heiohts slew OH z,,, 44143-14 Country USA 3. For FAA Use Only 4. Type S. Unit Identification Repair Alteration Unit Make Model Serial Number 0 El AIRFRAME (AS described in Item I above) CI O POVVERPLANT K O PROPELLER O O APPLIANCE Type tasrvisaune 6. Conformity Statement A. AgenCYS Name and Address Et Kind of Agency Nanny Nextant Aerospace I Armrest Cq Cleveland sure. OH zu 44143.1453 Country USA O U.S. Cenelicated Mechanic O Manufacturer O Foreign Certificated Mechant C. Certificate No. 0 Certificated Repair Station CRS # 25NR667B O Certificated maintenance Organization D. I certify that the repair and/or alteration made to the unit(s) Identified in item 5 above and descnoed on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Extended range fuel per 14 CFR Part 43 APP. B 0 05/30/2013 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit Administrator of the Federal Aviation Administration and is identified es in item 5 was inspected in me manner prescribed by the APPROVED 0 REJECTED BY FAA Flt Standards Inspector Manufacturer Maintenance Organization I Person Apart/wed by Canadian Department of Transport FM Designee X Repair Station Inspection Authorization Other Specify) Certificate or Designation No. CRS # 25NR667B 05/30/2013 EFTA00012003

lb • EFTA00012004

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration math and date work completed.) N493LX Nationality and Registration mark Part I of 3 The Following Equipment was removed along with Associated Hardware. 05/30/2013 EFD-871 622.9345-203 Electronic Flight Display EFD-871 622.9345.203 Electronic Flight Display MFD-871 622.9434.213 Multi Function Display ICU-85 622-6189-002 Internal Compensation Unit ICU-85 622-6189-002 Internal Compensation Unit AHC-85E 622.9336-400 Attitude/Heading Computer AHC-85E 622-9336-400 Attitude/Heading Computer SDU-640B 622-9735-001 Sensor Display Unit SDU-640B 622.9735-001 Sensor Display Unit DCP-5000 822-1028.011 Display Control Panel DCP-5000 822-1028.011 Display Control Panel ARP-851 622.9500-011 Altitude Reference Panel ARP-851 622.9500-011 Altitude Reference Panel AAP-851 822-0328-011 Altitude Awareness Panel AAP-851 822.0328.011 Altitude Awareness Panel CHP-850 622-7397-002 Course Heading Panel DBU-4100 822-0014-002 Data Base Unit DAU-650 622-9344.101 Data Acquisition Unit SDD-640A 622-9347-001 Sensor Display Driver IOC-4000 ( 4) 622-9814-514 Card Assembly MDC-4000 622-9818-751 Maintenance Computer CSU-4000 (2) 822-0049-002 Configuration Strapping Unit FMC-5000 (4) 822-0891-008 Flight Management Computer PWR-4000 (4) 622.9945.021 lAPS Power Card GPS-4000 822-0931-003 GPS Receiver Mounts 622-9430-002 EFD /MFD Mounts EFB Electronic Flight Bag Mounting 0 Additional Sheets Are Attached Date Form 337 (10.C6) EFTA00012005

• • • EFTA00012006

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality end registration mark and date work completed.) N493LX 5/30/201 Nationality and Registration Mark Page 2 of 3 Installed the Following Equipment along with Associated Hardware. Date Model Part Number Description Weight Arm CCP-3000 822-1746.002 Cursor Control Panel 2.60 90.0 CCP-3000 822-1746-002 Cursor Control Panel 2.60 90.0 DCU-3001C 822-2362-003 Data Concentrator Unit 5.0 325 DCU-3001C 822-2362.003 Data Concentrator Unit 5.0 325 ECU-3000 822-1200-209 External Compensation Unit 0.40 57.5 ECU-3000 822-1200.209 External Compensation Unit 0.40 57.5 FSU-5010 822.1543.101 File Server Unit (1° IFIS) 6.5 60.83 ECU-3000 822-1200.998 File Server Unit (1st IFIS) 0.40 57.5 AFD-3010E 822-1753.416 Adaptive Flight Display 12.90 89.2 AFD-3010E 822-1753.416 Adaptive Flight Display 12.90 89.2 AFD-3010E 822.1753-416 Adaptive Flight Display 12.90 89.2 AFD-3010E 822.1753-416 Adaptive Flight Display 12.90 89.2 IMT-3010 822-1140-401 AFD Mounting Rack 4.40 85.0 INIT-3010 822-1140-401 AFD Mounting Rack 4.40 85.0 IMT-3010 822-1140-401 AFD Mounting Rack 4.40 85.0 IMT-3010 822-1140-401 AFD Mounting Rack 4.40 85.0 10852801Y00 Fuel Quantity Conditioner 0.90 324 PC920-2A2000PH-2A1 Fuel Flow Conditioner 1.10 325 GPS-4000S 822-2189-004 GPS Receiver 6.0 37 CI 429-410 GPS Antenna 1.0 166.14 Amp Cluster N241100-002 DC Voltmeter 1.5 97.4 373-93-1501-1 Speed Switch (2) 0.25 89.2 DBU-5010E 822-3000-202 Data Base Unit 1.60 134.5 PS-8350 501-1228-004 Power Supply 12.5 52.9 MMT-5000 822-1811-003 File Server Unit Rack 0.30 57.5 MMT-3010 (2) 822-1290-003 AHS Mounting Rack 1.80 57.5 XM WR-1000 822-2031-002 XM Weather 1.5 41.0 CHP-3010 822-1280-003 Course Heading Panel 1.30 92.5 Options Configuration Module. OCM-4100 822-1463.228 WAAS/LPV 0.30 57.5 Options Configuration Module. OCM-4100 822-1463-228 0.30 57.5 WAAS/LPV El Additional Sheets Are Attached Form 337 (10.06) EFTA00012007

S • • EFTA00012008

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (II more space is required, attach additional sheets. Identity with aircraft nationality and registration mark and date work completed.) N493LX 05/30/2013 Page 3 of 3 Nationality and Registration Mark Date Model Part Number Description Weight Arm CSU-4100 (2) 822.1364.002 Configuration Strapping Unit 1.60 55.7 MDC-3110 822.1987.006 Maintenance Data Computer 0.80 55.7 FMC-6000 (2) 822.0868.123 Flight Management Computer 1.90 55.7 ADC-850D (2) 822.0389.468 Air Data Computer 5.30 60.83 AHC-3000A (2) 822-1378.001 Attitude Heading Computer 4.80 57.5 DCP-3030 (2) 822-1828-002 Display Control Panel 1.90 89.96 PWR-4000 (4) 622-9945-022 IAPS Power Card 1.3 55.0 IOC-4100(4) 822-1362-511 Input/output Concentrator 0.8 55.0 LT-4001.010 Master Caution Panel 1.3 87.0 Rev. Panel 373-91-3203-1 Pilot Reversion Panel 0.2 88.0 Rev. Panel 373-91-3203-3 Co-pilot Reversion Panel 0.2 88.0 9-PED 373-91-3203-9 9-Pedestal Panel 1.8 92.89 345.6196 ELT Switch 0.2 88.0 Annunciator led-42-12-BB-E0Y47 AUX BATT (1/2) Annunciator 0.05 88.0 Annunciator (2) Led-40-18-BB-E0Y45 Pull Up/ Terrain Annunciator 0.05 88.0 Annunciator 24840231 Terrain Inhibit/ Terrain Fail 0.05 88.0 In Accordance with STC ST109595C. See Attached Copy MM Supplement, Nextant Aerospace Doc. No. 373.00-0023 Rev IR Dated 09/02/2011 or later FAA approved revision, installed on Aircraft. Equipment Pilot Guides are Installed in the Aircraft as Portable Document Format (.pdf) via supplied I-Pad. NOTE: Portable electronic devices used to store required aircraft records required by Part 91.9 are considered Electronic Flight Bags (EFB) per FAA Advisory Circular AC 120-768 par 4-g. Commercial operators are required to obtain authorization for their use from their managing Flight Standards District Office. Instructions for Continued Airworthiness (ICA) Ref Nextant Aerospace Document 373-00-0002.Rev C or Later are included in the Aircraft Maintenance Records Carried out System Ground Test Plan PAW Master Drawing List (MDL) 373.00.004 Rev C. Carried out Hawker Beechcraft Service Bulletin 34-3431 Reduced Vertical Separation Minimum (RVSM) Airframe Inspection / Modification. Performed FAR 91.411Inspection per Part 43 appendix "E" Pitot Static & FAR 91.413 Inspection per Part 43 appendix "F" Transponder System checks. K Additional Sheets Are Attached Form 337 0046) EFTA00012009

• • EFTA00012010

• • • 11,1Ra "lain of Jkinerira Pepartment of Zranspotintion getter:II (Ablation cAbministrution $uppientental 'ape Certificate arletecalei 44.444.4relk• ../fianZies ST I 0959SC Nextant Aeros ace LLC Richmond Heights, Of! 44143 &WOW 44114 ereir 6 414 *WO eie441/444AretiliWIfiedaletede 44 da.M74/4AVO emaneavaaesoa 44-9,4erai 044-454e4arnev• .444ev‘O 4wr i„e„-..044. „wan...4 *end 25 ./4,4 Federal Aviation Avast (See Prima 3 and 4 for complete certification basis.) oniadail- sc;n4;474,44;ney, Al 6SW ./E0.4. Hawker Beechcraft Corp. ..sgedi 4O0A givertythao rano ntiosYlier Installation of Rockwell Collins Pro Line 21 Electronic Flight Instrument System (EFTS) with Rockwell Collins FMS-6100, Localizer Performance with Vertical Guidance (LPV) approach capability and Universal Avionics Systems Company (UASC) Terrain Awareness Warning System (TAWS) in accordance with Nextant Aerospace LLC Master Drawing List Doc. No. 373-00-0001 Revision W, dated March 29, 2012, or later FAA approved version. 24.n.r.gaivm ebuilf;v344.;viu : 1) The installer must determine whether this design change is compatible with previously approved modifications. 2) If the holder agrees to permit another person to use this certificate to alter a product, the holder must give that person written evidence of that permission. . 3) For aircraft equipped with Pratt & Whitney JTISD Engines FAA approved Airplane Flight Manual Supplement, Nextant Aerospace LLC Doc. No. 373-00-0008 Revision IR, dated 10/19/2009, or later FAA approved version, is required on board the modified aircraft. erehAe".44 cad a- ar da, 4, AA tryserisslawnetha rim ryl revie AvaLeiArroaoreei why...need envsione tv a kaniaer.44va dale resenr4ht 44144444441454 43rR .4444;s41,44.7494 la; Alevre 4.444.444,4 ./11.404sim4.14n4.4.4a Para eAreeesetm • June 26, 2008 gaze r/e....‘;w&-.4 October 19, 2009 Paleets...4.10eni: 512/P OrnelleAl : September 26, 2011; April 05,2012 anger, ys ems all g Chicago Aircraft Certification Office (lisle) Any *1 CCCCC Jon of this eertitlwce Jr pleas n0 a1,ON. Or S00 041K AOt Oxe010anp l yllerS. of both. TM Parw 1110.1110.0/1 O is coral lats. n4y aft trans need In neerderee win IM 1.4 . EFTA00012011

0 • 0 EFTA00012012

• • • ilnifebikafee Of America Pepartment of Zrunsportzation - 1:cberal cAbiation crthntiliistrittion Supplemental `Type Qlertificate (Continuation $lieet) te/ rande, ST I 0959SC rAswenen• October 19.2009 Date Amended; September 26, 2011; April 05.2012 Monlerlavio andrinsetaavki nevrawedi: 4) For aircraft equipped with Williams FJ44-3AP Engines, those engines must be installed under SIC ST0237ILA. 5) For aircraft equipped with Williams FJ44-3AP Engines FAA approved Airplane Flight Manual Supplement, Nextant Aerospace LLC Doc. No. 373-00-0023 Revision IR, dated September 2, 2011, or later FAA approved version, is required on board the modified aircraft. 6) Aircraft must have previously qualified for Operations in Reduced Vertical Airspace via: RK- I thru RK- I 17 and RK-I 19 thru RK-I39, Hawker Beechcraft Service Bulletin No. 34.3431. RK-I 18, RK-140 thru RK-224, Hawker Bccchcraft Service Bulletin Nos. 34-3228 and 34-3431. RK-225 thru RK-299, Hawker Beechcraft Service Bulletin No. 34-3431. RK-300 and after as original equipped from Hawker Beechcraft. 7) For aircraft equipped with Universal Avionics Systems Corporation (UASC) TAWS FAA approved Airplane Flight Manual Supplement, Nextant Aerospace LLC Doc. No. 373-00-0036 Revision IR, approved March 28, 2012, or later FAA approved version, is required on board the modified aircraft. 8) For aircraft with Collins Proline 21 FMS-6100 LPV Approach enabled FAA approved Airplane Flight Manual Supplement, Nextant Aerospace LLC Doc. No. 373.00-0032 Revision IR, approved March 28,2012, or later FAA approved version, is required on board the modified aircraft. Based on 14 CFR §§2 1 .1 15 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Hawker Beechcraft 400A aircraft is as follows: a. The type certification basis for the Hawker Beechcraft 400A aircraft is shown on TCDS Al6SW for parts not changed or not affected by this change. b. The certification basis for the parts changed or affected by this change since the reference date of application, September 29, 2009, is based on TCDS A I6SW and §§ 14 CFR Part 25 as shown on page 4 of 4 of this STC. Any ale &&&&& on of rerun Cleo is Duo aneela by a Gn0 of not *needing Si.000. Or inparsonmene Trot OACOOd.no 1 yo00. Or bOth. "a Man 4110.14(10431 PAU 3 of 4 eAGLI This certificate way be cransfyi red f., accordance Win FAA 11.0. EFTA00012013

• • • EFTA00012014

• • • Janda Slake of America Department of Zgransportntion - federal Abiation Atiministration $uppiettuntal 'Type aertificatt (a:Continuation $hnt) gkr4, ViAkanot October 19, 2009 Date Amended: September 26, 2011; April 05. 2012 Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the baseline Installation of Rockwell Collins Pro Line 21 Electronic Flight Instrument System (EFTS) with Rockwell Collins FMS-6100 modification was determined to be TCDS Al6SW and the following later regulations: Amda 124-4] 25.771 (a.e) MOORS-23) 25.301; 25.303; 25.581; 25.607; 25.611, 25.773 (aX1X2Xd) Amdt(25-310 25.1309 00(bXeXdflg); 25.1322 Amck.(25-40] 25.901 (b)0X0; 25.1549 (4X6X0 Amd1.125-411 25.1321 (a0(b)(c)(c); 25.1331; 25.1333 Mndt.(25-42) Amd1425-46] Ai/Mt(2544) Amdi.125-721 Am0112540) 25.1501 25.603; 25.605; 25.613; 25.1529 25.307; 25.571. 25.1307 25.1316 25.1329(h) NO; 23.1351 MOM 25.1381; 25.1521 (.Xc); 25.1543 (b); 25.1581; 25.1583 (a) Amdt425.861 Amd1425.901 Amdtl25.91) Amett25-102) Amdt[25.105J 25.305 25.1303 25.561 25.981 (a(6) 25.1585 (o) Amdt425.108) Amdl.(25.109] Amdc.(25-113) Amdi425-1221 Amc11425-1231 25.1325 00 25.1323 (a)(1)(g) 25.869 (aX4); 25.1431 25.1317 (aX6)(e) 25.1353 (aXM Based on 14 CFR §§ 21 115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Collins Proline 21 FMS-6100 with LPV Approach enabled and UASC TAWS was determined to be TCDS Al6SW and the following later regulations: AmattOriginali 25.601. 25.605. 25.609. 25.613.25.1301, 25.1357. 25.1381. 25.1525, 25.1541, 1S.1581 Amdr[24-41 25.771 (a) Amd1.(25-23) 25.301; 25.303; 25.305. 25.307, 25.561(c); 25.607; 25.611. 25.1307 Amdt.(25.381 25.603. 25.1322, 25.1583(O Amdl.(25.401 25.1585 (a) Ainc1i125-411 Aindi.(25-421 Amdt125-46) Amdl.(25-541 Amdt.(25-72) 25.1309 (a)(b)(401)(aXa) 25.1501 25.777(a)(c) 25.1529 25469(a)(1) 25.1351 (a)(1) Amdr(25-102) Amdt.P5-113i A=0(25-1231 25.981(aXb) 25.14310) 25.1353 (aXe) - END - Any &&&&&& On of t • COrtifiene II poniSOSO by • fPM 0f not ontoolling SI.000, or I pti SASS not •44•003n9 3 Hero. or both. FAA Mom 4110.2.1110.401 PS 4 Of 4 SOS Thin cortirIsto My M trensferrod in accordence .ith DA 21.17. EFTA00012015

• • • EFTA00012016

0 MAJOR REPAIR AND ALTERATION U.S OOPWITIAI Of (Airframe, Powerplant, Propeller, or Appliance) trenwraln-m Naomi Aviation AtIrnialcustron Form Approved omen° 2120-0O20 11/30,2007 Electronic Tracking Number For FAA Use Only INSTRUCTIONS: Print or type alt entries. See FAR 43.9 FAR 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition Of this fOrm. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act 1958) 1. Aircraft Nabonality and Registration Mark N493LX Serial No. RK 244 Make Raytheon Aircraft Company Model 400A Series 2. Owner Name (As shown on registration certificate) Flight Options .LLC Address (As shown on registration certificate) Address CT). Richmond Heights slaw. OH zip 4414 -14 Country 3. For FAA Use Only 4. Type 5. Unit Identification Repair Alteration Unit Make Model Serial Number 0 el AIRFRAME (As described in hem t above) 0 • POWERPLANT 0 O PROPELLER 0 . APPLIANCE Type stmeeaurer 6. Conformity Statement A. Agencys Name and Address B. Kind of Agency rim. Nextant Aerospace Adores, City Cleveland sta. OH zip 44143-1453 Cotrey USA O U.S. Certificated Mechanic O IManufacturer O Foreign Certificated Mechanic C. Certificate No. 0 Certificated Repair Station CRS # 25NR667B O Certificated Maintenance Organization D. I certify that the repair and/or Migration made to the unit(s) identified in item S above and described on the rever e or attachments hereto have been made in accordance with the requirements of P rt 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Extended range fuel per 14 CFR Part 43 App. 6 El Signature/Date of Authorized Individ 05/30/2013 7. Approval for Return to Service Pursuant to the authonty given persons specified below. the unit identified in item 5 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is @ A P P R O V E D 0 REJECTED BY FM Fit Standards Inspector Manufacturer Maintenance Organization Person Approved by Canadian Department of Transport FAA Designee X Repair Station Inspection Authorization i Other (Specify) Certificate or Designator NO CRS # 25NR667B Signature/Date of Authorized Individu. 05/30/2013 FAA Form 337 0-061 EFTA00012017

EFTA00012018

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable ainvorthtness requirements. 8. Description of Work Accomplished (11 more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) N493LX Nationality and Registration Mark Nextant Aerospace Completed STC # ST02371LA Removed Pratt and Whitney JT15D-5 Series Engines . 05/30/2013 Date Installed the Williams International FJ44-3AP Engines with Full FADEC and Associated Systems in accordance with Nextant Aerospace MDL -NXT-001 Rev IR Dated 08/22/2011 or later FAA approved revisions, and FAA Approved AFM Supplement NXT-1-AFMS Rev IR dated 9/15/2011 of later FAA Approved revisions. Installed Left Engine Part Number. 111000-202 Serial No. 252757 Installed Right Engine Part Number 111000-202 Serial No. 252758 ICA AFM Supplement was installed on Aircraft. Nextant Aerospace Instructions for Continued Airworthiness Document NXT-ICA Rev IR or later FAA accepted revisions are included in the Aircraft Maintenance Records. Carried out Engine Ground Runs and System OPS checks SAW Ground Test Plan 373.00-0024 Rev F. End K Additional Sheets Are Attached FAA Form 337 (10-06) EFTA00012019

l EFTA00012020

}loath Slake 01,P1merico Pepiirtmettt of "Mri iapnr ha lion - Athena cAb in tint' cainiiiiiistration $uppinnental Tut antificate -4400 fi ST02371LA 97L YlerrAWne.weee'n' Nextant Aeros ace, LLC Richmond Heights, Ohio 44143 er4eed /414 tArel /4 jfr o eirtifra/Se e'h/ Fara' /4 Atekheem andeanr44im& erre/fre rrevvtv//temon med.' /4 aewer/41;orvat terthwtevno•°Mad 25* oth -9,7viprzteathiv: -93efideravv. *Certification basis is set forth on Tan A I6SW and continuation sheets 3 and 4. .6:10.4.4101flotet Wee/r/ea/n./Kmres,".. Al 6SW Hawker 13eechcraft 400A Stverfer4kn gam Ylis t refe.wyn. Replacement of Pratt & Whitney JT15D-5 series engine with Williams International F144.3AP engine (TCDS E3GL) with Full Authority Digital Engine Control (FADEC) and associated systems, in accordance with Nextant Aerospace Master Drawing List No.: MDL-NXT-001, Revision IR dated 8/22/2011, or later FAA approved revisions and FAA Approved Airplane Flight Manual Supplement, NXTI-AFMS, Rev IR, dated September IS, 2011 or later FAA approved revisions. Nextant Aerospace, LLC Instructions for Continued Airworthiness document NXT1-ICA, Revision IR, or later FAA accepted revisions must be provided with this STC. Smitrom, anatvraimo.. The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of that aircraft. The approval of this modification applies to the above-noted airplane models only. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. (CONTINUED on page 3) Sot ewhiecalo emal/h arvyralearts riala reufrofis /4 irmajfice twravertraketemaria as elecl teethe Ornrenalreaffireonselerierweverviev a 4werrihthive dale' As ederrot;to evireadeal, ,Arketiteow/c, eyeen Fetrieredfitvideen dgriorriredretheva givenc4flactwiew, 51k4seAunonen.- March 24, 2008 September 27, 2011 .02/4 mti.senvi• ebvemaremi.- frithierriev. (Signature) Manager, Propulsion Branch Los Angeles Aircraft Certification Office (Title) Any eremites? of Mu certificate it punishable by a fine of not tweeting 31,004 or imprisonment not weeding 3 years, or froth. FAA ran 0110-200•441 Pete 1 at 4 .7 du eratferace may Sc transfenvi arronfaure ',nth fillt,27.47. EFTA00012021

EFTA00012022

INSTRUCTIONS: The transfer endorsement below may be used to notify the appropriate FAA Regional Office of the transfer of this Supplemental Type Certificate. The FAA will reissue the certificate in the name of the transferee and forward it to him. TRANSFER ENDORSEMENT Transfer the ownership of the Supplemental Type Certificate Number to (frame of transferee) attains of transfer) Oliallite and lora) (CYcz Shut, and Liptak) from (Name of gran tor)(Trint or type)_ (Address of grantor) Pato kr /al I aft) (plat Pete, end Zip rah) Extent of Authority (if licensing agreement): Date of Transfer: Signature of grantor an ink) Past 2 of 4 EFTA00012023

EFTA00012024

puilrb Auden (Of cAnterirn Prinirltitent of Vint ttoportn tion - gebertil cabintioat cAbmittiotra Non $upplatuntal Ewe Tertificate (Cfontinuation $liget) Afeeenie/< ST02371LA ..Waterrthirm3 ammo/la:ono. loomammeil • Nextant Aerospace, LLC, "Installation of Rockwell Collins Pro Line 21," Amended STC ST10959SC, dated September 26, 2011 or later FAA approved revisions is required as part of this alteration. • The new Vmca and Vmeg values arc 94 KIAS and 93 K1AS respectively. • The new engine minimum rated thrust is 3,031 lb at sea level, flat rated to an ambient temperature of 77°F. • Approved engine fuels are: Grade Specification Jet A ASTM-D 1655 Jet A-I ASTM-D 165.5 rerlejeeethewSewth The certification basis for this modification is as follows: The original certification basis for the Hawker Beechcraft Model 400A airplanes identified on TCDS Al6SW, Revision 26, dated March 17, 2010: Part 25 of the Federal Aviation Regulations effective Febmary I, 1965, as amended by 25.1 through 25-40, plus §§ 25.1335, 25.1351(d), 25. I353(cX5), and 25.1447 of Amendment 25.41; §§ 25.29, 25.255, and 25.1353(eX6) of Amendment 25.42; and §§ 25.361(b) and 25.1329(h) of Amendment 25-46. Part 36 of the Federal Aviation Regulations effective December 1, 1969, as amended by 36-1 through 36-17; SPAR 27 effective Febmary 1, 1974, as amended by 27.1 through 27-5; and Special Conditions No. 25-ANM-32 dated Febmary 22, 1990 (High Altitude Operation at 45,000 feet), and Special Conditions No. 25-ANM-33 dated June 18, 1990 (Lightning and Radio Frequency Energy Protection). (Sec NOTE 12) Equivalent Safety Items: (1) Out-of-trim characteristics § 25.255 (2) Pilot compartment view § 25.773033(2) (3) Passenger compartment door § 25.813(e) (4) Emergency exit marking §§ 25.811(d)(1) and 25.811(d)(2) Application for amended Type Certificate dated February 18, 1988. Regulation at a later amendments for components and areas affected by the change (Ref. FAA approved Compliance Check List): Subpart A - General : 25.2(25.99) Subpart B — Flight: 25.207(25-121), 25.255(25.42) Subpart C — Structure: 25.571 (25-96) piny dictation of tfiu marmite is ponisfrabb by a fine of not crow% 31,004 or imprisonment not eventing 3 rue or 6oth. FM roes M20-2110-411 Pete t of a 'MO eategete may fre tmeilerrel tit °creamy with f:P4t21.47. EFTA00012025

EFTA00012026

Nuittb "hilts Of America Pepartment of transportation - geberni ciliation cAbmittistrntion „Sup-plartental Type Certificate (gartfinurdion $ipet) Afeednlei, ST02371LA free4eathen Sera /conk:tam, Subpart D —Design and Construction: 25.603(25.46), 25.605(25-46), 25.611(25-123), 25.613(25-112), 25.625(25-72), 25.832(25-72), 25.863(25.46), 25.869(25.123), Subvert E — Powernlant: 25.901(25.46), 25.903(25-100), 25.951(25.73), 25.961(25-57), 25.981(25-125), 25.994(25-57), 25.997(25-57), 25.1013(25-72), 25.1019(25-57), 25.1021(25.57), 25.1043(25-42), 25.1045(25-57), 25.1091(25-100), 25.1093(25-72, 25.1103(25.46), 25.1141(25-115), 25.1143(25-57), 25.1163(25-57), 25.1165(25-72), 25.1181(25-115), 25.1183(25-101), 25.1185(25-94), 25.1189(25-57), 25.1195(25.46), 25.1203(25-123), 25.1207(25-46). Subvert/ — Equivalent& 25.1301(25-123), 25.1305(25-115), 25.1307(25-72), 25.1309(25-123), 25.1316(25-80), 25.1317(25-122), 25.1321(25.41), 25.1331(25-41), 25.1351(25-72), 25.1353(25-123), 25.1357(25-123), 25.1381(25-72), 25.1431(25-113), 25.1438(25-41), Subpart G — Operating Limitations and Information: 25.1501(25.42), 25.1521(25-72), 25.1527(25- 105), 25.1529(25-54), 25.1543(25-72), 25.1549(25-40), 25.1551(25-72), 25.1557(25-72), 25.1581(25-n), 25.1583(25-105). Subpart H - Electrical Wiring interconnection Systems (EWIS): 25.1701(25-123), 25.1703(25-123), 25.1705(25-123), 25.1707(25-123), 25.1709(25-123), 25.1711(25-123), 25.1713(25-123), 25.1715(25-123), 25.1717(25-123), 25.1719(25-123), 25.1721(25-123), 25.1723(25-123), 25.1725(25-123), 25.1727(25-123), 25.1729(25-123), 25.1731(25-123), 25.1733(25-123). 14 CFR Part 34 (34-3): 34.11 14 CFR Part 36 (36-28): 36.I--36.7, 36.101-36.105, 36.1501, 36.1581. The following Noxtant Aerospace Continued Airworthiness Supplements are applicable to airplanes modified in accordance with this STC: • Master Minimum Equipment List document No. MMEL Rev. 8, dated 02/21/2011 or later FAA approved revisions. • EWIS (Electrical Wiring Interconnection Systems) Inspection Procedure/Report No. NXTI-EA-007 Rev A dated 8/24/11 or later FAA approved revisions. -END- Any titivation of this entifstote is pintisita64 ky a fine of no ttrutatto $3.000, or imprisonment not to-ceding 3 years, or 6otk ma Foxe 6110.2420.481 Part • 04 4 ihiscertifiSote may 6: tmofertain areortanee with Tfilt,21.47. EFTA00012027

EFTA00012028

420 US Dispartinent MAJOR REPAIR AND ALTERATION at nainert1140 (Airframe, Powerplant, Propeller, or Appliance) Want Aviation Administration Form Approved OM No 21200020 11/302301 Electorsic Tracking Natter For FAA Use Only INSTRUCTIONS: Print or type all entries. See Title 14 CFR §43.9, Part 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report Is required by law (49 U S.C. §44701). Failure to report can result in a civil penalty for each such violation. (49 U.S.C. §46301(a)) 1. Aircraft Nationality and Registration Mark USA, N493LX Serial No. RK-244 Make RAYTHEON AIRCRAFT COMPANY ICAO AIRCRAFT ADDRESS CODE:51416115 Model 400A Series Not Applicable 2. Owner Name (As shown on registration certificate) FLIGHT OPTIONS LLC FLIGHT OPTIONS LLC Address (As shown on registration certificate) At:Cross City RICHMONO HEIGHTS State OHIO Le 44143.1453 3. For FAA Use Only 4. Type 6. Unit Identification Repair Alteration Unit Make Model Serial No. K ril AIRFRAME (As described In Item I above) 0 K POWERPLANT 0 IN PROPELLER 0 K APPLIANCE Type Manufacturer 6. Conformity Statement A. Agencys Name and Address B. Kind of Agency Hem. me U. S. Certificated Mechanic Manufacturer Adams Foreign Certificated Mechanic C. Certificate No. City Blichantica Style NY Cedificated Repair Station DJFA206D rip 13101 USA x Certificated Maintenance Organization D. I certify that the repair and/or alteration made to the unit s) identified in item 5 above and described on the reverse or attachments hereto have been made In accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Extended range fuel per 14 CFR Part 43 K APP. (3 Signature/Date of . rove or 0 0Service Pursue t to the authority given persons specified below, the unit Identified Administrator of the Federal Aviation Administration and Is L in item 5 was inspected in the manner prescribed by the Approved D Rejected BY FAA Fit. Standards Inspector Manufacturer X Maintenance Organization Persons Approved by Canadian Department of Transport FAA Designee Repair Station Inspection Authorization Other (Specify Certificate or Designation No. DJFA 206D Signature/Date of Autho FAA Form 337 rio-os) EFTA00012029

EFTA00012030

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. S. Description of Work Accomplished (If more space is required, attach additional sheets Identify with aircraft nationality and registration math and date work completed.) USA N493LX Nationality and Registration Mark 4/3/2012 Date Removed EFB Mount Assembly that was previously installed under Engineering Order M25-10/05-011. The aircraft weight and balance has been updated. INSTRUCTIONS FOR CONTINUED AIRWORTHINESS: None AA Form 337 no-as END Additional Sheets Are Attached EFTA00012031

EFTA00012032

UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE 1 NATIONAUTY AND 2 MANUFACTURER AND MODEL 3 AIRCRAFT SERtAL 4 CATEGORY Raytheon Aircraft Co. N493LX 400A RK -244 Transport REGISTRATION MARKS NUMBER 5 AUTHORITY AND BASS FOR ISSUANCE Thy almorthIrtess terra la Issued pursuant to Coi Federal /widen Act of1 958 end coreDea that. as of Ihe dabs of tuuance. the Omit to ittah Issued has been Inspected end toad to =don to Ou type corticate Nervfot, to Debt:I:neon for sate operettas end has been ahem to meet the 13(grernents of the appkable comprehensive end detailed atm.:stings' code seen: toed by Marox no the Convandon on ~aeon& tDMI Avtatkai. except es noted herein. ecoepeons: None 5 TERMS MD CONDMONS Unless *toner riumerared, stoponded. mob& or e torrnhattri date Is °View» oatab i by ITO Attnertseator, this idnecelhbeta Cereksto ta effectNe es Iona as the mal pre-rental:ye rnatitamance, and alterallona are performed In accordance oil Parts 21. 43. end 91 of the Foam: Airtet)on Redutothra te. and the a-YtTelbrotl-ktared h Pe Ulled Stem. DATE OP ISSUANCE R 10/01/1999 DESIGNATION NUMBER AEA -FSDO -23 My ~an norcducart. or raw of Cia cerCt•uu may he swittable Dye Pie sol escorstsp 11,000 a bralkeresnt nut n¢eedh+p3 ras or tat THIS CERTIFICATE aftt8T 88 DISPtAYED N THE AIRCRAFT P4 ACCORDANCE WITH APFUCABLE FEDERAL AYIATION REGULATIONS. FAA Form 81004 (3-08) EFTA00012033

II 4 EFTA00012034

ENGINEERING ORDER Aircraft Type Aircraft Number Serial Number Station Engineering Order Number M25-10/05-011 Revision Numbe Original Date 10-19-2005 Page 1 of: 1 E NG I NE ER I NG ORDE R T I TL E Electronic Flight Bag Mount Installation — Beechjet 400 Fleet Effectivity: Description: Accompanying Documents:. Aircraft serial numbers RK-123 and after To install a fabricated mount assembly near the co-pilots map light rheostat to hold the electronic flight bag computer Work Compliance Instructions Form. DER approved Engineering Directive EDW01-5. FAA forms 337 and 8110-3, For the effective aircraft to obtain a paperless cockpit environment Reason: Prepared By Keith Gawsyszawski Quality Assurance Robert Beaumont Approved By Todd Hattaway Regulat • ry Compliance Date 10-19.2005 Date ;eta -- Date Major Repair K Minor Repair FAA Approval (E) Yes K No Weight & Balance Affected (E) Yes K No Weight 4 lb increase Arm 108 Parts Required Yes, FG3500-400N, EFB mount assembly, 4 each AN3-5A bolts, 4 each NAS1149F0363P washers, 1 each -11 placard Drawings Required Yes, 1175TA, rev A. 5245D, rev B, 5244FC, rev B (included in the Engineering Directive) Publications Affected Equipment List Update K yes 18) No RVSM Status Affected None K Yes No AD List Affected K yes No Estimated Cost $176.00 Estimated Labor Hours 4.0 hours Distribution Remarks I References Z000000 Maintenance Planning Maintenance Quality Assurance Operations Procurement Aircraft Manufacturer Federal Aviation Administration The planning department shall add this EO to a scheduled work order whenever an effective aircraft is located at one of the Raytheon dedicated maintenance facilities and adequate down time permits. Priority Code (check all that apply) K Urgent IZ Mandatory K Attrition FO-09 GMIVI Revision 1 0912005 EFTA00012035

EFTA00012036

' .i sirr iZadrizia WORK COMPLIANCE INSTRUCTIONS .__--— 0...0,0— -- Page: Aircraft Number: Station: Work Order # Effectivity 1 of 2 RK-123 and after 0 Enginee ing Order Number: M25-10/05-011 OR 0 Fleet Campaign Directive Number: T I T L E Electronic Flight Bag (EFB) Mount Installation Procedures For Flight Options, LLC., Beechjet 400A's Item Work Description Mechanic Inspected 01 Document the maintenance action on a Flight Options maintenance transaction report form FO-501 with the following statement in the discrepancy side: 'Accomplishment of Flight Options EO M25-10/05-011 Installation of the Electronic Flight Bag, FG3500 mount assembly is due' 07 Remove electrical power from aircraft and disconnect main aircraft battery. 03 Loosen the upper glare shield and right side cover (which contains the reading fight and air-cell phone assemblies) by removing the mounting screws and separating the Velcro strips. : 04 Remove the three screws and 90 degree cover panel form the aft edge of the right side cover panel and discard. cr 05 With the glare shield and right side cover disconnected, locate the pre- existing fastener holes located on the shelf just below the copilots windshield and temporarily install the Electronic Flight Bag (EFB) mount assembly using the four AN3-5A bolls and NAS1149F0363P plain washers (included In the kit) to the pre-existing fastener holes. Snug but do not tighten bolts at this time. .-- . a rtt 06 Adjust the position of the EFB mount assembly to provide sufficient clearance between the existing ashtray and the EFB mount thumbscrew. - 07 When proper clearance Is achieved in step five. (thumbscrew does not touch the ashtray when rotated), tighten mounting bolts to 22 to 28 inch pounds (AMM Chap 20). 08 Reinstall the right side panel. Trim the aft edge of the panel as necessary to provide clearance between the panel and the 1175TA bracket, as identified in engineering Directive EDW01-5, figure 2, on page 3. Trim leather covering as necessary and secure with adhesive (contact cement or equivalent). .. e 09 hn. Verify condition of Velcro on the upper glareshield and right side panel for proper security. Secure as necessary. _ 10 Install the EFB computer (Fujitsu) into the holder bracket. „.. ?am 11 With the EFB mount installed, loosen the thumbscrew knob on the mount assembly % to one full turn maximum (do not allow the lioldlt arm to separate from the mechanical stop pin In the drawing number 1175 mount bracket). 12 With the EFB mount assembly arm loose; verify the co-pilots control column and wheel does not come in contact with the EFB mount assembly using the following procedure: Perform this task by moving the control column full travel forward and aft and rotating the control wheel full left and right while also rotating the EFB mount assembly in all possible configurations. Verify that the EFB mount assembly does not make contact with any part of the control yoke and wheel. If contact does not occur, proceed to step 17 and N/A and initial blocks 13 through 16. Form Completed By: Date: Log Page: F0-10 GMM Revision 1 0912005 EFTA00012037

EFTA00012038

.. ---... nrcria --- WORK COMPLIANCE INSTRUCTIONS Page. Aircraft Number. Station: Work Order # Effectivity 2 of 2 RK-123 and after El Engineering Order Number: M25-10/05-011 OR 0 Fleet Campaign Directive Number: T I TLE Electronic Flight Bag (EFB) Mount Installation Procedures For Flight Options, LLC., Beechjet 400A's Item Work Description Mechanic Inspected 13 If contact occurs, remove the mount assembly 'Hold-It' arm, identified in figure 2 of engineering directive EDW01-5, page 3, by completely removing the thumbscrew. Take note not to lose the wedge shaped bushing located in the eye of the 'Hold-It' ann which supplies the locking feature of the mount assembly. 14 Locate the small Allen type set screws and adjust as necessary to move the arm towards the more vertical position. Make''/. turn adjustments at a time. 15 Reinstall the 'Hold-Ir arm assembly, taking note to install the wedge bushing with the tapered end first into the eye of the arm assembly and tighten the thumbscrew. Caution: Make sure the mechanical stop pin located on the drawing number 1175 mount bracket fits within the machined slot on the inside part of the eye portion of the "Hold-It' arm assembly. 16 Repeat steps 10 through 14 until proper clearance between the control yoke and the EFB is achieved. 17 After the final adjustments are made to the Allen type set adjustment screws, apply a small amount of Loctite 242 to the screw threads to secure from loosening. 18 Resecure the upper glareshleld to the right side panel by reinstalling the mounting screws and resecurinq the Velcro strips. 4 i- 19 Attach the power plug to the EFB computer. .4 20 Install the fabricated '-11' placard as stated in the engineering directive EDW01.5, page 2, to the right cockpit side wan panel just below the side window. 21 Reconnect the main aircraft battery. Secure as necessary. 22 Complete the corrective action side of the Flight Options aircraft maintenance transaction form FO-501 with the fonowing statement: 'Complied with Flight Options EO M25-10/05-011. installation of the Electronic Flight Bag assembly FG3500-400N in accordance with DER approved Engineering Directive EDW01-5, see FM form 8110-3 dated 8- 12-05 and Flight Options Work Compliance InsDuchene. ri." .. ;As,• 23 Complete the accompanying Engineering Directive checklist on page 2 and the previously FM field approved form 337 by completing blocks 6 and 7 in its entirety. When completed, forward one copy of the 337 and the complete Engineering Directive package and Form 8110-3 to the 'Duality Assurance Department in Binghamton. New York and one copy of the FM form 337 and 8110-3 to the local Flight Standards District Office via US mail within two business days after completion of the installation. —END— -- 7414 t, . ili‘C.: t Form Completed By: Date: Log Page: FO-10 OMM Revision 1 09/2005 EFTA00012039

EFTA00012040

0 US Ciepailmant MAJOR REPAIR AND ALTERATION al WardpOrtalion (Airframe, Powerplant, Propeller, or Appliance) Fodor& Aviation Administratinn rovoti Form Aw OMB No. 2120-C020 I U30/2007 E isaron'c 'finking Number or FAA Us* Only INSTRUCTIONS: Print a type di entries See Title 14 CFR §43.9, Part 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U S.C. §44701). Failure to report can result in a civil penalty for each such violation. (49 U.S.C. §46301(a)) 1. Aircraft Nationality and Registration Mark N493LX Serial No. RK-244 Make HAWKER BEECHCRAFT CORP Model BEECHJET Series 400A 2. Owner Name (As shawl on registration certificate) FLIGHT OPTIONS LLC SHMITKA AIR INC SOUTHEASTERN MILLS INC IT AL AddreSS (As shown on registration certificate) Marta Oty Fddwriond itakifits Sale OH rip 14142.1453 County USA 3. For FAA Use Only 4. Type 5. Unit Identification Repair Alteration Unit Make Model Serial No. Er. O AIRFRAME (As described in Item 1 above) 0 POWERPLANT ill III PROPELLER Ill K APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency Mn kkaki O00ons. U.0 U. S. Certificated Mechanic I Manufacturer Aden, 27 Umr 0utr•Stito II Foreign Certificated mermanc C. Certificate No. Cky Mara Stow NY Certificated Repair Station DJFA206D rip 13104 Corny USA PC Cenificaled maintenance Organization D. I certify that the repair and/or alteration made to the unit s) identified in item 5 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Extended range fuel per 14 CFR Part 43 App. B 7. Approva or Return to Service Pursuant to the authority given persons specified below, the unit identified in dem 5 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is Approved EiRejected BY FAA Fit. Standards Inspector Manufacturer X Maintenance Organization Persons Approved by Canadian Department of Transport FAA Designee Repair Station Inspection Authorization Other (Specify) FLIGHT OPTIONS 135 AIR CARRIER CERTIFICATE Certificate or Designation No. DJFA 206D FAA Form 337 poem EFTA00012041

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. B. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark end date work completed.) USA N493LX SN-244 Nationality and Registration Mark 4/11/2011 Date REPAIRED LEFT FUSELAGE SKIN ABOVE PYLON IAW US TECHNICAL EO6110 227227. 8110-3 DATED MARCH 27, 2011. (WORK ORDER # 227277 SQ-208) WEIGHT AND BALANCE NEGLIGIBLE INSTRUCTIONS FOR CONTINUED AIRWORTHINESS: FOLLOW NORMAL MAINTENANCE PRACTICES FOR THE LT AFT FUSELAGE SKIN ASSEMBLY REPAIR AS CALLED OUT IN THE BEECHJET 400A MAINTENANCE MANUAL XXXXXXXXXXXUXXXXX)OOOO(XXXXXXXX)O(XXXXXXXXXXXJOOOOO(XXXXXXXXXXXXXYJCXXXXXX EFTA00012042

0 US OlOattnienl MAJOR REPAIR AND ALTERATION or litany:anew (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation Administration Fenn Approved OW) No. 2120-CO2O itiPlarit7 Searle Tracking Number Fee FAA Unlit* INSTRUCTIONS: Print or bre all fl ies. See Title 14 CFR §43.9. Part 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. §44701). Failure to report can result in a civil penalty for each such violation. (49 U.S.C. §46301(a)) Nationality and Registration Mark N493LX Serial No. RK-244 Make HAWKER BEECHCRAFT CORP Model BEECHJET Series 400A 2. Owner Name (As shown on registration certificate) FLIGHT OPTIONS LLC SHMITKA AIR INC SOUTHEASTERN MILLS INC ET Al Address (As shown on registration certificate) Mani City Itrearnand Heights Stale OH Zip 4042.1453 County USA 3. For FAA Use Only - 4. Type - - 5. Unit Identification • Repair Alteration Unit Make Model Serial No. B e O AIRFRAME (As described in Item 1 above) 0 O POWERPLANT 0 0 PROPELLER 0 O APPLIANCE Type Manufacturer 6. Conformity Statement A Agency's Name and Address B. Kind of Agency Notre Fitoctivent tic U. S. Certificated mechanic I Manufacturer Address 27 SWOOP. Subs Foreign Certificated mechanic C. Certificate No. City Einonsonn SW* NY - Certificated Repair Station DJFA206D Vp 13104 Corny USA Certificated Maintenance Organization D. I certify that the repair and/or alteration made to the unit s) Identified In item 5 above and deserted on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulatio s and that the information furnished herein is true and correct to the best of my knowledge. . . . . Extended range fuel per 14 CFR Part 43 App. B it • 7. Appro for Return to Service Pursuant to the authority given persons specified below, the unit identified in item 5 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is KApproved :7 :Rejected BY FAA Flt. Standards Inspector Manufacturer X • Maintenance Organization Persons Approved by Canadian Department of Transport FAA Designee Repair Station Inspection Authorization Other (Specify) FLIGHT OPTIONS 135 AIR CARRIER CERTIFICATE FAA Form 337 riootR EFTA00012043

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality end registration mark and da e work completed.) USA N493LX SN-244 Nationality and Registration Mark 3/8/2011 Date REPAIRED LEFT ELEVATOR IAW US TECHNICAL EO5770 226648. 8110-3 DATED APRIL 19 2010 (WORK ORDER # 227277 SQ-97) WEIGHT AND BALANCE NEGLIGIBLE INSTRUCTIONS FOR CONTINUED AIRWORTHINESS: FOLLOW NORMAL MAINTENANCE PRACTICES FOR THE ELEVATOR AS CALLED OUT IN THE BEECHJET 400A MAINTENANCE MANUAL XXXXXXXXXXXXXXXXXXXXXXXXXX)0000000(XXXXXXXXXXXXXXW)000000(XXXXXXXXWXX EFTA00012044

el MAJOR REPAIR AND ALTERATION US Coco lfr as-lent ct TransP0nEOP (Airframe, Powerplant, Propeller, or Appliance) Fedora, Aviation Administration Form Approved ore No. 2129.0320 I 1/30r2037 Flectonic Tracking Nome For FAA Use CMly INSTRUCTIONS: Print °inn: all Writs. See Title 14 CFR §43.9, Part 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U S.C. §44701). Failure to report can result in a civil penalty for each such violation. (49 U.S.C. §46301(a)) 1. Aircraft Nationality and Registration Mark N493LX Serial No. RK-244 Make HAWKER BEECHCRAFT CORP Model BEECHJET Series 400A 2. Owner Name (As shown on registration certificate) SHMITKA AIR INC ET-AL SOUTHEASTERN MILLS INC C/0 FLIGHT OPTIONS LW ASCENT I I LW PRIME TIMEASSOCIATES LIC Address (As shown on registration certificate) Addma ca Renmore Hoehn Shoo ON Zip 44142.1451 Country USA 3. For FAA Use Only 4. Type 5. Unit Identification Repair Alteration Unit Make Model Serial No Er • AIRFRAME (As described in Item I above) K • POWERPLANT 0 • PROPELLER El O APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency Name Flirt (Mims. LLC U. S. Certificated Mechanic I Manufacturer Addams 27 Link Din Suite a Foreign Certificated Mechanic C. Certificate No. city a no/WNW Sur NV Certificated Repli‘ Station DJFA206D Zas 13604 Cony uta X Certificated Maintenance Organization D. I certify that the repair and/or alteration made to the unit s) Identified in item 5 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Pan 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Extended range fuel per 14 CFR Part 43 App. B Signature/Date of Authorized IndiVidual /49 "'' I 9 -.26 /e) . pprova r eturn to Service Pursuant to the authority given persons specified below, the unit identif . in item 5 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is Approved —LRejected BY FAA Flt. Standards Inspector Manufacturer X Maintenance Organization Persons Approved by Canadian Department Transport FAA Designee Repair Station Inspection Authorization Other (Specify) FLIGHT OPTIONS 135 AIR CARRIER CERTIFICATE Certificate or Designation No. DJFA 2O6D Si nature/Date of Authorized Individual FAA Form 337(,008) EFTA00012045

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) USA N493LX SN-244 Nationality and Registration Mark 10/19/2010 Date SUBSTITUTED FASTENERS IN H-STAB LOWER SKIN PER EO5938 2272771FAD FROM US TECHNICAL 8110-3 DATED 10/18/2010 WEIGHT AND BALANCE NEGLIGIBLE INSTRUCTIONS FOR CONTINUED AIRWORTHINESS: NORMAL MAINTENANCE PRACTICES FOR THE HORIZONTAL STABILIZER ASSEMBLY AS CALLED OUT IN THE BEECHJET 400A MAINTENANCE MANUAL XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXWXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX EFTA00012046

0 MAJOR REPAIR AND ALTERATION US Department otTrwnocnaton (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation Administration form Approved ORD No. 21204020 2/20/2011 ElettfOtt Tracking lOwnber For FAA Usti0nly INSTRUCTIONS: Print or type all entries. See Title 14 CFR §43.9. Part 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for Instructions and disposition of this form. This report Is required by law (49 U.S.C. §44701). Failure to report can result in a chill penalty for each such violation. (49 U.S.C. §48301(a)) 1. Aircraft Nationality and Registration Mark USA N493LX Serial No. RK - 244 Make RAYTHEON AIRCRAFT COMPANY Model BEECHJET Series 400A 2 Owner . Name (As shown on registration certificate) AIR GHISLAINE INC SOUTHEASTERN MILLS INC ASCENT II LLC Address As shown on : • istration certificate) Address Co RICHMOND HEIGHTS stale OHIO PAP 44143-1453 Canto USA 3. For FAA Use Only 4. Type 5. Unit Identification Repair Alteration Unit Make Model Serial No. III ig AIRFRAME (As descnoed in Item 1 above) . O POWERPLANT In In PROPELLER D Et APPLIANCE Type manufacturer 6. Conformity Statement A Agency's Name and Address B. Kind of Agency Nam Fl IGHT OPTIONS I I C U. S Certificated Mechanic I Manufacturer mew 27 LINK DRIVE SUITE B Foreign Certificated Mechanic C. Certificate No. tab' niNSHAPiATON ewe NY Certificated Repair Sleben DJFA 206 D rs. 13904 Cowry USA / Certificated Maintenance Organization D. I certify that the repair andlor alteration made to the unit(s) Identified in item 5 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the Information furnished herein is true and correct to the best of my knov.ledge. Extended range fuel Signature/Date of Authorized Individual per 14 CFR Part 43 App. B et 0 7. Approval for Return to Service Pursuant to the authority g ten persons specified below, the unit Identified Administrator of the Federal Aviation Administration and is E in item 5 was nspected in the manner prescribed by the Approved D Rejected BY FAA Flt. Standards Inspector Manufacturer 1 Maintenance Organization I Persons Approved by Canadian Department 0 Transport FAA Designee Repair Station Inspection Authorization Other (Specify) Certi icate or Designation No DJFA 206 D Signature/Date of Authorized Individual a-7-)/0 orm 377 .10 55; EFTA00012047

, EFTA00012048

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with ail 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 date work completed.) USA N493LX Nationality and Registration Mark FEB 04 2010 Oate ACCOMPLISHED INSTALLATION OF MAIN LANDING GEAR HEAT SHIELD COVER KIT 128-1002-0001 SERIAL NUMBER 137 AS DESCRIBED IN ENGINEERING ORDER EO M32-10/08.023. ALL WORK ACCOMPLISHED I/ANV HBC MAIN LANDING GEAR HEAT SHIELD COVER KIT 128-1002-0001 SERIAL NUMBER 137 AND ENGINEERING ORDER M32-10/08-023 REV. A DATED 11-13-08. WEIGHT AND BALANCE NEGLIGIBLE. INSTRUCTIONS FOR CONTINUED AIRWORTHINESS: INSPECT THE HEAT SHIELD BLANKETS AND COVERS IIIVW FLIGHT OPTIONS INSPECTION PROGRAM OR THE MANUFACTURES INSPECTION PROGRAM AS APPROPRIATE. END D Additional Sheets Are Attached FAA Form 337 mum EFTA00012049

EFTA00012050

(«TED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE 1 NATIONALITYAND REGISTRATION MAWS 11:4931:: 2 MANUFACTURER AND MCGEE .ty, !"`1':-47 -:err.: '7'. Co. ga; 3 ~CRAFT SERIAL NUMBER 4 CATEGORY Tgre-rnert 6 AUTNORRY MID BASIS FOR ISSUANCE Thlo brontroas retkable hand pinuudbEls fornrrironAd of 1968 old corm est r of be fa of 199Ancr MINN90 broth hard hoe Os Imp~ anl MUM Enna:tom lo Ty bee torkslo ~doh b to In carbon for SO ~Or hoe alin area b mul81. niquIrsenb WIN opplerbo comprobonota and Ward otroptroo4 cor r pro0040 by Ara • b iho Oserflon on Irdonoronal cm AS «CS as ~el barb Escloptiort Hon? 8 TERMS AND CONDITIONS Unkba agnet aunendaried. aulpengeO, molted. Or a twolnation dab O WfrMls inee•••• by the Admlniatrator. INY alreenfleona or!~ aaata4r long at 034 ~Manna maintenance, and snore am pertonned n accorbanba Win Pans 21. 43. and 91 of Po Fodor Aviation Reauttgona, ond M olfcrtalrmrlorocl b M United SUS GATE OF ISSUANCE 10/01/199? FM RE DUE DESIGNATION NUMBER Any Sen. ogeOduCtlan. Or gang he 401~» may ba puNYlYN by • Ina not nogg% 11.000 r Saber ant eg ~gang 3 yearn r toet. THIS CERTIFICATE MUST BE °GRATED N THE ~RIFT IN Arymanobt WITH APPLICABLE FEDERAL AVIATION REGULATIONS MA Fans 81004 (308) uml ED STATES OF ~RICA DEPART MENT OF TRANSPORTATION—FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE I. IMTIDNALITYNIp • OBECOSTRATION MARRS 2 144NUFACTUREA AMR MODEL RAYTHEON AIRCRAFT COMPANY 3 AmicstArr SCRIM. CATEGoar N79STA 400A RK-244 TRANSPORT `5 to' AUTHORITY AND OASIS FOR ISSUANCE orronrnerartralo earl Purina& to Ina Fang& AnatOn Act ot ItiSS IMO Cowles g Maciata Col alumna& Wm • area fa *fin ogre hag son .rtypeaod and hawk] IQ contotre to Me NO* 4:011.1•414 urofoc lo Is In conenon 10f se OINC•140^ and has Ow Won a root IM tIlOv.~1,13 Of ins sortie cornAssAansoye an0 0415380 sonhos coco worry by 41•1•11110 ow Corson on Ingenabonal Crra AnanOn. agog r •04•0 Pina ~MOM NCNE • 6 Trim 5n0 CONORGNS onto moons .1NO 4I•3 01 • usmånaton 0411.4 Olhers.•• egubt.shee by Its Aenianraglet 11u• 0 oink. as kw, do the mentenanCe• 13•••rontam• mantanarc• ono imenorni all 0•00•1141d an ~nip ••••••••••• görg70,71bani cen.scate I.CCOrSDAC•wel•••fll 1 43 analll ot ma agatwarAnabon oproonT goo/psis and In* Won fl196~1.11f138UMN0 Sue • DATE OF ISSUANCE FAA -AESEN ATI ; If DESIGNATION ~ABER K-10/01/99 ACE—FSDC)--07 Ally anambOniagettuchOn. 0t m ,pro or ban. DNS CERTIFICA onATION REGULATIONS cal. may be Prohare tor hooncormara SUM ~soarer not exciorr93 MUST BE DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL 4. Form 81C-2 (ago o U.S 0.100311X19 889438 EFTA00012051

EFTA00012052

SIAM OF MJERICA EISSANTNENT OF THANSPORTATIOK-FEDETIAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE I NATIONALITY NED SEGSPRATION Maki t mAKTFACRIRCA »zo mODEL. RAYTHEON AIRCRAFT COMPANY 3 AnIt.AArt Spun. 1RASER I CATEGORY 11793TA 400A RK-244 TRANSPORT --:. S. ALJTWORITO MAD BASIS ton eatiOCE fM Yn10MNee I GAMIN I Slue Durward To Sa FealotalAYOrer Ap 01 Igi4 ar0 ~Ma riatelliitiflaYo M LIAlstile A stall s ortach GISMO NA tart Inspects, wry lourd by oysters to ma iypb ~La ~tot to a s condiron be NIS 0pefie0n and its boon Sown 10 mops tro ricistatrass W us ityspIsltie cosign/1es~ arel Oculderal ontitnrstall Slob as oroROPO by ~MI Scotto Corwenvon an Ifeanmeponai CM1 ARMS^ tre0Opl ad 'gen ~sin Exonaorts: NONE T EONS AND CONISTioNS Una some: Awrimiend, suwandest rtvekat CI s ternnallan S. Y onletren• altaplOtteO py OIa AdnlnCtnwl. Ste akworah sett Perireitr A fl ats K tenp.n 1M sorsimonsa pesetzlittatt insratranCa. ISO nerehCan re PRONNOO eI accordant* ...SP/JR21.4. t °Ss Fasterantia SST 'Oats as ASOropeate. Rid Se NSW: tY/Cryslonld ARIUS*. SWIM DATE OF LSSIMNde R-10 01/99 ACE-PSI:0-07 Any elltrAbOrt, riPrOdUCIA2/1.O/ mika may to NS Y • SO NA osstrAro SI .000. et+nwneonmemnol excipoiling 3 Pin, Os ADS THIS CEATINCesTE tAVST PE DISPLAYED IN, THE AC/CRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL W1ATION REOyIATIONS. .• . VE DESIGNATION NUMBER -2414~:44, t: ." - * V.B. o.no:tine 889058 • . EFTA00012053

z EFTA00012054

C C-A.A-Xdaa rt- cri-10 ' • e MAJOR REPAIR AND ALTERATION • a a (Airframe, Powerplant, Propeller, or Appliance) Federal Aviadon Administration Forth Approved OMB No. 2120-0020 For FAA Use Only Office Identification „Mk Ch-C4 ' PS00 -23 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Beechcraft Model 400A Serial No. RK-244 Nationality and Registration Mark N793TA 2. owner Name (As shown on registration certificate) NORTH CHANNEL LLC ET-AL Address (As shown on registration certificate) C Fll h ns LLC Richmond Heights H 43-1494 3. For FM Use Only THE TECHNICAL DATA IDENTIFIED HEREIN HAS BEEN FOUND TO COMPLY WITH APPLICAB ftWORTHINESS REQUIREMENTS AND IS HEREBY APPROVED FOR USE ONLY ON THE A @IB A RCRATT, SUBJECT TO litINSPECTION1Y-A-PERSON-IN-14-CFR PART-43:7:-- APPROVING INSPECTOR 3 0 JUN 2004 War OA FcTICI 91 4. Unit Identifies 6. Type Unit Make Model Serial No. Repair Alteration AIRFRAME X (As described in item 1 above) POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. B. Kind of Agency C. Certificate No. x U.S. Certificated Mechanic /O .2 it252 VS' ? 7 7 earjaHauji „ - icturt rz ts, 0" 44143 ond Foreign Certificated Mechanic Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Pan 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date /2- —02 .:9--017 Signature of Authorized Individual ------ tz_____-- 7. Approval for Return To Service Pursuant to the authority given persons specified below the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is X APPROVED 0 REJECTED BY FM Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FM Designee Repair Station Person Approved by Transport Canada Airworthiness Group i i O da , t Alkei to ll il flee Date of Approval or Rejection I,2 98- O11 Certificate or Designation No. CA2006is Sig FM Fenn MT MA% EFTA00012055

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed ) Installed the following equipment In Beechcraft 400A SIN RK-244: Equipment Install Manual Maintenance Manual Pilot's Guide TAWS 8000 (Class B) 009-18001.001 Current Revision N/A 009-18000-001 Current Revision Installed Goodrich Avionics Systems Landmark TAWS8000 system (TSO-C151a Class B) using Flight Options LLC electrical drawing 400-3446-20-01 and applicable manufacturers installation manuals listed above. This installation includes the optional Terrain Display function. FAA Approved Flight Manual SupplernenialoliA4i0iii6ist,oe,thrOci (Cid rithccaft when the Class B TAWS 8000 system is in use: • ' .• ' • The TAWS 8000 system has been previously approved for multiple Beechjet aircraft under STC ST01881CH-D, with the Terrain Display function enabled. This installation has been inspected and found to conform to the operational and technical characteristics of STC ST01881CH-13 with minor deviations in location of switching relays and wiring interface points as depicted on Flight 0plionSiLLC drawing 400-3446-20-01. Similarity to STC ST01881CH-D is the basis for this request for field approval. Using the respective manufacturer's instructions for post-installation ground tests. performed operational checks on all systems. The systems performed to manufacturer's specifications and no interference to existing aircraft systems was noted. In addition to specific instructions contained in the manufacturer's installation manual(s) noted above, all physical mounting considerations were made with reference to AC 43.I3.2A. Chapter I. Chapter 2. Chapter 3, and Chapter II as they apply to this installation. Regarding attachment to additional structure all alterations were inspected to comply with the aircraft manufacturer's structural repair and alteration specifications. In addition to specific instructions contained in the manufacturer's installation manual(s) noted above, wire bundles were fabricated using MIL-SPEC, Teful wire, that meets the acceptability requirements of AC43.13-1B, Chapter I I, Section 7, Paragraph 11-85 (a) and/or (b). paragraph 11.88. and paragraph 11.89. All wiring was masked in accordance with AC43.B-18, Chapter I I, Section 16, Pam. 11.206. 11.207, 11.208 (a) and/or (b) and 11.210 (a) and (b). Individual wires were formed into bundles by lacing and tying using the techniques described in AC43.I3-1B, Chapter II, Section 12, paragraph 11.158 (a) and (b). Cables were routed and secured in the aircraft using AC43.13-18. Chapter I I, Section 8, Para.11-96. (a) through (gg) as a guide. An electrical load analysis was performed per AC43 13-1B Chapter II Section 3 Paragraph 36. The maximum probable continuous electrical load does not exceed 80% of the generator(s) output capacity. All compasses aboard this aircraft were checked for accuracy on completion of this installation. The aircraft equipment list and weight and balance were updated instructions for continued aliworifftness (ICA) for thls aircraft alteration and Interfacing components are as follows; (1) Introththtion to the aircraft altered is explained above. (2) Description of the major alteration is explained above. —(3) —Demotion Information is described In Um doeurrientallstod above for each particular.product ----- (4) servicing, (8) Diagram, and icciii platy. (9) iir Ssrasiess ements, (10) Application of protective treatment') (11) Data, (12) LIM of Special Tools (14) Recommended Overhaul Periods. and (15) Airworthiness limitation section are not applicable. (5) Maintenance, (6) troubleshooting Information (7) Removal and Replacement, and (13) for commuter category alrenift of the products listed, will be IAW the appropriate and current manufacturers Installation manuals. (16) Revision wilt be in accordance with the manufacturers' maintenance manuals and submitted to the local FSDO. Antennas and other parts and materials Installed such as wiring, circuit breakers, switches, annunciators, clamps, doublers, shelves, and racks will be Inspected In conjunction with the Raytheon Sectchjet 400A Phase C Inspection program, for condition, *acuity of attachment evidence of damage, and normal operation IAW FAR 25.1529 and/or applicable manufacturers service instructions n Additional Sheets Are Attached 'U.S GPO 1994-568-012/00019 EFTA00012056

JAN 03 2005. • • MAJOR REPAIR AND ALTERATION 0 , us Dem-wont (Airframe, Powerplant, Propeller, or Appliance) FM.* Avision Mimi*Aram Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification .11-2- 4 C-74 - FS Da —2 3 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix 8, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Beechcraft Model 400A Serial No. RK-244 Nationality and Registration Mark N793TA 2. Owner Name (As shown on registration certificate) NORTH CHANNEL LLC ET-AL Address (As shown on registration certificate) CIO Flight ions LLC Richmond Heights OH 44143-1494 3. For FAA Use Only .._...._ _ 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME described in item X (As t above) POWERPLANT PROPELLER APPLIANCE Type Manufacturer S. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. Lynn H. Huyen c mon a g b 43-14114 X U.S. Certificated Mechanic A8P 278825845 Foreign Certificated Mechanic Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the uniqs identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date /*, -.2 .2- - 0 9/ Signature of Authorized Individual .7_______---- 7. Approval for Return To Service Pursuant Administrator BY to the authority g yen persons specified below the unit identified in item 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and is I213 APPROVED 0 REJECTED FM Rt. Standards Inspector Manufacturer Inspection Authorization Other ( i I ee FM Designee Repair Station Person Appro by Transport Canada invort ness Grou Date of Approval Rejection Certificate or Designation No. S FOAfilan SA NMI EFTA00012057

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Removed existing MK-VI GPWS system in conjunction with installation of new TAWS (EGPWS) system reference FM form 337 dated 12-22-O4. Aircraft weight and balance and equipment list data have been revised. END 0 Additional Sheets Are Attached *U.S.GPO:1994-568-012/00019 EFTA00012058

0 MAJOR REPAIR AND ALTERATION US Copan:nen 0 (Airframe, Powerplant, Propeller, or Appliance) Ffiderol Mutton Aclairattation Form Approved OMB No. 2120-0020 For FAA Use Only Office 0 t5'.--- 7/31.'-- INSTRUCTIONS: Print or type all entries. See FAR 43.9. FAR 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This repod is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed 24.000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make BEECHJET Model 400A Serial No. RK244 Nationality and Registration Mark N793TA 2. Owner Name (As shown on registration certificate) FLIGHTOPTIONS Address As shown on istration certificate) I NO H S.. OHIO 44143 3. For FAA Use On y 4. Unit Identification 6. Type Unit Make ' Model Serial No. Repair Alteration AIRFRAME descnbed in "ern 1 x (As POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Con ormity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. MPLETIONS INC. LEVELANCL HI 4143 U.S. Certificated Mechanic R4GR031Y Foreign Certificated Mechanic X Certificated Repair Station Manufacturer D. I certify that the repair andior alteration made to the units identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date 12-10-2004 f A rized Indiv' ual for Return To Se ce 7. Approval Pursuant Administrator BY to the authority given persons specified•below the unit identified in item 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and is l2; APPROVED O REJECTED FAA FIL Standards Manufacturer Inspection Authorization Other (Specify) RECEIVED FAA Designee X Repair Station Person Approved by Transport Date of Approval 12-10-2004 or Rejection Certificate or Designation No. R4GRO31Y Signature of Authorized Individual DEC 16 2004 ell r atite-- f AA Filar, 317 o,N EFTA00012059

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) AIRCRAFT: BEECHJET 400A N793TA RK-244 FABRICATED AND INSTALLED THE FOLLOWING USING APPROVED DER DRAWINGS SEE FAA FORM 8110-3 DATED 12-08-2004 1) Ft/H Galley 2) a) Assembly drawing #36G-200A006 b) Installation drawing #36G-200F006 There are no additional inspections required for continued airworthiness other than those prescribed by the aircraft manufacturer during regular inspections. END 0 Additional Sheets Are Attached •11.S.GP(11994-568-012/00019 EFTA00012060

0 MAJOR REPAIR AND ALTERATION Form Approved OMB No. 2120-0020 us c.vikvvnevii a For FAA Use Only (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation Administration _I Q OffArAliFS no INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent 1 2 3 thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result . it penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make RAYTHEON Model 400A Serial No. RK-244 Nationality and Registration Mark USA N793TA . 2 Owner Name (As shown on registration certificate) SAMAIR INC ET-AL Address (As shown on registration certificate) WICHITA, KS 67207 3. For FAA Use Only THE TECHN CAL DATA REQUIREMENTS AND TO CONFOR ITY INSPECTION -2-S103 IDENTIFIED HEREIN HAS BEEN FOUND TO COMPLY WITH APPLICABL NYORTHtNESS IS HEREBY APPROVED FOR USE ONLY ON TH BY A PERSON IN 14 CFR PART 43.7. APPROVING INSPECTOR BJECT DATE K.°1 AEA FSDO 23 4. Unit Identificall ype Unit Make Model Serial No. Repair Alteration AIRFRAME item (As described in 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. STEPHEN J. MAIDEN C/O FLIGHT OPTIONS LLC RICHMOND HEIGHTS, OH 44143 X U.S. Certificated Mechanic A 297605039 Foreign Certificated Mechanic Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requi ements of Part 43 of the U.S. Federal Aviation Regulations and Mat the information furnished herein is true and correct to the best of m knowledge. Date JUNE 10, 2003 7. Approval for Ret n To ice Pursuant to the authority given persons specified below the unit identified in m 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is jn APPROVED 0 REJECTED FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) OPTIONS FLIGHT SUPPORT, INC., dibia FLIGHT OPTIONS BY FAA Designee Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection JUNE 10, 2003 Certificate or Designation No. DJFA206D KEITH GAWSYSZAWSKI FM Form 31? mig EFTA00012061

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatiblewitlzall previous alterations to assure continued conformity with the applicable ainvorthiness requirements. 8 Description'9trork Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) INSTALLED ROCKWELL COLLINS, INC., SUPPLEMENTAL TYPE CERTIFICATE #ST00881WI-D, MODIFICATION OF COLLINS TCAS II SYSTEM INSTALLATION WITH COLLINS TTR-920 CHANGE 6.04a RECEIVER TRANSMITTER TO A COLLINS TCAS II SYSTEM INSTALLATION WITH COLLINS TTR-920 CHANGE 7 TCAS II RECEIVER TRANSMITTER IN ACCORDANCE WITH COLLINS INSTALLATION INSTRUCTIONS AS LISTED ON AML tt ST00881WI-D. AIRCRAFT FLIGHT MANUAL SUPPLEMENT INSERTED INTO AIRCRAFT FLIGHT MANUAL. NO CHANGE TO WEIGHT AND BALANCE. O Additional Sheets Are Attached *U.S.GPO:1994-568-012/CO019 EFTA00012062

1 3 JUN 2003 O MAJOR REPAIR AND ALTERATION US Department rd (Airframe, Powerplant, Propeller, or Appliance) Falderal Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification :31-f— stiCAgrESIX) can result 23111 penalty not INSTRUCTIONS: Print or type all entries. See FAR 43.9. FAR 43 Appendix instructions and disposition of this form. This report is required by law (49 U.S.C. to exceed $1 ,000 for each such violation (Section 901 Federal Aviation Act of B. and AC 43.9-1 (or 1421). Failure to report 1958). 1. Aircraft Make RAYTHEON Model 400A Serial No. RK-244 Nationality and Registration Mark USA N793TA 2. Owner Name (As shown on registration certificate) SAMAIR INC ET-AL Address (As shown on registration certificate) WICHITA, KS 67207 3. For FAA Use On y 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME described in X (As item 1 above) POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. Stephen J. Maiden C/O FLIGHT OPTIONS LLC RICHMOND HEIGHTS, OH 44143 X U.S. Certificated Mechanic A297605039 Foreign Certificated Mechanic Certificated Repair Station Manufacturer ' ' D. I certify hereto information that the repair and/or have been made furnished herein 10 June, 03 alteration made to the unit(s) identified in item in accordance with the requ' is true arid correct to t 7. 4 above and described on the reverse or attachments Date Pursuant Administrator BY Date fu to the authority g ven persons specified below, the unit identified of the Federal Aviation Administration and is X) APPROVED in it 4 was inspected in the manner prescribed by the O REJECTED FAA Flt. Standards FAA Designee or Rejection to too Manufacturer Repair Station Certificate or Designation No. DJFA206D Inspection Authorization Inspector AIR AGENCY CERTIFICATE Person Approved by Canada Airworthiness Transport Grow Other (Specify) FLIGHT OPTIONS LLC of Approval tad FM ?cal 33? IOW EFTA00012063

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. a -9 rict i; 8. Destflpli of Work Aecomplished (If more spacriseequired, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) INSTALLED ROCKWELL COLLINS, INC., SUPPLEMENTAL TYPE CERTIFICATE #ST00881WI-D, MODIFICATION OF COLLINS TCAS II SYSTEM INSTALLATION WITH COLLINS TTR-920 CHANGE 6.04a RECEIVER TRANSMITTER TO A COLLINS TCAS II SYSTEM INSTALLATION WITH COLLINS TTR-920 CHANGE 7 TCAS II RECEIVER TRANSMITTER IN ACCORDANCE WITH COLLINS INSTALLATION INSTRUCTIONS AS LISTED ON AML # ST00881WI-D. AIRCRAFT FLIGHT MANUAL SUPPLEMENT INSERTED INTO AIRCRAFT FLIGHT MANUAL. NO CHANGE TO WEIGHT AND BALANCE. END 0 Additional Sheets Are Attached *U.S.GPO:1994-568-012/00019 EFTA00012064

r Satiltbinalto of Amnia Pepartment of transportation — Aebtral tAbintion Abministralints $upplemental Jgpe Tertifirate ../14;9a 0./e ST00881 IN I. D .ffa trinVeale. t;hoowlie Rockwell Collins, Inc. 400 Collins Road NE, MS 164.100 Cedar Rapids, IA 52498 rerlOns arc/46 refer res a, r/rwirrsirfc 46Arreverionoarekne en 46 Snarteivra orairavnAiievpo derOr a.; bynee.Aftherevr nonAs t neivreedionmaree:vwennia Val • erst.4:: • derpottr/tivar. niaseetliteduce Vienckdres 1:24”4.- • •See attached FAA Approved Model List (AML) • No. ST0088IWI-D for list of approved airplane models and applicable airworthiness regulations. Sive.soraiv. rtf4r: Modification of Collins TCAS 11 or TCAS 94 (TCAS II) system installation with Collins TTR-920 Change 6.04a Receiver Transmitter to a Collins TCAS II or TCAS 94 (TCAS II) system installation with Collins TTR-920 or Collins 17R-921 or Cellists TTR-4000 Change 7.0 TCAS 11 Receiver Transmitter and optional TPR-901 in accordance with Collins Installation Instructions as listed on AML No. ST0088IWID, Revision -, or later FAA approved revisions. 5Saoardshei ( 0 Approval of this change in type design applies to the above model aircraft only. (2) Compatibility of this design change with previously approved modifications must be determined by the installer. (3) A copy of this Certificate and FAA Approved Model List (AML) No. ST00881WI-D issued June 30, 2000, or later FAA approved revision, must be maintained as pan of the permanent records for the modified aircraft. (4) Prior installation and approval of a Collins TTR-920 Change 6.04a Receiver Transmitter is a prerequisite to this STC. (5) If the holder agrees to permit another person lo use this certificate to alter the product, the holder shall give the other person written evidence of that pennission. .974, sada. .isenvevt&to ar/er rey(ori U Lf. ho.h‘l At, evreresiafattesentetU es 10e/ sena atenstAnet Jet.irina neater' Pe a AryesentieniVi Ate 0.l esCinvtvde nrferAitastafr ,,,Z1Lreereateer/re Vide !Rea- .1/4 ,-vtetwain . June 29, 2000 !Alt e/ti.i.tuageo June 30, 2000 firor:• trtwr«l. fere.o syno-sated. July 14, 2000, December I, 2000 11111111- Administrator, DAS-500864-CE My •iteronon of tai. tertifiCott le penialible by • tine of sot exteallO9 $1.000. Or Oar @Omen, aet OflteillIsfr J rears. Or boa. TOD Noy be into rrrrr to error et wf t0 PM 73.• . IAA r0t. $110-2110-44) Via I EFTA00012065

1 EFTA00012066

Avionics Cerblicalkan Center Rockwell Collins May 14, 2003 WO030737.DOC Fli ht O lions Cleveland, OH 44143 Tel: (216) 797-3500 Attention: Mr. Jody Kremsreiter/ Mr. Richard Fine (Collins on-site) Subject: STC ST00881WI-D Modification of Collins TCAS II System Installation with Collins TTR-920 Change 6.04a Receiver Transmitter and TPR-900 Mode S to a Collins TCAS II System Installation with Collins TTR-920, Collins TTR-921 or Collins TTR-4000 Change 7.0 TCAS II Receiver Transmitter and optional TPR-901 in Part 25 Aircraft Dear Mr. Kremsreiter: Enclosed is a compact disk with one copy each of the following FAA approved STC data: 1. STC ST00881WI-D Certificate, dated December 1, 2000. 2. FAA Approved Model List (AML) Number ST00881WI-D, amended April 15, 2003. 3. Drawing Index 992-4358-001. Revision M. 4. One copy of each drawing listed on Drawing Index 992-4358-001. 5. Airplane Flight Manual Supplement, ACC-00-105, Revision -. This letter is our authorization for Flight Options to use this STC as basis for the installation of our equipment in our at lanes based on the following model and serial numbers provided by Mr. of Rockwell Collins. EFTA00012067

'1 EFTA00012068