1 Aviation Fabricators Inc. 806 North Fourth Street Clinton, MO. 64735 SEAT BACK ASSEMBLY SEAT sonom ASSEMBLY ON CUSIECN A.A-CEMMI. Y REFFEChCF AM MOM Figure 1.0D FOAM ICA Document No.: AF•528 Revision (IR) Date: November 21, 2011 KOJI VELCRO NOOK VE11010 1.000 Page 8 of 16 SDNY_GM_02755203 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0(1242125 EFTA01327243

Aviation Fabricators Inc. 805 North Fourth Street Clinton, MO. 84736 ICA Document No.: AF-528 Revision (IR) Dale: November 21, 2011 2.0 INSPECTION REQUIREMENTS AND OVERHAUL SCHEDULE 1. To comply with14 CFR 25.1529, continue the new divan assembly (with restraint system) on the same inspection and maintenance schedule used per the Hawker Beechcraft Maintenance Manual for cabin section inspections. a. The new cabin configuration components require no service other than inspection at normal inspection interval of 200 hours. b. The safety belts require no service other than inspection at normal inspection interval of every 200 hours. c. Perform a detailed visual inspection of each passenger seat bottom and back cushions and covering of all cabin interior components to detect apparent or obvious defects or irregularities. On the cushion assembly, check for cracks and punctures within a 4' diameter circle. The cushion assembly can have no more than three defects found within the 4" diameter circle. If a cushion develops a "lump", check to see if there are no more than two lumps within a 4" diameter circle. Any damage to the cushions outside of the described limits will require them to be replaced. Visually inspect the covering assemblies for holes, punctures, and tears. If the damage to the covering is holes smaller than 1/2" in diameter or a cut at a maximum of 2" in length then the covering is satisfactory. The sewing of the cover assemblies is not to exceed 1" tearing. Any damage to the covering assemblies outside of the described limits will require them to be replaced. d. Visually inspect the divan and seat assembly tubes and diaphragm for cracks and deformation. Damaged conditions could be detected as a crack at the edge of the tube or along the length of the tubes or as a crack, tear or cut found on the seat bottom or back diaphragm. Visually inspect all hardware for excessive wear before and after installation. Replace the seat back and bottom diaphragm if two cracks or deformations are found with a 4" diameter circle. If a tear or cut is found with a maximum of 6", replace the diaphragm. There shall be no broken tubes. There shall be no sharp corners, edges, or protrusions that may Injure passengers. Replace the tubes if they are bent in such a way that they are more than r off center. Replace the seat tubes if crack length is found to be .125" or greater. Replace the tube if a dent Is found running longer than 3". Replace the seat tubes if deformation is greater than .25" the overall thickness of the tube diameter. Cracked or broken fasteners or fittings are to be replaced with new immediately. Page 9 of 16 SDNY_GM_02755204 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242126 EFTA01327244

Aviation Fabricators Inc. 806 North Fourth Street Clinton, MO. 64736 ICA Document No.: AF-528 Revision (IR) Date: November 21, 2011 For repair or replacement of damaged or broken parts or assemblies contact Aviation Fabricators Inc. 2. Inspection Time Limit for the cabin configuration Installations: 200 +1- hour inspection for the new cabin configuration components Task Code Schedule Date Mech Insp AFI-100 a. Inspect for damage to upholstery. AFI-101 b. Inspect safety belts for wear, cuts, fraying, damage, and deterioration. AFI-102 c. Inspect safety belt attachment fittings for wear and damage AFI-103 d. Inspect foot fittings for damage, security, and function. AFI-104 e. Inspect seat frame for damage, and corrosion. AFI-105 f. Inspect overall seat for fit and function. A. The new divan assembly and restraint system are on the same inspection and maintenance schedule used per the Hawker Beechcraft Maintenance Manual for passenger seats. Page 10 of 15 SDNY_GM_02755205 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242127 EFTA01327245

Aviation Fabricators Inc. 805 North Fourth Street Clinton, MO. 64735 3.0 DIMENSION AND ACCESS: ICA Document No.: AF-528 Revision (IR) Date: November 21, 2011 The installation of this cabin configuration does not change the dimensions of the aircraft or alter the access to any existing aircraft system. 4.0 LIFTING AND SHORING No change. 5.0 LEVELING AND WEIGHING Divan Maximum Allowable Seat Weight = 80 lbs w/ Seat Bottom Upholstery Base Weight of Divan Assembly w/ Restraint System = 50 lbs (includes empty drawer weight) 6.0 TOWING AND TAXIING No change. 7.0 PARKING AND MOORING No change. Page 11 of 16 SDNY_GM_02755206 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242128 EFTA01327246

Aviation Fabricators Inc. 806 North Fourth Street Clinton, MO. 64735 ICA Document No.: AF-528 Revision (IR) Dale: November 21, 2011 For repair or replacement of damaged or broken parts or assemblies contact Aviation Fabricators Inc. 2. Inspection Time Limit for the cabin configuration Installations: 200 +1- hour inspection for the new cabin configuration components Task Code Schedule Date Mech Insp AFI-100 a. Inspect for damage to upholstery. AFI-101 b. Inspect safety belts for wear, cuts, fraying, damage, and deterioration. AFI-102 c. Inspect safety belt attachment fittings for wear and damage AFI-103 d. Inspect foot fittings for damage, security, and function. AFI-104 e. Inspect seat frame for damage, and corrosion. AFI-105 f. Inspect overall seat for fit and function. A. The new divan assembly and restraint system are on the same inspection and maintenance schedule used per the Hawker Beechcraft Maintenance Manual for passenger seats. Page 10 of 16 SDNY_GM_02755207 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I 29 EFTA01327247

Aviation Fabricators Inc. 805 North Fourth Street Clinton, MO. 84735 3.0 DIMENSION AND ACCESS: ICA Document No.: AF-528 Revision (IR) Date: November 21, 2011 The installation of this cabin configuration does not change the dimensions of the aircraft or alter the access to any existing aircraft system. 4.0 LIFTING AND SHORING No change. 5.0 LEVELING AND WEIGHING Divan Maximum Allowable Seat Weight = 80 lbs w/ Seat Bottom Upholstery Base Weight of Divan Assembly w/ Restraint System = 50 lbs (includes empty drawer weight) 6.0 TOWING AND TAXIING No change. 7.0 PARKING AND MOORING No change. 1 Page 11 of 16 SDNY_GM_02755208 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I 30 EFTA01327248

Aviation Fabricators Inc. 805 North Fourth Street Clinton, MO. 64735 8.0 PLACARDS AND MARKINGS ICA Document No.: AF-528 Revision (IR) Date: November 21, 2011 Three (3) placards are required in conjunction with this modification: 1. The divan Installation requires placard part numbers 15-0288 and 32-0377-20 to be installed in plain view of the seat occupants on the forward divider. LIE VEST LOCATED IN WILIER SEAT COWARTLIEM PR4 15-0288 FASTEN SEATBELT MD SHOULDER FARNESS FOR TAXI. TMEOFF ONO LMDINO PIN 32-0377-20 Figure 8.0A 2. A placard stating "to install harness over seat occupant's fwd shoulder is sewn on to restraint system part numbers 3088-7-061-2396 and should be legible and easily viewed by the seat occupant. Figure 8.0B Page 12 of 15 SDNY_GM_O27552O9 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I 31 EFTA01327249

Aviation Fabricators Inc. 805 North Fourth Street Clinton, MO. 64735 9.0 SERVICE INFORMATION Typical Passenger Seating Service Instructions: A. Upholstery Cleaning: Service Instructions ICA Document No.: AF-528 Revision (IR) Date: November 21, 2011 1. Remove seat back and seat bottom cushion assemblies from the interior seating components. 2. Clean the cushions in accordance with instructions issued by the company responsible for the upholstery covering so that knowledge of the upholstery material's fire retardant properties are known and will not be compromised. 3. Clean and inspect restraint system for damage, fraying, cuts or seam deterioration. 4. Inspect all attachment fittings and replace if necessary. 5. Inspect overall interior component for fit and function. Typical Maintenance Instructions: Divan Assembly The divans are self contained complete assemblies that mount to the existing aircraft cabin seat track using standard fittings in accordance with approved floor plans. Refer to Figure 1.0A. Divan Installation Installation of the divan requires aligned the feet on the existing seat track and _attaching the divan legs using standard hardware. Refer to Installation Instruction drawing D-10666 for complete installation details and hardware part numbers. Divan Removal Removal of the divan requires loosening the attaching hardware and lifting the divan from its location on the seat track. The feet will be slid forward or aft to the end of the seat track or a gap in the track for their removal. Cushions Seat back and seat bottom cushion assemblies are removed by simply pulling the cushion inboard away from the Velcro on the sidewall or up away from the Velcro on the pan of the divan assembly, respectively. All covering and upholstery materials must comply with 14 CFR 25.853 as stated on the Finish Materials Listing AF-476. The cushion design and layout were determined & manufactured by the seat installer to match the design of the cabin interior in the aircraft. Refer to Figure 1.0D for Cushion Assembly Reference for basic assemblies. Page 13 of 16 SDNY_GM_02755210 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I 32 EFTA01327250

Aviation Fabricators Inc. 806 North Fourth Street Clinton, MO. 84735 8.0 PLACARDS AND MARKINGS ICA Document No.: AF-528 Revision (IR) Date: November 21, 2011 Three (3) placards are required in conjunction with this modification: 1. The divan installation requires placard part numbers 15-0288 and 32-0377-20 to be installed in plain view of the seat occupants on the forward divider. LIFE VEST LOCATED IN UNDER SEAT COMPARTMENT PM 164208 FASTEN SEATDELTAND SHOULDER HARNESS FOR TAXI. TAKEOFF AND LANDING PM 32-037740 Figure 8.0A 2. A placard stating "to install harness over seat occupant's fwd shoulder" is sewn on to restraint system part numbers 3088-7-061-2396 and should be legible and easily viewed by the seat occupant. Figure 8.0B Page 12 of 16 SDNY_GM_02755211 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 133 EFTA01327251

1 Aviation Fabricators Inc. 805 North Fourth Street Clinton, MO. 64736 9.0 SERVICE INFORMATION Typical Passenger Seating Service Instructions: A. Upholstery Cleaning: Service Instructions ICA Document No.: AF-528 Revision (IR) Date: November 21, 2011 1. Remove seat back and seat bottom cushion assemblies from the Interior seating components. 2. Clean the cushions in accordance with instructions issued by the company responsible for the upholstery covering so that knowledge of the upholstery material's fire retardant properties are known and will not be compromised. 3. Olean and inspect restraint system for damage, fraying, cuts or seam deterioration. 4. Inspect all attachment fittings and replace if necessary. 5. Inspect overall interior component for fit and function. Typical Maintenance Instructions: Divan Assembly The divans are self contained complete assemblies that mount to the existing aircraft cabin seat track using standard fittings in accordance with approved floor plans. Refer to Figure 1.0A. Divan Installation Installation of the divan requires aligned the feet on the existing seat track and ,attaching the divan legs using standard hardware. Refer to Installation Instruction drawing DA 0666 for complete installation details and hardware part numbers. Divan Removal Removal of the divan requires loosening the attaching hardware and lifting the divan from its location on the seat track. The feet will be slid forward or aft to the end of the seat track or a gap in the track for their removal. Cushions Seat back and seat bottom cushion assemblies are removed by simply pulling the cushion inboard away from the Velcro on the sidewall or up away from the Velcro on the pan of the divan assembly, respectively. All covering and upholstery materials must comply with 14 CFR 25.853 as stated on the Finish Materials Listing AF-476. The cushion design and layout were determined & manufactured by the seat installer to match the design of the cabin interior in the aircraft. Refer to Figure 1.0D for Cushion Assembly Reference for basic assemblies. Page 13 of 15 SDNY_GM_02755212 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242134 EFTA01327252

Aviation Fabricators Inc. 805 North Fourth Street Clinton, MO. 84735 ICA Document No.: AF-528 Revision (IR) Date: November 21, 2011 Inertia Reel Inertia reel removal is accomplished by loosening attaching hardware and removing from the divan frame bracket. Refer to Installation Instruction drawing D-10668 for complete installation details and hardware part numbers. Refer to Figure 1.0B. Seat Belt Seat belt and removal is accomplished by loosening attaching hardware and removing from the existing aircraft seat track. Refer to Installation Instruction drawing D-10666 for complete installation details and hardware part numbers. Refer to Figure 1.0C. B. RECOMMENDED OVERHAUL PERIODS No additional overhaul time limitations and requirements apply to the Aviation Fabricators' interior cabin configuration. Page 14 of 16 SDNY_GM_02755213 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242135 EFTA01327253

Aviation Fabricators Inc. 805 North Fourth Street Clinton, MO. 64735 10.0 AIRWORTHINESS LIMITATIONS ICA Document No.: AF 528 Revision (IR) Date: November 21, 2011 The Airworthiness Limitations section is FAA approved and specifies maintenance required under Sec. 43.16 and 91.403 of the Federal Aviation Regulations unless an alternative program has been FM approved. There are no new (or additional) Airworthiness Limitations associated with this equipment and /or installation. 11.0 TROUBLESHOOTING INFORMATION Refer to the existing Aircraft Maintenance Manual for troubleshooting the 3 place divan installation that is required beyond the information found on the installation drawing D-10666. For replacement parts or repair of damage parts: Contact Aviation Fabricators at (660) 885-8317. Troubleshooting this installation should only be accomplished by FM approved repair stations with the appropriate ratings or appropriately rated operator/individuals, with required test equipment and service data. Page 16 of 16 SDNY_GM_02755214 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242136 EFTA01327254

Aviation Fabricators Inc. 806 North Fourth Street Clinton, MO. 84736 ICA Document No.: AF-528 Revision (IR) Date: November 21, 2011 Inertia Reel Inertia reel removal is accomplished by loosening attaching hardware and removing from the divan frame bracket. Refer to Installation Instruction drawing D-10666 for complete installation details and hardware part numbers. Refer to Figure 1.0B. Seat Belt Seat belt and removal is accomplished by loosening attaching hardware and removing from the existing aircraft seat track. Refer to Installation Instruction drawing D-10666 for complete installation details and hardware part numbers. Refer to Figure 1.0C. B. RECOMMENDED OVERHAUL PERIODS No additional overhaul time limitations and requirements apply to the Aviation Fabricators' interior cabin configuration. Page 14 of 15 SDNY_GM_02755215 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242137 EFTA01327255

Aviation Fabricators Inc. 806 North Fourth Street Clinton, MO. 64735 10.0 AIRWORTHINESS LIMITATIONS ICA Document No.: AF-528 Revision (IR) Date: November 21, 2011 The Airworthiness Limitations section is FM approved and specifies maintenance required under Sec. 43.16 and 91.403 of the Federal Aviation Regulations unless an alternative program has been FM approved. There are no new (or additional) Airworthiness Limitations associated with this equipment and /or installation. 11.0 TROUBLESHOOTING INFORMATION Refer to the existing Aircraft Maintenance Manual for troubleshooting the 3 place divan installation that is required beyond the information found on the installation drawing D-10666. For replacement parts or repair of damage parts: Contact Aviation Fabricators at (660) 885-8317. Troubleshooting this installation should only be accomplished by FM approved repair stations with the appropriate ratings or appropriately rated operator/individuals, with required test equipment and service data. Page:M*116 SDNY_GM_02755216 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242138 EFTA01327256

U. S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS 1.DATE 5/02/2013 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2.MAKE Raytheon 3.MODEL NO. 400A AT Y PE(ALVano. EnstAv. Propthr. OA) Airplane 5.NAME OF APPLICANT Constant Aviation-CLM LIST OF DATA BIDENTIFICATION ?TITLE TP 22681 Rev A Dated 05/02/2013 . Skandia, Inc. Flammability Test Report Oil Burner Testing and Vertical Burner Testing Notes: 1) Work accomplished under Skandia Inc. WO # 254987-13, Ref Document ID 93685. 2) Flammability test witnessing only, does not constitute installation approval of the materials. 8.PURPOSE OF DATA Demonstration of compliance with material flammability requirements for S/N RK-244 9.APPLICASLE REOUIREMENTS(Llst specific sections) 14 CFR Pert 25.853 (a) Arndt 25-116 Appendix F Part I (a)(1)(ii) 14 CFR Part 25.853 (c) Amendment 25-116 Appendix F Part II 10.CERTIFICATION - Under authority vested by direction of the Administrator of appointment under 14 CFR Pan 183, data listed above and on attached examined in accordance with established procedures and found to comply Standards listed. C I ( Therefore Recommend approval of these data `*Approve these data and in accordance with conditions and limitations sheets numbered have been with applicable requirements of the Airworthiness 11.SIGNATUREIS) OF DESIGNATED ENGINEERING REPRESENTATIVE 12.DESIGNATION NUMBERS) 13.CLASSIFCATIONIS) e sc., ) V., ‘. X3 IC _O 5 tA r L .) Jane Bib tein -FAA DER DERY-832780-CE Structural Special FAA Forrt1 8110-3 (03/10) SUPERSEDES PREVIOUS EDITION SDNY_GM_02755217 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242139 EFTA01327257

SDNY_GM_02755218 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242140 EFTA01327258

FAA FORM 8130 - 6, APPLICATION FOR U.S. AIRWORTHINESS CERTIFICATE FORD ApptOvold O Mil No 21204318 Es ion Dale 02/2N2011 CI APPLICATION US 0404rvre4 N Federal Aviation AdMIAISAI FOR U.S.AIRWORTHINESS CERTIFICATE 000 •ISTRUCTIONS • PAM ar bp. Oo not Res In IMMO mat MM. ARM FM ......«..y. 360.6t ospeol airy la an whorttad FAA Ftfdateabwo 1462ftea 10621is requied. RR Olalmellt For *RR NM Oa 06164016 Smkans R V. end VII in *opiate z t: 0 I REGISTRATION NARK N493LX I AIRCRAFT SIALCERS RAW Awo Raytheon Aircraft Co 3 AIRCRAFT YODEL OCSOANTO4 400A 4 YR. YFR. 1999 MACOONO ua 0 5 ARCRAFT SERIAL NO. RK244 6 FIORE EMIZERS item mum Williams International T. BONE IMPEL DESIGNATION FJ44-3AP li 4 /410301 OF MODES 2 4 PROPELLER WADERS WAIF Rem N/A *PROPELLER 'MEL DESIGNATION 11 AIRCRAFT IS Mae mossy N/A I IMPORT APROCATOON IS NEARBY WOE FOR Meth mimeo ea) I A I STANDARD AIFMORDMIESS CERTIRCATE Ras mem I Ism I Iowa I la:SIC i I Moira° I I Orsiont I Ira. I I.' B 1 SPEW/ MPACRINNESS CERTIFICATE Mr mamba ownl PRIMITY I LIGNTRPORT more I I SI ' PeReFRRIM. I I WaifseR•Consis I I GRAM l ila...rile% Mr 2 OWED $ 1311(M9PO4. I CLASS; ram Real 3 PASSE C I AGMOULTURE NC PEST MORO. 2 ADIbu.SURvEr 3 MIMI ADVERTISING 3 nem FOOTED zees sere emsamemi 4 FOREST mum mmaam/ PATROLLED I REAMER COMO. i 0 OMNI MIMI 1 1 RESEARCH ANO DEVELOPMENT 2 AMATEUR MALT 3 FJOISTION 4 RACING AR RAC S CREW RIMING 6 MAR KET Sucwv 0 TO S/CMCCOAPLANCE WM THE CPR ° PkiRAIW3 fslarcayht NT WIT AIRCRAFT i I EXPERRIEVTAL EA foam ornate./ In arscatois craw* ll Onol melt 6 Mt 4 vece.m.evral remtveaM 6 COERATING fie OFRAR634/0165pcillOMAI S tr UORT.SPCRT SC Otal6T64361606 0,96o66 *tug steetilatiori wary aOsannots aselkaleunly 4 21.193 9 LIFIRANNED 91. asscuicrisziocevitozsein I SC 1 Icetwrrisimiza AftCRAFT te MARKET SURVEY 1 FERRY RIGHT FOR REPAIRS. ALTERATIONS. MMENAICE OR STORAGE SPEOAL FOCHT PERMIT mma 2 EVACUATE FROM AREA Of IMPENCINGOANGER 0 WOO, NI il•CO.A•St Fen sin* Saw Ng ve..graiwnet• oh. 3 OPERATION IN EXCESS OF MAXIMO CERTIFCATECITAKE.OFF REMIT 4 04LIWRING OR EXPORTING I S I I PACOUCTO. FLOM MTIRO I CUSTCMER 001ONSTRATICSIFUOIRS CI a mut.11PEE AftwORTtEMESS CERTIFICATE taw MOW 'Aiwa/ °tease ',Wined. . 1.~.. *0MM A REGISTERED OMER ve man Reams vennemsomi IF DEALER, CHECK HERE I Nat Fligh Options.LLC Fight Options LLC ACORESS 26180 Curtis Wright Parkway, Richmond Heights .OH 44143 0 AIRCRAFT CERTRICATON BASS MIR mem. wee ensamem me emeees4 NRCRAFT SPEOCICATION OR TYPE CERTIFICATE OATA SHEET awn& we Amen WI Nth i AIRWORTIGNESS mecum nr,..........annonnene................ eletaino arstbitar ^ow.... I. woo, as at awnsimiestay Oro w s Bi-Weeky 2013-09, 04/22/2013 - 05/05/2013 ft MICPAFT USTRIG (Own emet6/ N/A SLIPPLEVENTAL TYPE CERTIFICATE me ameetem VC Risme N/A C AIRCRAFT OPERATICRANOW.INTEMACE RECORDS i CHEOC IF WORN IN COUPLIAACE WTI4 I4 CFR Nctcolil 41T I TOTAL AIRMAVE NOIRES 8563.80 3 .'.Lame outtramemm.OrtYeafr...frneolowankoliwie a DGERTVICADCA - IWO'', ore" tal I am Me NORROOd [WM /ORS song oi re brain onabsO to. . OW Fe latCOSIIS wordem no Me 49 ce to ORM a Cod. 44631 is RN &FRIO,* riars Mtn Regano-A to nt re tosomross cecinas nested 0000111ad .an PS rISSE AWICA A010/10116.11 in Sash hos wIn L> awcaly ODOM bre DATE OF APPLICARCN 05/13/2013 NAME AND11TLE Memo./ ire Senior A.Ockwell I sorrotare k... A. TIE AIRCRAFT CESCRISEOABOVE NOS MN INSPECTEOMO cotta NR Oft BY mason. ass At cni eat as c§ 3 TA CFR OM 121 CIIIMICATI HCACERNA• cawasmo 3 CERTIFICA VW NEOIANC My Denim W1 6 a I CUMACATECIREPAR sumer oz. cziruiz wr 5 I I a I MRCRAFT ROMACTUREN 04 nem AM • z GTE i MU SKIMTUTE 031400446.0.M.004•444 Rea THE MUSCATS REOUESTED PI I It I MORN We Mot 0444.04d in Omen I as./ mats tapierneas Icy 1 AJAENIMOIT CR mCOFCATCet Cf CURRENT MOMIRMNESS CERTIFICATE i i t ImMOTaRm40404IRSIN Rem twee MUM Vel MIS COMPIOdd by, FAA NSFECTOR F AA CESIGsEE CERTIFICATE IC.OER l•CER id CFR an 6$ I IN CYR pen iIi OR Mi lli CFR pe 145 DATE II "WA* 1.306 300 Cf FOCI et-Cf ' FAA PECTORS a SIGNAT INS VRE AND 7.: 9 ita 7: &Meth DAVa tiliggi-CE , FAA INSPECTORS V CERTIFICATON ROSE 1) ATLI CE • at., Le It FM Form 41304 )Nn)AF Provan &Won SUPOOSO011:1 Pius felt SDNY_GM_02755219 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 Q D O 0 EFTA 00242141 EFTA01327259

SDNY_GM_02755220 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I 42 EFTA01327260

u 0 IF : A MANLIFACTURER *MME I ACMES 8 PROOLICliON SASS EaMeA 41/COSII SR PROP/CM/I CERTIFICATE MO PROMPT004/010 AVOW .... TYPE CERTIMCATE I I OTHER G GivE QUANTITY CC CERTIFICATES MOUND FOR OPERATOIG NEEDS OATS OF APOWATION I RIME NO TYRE (PAW w no* 9GHATuRE VD SPECIAL WONT PUNT PURPOSES °MERMAN PRODUCTION WONT TEST A CESCRPTDON OF ARCRAFT Re34TEREO OMER ACORES) GUIDER 8 MODEL SERIAL MATER REGISTRATION MN% II. CESCRIPTCH CF FLKIHT CIAITCMER COOMTRATION FLKINT5 CI ECHO NarplicoN) /RCM TO viA WARTURE DATE I OVATION C. CREW REO(SED TO CPERATE THE NRCRAFT MO ITS IOUNIMENT I 1 PILOT i I COALOT I 1 MGM MINIM I I OTHER (SOK* 0. TWAIN:RAFT OM NOT MEET TIE APPUCASLE AIRY/OMANI= ItIOUREUENTS AS FOUON3 E THE FOLLO8AAG RESTRCTOS ARE COOPEPEO NECESSARY FOR SAFE COERATICet MO Seinen I I necesssey) ..-. F GEAR/CATCH a Ivey ow, tel I An He ennwodonwe Ice he sonlI of MO • Wall FIISF..thad dew. M V* rat is forint rat il• /SS Araon AdreIsVaTol 11 salaam/ NH Tee 190F, M.20 Sm. Coo 44I0I As Am MONO. Federal AVOW. Regalices new re *Taal NF Ow Ingeoed ard Is AN te ire Ilor di ONA DATE HANE ARO nTLE "%WINN SIGNATURE w ni in i g I § 1 A. Omer., Lemma* rd HAWN In Camino Mth II CSR Soman 919. As Atolates O. Stamen. al Calcamy. FM Non II MS (Awn mMa ropes* H '°"o ArectiNmos Canerancmc• *von AVOWI pawn efiCa Ov.an:0 Y B Cum% @nip Linatted Mani C On °MAFIA PPSTSECIAMM.0 40.Knsietil IX I. Polproul Fentsers %sad In ACost/wa WM IF OFR S4CIOn At 3 a CAR IOVMPSOMal 1 D. 0 0• 4‘1001 *Wean Warren MAWS nAintel I maw Pa t BM Memien, FM Tam 337 Oalla NM ANNOY 'K 0 ACOnlanCe WIN j: nr4 CIRSOTOI .naihr. “2",4 7 71 " (Cove woo) S F. MS IIVOKIlerl ReCaltdOS WI Aliall1ROCCRIS Nr IC ore-Sple cHM Suies• of Commiseot FAA Finn SIJOIS Mtn* WWI /MIMI FM Fon" 81)34 OM) Al Petittari BIEN' Sup014040 FI•CleOlIC Fame. -PDF P•co 2 on SDNY_GM_02755221 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242143 EFTA01327261

SDNY_GM_02755222 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I 44 EFTA01327262

COMMICKTCV CAI EGORYOESIGNETISS WO VAT'S 0. AWEIWA TIVIerATTONI.Fttfly. Awn}, Armearmnou SPECIAL AIRWORTHINESS CERTIFICATE A EliORMEPETAL PURPOSE RsOnrch sod Ektialtillin . • MENU. FACTURER NILE 1 4; 0 ADDRE$$ IV C WENT FROM TO o N. alLIE SERIAL NO. MULE °UWE* (waft cenm meat a las E OM OE ISSISOCE fay I % EXPIRY nitwit°. I WA T Asynaldt ARE PART OF EMS GERI FICATE DOOMT01 CO OFFICE NO OARS 40014114E Ary 00,110. rep-COS Cr meta Cr In nil aIowa's tf a Mg IY•Karp $I.00:0 ct ernamint nal acme. 1 pin. co pow MS CIRTIOWATI W37 It CeSIRAYO) PI TIff allAst IMICCOVANCE will soWSEE ME ii COX OF MOM AIGULATO4SiCiRI y cm .) NylotInts. SONY_GI,1_027 55223 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00242 I 45 EFTA01327263

A I Ths swift...nun/co s akethrde he aeoilitl ROW Wm FJC4 49 l).0.0 Stfis Cc* n ! °MI HMI alt 1.• u Coot V F•Uta Fentinais ICFRI n Re yeshiva ourinca sown: ni "-outflowend cn Co nano WeConn potwar fiplInt rd m, f >Tear Vitali, damn *We* n Pierre No mien as c»64 p:0shr tip tort oft, on tarifa* III Care Prw • a rOcOnli, 13, matt*", We rott (21Carryty on: es ta etweim la tuiP•Pme at Stitt r The inKthreu anion Manes M WI waled Ai IN waif slIe b ea paw torn OW A D D. Ithterran olden main Mad to en d auks* MI lotla SC. wan Fa Om repaid am bat 1) frog t. t OktreiberiSti I M NO** CM Tile mitidus NI Mel III reomisd be mmHg* onashmeird SSW anatiosinctles poods1 briar. b il•Conielater rinovi Cal PasSI*003 Moan Rey epsnit tome MOM el IF• mine us oicoasi n amnia min re Koko* CFR Ina imam se lotto Isaias eta ,'" be ;viols, of Ma Friel Disoiliceit (2j ow asp lbw may shed to two pomun cats nay E Ins Caw kratiele.raoff0rActrircluot pa Ombra! onion sahet:re* ' datolcn ird War Se pram cresoted a UCIlk Pin 21. Sockn 2I 181 a 21.2O. SDNY_GIA_027 55224 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 00242146 EFTA01327264

MATEO STATES CF AMEND DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE 1 NATIONALITY NC REGISTRATION MARKS N493LX 2 IMNUFACTURER AIO SAOCEL Raytheon Aircraft CO. 400A 3 AIRCRAFT SENN. RUINER RK-244 4 CATEGORY Transport S AUTHORITY AND B.4.5G FOR ISSUANCE This *brat nos osolfaire is bawd pawl In to Fodor& MANN Ad of UM a/ Neigh* I ft CA IN NM of Sun to Wicnoll b Nth Rae, Ns ban impeded end found lo maga b to Ws cellecole torwror lobe In cayllion tor Se operan and has Won OWN. le 4444 br NifirwoRS 5NpONON Ofopyhosly• and dotabsd afrocotan4 NOR w proAdr3 by Arno Me M CemonIce cm Wereecni ON ANON% OWN M MINI Nur EARINafty None S TERIESANO CONSTIONS USN* New. novadould RACOrdid. nooks& ore isrmlwlka YM b atertiSs fisnatthad by Go Arbrinhlrelor. Ei. oinvatilmos collkOle McAsWw As bug as the Rflownas. worinIsthe ordnion and stostwe petered II saccolononee Pols 21.41 4.10 t of ow FeNna Avisti3nR4GARN34. . WrtnA fogIssonicl Into UM40 Slaw DATE OF ISSUANCE R 10/01/1999 REIZ seREACtic"". rgio . Perez CeIGNATCNNINISER AEA -FSDO -23 My anat.. noyossalon or sumo of Iwo armor TN ta NnINSAi RN AN eve saalodho SECO'," hwasoyrions not some. 3 NOM YOS. INS CLAYS KATE siuST SE DISPLAYED THE AMMAN' IN ACCORDN4CE YAM APPLICAIRE 1104ANRAATX44 RE044ATIONS. FAA Fonn 11004 pa) SDNY_GM_02755225 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242147 EFTA01327265

SDNY_GM_02755226 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242148 EFTA01327266

26180 (WM Wiithtnalway Nye/Pa 14111 1177 703.2348 wow Ilightoptions.om May 8, 2013 VIA HAND DELIVERY Nextant Aerospace. LLC 26180 Curtiss Wright Parkway Cleveland. Ohio 44143 Attention: James lmmke Re: RK-244 —Agent Authorization Ladies and Gentlemen: elltOptions 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 Edward T. McDonald Vice President of Whole Aircraft Acquisitions and Sales MADISON GOLDSTEIN NOTARY PUBLIC STATE OF OHIO My Comm. barn Aga 24.2016 C644:- O1B SDNY_GM_02755227 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I 49 EFTA01327267

SDNY_GM_02755228 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242150 EFTA01327268

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 1) 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 § 91.319(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 I4 CFR §91.409(e), (1), (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 I I) 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) NIA 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 SDNY_GM_02755229 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242151 EFTA01327269

SDNY_GM_02755230 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242152 EFTA01327270

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 acrobatic flight; that is, an intentional maneuver involving an abrupt change in the aircraft's attitude, an abnormal attitude, or abnormal acceleration not necessary for normal flight. 18) 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. 19) 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 Pan 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 requirements. of parts 14 CFR pans 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, ON 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 Anrinntl ;n Id era s 411 SDNY_Old_02755231 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA (10242153 EFTA01327271

SDNY_GM_02755232 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 154 EFTA01327272

EXPERIMENTAL OPERATING LIMITATIONS PURPOSE Research and Development MAKE Raytheon Aircraft Company 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. / Mark T, Reynolds 7:- VA Signatu e DARF-400148-CE. May 20.2013 SDNY_GM_02755233 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242155 EFTA01327273

SDNY_GM_02755234 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242156 EFTA01327274

nextant aerospace Quality Assurance Department To: Federal Aviation Administration Flight Standards District Office Great Northern Technology Park II 25249 Country Club Blvd North Olmsted, Ohio 44070 Date: May 13, 2013 From: lames F. Immke Director of Quality Assurance Nextant Aerospace Subject: FAA Program letter for Beech let 400k Serial number RK244, Registration Number N493LX. Ref: FAA order 8110.2G 1. Registered Owner: Flight Options LLC . Address: 26180 Curtiss Wright PKWY, Richmond Heights, Ohio 44143 2. Aircraft Description: Twin Engine Light let a. Registration: N493LX b. Aircraft Builder Raytheon Aircraft Co c. Year mfg.: 1999 d. Aircraft Serial Number: RK244 e. Aircraft Model Designation: Beech let 400A 3. The program purpose for the aircraft will be used To complete the flight performance profile in Research & Development Category in support of FAA Project SA 152501A-7 (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 5. Describe the areas over which the flights to be conducted and address of base operation: The base of operation is Cuyahoga County Airport, 355 Richmond, Cleveland, Ohio. Flights will be conducted in North America. 6. Describe the aircraft configuration: This Aircraft is a standard Beech 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 . 1T1SD 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. Senior inspector Nextant A r Tel Work Cell SDNY_GM_02755235 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 157 EFTA01327275

SDNY_GM_02755236 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242158 EFTA01327276

LOG BOOK ENTRY from Designated Airworthiness Representative (DAR) REGISTRATION NUMBER AIRCRAFT MAKE/MODEL SERIAL No. TT/13N LANDINGS/CYCLES N493LX Raytheon Aircraft Company 400A RK244 6563.8 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. imitations 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 utifized. 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 cants program letter. The Standard Airworthine C rtifmate da R 1 1/1999 has been superseded. / 415/20 /eta 7.-- Date Mark T. Reynolds, DARF-400148-CE SDNY_GM_02755237 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242159 EFTA01327277

SDNY_GM_02755238 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I 60 EFTA01327278

0 MAJOR REPAIR AND ALTERATION USDepernam el (Airframe, Powerplant, Propeller, or Appliance) Taws. mow mem sammrstion Patina:maul cwra No 212,34020 wrXx2C07 EISCIrOnie Tracking Number For FAA Use Only INSTRUCTIONS: NM or type all entries. See FAR 43.9, FAR 43 Amend* B. and AC 4194 for subsequent revision thereof) to. instructions and disposer* of this tom This report is required by taw (49 U.S C. 1421). Films to mix* can result MAGNI penalty not to exceed 11.000 Tar *OCR such viotafon (Section 901 Federal Awation Act 1958) I. Aircraft Nationality and Regisvation Mark N493LX Serial No RK-244 Make Raytheon Aircraft Company Model 400A Series 2. Chimer Name (AS Mow, on regraration terbfiCSM) Flight Options .LLC Address (As shown on Mgisfrafion cennica(4) Address 26180 Curtiss Wright PKWY Ccy Richmond HeiohLs SUM OH 20 19.1.43-1453 County USA 3. For FAA Use Only 4. Type S. Unit Identification WM Alteration Unit Mn Model Serial Number 0 0 AIRFRAME (As delCoDed in !fern 1 above) 0 0 POWERPLANT 0 El PROPELLER 0 0 APPLIANCE Intl fromecturrir I. Conformity Statement A Agency's Name and Address 8. Kim of Agency Name Nextant Aerospace Minn 355 Richmond Road my Cleveland she" OH Zo 441431453 Cani LISA 0 U.S Cenkated Mechanic O Manufacturer O Foregn CertfiCated Mechark C. Cenificare No 0 Certificated Repair Station CRS # 25NR667B 0 Certificated Maintenance Organization D. trendy that the repair andior alteration mode to the unit(*) identified in items above and deserted co the reverse or attachments hereto have been made in aomelance nth the requirements of Pan 43 of the US. Federal Aviation Regullians and that the information furnished hers, is Me and Correa to the best Of my knoMeelor Extended fuel pent par 14 CFR Pan 43 APP. El 0 Signature/Dale of Automat Indent*, A.Ockwell 4-12Lk A 05/30/2013 7. Approval for Return to Service Pursuant 10 the authonty given persons spectra/ beam. the unit Ideated In item S was inspected in the manner resented by the Administrator of the Federal Aviation Administration and is 0 APPROVED 0 REJECTED 8Y FAA Flt Standards InSpeClOr Manufacturer Maintenance OnaangabOrt Pride^ APPreree0 by Canadian Department of TranSpOrt FAA Designee X Room Station Inspection notariza Other (Specs?) CerneCate Or Dritriation No CRS # 25NR667B SignaturelDate el Authorized Indmdlual A.Ockwell a tion ldta 05/30/2013 FAA Form 337 ilOo” SDNY_GM_02 755239 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 Erl'A_00242161 EFTA01327279

• • • SDNY_GM_02755240 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242162 EFTA01327280

NOTICE Weight and balance or operating levitation changes shah be entered in the appropriate aircraft =ord. An alteration must be compatible with ea previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (ft more space is required, attach additional sheets. Identify wah aircraft nationality and registration mark and date work Completed N493LX 05/30/2013 Nationality and Ftegistratan Mark ueia Part I of 3 The Following Equipment was removed along with Associated Hardware. EF0-871 622-9345-203 Electronic Flight Display EF 0-871 622-9345-203 Electronic Flight Display MFD-871 622-9434-213 Multi Function Display ICU-85 622.6189-002 Internal Compensation Unit ICV-85 622-6189-002 Internal Compensation Unit AliC-8SE 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 ICK-4000 ( 4) 622.9814-514 Card Assembly MDC-4000 622-9818.751 Maintenance Computer CSU-4000 (2) 822-0049-002 Configuration Strapping Unit FMC-5000 (4) 822-0891.008 Flight Management Computer PWR-4000 (4) 622-9945-021 iAPS Power Card GPS-4000 822-0931-003 GPS Receiver Mounts 622-9430-002 EFD /MFD Mounts EFB Electronic Flight Bag Mounting 0 Additional Sheets Are Attacked Form 337 0046) SDNY_GM_02755241 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I 63 EFTA01327281

• • • SDNY_GM_02755242 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242164 EFTA01327282

NOTICE Weight and balance 0r operating limitation changes shaft be entered m the appropriate aircraft record. An Devotion must be compatible with as 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 ',shone*/ and regustrahon mark and date work completed) N493LX 5/30/2013 Nationality and Registration Mark Page 2 of 3 Installed the Following Equipment along with Associated Hardware. Date Model Part Number Deseriplion 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 CCU-3001C 822.2362-003 Data Concentrator Unit 5.0 325 OCU-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 FM/ -S010 822-1543.101 File Server Unit (1d IFIS) 6.5 60.83 ECU-3000 822-1200-998 File Server Unit (1st IFIS) 0.40 57.5 AFD-3010E 822.1753-416 Adaptive Flight Display 12.90 89.2 AFD-3010E 822-1753-416 Adaptive Flight Display 12.90 89.2 AFD-3010E 822.1753-416 Adaptive Flight Display 12.90 89.2 AFD-3010E 822-1753-416 Adaptive Flight Display 12.90 89.2 IMT-3010 822-1140-401 AFD Mounting Rack 4.40 85.0 IMT-3010 822-1140-401 MD Mounting Rack 4.40 85.0 IMT-3010 822-1140-401 AFD Mounting Rack 4.40 85.0 IMT-3010 822-1140-401 AFD Mounting Rack 4.40 85.0 10852801Y00 Fuel Quantity Conditioner 0.90 324 PC920.2A2000PH-2A1 Fuel Flow Conditioner 1.10 325 GPS-40005 822-2189-004 GPS Receiver 6.0 37 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 P5-8350 501-1228-004 Power Supply 12.5 52.9 MMT-5000 822-1811-003 File Server Unit Rack 0.30 57.5 MMT-3010 (2) 822.1290.003 AHS Mounting Rack 1.80 57.5 XM WR-1000 822-2031-002 XM Weather 1.5 41.0 CHP-3010 822.1280-003 Course Heading Panel 1.30 92.5 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 0 Additional Sheets Are Attached Form 33? 004.8 SDNY_GM_02755243 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA (X)242165 EFTA01327283

• • • SDNY GM 02755244 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA _00242166 EFTA01327284

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 appecable airworthiness requirements. 8. Description of Work Accomplished (If more space is reported attach additional sheets. Identify with aircraft nationality and registration mark and date work completed) N493LX 05130/2013 Pagc 3 of 3 Nationally 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-8500 (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-S11 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-40-18-86-E0Y45 Pull Up/ Terrain Annunciator 0.05 88.0 Annunciator 2-F840231 Terrain Inhibit/ Terrain Fail 0.05 88.0 In Accordance with STC ST109S9SC. See Attached Copy AFM Supplement, Nextant Aerospace Doc. No. 373.00-0023 Rev IR Dated 09/02/2011 or later FAA approved revision, installed on Aircraft. Equipment Pilot Guides are Installed in the Aircraft as Portable Document Format (.pdf) via supplied I-Pad. NOTE: Portable electronic devices used to store required aircraft records required by Part 91.9 are considered Electronic Flight Bags (EFB) per FM 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 NSW Master Drawing List (MOO 373-00.004 Rev C. Carried out Hawker Beechcraft Service Bulletin 34-3431 Reduced Vertical Separation Minimum (RVSM) Airframe Inspection / Modification. Performed FAR 91.411Inspection per Part 43 appendix "E" Pitot Static & FAR 91.413 Inspection per Part 43 appendix "F" TranspOnder System checks. K Additional Sheets Are Attached Form 337 (10-063 SDNY_GM_02755245 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242167 EFTA01327285

• • • SDNYGM_02755246 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242168 EFTA01327286

• • • !Lida $Lnitts of ,Ponrrirn !epnrtnlent of Transportation Arbera I cAbintinn cahminiatratinn $upplentental `Type Certificate avid/€.0,4•sii.yeisele .4 71.1.,021&" STI0959SC Nextant Aerospace LLC 26180 Curtiss-Wright Pkwy. Richmond Heights, OH 44143 ordani ort.epo ris /44yroanter/4.44/etuor:Inerekairirved4 dordridivo carietwalreeasas door Add negv/eaCtevwv.in.e.4., z.4 r/9od 25 ../a Federal Aviation aerta.ivi.i. (See Pages 1 and 4 foe comokit ccnification basis.) avirereanirrof- •girSerriVorae.rWrentere Al 6SW ..41,04. Hawker Beechcraft Corp. ..X.4.10,i 400A ghkwishm earn flwila P.;;Orr 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. 2eIdeffnaJe7/14%;Vid1.4.e•IJ: I) The installer must determine whether this design change is compatible with previously approved modifications. 2) If the holder agrees to permit another person to use this certificate to alter a product, the holder must give that person written evidence of that permission. . 3) For aircraft equipped with Pratt & Whitney ill SD 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. ervid/ool, /ad. anoirvddry as, a/Laird .cC .CQ& geyoryortufrot ',wooers al Wen! wrianeowisrineed Joyarsoadd ?wrested reale/rat/4"v do* 4. M4w,aM Min/ 44 .ArGradsriaa/n //a, Poileast. 4v:thew ./geGnigaileahrei Are Ardathm...lune 26, 2008 October 19. 2009 ghteek elAGe "file rlaWnrod September 26.2011; April 05.2012 v gnehile) Siena L Lardinois tanager. Symms and Flidhi Ten &ranch Chicago Aircraft Conificalitio Office A" rM FIMm sllo.nllo.t01 one this °mit JJJ * P.W.SIA.00.• by a lir.* or ro t titaliallAs !LOCO. Of 1•011.60.014.1 Re. •MCO•01•11 2 r1411. of path. rll I tao any be tr.gr.Ss i ab.Nnce+an yM 21.P. SDNY_GM_02755247 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024211 69 EFTA01327287

• • • SDNY_GM_02755248 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242170 EFTA01327288

• • • liniltb Slain of Atnerin Pepartinciff of Zronsportation - Aeberal (ablation eAbminiatrution (Supplemental `Type aertifirate ( ontinuation *Beet) Ateunte", 5110959SC #,i. et/luaanai October 19.2009 Date Amended: September 26, 2011; April 05.2012 HIrrafrideVIJ andi)tYldrianlo, ternavAnze./: 4) For aircraft equipped with Williams F144 -3A P Engines, those engines must be installed under S'I'C ST02371 LA. 5) For aircraft equipped with Williams F144-3AP Engines FAA approved Airplane Flight Manual Supplement, Nextant Aerospace LLC Doc. No. 373-00-0023 Revision IR, dated September 2, 2011, or later FAA approved version, is required on board the modified aircraft. 6) Aircraft must have previously qualified for Operations in Reduced Vertical Airspace via: RK- I thru RK-I 17 and RK-119 thru F1K-139, Hawker Beechcraft Service Bulletin No. 34.3431. RK-I 18, RK-I40 thru RK-224, Hawker Becchcraft 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. ..52tuu: 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 Hawker Beechcraft 400A aircraft is as follows: a. The type certification basis for the Hawker Beechcraft 400A aircraft is shown on TCDS Al6SW for pans 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 IGSW and §§ 14 CFR Part 25 as shown on page 4 of 4 of this SIC. Any ol[Orditron of Ulla conlircato is perfAhrbJ.0 by o lire et not ort•odsno 31.000. or JMPfICOAMMI eel extent,. J years. Or Dein. •M nap ells m rolls ICMCO wry be trono 'infra in ocean/roc, with FAR JI I>. SDNY_GM_02755249 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I 7 I EFTA01327289

• • • SDNYGM02755250 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242172 EFTA01327290

• • • blvillirb $1Inns of AltMICH giepartment of Zransporintion Actin:al Abiation Abministration Supplemental Zgpt Tertificatt ((gentinuation Sheet) 9041 Vit•UceOetteet October 19.2009 Date Amended: September 26,201 1; 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 (ENS) with Rockwell Collins FMS-6100 modification was determined to be TCDS A I6SW and the following later regulations: Arndt 121.4j 25.771 (a,c) Any:K[25.23J 25.301: 25.301: 25.581. 25.607: 25.611. 25.773 (00)(2Xd) Amdt.(25-381 25.1309 (a)(b)(0(0(eX10; 25.1322 Aind025-401 25.901 (b)0Xi): 25.1519 (aXbXe) Amcb125411 25.1121 (axemo): 25.1331; 25.1333 AmM125421 Amdt.12546) Anuttl25-54) Amdt 125.721 Amdl.125.801 25.1501 25.603; 25.605; 25 613; 25.1529 25.307;25.571.25.1307 25.1316 25.1329 (A) (OM. 25.1351 (a)(1)(d). 25.1381:25.1521 (a)(0; 25.1543(0):25.1581; 25158340 Amdt.125461 Amdl.125.901 Art41125-911 Amdt.125-102) Amdi.125-1051 25.305 25.1303 25 561 25.991 (aXb) 25.1585 (a) Amd7125-108) *m0125409) Arndt 1254 131 Amdt.125.1221 Amdi(25.1231 25.1325 (d) 25.1323 (exAS) 25.869 (aX1): 25.1431 25.1317 laX0Xe) 25.1353 (aXe) 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 Profile 21 FMS-6100 with LPV Approach enabled and UASC TAWS was determined to be TCDS Al 6SW and the following later regulations: AmdclOriginall 25 601.25.605.25.609. 25.613.25.1301. 25 1357. 25.1381, 25.1525. 25 1541, 15.1581 Arndt 1241 25.771 (a) Amdi. (25.231 25 301; 25.303. 25.305. 25.307, 25.561(e); 25.607:25 611. 25.1307 Arndt 125.381 25.603.25.1322. 25.158310 Amdt.1254101 25.1585 (a) Arndt (25411 Arndt 125.421 Alma 125461 Amdt.(25-541 Amdt.125.7211 25.1309 (3)(bX00)(e)(8,) 25.1501 25.777(01c) 25.1529 25.869(00) 25.1351 MO Amdt(25402) Amck125.1 01 Amdt 125-123) 21981(00) 25 1131(a) 25.1353 (s)(e) - END - Ay 000000000 or knee cotesticoce IA polusoes • riy • en• o not ••Cnellee• 51.000. Or 1ogg,o04.Oot nOt GoOoodeig 3 rare. Of WP. FM MN 4514.2.I110.1,1 VMS 4 of 4 PAGSS enis n.nl/. CAI* may M 00000000000 in occorOW•co wet,. •AA :$.4, SDNY_GM_02755251 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242173 EFTA01327291

• • • SDNY GM 02755252 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I 74 EFTA01327292

e MAJOR REPAIR AND ALTERATION S04910.11, 1 el (Airframe, Powerplant, Propeller, or Appliance) Trawallean reserstamme emensenism fi P0rovad Orm A .40 No 2,204:020 MAGOON Electronic Trackkm Number For FAA Us* Only INSTRUCTIONS: Prim or bye an entries. Ste FAR 43.e. FAR 43 Appendbe e. and AC 43.0.1 (or StreSequer4 nengon thereof) for mg/oceans and clisposnon of this form. Tlbs repot Is respired by law (49 U.S.C. 1421). Figure to report can result in a owl penalty not to exceed 11.O0O for each such vitiation (Setbon 901 Federal Aviation Ad 1956) Ai 1. rcraft Nabonality and Registrabon Mark N493LX SWIM No. RK 244 Heim Raytheon Aircraft Company model 400A Sines 2. Owner Name (As Mown on regestranon rertfiCell) Flight Options .LLC Afteas ms shown On reeistrabon CertleCate) ACOniss 26180 Curtiss Wright PKWY cry Richmond Heights sum OH I, eil33-145.1 firu-R1 OA 3. For FAA Use Only 4. ype 5 Unit kientincation Repair Mermen Unit Make Model Serial Number 0 0 AIRFRAME (As ereSCebert in item 1 above) 0 O POWERPLANT 0 O PROPELLER O O APPLIANCE Ti..;e 6. Conformity Statement A. Agency. Name and Address B Kind of Agency Nam Nexlant Aerospace Fem. 355 Richmond Road coy Cleveland sum OH zie 44143-1453 Carey USA 0 usCerosomed mechanic 0 Imenutaaurer 0 Foreign Cambria:40 mechanic C. Condon No. El CenDrated Repay Station CRS # 25NR667B 0 CM/Mated hlenienance Organgehon D. I certify Mat me repair anceOr alleratiOn made to the units) identified in item S stove and described on the reverse or atlacherienis nettle have been made in accordance *An the requirements of Part 43 of the U.5 Federal Aviator' Regulations and we me niorminion furnished herein,. true and correct to the best or my knowledge. Edenoee range tort P FR Penal APP re8 14 C O Signature/Date Of nut/Milled Indivilual 05/30/2013 F. Afgamil Mr Return 93 Swat Pursuant to the autnonty given pecans peeled below. the une dimmed in item 5 was:WOOS In the manner prosated by the Adminsemor of the Federal Av19101NA0111.10,119(100 and is 0 APPROvEO 0 REACTED BY FAA Ft Standards Inspector Manitactucer Maintenance Orgarszabon Person Approved by Canadian Depanmem el Transport FM Designee X Repair Sleben inspection Aulhorizabon Otter (SPeelfYi Cenificaio or Designation No CRS IS 25NR6676 SgnalurerOale e4AUlh00300 Inewdual ) ( I 05/30/2013 FAA Form 337 PC6) SDNY_GM_02755253 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242175 EFTA01327293

SDNY_GM_02755254 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242176 EFTA01327294

NOTICE Weight and balance or operating limitation changes shall be entered in the appropnate aircraft record. M alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements 8. Description of Work Accomplished (ft more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed) N493LX Nationahty and Registration Mark Nextant Aerospace Completed STC # ST02371LA Removed Pratt and Whitney1T15D-5 Series Engines . 05/30/2013 Date Installed the Williams International F144.3AP Engines with Full FADEC and Associated Systems in accordance with Nextant Aerospace MDL -NXT-001 Rev IR Dated 08/22/2011 or later FAA approved revisions, and FAA Approved AFM Supplement NXT-1-AFMS Rev IR dated 9/15/2011 of later FAA Approved revisions. Installed Left Engine Part Number. 111000-202 Serial No. 252757 Installed Right Engine Part Number 111000-202 Serial No. 252758 ICA AFM Supplement was installed on Aircraft. Nextant Aerospace Instructions for Continued Airworthiness Document NXT-ICA Rev IR or later FAA accepted revisions are included in the Aircraft Maintenance Records. Carried out Engine Ground Runs and System OPS checks IAW Ground Test Plan 373-00-0024 Rev F. End K A00610061 Sheets Are Attached FAA Form 337 0006) SDNY_GM_02755255 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I 77 EFTA01327295

SDNY GM 02755256 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242178 EFTA01327296

Puget. Platte OS Ruissisti Pepurtinent of Zruttapnrttition - @f awn( JAhintinii jAbininiatrution $upplemental `Type Certificate A te4O24. ST02371LA .14 A-4/140.taawnek Nextant Aerospace, LLC 26180 Curtiss Wright Parkway Richmond Heights, Ohio 44143 reAjetv frricreta, rAve ea/Aar re efetrAC /44iStivirffivediettpai imileritiv/J etateet44hint enienlerJ ringiteavennetten4 /4 at:wet/Su erytterrenve4 tegird 25* tea ...4rdwitenvichiw flterithivm. 'Certification basis is set forth on TCDS A16SW and continteu ion sheets 3 and 4. Cgov:so‘gthtetai firtISIMOtriaJKIMA•. Al 6SW .144' Hawker Beeelteraft 400A alel;a4S• arb glvisw Mir Replacement of Pratt & Whitney 11-1510-5 series engine with Williams International F.144-3M' 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 15, 2011 or later FAA approved revisions. Nextant Aerospace, LLC Instmetions for Continued Airworthiness document NXTI Revision IR, or later FAA accepted revisions must be provided with this STC. .9kmagahw• imillic..44Mviu. 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) erriatilet anne/efr.feyytevair dritz etati /4 4../taAr eyytnyvtedrenviartis ,.'. Oat/tea Jainvalte-roi Ja0tYnteme erwarevlar a Inwitimhivatatin t) edema eutateddasee; /4. often Feeirerti-Avir/Zvo.igebte:rebehivn OretteArtiedaron, March 24, 2008 giarat/onno..- September 27, 2011 4474, mowed.. giCIA ovnfrniod' 4.4.441.PAtnetv 1 (Signature) AC( I t )6- ) Manager, Propulsion Branch Los Angeles Aircraft Certification Office (Mk) pry dfielitriON of Mu artgicate is puma:WM by a fine of nor tweeting 11.0(4 a impthonmeut not .um4img 3 PM o, 604 rat Vern 6110.1114-44I no. 1 el 4 ifilteeff,telt maybemm.1am, inarrodam with lAtt.23.4z SDNY_GM_02755257 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242179 EFTA01327297

SDNY_GM_02755258 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I 80 EFTA01327298

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 h to hint TRANSFER ENDORSEMENT Transfer the ownership of the Supplemental Type Certificate Number to (Warne of tratujente) (jldirzss of Wa itsfird (ALiridrsel !IMO itfor. Jut ad Zip rea4) from (Name ofgmtitor)pthst or type) Otareu of grantor) Otalos • oaf soul) (Ciot. :rote. eni Zip tea) Extent of Authority (if licensing agreement): Date of Transfer: Signature of grantor On inkk Fay 2 of SDNY_GM_02755259 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242I I EFTA01327299

SDNY_GM_02755260 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242182 EFTA01327300

}herb Alnico Of America !gnu:Intent of tifransportntion - gehernI &Ablution cAbn l i ll istration Supplemental Type Certificate (gontinuation Age° Afteen4(ST02371LA gemietaiva sedlioncleravas/ocah.:74vai • Nexiant Aerospace, LLC, "Installation of Rockwell Collins Pro Line 21," Amended STC • ST10959SC, dated September 26, 2011 or later FAA approved revisions is required as part of this alteration. • The new Vince and Vmcg values are 94 KIAS and 93 KIAS respectively. • Tlx new engine minimum rated thrust is 3,031 lb at sea level, flat rated to an ambient temperature of 77°F. • Approved engine fuels are: Grade Specification Jet A ASTM-D 1655 Jet A-1 ASTM-D 1655 eiwid/rarhne• The certification basis for this modification is as follows: The original certification basis for the Hawker Becchcraft 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), 25.1 353(cX5), and 25.1447 of Amendment 25-41; §t 25.29, 25.255, and 25.1353(cX6) 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 I, 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 fed), and Special Conditions No. 25•ANNI-33 dated here 18, 1990 (Lightning and Radio Frequency Energy Protection). (See NOTE 12) Equivalent Safely Items: (I) Out-of-trim characteristics § 25.255 (2) Pilot compartment view f 25.773(6)(2) (3) Passenger compartment door § 25.813(e) (4) Emergency exit marking 9§ 25.81 (d)(1) and 25.811(dX2) 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) flay attention of this reateirrosidia64 6y n fine of nog anyerliaw $1,004 Of anliconloof not aroaruse 3 YAM or fer4 FAA Pars $110•1111•49) ono) *1 • Igis certificate lay be tmarfrmdia occon4nalviihfAlt21.47. SON Y_GM_02755261 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I 83 EFTA01327301

SDNY_GM_02755262 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242184 EFTA01327302

AMA 'Wm OM Amara Pepttriment of transportation - gebtral c/k6intion Abntitiistration „Sitypiemental Type Certificate (01antinuation Ailed) Afeednie, ST02371LA fredokaien Vanawsif Subpart A —Design and Construction: 25.603(25.46), 25.605(25.46), 25.611(25.123), 25.613(25-112), 25.625(25-72), 25.832(25-72), 25.863(25.46), 25.869(25-123), Subpart E —Powarvlantt 25.901(25.46), 25.903(25.100), 25.951(25.73), 25.961(2547), 25.981(25-125), 25.994(25-57), 25.997(25-57), 25.1013(25.72), 25.1019(25.57), 25.1021(25.57), 25.1043(25-42), 25.1045(25-57), 25.1091(25400), 25.1093(25-72, 25.1103(25.46), 25.1141(25-115), 25.1143(25-57), 25.1163(25-57), 25.1165(25-72), 25.1181(25-115), 25.1183(25-101), 25.1185(25-94), 25.1189(25-57), 25.1195(25.46), 25.1203(25-123), 25.1207(25-46). Subpart F — Emtinment; 25.1301(25-123), 25.1305(25-115), 25.1307(25.72), 25.1309(25423), 25.1316(25-80), 25.1317(25-122), 25.1321(25.41), 25.1331(25-41), 25.1351(25.72), 25.1353(25.123), 25.1357(25-123), 25.1381(25-72), 25.1431(25-113),25.1438(25.41), Subvert G - Oneratine Limitations and Information: 25.1501(25.42), 25.1521(25.72), 25.1527(25- 105), 25.1529(25-54), 25.1543(25-72), 25.1549(25.40), 25.1551(25-72), 25.1557(25-72), 25.1581(25-72), 25.1583(25-105). Subpart - Electrical Whine 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 CFB Part 34 (34-3): 34.11 14 CFR Part 36 (36-28): 36.1-36.7, 36101-36105, 36.1501, 36.1581. The following Mutant Aerospace Continued Airworthiness Supplemen is arc applicable to airplanes modified in accordance with this STC: • Master Minimum Equipment List document No. MMEL Rev. 8, dated 02/21/2011 or later FAA approved revisions. • EWIS (Electrical Wiring Interconnection Systems) Inspection Procedure/Report No. NXT1-EA-007 Rev A dated 8/24/11 or later FAA approved revisions. Any afitrahou of Mu ernireots as psoushoSk by a fine of not aridity 13,0013 of impuonavot Not (venlig.; }tam or 6014 TPA Fate ILLO.2110.Cii .49, 4 of I ibis unified's Noy Se tronsford so offonfonts nofb Mtn. 47. SDNY_GM_02755263 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242185 EFTA01327303

SDNY_GM_02755264 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242186 EFTA01327304

OW OW US Ceparent MAJOR REPAIR AND ALTERATION ci Tremortibm (Airframe, Powerplant, Propeller, or Appliance) Fothrol A Ratk. ermhinentiee Fain Neve., OmB No 21200020 11/X,0007 Iliedraik Tiact% Norte Fee FAA Unduly INSTRUCTIONS: Pint or type all entries. See Title 14 CFR §43.9. Part 03 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:514161I5 Model 400A Series Not Applicable 2. Owner Name (As shown on reglstrehon certificate) FLIGHT OPTIONS LW FLIGHT OPTIONS LLC Address (As shown on regisMition certificate) moan Mee CURTISS RIGHT ey(Ye Oi Ik/CESONO HEIGHTS Sees OHIO 4 44143.1453 3 For FAA Use Only 4. Type 6. Unit Identification Repair Mention Unit Make Model Serial No. O al AIRFRAME (As desalt:4PM Hem I above) 0 O POWERPUMIT • O PROPELLER O . APPLIANCE Type manvadurer 6 CoMormity Statement A. Agencys Name and Address B. Kind of Agen y Nene nem OPs:As PAC U. S. Condoms mechanic I PAanufarturer Minn 21 tint on. . s.so Foreign certiecateo medians C. Certificate No. CS/ angraffenn as NY Ceitricated Repair Station DJFA206D Zip I3OX USA a)( Ceoncaleo maintenance Orgianzmon D. I certify that the repair and/or alteration made to the unit 5) identified In kern 5 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the intonation furnished herein is true and correct to the best of my knovrtedge. Extended range fuel per 14 CFR Pad 43 O APO. B Signature/Date of Authortted indMd rence Foster 4/3.2012 r--........C. Y/3/ 70/} 7. oval for Ret o Service Pursuant to the authority given persons specified below, the unit Identified Administrator of the Federal Aviation Adrrinistration and is £ In hem 5 was inspected in the manner proscribed by the Approved O Rejected BY FM Flt Standards Inspector Manufacturer 5( Maintenance Organization Persons Approved by Camden Department of Transacts FAA Designee Repair Station Inspection Authorization Other (Specify Certificate er Desienatim No. DJFA 206D SapaturefDate of Authorized Individual ,R obert W. Vogt 40/2012 ..------,:a . 9. 774 20 A FAA Fonn 337 noon SDNY_GM_02755265 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242187 EFTA01327305

SDNY_GM_02755266 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I 88 EFTA01327306

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. ff. Description of Work Accomplished (If more space Is required, attach additional sheets. Identify with °Ate nationakty IMO lefilStfeben meek end date work completed.) USA N493LX Nationality and Registration Mark 413/2012 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 {loco) END Additional Sheets Are Attached SDNY_GM_02 755267 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242189 EFTA01327307

SDNY_GM_02755268 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242190 EFTA01327308

IWO SUMS OF AMEACA DEPARTMENT OF TRANSPORTATONPEDERAL AVIATION ADAW1WIRATION STANDARD AIRWORTHINESS CERTIFICATE I 144.1104OUTY/4/0 REGISTR4T0044103 N493LX 2 14/14WOCTURIER MOO& Raytheon Aircraft Co. 400A 3 Plielart ItIVAL MAINFA RK -244 4 CAROCOLY Ttansport ALMIORITYAND PAM FOR =VAS= nib 304sreibses eerObbS bad pawl teals F.drSANakeAn al MB 4nd <SOY tes. N al Os etels ofb.'a.0MSvl Ist•MItt Sued Is We tome! Ind but b ccelvis la 04 It ontee Peak. es bt cogdPke tar sets on." sod hos teen OA • 0 OM I I I I r•OXFIMON3 of Or agIcaits ancedberaM re tusked owativit cote Ira :Mated by Amex Fb CM Cowden nunisulP4M4Con. =mot es raid Noir. lea None I TOWS NIOCOICT3t13 Las bar vaientand. ancoVed real as tontallin Omits ~Se sesea Aererneer, Nb ersztVinne lettlIale MIS* esteg is Ce tweetilt, an. afallyte S. peendin exc.-axes it, Pets 31. a soft' Oft fetal ANN", RepAsOn. Yet Ose Cavil Y mgkessed a M1 Ur.d Veto& DATE CP IMAM FAA MOM 4KIICCI NOW R 10/01/1999 io . Perez AEA-FSM.23 etne-a *A meta ass Onsabetster by fro easel AO teleensami sseselbe 3 vie tel. TIP CERTIICATeleaTIS IXISSAY13) DS THE MOW/ PIACCOOMIWINAPPIXAM1FICDOWAVICIFIVIREQWIONIL FAA Form $1004 (1041 SONY_GM_02755289 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242191 EFTA01327309

\ . SDNYGM02755270 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I 92 EFTA01327310

g. .C.—C-- -all2bra T ENGINEERING ORDER Aircraft Type Aircraft Number Serial Number Station Engineering Order Number M25-10/05-011 Revision Numbe Original Date 10-19-2005 Paget of: 1 ENG I NEER I NG ORDER T I TLE Electronic Flight Bag Mount Installation — Beechjet 400 Fleet Effectivity: Aircraft serial numbers RK-123 and after Description: To install a fabricated mount assembly near the co-pilots map light rheostat to hold the electronic flight bag computer Accompanying Documents. Work Compliance Instructions Form. DER approved Engineering Directive EDW01-5, FAA forms 337 and 8110-3, Reason: For the effective aircraft to obtain a paperless cockpit environment Prepared By Signature Date Keith Gawsyszawski ,..".; - 44- C.- 10.19.2005 Quality Assurance Signature,. - Date Robert Beaumont 0 ‹ e :,./-0S-- Approved By SI? Date Todd Hattaway , / 01 /0/2-/i/4 74r Regulat'i ry Compliance 92 Major Repair 0 Minor Repair FAA Approval N Yes 0 No Weight & Balance Affected 0 Yes 0 No Weight 4 lb increase Ann 108 Parts Required Equipment List Update Yes, FG3500-400N. EFB mount assembly, 4 each AN3-5A bolts, 4 each NAS1149F0363P washers, 1 each -11 placard 0 Yes N No Drawings Required RVSM Status Affected Yes, 1175TA, rev A, 5245D, rev B, 5244FC, rev B (included in the Engineering Directive) 0 Yes N No Publications Affected AD List Affected None 0 Yes N No Estimated Cost Estimated Labor Hours $176.00 4.0 hours Distribution Remarks 1 References 0 Maintenance Planning @ Maintenance N Quality Assurance ek Operations 0 Procurement 0 Aircraft Manufacturer (E1 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 MI OW 0pp4') 0 Urgent N Mandatory 0 Attrition FO•09 GMM Revision 1 09i2005 SDNY_GM_02755271 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 I 93 EFTA01327311

SDNY_GM_02755272 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242194 EFTA01327312

g. t -WI iziata WORK COMPLIANCE INSTRUCTIONS Page: Aircraft Number: Station: Work Order If Effectivity 1 of 2 RK-123 and after 0 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 01 ....- Document the maintenance action on a Flight Options maintenance transaction report form, FO-501 with the following statement in the discrepancy side: 'Accompishment of Flight Options EO M25-10/05-011 Installation of the Electronic Fight Bag, FG3500 mount assembly is due. - 02 Remove electrical power from aircraft and disconnect main aircraft battery. 03 Loosen the upper glare shield and right side cover (which contains the reading 6ght and air-cell phone assemblies) by removing the mounting screws and separating the Velcro strips. re b 04 Remove the three screws and 90 degree cover panel form the aft edge of the right side cover panel and discard. 4.--r. -e-- 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 bolts and NAS1149F0363P plain washers (included In the kit) to the pro-existing fastener holes. Snug but do not tighten bolts at this time. 8 06 Adjust the position of the EFB mount assembly to provide sufficient clearance between the existing ashtray and the EFB mount thumbscrew. --r, 07 When proper clearance is achieved In step fare, (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 11751A 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). .♦ — ..... N-,, - b.ritsi i - - ..arj*..::: 09 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. 11 With the EFB mount installed, loosen the thumbscrew knob on the mount assembly 'A to one full turn maximum (do not allow the 'Hold-It 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 copiNots 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 white 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. II contact does not occur, proceed to step 17 and NIA and initial blocks 13 through 16. Form Completed By: Date: Log Page: FO-10 GMM Revision 1 09/2005 SDNY_GM_02755273 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242195 EFTA01327313

SDNY_GM_02755274 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242196 EFTA01327314

.. -:-.91:2361:11:1The WORK COMPLIANCE INSTRUCTIONS Page: Aircraft Number. Station: Work Order ft Effectivity 2 of 2 RK-123 and after ISI Engine ing Order Number: M25-10/05-011 OR 0 Fleet Campaign Directive Number: T I TLE Electronic Flight Bag (EFB) Mount Installation Procedures For Flight Op ions, LLC., Beechjet 400A's Item Wadi Description Mechanic Inspected 13 If contact occurs. remove the mount assembly liold-It' ann, 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' arm 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 Yr turn adjustments al a time. 15 Reinstall the 'Hold-It' 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 pad of the eye portion of the 'Hold-lr arm assembly. 16 Repeat steps 10 through 14 until proper clearance between the control yoke and the EF8 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 Resacure the upper glareshleld to the right side panel by reinstalling the mounting screws and resecurino the Velcro strips li ii.— 19 Attach the power plug to the EFS computer. 1..--dt 20 Install the fabricated '4 l' placard as slated 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 following statement: 'Complied with Right Options EO M25-10/05-011, installation of the Tt -7 Electronic Flight Bag assembly F63500-400N in accordance with DER approved Engineering Directive EDW01-5, see FAA form 8110-3 dated 8- 12-05 and Flight Options Work Compliance Instructions". 23 Complete the accompanying Engineering Directive checklist on page 2 and the previousty 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 Quality Assurance Department in Binghamton, New York and one copy of the FAA 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— *i2di jtein Form Completed By. Date: Log Page: Fo-lo GYM Revision 1 osnoos SONY_GM_02755275 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242197 EFTA01327315

SDNY_GM_02755276 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242195 EFTA01327316

eh VS 0roanneni MAJOR REPAIR AND ALTERATION el Tramp:hefty (Airframe, Powerplant, Propeller, or Appliance) innovel Ayieelen Adeenheation Fern Appoeed Ova No. ilen0020 Draw ' Enceteic TranceIluAtES Fee FAA Use 0MY INSTRUCTIONS: Print a type 41 auto. See Title 14 CFR §43.9, Part 03 Appendix B. and AC 43.9-1 (or Subsequent revision thereof) for instructions and disposition of this form. This report is required by taw (49 U S.C. 544701). 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 DEECRIET Series 400A 2. Owner Name (As shown on registrafion certificate) FLIGHT OPTIONS LLC SHMITKA AIR INC SOUTHEASTERN MILLS INC Er AI Address (As shown On negisfrabon corkficats) Mn,, MOO Cereselamm Pvn Citi Ridenvel Henan Siore OH hp 44112.1453 Caren USA 3 For FAA Use Only 4. Type 5. Unit Identification Repair Alteration Unit Make Model Senal No. Er O AIRFRAME (As describedin Item 1 above) E O POWERPLANT 0 • PROPELLER III O APPLIANCE Type manufacturer 6 Conformity Statement - A. Agency's Name and Address B. Kind of Agency win. F ot Oeisii. VC U. S 0linafiCated Mechanic I Manuleckeer hens 27 Um (Maga a ___, _ Faaign Cars/caeca Mechanic C. Certificate No. ow wawa Sins NY careaCated Repair Mahan DJFA206D bp '1004 Caney MA X caromed Maintenance 0rsanizabon D. I certify that the repair and/or alteration made to the unit s)klentified 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 Aft B ii Signature/Date of Authorized Individual Brian Kanya deCser A/ "reit 'I- // - //J-JOil 7. Approvallor Return to Service Pursuant to the authority g ven persons specified below, the unit identip in item 5 was inspected in the manner presorted by the Admnstrator of the Federal Aviation Administration and is Approved ITRejected BY FM Fit. Standards Inspector Manufacturer X Maintenance Organization PteSOnS Approved by Canadian Pepe/anent ot Tram0al FM Designee Repair Station Inspection Authorization Other (Specify) FLIGHT OPTIONS 135 AIR CARRIER CERTIFICATE Certircate a Designation No. DJFA 206D Signature/Date of Authorized IndMdual Brian Kenya 16.--04,44 "et ii.ownwit 1/- /Ada/ / FAA Form 337noa) SDNY_GM_027552T7 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242 199 EFTA01327317

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 actionably and registration mark end date work completed) USA N493LX SN-244 Nationality and Registration Mark 4/11/2011 Dale REPAIRED LEFT FUSELAGE SKIN ABOVE PYLON IAW US TECHNICAL E06110 227227. 8110-3 DATED MARCH 27, 2011. (WORK ORDER # 227277 SO.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 XXXXX)0000(XXXXXXXXXX)0(XXXXXXXX)0000(XX)00(XXX)000000(XXXXXXXXX)00CXXXXXXXXX SDNY_GM_02755278 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242200 EFTA01327318

0 Drop-rim MAJOR REPAIR AND ALTERATION of baemmmtM, (Airframe, Powerplant, Propeller, or Appliance) FoderM Aviation Administration km AOPMMM ova No. moboyo 11/14,20o) Dare Wean, meet. /et IAA Use ON, IS INSTRUCTIONS. Print or me as owes See Title 14 CFR §43.9. Pan 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this fpm. This report is required by law (49 U.S.C. §44701). Fail re to report can result in a civil penalty for each such violation. (49 U.S.C. 5463O1(a)) i. Aircraft Nationality and Registration Mark N493 LX Serial No. RK -244 Make HAWKER BEECHCRAFT CORP Model BEECHJET Series 400A 2. Owner Name (As shown on registration certificate) FLIGHT OPTIONS LW SHMITKA AIR INC SOUTHEASTERN MILLS INC r AL Address (As shown on registrabon cartilage) beam 16100CorisAWVI Mom City Pactoncod HMOS* au ON by 441124432 Counts USA 3. For FAA Use Only - 4. Type • • . 6. Unit Identification Repair Alteration Una Make Model Social No. Ni' O AIRFRAME (As described in Item 1 above) 0 • POWERPLANT 0 0 PROPELLER MI O APPLIANCE 1)be Manufacturer 6 Conformity Statement A Agency's Name and Address B. Kind of Agency novo pat. Stan SIC U. S SedtAC.310ditecnanic I Manuracturer Adds* 27 Lo* Orls•Sai • Foreign Cen.reted SWAM< C. Certificate NO. Car Isnainta Sams Mt CAttlifiCaSted Sepia Station DJFA206D tip Ixo, Contu, USA X Certificated maintenance 0rgarezabat Cl. I certify that the repair and/or alteration made to the unit s) dentified 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. FederalAviation Regulations and that the information tumefied herein is true and coned to the best et my knowle ge. Extended range fuel per 14 CFR Part 43 O App. B Signature/Date of Authorized Individual Brian Kenya dire/ it 3 - i t d' ° ii T. Appr for Return to Service P rsuant to the authority g ven 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 n . BY FAA Ft Standards Inspector Manufacturer X Maintenance Organqation lll Rejected Polon. Approved by Camden Doman:nem ot Transport FM Designee Repair Station Inspection Authorization Oth r (Specify) FLIGHT OPTIONS 135 AIR CARRIER CERTIFICATE Certificate or Designation No. DJFA 2O6D Signature/Date of Au hotted Individual Brian Kenya_ 46 ...1.4.-i Vededrfi--1, 3- "'JO // FAA Form 337 it 0.C6) SONY_GM_02 755279 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242201 EFTA01327319

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 einvorthineSS requirements. 8. Description of Work Accomplished tit more space is required. attach additional sheets. identify with aircraft nationality and registration mark and de e work completed) USA N493LX SN-244 3/8/2011 Nationality and Registration Mark Date REPAIRED LEFT ELEVATOR IAW US TECHNICAL E05770 226648. 8110-3 DATED APRIL 19 2010 (WORK ORDER # 227277 S0.97) WEIGHT AND BALANCE NEGLIGIBLE INSTRUCTIONS FOR CONTINUED AIRWORTHINESS: FOLLOW NORMAL MAINTENANCE PRACTICES FOR THE ELEVATOR AS CALLED OUT IN THE BEECHJET 400A MAINTENANCE MANUAL XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXYJMO(XXXXXXXXXXXXXXXXXXJ00(XXX)(XXXXXXXXX SDNY_GM_02755280 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242202 EFTA01327320

0 US Deparnern MAJOR REPAIR AND ALTERATION Of TriiMpirlinan (Airframe, Powerplant, Propeller, or Appliance) rodent Aviation Administration Fan, Ar Etearenk Tratitins flurn>tr eroved a s M . 2 I t 0 - 0 0 2 0 11/1:0037 et FAA WO Only INSTRUCTIONS: Print a nit di °tic< See Idle 14 CFR §43.9, Pan 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 Serves 400A 2. Owner Name Address (As shown on registration certificate) mem. 26‘10 CurlimsWned Pi1Mf (As :norm on registration cattalo) SHMITKA AIR INC ELM- SOUTHEASTERN MILLS INC CO FLIGHT OPTIONS LIC ASCENT II LLC PRImE TPALASSOCIATFS I LC cu, ilictimare Magnet Star OH no 411424453 Ca-ray USA 3. For FAA Use Only 4. Type 6. Unit Identification Repair Mention Unit Make Model Serial NO. El/ K O AIRFRAME (As described in Mont 1 above) . O POWERPLANT 0 0 PROPELLER El O APPLIANCE Type AlanulaCtagef 6 Conformity Statement A. Agency's Name and Address B. Kind of Agency Haat no% open tut U. S. CiffbfiCated MeCtene I Manufacturer Menu Mau Divs. Sias a Anti tat6catod Mechanic C. Certificate No. City ilnansmorm Sus We CertifiCale] Renoir Station DJFA206D IP ia204 Cater USA X Cactiacmcd 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 Indirndual 71,4444-1 / 7/ / /40.•'/,'"i2O/0 7. Approval Return to SWIG Pursuant to the authority given persons specified below, the unit dent in item S was inspected in the manner presented by the Administrator of the Federal Aviation Administration and s Approved 11 Rejected BY FAA Flt Standards Inspector Manufacturer X Maintenance Organization Persons Approved by Callltrill °enactment or Transport FM Designee Repair Station Inspection Authorization Other (Speedy) FLIGHT OPTIONS 135 AIR CARRIER CERTIFICATE Certificate or Designation No. DJFA 206D Sgnature/Dale of Au horized Individual 761. 44-6-7 .e.vf ilifervt-1,4 1O - J., - c)0/0 FM Form 337 tio-cot SDNY_GM_02755281 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA _OO2412O3 EFTA01327321

NOTICE Weight end 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 Wort Accomplished (If more space is required. anacI additional sheets. Identify with aircraft nationakiy 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 E05938 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 XXXXXX)0(XXXXXXXXXXXXXXXXXXXXXXXXY=XXX)0000(XXXXXJ000(XXXXXXXXXXXXXXXXXXX 0 SDNY GM 02755282 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242204 EFTA01327322

0 MAJOR REPAIR AND ALTERATION IA Ospertnirl {Skews:4Sn (Airframe, Powerplant, Propeller, or Appliance) 'Sind AvIallon ASInkiration Form Aqvanxi Otie No 21200020 MIMI i Marcos !mare Mu ter of FAA Us•Only INSTRUCTIONS: Print or type all entries. See T. 14 CFR §434. Pan 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for Instructions nd disposition of this form. This report is required by taw (49 U S.C. §44701). Failure to report can result in a civil penalty for each such viaticum. (49 U.S.C. §41330.1(e)) 1. Aircraft NebOrlality and Registration Mark USA N493LX Serial No. RK - 244 Make RAYTHEON AIRCRAFT COMPANY Model BEECHJET Series 400A =Owner Nam (As shown on registration certificate) AIR GHISLAINE INC SOUTHEASTERN MILLS INC ASCENT II LLC Address (As shown on registration certificate) Awns 251/10 CURTISS WRIGHT PARKWAY ay RICHMOND HEIGHTS sus OHIO _ _ so 44143-1453 Casty IISA 3. For FAA Use Only 4. Type 5. Unit Identification ROM Alteration Una Make Model Serial No. m n AIRFRAME MS MMedbed in /fern / Mew,/ . . 0 POn€RPLANT 0 0 PROPELLER 0 • APPLIANCE Type mioutaourer S. Conformity Statement A. Agra" Name and AeldriSis 8. KIM of Agency '-'a Fl IGHT OPTIONS I I C U. S Certecated Mechanic I Marofecrwer Midas 27 LINK DRIVE SUITE B Fccelpn Centime Mechanic C. Cerliicate No. cur BINGHAMTON Sils NY Cerlifteled Repihr Station OJFA 206 D be 13904 caw, USA •I Certificated mantenente °Minkel/an D. totality that the repair and/or alteration made to the unit( ) identified in Min 5 above and described an 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 inlormation Mashed Mien Is true and correct to the best of my knowledge. Extended range fuel per 14CFR Part 43 App.8 ■ • Sgnaltiretate OtAuthocrzei Individual RRICHARD EVANS A1„...,:,7,a,..?,:rD Cif ny a O 7. Approval for Return to Service Pursuant to the authority given persons specilied below, the tend klentifed In item 5 was nspected in the manner prescribed by tne Administrator of the Federal Aviation Administration and Is 2 Approved ID Rejected BY FAA Ft Standards Inspector Manufacturer 1 Maintenance Organization Pierian APpreved try Canaan Depertmem of TninspOt FAA Designee Repair Station Inspection Authorization Other (Specify) CertMcale or Designation No. DJFA 2060 Signature/Date of Authorized Indivklual sez57 RICHARD EVANS - _... A.,:0 thr dal Rio FAA Form 337 (wee) SDNY_GM_02755283 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242205 EFTA01327323

SDNYGM02755284 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242206 EFTA01327324

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft rd An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. B. Description of Work Accomplished (amore space is required. meal adoVthanai sheets. ?dismay Mthilifera nalionlgeY and regisrmtion mad( and date wadi aombraterl) USA N493LX FEB 04 2010 Nationality and Registration Mark Date 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/A/VV HBC MAIN LANDING GEAR HEAT SHIELD COVER KIT 128-1002-0001 SERIAL NUMBER 137 AND ENGINEERING ORDER M32-10108-023 REV. A DATED 11-13-08. WEIGHT AND BALANCE NEGLIGIBLE. INSTRUCTIONS FOR CONTINUED AIRWORTHINESS: INSPECT THE HEAT SHIELD BLANKETS AND COVERS WA/IN FLIGHT OPTIONS INSPECTION PROGRAM OR THE MANUFACTURES INSPECTION PROGRAM AS APPROPRIATE. END Additional Sheets Am Attached FAA Form 337 pool) SDNY_GM_02755285 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242207 EFTA01327325

SDNY GM 02755286 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242208 EFTA01327326

OWED MAWS OF AblEFOCA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE I NATONIADYN40 2 ILANUMCTURFAANDICOEL 3 AIRCRAFT SERVE. 4 C.ATEODRY REOSTRATIONIMOM MUM Rav 'hr .. c AfttrTf ': Co. 6 000 Tr7 - ^ - rrt 6 AVIDOR/TY AND $* FOR ISSUANCE 11i enollees@ Wilke* le twee paant to IN Pear& Arleta Pa AN obliges tat es of De des of hone. the NANA to vitro. awed Dee been InetieSsil eta ParOtocontennlotir lypiCierilket• theeelot to be in stobn kw este meas. al hes been Owen to reset the 10017ente. d CAS nolcstes orrenneneve end dead ainicoNnele ewe et ported bytemet ID M Casolanon so SiOstneesralCASI Arietkon except as toed beret Oesteese- Hen? IMAMS COSOrtierts Unto eon dierenclansi. suspended. motet or • tentifreson dee Y otenwee stable:sod by lie beefless. ON illrotellOnse• etellpiele awes es to •• Vie Ma nUed^:* iniaMityfee. ew slinacns are porkwoodflocaldne•Wth NM 21.43. est el We hears Melon Regolatiosi. u e OpW. end We elven Y Neekeed h the UMW SNOW DATE OF OSUANU IC/01/1902 row SC.' Perez DASONAllem MAUER eireern. apoNeext. watileae NM MISS Nerbeselseble to• retemeeene OEMs kopecrotinimeesease 3 pea as lIa CEROACATE WET SE 001PusfED el Tell NICANN NACCOIDINCE MTN OPPLICNRE NAATCOI REOULAICell FAA Fenn $100.2 Ga) umIto sto Es or wee. DEPARTMENT OF TRAOSSPOTTATON—FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE I. AATIONINJTY NC 2 WOOPACNONA Ate MOOD. 4. CATEGOON • NECIAORAVONWANCE . RAYTHEON AIRCRAFT COMPANY N793TA 400A RK- 244 TRANSPORT 's AvTICaTv AND SASS MA ISSUANCE TmeanorVineleCenineests issued punieem iotAttleowstAseten sag ittyiesietteste. pet nos 'se Oeie o/ essence ire • *eon to elAbA WWI MI Nrr 0•0•000 an] found w cottion• to IN Nee vaislicsie weeks. to es o casco lot see *OWNS/ WO hips Nen gap pm betel IN moan "mins Crt IN aDOCIOis cationonesso• toe .Mend avo.ovisness code is • wooded t. kw. to IN Cetera. on lowneinAsi Cod ...vomiting is NA*0 feet Estegecre Na st 3 ANCRAFt VIDAL Nut4601 r (Fen MO CONOMONS Limns wow sotteneenes wawa* moo*. es • wenosion awe ts aterots• tnettisead by Pie A0"""M•10( 0" enRoll.•••• C01.1Cal• 4 elects* se boo ei we IlybeinnOt rihrtillim. Maiintieriant• NO Nene its Pinioned o KONOtoc• is4APates2 I.43 nil 44 VW Fare &neon eguisteAl. 4•00400.44e. ins IN erne 9 •024101•0 al me owl Sa -.1 i . . s DAVAO. ISSUANCE IDA10/01/99 r epts 0 81!. ; wRi t • i 'l.h.c.F.1,2t OEsOmoom NUMBER ACE—FWD - 07 Any earpolco teetedookel. *reseal of Mounds:eta ess be Ossien•biebv• MwneWeebq MOD a tAIVA0'.. ." 0101‘.."6 3 • NNE et bah Teel CERIVICATE MUSE BE DISPUTED iN THE micamIT N ACCOMANCE WITH APPUCABLE IEOEAK WIATION AEOuuiliCe4 ram 610t.-2 sem • - Ud 0.010101$ SAO _ - SDNY_GIvl_02755287 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242209 EFTA01327327

SDNY_GM_02755288 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242210 EFTA01327328

SITITO SIAM 01 aliOeCA 0.EPARTP4 ENT OF TN OrkSPORTATION-FEOBIAL AVIATION AOSSIN16TRATCON STANDARD AIRWORTHINESS CERTIFICATE I NATIONALITY Awl) RE.G5TAATION aaa N793TA EVJ4PACIUPER MC 1•000. RAYTHEON AIRCRAFT COMPANY 400A 3 NACAAn SEP.AL (4 CATIGORY wvant RK-244 I TRANSPOFtT S. Assisioisitt AAO SASS FOR iSayilics Tim ginnwswea caNiciss he/veldoutman la ia isclonal AvIrcv, Ad a 193(Ism3 MHOS mas. e•sthltsdsbs 01. liUmin Int ^- a-ansl tl .Miff NONNI Wen rend in, gc•ra to conform to int type mutat, trestr. W t• M tonfica sot SU olfeltlort t,W ha Mon el(Per 10 'MS tie ICV FrersnlIbtillit swamis ccarshasom Ofiggle0 nortAinssi CPS Li by An a.O w the caarsaa on inuntoral Gnt AaVon. ItA NV at Wald herta fatnger. NONE TERNS AND OCNotTIONS UnIS seat Iliew‘lend susoadso. carped eta !errnarepuert aa is Ow**, snalashso in OR Marano/. GM alroalmAss clan* is Otani a tog -as as maimasnos. CowefiLabvi M.--asitet•Ca. PIO SOWS h ratbrwed sane* whhPoltsii.43. SI a ma Fans Am stiOm squInarts es salsottmaS. rd V...rfaf 9 M.I•'nd d'IMUrage SLAP On OF dIELIANCR DESIGNATION MASA R-10/01/99 ACE—FSDO-07 AT, alletate.notedueGott of marine Onlfaukpl.rayln luNsiala ITO/Nag sosmoNng$15:06. Consc r4nQ4.PMndilg0 ' yam co bah Tsn5 cZATinOTE MIST St OtSALAY/0 IN, Till AMMAR Pi AILCC0R0MMGC Wrrft APPUCAtli IEDCUL °NATION AtOk.A.AT IONS. . . , • -or - gtet tbitt • $ 0.P.Orliel Mae • SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, SDNY_GM_02755289 15, and 17 EFTA_001411I I EFTA01327329

Z SDNY_GM_02755290 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242212 EFTA01327330

Cc-iJL12--i-faz it3-4r) O' . MAJOR REPAIR AND ALTERATION Form us oePsmwr or (Airframe, Powerplant, Propeller, or Appliance) ripaintswition Awrissinikw Approved OMB No. 2120-0020 For FAA Use Only Office Identification 3 -1.—l. q.-C-71. • F-sao -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 penally not to exceed $1 ,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Reecheraft Mode! 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 Options LLC 26180 Curtiss-Wright Pkwy Richmond Heights OH 44143-1494 3. For FM Use Only THE TECHN CM. DATA IDENTIFIED HEREIN HAS BEEN FOUND REQUIREMENTS AND IS HEREBY APPROVED FOR USE ONLY TO-CONFORMITY-INSPECTION-BY-KPERSON-IN-14-CFR PART APPROVING INSPECTOR 30 JUN 2004 _TIATE AFA FPJXI 71 TO COMPLY WITH ON THE A E8 -43:7: - APPLICAB ftWORTHINESS IB A RCRAFT. SUBJECT - 4. Unit Identifies 5- Type Unit Make Model Serial No. Repair Alteration AIRFRAME described in I ro X (As m 1 above) POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B Kind of Agency C. Certificate No -ythu ii. tivAr"." CIO Fight Options LLC 26180 Curtiss Wight Pkwy. Richmond Heights, OH 44143 a U.S. Certificated Mechanic iii ?? , 7 SP 42.52 $/.5- 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 Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowiedge. Date AP- —0247--65/ Signature of Authorized Individual .--1--- ----- .n.------ -- 7. Approval for Return To Styles Pursuant Administrator BY to the authority given persons speofied below the unit identified in item 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and is frj APPROVED 0 REJECTED FM FN. Standards Inspector Manufacturer Inspection Authorization Other (Specify) A, ecot . edi ti (O4 flee :\ FM Designee Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection /02 /9 glO it Certificate or Designation No. tcA2O6L Signal e of A thorized IndAidual . a...-0 PIA roan !II emit SDNY_GM_02755291 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242213 EFTA01327331

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 confonnity with the applicable airworthiness requirements. 8. Description of Work Accomplished fit more space is required. attach additional sheets. Identify with aircraft nationality and registration mark and date work viliffdeted) 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 009-18000.00I Current Revision Installed Goodrich Avionics Systems Landmark TAWS8000 system (TSO-CISla Class B) using Flight Options LLC electrical drawing 400-3446-20-01 and applicable manufacturers installation manuals listed above. This Installation inctudes the optional Terrain Display function. not FM Approved Flight Manual Supplement 400-3446-240k be &craft when the Class B TAWS 8000 system is in use: The TAWS 8000 system has been preview* approved for muddle Bendel aircraft under STC ST01881CH-D. with the Terrain Display function enabled. This installation has been impeded and found to conform to the operational and technical characteristics of STC ST01881CH-D with minor deviations in location of switching relays and weird interface points as depicted on Flight Options LLC drawing 400-3448-20-01. Similarity to STC ST01881CH-0 is the basis for this request for held 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 13.2A, 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 manuals) weed above, wire bundles were fabricated using MIL SPEC, Tefal wire, that mats the acceptability requirements of AC43.13-18. Chapter I I, Section 7, Paragraph 1145 (a) saidira (b), Paragraph I I 48, and paragraph 11.89 All wiring was masked in accordance with AC43. I 3-ID, Chapter I I, Section 16. Para 11.206, 11.207, 11.208 (a) andthr (b) and I I-210 (a) and (b) Individual wires were formed into bundles by lacing and lying using the techniques described in AC43.13-I B, Chapter II. Section 12, paragraph I I-158 (a) and (b) Cables were routed and secured in the aircraft using AC43.13-18. Chapter 11, Section 8, Para 11-96, (a) through (gg) as a guide. An electrical load analysis was performed per AC43 13.1 B Chapter I I Section 3 Paragraph 36. The maximum probable continuous decimal load don not exceed 80% of the genaatods) output capacity MI 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 airworthiness (ICA) for this aircraft alteration and Interfacing components are as follows; (I) Introduction to the aircraft altered Is explained above. (2) DesedpUOn of the major alteration is explained above. -(3) -Operation in.ormation is described in the documents listed above fee each particular product - - - - — - - (4) 54`rVICIng. (4) 0latireffIS and access pines, Manacle Inspection rsoulramenta (101 Application of protective treat-manta (11) pre, (12) Vat of Spacial Tools. ( 14) Recommended Overhaul Periods. and (IS) Airworthiness Pmilatlon section are not applicable. (5) maintenance, (s)trouseddoono infomtitIon (7) Removal and Replacement. and 031 for commuter category aircraft of the products listed, will be lAW tie appropriate and current manufacturer, Installation manuals. (II) Reyeslon will be in accordance with the manufacturers' maintenance manuals and submitted tome loCal FSDO. Antennas and other parts and materials installed such as wiring, circuit breakers, switches, annunciators, clamps, doubler>, shelves, and racks will be Inspected In conjunction with the Raytheon Beadier 400A, Phase C Unseat-Pon program, for condition, security of attachment, evidence of damage, and normal operation IAN, FAR 25.1529 andlor applicable manufacturers service Instructions 0 Additional Sheets Are Attached 'U. S GPO 1994.568-012/00019 SONY_GM_02 755292 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242214 EFTA01327332

JAN 03 2005, C . • MAJOR REPAIR AND ALTERATION ., (Airframe, Powerplant, Propeller, or Appliance) near Avtmon ACI ISAMISOA Form Approved OMB No. 2120-0020 For FAA Use Only Office mange:aeon Xi- AZ14 '• PS OO -2 3 INSTRUCTIONS. Print or type all entries. See FAR 439. 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 N7937A . 2 Owner Name (As shown on registration certificate) NORTH CHANNEL LLC Er-AL. Address (As shown on registration certificate) CIO Flight Options LLC 26180 Curtiss-Wright Pkwy Richmond Heights OH 44143-1494 3. For FAA Use Only - - - - 4. Unit Identification 6. Type Unit Make Model Sena! No. Repair Alteration AIRFRAME described in X (As fern I above) POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Con ormity Statement A. Agency's Name and Address B Kind of Agency C. Certificate No. Lynn H. Huyen C/0 Flight Options LLC 26180 Curtiss-Wright Pkwy Richmond Heights OH 44143-1494 X U.S Certificated Mechanic ASP 278825845 Foreign Certificated Mechanic Certificated Repair Station Manufacturer D. I certify that the repair and/or 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 /*P- —02 ..2- — o 57 Signature of Authorized Individual .7„----- -- / 1I-------______ 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 In APPROVED 0 REJECTED FM Flt Standards Inspector /1 1 Manufacturer Inspection Authorization Other f r l ;O.4A er 6.1Y-filee4 FAA Designee Repair Station Person Ap by Transport Canada invort ness Group Date of Approval Rejection l er ilb 8119 4/ Certificate or Designation No / ATFPOA h Signal of hoed lndi ual n .. . /7.---- ----- WA AP MA SDNY_GM_02755293 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242215 EFTA01327333

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 12-22-04. Aircraft weight and balance and equipment list data have been revised. END O Additional Sheets Are Attached S GPO 1994-568-012/00019 SDNY_GM_027 55294 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002422 I 6 EFTA01327334

I O MAJOR REPAIR AND ALTERATION US Owervron, a (Airframe, Powerplant, Propeller, or Appliance) FosUN A.,Woo wwwwww Form Approved OMB Na 2120-0020 For FAA Use Only Office 6-401- 773e------- subsequent revision thereof) for can result in a civil penalty not INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or instructions and disposition of this /OM. This raped is required by law (49 U.S.C. 1421). Failure to report to exceed 51600 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. (Now Maine (As shorn on registralion oerfilicale) FUGHTOPTIONS Address (As shown on registration certificate) 26180 CURTIS WRIGHT PARKWAY RICHMOND HTS OHIO 44143 3. For FAA Use Only 4. Unit Identification a. Type Unit Make Mode: Serial No. Repair Alteration AIRFRAME ((suited In stem 1 X (As POWERPLANT PROPELLER APPLLANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. CLASSIC INTERIOR COMPLETIONS INC. 355 RICHMOND ROAD CLEVELAND, OHIO 44143 u.S. Certificated Mechanic R4GRO31Y Foreign Certificated Mechanic X Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the und(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 that the information furnished herein is true and correct to the ties of my knowledge. Date 12-10-2004 Signature of 7. Approval for Retain To Ss foe Pursuant Administrator BY to the authority given persons specifiedhelow the unit identified in item 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and is ES) APPROVED I:l REJECTED FM FtL Standards Manufacturer Inspection Authorization Other (Specify) RECEIVED FAA Designee X Repair Satoh Person Approved by Transport Oate of Approval 12- or Rejection 0-2004 Certificate or Designation No. R4GRO31Y __ Signature of Authorized Individual DEC 16 ess_aps 2114 IAA pall/ On" SONY_GM_027 55295 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242217 EFTA01327335

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 Of more space is required, attach additional sheets. Ideal), 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) R/H Galley 2) a) Assembly drawing SM6G-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 O Additional Sheets Are Attached tu.S.DF0:1994-568-012100019 SONY_GM_02755298 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242218 EFTA01327336

0 MAJOR REPAIR AND ALTERATION US Denwlmen or (Airframe, Powerplant, Propeller, or Appliance) Fedora, kelallea Adminisiration la Form Approved OMB No. 2120-0020 For FAA Use Only afAuccsno subsequent (23 thereof) can result it for penalty not INSTRUCTIONS: Print or type all entries. See FAR 43.9. FAR 43 Appe dix 8. and AC 43.9-1 (or instructions and disposition of this form. This report is required by law (49 U S.C. 1421). Failure to report to exceed 61.000 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 Hawn on registration certificate) SAMAIR INC ET-AL Address (As snow; Orr registration certificate) 101 S WEBB ROAD WICHITA, KS 67207 3. For FAA Use Only THE TECHN CAL DATA REQUIREMENTS AND TO CONFORMITY IN DATE 7..SlOS IDENTIFIED HEREIN HAS BEEN IS HEREBY APPROVED FOR USE SECTION BY A PERSON IN 14 CFR APPROVING INSPECTOR AEA FSDO 23 FOUND TO COMPLY WITH APPLI r THINESS ONLY ON THE Al C SUBJECT PART 43.7. Ca..- 4. Unit Identif teat . Type Unit Make Model Serial NO. Repair Alteration AIRFRAME deSCribed u) item 1 above)-- -- X — (AS POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address 8. Kind of Agency C Cart icate No. STEPHEN J. MAIDEN C/O FLIGHT OPTIONS LLC 26180 CURTISS WRIGHT PARKWAY 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 units) identified in item 4 above hereto have been made in accordance with the requirements el Part 43 of the U.S. information furnished herein is true and correct to the best of m knowledge. and described Federal Aviation on the reverse or attachments Regulations and that the Date JUNE 10, 2003 I Signatur I Authotiz nd 7. Approval for Ret n To e ice Pursuant Administrator BY to the authority g wen persons specified below the unit identified in 4 was inspected in the manner prescribed by Ibe of the Federal Aviation Adminisiration and is Xi APPROVED 0 REJECTED FM Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) OPTIONS FLIGHT SUPPORT, INC., dMa FLIGHT OPTIONS FM Designee Repair Station Person Aopeoved by Transport Canada Airworthiness Group Date of Approval or Rejection JUNE 10, 2003 Certificate or Designation Ni) DJFA206D Signature of ' nodual r za.,4:2 KEITH GAwSYS2Awsm IAA form )47 VI Ail SDNY_GM_02755297 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242219 EFTA01327337

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible, with all prewous alterations to assure continued conformity with the applicable airworthiness requireMONS. 8. DescrIptioie9Work Accomplished (If more spate. 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 It 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:1994-568-012/00019 SDNY_GM_02755298 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242220 EFTA01327338

13 y r JUN 2003 0 MAJOR REPAIR AND ALTERATION US 07Nrmre or (Airframe, Powerplant, Propeller, or Appliance) FedwalArletion .74nInIstralion Form Approved OMB No. 21200O20 For FAA Use Only Office Identification sairmAcrvF iSpo r can result in l penalty not INSTRUCTIONS: Print or type all entries. See FAR 43.9. FAR 43 Appendix B. and AC 43.9-1 (or Instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report lo exceed 51,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make RAYTHEON Model 400A Serial No. RK-244 Nationality and Registration Marti USA N793TA 2. Owner Name (As shown on registrabbn cedificatel SAMAIR INC ET-AL Address (As shown on registration certificate) 101 S WEBB ROAD 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 00 FLIGHT OPTIONS LLC 26180 CURTISS WRIGHT PARKWAY RICHMOND HEIGHTS, OH 44143 X U.S. Certificated Mechanic A297605039 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 hereto have been made in accordance with the requi ements of art 43 of the U.S. Federal information furnished herein is true and correct to the best of y noiMedge. and described on the reverse Aviation Regulations or attachments and that the Date 10 June, 03 Signet r f Authorized t I I`) 7. Approval for Rote To ce Pursuant Administrator BY to the authority given persons specified below the unit identified in it 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and is K) APPROVED 0 REJECTED FAA Flt Standards Inspector Manufacturer Inspection Authorization Other (Specify) FLIGHT OPTIONS LLC AIR AGENCY CERTIFICATE FM Designee Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection 3 u v-e.: to, 2003 Certificate or Designation No. DJFA20613 Signature of Auth ivIdual ? 4.5 c ) (6,e CAtetySTAuSei MA non nf OM. SDNY_GM_02755299 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024222 I EFTA01327339

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. ICI 8. 0401k Aedninthed Of more spaciriseequired. attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) INSTALLED ROCKWELL COLLINS. INC.. SUPPLEMENTAL TYPE CERTIFICATE eST00881 WI-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 It ST00681WI-D. AIRCRAFT FLIGHT MANUAL SUPPLEMENT INSERTED INTO AIRCRAFT FLIGHT MANUAL. NO CHANGE TO WEIGHT AND BALANCE. FAI) 0 Additional Sheets Are Attached *U.S.GPO.1994-568-012/00019 SDNY_GM_02755300 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242222 EFTA01327340

"Unita' *sin of Am:veto Pepartment of transportation — 'bruit (Ablation ,Abministration Supplemental Zgpt Tertifirate emeiimat o;immalle. ../Yeineet9,/e ST0088I WED Rockwell Collins, Inc. 400 Collins Road NE, MS I64-100 Cedar Rapids, IA 52498 rerseOrd dab& deer. e.• efewjant A. £6, rteM, remlerl mai £6 dMuir.feism sad 'wax: ae..-1••• NJ +NervAnaereser teal ;Nevraennia irreitineeissa syea., • a • ..Yerres/eivia. esvitirtrthwd&ce Tr. 2::•,./.0ktrAt &yaw • • See attached FAA Approved Model List (AML) ..405544- • No. ST0088 I WI-) for list of approved airplane models and applicable airworthiness regulations rieue.orlshe ..91im Aitifira tier: Modification of Collins TCAS II 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 1TR-921 or. Collins TTR-4000 Change 7.0 TCAS 11 Receiver Transrniner and optional TPR-90I in accordance with Collins Installation Instructions as listed on AML No. ST00881W1-D, Revision or later FAA approved revisions. • I) 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 detemuned by the installer. (3) A copy of this Certificate and FAA Approved Model List (AML) No. moan WI-D issued June 30, 2000, or later FAA approved revision, must be maintained as part 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 to use this certificate to alter the product, the holder shall give the other person wnnen evidence of that permission. .WM mm'Aork remit atvennes4t dm* sza remora tymmessesimitenneM jol mate, dmortvo4eret aeAreaded vsier‘ ertstmaMmerivr silk Al na rmenta• eurfresetiane4 £4 ...'emomine4/ealre 144 ..av emeetAsver/eivs (doh rtyrefort.fra June 29, 2000 tylkiesetaht AMC 30, 2000 Yl.rt• stenenolove.• July 14, 2000, December I, 2000 Anwesew hyst .42. John S. Bo Administrator, DAS-500864-CE Mite) My of are eeeeeee met is mot shselrey •Tt or sot avowing ILK& or M.:Ammar sot Wendt. 1 nom or mu. no MTN 0110.3i10-04) IMCS I My m ilanteefId L anefdana with OS A.O. SDNY_GM_02755301 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242223 EFTA01327341

I SDNY_GM_02755302 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242224 EFTA01327342