EFTA01326943

UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE 1 NATIONALITY AND 2 MANUFACTURER AND MODEL 3 AIRCRAFT SERIAL 4 CATEGORY REGISTRATION MARKS Raytheon Aircraft NUMBER N188TS Company 400A RK-244 Transport 5 AUTHORITY AND BASIS FOR ISSUANCE This airworthiness certificate is issued pursuant to 49 PROT769. § 44704 and certifies that, as of the date of issuance, the aircraft to which issued has been inspected and found to conform to the type certificate therefor, to be in condition for safe operation, and has been shown to meet the requirements of the applicable comprehensive and detailed airworthiness code as provided by Annex 8 to the Convention on International Civil Aviation, except as noted herein. Exceptions: -Nonextoz/tt/Aem 6 TERMS AND CONDITIONS Unless sooner surrendered, suspended, revoked, or a termination date is otherwise established by the FAA, this airworthiness certificate is effective as long as the maintenance, preventative maintenance, and alterations are performed in accordance with Parts 21, 43, and 91 of the Federal Aviation Regulations, as appropriate, and the aircraft is registered in the United States. DATE OF ISSUANCE R3/06/2014 Arnold Wolfe,(52:, s4? C,),VAL_. FM REPRESENTATIVE Any alteration, reproduction, or misuse of this certificate may be punishable by a fine not exceeding $1,000 or imprisonment not exceeding 3 years or both. THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. DESIGNATION NUMBER GL-25 FAA Form 8100-2 (04-11) Supersedes Previous Edition SOMIGM_02754903 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 I 825 PROT0 PROT414 EFTA_0024 I 826 PROT1 0 MAJOR REPAIR AND ALTERATION US Otooftrroft a Triespalatten (Airframe, Powerplant, Propeller, or Appliance) Federal ANSI AtiniMalereen erra la 2, 204020 Err SOWOIS Ottarcedt RCN Maw foe MA Use Only INSTRUCTIONS: Print or type an entries. See Title 14 PROT770 §43.9. Pal 43 Amender It and AC 43.9.1 (or subsequent revision thereof) for Instructions and deposition of this form. This report is required by law (49 PROT771. g44701). FaIn to repx1 can resultant:we penally lot each such violation. (49 PROT772. 946301019 1. Aircraft Nationality and Registration Mew UNITED STATES / N188TS Sent No. RK-244 /flake [VICTIM NAME REDACTED] Model 400A Series 2. owner Name (As shoal en regatrarion csrtMcate) THORAIR LLC Address (As shown on nyistration CV: ea) Amen [VICTIM NAME REDACTED] 2218 SANDUSKY Pa" OHIO re 44871-2218 Caret UNITED STATES 3. For FAA Use Only 4. Type 6. Unit Identilleadon - Reese Mention tall Mae Model Serial No. 7 in AIRFRAME PAYTMONeetts./teONAWe (As described M Item / show) me244 POWERPLANT O nPROPELLER APPLIANCE Typo arinurackar 8. Conformity Statement A. Agency's Name and Address B. Kind et Agency Nee. Constant Aviation LLC a a Caritated Methane Altai:barer ram [[VICTIM NAME REDACTED]] Folio CellicM•11A•shanle C. Catificate No. Ph CLEVELAND as. OH 7 Crallaslad Rasa Saari CRS#WC7R348J a 44143 ea ," USA Crailuad Maintananos Oraarristion D. I certify DUI the repair anaor alteration made to the unas have been made In accordance Wm the requremorks of furnished herein is true and correct to the best of my km i Warned In Plan 6 above and described on the reverse or attachments hereto Pad 43 al me U.S. Federal Aviation Regulatens and that the InfomiatIon Extended TIMO0 SI prir 14 PROT773 Put 43 App. 8 fid ar Silkily I Steven A. Watkins 10/04/2019 vat for RMiletitillervice Punsuanl to the authority Administrator of the Federal below. the wit in item 5 Adml end Is 1 eyed nnspected .n Inc manner prescribed by Inc Rejected BY - FAA Ft Standards Inspector Manufacturer Maintenance Organization - Pence* Areemed by Camden Deporiereal al Ming:toe - Other FM Designee MI Repair Staler) neaten Authorization (SPec4 Certi cat or DesVation No CRS# WC7R346J SIgnaturaTM 7 / *Mud David Kerr 10/04/2019 FAA Form 337 (10/06) Page I PROT415 EFTA_00241827 PROT2 NOTICE Weight and balance or operating limitabon changes shag be entered In the appropriate aircraft record_ M alteration must be compabble with all previous alterations to assure continued conformity with the eppricable airworthiness requirements. a. Description of Work Acton"liked pt mote apace brewer:oft attach plcStional sheets. Wen* wth aircraft nalicoally and regiftrallon ma* end dale were Cask* red) UNITED STATESMinn tOAW20I9 Plogioniay and Ribaeleslon Waal DMa Engine Inlet Rivet Repair Installed blind rivets in place of the damaged solid rivets on the lip of the right hand engine inlet forebody assembly part number 541000-004, serial number R0010, in accordance with nextant aerospace engineering order NT-EO-1118-31 rev IR dated 11/29/2018 with FM form 8110-3 dated 11/30/2018. Instructions for Continued Airworthiness: Follow the maintenance inspection practices in the aircraft maintenance manual. Inspection intervals shall remain as indicated in the aircraft maintenance manual or operators approved inspection program as appropriate. Weight and Balance unaffected. Reference Constant Aviation work order CCM-3160 END MAGUS:nal Sews NO needled FM Form 337 (10/06) Page 2 PROT416 [repeated 3 times] EFTA 00241828 PROT3 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION POMMSTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS 1. DATE November 30, 2018 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MARE Textron Aviation 1 MODEL NO. N541000-004 4. TYPE Meal &pia Papaw. MO Forebody Assy &NAME OF APPLICANT Nextant Aerospace LLC Cleveland, Ohio LIST OF DATA IL ICENTIREATION 7 TIRE NT-E0-1118-31 Rev. IR November 29, 2018 Engine Inlet Rivet Repair. data are approved herein. This the data listed above specified by paragraph and engineering data necessary for for the entire repair. --END Notes: 1) The structural aspects only of the above listed approval Is only for the engineering data. It Indicates demonstrates compliance only with the regulations subparagraph listed below as "Appicabie Requirements." 2) This form constitutes FAA approval of as the substantiation of compliance to necessary requirements s Pun Pose or OATA: Englneedng data to support repair procedure for Textron 400A Forebody Assy P/N N541000-004, SIN R0010 under Nextant Aerospace Work Order No.10565.1.1. a APFUCMAI REQUIREMENTS (UM spa seated) PROT774 Tide 14 Part 25.301(25-23], 25.303(25-23], 25.305(eXbXcX25-231, 25.307(aX25-23], 25.801(25-00], 25.803i0b)(cX25-38], 25.605(8)(25-00], 25.807(25-23), 25.609(aXbX25-00), 25.611(25-23), 25.613(aXb)(cX25-00], 25.61%25-23], and 25.625(eXbXcX25-231 10. CERTIRCATION - Under Son Pan la on few above end an nelleen teginimmla el InAlmomnies o Recommend veMed by Senn of the AdmInIetralet end Pt manna MM co,20a4 end emtetione of spinning order 14 CM ached inn illabtal a MVO ben eurrinod In scan:Ince et nalbtolietl teoceOns ale lowellocanolyMe Sunders Used. op/Novel of then dale then dela I OW Trenrere 0 APProve II. SIONATUREMICF DESIGNATED ENE4NEERND RE pRESENTATNEMI 12. DESIGNATION NUIMERS1M 13. CUSSFICATIONNI 0 0j24.4":"...,7: Paul Nodding DERT-410115-CE StrurAures FAA Form 8110-3 (01101 SUPERSEDES PREVIOUS EDITION File Number: H18777-01 Page 1011 PROT417 EFTA_00241829 PROT4 PROT418 EFTA_0024 I 830 PROT5 • nextant aerospace //elimaaRel0 /AMU //RUJORN EO t HM0.111841 I Title: Engine Inlet Rivet Repair ENGINEERING ORDER ARTICLE DESCRIPTION fficlotWodl."401 Team &Won 100A Mast snomen:3 See Ramona - 1 - 711 - Ds parpote cilia E0 Pio aloe for Na raulato of PM web (PM (R7212-540t)of mpqpiste lerpeti• pace d Pe dyne* NM Met (PM: 1620426A0540() al M seine ktel kxstotfastoenet The regal's' te Owomphhed en OM Fal /pre PIN forecdy mean* (RN 1154100X01. Sett R0010). REGULATORY •••••••••pithsoolleaan oar citeilluandllialt Oa erpaanapkid to dIatchomarim 10.6:4 OYES ONO maw OYES 0 NZI let OYES ONO kip.* lerbibtred OYES 0 PO PeWoveliloistIsperesallos OYES ONO Dom ON EOPpleconey Yed might. tudana. tad stremb. Writ ;stoma. Lowniant aorta ION dnledwa a Mc airtellisse aempR OYES MICR ONO pale Cal It El) be exargished bp:aped palm or elarbropereket? MINOR OYES • AP312 • O NO Seism*? MeN,Meld INIWC9r•MONefedeinaltiness7 IMJOR ta iis MINOR ONO Ones IS NAM 0 MCA 0 STC (NI STOWILA 1 towns hiss Dap OYES ONO FMAlffl0VIL ION Elms O mo GENERAL IMIINIONSIO RPM I:O~RIvM Waft m RN Emise MitIM (TwINISbaw) esamstueepas 0 YES 0 NO IleSallainras Met PM N541000004 WI 80010 WO. 10S65 I. i ppm! WO. R we amoval). IOOW (R.1 W0) OperiMes Proms Smdketax CA.1015 REWSION sta. tan Iteran1P. NM INaalaa IR 11129/40l$ Mel Prcpaal NM P. Pmbelimoy RI 10/1/2019 UpiSled b remwe wok number DUMP itm dectike. three is mixt and $110.3 N M Meth NYi P. Awhalsnav Acta. w r MN Remade), P. Awhatheav fall/2019 COaoad By K. Ifenefripi ION/2019 AWInd al , DbakInismd P. Awhelam Pinkhas AYSIIMMOV MII..... , . eve by Mir ION/2019 201t10010•1110 4CW ram No. NT.EOOI IRIPA Pas t 03 This Coconut Is Unconerolf *0 Ono Printed PROT419 EFTA_00241831 PROT6 PROT420 EFTA_0024 I 832 PROT7 nextant aerospace Natinuato //NW //WOW I E0 IfT.E0•1118-31 I Title: Engine Inlet Rivet Repair ENGINEERING ORDER PROCEDURES MN INAPUVO4 Fla 1 Veually inspett the trgle Se! Sp and barrel la arty otw damaged, nisang et loose banners. - II ao *Maw! draepandes are deteceet ecetnue MI Well IS C4101100 bib. - II iaS36:444 descepron we rcte canted Nutt,* ABIOGDOCS ingetabIt / 1414 2 VisuallyAmpect ihe arra rotor a deined in Sub T ask 724t-20420401 a/ Inman Inlemelimel LYE MANTENAACE 144NUAL -F.144-34P III poem reaskin) • II no allialel dscrepaxies wa dettete4 COMMA at remints Sinai toot - Indto,. ones:* se MK COMM Nubia Myopia lonfospilica CO 3 Longs dareplilvats MIMI, in Fgt., I and worn ovkanplably dill cal to teak., tamale men'. makog sure not lo Sage, gin OrPIRIZI ile Welt( kit pill it O 4 F'pacee be lidos alio wissirg Winn tor WY/ion albatrAlax Nat PR4CR3212-5.XX in lau of ncortai sold Nees MS2042104:64X - PinPern hobiby ay 444 mop 13 IS nawbed *MO" at NOM. per Chanyt tenni CA.1015 • Disinvie be careel avie lievei Ix tie anus 13 Is int slam Cheaytka cloosrent CA.1015 • Usip Os aianufullenea nasnandad inalahlte WI Intl tin eimi issianes per OweiyMax (band CA-1015 • Inspect the cargaled MIS loyally to bdiro ether hat bum Woad end Ihe stem has Wad Mt ugh Ito Oat head. Reba Carnytter donna CavIOIS ler Impede. raid tartan. AA .4 4 '••tc., lag -80 - LIMITATIONS Rene INSTRUCTIONS FOR CONTINUING AIRWORTHINESS RCA's) Mow Pt rairisike brredke pylon ii MSS nulnlenence ranuat In pedal .*wis shdl Wein as iniceled in be simnel inanionwics mina °rowan 44444ofilipstkai pommel 42,4044• COMPLIANCE tIMPAR WW1 GP aer 410 A AfOVEMOIMNI)31 N.1,88 7:5 /MOM IOW MAIM itg 2.446/ no OTIAWalsOialla*MOESVRoea..."0.6•100 ook4 /i• 1 14~' CRS, WC7R346J OAT fo/t/i1 En Ma NT4041 /R. A Paget d3 This Neuman. Uncontrolled Once Printed PROT421 EFTA_00241833 PROT8 PROT422 EFTA_00241834 PROT9 [repeated 3 times] nextant aerospace II NSMASIID MOW //MORN ENGINEERING ORDER EO k NT-E0-1118-31 Tttle: Ina Inlet Repair I Figure 1: Damaged Rivet Location on RH Engine Inlet Up (Typical Shown) P. 3 cI3 Form No. NT.E0-01 f Roy A Thls Docua*nl Is Unconirollod Once Prmied PROT423 EFTA_00241835 PROT10 PROT424.914 EFTA_00241836 PROT11 0 US Oen... Tninportallon Powerplant, Propeller, Appliance) now, 21204020 Es 501/201S Ibeeeee TnadneMetiew MAIM OM/ al (Airframe, or foists, Avilitlaa AdministeSs INSTRUCTIONS: Print or typo all entries. See Title 14 PROT775 gag. Pet 43 Appends 8, and AC 43.9.1 (or subsequent revision thereon for instructions and disposition or INS form. This repel Is required by law (49 PROT776. §41701). Failure to report can result in a civil penalty for each such Nankin. (49 PROT777. §46301(a)) 1. Aircraft Nationally and Registration Mak UNITED STATES / N188TS Serial No. RK-244 !make Model 400A Series 2. Owner Name (As shown as registabon caracole) THORAIR LLC Address (As shown on roghbation certificate) Anus PO 80X 22i0 VI SAPOUSXY saw OH 29 14$11 Cony VNITE0 STATES 4. 5. Unit Idendfication (Mt Make Model Serial No. Revak Alteration ii pi AIRFRAME MYIIIIECOMIKOVIT CCIONIf (As Omaha in Man :above) RK-2.11 POWERPLANT PROPELLER APPLIANCE Tee Manaiaret 6. Conformity Statement A. Agency's Mane and Address B. KM of Agency Mao WOW, MAYEN U. S. Garaged Mechanic rasnasons, Ado.. 300110•00.1000 Foreign canelcated Mechanic _j C. Certificate No. oar CUEVEI/J0 Ss OH Centres:[ADDRESS REDACTED]inson CRS# WC7R346J 2* 411411 ow" WNW STATES Z C•finteled Mantionanca Oryanizaton II I codify Met the repair andlet eleretton made to In unigs have been made h =men* with the requirements of furnished Meath tme and eared le the ow et my ko0.04.106. bandied In MITI 5 above and described on the reverse or SttlidifTWES hereto Pad 43 of the U.S. Federal Aviation Regttatkas and that Vie Information ended range bal Ext per 14 PROT778 Pad 43 App. B K Slonare/DetedAul . r #4, Ryan M Landes 10/7/2019 7. proval for Return to Service Pursuant to the authority gNen person speeded below, the wit Wenrtil Adrfilitistr atOr of the Federal ANation Administration and Is j In hem 6 Approved knpected In the mane( presorted by the Relecied BY - FM Fe. Standards Inspector - Manufachrer - Palmas Apiroved by Calm oepartmeni or Tramped r ......., FM Designee 7 Repair Station Inspection Authorizalion (Spray) Cerlificat or Designation No. CRS# WC7R346J SIgnatur died IndMduai David Kerr 10/7/2019 Page I SDNYGivi02754915 EFTA_00241837 PROT12 NOTICE iveighr end balance or operating Nmitafion changes she, be entered In the appropriate aircraft recent M Salon must bbl compatible with aff previous alterations to EISSUM continued conformity will the applicable airworthiness requIreinent*. O. Description of Work ACCOMPlithel pf move sate is Mend. attach 80010701 sheet Wen* hen arced a:steamily and registration met* and date nor* cempreted) UNITEDSTATES/NIWTS 1017/2019 Nalknalltyars3 Raglatelkat Mark Data INSTALLATION OF ADS-B OUT ON PART 25 AIRCRAFT Complied with installation of BHE & Associates, LTD. STC# ST11216DS Installation of Automatic Dependent Surveillance-Broadcast Out on Part 25 Aircraft IAW BHE & Associates,LTD. Master Data List (MDL) number [SSN REDACTED] Rev.G. Dated 8/29/2019. Reference BHE & Associates, LTD. Aircraft Flight Manual Supplement (AFMS) Installation of ADS-B Out on Part 25 Aircraft. Report number [SSN REDACTED] Rev.C. Dated 5/4/2019. Reference BHE & Associates, LTD. Electrical Load Analysis (ELA) Installation of ADS-B Out on Part 25 Aircraft. Report number [SSN REDACTED] Rev.B. Dated 10/9/2018. Reference BHE & Associates, LTD. Instructions for Continued Airworthiness (ICA) Installation of ADS-B Out on Part 25 Aircraft. Report number [SSN REDACTED] Rev.D. Dated 3/19/2019. Weight and Balance: Reference calculated weight and balance dated 10/7/2019. Equipment List: Updated. Reference Work Order: CCM-R3160. END 1dditional Sheets An Method FM Form 337 (10/06) Page 2 PROT425 EFTA 0024I838 PROT13 athee.s.tan efistries /Department efrrampottalint I;21,11cationflivithirtrathn Supplemental Type Cergficate Nailer. ST11216DS 7birenafrateivaedterBHE & Associates, Ltd. 12002 Warfield St. Suite 250 San Antonio, TX 78218 real per tbar at clap is the type juiptfintiefaffenag quad an' Me /inniations onaramennas dm:fitter specified Sena sear tie Onntuteineanrganratenis gifint25 itieFederal Aviation Regulations. Original Product - Tape Ct-rlilicate Numlict: Make: See attached AML Model: See attached AML See attached approved model list (AML) Description of 'Fyn Deakin Clamp:: Installation of automatic dependent surveillance-broadcast (ADS-B) out on Part 25 aircraft in accordance with Master Data List [SSN REDACTED], Revision IR, dated June 29. 2018 or later FAA approved revision. For Instructions for Continued Airworthiness and Airplane Flight Manual Supplement reference the attached AML Limitations and Conditions: 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 the other person written evidence of that pemaission 3. See attached AML for additional limitations and conditions. centfirate and's& supporting data guild is tie earn forappanniderrosoin in Oa unistsurmakrel, suspended snimiafroror a termination fate 4.r allientire andlisitify tendril-mi./Snuffing/tie falinnOnntion indinnairat iota Date of Application: February 9. 2018 Daic or lase:mem Junc 24. 2018 Dam kcissucd: Dow Am-acted: illy /Dina ion tit fidunnistrotar Seraame lit4 VT ORB Aviation Project ODA Administrator ODA-831473-SW My alwaecn of this certecate is eyeshade by a an al nal mewing 51.000. a Iftnicemaril not exceeding 3 yen a torn Pas cormcze may be transfeed or made evadable to third persons by brewing agreements er acepowee with IC PROT779 2147. Possession ulna Supplemental Type Ceder-roe (STC) OeCofrenl by persons order than the STC holier does net cortabbste rights to the design data nor to altar an small aroatl signs. of propeller The STC, supporting documented:a (dramoos. Aetna:We speokatons. figM manual supplements. etc) is the property of nit SIC homer An STC holier who least • person buying STC war an arrcraft awes ,none. ce propener must prove that pe so yam tynnen purression accepts* to the FAA. IRS 14 PROT780 21.120). FAA Form 5110-2 (914) Page 1 o12 PROT426 EFTA_00241839 PROT14 thuitiatatts °amnia apartment 17fransportathn FeafrativiattS/larministration Supplemental 7)Te Cent/lc-ate INSTRUCTIONS The transfer endonernent below may be toed to notify dw appropnne FAA Aixereft Certifieatial Office ache [mien of this Supplernmul Type Cartgkate. The MA will reissue the certificate m the nose of the transfereeand leeward it to him. Transfer'Endorsement Transfer the ownership of Supplemental Type Certificate Number: ST11216DS To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement): eau itraalit *mama Irina: My alleradon e this conthstia 4 punishable by a Me Of flat exceeding 51.000. of Imprisonment not escaertrg 3 yaws. a bath this certificate may be Rfingerred de made AMAMI 30 two Mein by Witernents In accordance with Id CPR 2147. Possession of this Supplemental Type CeMcra (STC) Saturnine by persons at than the STC hart& does not con:A/luta rights 10 the design data nor to stem an stvel, Srget engine. or propeller. The STCh supeoceng eleceneetehen (dnawrtos, ireeeeekee. weeneelehe fight manual supthements, etc) is the property of the STC toblet. M SIC maw wow stows a person lo use the STC b alter an aitheft. shalt engine, a propeller must prova Mt person with erten Permission acceptable to the FM (Ref. II PROT781 21.1201. FAA Form 8110.2(5114) Paget Of 2 SDNY_GM_O2754918 EFTA_00241840 PROT15 DocuSign Envelope a CFB621313.543FE8-4C8D.A4E34461F9B213045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS FOR THE INSTALLATION OF ADS-B OUT ON PART 25 AIRCRAFT REPORT No. [SSN REDACTED] Revision D Date: 03/19/2019 NOTICE: The contents of this document are proprietary to BHE & Associates. Ltd. and shall not be disclosed, disseminated, copied, or used except for purposes expressly authorized in writing by BHE & Associates, Ltd. BHE & Associates, Ltd. San Antonio, TX 78216 USA CAGE: N/A Pero By VT-DRB. FSCM 47MZ7, Snt 1 o139. 2019fMatf19 PROT427 EFTA 00241841 PROT16 DocuSgn Envetope CFS82885-6FES4C8D-A4E3-5461F9820045 NOTICES AND SIGNATURES Notices: Note: Paragraphs andror figure numbers followed by' i" indicate a change by latest revision. Approval Signatures: NAME SIGNATURE Prepared by: R. Zamora See rev IR Checked by: M. Graham See rev IR Approved by: M. Graham See rev IR REPORT No. [SSN REDACTED], Rev: D Page 2 of 36 Red By VT.DRB. FSCM 471127. Sit 2 01 39, 201944.1a/f19 PROT428 EFTA 00241842 PROT17 DocuSign Envelope ID: CFI36211185-6FE8-4C8D-A4E3-5461F9820045 Record of Revisions Revision Number Description of change - . .s. - RevislOn . Date Approved IR Innis] Release 5/9/18 MG A Page 8, Section 1.1 revised transponder and GPS part numbers. Page 10, Section 2 remove 'Flight Hours' horn Table 4 6727/18 MG B Page 4, Revised list of aircraft models in Introduction Pages 9.24-25, 28-29. Revised aircraft models in Tables 3, 7, and 9. Pages 8 and 28, clarified wording for installation. 11/6118 MG C Revised Table 3 on page 9 Revised Table 4 on page 10 Revised Table 5 on page 26 Revised Table 6 on pages 27 & 28 Revised section 6.1.9 on page 31 Revised figures on pages 13 & 20, Added figures on pages 14, 17 & 18 1/18/19 MG D Added STC number on page 4. Added figure on page 24. Revised form form in Appendix C. 3(14lict SHE & Associates, ltd. Page 3 of 36 Red By VT.DREI. FSCM 47M27. Sht 3 of 39. 2019/Mar/19 PROT429 EFTA 00241843 PROT18 DowSign Envelope ID: CF862885-6FE8-4080-a4E3-5481F9620045 INTRODUCTION These Instructions for Continued Airworthiness (ICA) document have been developed using the guidelines in Appendix 'if of 14 PROT782 Part 25 as required by §FAR 21.50 and §25.1529. This document is designed to provide avionics and aircraft technicians with sufficient information to inspect, troubleshoot, adjust, repair, test, remove, and install ADS-B on the following Part 25 Aircraft. Bombardier Inc. - CL-600-1A11, CL-600-2Al2, CL-600.2816 (Challengers) Gulfstream Aerospace -1125 Westwind Astra. Astra SPX. Gulfstream 100, 0150 Gulfstream - G-1159, G-1159A, G-1159B, G-IV. GV Gulfstream - 200 Sabreliner - NA-265-65, NA-265-70, NA-265-80 Textron Aviation Inc. - 500. 550, 5550, 560 (Citation) Textron Aviation - 400, 400A (Beechjet) Textron Aviation - 650 Textron Aviation - HS.125 Series 700A, HS.125 Series 700B, BAe.125 Series 800A, BAe.125 Series 800B, Hawker 800XP. Hawker 750, Hawker 850XP. Hawker 900XP Learjet - 60 (STC Aircraft) Dassault Aviation - Falcon 10, Mystere-Falcon 50, Mystere-Falcon 20-05/D5/E5/F5, Mystere-Falcon 200. Mystere-Falcon 900 Table 1: Equipment Type Description New CPN I Qty DO-260B ADS-B Out TDR-94 Transponder 622-9352.502 0, 1 or 2* TDR-94D Transponder 622-9210.502 0, 1 or 2* GPS1203C GPS Receiver 84327-50-XXXX 0 or 1 CI 429.200 GPS Antenna CI 429-200 0 or 1 GPS-40005 GPS Receiver 822-2189- 004/005/006/007/010/011/100 0, 1 or 2 *Either TDR-94 or TDR-94D will be Installed. The above equipment is installed in accordance with FM Supplemental Type Certificate No. ST11216DS . See the List of Applicable Publications (LOAP) in Appendix A of this document. The publications listed in the LOAP constitute the required information essential for continued airworthiness for the aircraft. The documents contained in the LOAP are a necessary part of this ICA and the latest revision should be available to maintenance personnel when performing maintenance. The STC holder will continue to monitor changes to the ICA that were the basis of the supplementary ICA and provide revised supplemental ICA as necessary. The information in this document supplements or supersedes the original manufacturer's maintenance manual only in those areas listed. For limitations, procedures and other information not contained in this document, refer to the aircraft manufacturer's maintenance manuals, illustrated parts manuals and wiring diagrams or the vendor manuals as listed in the LOAP. REPORT No. [SSN REDACTED]. Rev: BHE 8 Associates, Ltd. Page 4 of 36 Rye By VT-DRB. FSCM 476.127, SIB 4 a/ 39, 2019/MarD9 PROT430 EFTA 00241841 PROT19 DocuSign Envelope ID: CFS62885SFE8-4C8O-A4E3-5461F9B2D045 RECORD OF REVISIONS For continuous use of this document, this document must be maintained in current revision status. Each time the STC holder finds it necessary to revise this document; a revision will be distributed to all users of the STC. Revisions will be supplied to the customer by: a) E-mail with an attached PDF file, or b) Compact Disc (CD) via mail Changes to this document will be incorporated by an updated revision to the complete document. All pages will indicate the "new revision level. Upon receipt of the new revision, the previous revision should be discarded and replaced with the updated, current, revision. Changes to this document will be listed in the revision block on page 3. It is the responsibility of the person(s) performing maintenance on the installed system to ensure that this document is current prior to performing this maintenance. The current revision number may be verified by contacting the STC holder, BHE & Associates. Report any discrepancies to the installation of this STC using the form in Appendix C of this document. Once filled out the form must be sent to both the ODA and the STC holder. Their addresses are as follows: ODA VT-ORB Aviation Consultants 9800 John Saunders Rd San Antonio, Texas 78216 STC Holder BHE & Associates Ltd. 12002 Warfield Suite 250 San Antonio, Texas 78216 Page 5 of 36 Rah By VT-DRS. FSC51 47127. Sht 5 of 39. 2019fhtall 9 PROT431 EFTA 00241845 PROT20 Dzoof$Ign Envelope ID: CFB628B5-6FE8-4080•A4E3-5461F992D045 TABLE OF CONTENTS INTRODUCTION 4 RECORD OF REVISIONS 5 1 SYSTEM DESCRIPTION 8 1.1 GENERAL 8 2 AIRWORTHINESS LIMITATIONS 10 2.1 Inspection intervals 10 2.2 Inspection Program 22 2.3 Inspection Method 22 2.4 Eddy Current Inspection 28 3 MAINTENANCE PRACTICES 29 3.1 Removal/Installation 29 3.2 Access Location 29 4 POWER DISTRIBUTION 30 4.1 Circuit Breakers by Bus 30 5 SYSTEM TROUBLESHOOTING 31 6 INSPECTION REQUIREMENTS 31 6.1 Scheduled Inspections and Maintenance Checks 31 6.2 Wiring 34 Appendix A - List of Applicable Publications Al Appendix B - Special Tools and Equipment B1 Appendix C - Discrepancy Reporting Form Cl REPORT No. 584.00.0047, Rev: 0 Page 6 of 36 fiord By VT-OR13, FSCM 47M27, SIM 6 of 39, 2019/Mar/IS PROT432 EFTA 00241846 PROT21 DoteSign Envelope ID: CR3628115,6FE8-4C8ETME3.5461F9432O04S LIST OF FIGURES AND TABLES Table 1: Equipment 4 Table 2 Equipment List 8 Table 3 Equipment by Aircraft 9 Table 4 Inspection Intervals 10 Table 5 Manual List 28 Table 6 Access Panel Location 29 Table 7 Equipment Installation Locations by Aircraft 29 Table 8 New and Upgraded Equipment 30 Table 9 Maintenance Manual by Aircraft 33 BHE 8. Associates, Ltd. Page 7 of 36 Red By VT-ORB, FSCM 47MI7. Sht 7 of 39. 2019thlar/19 PROT433 EFTA_0024 I 847 PROT22 DozeSon Envelope ID: CF8132885-6FE8-4C80-A4E3-503IFOBADO4S 1 SYSTEM DESCRIPTION 1.1 GENERAL This STC will include installations and/or updates to equipment to allow for Automatic dependent surveillance - broadcast Out (ADS-B Out). ADS-B periodically broadcasts information about each aircraft, such as identification, current position, altitude, and velocity, through an onboard transmitter. The equipment list in Table 2 below details the equipment required for this installation. The TDR-94/94D Transponder(s) will be upgraded to part number 622-9352-502 (94) or 622- 9210-502 (94D), if not previously installed. The TDR-94/94D Transponder is an all solid-state, crystal-controlled receiver/transmitter. The transponder(s) will get the GPS information from either a newly installed Freeflight GPS1203C GPS receiver and dedicated GPS antenna; or, a GPS-40005 GPS receiver. Depending on the aircraft configuration, the GP$-4000/A/S may be previously installed. If the previously installed GPS- 4000/NS is not a part number 822-2189-004/005/006/007/010/011/100 it will have to be upgraded to one of these part numbers. (Reference Tables shown on drawing [SSN REDACTED] for applicable GPS installation based on aircraft model) Wiring is added dependent on the installed or replaced GPS receiver(s). Transponder(s), and annunciator installed. (Reference Tables shown on drawing 584.00.0004 for applicable installations based on aircraft model and subsequent Wire Routing drawing [SSN REDACTED]).See section 6.1.9 for details on inspection. An optional ADS-B Out annunciator can be installed to alert the pilot that the ADS-B function of the active transponder is not properly functioning. The ADS-B Out annunciator is required for all standalone GPS installations. Standalone means the GPS only provides data to the transponders. All 1203C installations and 4000S installations that only connect to the transponders are standalone. It can be installed as an option for installations where the 4000S is used for both ADS-B and FMS navigation. ((Reference Tables shown on drawing 584-00.0004 for applicable ADS-B Out Annunciator installation based on aircraft model) Table 2 E ui ment List Type Description New CPN Qty DO-260B ADS-B Out TDR-94 Transponder 622-9352-502 0, 1 or 2* TDR-94D Transponder 622.9210.502 0, 1 or 2* GPSI203C GPS Receiver 84327-50-XXXX 0 or 1 CI 429.200 GPS Antenna CI 429.200 0 or 1 GPS-40005 GPS Receiver 822.2189- 004/005/006/007/010/011/100 0, 1 or 2 *Either TDR-94 or TDR-94D will be installed. REPORT No. [SSN REDACTED]. Rev: D BHE 8 Associates. Ltd. Page 8 of 36 Rom By VT-ORB. FSCM 47MZ7, SN 8 of 39. 2019N.1419 PROT434 EFTA 00241848 PROT23 ()cooSign Envelope ID: CF/352885-6FE84C80-A4E3-9461F9820045 Table 3 below lists the equipment being installed by aircraft. The aircraft will leave with updated TOR- 94$ or 94Ds depending on the what transponder was already existing. Table 3 E ul ment by Aircraft Aircraft Transponder Installed/Retained/Replaced. GPS Installed/Replaced Antenna Installed Learjet 60 TDR-94s or 94Ds GPS-1203C or GPS- 40005 CI 429-200 Gulfstream Aerospace 1125 Westwind Astra, Astra SPX, Gulfstream 100, G150 TOR-94s or 94Ds GPS-4000S N/A Gulfstream G-1159, G-11598, G-IV, GV TOR-94s or 9413s GPS-1203C or GPS- 40005 CI 429.200 Gulfstream G-11594 GPS-4000S N/A Gulfstream 200 GPS-40005 N/A Textron Aviation 500 GPS- 1203C or GPS- 40005 CI 429-200 Textron Aviation 550, 5550, 560 GPS-1203C or GI'S- 40005 CI 429.200 Textron Aviation 400 GPS-1203C or CPS- 4000S CI 429-200 400A GPS-4000S N/A Textron Aviation 650 GPS-1203C or GPS- 4000S CI 429-200 Bombardier CL-600- 1411 CL-600-2Al2, CL- 600.2816 CPS-1203C or CPS- 40005 CI 429.200 Sabreliner NA-265- 65, NA-265-70, NA-265- 80 GPS-4000S N/A HS.125 700A, BAe.125 800A/800B, Hawker 800XP GPS-1203C or GPS- 40005 CI 429-200 HS.125 7008, Hawker 750/850XP/900XP GPS-40005 N/A Dassault Aviation Falcon 10, Mystere- Falcon 50, Mystere- Falcon 20- C5/D5/E5/F5, Mystere-Falcon 200, Mystere-Falcon 900 TOR-94s or 94DS GPS-40005 N/A Page 9 of 36 Red By VT.DRB. FSCP..1 44127. Slit 9 of 39. 2019rtcladi9 PROT435 EFTA 00241849 PROT24 DoomSign Enveleft ID: CFB628B5-6FE8-4C8D-ME3-5461F9620005 2 AIRWORTHINESS LIMITATIONS The Airworthiness Limitations section is FAA approved and specifies maintenance required under 14 PROT783 H43.16 and 91.403 of the Federal Aviation Regulations unless an alternative program has been FAA approved. 2.1 Inspection Intervals The following items require high Frequency Eddie Current inspections including 2.0 inch detailed visual inspection around periphery of the installation. Inspections as listed in the table below. Table 4 Ins ion Intervals Inspection requirements are for AML fuselage modification Inspection In ervals (Flight Cycles) Detectable Crack Length (in.) Threshold Recurring Fwd bulkhead penetrations 4,000 4,000 0.200 GPS Antenna Installation 6,700 6,350 0.200 GPS Antenna Installation (See Note 1) 5,650 5,400 0.200 Note1: These intervals are applicable to the Textron Aviation Cessna 650 and all the Gulfstream Models The following images specify antenna installation and bulkhead feedthrough installation locations. Page 10 of 36 Rerd By Vf -ORB. FSCM 47MV. Sol 10 of 39: 2019/Marf19 PROT436 EFTA_0024 I 850 PROT25 I 58 I ti00-V.L.43 cr) C co H H n -O O n H H 3D C 3D -O 3D 3D -O Vf • 1 OD LD I - cn P 2lc) co -4 CD - L'S I_a r - 1000O3 I ,41.3 DocuSign Envelope ID: CFB628135-6FEB-4C8D-A4E3-5461F9820045 BOMBARDIER INC. CL-600-1A11 (CL-600), -2Al2 (CL-601), -2B16 (CL-601-3A VARIANT, CL-601-3R VARIANT, CL-604 VARIANT) ACC DOABLE LOCATION TS CS OM USW 0t 47115 SAO 5300 55 rs mm no O MO r'S na rs 29100 I 1":* IS r'S a AS AS 4513▪ 0 T REPORT No. 584.00.0047, Rev: D SHE & Associates, Ltd. Page 11 01 36 Reid By VT-ORB. FSCM 471427, Shill al 39. 2019;161mM PROT26 c581 ti:00-V.Ld3 cn C co H H ITI -o 3D H H 3D C 3D-O 3D G.) -O 0 LO cn P 'O im O su -4 g DowSion Envelope ID: CF862885-6FE8-4030-41E3-548iF9821)045 20.20 TEXTRON AVIATION 400 ACCEPTABLE LOCA11ON IS FS 172.24 196.41 FS [repeated 7 times] 124.61 141 14 71.65 FS 203.35 221.46 240.75 26404 FS 11734 13747 1503.20 266.1 18 S 4 212.40 231. FS 42 250.39 269.69 Ft I FS PRESS WOO I F L js is I 80.91 I 99.02 FS FS 88 96 106.07 :0: 0 hrt , litu REPORT No. 584.00.0047, Rev: D Page 12 of 36 Red By VT-DRB. FSCM 4714Z7, SIR 12 o139. 2019/Man19 PROT27 V) DocuSign Envelope ID: CFB62885-SFE8-9C8D-A4E3-5461F9B2D045 C £ SS I PZOCV.L43 O3 t. O 73 0 0 70 73 V) SO lO N p ,G) U E Ca ) O.; lea TEXT -PON AVIATION INC. 550, S550, 560 ACCEPTABLE LOCATION FS 59.00 FS FS 151.00 179.02 Fs F5 FS Fs 134.00 165.00 94.00 FWD 117.00 PRESS I BLKHD r _I 1 FS 225.23 23 (560) FS 223.40 , id? , FS 216.10 (560 ONLY) Page 13 of 36 Redd By VT-ORB, FSCM 47PAZ7, Ste 13 01 39, 2019/Mar/19 PROT28 V't DaceSoon Envelope ID: CF8628854FE/54C8D-A4E3-5461F902D045 C INSTRUCTIONS FOR CONTINUED AIRWORTHINESS tgi? I ti00-V1-13 co n H ITl -0 0 0 C ITl po -0 po -0 : 3/4400 .93 cn P :4 0_ it, FS 58.00 TEXTRON AVIATION INC. 650 FS 94.00 PRESS 8VHD FS FS 172.00 202.00 FS FS 157.00 187.00 FS FS 261.00 288.76 I FS 00 272.00 I i C: 1 0 1 I I i M l ill I ha SHE 8 Associates. Ltd. Page 14 of 36 Red By VT-DRB, FSCM 47M27, Snt 14 of 39. 2019/Mer/19 PROT29 558 I ti:00-V.L.43 C rn H H -o 0 H nr" H rn 0 0 rn 70 -o 7s G) ,z) -o 1) cn P 2 ,G) co cp_ I_a DocuSign Envelope ID: CFB6288543FE8AC8D-A4E3-5461F9B20045 TEXTRON AVIATION HS.125 SERIES 700A, BAe.125 SERIES 800A & 800B, HAWKER 800XP 67.0 1800 2043 224 • ra MA •I0 11; I Ur 241 Sn • 2822 FICIA ;II ET- (71 1.10 10I0I I I i 1) - 1 I irl n I1 14 n 101.0 two own simony O i l I I I rT 6 - r - - 1 - - _Cr BHE & Acanriates, Ltd. Page 15 of 36 Reid By VT-ORB. FSCM 47MZ7. Sht 15 of 39. 2019/Mar/19 PROT30 cn C co rn H H n -o 7o 0 H rn n H rn 0 31 ci rn 73 -o 73 -o to Co L0 Cn P IC) O CU 958 1 ti00-V.Ld3 33491 DocuSign Envelope ID: CF862885-6FE8-4C8D-A4E3-5461F982OO45 LEARJ ET 60 110.99 17 124.39 151.19 17549 20 .79 232.1 2 274.51 302.59 323.5 r3.3 9 305.11 137.79 FIO r 2 99 F144 Fl p.59I209 F-21 I ;23 90 .57 r• F. 144.59 till 1210.19 197.59 F1S 2 r19 246.59 T3INS1 341143 F204 1 r23 rt4 20.39 riI REPORT No. 584-00.0047, Rev: D Page 16 of 36 Reed By VT-ORB. FSCM 47M27. Sol 16 of 39. 2019iMart19 PROT31 L 58 I ti:00-V1.43 cr) C co n H H ITl 0 H n 0 3D -o 6) -o Vf CO 1n oz lc) SD -4 ca CD_ ,.(f, I_a FRCSs FS FS 145.0 .0 193.0 133.0 rs 1:10 DowSign Envelope ID: CFB62885-6FE8-403D-A4E3-5461F9B2D045 GULFSTREAM G-1159, G-1 159B, G-IV Fs 63.0 BU010 L - P\ - I I I I t _ _ _LS 1 I REPORT No. 584.00-0047. Rev: D BHE 8. Associates. Ltd. Page 17 of 36 Ftefd By \MORD FSCM 47MZ7, Shl 17 of 39, 2019IMart19 PROT32 cn C co H H -to 3D n H IT IT 3D C IT 3D -0 3D -0 Ln 2 3 : D cn oz O co NNAy 858I ti:00-V.Ld3 DocuSion Enveboe ID: CFB62885-6FE8-4C8D-A4E3-5481F9132D045 GULFSTREAM GV FS [repeated 4 times] 157.. S 181.0 205.0 229.0 FS 145.0 1.3.1 I 193.0 217I.0 241.0 FS I FS I FS I FS 63.0 FWD 8U1HO - -Jill T1 n PRESS I 1 I 1 [repeated 5 times] 11 1 1 11 i a .• a =II 1 r- ie a 1 l 'P.41 I I i 100 - a_ 1 II I I. i i i i 1 I i (:( I [repeated 4 times] I I I I I II II - I--i - 1 _i_ p_ _p_ i i I [repeated 5 times] BHE 8 Associates. Ltd. Page 18 of 36 Reid By 1/7-DRB, FSCM 41M17, SIR 18 of 39.201911Am/19 PROT33 6 g2 I VZOCVJ.d3 (r) C co n H rT -0 0 n H rT H 73 ;a -o 73 Gl 73 -0 I O I-' IE E a E.: DoctiSign Envelops I0: CFB628B5GFE8-4C8D-A4E.95461F9B2D045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS r " ri- --- - : T -"- -- I, I II I I I. I I i I ll II / (gggli Ott OO III ( ( OOO t I i -ID,- -144- I Itl--=:-- 1 ii n I III I 1 \''\ II III I III II /: N I I I I I I I I i I li N I II i ii \t i l! III I I I I I 117 1 I I I V H[L LOOKING AFT AT FWD SIDE OF FORWARD PRESSURE BULKHEAD (TEXTRON AVIATION 400) BRE & Associates, Ltd. Page 19 o136 Reif By VT-DRB, FSCM 471.427, Sht 19 of 39. 20i9ThAv/I9 PROT34 V) DowSipn Envelope ID: CFB628B5-6FE8-4C8D-A4E3-5461F9E2D045 C Co .93 to LOOKING AFT AT FWD SIDE OF FORWARD PRESSURE BULKHEAD ZCI (TEXTRON AVIATION INC. 500, 550, S550, 560) O 0 1,1 I-4 IJ 00 O Page 20 of 36 Raid By VT-DREI, FSCM 47MZ7, SM 20 of 39, 2019/Marit9 PROT35 I9SIKOCV.L.43 in C L1.0:1 0 73 0 73 70 70 DD ,93 O 2 0.1 CL it GocuSIgn Envelope ID. CFB62885-6FE8-4C8D-A4E3-5461F9B20045 CAL1191tOOE WAD* , ay.; , .-r4 .17ir ,t, tit tel l ti: tS -it tj.t 41_ rir si ti I • • rh I Tteirh rfi 4. 4 LI 0 oi pp I: 0 j j gMET:EfiftlEF ! I I ' I I I I I le l : I It 4 11\ I I:1 II ;T+4 I: rh 1 44 fprim. -*-174-ditrati- +. 4 41 +. ifolCatshig{q- I I III I I I I 2: -1-r- 0 '....thrietiz r-fit ii-711 i+ E-- I I I I LOOKIC SIT AT FOB SEC OF TOIFORD NOM MOEN (LEARJET 60) REPORT No. 584.00.0047, Rev: D Page 21 of 36 Rohl By VT-DRB, FSCM 47MV. Sht 21 o139, 2019A1ail19 PROT36 DocuSIgn Enveope ID. CFB628B5-6FEB-4C8D-A4E3-5461F962D045 2.2 Inspection Program Perform additional fuselage modification inspections. 2.3 Inspection Method Inspect fuselage skin in the modification area, doubler fastener holes area, using high frequency eddy current inspection techniques, according to the intervals outlined in table 4. The detectable crack length for eddy current inspection techniques Is 0.200'. For the fastener holes, the inspector should look for cracks on the surface of the skin and doubler around the fastener holes. Page 22 of 36 Red By VT-ORB. FSCM 47MZ7.Sht 22 of 39.201917.18:119 PROT437 EFTA 00241862 PROT37 DocuSIgn Envelope ID: CFB8288543FES4C80.04E3•5461F9B20045 LNSPECTION AREA & METHOD FWD BULKHEAD PENETRATIONS typical InstaIlation,shtnvg kspcctions applicable to all PadttatilWiiiitailkiiciai: Ni• "19,4 pcction NefirdSi Eint lldthiS2t11 411Vtigta l l j cry of installation LiNs. tra alit SHE & Associates. Ltd. Page 23 of 36 Red By VTCRB, FSCM 47M27, Shl 23 of 39. 2019/M91119 SDNYGtv1_02754941 EFTA_00241863 PROT38 (locoSago Envelope ID: CF862885-43FE8-4C6D-A4E3-5461F91320045 INSPECTION AREA & METHOD FWD BULKHEAD PENETRATIONS BHE 8 Associates. Ltd. Page 24 of 36 Reid By VT.DRB. FSCPA 47MZ7. $01 24 o139. 20194Am/19 PROT438 EFTA 00241864 PROT39 DocuSign Envelope III CF13628B5-6FE8-4CBD-A4E3-5461F9432D045 INSPECTION AREA & METHOD GPS Antenna Typical Installation sbown"Inspections are applicable to all antenna installations REPORT No. [SSN REDACTED], Rev: 0 Page 25 of 36 ReRI By VT-ORB. FSCM 47M27. SM 25 of 39. 2019iMarti 9 PROT439 EFTA 00241865 PROT40 DocuSogn Envelope ID: CFI362895-6PE8-4C6D-ME3-5461F9620045 INSPECTION AREA & METHOD GPS ANTENNA Typical InstallatiOnshOlit; Inspections arc applicable to all. antenna installations 1111544 ,ta, "fa Learthiz..4 al. i.ioziqnrr.-:z BHE 8 Aqsartates, Ltd. Page 26 of 36 Red By VT-DRB, FSCM 47M/7. She 26 of 39. 20150.ierng PROT440 EFTA_00241866 PROT41 FInfogign Envelope ID: CFB62/995-6903-4C8D-A4E3-546199820045 INSPECTION AREA & METHOD GPS ANTENNA Typical. Installation shown. 100;eetions are 4P01FOle !P. 01 WAAPP1Ps101019FIL ifFcz4R#tioxi:Aita,,o-ilmer tit 93-7.!,....E94..._ . Nif ts. rotr., T -9,:'' 'z realel_.. 4 I ..9.4-# -3.143_. Pat atijt lin g tet0 3 F RICWS4 W i Paa t4 CRIW4 S A4 T J ' 4 4 arcnlnd kmia tle.il. .. 4-41 4 1.4L,4,1" ajcyjnia*FipeirIdt, ygSyt ,t<ti . z...4_,.. Tellie, .1:.! - - zPrr .rpil*:;-: - ..As= a'l. Page 27 of 36 Reid By VT-DRB, FSCM 479427. SN 27 of 39. 20191.4aill9 PROT441 EFTA 00241867 PROT42 DowSIgn Envelops ID: CF1352193.543FES-4C80-A4E3-546 I F9B2D045 2.4 Eddy Current Inspection For eddy current inspection requirements and procedures, refer to the referenced documents in the table below for the different aircraft types. The following documents describe the various procedures and requirements for HF eddy current inspection including personnel, instrumentation, equipment setup and standardization, probes, special tools and equipment eddy current standards, and eddy current test procedures required by the Cessna Aircraft Company. The defects identified by this method are incipient fatigue or corrosion stress cracks in bores, machining radii, shoulders and countersunk holes, and in the actual skin. The direction of propagation defects are perpendicular to in-flight stresses in the case of fatigue stress cracks, or perpendicular to internal stresses for stress corrosion cracks. This method also detects minor corrosion-induced surface damage. Table 5 Manual List Aircraft Manual Document Number • Learjet 60 Non-Destructive Inspection Manual NDI-2 (Chapter 3) Textron (Citation) 500,550, S550,560 Series 500 Non-Destructive Testing Manual 5056ND (Part 6, Chapter 20) 650 Model 650 Non-Destructive Testing Manual 65ND (Part 6, Chapter 20) Textron (Beechjet) 400, 400A Model 400/400N400XP Maintenance Manual 128-590001-9C29 (Chapter 20-80-03) Textron (Beechcraft) HS.125 700A. Bae.125 800A. Bae.125 8008, Hawker 800XP 125 Series 1-800, Hawker 750, 800, 800XP, 850XP. and 900XP Non-Destructive Testing Manual N/A (General Techniques - Part B) Challengers Structural Repair Manual N/A (Chapter 51) Gulfstream G-1159, 6-11598,6- IV, GV Structural Repair Manual N/A (Chapter 51) Oscars' 91, FAA APPROVED: 405,106FIC36743,- Danyl Seow, Project ODA Administrator VT DRB Aviation Consultants A Division of VT San Antonio Aerospace, Inc. 9800 John Saunders Rd, San Antonio, TX 78216 Date 3/21/2019 Vant SW" I Page 28 of 36 ROM By VT.C4iS FSCM 47127. SM 28 of 39. 2019/MaTh9 PROT442 EFTA_00241868 PROT43 DowSign Envelope ID: CF9628BS6FE8-4C8D-ME3-9461F9132D045 3 MAINTENANCE PRACTICES 3.1 Removal/Installation The following installation manuals contain complete, detailed instruction for the installation and removal of equipment. Installation locations for the equipment vary by aircraft, reference tables 6, 7 and 9 for more details on equipment locations and respective maintenance manuals. • Equipment Installation Manual for the FreeFlight System Model 1203C GPS/SBAS Sensor, document 86764, Installation Section • Collins GPS-4000( ) Global Positioning System Installation Manual, document 523-0780545, Installation Section. TDR-94/94D ATC/Mode-S Transponder System (-5XX), document 523-0821492, Installation Section 3.2 Access Location Refer to the Aircraft Maintenance Manuals listed in table 9 (or additional details. Table 6 Access Panel Location Location of Access Access Panels Nose Avionics Bay Forward Nose Access Panels (Right & Left) Cabin EE Racks N/A Instrument Panel & Pedestal N/A Tail Avionics Bay Tail Access Panel Table 7 Equipment Installation Locations by Aircraft Aircraft Transponder Location GPS Location Learjet 60 Nose Nose (GPS-4000S) Cabin (1203C) Gulfstream Aerospace 1125 Westwind Astra, Astra SPX, Gulfstream 100. 6150 Nose Nose Gulfstream 200 Nose Nose Gulfstream G-1159, G- 1159A, G-11598, G-IV RH EE Rack, Cabin RH EE Rack, Cabin Gulfstream GV LH & RH EE Rack, Cabin LH & RH EE Rack, Cabin Textron Aviation 500, 550, S550, 560 Nose Nose Page 29 of 36 Reid By VT-DRS. FSCIA 471.427. Sht 29 of 39. 2019Staf/19 PROT443 EFTA 00241869 PROT44 DecoSign Envelope ID: CFB628435-6FE8-4C8D-A4E3-5461F9820045 Aircraft Transponder Location GPS Location Textron Aviation 400/400A Nose Nose Textron Aviation 650 Aft Cabin Nose (GPS-4000S) Cabin (1203C) Bombardier CL-600-1A11 CL-600-2Al2, CL-600-2816 Under Floor, Cabin Under Floor, Cabin Sabreliner NA-265-65, NA-265.70, NA-265-80 Nose Alternate: FWD EE Shelf Nose Alternate: FWD EE Shelf Textron Aviation HS.125 700A/7006, BAe.125 , 800A/800B, Hawker 750/800XP/850XP/900XP Nose Alternate: AFT EE Shelf Under Floor, Cabin Alternate: AFT EE Shelf Dassault Aviation Falcon 10. Mystere-Falcon 20- 05/D5/E5/F5, Mystere- Falcon 200. Mystere-Falcon 900 Nose Nose Dassault Aviation Mystere- Falcon 50 Nose Nose Alternate: Aft Avionics Shelf 4 POWER DISTRIBUTION 4.1 Circuit Breakers by Bus There are multiple options for the installation, the table below shows the possible equipment part numbers that may have changed with this update and the associated electrical load. The following equipment part numbers may have changed with this update. Table 8 New and Upgraded Equipment Equipment/System Model/Part Number • Max Load in Amps TDR-94 622.9352.502 1.79 TDR-94D 622-9210.502 1.79 GPS RECEIVER GPS1203C 84327-50.XXXX 0.179 GPS RECEIVER GPS-40005 822-2189- 004/005/006/007/010/011/100 0.56 Page 30 of 36 Read By VT-DRB, FSCM 47M27, Set 30 o139. 2019!Mar/19 PROT444 EFTA 00241570 PROT45 DocuSgn Envelope ID: CF862885-6FE8-4C80-A4 E3-546 I F9B2D045 5 SYSTEM TROUBLESHOOTING For troubleshooting information, refer to the following; Equipment Circuit Breaker Document GPS1203c ADS-B GPS Equipment Installation Manual for the FreeFlight System Model 1203C GPS/SBAS Sensor GPS-4000S ADS-B GPS Collins GPS-40005 Global Positioning System Installation Manual, document 523.0780545, Maintenance Section TDR-94D TDR TDR-94194D ATCIMode-S Transponder System (-5XX). Document Number 523-0821492, Maintenance Section 6 INSPECTION REQUIREMENTS 6.1 Scheduled Inspections and Maintenance Checks This section of the document contains information regarding Time Limits - Inspection and Maintenance Checks, Overhaul and Replacement Items and Inspection Requirements. 6.1.1 Time Limits - Inspection and Maintenance Checks Note: Recommended inspection/maintenance intervals do not guarantee that the item will function properly between inspection/maintenance checks. The inspection intervals are based on average usage and environmental conditions. Aircraft operated under extreme conditions, (extreme hot, extreme cold, high humidity, salty air, etc.) may require more frequent maintenance than the intervals specified in this document. The aircraft operator may perform more frequent inspection/maintenance checks based on his usage. 6.1.2 Visual Inspections The equipment necessary for conducting a visual inspection usually consists of a strong flashlight, a mirror with a ball joint, and a 2.5x - 4x magnifying glasses. A 10x magnifying glass is recommended for positive identification of suspected cracks. 6.1.3 Corrosion Treatment Before attempting a close, visual inspection of any selected part or structural area, it should be checked for signs of corrosion. Any corrosion found should be tested to discover its extent and severity. Heavy or severe corrosion requires immediate corrective action. If mild corrosion is present, it should be carefully, but completely, removed before continuing with preparations for the visual inspection. 6.1.4 Structural Failure Determination. The first step in a visual inspection should be an examination of the area for deformed or missing fasteners. These should be identified for subsequent replacement. A close examination for cracks in the surfaces of structural members should then be made with the aid of a flashlight. The majorities of cracks start at, and progress from, points of concentrated stress such as sharp corner cutouts and fastener holes. Cracks may also occur in sheet metal bend radii and similar places that were subjected to severe forming operations during manufacture. REPORT No. 584-00.0047, Rev: D Page 31 of 36 Reid By VT-DREI, FSCIA 47W7. Shl 31 of 39. 2019iMat/19 PROT445 EFTA_00241 I PROT46 DocuSign Envelope ID: CFB62885-6FE8-4C80-A4E3-5461F9920045 6.1.5 Cleaning of Structural Parts All parts of areas from which mild corrosion has been removed should be thoroughly cleaned using an approved solvent. (Metal conditioner should not be applied at this time as it may interfere with subsequent dye penetrant inspection.) 6.1.6 Cleaning Other Areas All other areas to be inspected should also be cleaned of any deposits that might hinder the discovery of existing surface flaws. The protective finish need not be removed. The cleaning should be performed using any approved solvent. For cleaning high heat-treat steel parts, or areas in which a high heat steel part is installed, use only the approved solvents. 6.1.7 Crack Detection Technique When looking for surface cracks, the inspector should point his flashlight towards himself and hold it at an angle of 5° - 45° to the surface. (See Figure 6) The extent of the crack may be traced by directing the beam at right angles to the crack. Never direct the light beam at such an angle that the reflected beam shines directly into the eyes. The proper procedure is to keep the eyes above the reflected beam. FLASHLIGHT INCIDENT - LIGHT BEAM FAYING SURFACES EYE ABOVE REFLECTED LIGHT BEAM REFLECTED LIGHT BEAM CRACK OPEN TO SURFACE Figure 6 - inspection for Cracks 6.1.8 Verification of cracks A 10x magnifying glass may be used to confirm the existence or extent of a suspected crack. Page 32 of 36 Rord By VT.098. FSCM 47MZ7. SM 32 of 39. 2019/Maff 19 PROT446 EFTA 00241872 PROT47 DocuSign Envelope ID: CFB628B5-6FES4O9O.AcES5461F962O045 6.1.9 Visual Wiring Inspection Perform visual inspections of the wiring. These visual inspections should be performed as part of the existing applicable inspection cycles, not to exceed 1200 hours. (Reference Tables shown on drawing [SSN REDACTED] for applicable installations based on aircraft model and subsequent Wire Routing drawing [SSN REDACTED]) Refer to the pertinent Maintenance Document listed below: Table 9 Maintenance Manual by Aircraft Aircraft TCDS Model Learjet 60 60 P/N MM-103 Bombardier Inc CL-600- 1A11 CL-600-1A11 PSP 601-2 Bombardier Inc CL- 6002Al2, CL-6002B16 CL-600-2B12, CL-600- 2816 CL 604 AMM Dassault Aviation Falcon 10 Falcon 10 Dassault Falcon 10 Dassault Aviation Mystere-Falcon 20- C5/D5/E5/F5, Mystere Falcon 200 Mystere Falcon 20- C5/D5/E5/F5 Dassault Fan Jet Falcon Dassault Aviation Mystere-Falcon 50 Mystere Falcon 50 Dassault Falcon 50/50EX Dassault Aviation Mystere-Falcon 900 Mystere Falcon 900 Dassault Falcon 900 Galaxy/Gulfstream G100/SPX G100/Astra SPX P/N G100-1001-11-1 Galaxy/Gulfstream 1125 Astra 1125 Astra P/N 25W-1001-11-1 Galaxy/Gulfstream 200, Gulfstream G150 Gulfstream 200, G150 Gulfstream G-1159, G- 1159B G-1159, G-1159B Gulfstream II Gulfstream G-1159A G-1159A Gulfstream Ill Gulfstream G-IV G-IV Gulfstream IV Aircraft Gulfstream GV GV Gulfstream V Aircraft 500/550/S550 500/550/S550 Model 500 Maintenance Manual Page 33 of 36 Res By VT-ORB. FSCAI 47M27. Sht 33 of 39. 2019/Mar/I9 PROT447 EFTA_0024 I 873 PROT48 DowSkr Envelope ID: CFB62841.543FEB-4C80-ME3-5461F96213045 560 560 Model 560 Maintenance Manual 650 650 Model 650 Maintenance Manual Textron (Beechjet) 400, 400A 400/400A P/N 128-590001-9C HS.125 700A, 700B 700A, 700B AFMS-125-700 BAe 125 800A. 8008 800A. 800B AFMS-800 750 750 AFMS-800XP 800XP 800XP AFMS-800XP 850XP 850XP AFMS-800XP 900XP 900XP AFMS-800XP Sabreliner Aviation NA-265-70, NA-265-80 NA-265-70, NA-265-80 P/N SE 0405 MM Sabreliner Aviation NA-265-65 NA-265-65 P/N SE 0303 MM A "visual nspection" is defined as the process of using the eye, alone or in conjunction with various aids, as the sensing mechanism from which judgments may be made about the condition of a unit to be inspected. This level of inspection is made from within touching distance unless otherwise specified. A mirror may be necessary to enhance visual access to all exposed surfaces in the inspection area. This level of inspection is made under normally available lighting conditions such as daylight, hangar lighting, flashlight, or droplight. A visual inspection may require the removal or opening of access panels or doors. Stands, ladders, or platforms may be required to gain proximity to the area being checked. The inspection criteria provided below is intended as general guidance. Conduct special inspection as deemed appropriate by each operator based on aircraft experience. Any discrepancies found should be repaired. 6.2 Wiring The inspection criteria provided below is intended as general guidance. Special inspection should be conducted as deemed appropriate by each operator. Any discrepancies found should be repaired. a. WireNVire Bundle - Inspect for: Aluminum drill shavings, lint or dust on or inside wire bundles. Aluminum shavings can, with vibration or other motion, cut through wire insulation and provide a conductive path between wires in a bundle or to adjacent grounded structure. Lint and dust can accumulate on wire bundles and may, if subjected to overheated wires, ignite or possibly feed an electrical fire. Page 34 of 36 Red By VT-DRB. FSCM 47IAZ7. Shl 34 of 39. 2019:Mar/19 PROT448 EFTA 00241x74 PROT49 DowSign Envelope ID: CF882885.8FE8-4C80•ME3.5481F9820045 Wire insulation that has become brittle. Wire may be more susceptible to cracking. Damaged insulation and/or exposed conductor material of wires. Cracked, chafed and cut insulation can provide a conductive path between wires in a bundle or to adjacent grounded structure. Pinched wires can occur at wire clamps, connector backshell clamps, excessively tight cable ties. etc. Inappropriate/improper wiring repairs such as the use of duct tape, electrical tape, poor crimp splices, etc. Wire insulation damage due to fluid leaks (i.e. fuel, hydraulic fluid, etc.) Separation of electrical wires from hydraulic, fuel and oxygen lines. Ensure a minimum of 0.5-inch separation and any wiring routed within 2.0 inches must be clamped to provide separation. Small bend radii of wire. Wiring subjected to excessively tight bend radii may sustain damage to the wire insulation. Sagging wire bundles. Ensure bundles are not allowed to droop onto structure, components, cables, hoses, other bundles, etc. Wire attached to the outside of a wire bundle using plastic ties instead of being installed under existing wire damps. Can cause chafed and cut wire insulation. Unsupported wires running into conduit or wire supported in such a way as to pull the wire against the side of the conduit entrance instead of into the center. Can cause chafed and cut wire insulation. Proximity to high temperature equipment. Wiring shall be kept separate from high temperature equipment, such as resistors, exhaust stacks, heating ducts and deicers, to prevent wire insulation deterioration. Wires with different insulation types should not be routed together, where possible. Certain wire insulations may be easily abraded by other types of wire insulation. b. Wire Harness Clamps - Inspect for Condition. Ensure any protective material on the wire clamp (i.e. rubber, plastic, etc.) is in serviceable and functional condition. Clamps should be secured to structure and wire bundle should be snug in clamp. Ensure clamps are not installed over splices. c. Connectors - Inspect for Condition. Make sure connectors are free of corrosion, moisture, dust and metal shavings. Check for worn environmental seals, loose contact tension, proper contact locking, missing seal plugs, missing dummy contacts. etc. Drip loops should be maintained when connectors are below the level of the harness and tight bends at connectors should be avoided or corrected. d. Backshells - Inspect for: Condition: Wires may break at connector backshells due to excessive flexing, lack of strain relief or improper buildup. Loss of backshell bonding may also occur due to these and other factors. REPORT No. 584.00-0047, Rev: D Page 35 of 36 Rem By VT-ORB. FSCM 47M27. Shl 35 0( 39. 2019/Mar/19 PROT449 EFTA_00241875 PROT50 DocuSign Enveiooe ID: CFB628B5-6FE8-4C613-A4E3-5461F9432D545 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS e. Electrical Conduits and Sleeving - Inspect for Susceptibility to water/moisture entrance: Conduits should not be susceptible to the entrance of moisture. If moisture going into conduits and sleeving is unavoidable, provisions should be made in the lower portions of the conduit to drain any moisture and prevent accumulation. Condition: Damage to sleeving and conduits, if not corrected, will often lead to wire damage. Make sure components are free from corrosion, moisture, dust, and metal shavings. Check that conduit is secured to structure. f. Terminations - Inspect for Condition: Terminal lugs and splices are susceptible to mechanical damage, corrosion, heat damage and chemical contamination. The buildup and nut torque on wire lugs is critical to their performance. Grounding Points - Inspect for Condition: Grounding points should be checked for security (i.e. tightness) condition of termination, cleanliness and corrosion. Any grounding points that have corroded or have lost their protective coating should be repaired and checked for proper resistance. CAUTION Use care when disturbing or removing wire harness/bundles to minimize the possibility of wire insulation damage or cracking. Care must be especially used in areas with severe moisture problems. During any repair, modification, or installation work in close proximity to wire bundles, mounts, connectors and systems, ensure that these areas are protected from and/or cleaned of metal shavings and debris. REPORT No. [SSN REDACTED], Rev: O Page 36 of 36 R•I'4 8y VLDRB. FSCM 473AZ7, Sht 36 of 39, 20194A8r/19 PROT450 EFTA 00241676 PROT51 DocuSign Envelope ID: CFB828B54FE8-4C80.ME3.5461F9820045 Appendix A - List of Applicable Publications NOTE: The latest released revision of the publications listed in the LOAP constitutes the required information essential for continued airworthiness for the aircraft. Document TM. Document Numbei Airplane Flight Manual Supplement [SSN REDACTED] Master Data List (includes wiring diagrams, equipment installations and ground test) [SSN REDACTED] TDR-941940 ATC/Mode-S Transponder System (-SXX) Install Manual 523-0821492 GPS-4000( ) Global Positioning System Installation Manual 523-0780545 Equipment Installation Manual for the FreeFlight System Model 1203C GPS/SBAS Sensor 86764 REPORT No. 584-00.0047, Rev: D Page Al of Al Re -O Red By VIFtS. FSCM 471/27. Sht 37 ol 39. 2019nNadt 9 PROT451 EFTA_0024 I 877 PROT52 DocuSign Envelope ID: CF8628B5-6FE8-4C8D-A4E3-5461FSEQ0O45 Appendix B - Special Tools and Equipment Transponders - Aeroflex IFR-6000 or equivalent test set. GPS - JCAir 429 or equivalent 429 Bus Reader GPS - Oscilloscope REPORT No. 584.00.0047, Rev: D Page 81 of 81 Red By VT.DIRD FSCM 47M27, Ste 38 ol 39. 20i9iMar/i9 PROT452 EFTA_0024 I 878 PROT53 DowSign Envelope la CF882/9354FE8-4C8O-A4E3-5461F982O045 Appendix C - Discrepancy Reporting Form This form to be used by aircraft owner operators and modification centers to report discrepancies with modifications and repairs approved by the ODA. DATE DISCREPANCY DISCOVERED: Self explanatory. DISCREPANCY: Describe the discrepancy in detail. RECOMMENDED CORRECTIVE ACTION: Describe what actions you recommend faking fo correct the discrepancy. REPORTED BY: COMPANY NAME: PERSON TO NUMBER: Sell explanatory. PHONE CONTACT: TITLE: Signature: Sell explanatory. Date: Self explanatory. Please submit the completed form to the following contact: VT DRB ODA Unit 9800 John Saunders Rd San Antonio, TX 78216 USA Phone: (210) 293-3720 Email: service.su000rtevt-drb.com SHE & Associates, Ltd. Page Cl of Cl Red By VT-DRS FSCM 471427. Ste 39 of as. 2019thlar/19 PROT453 EFTA 00241879 PROT54 PROT454 EFTA_0024 I 880 PROT55 US Deasvrat MAJOR REPAIR AND ALTERATION a. !teants) Fel are Avian Adminisizafte tan Ma. 21 X.0320 Fa SWOON E fistrarIc Tenho MSS FAA Usaoalif INSTRUCTIONS Pmt or type all entries. See Title 14 PROT784 543.9. Pal 43 Agana B, aid AC 43.9-1 (or subsequent revision thereof) for InStruCtICOS and clam:salon of MIS form. This report Is required by law (49 PROT785. 444701). Faits° to moon can result In a col penalty for each such violation. (49 PROT786. 94630101B 1. Aircraft Nato/way and Registration Mark UNITED STATES / N188TS Senal No. RK-244 'make Model 400A Series 2. Chimer ITHORAIR Warne (As shoos o n registration owflAsete) LLC Address (As shown on reghtration certlAcats) mars PO BOX 2218 on SANDUSKY Sae OHIO zo 44871-2218 carer UNITED STATES 3, For FAA Use Only 4. Typo S. Unit Identification Repair nitration Unit Stake Make Model Serial No. 7 n AIRFRAME Aeneas co..huff (As described hi Iron I above) RK.244 POWERPLANT O D PROPELLER K ri APPLIANCE type Namotassaw A. Agency, Name and Address B. Kind of POORCy Tee Cmistant AdatiCli LLC U. S. Cesislcated Mechanic I Macelaclunu mean 355 RICHMOND ROAD r Foreign Ceraficead Mechanic cos CLEVELAND Os Gii Catfrated RepeIrStsfee CRS#WC7R346J es 44143 es",," USA Ceteketed Maintenance Oreantteb:o D. I certify Mal INC repair and/cr alteration made to the IAMB Identified in Wen 5 gave and described on the reverse or attachments hereto have been made In accordance Wth the requirements of Pan 43 of the U.S. Federal Aviation Regulatons and that the Wormation furnished herein h true and coned to the bop, my Eden:sec range fuel per 14 PROT787 Part 43 AP. B Signs I Steven A. Watkins 10/04/2019 7 apron] for Return To 9erVIC. Pursuant to the authority g' a below, the Lott Idengogg Administrator of the a' Adminkstreg and la VIA:droved in nun 5 nspected in the manner presated by the rejected BY FAA Flt. Standards Impeder Manufacturer Palma &graved by CaraMen Departmental Teramxt FM Designee Repair Staten spectionAuthanoton her Cattalo a Designation No. CRS# WC7R346J Signature/0 AtA indMdual David Kerr 10/04/2019 Page I PROT455 754959 EFTA_00241881 PROT56 NOTICE Weight and balance o r operating amliation (tenses shall be entered in The approplefe aircraft record. Melioration must be compatible with ail previous alterations to assure continued conformity **a the applicable ainvorthiness requirements e. Oescriptkei m Work Accomplished (II more space Li ',puha% attach adaborrei sheets. Identity mat &kalif nations* and registration meet and date salt completed) UNITED STATES /PINTS iettordie NOWAY and ROW: Oboe Merit Date Engine Inlet Rivet Repair Installed blind rivets in place of the damaged solid rivets on the lip of the right hand engine inlet forebody assembly part number 541000-004, serial number R0010, In accordance with nextant aerospace engineering order NT-EO-1118-31 rev IR dated 11129/2018 with FM form 8110-3 dated 11/3012018. Instructions for Continued Airworthiness: Follow the maintenance inspection practices in the aircraft maintenance manual. Inspection intervals shall remain as indicated in the aircraft maintenance manual or operators approved inspection program as appropriate. Weight and Balance unaffected. Reference Constant Aviation work order CCM-3160 END C:DAddilional Sheets Pee Attached Page 2 PROT456 EFTA 00241882 PROT57 WI DIPPATTARIT OF TRANSPORTATION FEDERAL AVIATICNACOMPASTPADM I. DATE November 30, 2018 2. WM S. SOX I. NO. N541000-004 4. TYPE Mint Era MOAK NM Embody Assy a NAME or APPLICMY Florian Aerospace LLC Cleveland, Ohlo LIST OF DATA I. IDENTOCATION 7 TIRE NTE0•1118-31 Rev. IR November 29, 2018 Engine Inlet Envoi Repair. Notes: 1) The structural aspects only of the above listed data are approved herein. This approval is only for the engineering data. It indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and subparagraph listed below as 'Applicable Requirements.' 2) This form constitutes FAA approval of all the engineering data necessary for substantiation of compliance to necessary requirements for the entire repair. t morose or DATA: Engineering data to support repel procedure for Textron 400A Forebody Assy P/N N541000-004, SIN R0010 under Nextant Aerospace Work Order No.10565.1.1. S. APPLICAEUE REOUREMENTS FAI walk acts) PROT788 Title 14 Part 25.301(25-23), 25.303(25-23), 25.305(eXb)(c)(25-231, 25.307(eX25-231, 25.601[25-04 25.8030104(c)(25-38), 25.605(aX25-00j, 25.807(25-23), 25.609(aXbX25-00I, 25.811[25-24 25.813(aXb)(c)(25-00). 25.819[25.24 and 25.625(a)(bXcX25.231. M CERTIFICATION . Under whyty vamml by drachm of Me AdmInIstrata and Vi accordance WA conclaIons md Rations of appolmmem under 14 PROT789 PM MI data IMO alma ad en tithed Meets motored _KUL Moe been examined In Kendra siD estotallm1 procedures and kmdbeemply wit, apalicam reourarims a ma Manion. Manderds Wed El Recommend Mown, of Masa data I(1W) TISMON reA Approve dime data It SKINATUREDDCF OESMNATE0 ENCREERING REPRESENTATNEER 12. DESIGNATION NUMBERS(131 13. a ASSFICATOIES) P rae" .9 • /7.7 t Paul Hedding DERT-410115-CE Structures FM Form 8110-3 (03.101 SUPERSEDES PREVIOUS ED(TX)11 File Number: 1118777.01 Pane 1 of 1 PROT457 EFTA_00241883 PROT58 PROT458 EFTA_0024 I 884 PROT59 fi Sy US D•firrintot of rransponstion (Airframe, Powerplant, Propeller, or Appliance) a nista Miele, Administration am i 2,20 0020 Ent Si3t/20.13 Moran Teinkrio N.insoi For ant Ufa Only INSTRUCTIONS: Print or type all entries. See Tele 14 PROT790 §43.9. Pan 43 Anaemia B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This capon is required by law (49 PROT791. §44701). Failure to report can result in a civil penalty for each such violation. (49 PROT792. §46301(a)) 1. Aircraft Nationality and Registration Mark USNN493LX Serial No. RK-244 Make Raytheon Aircraft Company Model 400A Series 2. owner Name (As shiywn on reoisOstion oertificate) Flight Options Address (As shown on regisrfation certificate) Mavis 26100 Cures, Wnsht PKWY Cry RiChniond Ilitighia SLY OH 20 44143.1453 Catty USA 4. Type 5. Unit Identification Repair Alteration Unit Make Model Serial No. O El AIRFRAME ii.............wriem (As described in Item I above) O POWERPLANT O PROPELLER O APPLIANCE Typo manufacturer 6. Conformity statement B. Kind of Agency Na. unantAseepar.• U.S. CeMcated Mechanic f klanutacturet Adam HS Rawohli row Foreign Certificated mechanc oh pewees Ox x Centicated Repair Staten CRS# 25NR6678 ;to 11113-14S3 Camay USA Certificated Maintenance Organnaion 0. I certify that the repair andior alteration made to the tine( ) identified in item 5 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Extended range fuel per 14 PROT793 Part 43 App. B Signature/Date of Authonzed Individual 2.- 1 -1 0/--r .4 7. Approval for Numt ervic -In -_..2(7/ Y P rsuant to the authority g yen persons specified below. the unit identified in item 5 was 'nspeded in the manner prescribed by the A minetrator of the Federal Aviation Administration and S InApproved JDRejected BY FAA Fit. Standards Inspector Manufacturer PiaraOnS ArCeOveci by Cartbdian Deparallell of Transccet FM Designee X Repair Station Inspection Autheiftabon Other (Specify) Certificate or Designation No. CRS# 25NR667B Signature/Date of Authorized Individual 7 i 7-A1A? Page I p5f-o/- 20/ p PROT459 EFTA_00241885 PROT60 NOTICE Weight and balance or operating limitation changes shall be entered m the appropriate aircraft record An alteration must be compatible with all previous alterations to assure continued conformity with the appltable airworthiness requirements S. Description of Work Accomplished (If nave space is required attach adationat sheets Identify with aircraft nationally and regatta:ran mark and So work completed) /4193LX Date It/2912013 This 337 is amended 01APR2019 to correct a Typo in block 8. Installed New Pitot Probes in accordance with STC ST10959SC. Nextant Master Drawing List Document [SSN REDACTED] Rev CC EO24-11. Removed Pitot Probes Part Number PH1100-MU-R-1 Removed Pitot Probes Part Number PH1100-MU-L-1 Installed Pitot Probes Part Number PH1100-MUR-EN Serial Number 1975803 Installed Pitot Probes Part Number PH1100-MUL-EN Serial Number 1728401 Leak Check carried ouit Beechcraft Aircraft Maintenance Manual Chapter 34-12-00-201 ICA Continue with Normal Hawker Beech Maintenance Practices for this area. END ditional Sibeets Are Attached I'aec 2 SONY_GM_02754964 EFTA 00241886 PROT61 DEPARWENTOFTRANSPORTATION-FEDERALAVIATIONAMAINISTRATION I MATIONAUTY AND 2 MARUFACTURER AND 1•30E1 3 aURCRAFT SERIAL 4 CATEGORY REGISTRATION MARKS NUMBER N188TS Company 400A RK -244 Transport AUTHORITY APO OASIS FOR ISSUANCE Dm incest. tons 19 imed pew* b49 USG MINA Wank. SK &idly 41% cl aunt the moat myna sam3 Ms Won immelid ell bee m <atm ttm tot tinker twece, bbn cerata tette memo% atm We Own13mM be NO•remb d ft icoxits cenrcamm ref *MIS inereres me.4 amok., MM.= gm to Can, to rooked CeelAestexcome 1:44 New fatten -None- I TERMS AND CONDITIONS llim4 WOW IMM01041.11SMO. *MK SAMaIMM b Ante isloMiNd by A. FM 1m srmetmemetkele is dubs by as nailesomi. motel* mailmemt aY Swim re ',etym.) nAmdamm M21,4 91dt% hand AmpamRatin is *ROOM In all BROOM m MUM'S Pitt /ATE OF ISSUANCE FM REPRESEI4TATIVE DESP3MATION NUMBER $3/06/2014 Arnold Wolfeat Ae GL-25 Mry alstake. wed.. if am deo weak mix patella bp be ad est, $1101 ispbeammail ammtkop mos a Mt 14 CERBRWE WM SE MAYER TEMTOUrt BUCCOMMICE turn NPUCAILE CEOBUL MOON MIAOW. A Rem 1100.2 (0441}Sesedis Pesebus Edam COPY rzoN\ P. atackcr PROT460.O65 EFTA_00241887 PROT62 Y400 PROT461 EFTA_00241858 PROT63 譬°C=m吗胃、。旦更嗖忾切工α<工O<工<α缶D工○山>二U岂○工42一U山「山Dh曲3蔼~~白∑凹>z8 P。 Q 。畅el1讧碰 扫各匡 達~凿 z 蓬啦衰怎 嚥8差盒G孬 PROT64 PROT462 EFTA_00241890 PROT65 C U.S.Department Cleveland Fight Standards District Office cr latsportoean 25249 Country Club Blvd North Olmsted, OW 44070 Federal Aviation 440-686-2001. Fax, 440,686-2080 Administration October 9, 2018 Aircraft Registration Branch AFS-750 To whom it may concern: During review of AFS-750 records it was found that a discrepancy existed of the Airworthiness Certificate for N188TS, Make: Raytheon Aircraft Company, Model: 400A, Serial Number RK-244, it was noted that the Airworthiness Certificate registration number did not show the required Nationality letter "N". During inspection of the aircraft it was found that the original Airworthiness Certificate did in fact have the required Nationality letter. Made a copy of the original Airworthiness Certificate and forwarded to AFS-750. If you have any questions in this matter, please contact me at 440-686-2053. Sincerely, Athen J. Neuman. FAA PMI CLE FSDO (440) 686-2053 Office athen.neuman@faa.gov PROT463 EFTA 00241891 PROT66 PROT464 EFTA_0024 I 892 PROT67 0 US barna 0 00.3001100., (Airframe. Powerplant. Propeller, or Appliance) reel. Aviation Atislaliplratiell DVS Pea 200.0020 bp SOU2On ewer . Troop.; Nee. sera Osten,. INSTRUCTIONS: Print Or type all entries, See Title 14 PROT794 §43.9. Part 43 Appendix B. and AC 43.9-1 (Or Subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 PROT795. §44701). Failure to report can result in a owl penalty for each such violation. (49 PROT796. §46301(a)) 1. Aircraft Nationally and Registration Mark USA/ N188TS Serial No. RK-244 Make Model 400A Series 2.owner Name (As shown on sew:ratan terttfreste) THORAIR LLC Address (As shown on registration certrkate) bras PO BOX Me Oty SAflDUS(V Sate OHIO Z. mamma Celery UWTEDSIAMS 4. Type 6. Unit Ident/fleadon Unit Make Model Serial No. Repair Alteralion n Fi i. ass" ft mecomowteepava. (As deserted In Item 1 above) AIRFRAME K POWERPLANT X PROPELLER APPLIANCE to. Kanuteaurer B. Kind el Agency Nn Newt A010,01K0 U. S. Connoted Mechanic I Macula:as Ado,. sedoarceenteeNv Fenian Cartecetad Iletharsa C. Cerbacate No. Or/ deified Vas x110 7 Cerbkated Raper Station CRS# WC7R346J De 44143 o w ",,,,, UMW SIMS Cerlikatad laMMOMIPS Organ/Wan O. I certify Mat the repair anctior alteration made to the Lait(s identified in item 5 above and described on the reverse or attachments hereto have been made in accordance with the restatements of Pan 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and cared to the best or my knowledge. Extended range fuel per 14 PROT797 Part 43 Ape. B K Signatur ate of Authonzed ( - C I nOMdual Chad Graham 10/06/2017 7. rovel for Return to Service idenggiag 5 in the by the Pursuant to the authority g yen persons specified below, the and Administrator of the Federal Aviation Administration and is I i IApproved in den nspected manner prescribed Rejected BY - FM Al. Standards inspector - - Manufacturer Panora Approved by Canadian Desennentet Tranesen - FM Designee - L Repair Station E Inspection Authorization Other apoulY) Certiltat or a ...a ., Designation No. (Alba WC7R346J Signahare/Cat On led Indnadu Steven A. Watkins 10/06/2017 FM Form 337 (10/06) Page I SDNY_GM_O2 754971 EFTA_00241893 PROT68 NOTICE Weight and balance or operating limitation changes shall be entered in the appropnate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (if more space is remirect attach Saban& sheets Man* Nib Mitre nationally and ritgisfration mark and dere sot completed) USA? HINTS Igebonelly and Pei:peahen Mark Date 1008/2017 STC# ST02371LA Wing let Option Installation Installed Nextant Aerospace Winglets IAW Nextant Aerospace STC# ST2371LA amended date 3/10/2017, Master Data List# MDL-NXT-001 Rev J, dated 2/14/2017, and minor deviations IAW EO# NT-EO-0817-09 Rev A and NT-EO-1017-09 Rev IR. Removed Equipment Item Left Wingtip Assembly Left Strobe/Position Light Assembly Wing Tip Lens Right Wingtp Assembly Right Strobe/Position Light Assembly Wing Tip Lens Tail Strobe Light Tail Position Light Strobe Power Supply Installed Equipment Item Left Winglet Assembly Right Winglet Assembly Left Winglet Light Assembly Right Winglet Light Assembly Tail Strobe Cover Plate Tail Position Cover Plate Part Number 45A10552-001 45A88750-22 8888-170000-01 45A10552-002 45A88750-22 8888-170000-02 4588315-121 45A88754-11 01-790080-00 Part Number NEXT-SA15250LA57-10001 NEXT-SA15250LA57-10002 87-03916-001 87-03917-001 NX0047-3340-0101-001 NX0047-3340-0102-001 Serial Number 00575 Serial Number S-NEXT-0001 S-NEXT-0001 00214 00216 ICA Follow the maintenance inspection practices in the Nextant Aerospace Instructions for Continued Airworthiness Document No. NX0047-ICAO-0101 Rev. A, dated 6/20/2016 or later FAA approved revisions. AFMS FAA Approved Airplane Flight Manual Supplement Document No. NX0047-AFMS-0101 Rev. IR, dated 3/10-2017 or later FAA approved revisions have been added to the Airplane Flight Manual Weight and Balance Reference Weight and Balance Report dated 10/06/2017 END (ditional seems AM Attached Page 2 PROT465 EFTA 00241594 PROT69 viltb Smut OH ekserrir irpzir burnt of Zraltspur felon ehrral gittriation ithutinistratinu $upplemental `Type Certificate ..fre;,/ohe ST02371LA gra.. a:v4ear.o.,:vaeark Nextant Aerospace, LLC 355 Richmond Road Richmond Heights, Ohio 14143 eencias dretref4afor E4 kJ! 44.104,40. Ie4Aall067,7,40•14%e Mac deP71444,44 efritlea,SAVIal likelier Ca 4400(10(21/4.00a/13.64, ,(h theelivoeltinow etreeaysowtoN eyegatool 25* 6/64. reeteratfAvaileive Array& . *Certification basis is set forth on TCDS Al6SW and continuation sheets 3 and 4. 9.-fraaitAileme agme. -4-(4/ Al6SW Beechcraft Corporation 400A .94,3 cosi I eao; oo talfeys Zr , Alteration of a Beechcraft Corporation 400A airplane, to replace Pratt & Whitney JT15D-5 series engines with Williams International F344-3AP engines (TCDS E3GL) with Full Authority Digital Engine Control (FADEC) and associated systems (Coatis. A) and (/or) the installation of Nextant Wingless (Config. B), in accordance with Nextant Aerospace Master Drawing List No.: MDL-NXT-001, Revision 1R. dated 8/22/2011, or later FAA approved revisions and the appropriate FAA approved Airplane Flight Manual Supplement(s) for the applicable installed configuration(s): Con& A: NXTI-AFMS, Rev IR, dated September IS, 2011 or later FAA approved revisions Contr.. U: NX0047-AFMS-0101, Rev IR, dated March 10, 2017 or later FAA approved revisions Stilleb4494 end KWh:47414d. 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 leo. Other person written evidence of that permission. (CONTINUED on page 3) A , a.-444arl4•awmiet4ienoirreas tethi aide /4 ekratA• grattevidentrarmesa air e ice' arta. ottermeeltreaeokanaiset: eotrAfewetko t lasootettwieto actie dee•Tri4), Ita144 64. tgaigotho3tr000koo ol;34 grit iteriorshOw Owe tairecno• March 24, 2008 September 27, 2011 gluaffnie.wile.. March 10, 2017 • 1 1 (Sigirature) Manager, Propulsion Branch Los Angels Aircraft Certification Office Made ,fry attention if this ("Afton* is pmcnis6a64 byelaw of rot cozotorio Wog or ler& meat oat mooting 3 yostre or bosh Ma lion IMO-MO -de rg.r of 914 mtge.,: ray fie uaufemiia ottordlout with fir 01.47. PROT466 EFTA 00241895 PROT70 PROT467 EFTA_0024 I 896 PROT71 )triitrb Auntie ail America Prpurhurait of transportation - getter:II ithiartirm Abininintration Supplemtntal ¶gpe Certificate (Qlcmtinuatiuu Afite0 ,M;Padeic ST02371LA Siarackener erearard iii.rdiareeta • Nextant Aerospace, LW, "Installation of Rockwell Collins Pro Line 21," Amended STC ST10959SC, dated September 26, 2011 or later FAA approved revisions is required as pan of this alteration. The new Vmca and Vmcg values are 94 K1AS and 93 KIAS respectively. The new engine minimum rated thrust is 3,031 lb at sea level, flat rated to an ambient temperature of 77°F. Approved engine fuels are: Grade Speeifisaties Jet A ASTM-D 1655 Jet A-I ASTM-D 1655 FAA accepted revisions of the Nextant Aerospace, LLC Instructions for Continued Airworthiness document must be made available to the operator with the installation of the STC configuration(s). o Coat A: NXT1-ICA, Revision IR, or later FAA accepted revisions. o Confin, B: NX0047-ICAO-0101, Revision A, or later FAA accepted revisions. CriValv.iv• JJvrJnJ The certification basis for this modification is as follows: The original certification basis for the Hawker Beechcraft Model 400A airplanes identified on TCDS AI6SW, Revision 26, dated March 17, 2010: Part 25 of the Federal Aviation Regulations effective February 1. 1965. as amended by 25.1 through 25-40. plus §§ 25.1335, 25.1351(d). 25.1353(c)(5), and 25.1447 of Amendment 25-41: §§ 25.29, 25.255, and 25.1353(c)(6) of Amendment 25.42; and §§ 25.361(6) 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 February 1. 1974. as amended by 27-1 through 27-5; and Special Conditions No. 25-ANM-32 dated February 22, 1990 (High Altitude Operation at 45.000 feet), and Special Conditions No. 25-ANM-33 dated June 18, 1990 (Lightning and Radio Frequency Energy Protection). (See NOTE 12) Equivalent Safety Items (I) Out-of-trim characteristics FAR 25.255 (2) Pilot compartment view FAR 25.773(b)(2) (3) Passenger compartment door FAR 25.813(e) (4) Emergency ail marking FAR 25.811(d)(1) and 25.811(d)(2) Application for amended Type Certificate dated February 18, 1988. Any oftertaion of Weis orrtiftarto u nutinia64 Cy a fw of not awing $1,004 or ispironatrer sec qtatallS 3 on or born. MA Pas 01.14.30,0.4•11 "op et • ggir cortifirste say 6s tnissformfin mandato via f Aft.21.4 7. PROT468 EFTA 00241597 PROT72 PROT469 EFTA_0024 I 898 PROT73 Xuittlt 'tales P.uterita gleparhneul of trausportatimr - Actual Ablation Abministration Aupytentental alertificatt (Continuation Alizet) Ireednir ST02371LA g;nce.artan.99O.4, 4.-468sco(/ Regulation at a later amendments for components and areas affected by the change (Ref. FAA approved Compliance Check List): Subpart A - General : 44 25.2(25.99) Subpart B - Flight; 4425.207(25-121), 25.255(25-42) Subpart C - Structure. 44 25.571 (25-96) Subpart D - Design and Construction: 44 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 - Powerplant: 44 25.901(25-46), 25.903(25-100), 25.951(25-73), 25.961(25-57), 25.981(25-125), 25.994(25-57), 25.997(25-57), 25.1013(25-72), 25.1019(25.57), 25.1021(25.57), 25.1043(25-42), 25.1045(25-57), 25.1091(25-100), 25,1093(25-72), 25.1103(25-46), 25.1141(25-115), 25.1143(25-57), 25.1163(25-57), 25.1165(25-72), 25.1181(25-115), 25.1183(25-101), 25.1185(25-94),25.1189(25-57), 25.1195(25-46), 25.1203(25-123), 25.1207(25-46). Subpart F - Eauipntenn 4425.1301(25-123), 25.1305(25-115), 25.1307(25.72), 25.1309(25-123), 25.1316(25-80), 25.1317(25-122), 25.1321(25-41), 25.1331(25-41),25.1351(25-72), 25.1353(25-123), 254357(25-123), 25.1381(25-72), 25.1431(25.113), 25.1438(25.41), Subpart G - Operating Limitations and Information; 44 25.1501(25-42), 25.1521(25-72), 25.1527(25-105), 25.1529(25-54), 25.1543(25-72), 25.49(2540), 25.1551(25-72), 25.1557(25-72), 25.1581(25-72), 25.1583(25-105). Subpart H - Electrical Wiring interconnection Systems (EWIS); 44 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 PROT798 Part 34(34-3); 3411 14 PROT799 Part 36 (36.28): 36.1-36.7, 36.101-36.105, 36.15D1, 36.1581. The following Nextant Aerospace Continued Airworthiness Supplements are applicable to airplanes modified in accordance with this STC: • Master Minimum Equipment List document No. MMEL Rev. 8, dated 02/21/2011 or later FAA approved revisions. • EWIS (Electrical Wiring Interconnection Systems) Inspection Procedure/Report No. NXTI-EA-007 Rev A dated 8/24/11 or later FAA approved revisions. lay thorn:ion of this ratifies:a u punishable 6y n foot of not met:fats $1,000, or Imprisonment sot waling 5 yin or boot not. rem 11110-200.40 pogo 4 or • Ili; certificate /1416. tram/erred ocoortfoors nog CAR.21.47. PROT470 EFTA_00241899 PROT74 PROT471 EFTA_0024 1900 PROT75 0 1S Onsaint to (Airframe, Powerplant, Propeller, or Appliance invirssunin 'KS Aviation Adeaffila,004 ram Append Ow No v20-ccoo NoonElectroric Tracking NurDer For FAA Use Only INSTRUCTIONS PAM or type al ones. See FAR 43.9, FM 43 Append& 8, and AC 43.9-I (or subsettuent revision thereof) for instructions and disposition ol this form. TNs repot is Waal by taw (49 U.S C 1421) Failure lo report can Molt howl penalty not to maid $1.000 la each such Notation (Section 901 Federal Aviation Ad 1959) I. Aircraft Natonalty and ReDstraton Mark N493LX Serail No. RK 244 Make Model 400A Senn 2. Ovmet Name (As sham on nmsfration comet:de) Flight Options .LLC Address (As sherds on reddration certsfitted Am.,. 26180 Curtiss Wriaht PKWY CO). Richmond Hetanta sate OH La 44143-1453 Coaltv USA 3. For FM Use Only 4. Type S. unn mentification Repair Moreton Unit Make MOON WM Mantel 0 0 AIRFRAME (As dncnbed in Rem I above) 0 O POWERPLANT 0 Ei PROPELLER O APPLIANCE Type manzeauw & Conformity Statement B Kim or Agency Now Constant Aviation Adam [ADDRESS REDACTED] can Cleveland ass OH 2p 44143-1453 Canty USA O USCerbficated Mena/Ain O ManutaCturef O Foreign Generated Mechanic C. Ceases No. 0 Certificated Ryas Station CRS # WC7R346J O Certificated MaiMenance Organization 0 Imlay Mat the repair ancitor alteration made to the urn(s) Identified in item 5 atom and detrained on the reverse ot attachments hereto have teen made in accordance ash the requirements of Pan 43 of the U S. Federal Aviation Regulations arid that the information (limn/had herein is the arid correct to the best of my ki Extended range fuel pee 14 PROT800 Part 43 App. 8 0 SonalureJOMe or Authorized land Waal ISI f OWSep/2017 7. Approval tar Return to Service Pursuant lo the authority given persons specified below. Me unt idensEed in item S was inspected in the manner prescribed by the Admintstrator of to Federal mann Adinamaratan and N 0 Anstovso 0 REJECTED BY FM FR Standen% Inspector Manufacturer Manufacturer Maintenance CrsersizatiOn Person Approved by Canadian of Transport FM De ghee X Ream Swoon inspeceon Aflizabon Other (Smolt/ Cattalo or Designation No WC7R346J Signature/Da aka:1.0,4nd InSvclual 09/Sep/2017 FAA Form 337 paw SDNY_GM_O2754979 EFTA 00241901 PROT76 NOTICE Weight and balance a operating halnahOrt changes Shia be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued contomMy with the applicable ainvorthiness requirements. (It more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed) N493LX 12/Sep/2017 Date This is a revised FAA 337 to correct the Serial Numbers of the Engines that were installed by Nextant Aerospace CRS # 25NR667B on FAA 337 Dated 05/30/2013 Nextant Aerospace Completed STC # ST02371LA Removed Pratt and Whitney JT15D-S Series Engines. 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. 252767 Installed Right Engine Part Number 111000-202 Serial No. 252768 ICA AFM Supplement was installed on Aircraft. Nextant Aerospace Instructions for Continued Airworthiness Document NXT-ICA Rev IR or later FAA accepted revisions are included in the Aircraft Maintenance Records. Carried out Engine Ground Runs and System 0PS checks IAW Ground Test Plan [SSN REDACTED] Rev F. End Id Additional Sheets Are Attached FAA Form 337 (10-C6) PROT472 EFTA 00241902 PROT77 umnovantaMetCA OEPHITMENT OF TRAKSPORT41101.FECEPAl AVIATION 0/010TRATION • STANDARD AIRWORTHINESS CERTIFICATE liCOWJIV Ye I ...masa( tarn mt.-Val I .a•cwt *My a Canteara 41CISMAIW"..3 18813 Canpany 4COA • Aralarrs160.414,4/1Coanal..( Faalaw••••••• ..•••••,...... I' Oa. wry /sin Oa mat aka add MOW •14.1•1•1 ••••• teatlatanallotalfa•la. fa am. f a woo Po allallasalenStaimaliaeok •ffdli II ell COMV•Pli. gr•Pli atom RK-244 Transport I ad MO coronas San , WM.. IMMO. •••••3 man lill•S•0014011•144.10••••••••• ▪ alliMas lamas ._. PIAIMemien Wasilmaroslan. malmadbalnalk 0of tegifliamiSes Calal 00 *WC tilienAlen NASA 0.3/06/2014 Arnold Wolfe carn .......•OnnaleilInntaikaameg inialelmnairgerasSe pilitea INCOITCASIOSIC DOWIT la al SataMa ••= 8:0•Cl Val late! ROM 00.0:5140.4100 hnT c'YIa SDNY_GOA 02754981 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00241903 PROT78 PROT473 EFTA 00241904 PROT79 trCIOMISO. ANIMA CEPIRTVIENT Or MANSPCMATION.F MEWL AVIATON ADIAINISTPATION STANDARD AIRWORTHINESS CERTIFICATE sedmarnit 4 .....DttnA 0-0 vita I AMOT fa* • CAROM a." 3" .." Raytheon Aircraft re1 11493LX C:ICompany 400A R 44 ransport uNINNA•14.1. ••••pell et it SOOMISISIN. ad Ss. wank •••••Illt 4 11•••••••••••011011•1•NIMISIMIS Ma••••••• snit wear O110• 4•11nikrOlillaipPkiliamemOmMt••••••••••••••110.1 110.0 4•NnieulaitO•••••••••iimaSin IRS *NOnti• sa stsiongeet said ...Willie...I invenitataa•••.fra e• Saw MS, gar snag N. Rae. ••••••••• ••••••••••Wel. It ell II ill. lan••• kiln, wil• 03/06/2014 Arthur Ockwell 1 I DARTS 339 4 IG: Pit *A.I.MIL ist Maisallyi %MO IIMIMIPPS • ••••41:4•Vtt "Or===r n. PROT474 754983 EFTA 00241905 PROT80 SONY_GM_02754984 EFTA 00241906 PROT81 4/10/2014 Flight Standards District Office Great Northern Tech Bldg. II 25249 Country Club Blvd. North Olmstead, Ohio 44070 Cleveland Flight Standards District Office: ThorAir LLC. would like to request a new airworthiness certificate for Serial number RK-244, Raytheon Aircraft Company 400A. The reason for requiring an airworthiness certificate change is a new registration number is being placed on the aircraft. Included with this letter is AC Forum 8050.64 issue date Apr 03, 2014 showing the change in registration number from N493LX to N188TS. Signature of Owner: Title of Owner: President of ThorSport, Inc., ThorAir, LLC. It's Member PROT475 EFTA 00241907 PROT82 SIDNY_GM02754986 EFTA 00241908 PROT83 FAA FORM 8130-6, APPLICATION FOR U.S. AIRWORTHINESS CERTIFICATE FONT AWOMONI OM O. No. 21204015 Fapimian DOW 02228/2013 0 APPLICATION FOR LIS OeNrIMAI U.S. AIRWORTHINESS orNammteben Faleal A.I•Ilon CERTIFICATE A/Mmunlion INSTRUCTOONS • PrAmon)90. DO rat wills In sno0•1 sew t.,. woe FAA mI4 MN SANT, 6•60 40; Oar le oft sulhalle1FAA RACOMAINIrtt N sikklovl Wows mound. msonschAwIl Ftie &pedal Nolv pones Ample, Socha I. N. and VII es ocolcale L AIROtAFT ousoupnow I AMSTRAD:IN MARK N493LX 2 AIRCRAFT BOXERS NAME Rua Raytheon Aircraft Co 3 AIRCRAFT IACJOEL DESIGNATION 400A 4. YR MFR. 1999 FM COD NG S ARCRAFT SERIAL NO. RK-244 6 ENDRE WADERS NAME plow Williams Intemational 7. OGRE /ACOEL DESIGNATION FJ44-3AP 9 KAMER OF INGRES 2 9 PROPELLER WADERS MK me, N/A W. PROPOSER 1100EL OFFIGNATION II. AIRCRAFT 6 rim dowoutt NIA I MAORI P !3 ; g R V t a S ARAM...TON IS HERM MACE VCR p.ss roses* Assl I A I .1 STAIOAROAWACRTHNESS CERT/MATE Omamewmf 1 1 5.55+ i 1.40" I I acsay I (hassle i I eosin' I 1•W0,' I 1 PAD a SPECIAL NRAORGINEES CERTIFICATE Os emwoN 'NW 7 PRIMARY 9 LIGHT I I MS* I 1 PoseAPanchvia I I valp-955Custi I I Sew I I At 2 -SPORT ...mar UNITED ran S PROVISIONAL d I CUS i pms. m/ 2 35 • CUS I MORCIATIAE MOPES! WAWA 2 Nam. SURVEY 1 WEAL AOYERTERNO 3 RESTRICTED eN mops eraufe 4 FCREST amok N3 PATROLU 5 %%RATHER CCHTROL pie RON) 0 fares.; ODER MAW I RESEARCH ANDOEVELOFIENT 2 AMATEUR MALT 3I 6304EITICA4 AIR RACING 5 DEW MOOG 6 NAFMET SURVEY 0 TO WOW CCMPLIANCE WITH DE PROT801 7 OPERATING PIANDOWWN MT SALT AIRCRAFT EXPERIMENTAL M OdolrumnINAT.M an marnows anion 4 Mow me4I 9 I03.1 4 Miss •••••00/ a* co.Scle. 0 OPERATING II3 OvensaNUOIScal Kean LIGHT-SPORT SC OWEN "MOM MA 93W* MAXI IWICIO ROMPPI MO9Ory 9.wworm4 calks& Labe 5 21.' UNMANNED OA RESIAROI MD CEMELCONIENT I IC i [CREW TRAINING ARCRAFT te MARKET SURVEY 1 FERRY FLIGHT FOR REHIRE N.TERATICNE IMMTENNICE. OR STORAGE SPECIAL FLIGHT PERMIT MONO 2 EVACUATE IRCIA AREA CV RAPEICING DANGER a or04 CO•Mist 11,44 OS a. rano:am S mil 3 OPERAT Cod IN EXCESS OF MAXIMUM CERTIFICATED TAKEOFF WOW! MARINO OR EXPORTS] i 9 1 . I PRODUCTION NOR TEEMS 6 CUSTOMER 00A3MYRATION FUMES ci 6 WA ME AIRWORTAMESS aRTWICATE tOve SW *bar e °prawn tees tileatalegiaMal M. OMER'S CEA TIT ICATIOM A REOSTERED OWNER 04 ~An mom issammtam IF MAUR POCK NERIS- I i NAME ThorAir LLC ACCRUE PO Box 2218, Sandusky. OH 448/1 ARCM,' CERTIRCATADN BADS M•P IMAM NNW essmwor ten. b* AIRCRAFT sseCSICANCea CR TYPE CERTIFICATE DATA WEFT town. m I gess./ • i A18SW Rev 26 1 AiRwORTM Ness DRECTNESICANIOMMMIMOI •••••••••••••••••••••••••• ~an 0 !WS° a wawa. Ise •.*** ow • • a II ens tlegialso Bi Weekly 2014 2/10/2014 - 07/23/2014 AIRCRAFT USTM3 Km Pe Im/IPM N/A SUPPLEST& TYPE CERTIACATE me /ewes ems ETC See Attached Sheet C AIRCRAFT OPERATON NO IINNIVAICE RECORDS CHECK IF MOCKS IN 1 U cououracevam 0 M sociwoO 4 TOTAL AIRFRAME MAWS 8816.1 TTAF 3 EXPERIMENTAL CM, itanoa bon Sas I a lainedadDlini ...NM N/A 0. Clanne5n 5NN• I MY, / oar/ 1700 I 4.6 lososans en Thy to e vs I.$5 NNI Seem n-1/MIS cswa nailed DADDOWOROMO NINE Awn° of FR haS eiscrees mow ow ow non Cob NAM Ells Ned Mite* F•Seml AMROI ROMPONI. and OM Do is mond Am VS own man Aemvsnom v. NUM Ms Wm niptoso AMR /MTh RN EOM 92/ DATE OF APPLICADCA: 03/06/2014 NAVE AND mu ••••• MN Anton Kcarivnik Agent SIGNATungtc.. .0.1,z I I i 1 i A OE ARCRAFT DESCRIBED ABOVE KM OF EN INSPECTED NO FOUND NRW3RMY BY: grump. rm. 5v, a cams P. Pad 1 "cm fr , '?' Conr an racer may CERTOICATEOAIECAMIC RNA UMW, AM 3 i I 6 CERTIFICATED REPAOSTION //vn comm. -I 5 AIRCRAFT MUNI AMMER IN,.. mob.. DATE TILE SIGNATURE V. MA REPRESENTATVE CERMICATION Osamtargasmosi 4 /411 el i NE CERTIFICATE nova Teo A I Ito ow re atm* butted P Swami M Wiesen imams la 4 AMENDMENT CR NOCIFKATICN OF CURRENT MMORIWNESS CERTMCATE B. inglocia, to VINS5VOWNIN ARAM SKIS' NI RN ONONININ FM DEFECTOR FM nourusE CERTIFICATE MIXER LACER m PROT802 pal 66 I J 14 06401121Cit OS I I 14CFR PIN IM OATS 03/08/2014 AUCOC*300 CFFICE GL-25 4 FM SA =COI A Odovell 3 1 r TYRE REVIEW OART833943Cal. a k • • E AST FM Fan elan (4/11)A4 Promos Comm Sulermwo EYLMOncF -PDF RECE MAR 1 U 2014 CLE-021. PROT476 754987 0 0 a EFTA_0024I909 PROT84 9 CC I P A AIMILVACTUPER I NM* I AC M" B. PRODUCTION WES PTHOCEPAPHOWS4 PrODUCTICH CERT PICATE (G. pe/aceinatitEtSmate) TYPE CERTIFICATE OTHER C GNI OUATITHY OF CERTIFICATES RECIARED FM COERAHNO NEEDS DATE CP APPUCATION twae notate ows ace? SIGNATURE ro i g I i 1 I • i I ii I g A MORMON OF AEICRAFT REGISTEREDDARER ADDRESS MADER (AAMH MODEL SERIAL NUMBER REGISTITATKIN NAM S DESCRIPTION OF RS! O./STOWS cauctssTRAncrt mows O tot•cmcon_ FRIER TO NA DEPARTURE DATE I OJRATICN C. CREW RECTAREDTO OPERATE TIE AIRCRAFT AND ITS 'MOMENT I I PROT I ICOPILOT I I WENT (SEER I I one, ispoom D. TIE amain DOES Nov men ne AFRICAME MMORTHINESS REOUPEMENIS AS REELOAS: THE rettOtemG RES T RCTIONS ARE CCATSIOIRED NECESSARY ICISAFE OPERATOR (Use mcreen Ofrocesmy) F CM T MAT ON • I NPR" anti PR I PH HA *paw tees for Rs WHO TI HO small *notes tom IM dv Ana is Nguema wt Ho Fa *nun Acnnecnaen in axcearcooth T404901 a* unisS Rat Oa 44101 EUEs ird Riga** Fears /San ANfrolierts. And MM Ho sive Si ton repoRPO ltd b EWE. tho fISH asacreat ()ATE HARE AND TITLE (11rol WS) SAGIEETURS 14 i 1 III 0 if A Oponero uirraotrend Sam* in Corpfarci MA 14 en $40/44. 91 O. As Pcpcstto G. Sranmei ri Calm*, FM Item Ma PEW/ aver M40•Ct H kept Alrolints CoiRcitan Aron G eplenfrig WSW, AliKlad bingai (Abdo I n do i A SWAM C. Oa Oa*. Proagnithl OK emsch.then reptc0 I PmApaPastahhips C**Me IsAued M AcwOinc• Van PROT803 gods 21.191(0 c&. (0-0 TmerlicretE 0 Oann WIVE ni Mara Irnemitst Amilibe MINI, E 04Not RSA, And Manic" AAA Ponit rs APO Orr MUM/ i 1 Gni Aetcalropu CCelia % tsHNEHT Hxedince WEE i 4 ce,i $",vc., 21.1839D toopy ~o I F THE IrePIERH Roan/WM Ma Rom* K I.GIT.Spen Anne Spinet clCorourat FM FOITII SOWS (AIWA .4111.• _d? FAA Faro 1304 It) ANPfertvileclitOnt$04WMCM0 £wOR* Forma -POP Pops 202 PROT477 754988 EFTA_002419 I 0 PROT85 61.1110 VETO a AVOCA DEPARTMENT OF TRARSPORTATCAFECOAL AvtAnCei AD1PNISTM? , " / Woke K ra• MO Mai I /SOAR WPM • CC! DIGSMATO•10/03 Raytheon Aircraft 444.4 11493LX Conpany 400A RK -244 Transport I% ovens rata • mat ~no n la 40 mien Yawn. al tut taeatainewili WIN •Ils • amill•Ineraa ma ain nano... en• igOtot sweasimme•Wal atrieMa• asseafis • no tan *NONE* I TOWS WOW" CAS W•ii ••••nitimuinig SAN wt.. • new 16.• me...alien miens •••••••nssa re Wine* woes •••••11.4 anv I. ...We ••••••M. /1/1. neWl.m4 1:411(TOON WOW OS/06/2014 arena, nrkwal 1 .'tie, 1 DARTILUR 4 ictE. maamtAcura. a Ams•AntanioNNYSNINAnang*PWARARInsaaNirahaNsilh , 443:intaillgrilWatill100:04700XCAKtOrrStOOLIM:01.14 -411.11X011. •Weettenri " imam 'nada,. PROT478 754989 EFTA_0024 19 I I PROT86 SONY_GM_02754990 EFTA 00241912 PROT87 w11O MIS IX MAMA 01.011 Wee 00 tiltANSIPOIttetts • I COI *AL AnnONAOMSTIMTC. SPECIAL AIRWORTHINESS CERTIFICATE A CATEGORYASESiGNATICR Exp•rian Til PURPOSE Ma rket-OSta r Ye o )44mu- KAcTuRKR NAME - N Th c - ADDRESS '7, C PLIGHT TO D 4. 4931,X SERA& so RK-244 &ULCER f I eythcon I -ate! CT 7' '&004 400A E MITES ISSUANCE F V OW /tv wp' Aua/04/7014 tonna L tV/TA• S T eb OS 2 01 *RE PART OF DES CERTIRCETE irneenal a mut ins scvm, Arthur Ockwell DART833943G1 Mt .44..sytmoroaceon a on...* <4 Os MMUS inOy M De pastube oya V* AP I.1 n1 II OW a inplevist ea a., ),,w, e! W. My CC ICAlt W Ea O6•LAYZO 14 %le DI ACCOlIONCE WITH MPUGOOLE RILE u CCM Of Mau V faclualiOns KM' NRCRNrt tAt404040) SONY_Ghl02754991 EFTA_002419 I 3 PROT88 A Pa arestanits mita a sun watt* liatytthtlic tam !Rd It LSO Rai CON' rum wris al rat ri tabu l C ter•• nitgaaca 1 ORA B Ihrientinossantiftattatralte srentitswendol nt wpm se• iv ono roacuAllp•Stigt anlaypothobap4 NM of wog repinnel obi nom No mac Off 0,463dredianig(lttli vatthit waft* 0) Cugiop Rims et nu" braawasse cc Re se la CRYMORnires, antroft0 INIRROI OR'S C al, anaa,n 3 ORRIN ARUM M SO Raft; Rine rows Raab to Rim Rana ROA D Pie aneaRiess coRalpoone rut ROM ale c hasa, Mace epic. WOO ha; mm norS0 la Ratio and fonowcares der Rhabb VA Movie No Wane rhe (Ran ,* OrIntoket anpiRARt /NW RoWswoRitss ma as mad 47 An. Mitt Orestroi On MornilanalOntAmMon No Ram tag apas Rapt cin:Rod at ES roman* (!) moot n accntnotwen es sewn Ca gni n ameba witancskra end SS, eti., My Of MIS/ 0 reAReteak, fl at 0 Rs OARS ID ow RP RIP may*Ra IwicoR pays a IN Can E ars Rotor tonnsted sawfdr1 [newt"; ha aNCIII27•0 Pada Ofettml R IV Min: 0 safe Iftnatams motel n IA ()lithe 21 Seam 2. talc al 2I7 S/3NYGM25 EFTA 00241914 PROT89 ThorAir March 3, 2014 ThorAir, LLC. PO. Sox 2218 Sandusky, Oh Re: RK 244 - Agent Authorization To whom it may concern: This letter is to confirm that ThorAir, LLC, authorizes Nextant Aerospace, LLC, as ThorAir's agent for a Beechjet 400A, bearing serial number RK-244 and FAA Registration number N493LX, which is owned by ThorAir, liC., and operated by ThorSport, Inc., for any and all authorized FAA actions needed. Sincerely, ThorAir, LC By: Mci\ sZ/N\Y ZS 1-1\\AQ ° A 9 Notary's Official Signature Sworn and subscribed to me this dayaof VC\ ON O\ 2014 btyk -,\NAt -AX:f-C.A) ThorAir • P.O. Box 2218 • Sandusky, Ohio 44870 Phone: (419) 621.8800 • Toll Free: (888) 394.7325 ThorAfr PROT479 EFTA 00241915 PROT90 PROT480 EFTA_0024 19 16 PROT91 R K-244 STC list (03/05/2014) Reference 8130-6: Application for Standard Airworthiness Certificate Transport Category, dated March 6, 2014 Reference section III owners certification ST02371LA: Replacement of Pratt & Whitney JT15D-5 series engine with Williams International FJ44-3AP engine (TCDS E3GL) with Full Authority Digital Engine Control (FADEC) and associated systems. ST10959SC: Installation of Rockwell Collins Pro Line 21 Electronic Flight Instrument System (EFIS) with Rockwell Collins FMS-6100, Localizer Performance with Vertical Guidance (LPV) approach capability and Universal Avionics System Company (UASC) Terrain Awareness Warning System (TAWS) ST03960AT: Installation of Aircell Axxess Cabin II Iridium Phone and High Speed Internet System with Wireless Local Area Network (WLAN), Astronics 115VAC 60Hz Cabin Inverter and Bonner LED Cabin Lighting System. ST01572WI: Installation of four (4) model 400A OEM seats, one (1) three-place divan, one (1) aft toilet, one (1) set of aft pocket door dividers, one (1) set of forward pocket door dividers and LED lighting. STC01794LA: Installation of Hawker 97650W0370 or 9750W0370-8 battery ST000812SE: Group airplane approval for Reduced Vertical Separation Minimum - (RVSM) PROT481 EFTA 00241917 PROT92 PROT482 EFTA_0024 19 I 8 PROT93 PROT94 PROT483 EFTA 00241920 PROT95 PROT484 EFTA 00241921 PROT96 PROT485 EFTA 0024I922 PROT97 PROT486 EFTA_00241923 PROT98 PROT487 EFTA 00241924 PROT99 FAA FORM 8130-6, APPLICATION FOR U.S. AIRWORTHINESS CERTIFICATE Form Approved 0 NA B. No. 2120-0018 0 APPLICATION FOR U S Omellial U.S. AIRWORTHINESS of TonsporliNen Festal MISR CERTIFICATE Aassberollon INSTRUCTIONS - PSI or IsTe. Do nce wile on shaded areas: Mow ate W FM woolly. SOW, ofOrill ref 10 en 444hanzed FM Representative II addional VW It MONfed. WO ellachmeN For SPOON MON Wrote 00TOINe Seaon II. A. and NI as applicable. r... § * o. 22 I REGISTRATION MARK N493LX 2 AIRCRAFT (WADERS NAME Wow 3. AIRCRAFT MODEL DESIGNATION 400A 4. YR /OR 1999 FM COOING $ AIRCRAFT SERIAL NO. RK-244 6 EROTIC BUILDERS NAME way Williams International 7 ENGiNE MODEL DESIGNATION FJ44-3AP S MUSSER OF ENGINES 2 9 PROPELLER GUILDERS NAME PAN N/A ICI. PROPELLERMOM GESIGOLATION s I AR CRAFT IS rtme. 4 A i N/A WORT o Vs C Si cc Li 4, APPLICATOR IS HERESY MADE FOR !Chid mitaliki• SU I A I I STAROAR0 AMYARTMNIESS CERTIFICATE passneasown I I I I vni u I Hama ', III `AN., " I I " A ' I I s oom 1 I ..'" (I SPEWS. AMWORTHNESSCERWICATE /0•••••••••• Nan 7 PRITmRY 9 LIGHT-SPORT I I Arran. I I PowrasseNA• I I LWAri-Shill.Conaol I I GOF I 2 E.4....o.. LIIIITE0 art M 5 PROVISIONAL maws SU I CLASS, 2 CLASSY I AORCULTURE AND PEST CONTROL 2 AERIAL SURVEY 3 AZ NAL ADVERTISING 3 A le =nay.. faemsepral140, 4 FOREST M a Rea** PATROLLNG 6 MATTER CONTROL 0 OTHER !swam I RESEARCH ANO DEVELOPMENT 2 AMATEUR SUIT 3 OGISITION 4 AR RACING 5 CREW TRANING 6 I MARKET SURVEY 0 TO SACAVGONPUNICE NTH THE PROT804 7 OPERATING Mawr Carasor NT CULT NRCRAFT EXPER MENTAL IA &Mho einnAwAho-e en anclitness ortice.e t Oa MAHN $ 1011 ..........o....ye am oaldtaIO OPERATING a Ocersdra LepaSoarl Kilda, ueirr-socat ric OIFIR4V9 IFORCei PWCUSI4 Wild CMS RIVRPOrl Magary ahcoviness ceNleslovieW$ 2t.ITO 9 UNLIAMED 9A RESEARCH MID DEVELOPMENT I 9C I I CREW TRAINING AIRCRAFT 56 WARM' SURVEY I FERRY FLIGHT FOR REPAIRS. ALTERATIONS. MAPRENANCE OR STORAGE SPECIAL FLIGHT PERMIT memo 2 EVACUATE FROM AREA Of IMPENONG RANGER S Apnea* a OA emateld Pon Oarial• FRIORA.4 IR al •404$01. RIR 3 OPERATION IN EXCESS CF IMALIUM CERTIFICATED TAKEOFF MIGHT DELIVERING OR EXPORT/4G 1 5 I I PRODUCTION FLOW TESTING 6 CUSTOMER DEMONSTRATION FLOGS CI 6 MULTIPLE AIRWORTHINESS CERTIFICATE Kama moon Nmemeceam... Parbovilenre Wet a • WRY.) O 8 14. lcis u a kr A REGISTERED OMAR Ms ewe semnessionna mos, FORAMCHIC% HERE- 0 I NAME F ight Options LLC ADORERS 28180 Curtis Wright Parkway. Richmond Heights .OH 44143 B. AIRCRAFT PROT805 T IF CAT ION OASIS (ORA •00444.0 14104 .49 MVO* IS 00 ARON* AIRCRAFT SPEGFICATION OR TYPE CERTFCATE DATA SHEET /ow re .0 i Avrenne) A16SW Rev 28 I NAWCRTHINESS DRECTIVES Nr••• vas arker•Aa. on otapar re gon eronentee sem bit AO $VPASIENT neat* At. OWINI WY anions* if appiner. Bi Weekly 2013-25 12/02/2013 - 12/15/2013 AMAMI LISTOIO 0.1.0Salealt N/A I SuPPLEMENIAL TYPE CLAWCATE Am ame s.* srchaemmem) See attached sheet C AIRCRAFT OPERATION AND MAINTENANCE RECORDS CHECK F RECORDS IN WTH I G A OMP PROT806 LLANC N E ateP AU I I TOTμ MRFRAME HOURS TTAF 8581.43 3 EAPERMENTμ ONLY oror.ors dem snap row NoVoser mon 04444441 2.81 0 CERTIFICATION dwelt/ easy ral I 8 403.00. ROI To. 43 44 R4 URI44 SRNS atrevainaleanioao wowed wow Mn Ivo ncsesceol oars (a Ns nem) of re emaek deSCADed to.. MN to *welt CAM 44MI tag ird Sab* Federal AR011ori I4494sbou. moths ma sacra 4 regs•el war Po AFARS Melia, Acenwuraca in Ma porn Anoeded to 4 IkrwrAPry Fa el ode Re she APPLICATION DATE OF APP 12/29/2013 LAME MD TITLE (Ana,...) Anton J. Koprivnik Agent SIGNATURE by )1", a igi S I 6 A. TIC NRCRAFT ()ESCROW MOVE HASSEEN NSPEGTE0 AND FOUND NRWORTRY BY coma ea semen, yr om awn. Icy "sou 2 HI PROT807 zt ) 121 CERTIFICATE HOLDER 11, \ • 3 CERTIFCATED TECHNIC ANeas etarlai 5 I CERTIFICATED REPAIR STA Rao Geo. PO) AIRCRAFT MONUFACTURER Chose saw/ DATE TITLE SIGNATURE i g s Mani aersma oinfraw4 A *MN I THE MITIGATE REOUESTEO A IRO Mel as ANSI booted h Samos i or Vii rads IVIVIVIIWII RR 4 MIENDMENT OR mODFICATION OF CURRENT NRWORTNINESS CERTIFICATE S 916040101 IN • Rhoaal WI Dame Leder SWAN VII an comk40•3 Di. FM INSPECTOR FM DESIGNEE CERTIFCATE MOLDER UNCER RACER No 65 I 'M PROT808 pal IV OR OS I !IA PROT809 pen 145 DATE 12/29/2013 16000500 OFFICE CLE-25 F FAA INSPECTORS SIGMA SIGNATURE AND NO Arthur•Ockwell DART83.3943GL 015 1 t i\ 1 F CTOR TION REVIEW S HA E ED lb 1.• LUW AC- 3/304ru11)AJPhWoi4 ENans SuC*SONNI EleeVorse Fermi -PDF 2 PROT488 n 3 a 0 3 O 0 EFTA_00241925 PROT100 PROT489 EFTA 00241926 PROT101 K 'ROOK-nom FLIGHT itSnNO A MAILIFACTURER NAME ADDRESS 8 PRODUCTION BASIS (CNKS•04•01• AWN PROCUCT KM CERTIFICATE (Gm. peckcata catiftdos twits) TYPE CERTFICATE OTHER C. GNE OUMITITY OF CERTIFICATES REQUIRED FOR CPERATIM NEEDS DATE OF APPLICATION IMAM MO ne PAM a OFF) SIGNATURE H t o i V 5 P i 0 I 1 g I t t I A OESCRP TC/N OF AIRCRAFT REGISTERED OMER ADDRESS BULGER MODEL TAMM SERIAL NUMBER REGISTRATION MARK 8 DESCRIPTION OF FLIGHT CUSTOMER DEMONSTRATION FLIGHTS 0 (GINce /appestat) FROM TO MA CEPARTURE DATE DURATION C CREW REQUITED TO OPERATE THE AIRCRAFT NC ITS EOUPMENT I I PROT I I CO-PILOT I I FLIGHT ENGINEER I I OTHER (Stec*) THE AIRCRAFT GOES NOT /MET THE APPLICABLE AIRNORTHINESS REQUIREMENTS AS FOL LONG. E. THE FC4.1.0WIM RESTRICTIONS ARE CONSIDEREDNECESSARY FOR SAFE OPERATION (Use Maammal ihmeisse00 F CERTIFICATION- I herite oewy 'hell in tie regstered yew lot Ns apse) cd 04.resnoca nocooreence wet Tile 49 et the Unto] Dais Cole44101ns are isle teethe/Ire Pleated to oteeiteemileed abHe.the Its matt is registered win OM F•cl•relkvikoct FASO MAMA RegAmene. enrol Ms Om applleatei were the impeded AM ni GATE NAME AND TITLE (Palls ME SIGNATURE z I i e 1 E li g ar i P. Ope• en, LII•Ulare aryl Mariam. n Domonce MN 14 PROT810 Seam 91 S. As AWLesbie G Stammered Conionney. FM Fan 8133-9 MRCP ofiefONAM0 H. rotor Alownhans Corthaan Ice linpri Altaall WI Sam legume) (# ad El CANON Omen, LeHalsze Mated 1 C DMA ONIRPOIL IFIKNOMM. eta (Mach Moe rented) 1 PreHme Aft*ITW011 Celicilt• loved n Ace:atria Win i4 PROT811 Realm 21.191 (a) cm IGATMAMICAM 1 0. Camel WADY end gatirce IrtanaboulmeetienAtaeli 1 /Map RES vd Atmekal. FM Fan 33T (MOM Men Amme) 1 J Drool Are:Moen Comma Issued c Moyearce VAT g id cm s law, 21.181 (a) Jeavyannfro 1 F TM niceceol Recerclia HAMM Ftezeds K tgle-SWI Anise 510~ 110 Germaine. FM Font 813045 (Mad% ..San Mtlia0) FAA Finn 130-6 WI 1) AI Previous EdOene Smpenaled Eletlttelie FORM -POE Page 2 d2 PROT490 EFTA 00241927 PROT102 SONY_GM_02755006 EFTA 00241928 PROT103 6Z6 I VZOCVJ..43 n rn 0 70 s moms...um Are Price Truincei N493LX 2 WillJFACTURER APO COIL Raytheon Aircraft Company 400A S SACRA*T SERA. Immo RK -244 FCAMORT ranspor t $ AuNow. MID asiliti ISSUMIC4 M Cn Downes anti. • dead James I tiSC SHIM woods Salae es ifisiaM bee east De termateat manlyo n= Yee ameba M M .I. Me iirelimat lob Ad en low 70 C Yes. Saw Is spa' a *Lipka, copra ea al *WM meas. MM AMT libruisigeM mon ea is sad Wm Wm, 410 to 'V 1O hopenc D3 70 GI ll 4 tOmi 70 US laninniadni Ewa Worm melirlo *sws od mein lamina Of edam isloWid brie Mit SWIMS eta in fddriwa sato M Masa ni I , note" Minim MINS* ay Mood I OATS OF ASS FM AMESENTAME. r 12/29 013 Arthur Ockwell (S. L E:R:83 '1394 E3RG L NI Ilingek gTelart V no el Ix cede,. onto waning a Ire ni tatIonlIthrryteirori tratibi 1 I'm no V3 IL Ma CtoriWn rep• (AMMO li T. Ulfflft P MIXIMIGICI YAM 00K NU 'ww arimougoamoia : 4 00 WTED STATES COMMA DEPARTMENT Of TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION * None * n qk PROT104 PROT491C6 ECTIVE ORDER PARAGRAPHS 7, 8 EFTA 00241930 PROT105 well, SUMS OFAMINO DEAurnaba OF TIWASPORTATCN • r [WM wATION..0ANSPIAnN SPECIAL AIRWORTHINESS CERTIFICA A CAT EGORYADESIGNATICO1 MILL PURPOSE RICE i a R. MAKS II/CURER ADDRESS ) C rimprr "lc" L.-. m D N- 493U( 1 SERIAL NO a_ MI BUILDER parthecn RYA E DATE OF ISSUANCE / 1, ET Ain I? 2)14 OPf. RAMS MIMI 8.20y PART OF DOS CERTICCATE bowknot cs is.* A. ciL. porno. .anima NO DIRTECCOML 0, ray be ?Ninnies ty • Int ns comas Si Ma CEPTSICAT E MAT DE PSPLAYE0 N NE A.OGRAFT 000C OF PCCEPAL PcouumoNs (on musr a no maks* - to 3 t.lw ) or int INS DANCE viini IOALS Mu U. Fee MiraPROT492 EFTA_00241931 PROT106 a et tat Nrellnist collate a sway*. ft mita* d Pa tat 1044 0 and Sin Co* RISC Jaya nu $4 CoO/Folocilastrnms OM B Thi arnitmss anksir uroctres pa eartacior named on PAO Masi WO RI Ora P°4"'" Wm*. "mot node, NO Ma d mu* wane as ire lb mai my =Psi ~at hp lesn ~as attune (l) Ct.n Want 00 OttearketerealnIMIto to Pv• eat M Caine'= as mutation • prom claw Vt. r Pis ancarn alibi, saves Ito 101 %sae .1 co r• Forme aft billion** Movie ill:t1A 0 Mt inotenms onion; cotes nen oflhe de desaiot ti aka/ le Sidi iss•Shis two twat) at b•el *ant IM imaffivelti time aka. CIA M nonfat /Op AUer•If PO riginnieti SIN arsacablecerramm .t sal orowierste cab as pegdernyAnt 84 ite Cawtoi Cu, .1scretrof Cm/ ANSA AV War may way in new.* tate. an f ihrinniC0 • PI npltiniceve we)te opOrAOS an am oscoreciam oh ancIttre eV laabens rani may a rooted by the him:Mx as col 5 Ws arida MOW sry bail cony aft/ IM (NOM pianism <Mir wanly E oris WSW lietwant lottps**1 a sad Nawing, att.* is Acne/ for Po data M WI • 0. i Ordttet• mooted al 14 UR. Pat 2f. Swoon 21 IV cr 21217 PROT493 EFTA 00241932 PROT107 RK 244 STC list (12-26-2013) Reference 8130-6: Application for Standard Airworthiness Certificate Transport Category, dated December 26, 2013 Reference section III owners certification ST02371LA: Replacement of Pratt & Whitney JT15D-5 series engine with Williams International FJ44-3AP engine (TCDS E3GL) with Full Authority Digital Engine Control (FADEC) and associated systems. ST10959SC: Installation of Rockwell Collins Pro Line 21 Electronic Flight Instrument System (EFIS) with Rockwell Collins FMS-6100, Localizer Performance with Vertical Guidance (LPV) approach capability and Universal Avionics System Company (UASC) Terrain Awareness Warning System (TAWS) ST03960AT: Installation of Aircell Axxess Cabin II Iridium Phone and High Speed Internet System with Wireless Local Area Network (WLAN), Astronics 115VAC 60Hz Cabin Inverter and Bonner LED Cabin Lighting System. ST01572WI: Installation of four (4) model 400A OEM seats, one (1) three-place divan, one (1) aft toilet, one (1) set of aft pocket door dividers, one (1) set of forward pocket door dividers and LED lighting. STC01794LA: Installation of Hawker 97650W0370 or 9750W0370-8 battery ST000812SE: Group airplane approval for Reduced Vertical Separation Minimum - (RVSM) PROT494 EFTA 00241933 PROT108 SDNYGNI02755012 EFTA 00241934 PROT109 26180 Colin Weighi Pathway 'Cleveland. Ohio 44143 W.703.2148 www.11ighlopiiontam December 26, 2013 Nextant Aerospace, LLC 355 Richmond Road Cleveland, Ohio 44143 Attention: James Immke Re: RK-244 - Agent Authorization To whom it may concern: aliLOptions This letter is to confirm that Flight Options, LLC ('FO's) authorizes Nextant Aerospace, LLC, as FO's agent, for a Beechjet 400A, bearing serial number RK-244 and FAA Registration Number N493LX (also identified as a "Nextant 400XT'), which is owned by FO, for any and all authorized FAA actions in regards to: Airworthiness Classification Experimental X Airworthiness Classification Standard Sincerely, Flight Options, LLC By: Michael Metera Vice President, Administration & Contracts --777,,46/-det occitted Si Aure Sian and Subsortbez1 4o me 4416 do,/ -z-c,c,c bectenber O.c 2ni h4 C•N'e.1.-,4246 tAelrere, • PROT495 EFTA_00241935 PROT110 SDNYGA0102755014 EFTA 0024I936 PROT111 PROT496 EFTA 0024I937 PROT112 PROT497 EFTA 00241938 PROT113 0 MAJOR REPAIR AND ALTERATION u S Cupeemni a TranneriallOn FokinaInlaillea Aderilalotralca sorra nocrored CMS Pro 21204020 iirsorsoca Stet:Ciente Tracking Number For FAA Us* Only INSTRUCTIONS' Pail Cr Nye am envies. See FAR 43.9. FAR 43 Appendix 8. ant/ AC 43.9.1 (or sut4equent revision thereof) for instrictora and clisposito of this form. This meat is required by bw (49 U S.C. 1421) Failure lo roped can result in a civil penalty not lo exceed 51030 f0r each Such NobiliCel (Section 901 Federal AMIlon Ad 1958) I. Aircraft etaboraley and Registration Mark N493LJ( Seel No RK-244 Make Model 400A Series 2. Owner Name (As shown on registration certificate) Address (As shown on tegiatrelion certificate) Imes 26180 Curtiss Wright PKWY city Richmond Haightc ea. OH a M14114/3 Caner Sap 4. Type 6. Unit Identification Repair Alteration UM tame weal Serial Number 0 CS AIRFRAME (AS desalt:media Rent f above) 0 O POWERPLANT MI O PROPELLER O O APPLIANCE Trap mrecreaser A Agencys Name and Address B Keg &Agency NOM Nextant Aerospace Meets 355 Richmond Road Cm Cleveland ea. OH Al 44143-1453 cowry USA O U.S Certificated mechanic O IManulacturer O Foreign Centfecared Mechanic C. Caleicale No. Lil Certificated Repair Station CRS # 25NR667B 0 Generated Maintenance Otani/seen 0. I Certify that the repay and/or meraton made to the und(s) Moaned m tern 5 above and described On the reverse or anachrnents hereto have been made in accordance with the requirements 01 Part 43 ol the U.S. Federal AWMkin ReguYekris and that ale MIcanaton Extended range hat per I 4 PROT812 Part 43 Ama. 6 0 Signature/Oa A.Ockwell Signature/Oats of Authorized individual ki.. 05/30/2013 7. Approval for Return to Service Pursuant to the authority given persons penned hams the unn Menhfred Aare:strata of Me Federal Aviabon Adrnmiseatoon and 4 m item 5 was inspected Into manner presented by the AlJeFt0YED 0 REJECTED FM FP Standards Inspector Manufacturer Penal APOroved by Canadian Department ol Transport BY FM Designee X Repair Staten Inspection Au Other (spew izaton c.a.:hie." Dempster., No CRS # 25NR6678 SignaturetOale of Authorized Mdiddual A.Ockwell 05/30/2013 eeeAL FAA Form 337 (7006) PROT498 EFTA 00241939 PROT114 PROT499 EFTA 00241940 PROT115 NOTICE Weight and balance or operating Ametation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with ad previous alterations to assure continued conformity with the applicable airworthiness requirements. Of more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) N493LX Part I of 3 The Following Equipment was removed along with Associated Hardware. 05/30/2013 EFD-871 622-9345-203 Electronic Flight Display EFD-871 622-9345-203 Electronic Flight Display MFD-871 622.9434-213 Multi Function Display ICU-85 622.6189.002 Internal Compensation Unit ICU-85 622-6189-002 Internal Compensation Unit AHC-85E 622-9336-400 Attitude/Heading Computer AHC-SSE 622.9336-400 Attitude/Heading Computer SDU-6408 622-9735-001 Sensor Display Unit SDU-6408 622.9735-001 Sensor Display Unit DCP-5O0O 822-1028-011 Display Control Panel DCP-5000 822.1028.011 ARP-851 622-9500-011 Altitude Reference Panel ARP-851 622-9500.011 Altitude Reference Panel AAP-851 822-0328.011 Altitude Awareness Panel AAP-851 822-0328-011 Altitude Awareness Panel CHP-850 622-7397-002 Course Heading Panel D8U-4100 822-0014-002 Data Base Unit DAU-650 622.9344-101 Data Acquisition Unit SOD-640A 622.9347-001 Sensor Display Driver IOC-4000 ( 4) 622-9814.514 Card Assembly MDC-4000 622-9818-751 Maintenance Computer CSU-4000 (2) 822.0049-002 Configuration Strapping Unit FMC-5000 (4) 822-0891-008 Flight Management Computer PWR-4000 (4) 622.9945.021 IAPS Power Card GPS-4000 822-0931-003 GPS Receiver Mounts 622-9430-002 EFD /MFD Mounts EFB Electronic Flight Bag Mounting E Additional Sheets Are Attached Date Form 337 oci-osi PROT500 EFTA_00241941 PROT116 PROT501 EFTA 0024I942 PROT117 NOTICE Weight and balance or operating linwtation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with ell previous alterations to assure continued conromtity with the applicable airworthiness requirements. (If more space is metered attach additional sheets. Identity with aircraft nahenalety and registration mark and date work completed) N493LX 5/30/2013 Page 2 of 3 Installed the Following Equipment along with Associated Hardware. Date Model Part Number Description Weight Arm CCP-3000 822-1746-002 Cursor Control Panel 2,60 90.0 CCP-3000 822.1746-002 Cursor Control Panel 2.60 90.0 DCU-3001C 822-2362-003 Data Concentrator Unit 5.0 325 DCU-3001C 822-2362-003 Data Concentrator Unit 5.0 325 ECU-3000 822.1200-209 External Compensation Unit 0.40 57.5 ECU-3000 822-1200-209 External Compensation Unit 0.40 57.5 FSU-5010 822-1543-101 File Server Unit (1." IFIS) 6.5 60.83 ECU-3000 822-1200-998 File Server Unit (1st IFIS) 0.40 57.5 AFD.3010E 822-1753.416 Adaptive Flight Display 12.90 89.2 AFD-3010E 822-1753-416 12.90 89.2 AFD-3010E 822-1753.416 12.90 89.2 AFD-3010E 822-1753.416 12.90 89.2 IMT-3010 822-1140-401 AFD Mounting Rack 4.40 85.0 IMT-3010 822.1140-401 4.40 85.0 IMT-3010 822-1140-401 4.40 85.0 IMT-3010 822.1140-401 4.40 85.0 10852801Y00 Fuel Quantity Conditioner 0.90 324 PC920.2A2000PH-2A1 Fuel Flow Conditioner 1.10 325 GPS-40005 822-2189-004 GPS Receiver 6.0 37 Cl 429-410 GPS Antenna 1.0 166.14 Amp Cluster N241100-002 DC Voltmeter 1.5 97.4 [SSN REDACTED]-1 Speed Switch (2) 0.25 89.2 DBU-5010E 822-3000.202 Data Base Unit 1.60 134.5 P5-8350 501-1228-004 Power Supply 12.5 52.9 MMT-5000 822.1811.003 File Server Unit Rack 0.30 57.5 MMT-3010 (2) 822-1290-003 AHS Mounting Rack 1.80 57.5 XM WR-1000 822-2031-002 XM Weather 1.5 41.0 CHP-3010 822-1280-003 Course Heading Panel 1.30 92.5 OCM-4100 822-1463-228 Options Configuration Module. WAAS/LPV 0.30 57.5 Options Configuration Module. OCM-4100 822-1463-228 0.30 57.5 WAASAPV Additional Sheets Are Attached Form 337 ('006) PROT502 EFTA 00241943 PROT118 PROT503 EFTA 00241944 PROT119 NOTICE Weight and balance or operating limitation changes shall be entered M the appropriate eimme record. An alteration must be compatible with all previous alterations to assure continued conformdy with the applicable airworthiness requirements (II more space is required. attach additional sheets. Identify with aircraft nationably and registration mark and date work completed) N493LX 05/30/2013 Page 3 of 3 Date Model Part Number Description Weight Arm CSLI-4100 (2) 822-1364-002 Configuration Strapping Unit 1.60 55.7 MDC-3110 822-1987-006 Maintenance Data Computer 0.80 55.7 FMC-6000 (2) 822.0868-123 Flight Management Computer 1.90 55.7 ADC-850D (2) 822-0389-468 Air Data Computer 5.30 60.83 ANC-3000A (2) 822-1378-001 Attitude Heading Computer 4.80 57.5 DCP-3030 (2) 822.1828-002 1.90 89.96 PWR-4000 (4) 622-9945-022 IAPS Power Card 1.3 55.0 IOC-4100 (4) 822.1362.511 Input/output Concentrator 0.8 55.0 LT-4001-010 Master Caution Panel 1.3 87.0 Rev. Panel [SSN REDACTED]-1 Pilot Reversion Panel 0.2 88.0 Rev. Panel 373-91.3203.3 Co-pilot Reversion Panel 0.2 88.0 9-PED [SSN REDACTED]-9 9-Pedestal Panel 1.8 92.89 345-6196 ELT Switch 0.2 88.0 Annunciator Led-42-12-BB-E0Y47 AUX BATT (1/2) Annunciator 0.05 88.0 Annunciator (2) Led-40-18-BB-EOY4S Pull Up/ Terrain Annunciator 0.05 88.0 Annunciator 2-F840231 Terrain Inhibit/ Terrain Fail 0.05 88.0 In Accordance with STC 51109595C. See Attached Copy AFM Supplement, Nextant Aerospace Doc. No. [SSN REDACTED] Rev IR Dated 09/02/2011 or later FAA approved revision, installed on Aircraft. Equipment Pilot Guides are Installed in the Aircraft as Portable Document Format (.pdf) via supplied I-Pad. NOTE: Portable electronic devices used to store required aircraft records required by Part 91.9 are considered Electronic Flight Bags (EFB) per FAA Advisory Circular AC 120-7613 par 4-g. Commercial operators are required to obtain authorization for their use from their managing Flight Standards District Office. Instructions for Continued Airworthiness (ICA) Ref Nextant Aerospace Document 373-00.0002.Rev C or Later are included in the Aircraft Maintenance Records Carried out System Ground Test Plan IAW Master Drawing List (MDL) 373-00-004 Rev C. Carried out Hawker Beechcraft Service Bulletin 34-3431 Reduced Vertical Separation Minimum (RVSM) Airframe inspection / Modification. Performed FAR 91.411Inspection per Part 43 appendix "E" Pitot Static & FAR 91.413 Inspection per Part 43 appendix "F" Transponder System checks. Form 337 O0-06) PROT504 EFTA_00241945 PROT120 PROT505 EFTA 00241946 PROT121 *Web 'hats el jlonerica !apartment of transportation -- 311eheral "thintion Pibministration $upplemental 'Type Certificate emteimersettiststeeek A140924" ST10959SC 26180 Curtiss-Wright Pkwy. Richmond Heights, OH 44143 araAidasa46411549th elA *MI iteeithA• ayeereerthnteddelaVa '01•7414M104442.0'etha.•a01 014•01 lefe fni•en IMMO ka efthreeed(thAV PrIthrneaa IAA( 25 944 Federal Aviation $801w4.64su (Sec Pages 3 and 0 for complete certification basis.) CarraePendant. gon..14:.;,44a,b.Z...14.. A 6SW Hawker Beechcraft Corp. sg,i,z 400A nuorares tsars frArs glair Installation of Rockwell Collins Pro Line 21 Electronic Flight Instrument System (EFTS) with Rockwell Collins FMS-6100, Localizer Performance with Vertical Guidance (LPV) approach capability and Universal Avionics Systems Conically (UASC) Terrain Awareness Warning System (TAWS) in accordance with Nextant Aerospace LLC Master Drawing List Doc. No. [SSN REDACTED] Revision W, dated March 29, 2012, or later FAA approved version, Snider/ n) cad wasa•us: 1) The installer must determine whether this design change is compatible with previously approved modifications. 2) If the holder agrees to permit another person to use this certificate to alter a product, the holder must give that person written evidence of that permission. . 3) For aircraft equipped with Pratt & Whitney JT15D Engines FAA approved Airplane Flight Manual Supplement, Nextant Aerospace LLC Doc. No. 373.00.0008 Revision IR, dated 10/19/2009, or later FAA approved version, is required on board the modified aircraft. ow/ ee- an.,.-4," dale Gate <4. ?ewe A- eyfrawrzteOtsenesta'v .16,c 4 nyydnels, a kanandava dart a ediearaw euknetawled4 ae. ..45dataadak..- ,97niearl. 4veram ./Inteakaatadase. giaernAarioaaaa' ..fune 26, 2008 ff trie nhaenana October 19.2009 .fiteeteeseaned giek cotioneree September 26, 2011; April 05, 2012 n-s e) Steven L Langnois mrrater. Systems and Flight Test Mach Chicago Airenft Certiliestien Office Ink) Oe or taleettis • la pi • try* cane e r. ncl n ..%e. ar aapt newne nnl no MP • or awn. l'AA Min 11.110.2120.4111 PAU 2 et 4 PULS nal terelliC•10 Sky b• transit vied Je acteraerte• oat. /AR 27.41 PROT506 EFTA 00241947 PROT122 PROT507 EFTA 0024I948 PROT123 3!Initeb filtehe of cAnterics !epnrhnent of Zgranspurtation - rebernl jthintion Abministration $upplententai Zurre Tertiftrate ((continuation *lee° ifi randee STI0959SC §42.44v5.4.ukynen. October 19, 2009 Date Amended: September 26, 2011; April DS, 2012 -Weedlohivw onaniAndthAw tervskaasei: 4) For aircraft equipped with Williams F344-3AP Engines, those engines must be installed under STC ST02371LA. 5) For aircraft equipped with Williams F144.3AP Engines FAA approved Airplane Flight Manual Supplement, Nextant Aerospace LLC Doc. No. [SSN REDACTED] Revision IR, dated September 2, 2011, or later FAA approved version, is required on board the modified aircraft. 6) Aircraft must have previously qualified for Operations in Reduced Vertical Airspace via: RK-I thru RX-I 17 and R.K-I 19 thru RK-139, Hawker Bcecheraft Service Bulletin No. 34-3431. RK-I IS, RK-I 40 thru RK-224, Hawker Beechcraft Service Bulletin Nos. 34-3228 and 34-3431. RC-225 thru RK-299, Hawker Beechcraft Service Bulletin No. 34-3431. RK-300 and after as original equipped from Hawker Beeclicraft. 7) For aircraft equipped with Universal Avionics Systems Corporation (UASC) TAWS FAA approved Airplane Flight Manual Supplement, Nextant Aerospace LLC Doc. No. 373.00.0036 Revision IR, approved March 28, 2012, or later FAA approved version, is required on board the modified aircraft. 8) For aircraft with Collins Proline 21 FMS-6100 LPV Approach enabled FAA approved Airplane Flight Manual Supplement, Nextant Aerospace LLC Doc. No. 373.00.0032 Revision IR, approved March 28,2012, or later FAA approved version, is required on board the modified aircraft. V:-.-.4Aeway, Based oil 14 PROT813 §p I.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Hawker Beechcraft 400A aircraft is as follows: a. The type certification basis for the Hawker Beechcraft 400A aircraft is shown on TCDS A IGSW for parts not changed or not affected by this change. b. The certification basis for the parts changed or affected by this change since the reference date of application, September 29, 2009, is based on TCDS A1GSW and §§ 14 PROT814 Part 25 as shown on page 4 of 4 of this STC. Any ccccccc Jon of (Ala csitIllen• Is puniseable by I floe of nee •ryncueq si.000. of INICI tamen net eoceetting S years. ar bets. IAA IOU 4110.1.1.10•601 mos I or I Nan MTh C•It4flontip soy b ccccc non, In acre/donne eJ I AS SI.ci. PROT508 EFTA 00241949 PROT124 PROT509 EFTA 0024I950 PROT125 /AtlikJ $1alco of America pepartment of Zumaportntion - Aeberal Ablation Abministration Supplemental 'Type Tertificate (aantinuation *pet) ,9404 eihwasot October 19.2009 Date Amended: Sep:ember 26, 2011; April 05, 2012 Based on 14 PROT815 §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the baseline Installation of Rockwell Collins Pro Line 21 Electronic Flight Instrument System (EFTS) with Rockwell Collins EMS-6100 modification was detennined to be TCDS A16SW and the following later regulations: Am& [244) 25.771 (a,c) Amdtl25.23J 25.301:25.303:25.581; 25 607: 25.611. 25.773 (0)(1)(2Xd) Amd1.125-38) 25.1309 (aXti)(c)(6XeX8): 25.1322 Amck.[25.401 25.901 (b)0X1); 25.1549 (a)(9)(e) Amde[25.41) 25.1321 (a)(b)(c)(c): 25.1331:25.1333 Amdi.(25421 Anich. [2546) AnWt[25.541 Amde[25-72) Amdt.(25-80) 25.1501 25.603:25.605: 25.613; 25.1529 25.307; 25.571, 25.1307 25.1316 25.1329(h) (c)(c); 25.1351 (a)(1Xd): 25.1381; 25.1521 (.)(c); 25.1543 (b): 25.1581: 25.1583 (a) Arndt [2546) Andtt25.90) Am01.12541) Amdel25-102) Arm:X(2510g 25.305 25.1303 25.561 25.981 (MXb) 25.1585 (a) Amdi.(25-108] Amt11[25-109) Amdt[25.113) Aindel25-1221 Amdl.(25.123J 25.1325 (d) 25.1323 (a)(1)(g) 25.869 (a)(4); 25.1431 25.1317 (a)(b)(c) 25.1353 (axc) Based on 14 PROT816 §§ 21 Mend 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Collins Proline 21 FMS-6100 with LPV Approach enabled and UASC TAWS was determined to be TCDS A I6SW and the following later regulations: Arndt (Ckinjnall 25.601. 25.605, 25.609. 25.613.25.1301. 25.1357, 25.1381. 25.1525, 25.1541, 15.1581 Amdi [24-4) 25.771 (a) Amd1.(25-23) 25.301; 25.303; 25.305, 25.307.25.561(c); 25.607; 25.611, 25.1307 Amcti.)25-311) 25.603, 25.1322. 25.1583(0 Amdt.(25-40) 25.1585 (a) Amdt[25-41) Arndt [2542) Amdt(25-46) Amei.D5.54J Amdi 125.72) 25.1309 (aX8)(cXdXe)(8) 25.1501 25.777(aXc) 25.1529 25.869(100) 25.1351 (aXI) Amdl(25.102J Amdt [25-1131 Amdl.[25.123J 25.9111(aX17) 25.1431(a) 25.1353 (axc) -END. Any *Icon el at Rh pia/ ln.alt OY a SO !1.000. w 1ptlfors a. net *scowling 1 yens, o• btn. FAA rom 411.0.1•141.4.44) Plea 4 44 4 Plat mt. cocci OW* .. y be ceenteistd in •ccorame nth IAA 21.0. PROT510 EFTA_0024 195 1 PROT126 PROT511 EFTA 00241952 PROT127 a MAJOR REPAIR AND ALTERATION us twormonter (Airframe, Powerplant, Propeller, or Appliance) nameenown Fowl Worn MOW 2120-0)10 it/WV/COT Electronic Tracking Number For FM Us* Only Fats mutton Arenaunmen INSTRUCTIONS: Print or type all entries. See FAR 439. FAR 43 Appendix B. and AC 439.1 (or subsequent reviler, thereof) for insPucticas and disposalo al tlis Semi This meet is required by law (49 PROT817. 1421). Failure to report can result Macaw( penalty not lo emend $1.000 for each such riolallon (Section 901 Federal MAMMA Act 1958) 1. Altera Nations* and Recta/aeon Mark N493LX Serial No. RK 244 Make Model 400A Wes t. 0*.,.. Name (As shown on Mentionwocellitere) Address (As shown on rIgiStainOn cernIOSIO) Awns. 26180 Curtiss Wriaht PKWY ON Richmond Height% Ram OH zo 44143-1453 Cann M 4. Type 5. Unit Idendfleadon Repair Alteration Unit Matte Model Serial Number 0 S AIRFRAME (As 00020 in nem I above) 0 POWERMANT 1:1 o PROPELLER O O APPLIANCE Tan renreeLre A. Agency's Name and AddreSS B K nd of Agency tame Nextan1 Aerospace Adenns 355 Richmond Road City Cleveland hare OH zp 44143-1453 ceralay USA 0 us Certificated Mechanic 0 I Maniiacturcr 0 F"epn Certificated Mechanic C Cenacee No Ili) Cenilicared Repair Station CRS it 25NR6678 0 Cenificated Maintenance Organitabon 0. I cenifirilhaf the teen and/or alteration made to the unt(s) dentified in hem 5 above and described on the reverse or allacliments hereto have beam made in accordance with the requirements ei Pan 43 of the V.S. Federal Aviation Regulators and that the information furnished herein is true and correct la the best of my knowledge. ExtendedfR range NM et II p C Pane App. Ei 0 Sitnature/Dale of Authorized Individual (.1' 05/30/2013 Pursuant to the authority given perscos weaned woe. the unit c'lentate4 in item 5 was inspected n the manner rammed by the Administrator of the Federal Aviation Adnimsbatkin and Is ®APPROVED 0 REJEC7E0 BY FM FR Standards Inspector Manufacturer Maintenance OrganistPoser. Approved Of Candi:tan Department of Transport FM Designee X Repair Station Inspect-on Auttorizaeco Cerblatte Or CRS # 25NR6678 Manalure/)ate of Authonzed Mai dual II 05/30/2013 ..ckulk FAA Form 337 pooh PROT512 EFTA_00241953 PROT128 PROT513 EFTA 00241954 PROT129 NOTICE Weight and balance or operating limitation changes shall be entered in the 8POrnenale olltren record. An alteration must be compatible with a# previous alterations to assure continued conformity with the applicable aitworthineSSreqUireMenit (If more space is (required attach additional sheets. Identify with aircraft nationality and registrabon mark and date work completed) N493LX Nextant Aerospace Completed STC # 5102371LA Removed Pratt and Whitney JT15D-5 Series Engines . 05/30/2013 Date Installed the Williams International 1J44-3AP Engines with Full FADEC and Associated Systems in accordance with Nextant Aerospace MDL -NXT-001 Rev IR Dated 08/22/2011 or later FAA approved revisions, and FAA Approved MM Supplement NXT-1-AFMS Rev IR dated 9/15/2011 of later FAA Approved revisions. Installed Left Engine Part Number. 111000-202 Serial No. 252757 Installed Right Engine Part Number 111000-202 Serial No. 252758 ICA AFM Supplement was installed on Aircraft. Nextant Aerospace Instructions for Continued Airworthiness Document NXT-ICA Rev IR or later FAA accepted revisions are included in the Aircraft Maintenance Records. Carried out Engine Ground Runs and System 0PS checks IAW Ground Test Plan [SSN REDACTED] Rev F. End K Additional Sheets Are Attached FAA Form 337 06667 PROT514 EFTA 00241955 PROT130 PROT515 EFTA 00241956 PROT131 e3tniItbfrIolte431,f1intricn Xlepartmcnt of Zrattspartntiatt - gebentI ?britiniatrn lion $upplententat Type Certificate Ata02,e" ST0237ILA Me6lograsatura Nextant Aerospace, LW 26180 Curtiss Wright Folkway Richmond Heights, Ohio 44143 cre4egveathatenti Pie 44(f/fin aniOnAraryiegervivivemotativa de intrZahew endeeteedfaivar //levey4. to- regfecatteea men* arrow/Strew eeyeti3ceetwiCi aunt 25* Var. givaireavaeheva "Berdttiti lea t. *Certification basis is set forth on TCDS A I6SW and continuation sheets 3 and 4. (gril;metarsene col Ifenpfera4vilc A I6SW desed": Hawker BeechcraR ..sgeeles, 400A taVere?-4 1.91". 93kter Virverpt Replacement of Pratt &. Whitney ITI5D-5 series engine with Williams International FI44-3AP engine (TCDS E3GL) with Full Authority Digital Engine Control (FADEC) and associated systems, in accordance with Nextant Aerospace Master Drawing List No.: MDL-NXT-00I, Revision RI. dated 8/22/2011, or later FAA approved revisions and FAA Approved Airplane Flight Manual Supplement, NXTI.AFMS, Rev TR, dated September 15, 2011 or later FAA approved revisions. Nextant Aerospace, LLC Instructions for Continued Airworthiness document NXT I -ICA, Revision IR, or later FAA accepted revisions must be provided with this STC. Smiamwo widie,w424heiv.. The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of that aircraft. The approval of this modification applies to the above-noted airplane models only. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. (CONTINUED on page 3) eetiOak mniedci strav4ilys dace reditheeli eteyf eyyteeevriatmencvat:s Sid untie swarmed-ma( !keret:1e I erwAireacv• a fentreiraieen th eatereirao adertfAirea ..4dettio0trate, onto rnerettavetheta ..346633theakalleer OitotAr genakit. March 24, 2008 91.4,04:uffeme0.. September 27, 2011 Act )6) erraktoil.. gl""greble#1:. tkiliye/e neriCilevier Pgrowstret Manager, Propulsion Branch Los Angeles Aircraft Certification Office (Title) /toy afreterion of lick cceilicore LI pinia6a6k 6y it fin of mot 'wrote 61,004 or nerfromerar Ira ttnertaitil 3 yen, or &HA VAS riPlIR 6110,2(10.G1) Pogo t el • Oho tenfrtatemay& icearfrtreif aeromOitre il6 file:221.47. PROT516 EFTA 00241957 PROT132 PROT517 EFTA 0024I958 PROT133 INSTRUCTIONS: The transfer endorsement below may be used to notify the appropriate FAA Regional Office of the transfer of this Supplemental Typc Certificate. The FAA will reissue the certificate in the name of the transferee and forward it to him. TRANSFER ENDORSEMENT Transfer the ownership of the Supplemental Type Certificate Number to (Warne of transferee) (Rana of trantftd 6.484fromfaita) OA Pat, t. roe) from (Aran of grantor)(Tritit or type) Winn °fatalism) (Mager oaf sirte) Ogee.% swanned° Extent of Authority (if licensing agreement): Date of Transfer: Signature of grantor (In Fage2 of PROT518 EFTA 00241959 PROT134 PROT519 EFTA 00241960 PROT135 guitar Pates OH Sumac.' Pepurtment of ¶rnnaportution - greberal Ablation cAhntittiotrntioxr $upplemental 'Type Tertificate (gatitinuation Sheet) Afe.eei24, ST02371LA Sem%haw atm./Wean/draw loonanataii • Nextant Aerospace, LLC, "Installation of Rockwell Collins Pro Line 21," Amended STC STI0959SC, dated September 26, 2011 or later FAA approved revisions is required as part of this alteration. The new Vmca and Vmcg values are 94 KIAS and 93 KIAS respectively. The new engine minimum rated thrust is 3,031 lb at sea level, flat rated to an ambient temperature of 77°F. Approved engine fuels are: Grade Specification Jet A ASTM-D 1655 Jet A-1 ASTM-D 1655 ntlelicandiroaiew.4 The certification basis for this modification is as follows: The original certification basis for the Hawker Becchcraft Model 400A airplanes identified on TCDS A I6SW, Revision 26, dated March 17, 2010: Part 25 of the Federal Aviation Regulations effective February 1, 1965, as amended by 25-1 through 2540, plus §§ 25.1335, 25.1351(d), 25.1353(c)(5), and 25.1447 of Amendment 25-41; §§ 25.29, 25.255, and 25.1353(cX6) of Amendment 25-42; and §§ 25.361(6) and 25.1329(h) of Amendment 25.46. Part 36 of Ihe Federal Aviation Regulations effecliye December 1, 1969, as amended by 36-1 through 36-17; SPAR 27 effective February 1, 1974, as amended by 27-I through 27-5; and Special Conditions No. 25-ANM-32 dated February 22, 1990 (High Altitude Operation at 45,000 feel), and Special Conditions No. 25-ANM-33 dated June I8, 1990 (Lightning and Radio Frequency Energy Protection). (See NOTE 12) Equivalent Safety Hans: (I) Out.ottrim characteristics § 25.255 (2) Pilot compartment view § 25.773(b)(2) (3) Passenger compartment door § 25.813(c) (4) Emergency exit nnrking §¢ 25.81 l(dXI) and 25.811(d)(2) Application for amended Type Certificate dated February 18,1988. Regulation at a later amendments for components and areas affected by the change (Ref. FAA approved Compliance Check List): Subpart A - General : 25.2(25-99) Subpart B - Flight: 25.207(25-121), 25.255(25.42) Subpart C - Structure: 25.571 (25-96) Any damning El 14it rmfreate 4 Janata& by a As of riot earenang Boa or isopttoemini mm tureing J pan, or firll IM ono 020.2110.40 rya 3 Of 4 IfinerrtOrate may de transftrmf acconfanottath CAt21.47. PROT520 EFTA 00241961 PROT136 PROT521 EFTA 00241962 PROT137 pullet' "Malta (91 Aim Its Peparfaunif of Igrmusporintion - geberni c&bintion cabininistratinit $uppiemental ZUgpe Certificate (Gffontinuation Atet) ireuniee ST02371LA 51,444:.samSas4/conkrae.(1 Subnart D- Design and Construction: 25.603(25.46), 25.605(25.46), 25.611(25.123), 25.613(25-112), 25.625(25.72), 25.832(25.72), 25.863(25-46), 25.869(25.123), Subpart E - Powernlant: 25.901(25-46), 25.903(25-100), 25.951(25.73), 25.961(25.57), 25.981(25.125), 25.994(25-57), 25 997(25-57), 25.1013(25-72), 25.1019(25-57), 25.1021(25.57), 25.1043(25-42), 25.1045(25-57), 25.1091(25-100), 25.1093(25-72, 25.1103(25-46), 25.1141(25-115), 25.1143(25-57), 25.1163(25-57), 25.1165(25-72), 25.1181(25-115), 25.1183(25-101), 25.1185(25-94), 25.1189(25-57), 25.1195(25-46), 25.1203(25-123), 25.1207(25-46). $ubnart F - Equipment; 25.1301(25-123), 25.1305(25-115), 25.1307(25-n), 25.1309(25423), 25.1316(25-80), 25.1317(25-122), 25.1321(25-41), 25.1331(25-41), 25.1351(25.72), 25.1353(25-123), 25.1357(25-123), 25.1381(25-72), 25.1431(25-113), 25.1438(25-41), Subpart G - Oueratina Limitations and Information: 25.1501(25.42), 25.1521(25-72), 25.1527(25- 105), 25.1529(25-54), 25.1543(25-72), 25.1549(25.40), 25.1551(25-72), 25.1557(25-72), 25.1581(25-72), 25.1583(25-105). Subpart R - Electrical Whine interconnection Systems 25.1701(25-123), 25.1703(25-123), 25.1705(25-123), 25.1707(25-123), 25.1709(25-123), 25.1711(25-123), 25.1713(25-123), 25.1715(25-123), 25.1717(25-123), 25.1719(25-123), 25.1721(25423), 25.1723(25-123), 25.172.5(25423), 25.1727(25-123), 25.1729(25-123), 25.1731(25-123), 25.1733(25-123). 14 PROT818 Part 34 (34-3): 34.11 14 PROT819 Part 36 (36-28): 36.1--36.7, 36.101-.36.105, 36.1501, 36.1581. The following Nextant Aerospace Continued Airworthiness Supplements are applicable to airplanes modified in accordance with this STC: • Master Minimum Equipment List document No. MMEL Rev. 8, dated 02/21/2011 or later FAA approved revisions. • EWIS (Electrical Wiring Interconnection Systems) Inspection Procedure/Report No. NXT1-EA-007 Rcv A dated 8/24/11 or later FAA approved revisions. flay diennioo of t44 anifteato is yriatiba6ii 6y a fine ewe twafio, $1300, or hopthoowoot NO4 midi"), 3 part or 6014. FM Piro 1110.2114-GGI n. a 4 Oinatrscotemay6ornouforreintercon4otelooliimnoz PROT522 EFTA_00241963 PROT138 PROT523 EFTA 00241964 PROT139 0 MAJOR REPAIR AND ALTERATION ki.9 agermentor (Airframe, Powerplant, Propeller, or Appliance) trangalalite Frn APWOMIO cum go 21204:020 II, Elected:et Tracking Number Fid401 ASPIMM Kedmoriden INSTRUCTIONS: RIM or type as entries See FAR 43.9. FAR 43 Appendix B. and AC 43.9-1 fee subsequent revision thereof) foe instruction and dieddiaCel 0 Mg Rim TM repOrt IS required by taw (49 PROT820. 1421). Failure to (Open can reseal mauve penally not to exceed SLOCO for eaCC Such MNItkon Minion 901 Federal Aviation Act 1958) i Ad reel Nakinally 80day:43600 ,4am N493LX Sinai No. RK 244 Make Model 4OOA Series 2. owns Nero (As shown on tegisre aeon ceingage) Address (As shown on registration certificate) memos 26180 Curtiss Wrieht PKWY cry Richmond Heiehte sew OH ze, 44143-1453 county LIbia 4. Type S. Unit MeMllication Repair Alteration Unt Make Model Serial Number r AIRFRAME (As descnbed in Item 1 above) O O POWERPLANT 0 O PROPELLER lE1 El APPLIANCE r ype maroaavo. B K nd of Agency 111~ Wotan( Aerospace Adam 355 Richmond Road Coy Cleveland den OH re 44143-1453 Cony USA 0 U S Certificated Mechanc 0 i Manufacturer 0 Foreign Certificated Mechanic C Certificate No El Cogitated Rebate Station CRS # 25NR6678 0 Certificated Maintenance Organization D. I certify that me repair andor aeration made to tne unites) identified In item 5 neve and described on the reverse or attach:roots hereto nave been made h acccedance with the requvements of P ri 43 Of Ito U.S Federal Aviation Rogialicns and that the information furnished herein a true and comely:. the best of my knowledge Air PROT821 Pan 43 Extended range fur APR B 72/292013 Signature:Date of Authorized Ircligdu r ,.."1 7. Approval foe Return Pursuant to the loth:fey given person; Spedtled Wog. the unit idettled Admiritarate Of the Federal Aviation Administration and is O:C in fern 5 was inspected In the manner presets by the APPROVED 0 REJECTED BY FAA Fit Standards IMpeCler tilanklecturer Person Approved by Canadian DepartmeM of Transport FAA Designee X Repair Station inspeebon &Swingle° Other Morel CetifiCate co Designs:Om No. CRS* 25NR6678 SignatureiDale of AlAhorived Individual 's 12/29/2013 FM Form 337 0040 SONY_Gt4_O2755O43 EFTA_00241965 PROT140 PROT524 EFTA 00241966 PROT141 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous afterabons to assure continued conformity With the applicable airworthiness requirements (If more space is required. attach additional sheets Identify with aircraft nationably and registration mark and dale work completed) N493LX Nanonality and Registration Mark 12/29/2013 Date Installed the folowing InFlight Entertainment System in accordance with STC # ST03960AT and in accordance with Nextant Aerospace Master Drawing List DB1002067. Revision F.05 Dated: October 9, 2013. Installed Bonner Cabin LED Lighting System without the Venue System in accordance with NX330-1304002. Rev B Dated October 17, 2013. Ref. drawing for parts list. ICA Requirements. Ref FM Order 8100.17 Page 7.5 and 7-6 Use FAA publications such as AC 43.13-1, Acceptable Methods, Techniques, and Practices - Aircraft Inspection and Repair, and AC 43.13-2, Acceptable Methods, Techniques, and Practices - Aircraft Alterations; part 43 appendix 0, or other applicable aviation standards. Installed Iridium Sat Comm (Cockpit Phone only) and Broadband Internet System with Aircell Axxess II and ATG 4000 in Accordance with DB 1001013. Rev E ICA for Aircell System Ref to Nextant Aerospace Document No 081105003. Rev A dated September 22 2011 or later FM Accepted Revisions The following manuals contain complete detailed maintenance instructions and should be consulted for all maintenance activities not covered within this ICA: Aircell Axxess II Installation Manual 012004 Revision E, dated March 2010 or later applicable revision Aircell ATG-4000 Installation Manual 013485 Revision B Dated November 2009 or later applicable revision Aircell Axxess II WLAN AFM Supplement 061002072 Rev IR dated March 22 2012 for the has been Installed in the AFM Installed the Astronics DC•AC 115 VAC Power Supply in Accordance with D81002067 Rev F.04 Dated 10/9/2013 This is Located under the Seat Divan ICA for Astronics 115 VAC Cabin Inverter Ref to Nextant Aerospace Report No DB1108018 Rev IR Date 9/22/2011 or later FAA Accepted Revision. Aircraft Flight Supplement DB1109012 has been installed on the Aircraft See Current Weight and Balance Dated: December 29, 2013 End K Ado it anal Sheets Are Attached FAA Form 337 peoc, S ON Y_GM_02755045 EFTA_00241967 PROT142 A. PROT525 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 1 EFTA 0024196% PROT143 Uniith Slates of cRourica pepariment of ffiranoportation geberal (Ablation Pministration $upplemental Egpe Tertificate at) nr/Oivele impale ST03960AT Nextant Aerospace LW 3800 Southern Blvd. West Palm Beach, FL 33406 err//4' aline/:4 nivasse Or 4n touroer Aleve4entrekt/ tr•dr /4 ttro44/4ved nanfernalhirn den/te +neeArtienen at r/.' rtn;WellitineJJ nrithontnal r/ fikne25 r//4 Federal Aviation :iayskaivna. 65,-,frewnegAnket. jen rievolva, Aantrew Al6SW .414.9,4 Hawker Beechcraft Corporation ...eeevr-ae, 400A lotunfo/Arn r/rvfie lawiter War.. Installation of Rockwell Collins Venue In-Flight Entertainment(IFE), Airccll Axxess Cabin II Iridium Phone and High Speed Internet System with Wireless Local Area Network (WLAN) Astronics 1 I SVAC 60HZ Cabin Inverter, and Emteq LED Cabin Lighting System in accordance with Nextant Aerospace LW, Master Drawing List D131002067, Revision E, dated January 26, 2012, or later FAA approved revision. envana4M-en.. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determine by the installer that the interrelationship between this change and any other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. at) en-44, t4P wain!, Jerneelekp dant fritiMetz; f:va)Aertaternts/VW/ernefftio 44/ win/ ,intweetteerri Jenierrornevi reve'neere re kniniverhivit eler* elienrae Nien(Avieelify .4.4e4reWerekt- V/4 '..7v/ /Al • / • /te/ • )/ /' 26.74. r/I:v/re;:vileew July 28,2012 t':Gt/e tyle).iteortm• March 22, 2012 fay* erniareene.• a' rle tante/hien, tfteet.)/erf4-,- nl Melvin D. Tay Manager Atlanta Aircraft Certification Office Any alteration of all. cortsticipt• it pwatado es/ • tins of not annd.frq 31.000. or norlsom•ot ror ....my 3 ye•rs. or Dorn. OA Oa 0110-2110.44i Mt I of . eMdt lAL certalfet• ray et unarmed is eccoll•N• with PAR 11. PROT526 EFTA 00241969 PROT144 PROT527 EFTA 00241970 PROT145 Pniltb Stotts of Amccica gieparhnint of transportation - Athena cl' biation ADministration $uppietturrtal Zug Tertificate (Tantinuntion *Fel) tfriendese ST03960AT When the Rockwell Collins Venue system is installed Airplane Flight Manual Supplement, DB1106015, Revision A, dated March 22, 2012, or later FAA approved revision, is required. When the Aircell Axxess II system is installed Airplane Flight Manual Supplement, DB1002072, Revision IR, dated March 22,2012, or later FAA approved revision, is required. When the Astronics Cabin Inverter system is installed Airplane Flight Manual Supplement, 0811090I2, Revision IR, dated March 22, 2012, or later FAA approved revision, is required. This system is intended to provide Internet connection and email services to the airplane's cabin using portable electronic devices (PEDs). Any other intended function of this equipment will require a re- examination of the certification basis. When the Rockwell Collins Venue system is installed Instructions for Continued Airworthiness (ICA), Nextant Aerospace Document No. DB1002068, Rev IR, dated September 22, 2011, or later FAA accepted revisions must be made available to the operator at the time of installation. When the Aircell Axxess II system is installed Instructions for Continued Airworthiness (ICA), Nextant Aerospace Document No. DB1105003, Rev A, dated September 22, 2011, or later FAA accepted revisions must be made available to the operator at the time of installation. When the Astronics Cabin Inverter system is installed Instructions for Continued Airworthiness (ICA), Nextant Aerospace Document No. DBI 103018, Rev IR, dated September 22, 2011, or later FAA accepted When the Emteq LED Cabin Lighting system is installed Instructions for Continued Airworthiness (ICA), Nextant Aerospace Document No. DB1108019, Rev IR, dated September 22, 2011, or later FAA accepted My tlt•ncIOn or tAlt ttttt 11C•C• It SSUSA•ble by • Ube of not txf•MLIng $1.040. at lapilsosent not oKIM i ynrs, or bac, in now 5110-2.100.0) ma 2 .4 1 flat MIS ***** fICM• Yy be Monter 5. mtbriSSIK• Ida YAK ILO'. PROT528 EFTA_00241971 PROT146 PROT529 EFTA 00241972 PROT147 !Nitta Shahs of Anttrifit pepartment of raransportation - *bend Ablation elbministratioo $upplemental `Type Tertificate ((llontinuntian *lett) Aa/IdeleST03960AT 444/.;mg The Certification Basis for this installation is per Type Certificate Data Sheet A I6SW original Certification Basis, Federal Aviation Regulation (FAR), Part 25 as amended by Amendment 25-I through 25.40 plus FAR 25.1335, 25.1351(d), 25.1353(cX5), and 25.1447 of Amendment 25-41; FAR 25.29, FAR 25.255, and FAR 25.1353(cX6) of Amendment 25.42; and FAR 25.361(b) and 25.1329(h) of Amendment 25-46. In addition the following specified rules amendment levels were used for this installation. 25.571 25.1353(aXc) 25.1357 25.1431 25.1529 125.541 (25.1231 (25-123] 125-1131 125-541 (-) Indicates amendmen level Any Ncsrstlon of tAl• Corti tttttt Is puitl•habl• by s firm of sot esc•eding /Ltd; or 'enlacement net exceeding l deers. or both. • of • Any strop:Onto with IM 11.17. PROT530 EFTA 00241973 PROT148 PROT531 EFTA 00241974 PROT149 e MAJOR REPAIR AND ALTERATION cI .. 5. Can p aw. ,: d (Airframe, Powerplant, Propeller, or Appliance) rift...U.00m Aemerndon rem Seam OMB the 21204020 ludato? Elect/Oak Mocking Nwtot For FM Use Only INSTRUCTIONS: Prd or type al ands Ste FAR 43.9, FAR 43 Appendw S. end AS 431-1 (or 44014quen resllkn Theo() for insauclions and esoodaton of iris rant Iles walls Nene team (4911.S.C. 1421) Fabare to raped an mull Placid penally not to exceed 31.000 tor *en such skidon (Secan 901 Were, Adam Ad 1956) Nadonalty and Rogledraem PARR N493UX Seed No. RK244 Masa Raytheon Akaaft Company Mode 400A Sales 2. Owner Name f As sham, on regthrfarlon netttale) Flight Options, LLC Aetna (As shown on rodstratten cerdtedd 463.46180 Curtin Wright PKWY carRichmond Heiohts sw,iohio 4,44143-14U cealn4)- 4. Type 6. Untl IdentMcallon Repair Abatedn Unit Mew Mo0&t Sad Number CI e AIRFRAME (As deSnitted I Gem / Steve) ID O POWERPLANT O O PROPELLER O O APPLIANCE Type Mattilaste 6. ContonnRy Statement A Agencys Name and Added B Redd Avert/ •,,,,,sConstant Aviation 0 U.S. Cerlincated lisschink 0 IManutaduret nass,[ADDRESS REDACTED] 0 roman Centlealer methane C. CaNfaa No. ratCleveland StawOhi0 0 c.nkakd Repair Salon CRSOVC7R345J zp44135 eornerUnited 5jame 0 CerldcMed Mantensece Orgendiron 0. I web Walesa repair actor aaaallen made to the wil(s) kienelled In Ilan 5. Abeva and dosolDed on Inc raVelle a alladienCrila hereto have been male h SCCOnlanee wed the requrementi of Pad 43 dem U.S. Federal Aviation Rag-J.1:cm and that Ino neotiyelen turnewid wen Isms aM moo to the best <Amy Emmett*. &ladled arcs Fad per 14 PROT822 Pan 43 APP. B O SIgnalurSale Authorized lelvIdual .../ Date: December 30, 2013 T. Pro &turn to Sento Pursuant to MOMAWItyaben MOWS IC•Xted below. Ih0 uftt toenw In iron 5,W5 impeded to the manner presabial by tied wow:side d lie FOSeral Aviation Adeninittabco and is ®APPROVED O REACTED AY FM Fa Slarearda 'Weds( Manubcturet Malnionerce Organtairn POW APPIted by Cansden ospartmerdoiTtareprt FM Designee X Repair Elam Impeden Aumorization °uncaps(*) calked or Dcsignallon Na CRSIA/VC7R346J Signature/Oale 44 Au0716 indivifraki i 4 _pi Date: December 30 . 2013 FAA Form 337 mote PROT532 EFTA_00241975 PROT150 PROT533 EFTA 00241976 PROT151 NOTICE Weight and balance or operating ACPtalon changes shall be entered In Ina epprOpriale aircraft record An aftentliOn MSS be compatible with ell previous afterations to assure continued conformity WA Ina applenbie eirworterness fl at 1107010. 8. Description 01 Work Accra/nen/lad (17 more apace is reradred. aback addreonal sheets. Idenlity will aircraft nalionekly and regislabon mark end dale work completed) N493LX 12/30/2013 Nationality and ROgnretIon Mark OMB ACCOMPLISHED INTERIOR REFURBISHMENT/MODIFICATION AND 3 PLACE DIVAN INSTALLATION 111E FOLLOWING AIRCRAFT WTERICIR ITEMS HAVE BEEN FIEFURRISHETT Repoli-tea rtmosemd carnal columnsen Mane Nan Leather Accordance. mm, Betenlel 400A AMM 2970:07401, 73470-0d431 Removed and /Inland Glare weal and Eyebrow panel rrzeetia min Mac Black Leatner n AmotOonCe byth kettle 400A AMFA 20-60-00.201. Removed and Rcptaoed CoMpl &dawn maieral YAM Male Nark Leather n Accor0.1100 WIT' Regan( 400A AMM 20 so 00.701. Removed end stewed Pilot Seal Pan Mann TAOHIOOPIS0001 Serial Numb, 62. Foam and recovered rim Garret Steenkin Oak and Excel CaPPOCCIne Leather. Removed end laplixibil Conn Seal Pan Number TAOHIOOCIA00-01 Soul Number 240. Foam and mooned win Care% Sheennt Oak and Exton Cappuccino Leann Honnyed end Replaced Let Hand ea Passenger Seal Pal Number 2524414(430A) Serial Writer 9907194 Foam and recovered with Townsend Lester (1, tag Been) Removed and replaced RDA Hand N5 Passenger Seal Pan Inner 7524.014(4308) Sabi Number 000428.7 Foam and recovered wen Townsend Leather(reisago (Veen) Removed and Replaced Let Hand Se Passenger Seal PM Number 7574-014(5308)Serlal Number 0303484 foam and meowed wet TonnSend Learner Mentage r340^^) Removed and replaced ROM Hand sir Passenger Seal Pad Number 2524014(530A) Serial Number 030708-2 FOAM and ItCovered with Townsend lea:her (Ileolape Brown) THE FOLLOWING MANUALS ANDAPPROVED DATA HAVE BEEN UTILIZED FOR OASIS OF REFURBISHMENT: Skande Flamm/RAIN TOM 5254078 as approved by FM DER lane elberveln (DERV 832780-CE) en FM fain 5110-3 doled 4/23/2013 Fenn Cut 1 ammabely Teal 4311 19 e*eved by FM DER limb Reed II (OERT.230293-CE) on FM Finn II 10-3 doled 17/23/2013. Skanda I anrnablN UM Report TP 22081 Rey A as approved by FM DER Jane Eliterslen CERY432780-CE) on FAA term 8110-3 Men 05/02/2013. Tine Place Divan installation 'twined (3) Pacenon par Number 3743390(450131)T123.K02 SIN 003702k. Ancrdante wan Aviation Fannin STC4 ST0157204 and Marna Hannan* toy. retnn 5754078 per Jane Bibersleln FM GER (DERY4132753-CE) dated 4/73.2013 THE FOLICAMNO INTERIOR ITEMS HAVE BEEN MOOIFIED. UPI GsAy Any, RAI Gnaw Ndy. Man Any. UN Gat/ Asey and Irmiall per Della G drawing DGOCA01.101 Rev D. OdA CA01.101 EO E.I. Lai Galey 'Waft Da/D.409501 Roy BOA-I. 000-CAOI.501 Rev IR as EipprOeid on FAA lam 81104 pet FAA DER Donald Genre (DERT-790135-SW) doled Meryl 25 2013. 511 Gain Assy and Instil per Dna G drnengs DOD-CAW-101 Rev B. CGGCA02401 Rev IR as approved on FM form 81103 by FAA DER Donald tDERT-750135SW) dated Mardi 23. 2013 Divan May per Dab 0 Manage OGLIDA00401 Rev C rid DOODADS-101 CO DI as approved of FAA loon 5110.3 per FAA DER Own Gilasple (DERT 750135414) dated march 75 7013. Berner IN Wesel assy Many 7553-0038 Rev C. Inner Scieledge any drawing 2537.0037 Rev C. Bonner KII Foldout Tette assy drawings 25530041 Rev C and 2559-0040 Rev B. Scam XTI Ivies Ka Inn Penn 2553-0037 Rey C Appioved on FAA torn 81 £0.3 pia Stesmen Forman DERT.230238-CE dein Dec 20. 209 INSTRUCTIONS FOR CONTINUED mRwOrtalitts$ THE REMOVAL OF THE INTERIOR IS OH THE CONDITION OF FAILURE. THERE ARE NO ADOITIOWIL INSPECTIONS REQUIRED. CONTINUE TO INSPECT LAW MANUFACTURERS NAM. SRN. OR CMM AS AfinLICMILE AIRCMFT EQUIPMENT LIST AND WEIGHT AND BAUVICE WERE UPDATED BY THE CUSTOMER END- O Additional Shoots No Attached FAA Form 137 (tocs) SON Y_GM_02755055 EFTA_00241977 PROT152 PROT534 EFTA 0024I978 PROT153 US DEPARTMENT OF TRANSPORTATION EDERAL AVIATION ADMINISTRATION STATEMENT OF CONIPI IANCE WITH THE FEDERAL AVIATION REGULATIONS DATE Dec 26, 2013 MAKE Beechcraft Corporation MODEL 400A TYPE (Airpione. Radio. Helicopter. etc.) AIRPLANE NAME 0 'APPLICANT NEXTANT Aerospace Cleveland_OH. LIST OF DATA IDENTIFICAITON TITLE REPORT: BEECHJET 400A INTERIOR STRUCTURAL SUBSTANTIATION BEECHJET 400A XTI LINER KIT INSTL. Beech Jet 400A, Aircraft Serial No. RK-244 Certification Bases for this aircraft modification is per Type Cenificate Number A I 6SW Revision 28 dated April 12,2013 RKG3282 Rev. IR, 8.28.2013 2553-0037 Rev C, dated 8.30.2013 PURPOSEOF DATA DESCRIBE AND SHOW VERIFICATIONS FOR NEXTANT INTERIOR INSTALLATION ON BEECHJET 400A, AIRCRAFT SERIAL NO. RK-244 APPLICABLE REQUIREMENTS ( List specific sectoom) 14 PROT823 Pan 25 §.301, 303, 305, 307a), 365, 561, 571, 601, 603, 605, 609, 613 CERTIFICATION - Under authority of appointment under Pan 183 Mille have been vested by direction of the Administrator and in accordance with conditions Federal Aviation Regulations, data listed above and on attached sheets examined in accordance with established procedures and found to comply Regulations approval of these data Approve thew data and limitations numbered with applicable requirements of the Federal Aviation I04 Therefore 0 Recommend ,ii SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATIONS) Suphai Fames DEBT-210238-CE STRUCTURES AND DAMAGE TO1ERANCE .13 2 FAA Form 8110-3 wit) SIDUEDS unmans amen 00 WI -41) PROT535 EFTA 00241979 PROT154 SONY_GM 02755058 EFTA 00241980 PROT155 FAA FORM 8130-6, APPLICATION FOR U.S. AIRWORTHINESS CERTIFICATE Form Approved O.M.B. No. 2120-0018 Ex irahon Dec 02/2602013 la APPLICATION FOR U S aim U.S. AIRWORTHINESS 0 T,Insoce.wat Federal A awn CERTIFICATE 4.4nenstrica. INSTRUCTIONS • PAN a We Co AM Ante A shmImi meas. Ira re Ice FM '44 onry Soter4 pig nal only AA On OATonnsl FM Rimesorisugo I oddmovi ram m tecsanog use etschment For sow/ ilosi pennals compbm Sealant IL VI. rod VI As ecolcablo ,T. € 2 : V5 :g i REGIS !RATON MARK N493LX 2 AIRCRAFT TMUTETTS NAME 4.•4•6 3 NRCRAFT ROCS DESIGNATION 4OOA I YR. MFR 1999 FM COOING 5 ARCRA77 SEAM. 143 RK-244 6 DOPE Ka DERS MME Mow Williams International 7 OGRE MOOR CESKIMATION F444-3AP It RIMIER CF DORIS 2 9 Amapa]. ER LANCERS RAW Amy N/A XI PROPELLER MOOSE CES044T04 II NRCRAFT IS /Coss nmemmi N/A I &PORT 0 i S V A 4 g APPUCATON IS HEREBY MADE FOR Mow mAltRom•I I A I STAICAPONRYC.RTKNESS CERTFCATE Oramos pro I I •mm't I I T"`"` I ram 44 I I •••••••41 I I "way' I I 1414414 Home 6 .4 SPEOAL AiRAORDI NESS CERTIPICATE Om remmesisso PROURY 9 UGNTSPORT I I Arlan I I Pommarscru. I I WilisflEtsflOATIM Helder I I 2 Ara.. UNTIED Wm Man Of I CUSS I 3 PRORSIONAL nAme• env 2 CUSS I 1 ACIRCIARITE NO PEST CORROL 2 AERIAL SURVEY 3 AERIAL ADVERTISING 3 RESTI A ECTED poss. meal 4 CREST S PATROL/4 6 HOTPOT CONTROL to ems** 0 OTHER Norm I i IIMMROI AND CEVELOPMENT 2 AMATEUR Out 1 3 ONEITIOI 4 NRsRAON3 S CREW TRAINIC 6 MARKET SURVEY 0 TOHav compuencE %%mum am 7 OPERAnNG Pam* 649 ..NITK CAT AIRCRAFT i EXPEFtMENTAL IA Emir! MOMMA an racrIhress orettical• 199 nal awl EMI 4 OMAN meal seniassie I OtiERATAG w onto/ Etnspa• oar LIONTOORT EC Orsuna banal oieeuse sued spew. erlispon emery avezononi agleam wet $ 21 193 OMMORD IA RESEARCH ANCIOEVELOVERT ICI RAW/ TRAI/61/3 NRCRAFT IS AWNS SURVEY 1 FERRY RIGHT FOR REPAIRS. ALTERATIONS. TINARENTACE. OR STORAGE SPECIALEDGAR PEROT RAMS 2 EVACUATE NOM MO OF IMPOONG OA/43ER I coln••••••••••ANA Ono.* 2...., w. w... ~2 ,...... 0. 4 3 OPERATOR IN MESS OF MAXIMUM CERTORCATEDTAKE4)FF REIGN 4 CeuvetwooR EXPORTING I S I I mooucnotiFUOIT TOMO 6 CUSTOMER DEMONSTRATOR FLOWS CI 6 MULTIPLE AiRWORTHAIE3SCERTIFCATE CosnalCatibeerwOrosive in elSow a bar a wolge/ 2 c A REGISTERED WATER IA TiencaeaslossienmenigaNITTO IF 00116. CTICCX REFS--. I muff F igh Options LLC ADDRESS 26180 Curtis Wright Parkway, Richmond Heights .OH 44143 B ARCRAFT CERIFICATICAI BASIS tom falkSiill t Oa in (p.m. row ea vowed AMC:RAFT SPEOFICADCR OR TYPE CERTIFKATE DATA SHEET 0.06.4 Ammm.vAl N/A I atimcarmaEss onscnvEs Kan. nia...sas......a................... now A sumfmOrwsom As wmoy Ara a /oar emmesso Bi Weekly 2013.22 10121/2013 -11/032013 APOIAFT UST46(0.•••••^01•414.7 N/A SUPPLEMENTAL TYPE CERTIMATIE ase A....../..6.3762.6Amnso N/A C AIRCRAFT OPERATION AND MAINTENANCE RECORDS ORCX F REcfl IN I COUPWACE 551714 14 PROT824 sec6591 417 TOTAL AIRFRAME TOPS TTAF 85M.82 3 EXPENMERTAL ONLY Me mos Am. mm Assam se A AA A 4 0 14.82 0 CERT F CATION .1746•16. ON* tel 1 114404•551•415 *al 49 Ors VIM 747110 sesonnress marcme mammal wn ire mcpmna ma (or In PPM / to PIMIII 4444454.7 SAL Maim 640415 6674 44101 66666 AM Makatle F•dere MAMA Accisfons. And MN ITO IS 1'1011•0 6111 FM Fail AAleknAOTITesirsIa,15 *MA 666 Wen jowled o'd 17 apt" and SOO 174 to DATE 07 APPUCATOI 11/18/2013 NAME ANO TITLE Sem Owl Antony. J. KoPrhtra Agent SOJATURE e 4 11.2.'".. 1 I i i I A THE NRCRAFT DESCRINO MOVE HAS BEEN Ir4PECTECIMO FOUND AMORIST EIY:e0esIseim mem cay 14111Asee 171•••••••1 r 2 NUR ,prj 121 CERTIFICATE scam*. 3 CEFITIFICATED ARCHAIC Oa ColOw• mo I 6 CERIVICATE0 REPAIR STATION Au, Ceske Ts/ 5 AIRCRAFT MAIRVACTURER SIM.° An/ OM 1111E SIGNATURE v. FM RtPRISINTAffill CCRIVIWION itaTe1•Ltemitainx•••••••411, I DM CERTIFICATE REQUESTED A I MOM Ito oat Ammo 04400, I.. vil mwasmonons b maws ON LICX4FICATICITI OP CURRENT ASTACRTHINESS CERT1FCATE a awastn kr • NOM AV4 pan. retlerSocion VII esIn - Or FMINSPECTOR FM DESIGNEE CERT/CATE POWER DEER 14 CIR Asia I I I4 PROT825 Pal 121 OR OS 1 114 ma/inns DATE 11/18/2013 1600.300 CC ACE CLE-25 4 FM INSPECTORS SIGNATUR CESGNEES SIGNATURE MCC. Arthur Ockwell DART833943GL Q. 1 FM CRS Celtic M UNE bp., J...',...tisr--., FM Fan 013041"I II AA Pa AGA 601110413 Super$17104 Eseaseve FoXISOI -POF Et. vvED DEC 1 9 2013 CLE Otr SDNY_GM_O2755O59 ffi O a EFTA_00241981 PROT156 t I PROT536 EFTA 00241982 PROT157 P E t i PROOJCTION g a A. IIVARIACTURER NAME *OGRESS P R O P M e i I A S I S (CAW o a r A c o N o on CERTIFICATE (Give prtelleivi O.t10 Nat% WOE CERTIFICATE OTHER C. GIVE OUANTITY OF aRTECATES REWIRED f OR CREAMING NEEDS DATE OF APFIJCATION NAME ANOMIE IAN Of WE SIGNATLRE i I I O 1 5 S i 2 i 0 0 A DESCRIPTION OF AIRCRAFT REGISTERED OMER AGGRESS BIALCER (WV ACM SERIAL RIMIER REGIST RATER IMRE a DESCRIPTEN OF RIGHT DETOSER DEMONSTRATION EMIRS O (Cwt itmalcitau FR011 TO VIA DEPARTLRE DATE DURATION C. CREW REOLIRED TO OPERATE TIE NRCRAFT ANO ITS EOLEVENT I I PILOT I COPILOT I I RIGOR ENGPEER I I OMER (SPORN D TIE PERCRAFT OCES /CT MEET TrE APPUCAFAE MANGROVE% RECNAREMENTS AS FOLLOWS. E TIE FOU.OAING RESTRICTIONS ME CONSIDERED NECESSARY FOR SAFE OPERATION (On Firechworl It nO0Fsmy1 F CEATIFEATION - I MEN panty Ms I an M WOES owe (of lw POEM of Fe Rola *noted sews. WE Pe Mein is nose*, NM H FENS Avalon All•Oltteka In =Wave Mn Tao re DA N Wed %An GNP 400' iLma as Eclat* Fan Mom Rpoinora n ON re WMPm tem reseed Rd es We ler Ur VI Sweat DATE IMRE AM TIRE JAW 0/ Fa) SORT UK 1 1 IE i 1 g I J A 2proVE UMW.* Ird Vedni, In CamIrc•IMP II CIR Slate 91.1 D. Stiewnve al Carta/MN. FM Form 6130. fAciaot Vim stoat° II Foy,. Mrecettris CASIsion tor Awl AMA Dawn MAT AMERI) R. Cornet CESARE LRAItons Altana C. DM Dote. MVP" Pc WEN PAM *MOE i RvIRa Anhannvo OMAR. NERO nApartlenco NM IA PROT826 Sicson 21.19 1 (a) am (Onanagnaao 1 at Waft Waft Fla Bain:* INN*._ Avairas Marva I Valor REpOrird ~MA FM Fain 337 CAPRA seen AMINE 1 . . Omni Ancennics CrVica Awed /*Am:Nino NM I d ("fa no , 21.191(a) toanotama) F TM Ricceten REWIRE hAiv•II ReComb I( Liyagn Ana %int of COVIact EM Ewa PINY'S 0.11•01 PISA APOREE FM Form 1304 I 4/10 Al PilhiCta UPON Supine:Rd Electronic Fond -PDF Pop 2 ol 2 PROT537 EFTA 00241983 PROT158 PROT538 EFTA 00241984 PROT159 %sierra STATIc Ce MOW. OMATIIIINT Or TRAMPORTare. • SIC€RM "WOW ACildwaTRA11O.4 SPECIAL AIRWORTHINESS CERTFICATE A CATEGORYRICSIGNATCHI =WEAL PURPOSE MEWS 6 DM n R. ILFAXU- IIACRFREA NAME ,i1/ 'DURESS e C FLIGHT F u \ L . TO T O 4A•• I . D " Milt SER NO w -≥44 o. EARLISER nFIGRETRI A REACio ry ),...i f UO L AIM E OATE CR LSSUARICE I e V E $n 12.X114 OPERAUNG um T Ns tEo -- ku FE:2013 ,. . RAPTOR DRSGERTRCATE socase of trantr•cs9+ Pithy °Wel 1 1. SConliceiNt0FAC400) OFT831063al. AFF sewn ilpalanotrusairofna tomato wry. Nana* by • Ire cm seeding PACO cv iftrionraer4r0i isondrq >pen*. ton NIG COHOICATEWST OE DORLArti) ON 1)t W1 IN ACCORPOCE WITH mw le-astral CODE 0 'MAN ROMA7014 (CM YNrNymAnMLu PROT539 EFTA_00241985 PROT160 A TM anioRass aortic:me turas inn art** a' Rat la $04-6. 0 VS/ gin** 00 44701 an! /IV Ilea d Semi Peinincea KM ip B The sewaikins coldest aura. 1%. ,ndnAaSur Inotn Sworn oh* 0 ordO Podscro, :We al fat cgOi "Sabi OW Mat 01 Mc n tegarved Alb meg Wandcoy ontxtpolckm Site um Leder*. anemia' pso Re consvaol or Pat sib (2)Cengporws rd ecorctilto Pawpaw (le 174 C no analw'bucetkab Ontalin be aftl wan*, PO TOW IS ke te pomp awn 11b, A O Di invihnns cot SR calks nita One SW claret IN nth sMI coved,. Ka royale,/ ttM i 0~ hi 'snits till* Metal* OR 7b not OM Ni MO anepatirMett al Wadi conwheets sod ducial advalhem (Of r a posa4 be /mix 1b RN Croon°, On bitIMICOVICalASIo• ?Wow gurs mato Stead Onutelco int yen. MY (I) meal n moils= td. to ;plat* Ofianin =minx ofeandecne •-0 Invaots .0.0, est* posm10 by theAtanisrece at pd Otis wits" al army bap =myvita:Pe spear masa, dab °sorry E Wris NOW unnIncl worded nolo/ Res olingroteis conkier • 'MAW *SR etralat aid wolef Ps onto+, Pearlte.10 It CIA Pm V. Seam 21 1St of 11.21t SONY_GM_02 755064 EFTA 00241986 PROT161 tILITIO ELATES," MIKE DIEVRITADCT CP lIVMEOMALKPI• TOLOW , IALTEINVIAIIIIMILTIN SPECIAL AIRWORTHINESS CERTIFICATE A CATtOORTUNGNAIKa EXPERIMENTAL PURPOSE andbankipeal El two FACTURER RAW ti Ammo D FLOW FROIA TO t- D TA MT1E X BUILDER Mutate UCCIEL ARRA E RATED, CRUM idui yrjanen A MEE annum. T Midi T. Rey/KEPI ME PART Of THS MIME( INSITITATION CR DEE a PC OARFJOOI4SCE T. kty imapRovert INACO3RONECE eirmot reventita g d Ds aM6Y way bit Weltle tE II MO a ELOIEOLE SI COO W rot oottoug 3 row Teton TAG CERTIFICATE KIST OE OISELAYED -NNE MIME, AIN APPOCES.E TITLE It COCE OF Eta IILL REOULAII0'4 OE I PROT540S5C6S EFTA_00241987 PROT162 A n na weesheas colleen Masi Well. airety al Pat Us 10140/0010 SIM MM MP 44/04 and la Ti Cali cl WO, 419 002'0010 D Thorootwessanksinseera ite marbant rarelathl *WOOS* bareict froAcks Wit but PI cek "Ada. Or INK al liCall 1St* 0 Wen NO pirK0 ft* C a* a co:Wool quest. we r rs antra (1)Carn pews open • r a na sakn ce Imo sae 0ICerag pml el tenitil I, Or i0014 cite NW C Do •••••••••• conks* lairs to nita 40.041 0 IM twa Wag be mon twin lbs.& D Ths anagram nintlet t ad IV la d earat IV mat b Midi mold ta ton ended ward Wiwi IV an west. eft* *Oa CM U. Snit ea. td Nos Ito name. dr* scratecevonwo M. OWN ~Inn ODOM padof by MM. 50 be tametcn as arra:al OS MO a. No ciao nry opts bs scat aorta cm to nre•I Se (I I earn a Main MM.. COMA! CPR ard n IKKOdInCe at wanes. lantlikes./0 rep 01 CUSS CI to FM at pi elINOP11011. MOS Mg Sir Why Eitel to wail Rana d hi earn E'• stagnant suceacc a racied. M scents ohms is °MON b Re Salem MI tre IN Mare {retorted .• 14 CR. Pan 21. Sesks11 Mail 217. PROT541OS6 1" TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 00241988 PROT163 O.S.Oapartment of Transportation Administration REG. NO. N493LX EXPERIMENTAL OPERATING LIMITATIONS For Research and Development (R&D) MAKE: MODEL 400A FAA Cleveland FSDO Great taxihem Yamada,/ Park II 25249 Courily Club 0940. NOM amulet,. Ohio 44070 (440 6803-7000 SERIAL NO: RX - 244 THESE OPERATING LIMITATIONS SHAH. BE ACCESSIBLE TO THE PILOT 1. No person may operate this aircraft unless the FAA Form 8130.7, Special Airworthiness Certificate. is displayed at the cabin or cockpit entrance and visible to passengers or flight crew members. 2. No person may operate this aircraft for other than the purpose of Research and Development to accomplish the flight operation outlined in the applicant's program letter Dated November 13.2013, which describes compliance withl4 PROT827 21.193 (d) and made avadatte to the pilot in command of the aircraft In addition, this aircraft shall be operated in accordance wah applicable air traffic and general operating rules of 14 PROT828 part 91,and all additional limitafonsherein prescribed under tho provisions of 14 PROT829 91.319 W. 3. R&D flights must be conducted lAW Nextant Aerospace's Program Letter Dated November 13. 2013, within the geographical area described In the program letter. R&D Akins will be conducteiln North America 4. Except for takeoffs and landings, this aircraft must not be operated over densely populated areas or in congested airways. 5. This aircraft must not bo operated unless it is maintained and inspected in accordance with the appropriate military technical publications and/or manufacturer's recommendation. The ownerioperator must select, establish, identify, and use an inspection program set forth in 14 PROT830 91.409 (e), fib (g), and 04. This inspection program must be recorded in the aircraft maintenance records. 6. The Pilot In Command of this aircraft must hold an appropriate category/class rating. If required for the type of aircraft to be flown, the Pilot In Command also must hold either an appropriate type rating or a Letter of Authorization issued by an FAA Flight Standards Operations Inspector. 7. This aircraft may bo operated under VFR, day and/or night. 8. Thb Aircraft may be operated under IFR, and must be properly equipped for instrument flight in accordance with 14 PROT831 91.205. 9. No person may operate this aircraft for carrying persons or property for compensation or hire. 10. No person may be carried in this aircraft during flight unless that person is essential to the purpose of the flight 11. The Pilot In Command of this aircraft must advise each passenger of the experimental nature of this aircraft. And explain that It does not meet the certification requirements of a standard certified aircraft. 12. This Alrcraftmust containthe Beech Model 409A Flloht Manual with Nextant 400XT AFM Section lnsert, Placards, markings, etc. (or other operating instructions developed loran STC modification), as required by14 PROT832 91.9. 13. This Aircraft is Prohibited from Aerobatic Flight, that is an intentional Maneuver involving an Abrupt change in the Aircrafts attitude, an abnormal attitude, or abnormal acceleration not necessary for normal flight, unless part of show compliance flight testing 14. This aircraft shall rot be used for glider towing, banner towing, or intentionalparachutejum 9 Page I al 2 SONY_Glil_02755067 EFTA_00241989 PROT164 PROT542 EFTA 00241990 PROT165 U.S. Department of Transportation Administration FM Cleveland FSDO Ghat Atntlern TOckly0109Y Park II 25249 Country Ovo Blvd Nom COnstead (440)44154000 15. No person shall operate this aircraft unless within the preceding 12 Calendar months it has had a condition inspection performed in accordance with 14 PROT833 Part 43, appendix D,or other FM approved programs, and was found to be in a condition for safe Operation. This inspection will be recorded in the aircraft maintenance records. to. FAA-certificated Repair Stations and FM - Certified mechanics with appropriate ratings, as authorked by 14 PROT834 43.3 may perform inspections required by these limitations. 17. Inspections shall be recorded in the aircraft maintenance records showing the following or a similarly worded statement: "I certify that this aircraft has been inspected on (insert data) in accordancewith the scope and detail of 14 PROT835 part 43, appendix 0,or other FAA approved programs and found to be in a condition for safe operation." The entry will Include the aircraft's totaltime-in-service, and the name, signature, certificate number, and type of certificate held by the person performing the inspection. 18. If the aircraft, engine, or propellor operating limitations are exceeded, an appropriate entry will be made in the aircraft records. 19. 11% aircraft must not be operated unless it is maintained and inspected in accordance with the requirements of 14 PROT836 Part 43. 20. This aircraft must display the word "EXPERIMENTAL"in accordance with 14 PROT837 4523lb). 21. The Pilot In Command of this aircraft must notify air traffic control of the experimental nature of this aircraft when operating into or out of airports with operating control bees The Pilot In Command must plan routing that will avoid densely populated areas and congested airways when operating VF R. 22. This aircraft does not meet the requirements of the applicable, comprehensive. and detailed Airworthiness code as provided by Annex 8 of the International Convention of Civil Aviation. The Owner/Operator of this aircraft must obtain written permission from another country's Civil Airworthiness Authority (CM) prior to operating this aircraft in or over that country. That written permission must be canted aboard the aircraft together with the U.S. airworthiness certificate and, upon request be made available to an FAA Inspector or the CAA In the country of operation. 23. Arcraft instruments and equipment installed and used under 14 PROT838 91205 must be inspected and maintained in accordance with the requirements of 14 PROT839 parts 43 and 91. Any maintenance or Inspection of this equipment must be recorded in the Aircraft Maintenance records. 24. Application must be made to the geographically responsible FSDO or MIDO for any revlsicn to these operating 25. 14 PROT840 47.45 requires that the FM Aircraft Registry must be notified within 30 days of any change it the aircraft registrant's address. Such notification Is to be made by submitting Aeronautical Center Form 8050-1, Aircraft Registration Application, to MS-750 in Oklahoma City, OK. 26. Condition Inspections must be performed in Accordance with 14 PROT841 Part 43 Appendix D at least every WO Hrs Flight Hours. This Inspection must be performed by an FM Certified Mechanic with the Appropriate Ratings as deemed in 14 PROT842. 43.3 27. The Special Airworthiness Certificate and Operation Limitations will copke on. Jan 12.2014 Arthur Ockwell Designated Airworthiness Representative DART833943GL Issued at Cuyahoga Airport Date Issued: Nose-nter IS 2013 Page 20(2 PROT543 EFTA_00241991 PROT166 I SONY GM 02755070 EFTA 0024I992 PROT167 nextant aerospace Quality Assurance Department To: Federal Aviation Administration Flight Standards District Office Great Northern Technology Park II 25249 Country Club Blvd North Olmsted, Ohio 44070 Date: November 13, 2013 From: Chief Inspector $ubiect; FAA Program letter for Beech let 400A, Serial number RK-244, Registration Number N4931.X. Ref: FAA order 8130.2G 1. Registered Owner: Flight Options LLC. Address: 26180 Curtiss Wright PKWY, Richmond Heights, Ohio 44143 2. Aircraft Description: Twin Engine Light let a. Registration: N493LX b. Aircraft Builder Raytheon Aircraft Co c. Year mfg.: 1999 d. Aircraft Serial Number: RK-244 e. Aircraft Model Designation: Beech let 400A 3. The program purpose for the aircraft will be used To complete the flight performance profile in Research & Development Category in support of FAA Project SA 152S0LA•T (Replacement of Wingtips) 4. Program Duration a. List the estimated flight hours required for program: 20 Hrs b. Number of flights: 20 c. Number of days: 60 5. Describe the areas over which the flights to be conducted and address of base operation: The base of operation is Cuyahoga County Airport, 355 Richmond, Cleveland, Ohio. Flights will be conducted in North America. 6. Describe the aircraft configuration: This Aircraft is a standard Beech set 400A with new Williams F144-3AP engines and upgraded avionics with full authority digital engine controls (FADEC) a. Maintenance Program 1. Hawker Beechcraft Maintenance Manual Chapter 5 Rev C22 or later with the exception of the 1115D Engines. 2. Williams International recommended El44 3A Maintenance manual (FADEC maintenance is covered in 71-00-00 of this manual) 3. Maintenance Requirements for the Throttle Quadrant is addressed in the Instructions for Continued Airworthiness on the F144-3AP STC. Chief Insdfct r Tel Work 216-797-8257 Cell 216.225.8645 PROT544 EFTA 00241993 PROT168 i PROT545 EFTA 00241994 PROT169 16180 Curbs, Woght Pathway Cleveland. Oluo14143 877.703.2348 www.11ightoptions.com November 13, 2013 Nextant Aerospace, LLC 355 Richmond Road Cleveland, Ohio 44143 Attention: James Immke Re: RK-244 - Agent Authorization To whom it may concern: Options This letter is to confirm that Flight Options, LLC ("FO") authorizes Nextant Aerospace, LLC, as FO's agent, for a Beechjet 400A, bearing serial number RK-244 and FAA Registration Number N493LX (also identified as a "Nextant 400XT), which is owned by FO, for any and all authorized FAA actions in regards to: X Airworthiness Classification Experimental PROT546 Airworthiness Classification Standard Sincerely, Flight Options, LLC By: MOLLY KEANE NOTARY PUEIUC STATE OF ONK) My Corm upen Am 24.2016 Michael Metera Vice President, Administration & Contracts -1-eccick, EFTA 00241995 PROT170 PROT547 EFTA 00241996 PROT171 MAJOR REPAIR AND ALTERATION u s oupwwirt a (Airframe, Powerplant, Propeller, or Appliance) reesrAirlan (torsi kola', A4mIrist,KOCI Fan frowww Ore Ns 21200O20 I I Ns Elsdrenk Tracking Number For FAA USG Only INSTRUCTIONS: Print or type as snarled See FAR 43.9. FAR 43 Appendix B. and AC 43.9.1 (0 subsequent revision thereof) for instruCtiOns and disposition Cl this form The report is required by Inv (49 PROT843. 1121). Failure lorePart Cal Mater in a civil Pena), not re IMMOST.0W for each such vialation (Section 901 Federal Actaeon Ad 1955) I. Aircraft Natrona* and Regisbatian Mark N493LX Serial No. RK 244 Make Model 400A Series 2. Owner Name (At snOirm on registration candCON) Rig ht Options .LLC Address (As shown on registration cerriscrreel Athirst 7.6180 Curtiss WrIcht PKWY coy Richmond Height slake. OH ao 44143-1453 cover? OA 1. For FAA Use Only 4. Typo Repair ikaarebon UM Make Model Serial Number O El AIRFRAME (As dunned, M nem I above) 0 O POWERPLANT O O PROPELLER O O APPLONCE ;le !Jar:ix-Low 8. Conformity Statement A. Agency, Name and Addren B. Kind o4 Agency Nam Mows [ADDRESS REDACTED] Car Cleveland sure. OH co 44143.1453 coney USA 0 U.S. Certificated Mechanic 0 Manufacturer 0 Foreign Certificated *anon Ell Certificated Repair Station CRS # 25NR667B O Certificated Mahlenance organization D. Inertly that the repair andror allerabon made to the 'mills) ides ed in Item 5 above and described on the reverse or attachments hereto have been made k accordance with the retedrements of P rl 43 of Ste U.S. FederalAviation Ragulabans and that the information furnished herein neve andconed to the best of my enornedge. Extended range fist per I4 PROT844 Part 43 App B O Signahrtan)me of Aug-coked Individual 12/29/2013 7. Approval for Return Pursuant lo the authority given persons peofied bekvr. the un I Mangled In item 5 was inspecsed 0 mo manner retuned by the Administrator or the Federal AnalionAdministralion and is 0 44PROvso O Rt./Mt:EP FAA FR Inspect sunwards or Manufacturer Mantenance Organization !Perso Approved by Canadian Depa el Pansport renent BY FAA Designee Instal:moan Authorization Dew (Spear) Cartiaimre or Design # 25NR6676 don No. CRS SianalureiDate of Armoczed menden 12/29/2013 FAA Form 337 (10-06) PROT548 EFTA_00241997 PROT172 PROT549 EFTA 00241998 PROT173 NOTICE Weight and balance or operating Mutation changes shall be entered in the appropriate &Mae record. An alteration must be corvette,* mill all previous alterations fo assure Continued conformity with the applicable airworthiness requirements. (If more space is required, attach additional sheets. Identify with aircraft nations/fly and registration mark and date work completed.) N493LX 12/29/2013 Date Installed the following In-Flight Entertainment System in accordance with STC U ST03960AT and in accordance with Nextant Aerospace Master Drawing List DB1002067. Revision F.05 Dated: October 9, 2013. Installed Bonner Cabin LED Lighting System without the Venue System in accordance with NX330-1304002. Rev B Dated October 17, 2013. Ref. drawing for parts list. ICA Requirements. Ref FAA Order 8100.17 Page 7-5 and 7-6 Use FM publications such as AC 43.13-1, Acceptable Methods, Techniques, and Practices - Aircraft Inspection and Repair, and AC 43.13-2, Acceptable Methods, Techniques, and Practices - Aircraft Alterations: part 43 appendix D: or other applicable aviation standards. Installed Iridium Sat Comm (Cockpit Phone only) and Broadband Internet System with Aircell Axxess II and ATG 4000 in Accordance with 08 1001013. Rev E ICA for Aircell System Ref to Nextant Aerospace Document No DB1105003. Rev A dated September 22 2011 or later FM Accepted Revisions The following manuals contain complete detailed maintenance instructions and should be consulted for all maintenance activities not covered within this ICA: Aircell Axxess II Installation Manual D12004 Revision E, dated March 2010 or later applicable revision Aimed ATG-4000 Installation Manual D13485 Revision B Dated November 2009 or later applicable revision Aircell Axxess II WLAN AFM Supplement DB1002072 Rev IR dated March 22 2012 for the has been Installed in the AFM Installed the Astronics DC-AC 115 VAC Power Supply in Accordance with DB1002067 Rev F.04 Dated 10/912013 This is Located under the Seat Divan ICA for Astronics 115 VAC Cabin Inverter Ref to Nextant Aerospace Report No DB1108018 Rev IR Date 9/22/2011 or later FM Accepted Revision. Aircraft Flight Supplement DB1109012 has been installed on the Aircraft See Current Weight and Balance Dated: December 29 2013 End FAA Form 337 0046) PROT550 EFTA_00241999 PROT174 PROT551 EFTA 002420((1 PROT175 pilteb $Iatta of Atrorica !apartment of Crannporfation - 31reberal jkbiation jthtnittistr anon (Supplemental Type (Certificate ,fl) tee/Arte eietnnfle, ..4'984 0 ST03960AT 3800 Southern Blvd. West Palm Beach, FL 33406 tre-fOu //et I de neer &re elevrei'o deAtetbreiptonvArinvAf /de etettrectehte trzenientStre efeereAr eta reelleekterronmee4 de erkeecava At/weirs:rah eye fikei 25 Va. Federal Aviation Siter ikai•••• 6:-#thalOrdemot sfrow4.-44ntte,.develd.• gliverfrika Our* Mr Al6SW Hawker Beechcraft Corporation 400A Installation of Rockwell Collins Venue In-Flight Entertainment(IFE), Aircell Axxess Cabin 11 Iridium Phone and High Speed Internet System with Wireless Local Area Network (WLAN) Astronics 115VAC 60HZ Cabin Inverter, and Emteq LED Cabin Lighting System in accordance with Nextant Aerospace LLC, Master Drawing List DB1002067, Revision E, dated January 26,2012, or later FAA approved revision. ..95;;wezthew., ffaiftwafmt• This approval should not be extended to other aircraft of this model on which other previously approved modifications arc incorporated, unless it is determine by the installer that the interrelationship between this change and any other previously approved modifications will produce no adverse effect Upon the airworthiness of that airplane. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. ..974 tw/92674 reed/4 .myyrethity wale t;i de 4J6 erierreteet.4eKetrowettiv tio *Or/t nit ••••••warryrd. •flyinenteed erg:drier re &teenier/4w toile b aftere4e sutatfeweenf err de .4.4,47,i4revr.. ty(de 9reitnedect;r/tete ...thetisti/tethive, Owe r.Artie.vmw July 28,2012 Oat r/Atetetwer March 22,2012 /e nva•••ed.• "Gilt mwenelevoC. ..V,•• en' ntitidevtlet• Melvin D. Tay Manager Atlanta Aircraft Certification Office Ity am/scion of can cortilleac• 4 puninad• kr a Imo et net atcoetin shoot, or is inners: nee azenolni 1 rests, et bath. ttlfofat• / to aYUbr PROT552 EFTA 0024200I PROT176 PROT553 EFTA 00242002 PROT177 Limo Preis of America Xleparhnent of transportation - Atberal Ablation gthministration Supplemental Zgrie Certificate (C[cmtinuatiort *get) tirttathieST03960AT When the Rockwell Collins Venue system is installed Airplane Flight Manual Supplement, DB1106015, Revision A, dated March 22, 2012, or later FAA approved revision, is required. When the Aircell Axxess II system is installed Airplane Flight Manual Supplement, DB (002072, Revision IR, dated March 22,2012, or later FAA approved revision, is required. When the Astronics Cabin Inverter system is installed Airplane Flight Manual Supplement, DB1109012, Revision IR, dated March 22, 2012, or later FAA approved revision, is required. This system is intended to provide internet connection and email services to the airplane's cabin using portable electronic devices (PEDs). Any other intended function of this equipment will require a re- examination of the certification basis. When the Rockwell Collins Venue system is installed Instructions for Continued Airworthiness (WAX Nextant Aerospace Document No. DB1002068, Rev IR, dated September 22, 2011, or later FAA accepted When the Aircell Axxess II system is installed Instructions for Continued Airworthiness (ICA), Nextant Aerospace Document No. DB 1105003, Rev A, dated September 22,2011, or later FAA accepted revisions must be made available to the operator at the time of installation. When the Astronics Cabin Inverter system is installed Instructions for Continued Airworthiness (ICA), Nextant Aerospace Document No. DB 1108018, Rev IR, dated September 22,2011, or later FAA accepted When the Enneq LED Cabin Lighting system is installed Instructions for Continued Airworthiness (ICA), Nextant Aerospace Document No. DB11080I9, Rev IR, dated September 22, 2011, or later FAA accepted My elrrnUwn or L1L wrUtlnN L pnbneplr by • bar et net rnerOlnp 11,04 • er lyrbawnr rx oxen so l non, Or bin. TM rose 8110-2 -1110-1,) ?WI 2 of 3 'ACM nilw soy b tranaterml In oiccoto4Ace vI lb FAR 11.17. PROT554 EFTA 00242003 PROT178 PROT555 EFTA_00242004 PROT179 Putteb Ateles of .Avarice !tom:fount of litransportation - Aeberal j16izif ion ciA bininisl ration Supplemental 'Type Certificate (Enntinuation Sheet) Jirtt/2Am ST03960AT fraPojieles/eiv..36144/).. The Certification Basis for this installation is per Type Certificate Data Sheet AI6SW original Certification Basis, Federal Aviation Regulation (FAR), Part 25 as amended by Amendment 25-1 through 25-40 plus FAR 25.1335, 25.1351(d), 25.1353(c)(5), and 25.1447 of Amendment 25-41; FAR 25.29, FAR 25.255, and FAR 25.1353(eX6) of Amendment 2542; and FAR 25.361(6) and 25.1329(h) of Amendment 25-46. In addition the following specified rules amendment levels were used for this installation. 25.571 1 25.1353(a)(c) [25-541 [25-1231 [-] Indicates amendment level 25.1357 [25-1231 25.1431 [25-1131 25.1529 (25-541 AAy alcerstfon of chip cnititicoco Is putiShataf by a hi* of MC excreting 12410, or loprisonseat not •nendleg I rya/s. or lea. rM Rom 1110-2-1410-tfl Hat 3 of 3 h.413 This certificate may be tea ***** rod Is sccoreosce WU, I1.0). PROT556 EFTA 00242005 PROT180 PROT557 EFTA 00242006 PROT181 3800 Southern Blvd Bldg. 1625, Suite 307 West Palm Beach FL 33406 Approved By Report No: DB1002067 Revision F.05 Master Drawing List Document Number: DB1002067 Revision: F.05 10/18/2013 in-Flight Entertainment HAWKER BEECHCRAFT 400A Aircraft FAA STC ST03960AT Date 1-4-2013 Page 1 of 7 PROT558 EFTA 00242007 PROT182 PROT559 EFTA_00242008 PROT183 US D4WInael a Treopmation Eutaw Aviation mminermon ram Ow coed ova Ho. 2120{020 I I/302007 Electronic Tracking Number INSTRUCTIONS: Print or type all entries. Sat FAR 439. FAR 43 Appendix B. and AC 439.1 (Or subSequont reviponthereol) for -nsisuctons are disposition of this form. Tins report is required by bw (49 PROT845. 1421). Failure to report can result on a civil penate not to elMCCI $1.000 for each suannolation (Section MD Federal Aviation Ad 1950 I. Aircraft Nahonally and posistraion Mark N493LX sena No. RK 244 Make Raytheon Aircraft Company model 40OA Smes 2. Owner Nwne (As show° on reg#fraton eettakele) Address (AS 51101vit on legilltatiOn cerbkafel Manes 26180 Curtiss Wriohl PKWY cb,. Richmond Heights Mete OH zit 44143-1453 Cooney 06 3. rif FAA Use Only a. Type 5. Und Identification Repair Alteration Urst Make Model Serial Number 0 it AIRFRAME (As anent.; on Rem I above) ill ID POWERPLANT El El PROPELLER El el APPLVWCE Tyne lAnteciwig A. Agency, Name and Address Mere Nextant Aerospace mow 355 Richmond Road cry Cleveland snare OH ao 44143-1453 Corny USA 0 LI.S. Cenrcatea mecnark 0 Ilearniactund 0 Foreign C•rorcairo mechanic C. Cortikab) No. ea Ceet•catied Repair Stabil CRS # 25NR6678 0 Cerkficaled Maintenance Organization 0. I teitfy that the repair bildlee allerabon made to liw unit(s) identified in item 5 above and described on the reverse Or attachments hereto have been made in accordance won the requIrements OW 11 43 of !M U.S. Federal McMinn Rev:eh°, s and that the -nrocfiatied furnished harem is true and 03Crea to the best of my knoorledge. Emended range fuel eel de PROT846 Part 43 Apo 9 0 SignalureDale of Authorized Individual Anton J. Koons/Mk 12/29/2013 7. Approval toe Return to rustic Pusuanl to the aulhonty given persons Wended berms the unit identified in item 5 was inspected in the manner preScnbed by the Administrator of the Federal AwananAdmineadeen and M El APPROVED 0 REJECTED BY FM Fit Standards Inspector Manufacturer M aintenance Orgarmation Parson Approved by Canadian Department of Transport FAA Designee InSP4010n AufiVrilabon Omer Specify) Cents*, Delbration No. CRS N 25NR667B S rature/Date of AuMortzed Mcbcdual de 7 7 t 12/29/2013 err d FAA Form 337 poem PROT560 EFTA 00242009 PROT184 PROT561 EFTA 00242010 PROT185 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record An alteration must be Compatible with aft previous alterations to assure continued conformity with the applicable northiness requirements (If more space is required, attach additional sheets identify with aircraft nationally and registration mark and date work completed.) N493LX 12/29/2013 Date Upper Aft Baggage Panel Mod Modified Baggage Ceiling Panel to Accommodate the Engine FADEC wire harness. 1. Fabricated two panel pieces, N251103-001 and N251103-002. 2. Installed N251103-001 to existing baggage compartment structure 128.440095-1 using two screws and install N251103-002 as shown with a trim to fit honeycomb piece fabricated from interiors using potted inserts. 3. Attached honeycomb baggage panel to N251103-001 in upper aft baggage area using three 40S5-21 Camloc quarter- turn fasteners and 214-16D receptacles. Secured N251203-002 to existing upper aft baggage panel with two Camloc 4055-21 quarter - turn fasteners and 214-16D receptacles. See attached FM Form 8110-3 Signed by DERT-410115-CE Paul Hedding on February 12. 2013 using Nexlant Aerospace Engineering Order EO 029. Rev E Dated February 8.2013 ICA Weight change is Negligible. Continue with Beechjet 400/400A Maintenance Manual Inspection Procedures for this Area End FAA Form 337 (ckos) SONY_GM_027550139 EFTA_0024201 I PROT186 PROT562 EFTA_002420 I 2 PROT187 FEOERAL AVIATION AOMINISTRATION 1 DATE February 12, 2013 2. MAKE Hawker Beechcraft Corporation 3. MODEL NO. 400A 4. TYPE (Aircraft ErKene. nrOneder. eSc.) Aircraft 5. NAME OF APPLICANT Richmond Heights, Ohio LIST OF DATA 6 IDENTIFICATION 7 TITLE EO 029 Rev. E February 8, 2013 Upper Aft Baggage Panel Mod. END Notes: 1) The structural aspects only of the above listed data are approved herein. This approval is only for the engineering data. It indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and subparagraph listed below as "Applicable Requirements." 2) This form constitutes FM approval of all the engineering data necessary for substantiation of compliance to necessary requirements for the entire alteration. S. PURPOSE OF DATA Engineering data in support of major alteration to Hawker Beechcraft 400A, SIN RK-244. 9. APPLICABLE REQUIREMENTS (List Weak WS4) PROT847 Title 14 Part 25.301[25-23], 25.303(25-23], 25.305(a)(b)(c)(25.23J, 25.307(a)(25-23], 25.562(c)(25-23], 25.601[25.00], 25.603(a)(b)(c)(25-38), 25.605(a)(25-00), 25.607{25-23], 25.609(a)(b)(25.00), 25.611(25.23], 25.613(a)(b)(c)(25-00], 25.619(25-23], 25.625(a)(b)(c)(25-23], and 25.789(25-32]. 10. CERTIFICATION • Under authority Part IB3, data Wed above and on apcimble requirements of Ito AinCettaleSS vested by deecton 01 the Administrator and I, accordance vsth condsons and nmsa5cns of appcintrneM under 14 PROT848 Washed sheets numbered WA have been examined in accordance wee establ.wed procedures and Found to comply with Standards Listed. approval of New data these data Recommend I (We) Therefore 0 Approve I1. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(5) 12. DESIGNATION NUMIERS($) 13. CLASSIFICATION'S) •sr ---"407 - Paul Hedding DERT-410115-CE Structures FAA Form 81103 (0110) SUPERSEDES PREVIOUS EDITION We Number H13107-06 Page 1 of I PROT563 EFTA 00242013 PROT188 PROT564 EFTA 00242014 PROT189 e MAJOR REPAIR AND ALTERATION uSOirawmort or (Airframe, Powerplant, Propeller, or Appliance) cirsoontoot reword Arbon 4.4minsireim Fenn Aerate OW. 212043320 CCM Eltchonn Tracking Number For FAA Ufa Only INSTRUCTIONS: PrM1 or type a alai. See FAR 4&9. FAR 43 Appendix & and AC 43.9-1 (or subsequent revision Memo° for instruckas and diSposilion of this form. This report Is required by law (49 PROT849. 1421). Failure le report can result In a call penalty not to exceed 31.030 for each such ligation (Section 901 Federal AUabal Ad 1953) 1. Aircraft NeleAlidy and Reczalraben Mark N493U( Serial No. RK 244 Make Model 400A Series t. Owner Perna (As skim on rflistrafron CerhOCOM Flight Options .I.LC Address (As shown on rep/save% centekafe) Peeress 26180 Curtiss Wright PKWY ciiy Richmond Heights sum OH Z9 44143-1453 So-ant Oa 4. Type Repay Metalled Unit Make Model Serial Number O 0 AIRFRAME (As described in nem f above) O POWERPLANT El O PROPELLER O O APPLIANCE Type NtrivJaeder 0. Conformity Stet mom B. lard of Agency Nam Addroris 355 Richmond Road coy Cleveland sink OH za 44143.4453 Cony USA 0 lie °MACAW Mechanic 0I Mankfacturer 0 Ferias Camas's rarrthanic c. cerebra No. i Cildideated Repair Station CRS # 25NR687B 0 castrated Maintenance organizawa 0. I anbly that the repair &Wry alteration made tome una(s) denlifieti in ilem S above and described on Me serene or attachments hereto have been made in accordance Nile the requirements of P rl 43 Of the U.S. Federal AviabOn Regulations a nen a: the ink:mar:ton furnished heron is Irue and arrecl 10 the beg Of my knowledge. Extended range fuel per 14 PROT850 Pan 43 Pep. e - Signaturetele c4Autixtrilet InOsidual 12/29/2013 l 7. Approval for Return to ce sa Pursuant lo the authority given persons peened below, the unit dangled in item 5 was inftpeeled in the manner prescribed by the Administrator of the Federal Aviation Administration are is 121 APPROve0 O REJECTED FM Flt Standards Inspect*: Manufacturer Maintenance Oramizalion Department of Transport BY FM Ochres X Recast Sleben Other ) InspecionAulhorizabon ceteraOr Desiginalian No. CRS ft 25NR66713 Scraturntale of Amhonzed Indrddual 4 1229/2013 FAA Foam 337 (loam PROT565 EFTA_002420 I 5 PROT190 PROT566 EFTA_00242016 PROT191 NOTICE Weight and balance or operating limitation changes shalt be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations fo assure continued conformity with the applicable airworthiness requirements. (If more space is required, attach additional sheets. Identify with aircraft natkaulley and registration mark and date work completed) N493LX 12/29/2013 Date Installed New Pitot Probes in accordance with SIC ST10159SC. Nextant Aerospace Master Drawing List Document [SSN REDACTED] Rev CC E024-11 Removed Pitot Probes Part Number PH1100-MU-R-1 Removed Pitot Probes Part Number PH1100-MU-L-1 Installed Pitot Probes Part Number PH1100-MUR-EN Serial Number 1975803 Installed Pitot Probe Part Number PH1100-MUL-EN Serial Number 1728401 Leak Check carried out IAW Beechcraft Aircraft Maintenance Manual Chapter 34-12-00-201. ICA Continue with Normal Hawker Beech Maintenance Practices for this Area End K Addilional Sheets Are Attached FAA Form 337 (mob) PROT567 EFTA 00242017 PROT192 PROT568 EFTA_002420 I 8 PROT193 a U.ElDeementrace (Airframe, Powerplant, Propeller, or Appliance) teeepeetplee areas AViabla mairastre.on Fab cov anonco7 ea ONO Ne. mooElects* Tracking Number INSTRUCTIONS: Print ce type all envies. See FAR 43.9. FAR 43 Appendix B. and AC 43.94 (or subsequent revision thereol) for astrumans and atbeatiOn Of thiS Rum. This Meal iS required by law (49 PROT8511421). Failure tie tat can result in a civil penalty not to exceed $1.000 for each such violation (Section 901 Federal Aviation Act 1958) I.Aircraft Nabonalty and Regestraton Mart N493LX Serial No. RK 244 Make Model 400A Series Owner Name (As show, on registration cortthcata) Address (As shown on registration oerhficate) meow, 26180 Curliss Might PKWY 2. any Richmond Heights sin OH zo 4±11,4a4.53 country USA 4. Type Repair Menem lJed Make Model Serial Number El 0 AIRFRAME (As discrete in item I awe.) 0 O POWERP1ANT CI O PROPELLER s O APPLIANCE Typo Menulackeer II. Conformity Statement A. Arrays Name and Acmes: a Kind of Agency Novi Adam [ADDRESS REDACTED] Carey USA 0 0 S. Cenncated arecAanic 0 Man Vacever CI Foreign Cortical Mechanic C Ceti riCale No 0 Cendicated Repair Station CRS # 25NR6678 0 Cerbficated Maintersarbe Organized*, D. I tatty that the repair (index alteration made to the Lobs) identified in item 5 above and described on the reverse a attachments hereto have been made in accordance tirrh the requirements of P rl 43 el ,,c U S Federal Aviation Republica. and Mal the informanm furnished herein *lrue and correct ID the beet 01 my knowledge edended range fuel per 14 PROT852 Pan 43 APP. B O Signature/Date of Autheilted Individual 12)29/2013 2i 7. Approval for Return Ma Pursuant lode authority given persons pecited below. the unit identified Administrator of the Federal Aviation Administratim and is rb in Om APPROVED 5 was in:peeled in Me manner prescribed by the REJECTED By FM Fe Standards Inspector Manvlacurer Makeenance ClightliZZAka Department of Transport FAA Designee X Regale Station impectonAuthoozetion Other (Sce00) Certificate or Desapraton nib. CRS # 25NR6679 Manature/Date of Authaized Individual J. Koprivnik 12129.'2013 at FAA Form 337 DOOM PROT569 EFTA_00242019 PROT194 PROT570 EFTA 00242020 PROT195 NOTICE Weight and balance or operating limitation changes shall be entered in the Appropriate airaaft record. An alteration must be compatible with at previous aerations to assure continued conformity mth the appaable airworthiness requirements (If more space is required. attach additional sheets. Identify with aircraft nationality and registration mark and date work completed) N493LX NationaMy and Registration Mark Provisions for 19107 in Cockpit Sidewall at F5122.735 12/29/2013 Date Added Mount provisions for19107 in bracket assy. 45A88588-3 at Flight Station 122.735 provided in Structure Repair Manual Document 53.20.05-001. Use receptacle MS3470W18. See attached FAA Form 8110-3 Signed By DERT-410115-CE Paul Hedding. Dated December 28, 2012 using Nextant Aerospace Engineering Order 115-12 Rev C, Dated November 27, 2012 for details. ICA Weight change is Negligible. Continue with Beechjet 400/400A Maintenance Manual Inspection Procedures. End FAA Form 337 (I 046) PROT571 EFTA_00242021 PROT196 PROT572 EFTA 00242022 PROT197 U S. DEPARTMENT Of TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 1. DATE December 28, 2012 2 MAKE Corporation 3. MOOEL NO 400A 4. TYPE (AVCratt Enpne. Propeller. eta) Aircraft 5 NAME OF APPLICANT Nextant Aerospace LW Richmond Heights, Ohio LIST OF DATA 8 IDENTIFICATION 7 TITLE EO 115-12 Rev. C November 27, 2012 - Mount Provisions for J9107. - END - Notes: 1) The structural aspects only of the above listed data are approved herein. This approval is only for the engineering data. It indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and subparagraph listed below as "Applicable Requirements.' 2) This form constitutes FM approval of all the engineering data necessary for substantiation of compliance to necessary requirements for the entire alteration. a. PURPOSE OF DATA: Engineering data in support of major alteration to Hawker Beechcraft 400A, S/N RK-244. 9 APPLICABLE REQUIREMENTS Gist spear stollens/ PROT853 Title 14 Part 25.301(25.23), 25.303(25-233, 25.305(a)(b)(c)(25-23), 25.307(a)(25-23), 25.601[25-00], 25.603(a)(b)(c)(25-381, 25.605(a)(25.00], 25.607[25-23E 25.609(a)(b)125-001, 25.611(25-231 25.613(a)(b)(c)(25- 00j, 25.619[25-23], and 25.625(a)(b)(c)(25-231. ID. CERTIFICATION • Under autos* vested by direclico of the Admire:Oak( and in accordance with ccarlibons and limitations of app9mment Lamer 14 PROT854 Pad 113. data toned above and on adached sheets numbered _NM have tern twined in accordance vai established procedures and found to comply with appaceble requirements of the Ainverthioess Standards Listed. 0 Recommend approval of these data 0 Approve those data it $iGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATNE($) 12 DESIGNAGON NUMBERS(S) 13. CLASSIFICATION(S) Igtg ' 2- Paul Hedding DERT-410115-CE Structures FAA Form 8110-3 (03.10) SUPERSEDES PREVIOUS EDITION Fee Number H1274043 Page 10(1 PROT573 EFTA_00242023 PROT198 PROT574 EFTA 00242024 PROT199 0 U S Desennial ce (Airframe, Powerplant, Propeller, or Appliance) haiseaseat Feeeni Aviation Adoinhintien Form Apprma O1AS Ho. 21204020 in-8mo/ Elector Tre:f.0ng Number INSTRUCTIONS Prim co type all entiles See FAR 43 P FAR 43 Appendix 0. and AC 43 9.1 (or sarsequem caws on thereof) for mStruCcres are disposinon of MIS rpm. ThiS rennet is required by law (49 U S.C. t421) Failure b report can renal in a civil penny nol lo acted 51.000 kw iaacA sodi iolation (Section 901 Federal Aviation Act 1955) 1. Aircraft Natananty and Registration Mark N493LX Serial No. RK 244 Make Model 400A Series 2. Owner Name (As skean on regaltabon cookers, Address (As shown on registration arbficate) Aosess 26180 Curtiss Wright PKWY CA, Richmond Neigh% Nem OH 20 4A14344)51 canry USA 4. T pe 5. U It Identification Repair menden um Mao Model Serial Number El 0 AIRFRAME (As descasel in Item I above) 0 O POWERPLANT 0 O PROPELLER IN 0 APPLIANCE Ty", "wawa 6. conteemity Statement A. Ageneys Nana and Address 8. Kind a Agency Name Mott [ADDRESS REDACTED] corer USA 0 U.B. Cenidcated Mechanic 0 IManufaceser 0 Foreign cenNeatee Memaic C Cerbficabn No. a Certificated Repay Slam CRS it 25NR6678 0 Carbecateg Manlenance Organization 0. I certify that the repair ander alteration made to the trid(s) emirs in item 5 above and dilated on the reverse Of attachments WOW have been made in accordance wen the requiter/ferns ciParl 43 of the U.$ FederalAviation Regulations and that the Oformation Wished herein is true and correa to the beet of my knowledge. Exergea range fuel per Ade0 14CFR Partin O SignetUrealate omuthonzeo Indio 12/29/2013 7. Approval for Return to Se Pursuant to the autInor3y green persons Spected bebet, the un lidentifild Admirestiala or the Federal ARKIN' Administraeon end Is 0 In dem APPROWO 5 was inspeced In the manner Faulted by the Attctto BY FAA Fit standar/Is inspector Manufacturer Persia) b ian Department of ransom FAA Designee X Repel Simon Inspected Authorization Other (Speedy) Certificate or Desitastion No. CRS # 25NR6676 SigneuraVale or Authorized Individual 7C 12/29(2013 FAA Form 337 (loos) PROT575 EFTA_00242025 PROT200 PROT576 EFTA 00242026 PROT201 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous arerations to assure continued conformity with the apPbCable aiworthinesS requirements (tenure space is required attach additional sheets Idenbly with aircraft nation's* and registration mark amidst* work completed.) N493LX Nationany and Registration Mark Title: Ice Detector Master Caution / Master Warning Light on Constantly Re-Installed the previously removed components ( Ref S/B 30-2600, Rev 2) 12/29/2013 Date 1.) Isolation Relay K255 P/N: 50-380048-1 2.) Diode CR654, P/N: 132408-22 3.) Ground stud GS151A P/N: MS35206-246 (Stud may be marked GS152) As shown in chapter 30-01.01-01 of AMM. 4.) Wire number corrections on wiring diagram 30-01-01-01 Page 1 correct drawing errors on original drawing. Inspect, verify and correct wiring per EO corrections on EO page 2 See attached FAA Form 8110-3 signed by Daniel Buzz DERT-230019-CE. Dated 8/13/2012 using Nextant Aerospace Engineering Order EO 0130 Rev D. Dated 7/18/2012 ICA Weight and Balance Changes are Negligible Continue to Use Existing Beechjet 400/400A Maintenance Manuals Inspection Procedure for this Area END FAA Form 337 papa) PROT577 EFTA_00242027 PROT202 PROT578 EFTA [ADDRESS REDACTED]ATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS • 1. DATE 8-13.2012 2. MAKE '.. 'Iwker Eleechceatt 3. MOOEL NO 400A SIN RK-244 Only 4. TYPE (Airplane. Radio. Herospfer. etc) Airplane Nexcent Aerospace. LLC LIST OF DATA 8.IDENTIF/CATION 7. TITLE Revive Aerospace Document 130-12 dated 7.18-12 Rev. D Engineering Order Ice Detector WNW Light On Constantly END ThiS approval is for the actrical systems aspects only. S. PURPOSE OF DATA Support major elleiragen to Micron Hawker Ecerchcrall 400A RK.244 Only. 9. APPlICASLE REOUIREtJeNTS (L:Nwedge Su) 14 PROT855 25.1301(a) (O.1g1 Note: Compliance has been found to the amendment levels inckaled on Homes Beechcrefl TCDS Revision 26 Pad 25 Amendment 25-1 through 25-40 to the above applicable reoutremeMs. 10. CERTIFICATION - Under math why vested DV direct«. of he AcInkcestralor and in aTandanat Milli POIXD10n5 and limitations of appointment under 14 PROT856 Pan 183 of the Federal Aviation Regularlons. data Crated Mho and on mired sheets neurtnoil M:8 have been MarTIMMil et accordance with established procedures and round to comply with applicable requirements of the Airworthiness Standards listed. I (We) Therefore approve these data. - it SIGNATURE( NATE E NE RINQ REPRESENTATNE(S1 it DESIGNATION NUMBERMS) 13. DtAssiFicATI0NtS) - Dade] i.. Bunt DERT.230019-CE Systems and Equipment ..AA Form 8110-3 (03110) SUPERSEDES PRENK0US EDITION GPO 9014113 PROT579 EFTA_00242029 PROT204 PROT580 EFTA_00242030 PROT205 0 MAJOR REPAIR AND ALTERATION i)a S arms a T pas Fedenol 444404 Adolnistraben Fran ammo Maw N20-0320 II/307007 Electronic Tracking Number For FAA Uso OalT INSTRUCTIONS Print or type an mines See FAR 43.9. FAR 43 Appendix B. and AC 43 9-1 (or subsequent rata thereof) la instruCbCns and disposeion a This form. This tenon is required by law (49 U.S C. 1421) Fare to sepal can result in crid penalty not to exceed $1000 Ion each such votatcin (Sean 901 Federal Aviation Act 1958) I. Aircraft N493LX Sail No. Rt< 244 Make Model 400A Sees 2. Owner Name (As Moen on reeistraboo Certarcate) Adckess (As shown on reg#Irabon awfikate) Moan Curtiss Wright PKWY car Richmond Heights slat OH to 44143-1453 COL443 ai 4. Type 5. UMW'S:Mention Reps Alerabon Veit Make Model Serial Number El O AIRFRAME (As desonbed In ffem 1 above) 0 El POWERPLANT O O PROPELLER O O APPLIANCE Tyne mar asoa ll Conformity Statement A Agency's Name and Address B. KM of Agency 1411441 Asa [ADDRESS REDACTED] citi Cleveland smut. OH zo 44143-1453 cony USA 0 U.S. Cerlificaled Mechanic 0 IManufsdorer 0 Foreign CerIfical Mechanic c. cantata. No 0 Certificated Repair Sieben CRS # 25NR667B 0 Cartricaim maintenance °roam/aeon O. I ably that the repair anovot aaaratian made to the unt(s) Mead in item 5 above and descnbed on the reverse or Naval, hereto have been made in accordance with the requirements a PM 43 of ton U.S. Federal Aviation Rep/taws and that the information furnished herein is Ma and coned to the al of my knowledge. Extended range fuel pe 14 PROT857 Pan 43 As 8 O SignaharMoste OASIS:cid Individual Anton J. Komivnik a 720.._ cii t y 12/29/2013 7. Approval for Return nice Pursuant to the avirtority awl persons waited below. the un Identeled in nem 5 was impeded in the manner prescribed by the Adrithistrakx of the Federal Aviation Administration and is ®APPROVED O REJECTED FM Fit Standards inspector Mani/Kam Departrnent or Transport BY FM Designee X Raper station Oktra (Spearly) inspeCl/On AuthorizMion Comical° or CRS it 25NR667E1 Signature/Dale c4 Authorized IndMdual d e,,t' y 12/29/2013 a e< ate FAA Form 317 tto-cist PROT581 EFTA_00242031 PROT206 PROT582 EFTA 00242032 PROT207 NOTICE Weight and balance 0, operating limitation changes shall be entered in the appropriate °Wren record. An alteration must be compatible with alt previous alterations fo assure continued conformity with the applicable einvorthiness requirements. (If more spec* is requited. attach additional sheets. Wen ify with aircraft nationality and registration math and date work completed.) N493LX Antenna Repair Patch 12/29/2013 Date After removing the forward lower "I? Band Antenna, Instead of removing the Antenna doubler and filling the connector hole with a coin patch and installing nut plate plugs P/N. DB1105020-189-25, the antenna repair doubler P/N. DB104042-001 was installed on the existing antenna doubler and two coin repair patches Pin. DB1104042-002 were installed, one on top of the other to allow for a flush skin repair. The existing nut plate holes were filled with 4 screws P/N. AN525-10R7. See Attached FAA Form 8110.3 signed by DERT-410115-CE Paul Hedding dated August 15, 2012 using Nextant Aerospace Engineering Order 139.12 Rev C Dated August 03, 2012 for details. ICA Weight and Balance change is Negligible. Continue with Beechjet 400/400A Maintenance Manual Inspection Procedures. End K Ackhlional Sheets Are Attached FM Form 337 (10.06) PROT583 EFTA_00242033 PROT208 PROT584 EFTA 00242034 PROT209 FEDERAL stAllATION ADMINISTRATION 1. DATE August 15, 2012 2 MAKE Corporation 3. MODEL NO 400A a. TYPE (Airaart End** Prope*r. etc) Aircraft 5 NAME OF APPLICANT Richmond Heights. Ohio LIST OF DATA 7 TITLE EO 139-12 Rev. C August 3. 2012 Antenna Repair Patch (L-Band Notes: 1) The structural aspects only is only for the engineering compliance only with the below as 'Applicable Requirements: 2) This form does not constitute necessary for substantiation entire alteration. The electrical and require separate approval. Antenna Moved). of the above listed data are approved herein. This approval data. It indicates the data listed above demonstrates regulations specified by paragraph and subparagraph listed FM approval of all the engineering data of compliance to necessary requirements for the requirements are not included in this approval s PURPOSE OF DATA: Engineering data in support of FM STC ST03960AT. 9. APPLICABLE REQUIREMENTS (Lel setae wows) PROT858 Title 14 Part 25.301(25-23], 25.303(25-23), 25.305(a)(b)(c)[25-23], 25.307(a)(25.23], 25.365(a)(b)(c)(d)(f)(g)(25.00). 25.562(c)(25-23), 25.601)25-00]. 25.603(a)(b)(c)[25-38], 25.605(a)(25-00), 25.607[25-23), 25.609(a)(b)[25-00], 25.611(25.23). 25.613(a)(b)(c)(25-00), 25.619125-231, 25.625(a)(b)(c)(25.23), and 25.789(25-32]. 10. CERTIFICATION - Under autbety Part 183. data Wed above as on apecatto requirements of Me Atmerteness vetted by Cfneetage of Me Mreistralor and e accedence we, condemn and Neatens of appelment under to PROT859 attached sheets numbered N/A have been teamed in accordance MN estatened procedures and Iced to cane we &Wards Listed. approval of these data thee data Recommend I (W) Therefore tg Approve II. SIGNATURE'S) OF DESIGNATED ENGINEERING REPRESENTATMEIS) 12. DESIGNATION NUMBERS'S) 13. CLASSIFICATION(S) c'e'a"-- Paul Hedding DERT-410115-CE Structures FAA Form 81104 (03.10) SUPERSEDES MUMS EDITION File tenter. H12418-02 Page 1 of 1 PROT585 EFTA_00242035 PROT210 PROT586 EFTA 00242036 PROT211 e US Oapatmeni el (Airtrame, Powerplant, Propeller, or Applianco) nusatwen lama Adatlen Marnistneen reinsame 0618No. 2120.0320 1.1 ElectrooRTrackng Runt« Fm FAA Us* On& INSTRUCTXWS: Pantar type an tablett. See FAR 43.9, FAR 43 Appendix B. and AC 43.9-1 (or subseguenl Maisen ~ei) for instrwlions and 66006666 end form. 1TR nidorl is requirecl by latv (49 PROT860. 1421). raken »repp:tam endt in a cml gray not to exeeed $1,000 Mr esch suck oblaten (Selvion 901 Federal Realitet Ad 1958) 1. AlreraR Naroonalay and Registra-1N Man N493LX Serai no. RK 244 Mane MOdel 400A Settes 2. Ormer Naine (fl shOmi on reoistagon ~Son) Meien (As shows on (s~ation "ne) Øs CurtissWriaht PKWY os Richmond Heights sta OH u 44143-1453 venn Q8 3. For FAA Un Onty 4. Type 5. U It Wentification Repair Atleraten Unn Make Model Sedd Runder D s AIRFRAME (As aescntel pn (km I *bose) D O POWERPLANT 0 O PROPELLER O O APPLLANCE Type Manuiedvet 6. ConformNy Statoment A ~dis Norne and Addtess B. knea Agency Nyre Nextant Aerospace rams 355 Richmond Road on Cleveland sua OH vo 44143-1453 Gule USA a U.S. Ceitidealed hiechand o I Manufseturer 0 Foreign emnes:dl Mechanie C Gen/kote No. Ø Cefl&aled Repet Motion CRS It 25N R662B a Cenincated Mainlenance Organizahon D. I cenify dial the repet ania)0, ~i made to the tinde) identified in Hein 5 aten« and clescnbecl on the (Nede ot allachments hegle neve ban made in accareanca un the requiremenIS of P n 43 of the U.S. FeelnalAviatinn Regulator: and Nat the informabon luntende hereln is Na ard atirrict lo the best of my iironeedge. Extended range lidi per 14 PROT861 Pan 43 APP. B D Signaturallate ol AulhOrneel Indiviebal Anton J. Koptivnik 12/29/2013 f .....,fle f 1. Ap val til to Servl Insinuant lo the mitimmy given persons emne) belma, am un I iderilMed in den 5 was inspecied in Ne manne veoxibtrl by gle Adilinelreke Cd the Federal Mima MministratOn and is Ø APPROVED Cl ROECTED FM Fl Siantlads Inspector idanufactufer Maintenanco Organization Person Approvecl by Canaoian Departrrmintof Transport BY FM Designe. X Ropa« Stausn inspection Authorizahsn ONN (SP•Fdd Naticale or ougneten aa CRS S 25NR6678 s s SpnattrelDale N AuSionzed Individvaair 12/29/2013 in FAA Forn 337 (10-06) SONY_GM_02755115 EFTA_00242037 PROT212 PROT587 EFTA_00242038 PROT213 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all prewoos alterations to assure continued conformity with the applicable ainvorthiness requirements. Of more space is required attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) N493LX Nationality and Registtation Mark Title: Pedestal cover extension Modification 12/29/2013 Date After STC modification of pedestal per 373-94-I 000)3, existing pedestal close out tray needs to be extended to cover appropriate areas. Modification of the close out tray is required. Modify the pedestal close out tray per drawing NX25 I - I 0002. See attached FAA Form 8110-3 signed by Paul Hedding DERT - 410115-CE. Dated 11/8/2013 using Nextant Aerospace Engineering Order EO1018 Rev F. Dated 10/9/2013 ICA Weight and Balance Changes are Negligible Continue to Use Existing Beechjet 400/400AMaintenance Manuals Inspection Procedure for this Area END FAA Form 337 (1046) PROT588 EFTA_00242039 PROT214 PROT589 EFTA_00242040 PROT215 V.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ACAIIMSTRATK)N 1. OATE November 8, 2013 2. MAKE Corporation 1. 1.010EL NO 400A 0 TYPE (Aircraft Enpne, PeopeNtr. Et) Aircraft 5 NAME OF APPLICANT L Cleveland, Ohio LIST OF DATA 8 IDENTIFICATION 7 TITLE EO 1018 Rev. F October 9, 2013 Pedestal Cover Extension Modification. Notes: 1) The structural aspects only of the above listed data are approved herein. This approval is only for the engineering data. It indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and subparagraph listed below as "Applicable Requirements' 2) This form constitutes FM approval of all the engineering data necessary for substantiation of compliance to necessary requirements for the entire alteration. a. PURPOSE OF DATA Engineering data in support of major alteration to Hawker Beechcraft 400A, SIN RK-244. 9. APPLICABLE REQUIREMENTS (UM speak womb PROT862 Title 14 Part 25.301[25-23j, 25.303[25-23), 25.305(a)(b)(c)(25.23), 25.307(a)(25-23), 25.562(c)[25-23], 25.601[25.00), 25.603(a)(b)(c)[25-38), 25.605(a)(25-00), 25.607[25.23], 25.609(a)(b)[25-00], 25.611(25-23), 25.613(a)(b)(c)(25-00], 25.619(25-23), 25.625(a)(b)(c)[25-23], and 25.789[25-32]. 10. CERTIFICATION • Under autheriN vested by Orman of the Administrator and In ace dance with earthen; and limitatbres et appoiMmem 'Ada 14 PROT863 Partin. data stied above and on attached sheets numbered NIA_ have been examinee in mconlance nith estabished procedures and found to ecniptivith applcaoh requirements of the kiwortrtirms Standards Listed. 0 Recommend approval of these data (23 Approve these data II. SIGNATURE1S) OF DESIGNATED ENGINEERING REPRESENTATIVES) 12. DESIGNATION NUMBER$($) 13. CLASSIRCATIONoa Olt 5.', --> 17 Paul Hedding DERT-410115-CE Structures FAA Form 81104 (03-10) SUPERSEDES PREVIOUS EDITION Fie Number H13817-04 Page 1011 PROT590 EFTA_00242041 PROT216 PROT591 EFTA 00242042 PROT217 0 MAJOR REPAIR AND ALTERATION u S Deerninl el Tv mlioxtake. Nano Aria*. Modrisliallon folnAwckad O M No 21204020 I ifXv2C07 Eiectionic Tracking Number INSTRUCTIONS: Print or tweet enbies. See FAR 43.9. FAR 43 Appendix B. and AC 43.9-1 (or sub's:pent revision memo for instructions and cesposigcn of Ins form That report a required by law (49 PROT864. 1421). Failure to rePerf oan result in • c)if Penal not to need $I.kat eath SuCh *talon (SeCkie 901 Federal Aviation Act ISM) I. aroMl Nabortaidy and Repatriation WA N493LX Serial No. RK 244 Make Raytheon Aircraft Company more 400A Sates 2. Owner Name (As shown on registration confined Address (As shown on registration ortificar4) Address 26180 Curtiss Wright PKWY cry Richmond Heights sw, OH zo 44143-145_3_ Carry USA 4. ype Repay Allerebon Unit Make model Serial Number CI AIRFRAME (AS descnatain Hem I above) 0 O POWERPLANT ID O PROPELLER ID MI APPLIANCE TOO IMMULICIartit 6. Conformity Slat mont A. AgeMYe Name and Address B K nd of Agency Pa Neaten( Aerospace *anis 355 Richmond Road Cory Cleveland sue. OH ip 44143.1453 aunty USA _0 0 u S. Certificated Methane 0 ManufaCturer 0 FOreqn Cenficaled *chant C CetifIcate No. 0 Seitlitated Repair Station CRS # 25NR667B Caroficaled Mentionsme Organization O. lc:edify that the leper artier attention made to the unit(s) identified in item S above and descnbed on the reverse or anennents hereto RUG been made in accordance with the requirements of P rt 430f the U.S. Federal Maiden Regulations and OW tie INCX11134011 furnished beret, is hue and correct to tie beat of my knowledge. &ended farce rue 14 per PROT865 Part 43 App. B El Signalure/Vate of Authorized individual Anton J. Koprivnik tape7, 12/29,2013 7. Approval for Return to Settee Pursuant to the adhoilty given pe sons molted below. Me unit Adminisbanc of the Federal AMMIC41 Admonition and is in den led in men 5 was inspected In the manner deserted by the APPROvE0 0 REJECTED ay FAA FS Standards inspector Manursolurer Oeparuners of Transport FAA Designee X Repay Station Inspection Autheetnace Omer (Spicer) Certificate or Desi NO. ton 25NR6676 CRSgn rt SidnalwerDatio of Authorized Individual ....94::> 12/29/2013 4 " FAA Form 337 (10-00) PROT592 EFTA_00242043 PROT218 PROT593 755122 EFTA 00242044 PROT219 NOTICE Weight and balance or operating /imitation changes shall be entered in the appropriate aircraft mead. An alteration must be compabble with all previous alterations to assure continued conformity with the applicable airworthiness requirements 8. Description of Work Accomplished al more space is required attach additional sheets. Identify with aircraft nationality and registration mark and dale work completed.) N493LX DEACTIVATE CLOCKS 12/29/2013 Date For Pilots Clock Deactivation: I.) Removed PLT CLOCK circuit breakers from LH FWD CB Panel. Spliced feed wires together. Cap and Stowed Load side wires. 2.) At Radio Junction Box: a.) disconnected wire W78-I9 from 3931125 PIN R & S. b.) Spliced wire W78-19 from pin R with 3931122 wire W7I-3 (20) pin D•. For Co-Pilots Clock Deactivation: 4.) Removed COPLT CLOCK circuit breakers from LH FWD CB Panel. Spliced feed wires together. Cap and Stowed Load side wires. 5.) At Radio Junction Box: a.) disconnected wire W78-45 from 393 ITBI 3931R3 pin 3. b.) cap and stowed wire. c.) Installed jumper from pin 3 to 3931322 pin P (splice with wire W7I-4 (20)) 6.) Tcstcd all WOW interface circuits at HI & #2 DCU, # 1 & #2 DCP,41 & #2 PEWS' & #2 MFD, DAU, 41 &#2 ADC, 4 I & 42 GPS, 41 & 42 FEU, #I & 42 TDR. 7.) Changed power wiring for ELT from 42 Clock to #2 Audio panel. Disconnected wire from inline fuse ELTFI feed side and connected to Audio power input 2350P4 pin 8 (spliced with wire W965.019 (20)). Tested ELT. This removal was electrically approved by Daniel L. Bun FAA DERT-230019-CE using a FAA 8110-3 Dated November 15, 2013 Using Nextant Engineering order 1165 Rev B Dated 11/13/2013 End FAA Form 337 00-00 PROT594 EFTA_00242045 PROT220 PROT595 EFTA_00242046 PROT221 1 DATE 11-15-2013 2. MAKE - Hawker Beechcraft 3 MODEL NO. 400A Stal RIC-244 Only 4. TYPE (Airplane. Raft AMMOMm; eft.) Airplane LIST OF DATA &IDENTIFICATION 7. TITLE Document EO 1185 dated 11.13.13 Rev. B Engineering Order Deactivate Clocks elecb-ical systems - - This approval is For the END-aspects only. 8. PURPOSE OF DATA Support mayor alteration to aircraft Hawker Beechcraft 400A RK-244 Only. 9. APPLICABLE REQUIREMENTS (List sneak sections) UT PROT866 25.1301(8)(0dg] Note: Compliance has been kund to the amendment levels indicated on Hawker BeeChtraft 400A TCOS Revision 28 Part 25 Amendment 25- 1 through 25-40 to the above applicable requirements. 10. CERTIFICATION - Under authority vested by direction of the Administrator and in accordance Min conditions and imitations of appointment under 14 PROT867 Part 183 of the Federal Aviation Regulations. data listed above end an altsched sheets numbered TE5 have been examined In accordance with established procedures and found to comply with ape/male requirements of the Airworthiness Standards lived. I (We) Therefore approve these data. ii. SIGNATDRE(S a, ESIGNA, D ENGINEERING REPRESENTATNE(S) 12. DESIGNATION NUMBERS4S) 13. CLASSMCATIONISI i DERT-230019-CE Systems and ErnftorneM Daniel L. 9. • .r AA Form 8110-3 (03410) SUPERSEDES PREVIOUS EDMON GPO 901413 PROT596 EFTA_00242047 PROT222 PROT597 EFTA 00242048 PROT223 0 MAJOR REPAIR AND ALTERATION u soshienme, Transports* rest Ass mareasaron roan Approved OMB NO. 2120.0020 or3D2337 Etectionlc Tartan Number Foe FAA UM Only INSTRUCTIONS: Print or type an wan. See FAR 43.9. FAR 43 Appendix 9. aid AC 43.9-1 (or subsequent revision Smog for instrucarrt and t1SpOsilion of this form This report is required by law (49 PROT8681421), Faire to report can result In a Call penalty not lo exceed $1.000 for each such violets (Saba 901 Federal Aviation Act 1958) 1. Aircraft Mahwah'', and Registracer Mark N493LX Serial No. RK 244 Make Model 400A Series 2. Owner Name (As snows on registrar ron cerhfictrM) Flight Options .(SC Address (As snows On reparation centre/Cafe) Moots 26180 Curtiss Wright PKWY cry Richmond Heights sirs OH zo 44143-1453 cony UM 4. Type Repair Alteration Unit Make Model Seas Number C III AIRFRAME (As deserted in /em I aborts) D O POWERPLANT 0 O PROPELLER O O APPLIANCE Two orandactwor 6. Conformity Stat mont A Agency, Name and Meese 8. K nd ciAgenCy Name Adam 355 Richmond Road CM Cleveland swh OH ao 44143-1453 cony USA 0 u.s.cerbothied Mechanic 0 Manufacturer O rotor cenacated Mechanic C Certificate No 0 Certificated Repair Sias CRS it 25NR6678 0 Cerbficatro Maintenance OrgaMarton D. I certify that the reps; andarx alteration made to the alga) Wearied in item 5 above and desabed on the reverse or attachments hereto have ban made in accordance will the requiononts of Part 43 Of the U.S. Federal Aviation Regratoris and that the rocernafion furniihed herein is true and anneals, the best of my knOwledge. Extended range fuel per 14 PROT869 Part 43 APP. 9 D Signature/ale Of Autry:aired Individual :117 12/29/2013 7. Approval for Return to Ice Pursuant Io the authority given persons specified below, the umt den IMO in Rem 5 was inspected in the manner prescribed by the Administrator of the Federal Matron AdmOisabOn and is el APPROVED 0 REJECTED BY FAA al StarKlards Inspector Department Manufacturer Mantenance Organization Person Approved by Canadian et Transport FM Designee InsPeCan Authorization Other Specfird Certificate a Deagnallon NO. CRS ft 25NR6678 SigruturelOate of Authorized IndiScar 12/29/2013 <9Z Cea ti ./. FAA Form 337 room .7 PROT598 EFTA_00242049 PROT224 PROT599 EFTA 00242050 PROT225 NOTICE Weight and balanCe or operating Limitation changes shah be entered in the apIxopliste aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements 8. Description of Work Accomplished flf more space is required. attach additional sheets Identify with aircraft nationality and registration mark and date work completed.) N493LX Nation** and Registration Mark 12/29/2013 Date TITLE: Aircraft Windshield Sealing Process Deviation: Mow Deviation from AMM 56-10-00-201 for the sealing of the aircraft windshield process. Temporary fasteners are not necessary during the sealing of the windshield. Original 8 typical bolts for installation may be used during the process, to keep retainers and shims in place during the entire sealing & installation of the windshield. After proper sealing time had elapsed. torqued bolts for installation of windshield per AMM. See attached FAA Form 8110-3 Signed By DERT-410115-CE Paul Hedding. Dated June 12, 2013 using Nextant Aerospace Engineering Order 1257, Rev. A, Dated May 21, 2013 for details. ICA Weight change is Negligible. Continue with Beechjet 400/400A Maintenance Manual Inspection Procedures. End FAA Form 337 gots) PROT600 EFTA 0024205I PROT226 PROT601 EFTA 00242052 PROT227 O.S. DEPARTMENT Of TRANSPORTATION I. DATE June 12, 2013 2. MAKE Corporation 3. MODEL NO. 400A 4 TYPE (Amok Ear.. Axe*. etc) Aircraft Richmond Heights, Ohio LIST OF DATA JJAENTIFICATION 7. TITLE EC) 1257 Rev. A May 21, 2013 Aircraft Windshield Sealing Process Deviation. Notes: 1) The structural aspects only of the above listed data are approved herein. This approval is only for the engineering data. It indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and subparagraph listed below as 'Applicable Requirements.' 2) This form constitutes FM approval of all the engineering data necessary for substantiation of compliance to necessary requirements for the entire repair. is PURPOSE OF DATA Engineering data in support of major repair to Hawker Beechcraft 400A, S/N RK-244. 9. APPVCABLE REOUIREMENTS (Lin specific sectOns) PROT870 Title 14 Part 25.301(25-23), 25.303[25.23), 25.305(a)(b)(c)(25-23), 25.307(a)(25-23), 25.601[25-00), 25.603(a)(b)(c)(25-38], 25.605(a)(25-00], 25.607(25-23), 25.609(a)(b)(25.00), 25.611(25-23), 25.613(a)(b)(c)(25- 00), 25.619[25.23), and 25.625(a)(b)(c)(25-23). 10. CERTIFICATION • Under audiority Pan Mt data listed above and On applicable requirements of the Airworthiness vested by direction of the Adrrireara1Or and in accordance with Ca ns and mnitalkns of ameontment ureter li PROT871 attached Vita numbened _DIA_ have been examined In accordance with estaUtshed procedures and found lo comfy with Standards Listed. approval of these data these data Recommend Approve II. SiGNATUREIS) OF DESIGNATED ENGINEERING REPRESENTATNE(S) 12. DESIGNATION NUMBERS(S) 13. CLASSIFICATIONISI tat Paul Hedding DERT-410115-CE Structures FAA Form 81104 (03-10) SUPERSEDES PREVIOUS Eamon Eft Number. H13357.01 Page 1 ell PROT602 EFTA 00242053 PROT228 PROT603 EFTA 00242054 PROT229 MAJOR REPAIR AND ALTERATION u.Sovaineereer Trangswien reeenceviatim Aik•Milstale. rorm Amami( cub NP. 2t204020 tioadeOf Electronic Tracking Number INSTRUCTIONS: Print or type all entries. See FAR 43.9. FAR 43 Appendix B. and AC 43.94 (or subsequent revision theme° for instructions and disposition or des Icon. This report is required bylaw (49 PROT872. 1421). Failure le MPW1can result m *chi Penal nee to raced 31.1:00 for each such violation (Section 901 Federal Awalkm Act 19513) I. Aircraft Nation:My and Registration Mark N493LX Serial No. RK 244 Make Model 400A Series 2. Owner Nome (As shown on registration cetldicate) Address (As shown an registration certificate) access 26160 Curtiss Might PKWY Ca Richmond Heights sw. OH zit 44103-1453 Corny OA 4. Type Repel( AllerabOn Veit make model Serial Number MI P. AIRFRAME (As descnted in Nem i above) 0 El POWERPLANT El O PROPELLER 0 MI APPLIANCE ace rem.rectme 6. Conformity Sul moot A. Agency. Name and Address B. K nd of Agency Nene Parma 355 Richmond Road Cm Cleveland sloe. OH Ze 44143-1453 Cowley USA 0 u S. Cenrcated Methane 0 Manufacturer 0 Foreign Gen/loved methane C Certificate No. 0 Cerlfcaied Repair &non CRS # 25NR667B 0 Cenificated Mai nienance Organize: on D. I certify that the repair anctioc al enition made to the unit(s) identified in sem 5 abort and deserted on the reverse or attachments hereto have been made in aCCOlanceml the requirements of Part 43 of the U.S Federal Aviat on Regtiat ons and nal me intonation furnished herein Is true and correct to the best of my kevAleace Edencled range fuel per 14 PROT873 Part 43 APP. B El Signahre/Dete of Authorized Individual 12292013 7. Approval for Return Service PuntuaM to the authorityOen persons speafied below. the unit identMed in item 5 was inspected n the manner presaged by the Administrator 04 the Federal Avutice Administration and is ®APPROVED 0 MUTE° BY FAA FPI Standards inspector Manufacturer Mantenance Organization DepartmeM ol Transport FAA Designee X ReaviSta50(1 Inspection Authorization Other (AMA') CertiScate or CRS IS 25NR6678 SigneturelDate of &Merited individual 2 ., 12/292013 CA.,44 FAA Form 337 Dam PROT604 EFTA_00242055 PROT230 PROT605 EFTA 00242056 PROT231 NOTICE Weight and balance or operating limitation changes shall be entered in the appropnate aircraft record. An alteration must be compatible with all previous alterations fo assure continued conformity with fhe applicable ainvorthiness requirements. Of more space is required. attach adotional sheets. Identify with aircraft nationahly and registrabbn mark and date work completed) N493LX 12/29/2013 Date Requested for use of new processes & materials for the removal and installation of Main & Side Windscreen, deviation from HBC AMM When performing the removal and installation of the windscreen and/or cockpit side windows, the following deviations from the HBC AMM are allowed & recommended: 1. During the removal & installation of the main windscreen, reference FO-AMMS document, chapter 56-10-01 for the main windscreen installation using AVDEC materials. This document correctly defines the processes and materials to be used for the removal and installation of the main windscreen. 2. During the removal and installation of the cockpit side windows, reference Flight Options FO-AMMS Document, chapter 56-10-10 & 56-10-11 for the replacement of the side window inner rubber gasket. This document correctly defines the processes and materials to be used for the replacement of the cockpit side windows inner rubber gasket. NOTE: TG8498 & HT3935-7 may not be used on exterior surfaces unless sealant is to be painted after curing for protection against UV light. PERMISSIBLE TO PAINT OUTER WINDSHIELD RETAINER WITH Chevron White JET GLO, CMOS70513 (Sherwin-Williams) This Alteration was FAA Approved by Paul Hedding FAA DERT-410115-CE using an FAA Form 8110-3 dated December 28, 2013. Using Nextant Aerospace Engineering Order 1303 Rev B Dated November 13, 2013 ICA Continue with Normal Hawker Beech Maintenance manual Inspection Requirements for this Area End FAA Form 337 (loos) PROT606 EFTA 00242057 PROT232 PROT607 EFTA_00242058 PROT233 FEDERAL AVIATION ADAtNISTRATION 1. DATE December 28. 2013 2 MAKE Corporation 3. MOOEL NO. 400A 4. TYPE (Mott EnPne. PrOPeag etc) Aircraft 5 NAME OF APPLICANT Richmond Heights. Ohio LIST OF DATA A IDENTIFICATION 7 IptE EO 1303 Rev. B November 13, 2013 Process & Material Deviation for the Removal and Installation of the Main & Side Windscreens. - Notes: 1) The structural aspects only of the above listed data are approved herein. This approval is only for the engineering data. It indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and subparagraph listed below as -Applicable Requirements! 2) This form constitutes FAA approval of all the engineering data necessary for substantiation of compliance to necessary requirements for the entire alteration. - 8. PURPOSE Of DATA: Engineering data in support of major alteration to Hawker Beechcraft 400A. SIN RK-244. 9. APPLICABLE REOUIREMENTS pal Wed& eneltens) PROT874 Title 14 Part 25.301(25-23), 25.303[25-23], 25.305(a)(b)(c)[25.231, 25.307(a)(25-23), 25.562(c)(25-23). 25.601[25-00), 25.603(aXb)(c)(25-38). 25.605(a)(25-00i, 25.607[25.23J, 25.609(a)(b)[25.00), 25.611[25.23]. 25.613(a)(b)(c)125-00), 25.619[25-24 25.625(a)(b)(c)(25.23), and 25.789[25-32). ID. CERTIFICATION • Under atilt.* Pad 183. dale Wed above and on optical)* requkernents of Ihe AinvortNneSS 0 Recommend vested by direction of the Administratex and in accordance vet conditions and linstabonis of appointinatt under 14 PROT875 attached sheets numbered NM have been examined in acwdance wIth ettabaShed ptocedwes and Sound to campy with Slandeds Oiled. approval of these data these data I Me) IlterefOre Approve It SIGNATURE(S) OF DESIGNATED ENGINEERING REPRE$ENTAT1VE(S) 12 DESIGNATION NUMBERS(S) 13. CLASSIFICATION(SI r -r--1 - Paul Redding DERT-410115-CE Structures FAA Form 81104 (03.10) SUPERSEDES PREVIOUS EDITION File Number 1113949-01 Page Tot I PROT608 EFTA_00242059 PROT234 PROT609 EFTA_00242060 PROT235 0 S eastanice Tarnorao, ask' enema amasineen Fan, Panned Os. No. 212oco2o i inor2C07 Etat:coca Tracking Number INSTRUCTIONS. Print or ape all entries. See FAR 43.9 FAR 43 Appendix B. and AC 4314 (or subsequent redskin thereof) for in true and ciatoskon a tit's form. This report is required by law (49 U S.C. 1421). Failure to report can rest on a Cava penatly rot to exceed 31.400 for each such nation (Section 901 Federal Analion Act 1958) I. Mrcraft Nationality and Registrant' Mack N493LX Siorial No. RK 244 Make Model 400A Sines 2. Owner mime (As show, or, regnittsensn cerbicaSit) Address (As shown on regisbation certificate) mans 26180 Curtiss Wright PKWY ely Richmond Heiohts Ps. OH zo 44143-145I carih. USA A Type 5. Unit identification Repair Altenatean Lint Matte Model Serial Number 0 lE) AIRFRAME (AS daunted In Sat f above) 0 O POWERPLANT 0 PROPELLER 0 APPLIANCE Type mentoant 5. Conformity Statement A. Agency's Nara and Address B. KIM of Agency we. Nextant Aerospace mom [ADDRESS REDACTED].1453 cony USA 0 V.S. Cedlliated Mechanic 0 !manufacturer O Foreign Cenocated Mechanic El cerusared Repair Sudan CRS # 25NR667B 0 Certificated maintenance oromirehon O. lanky that the Ma ander aeration made lo the itt(s) identified in nem 5 above and described on the reverse or attachrents hereto have been male in accordance with the rerrurrernent5 of Pan 43 of the U.S. Federal Aviaan RegutaNans and that the intamanon furnished herein is Ina and correct to the best of my knowledge. Enacted range fuel Per 14 PROT876 Part 43 App. El 0 SignatureiDate of Aul 11Oreer3 Inclrec j r.7 12/29/2013 7. APPrOval for Raunseervice Pursuant to the authOnly given persons petalled beast the unit Wen fled in item 5 was inspected in to manner prescribed by the Ackniriseettor dine Federal Aviation Arkninislealon and Is Egji APPROTED 0 REJECTED FAA FR Standards Inspecla Department ManufaCturer DetranAPPrOved by Canadian of Transport BY FAA Designee X Read Sueon Ogler (SPSalY) Inspection Attexcization conics°, Designated No. CRS St 25NR667B soneummeleorAumenzeo tnewsus a 74 12/29/2013 FAA Form 337 it ooN PROT610 EFTA 00242061 PROT236 PROT611 EFTA 00242062 PROT237 NOTICE Weight and belenCe a, operating limitation changes shall be entered in the aPPropriare aircraft record. An alteration must be compatible wrth all previous alterations to assure continued conformity with the applable airworthiness requirements. Of more space is required, attach additional sheets. Went,* with aircraft nationality and registration mark and date work completed) N493LX Title : Replace MD-302 with Round Style Standby Gauges 12/29/2013 Date Aircraft with MD302 digit SAM instruments must be reverted back to using round standby gauges until issues are resolved. Modified Instrument Panel (373.92.4110-14) to allow the installation of the original round standby gauges per drawing NX311-10007.03 Rev A Fabricated round indictor subpanel per drawing NX311-10007-01 Rev B Installed instruments into subpanel and install subpanel into main instrument panel per drawing NX311-10007. See Attached 8110-3 DERT 410115-CE Paul Redding dated November 8, 2013 per Nextant Aerospace EO 1543 Rev D dated October 23, 2013 End FAA Form 337 (loos) PROT612 EFTA_00242063 PROT238 PROT613 EFTA 00242064 PROT239 U.S. DEPARTMENT Of TRANSPORTATION FEDERAL AVIATION ADMINISTRAMON I. DATE November 8, 2013 2. MAKE Corporation 1 MODEL NO. 400A 4. TYPE (Ahvn& Engine. PropeNer. oft) Aircraft LIST OF DATA 7 TITLE EO 1543 Rev. D October 23, 2013 Replace MD-302 With Round Style aspects only engineering only with the Requirements." not constitute substantiation The electrical separate approval. Gauges. Notes: 1) The structural is only for the compliance below as "Applicable 2) This form does necessary for entire alteration. and require - of the above listed data are approved herein. This approval data. It indicates the data listed above demonstrates regulations specified by paragraph and subparagraph listed FAA approval of all the engineering data of compliance to necessary requirements for the requirements are not included in this approval 8. PURPOSE OF DATA: Engineering data in support of major alteration to Hawker Beechcraft 400A, SIN RK-244. 9 APPLICABLE REQUIREMENTS 0.1s1 specific sections) PROT877 Title 14 Part 25.301[25-23), 25.303[25-23], 25.305(a)(b)(c)[25.23J, 25.307(a)(25-23), 25.582(c)(25-23), 25.601[25-00), 25.603(a)(b)(c)[25-38), 25.605(a)125.00). 25.607[25-23], 25.609(a)(b)(25.00], 25.611[25-23], 25.613(a)(b)(c)(25-00), 25.619(25.23], 25.625(a)(b)(c)[25-23), and 25.789[25-32]. 10. CERTIFICATION - Under audio* vested by drec*cn d toe Adrrirestrator and in accordance rah cord:bans and imitator* of appointment ulcer 14 PROT878 Pan 183. data listed above and on attached sheets numbered Nth have been examined in accordance with eStatilithed prOCedunis and found to comply with applicable requirements of The airstetheinS Standards Listed. 0 Recommend approval of these data El Approve these data II. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESEWMTNE(S) 12 OESIGNATION NUMBERSIS) 13 CLASSIFICATIONS) ratVlae - Paul Hedding DERT-410115-CE Structures FM Form 8110-3 (0340) SUPERSEDES PREVIOUS EDITION File Number. H1351841 Page I off PROT614 EFTA_00242065 PROT240 PROT615 EFTA_00242066 PROT241 t il e/ MAJOR REPAIR AND ALTERATION u 5 zal.eit of (Airframe, Powerplant, Propeller, or Appliance) nssewwnston 0 eon, Munion ReninIstraisca 70nencennes Owe No Woman togas:col Electronk Tradurg Number INSTRUCTIONS: Print a type MI entries. See FAR 43.9, FAR 43Apperdix EL and AC 43.9.1 (cc subsequent revition thereonfor insIntiorn and d.sposnion of this tomm. Misreport is required by law fag PROT879. 1421). Pal...Nolo report can result in acres penalty not lo exceed S1.000 IN each such iolation (Section 901 Federal Ayiaton Act 1958) 1. Aircraft N4931.J( Serial No. RK 244 Make Model 400A Series 2. Owner Name (As sbonn on rep)stranion ca ticate) Address (As shown on resibearbn COROD/f0) ORDIRss 26180 Curtiss Wright PKWY eel Richmond Heights sale. OH to 44143-1453 Corso USA 4. Typo Repair Alteration UM Make Model Serial timber O El AIRFRAME (As (Jason:v.1m (tern I above) O D POWERPLANT I0 O PROPELLER O O APPLIANCE Type manutenurer 0 'Ord of Agency one Nerlant Aerospace Perin 355 Richmond Road car Cleveland sung. OH 20 44143-1453 CCouvry USA 0 U.S. tearless seeossne kends:lure/ 0 Foreign Cersccaied Mechanic I rtificate No. C. Certificate 0 Certificalpi Repair Station , rcRs# 0 Cerlikated Maintenance Organization 25NR667B 0. I certify that the repair vitior alteration made to me unit(s) klenbeed in deco 5 above and described on Me reverse or tot:tro/Ns here:o have Coen made in itC4:013r.00 with the requrnmonts of Parl 43 of the U.S. Federal Aviation Regulaoons and that the nfornEon furnished herein is true and correct to the DOD of my knowledge. Extended range fuel 14 CFRPart43 APP. Ill O Signaturethate ol Authorized Individual pp a ./C 12/29/2013 7. Approval for Ret Servl Pursuant ba the authority even persons specified belmv, the twit denbfied in hem Admiristrotor el the Federal Aviation Administration and is la APPROVED 5 was II inspected in the manner resorbed by the REJECTED FAA Fe Standards Inspector PAartultxture °enactment of Transport FM Designee X Repair Station ineeedionntenonzabon Other MOW Crick. or Desenabon No. CRS N 25NR667B $itrattestate of Authorized Individua2..7 x54_ i 9 12/29/2013 i A i FAA Form 337 (1046) SONY_GM_02755145 EFTA 110242067 PROT242 PROT616 EFTA 0024206% PROT243 NOTICE Weight and balance or operating limitation changes shah be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. (If more space is required, attach additional sheets, identify with aircraft nationality and registration math and dale work completed) N493LX Spoiler Linkage Closeout Modification 12/29/2013 Date Modified the Cockpit Floor Close out Panels Part Number: LH 45A30839.7 (Pilots) and Part Number: RH 45A30839-7 ( Co-Pilots) . Installed Nextant Aerospace Closeout Panel Part Number NX532- 1004-1 between these Panels to allow room for the New Throttle Quadrant to fit under the Center Pedestal This Alteration was FAA Approved by Paul Hedding FAA DERT-410114-CE using a FAA 8110-3 Dated December 28, 2013 using Nextant Aerospace Engineering Order 1563 Rev. 8 Dated December 24, 2013 ICA Continue with Normal Hawker Beech Maintenance Manual Inspection Requirements for this Area End FAA Form 337 time) PROT617 EFTA 00242069 PROT244 PROT618 EFTA [ADDRESS REDACTED]ATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS i. OATE December 28, 2013 2. MAKE Corporation 3. MODEL NO. 400A 4 TYPE (Arcralt Engine. Propeller. ek) Aircraft S. NAME OF APPLICANT Cleveland. Ohio LIST OF DATA 7 TITLE EO 1563 Rev. B December 24, 2013 Spoiteron Linkage Closeout Modification. END Notes: 1) The structural aspects only of the above listed data are approved is only for the engineering data. It indicates the data listed above compliance only with the regulations specified by paragraph below as 'Applicable Requirements." 2) This constitutes FM approval of all the engineering data substantiation of compliance to necessary requirements herein. This approval demonstrates and subparagraph listed necessary for for the entire alteration. a. PURPOSE OF DATA. Engineering data in support of major alteration to Hawker Beechcraft 400A, SIN RK-244. 9. APPLICABLE REQUIREMENTS (UM ipecac sections) PROT880 Title 14 Part 25.301[25-23]. 25.303[25-23), 25.305(a)(b)(c)[25-23). 25.307(a)[25-23), 25.601[25-00], 25.603(a)(b)(c)[25.38), 25.605(a)[25-00j, 25.607[25-23], 25.609(a)(b)[25-00), 25.611[25.23), 25.613(a)(b)(c)[25- 00]. 25.619[25-2n and 25.625(a)(b)(c)(25.23). 10 CERTIFICATION • Under authority Part 163, dela listed above and en ac liable requirements of We Airtatberess veiled by Brecon of Ire Adminielrefor and In accordance with cordnorts and Invlatons ot appointrnere under 14 PROT881 attached sheets numbered NIA have been inarnhed In accordance web established procethees and Mond to comely wan Standards Listed. approval of these data these data Recommend I (We) TherelOre C Approve I I. SiGNATUREIS) OF DESIGNATED ENGINEERING REPRESENTATNE(S) 12 DESIGNATION NUMBERS(S) 13. CLASSIFICATIONIS) 1.19. / - Paul Hedding DERT-410115-CE Structures FAA Form 81104 (03-10) SUPERSEDES PREVIOUS EDITION Fite Number 1413950.01 Papa 1 el I PROT619 EFTA_0024207 I PROT246 PROT620 EFTA_00242072 PROT247 S Dapaterital Of Ten/Plealeel News *sawn Adifttelleekte (Airframe, Powerplant, Propeller, or Appliance) rem Approroci OMB the 21204020 IfielY2C07 EtectraticTraclerg Ambit INSTRUCTIONS: Print Cr type all entries See FAR 43.9. FAR 43 Appendix 8. and AC 43 94 (or subsequent revson thereof) Ice indruCikass and disposition of (Ns !sm. This report is required by law (49 PROT882. 1421). Failure lo report can rcsub in a cvs penalty not to exceed 11.000 for each such violate:ft (section 901 Federal Reseal Act 1956) 1. Aircraft 2. Owner Nabonairy aid Registration Mark N493LX Serial No. RK 244 Make Name (AS sham on rag:oath:on certithafe) Model 400A Senn Address (As shown on rathafrabon carbficare) moths 26180 Curtiss Wright PKWY Cey Richmond Heights suit OH iv 44143-1453 co,riry USA 4. Type 5. Unll Identification Repair ',Aeration Una Make Model Serial Number AIRFRAME (As deserted in nem r above) POWERPLANT PROPELLER APPLIANCE thew manischew 6. Conformity Slat ment U.S. Celli tmed Mechanic 0 I Manufacturer mth. mo.th 355 Richmond Road 0 C. teacart No. cey Cleveland yr. OH St Certificated Repair Szabon zc 44143.1453 Cony USA 0 Certificated Maintenance Organizatice, CRS # 25NR6678 D. I ceney that the repair ardor alteration made to the uNt(s) iderilifed in den 5 above and devAbed on the revere. Cr allachmenls hereto have been made In accordance with the requirements of Part 43 of the U.S. Federal AMIN, Regulabors and that the thIcemalion Extended range fuel per 14 PROT883 Part 43 App.B Signature/Date of Asti:deed Indwidua ic; sI trrie, 12129/2013 Pursuant to the authority given peruse specified blow. the unit identSed in item 5 was Inspected in the mime( prescribed by the Administrator of the Federal Adaiken Administration and is 0 'AVOWED 0 REACTED 8Y FM FR Standards InspeClOr Manufacturer Department ci Transport FM Designee X Reps Station Inspect:an Aufitheization Other (SWAY) Certificate or Designation NO. CRS ft 25NR6678 FAA Form 337 BOOB Sign %regale &Authorized I nainsiagsp Anton J. Koptivnik 12/292013 SDNY_OM_02755151 EFTA_00242073 PROT248 PROT621 EFTA 00242074 PROT249 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to enure continued conformity with the applicable almortflineSa requirements- (If more space is requited, attach additional sheets. Identify with aircraft nationality and registration mark and dale work completed.) N493LX Nextant Aerospace Carried out a Repair to the Horizontal Stabilizer Ribs 12/29/2013 Using Nextant Aerospace Kit Part Number NXK-128-6200 Rev B. Dated July16. 2012. The following Ribs were replaced. NXR-45A21112-007 NXR-45A21113-007 NXR-45A21101.021 NXI1-45A21116-007 NXR-45A21117-007 Rib - H Stab Cant STA 13.779. Rib - H Stab Cant STA 29.921. Rib - H Stab Cant STA 46.063. Rib - H Stab Cant STA 62.205 Rib - H Stab Cant STA 78.346 The following Ribs were not Replaced as there was not Damaged. NXR128-620020-001 NXR128.620020.002 Date This Kit was FAA Approved by Paul Hedding DER-T 410115-CE Structures on an FAA 8110-3. Dated June 12, 2013. Using Nextant Aerospace Engineering Drawing NXR-128-6200 Rev B Dated July 16.2012 END K Additional Sheets Ate Attached FAA Form 337 ham PROT622 EFTA 00242075 PROT250 PROT623 EFTA 00242076 PROT251 U S. DEPARTMENT OF TRANSPORTATION 1. DATE June 12, 2013 2. MAKE Corporation 3 MODEL NO 400A 4. TYPE (alectalt. Enprna Propene,. etc) Aircraft S. NAME OF APPLICANT Richmond Heights, Ohio LIST OF DATA 8 IDENTIFICATION 7. TITLE NXR-128-6200 Rev. B July 18, 2012 NXR-45A21112-007 Rev. C July 13, 2012 NXR-45A21113.007 Rev. B July 13, 2012 NXR-45A21114-007 Rev. El July 13. 2012 NXR-45A21115-007 Rev. C July 13, 2012 NXR-45A21101-021 Rev. A July 19, 2012 NXR-45A21116-007 Rev. B July 13.2012 NXR-45A21117-007 Rev. B July 13. 2012 Kit - Horizontal Stabilizer Rib Replacement Installation Instmclions. Rib - H Stab Cant STA 13.779. Rib - H Stab Cant STA 29.921. Rib - H Stab Cant STA 46.063. Rib - H Stab Cant STA 46.063. Rib Assy - H Stab Cant STA 46.083. Rib - H Stab Cant STA 62.205. Rib - H Stab Cant STA 78.348. a. PURPOSE OF OATA. Engineering data to support repair procedure for Horizontal Stabilizer PIN 45A21002.0121 on Hawker Beechcraft 400A SIN RK-244. 9. APPLICABLE REQUIREMENTS Oast specific seams) PROT884 Title 14 Part 25.301[25-231, 25.303[25-23I, 25.305(a)(bftc)[25-23), 25.307(a)(25.23J, 25.601[25-00]. 25.603(a)(bftc1125-381, 25.605(a)(25-00), 25.607[25-2n 25.609(a)(bft25-00], 25.611[25-23], 25.613(a)(b)(c)(25- 00], 25.619(25-23J, and 25.625(a)(b)(c)(25-231. I0. CERTIFICATION - Under authority Pen in data seed above and on apPlicable requirements of the Favronaineas veiled by &ec%on or tie Admire:W*1er and in at-cadence watt ccadltions and liermatons of appointment unoer 14 PROT885 attached sheets marcane 2_ have been examined in accordance YAM estaNished prorAdures and found to comply rah Standards Listed. approval of dine data these data Recommend E Approve I I. SIGNATLIRE($) OF OESIGNATED ENGINEERING REPRESENTATNE(S) 12. OESIGNATION NUMBERS(S) 13. CIASSIFICATION(S) teacP4L Paul Redding DERT-410115-CE Structures FAA Form 8110-3 (OS WI SUPERSEDES PREVIOUS EDITION Fie /lumber H13370.01 Page 1 of 2 PROT624 EFTA_00242077 PROT252 PROT625 EFTA 00242078 PROT253 FEDERAL AVIATION AOMNiSTRATION 1. 0.47E June 12, 2013 2 MAKE Corporation 3. MOOEL NO. 4OOA 4. TYPE (Aerie. Engine. Propeller. efc.) Aircraft S. NAME OF APPLICANT Richmond Heights. Ohio LIST OF DATA 7 TM E END Notes: 1) The structural aspects only of the above listed data are approved herein. This approval is only for the engineering data. It indicates the data listed above demonstrates compliance only with the regulations specified by paragraph and subparagraph listed below as 'Applicable Requirements.' 2) This form constitutes FAA approval of all the engineering data necessary for substantiation of compliance to necessary requirements for the entire repair. e. PURPOSE OF DATA. Engineering data to support repair procedure for Horizontal Stabilizer PIN 45A21002-0121 on Hawker Beechcraft 400A, S/N RK-244. 9. APPLICABLE REQUIREMENTS (list swank sectOns) PROT886 Title 14 Part 25.301[25-23), 25.303)25-23], 25.305(a)(bftc))25-23], 25.307(a)[25-231, 25.601[25-00], 25.603(a)(b)(c)[25-38], 25.605(a)(25-00), 25.607[25.23], 25.609(a)(b)[25-00]. 25.611[25-23], 25.613(a)(b)(c)(25- 00), 25.619[25-23], and 25.625(a)(bftc)(25-23). 10. CERTIFICATION • Under autftnly Pad 113, data wed above and on applicable requirements 04 the Avwxtnaress vested by eirecdee ca the Administrator and in accordance with conditions and smarms of appetranwnt under la PROT887 attached sheets numbered _z_ have been Ozirrined 01 ac dance with eStatiithed protectors and round to corn* v401 Standards limes approval of these data these data Recommend 0 Approve II SIGNATURE($) OF DESIGNATED ENGINEERING REPRESENTADVE(S) 12. DESIGNATION NVIABERS(S) 13 ClASSIFICATION(S) ' If-V.9-- Paul Hedding DERT-410115-CE Structures FM Form 131104 (03-10) SUPERSEDES PREVIOUS EornoN Hie Winter. H13370.01 Page 2 of 2 PROT626 EFTA_00242079 PROT254 PROT627 EFTA 00242080 PROT255 0 3 1 9.5 Omannwor a tam Apremea OM No.21204020 ii/30rXIM Electronic Tracklna Matter trinsemiem Federflerliefra• Afinktiereke INSTRUCTIONS: Print:4'09e all fl ier Set FAR 43.9, FAR 42 Appendix B, and AC 43.9.1 (cc subsequent revision thereof) for Inatnxborts and Oepoelon of Das Wm. This report is rewire] by law (49 PROT888. 1421). Failure to sport can result In crinl penalty not to exceed V .000 b each such rialtos (Section 901 Federal Aviation AMISS") 1. Aircraft Natkonality and Reg:snow Mark f4493LX Serial No. RK244 Make Model 400A Series 2. Owns NOT* (As Mown on inarabon mace*, Flight Options, LI: Address (AS Siam on registration Migrate) Arness26180 Curtiss Wrioht PINNY enRichrnond Heights stat42997 ip44143-1453 ediar04118 3. For FAA Use Orly 4. Type Repair Alteration Um, mese model Serial Number El .4 AIRFRAME (As deserted in hem t atom) 0 O POWERPLANT 0 PROPELLER II APPLIANCE Type sorwtariurer 6. Conformity Statement k Agency's Name and Address B. K rd OlAgenCY Har•Constant Aviation 0 U.S. cenecateo mechanic 0 MwiAacturer reeys[ADDRESS REDACTED] 0 C. Cortical', No. core Invelancl sweOhio SI centr•catee Repair Station CRSINVC7R346J se[ADDRESS REDACTED]ate; 0 Certificated uweeseanse Organization 0. I certify that me repair arclior alteration made to the urt4(s) identified in e.ern 3 above and described on the reverie et attachments hereto have been nude in accordance win the requiem/nu. ci Pan 43 ol the U S Federal Aviation Reptilian and that the informalfurnished herein is true and correct to the best 01 my knowiedge. Extended raro$ NM per 14 PROT889 Pert 47 APO. B Sitnalurt(Dala Authorized Individual Date: December 30. 2013 7.47ro ,tum to Service Putsuam to me aulhomy even persons speared below. the und ideOb CO in dent AdelettfelOt of the FederalAnal= Adrrirestralion and is 0 APPROWD 5 was U inspected is the manner prescribed by the REACTED FM Fe Standards IASOCCIOI folaftleICIOref Departnent ci TrustBY FM Designee Inspection Authonzatron Ogler (spear) Ceillkele Of Desgriabon No CRSFANC7R346J SiOntlfUfel0 or A Inc r. Date: December 30. 2013 4: `9 / efla----- FAA Form 337 tuna) PROT628 EFTA_0024208 I PROT256 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alterabbn must be compatible with all previous alterations to assure continued conformity with the Baehr...able airworthiness RIQUIRNNINNS. (f more space is required, attach additional sheets. Identify with aimmft nano:teary and registration mark and date work completed) N493LX 12/30/2013 Date ACCOMPLISHED INTERIOR REFURBISHMENT/MODIFICATION AND 3 PLACE DIVAN INSTALLATION THE FOLLOWING AIRCRAFT INTERIOR ITEMS HAVE BEEN REFURBISHED' Repainted. recovered control °Arms MA Matte Black Leather Accordance wish Beath« 400A MIM 207040.701. 25-00-C43-001 Removed and Retraced Glare shied and Eyebrow panel materiel with Matte Black Leather ri Accordance with Beeehjet 400A Mid 204041201 Removed and Rep:aced COPPS Sidewell material with Matte Meta Leather m Accordance with Beecher 400A MAI 216100.201 Removed and replaced Pilot Seal Pan Number TABH100P1.40001 Serial Number 62. Foam and recovered with Garrett Shrepskn Oak and Excel Cappuccino Lanier. Removed and replaced Co -Pilot Seal Pan Number TABH100CM00-01 Serial Number 246. Foam and recovered with Garrett Sheepskin Oak and Excel Cappuccino Leallier. Removed and Ref/Laced Left Hard II Passenger Seal Part Number 2524.014(-530A) Serial Number 9907114 Foam and recovered with Towncend Leather (Heritage Brown) Removed and replaced Right Hard re5 Passenger Seal Pan Number 252443148130W Serial Number 990426-7 Foam and recovered with Townsend Lealner(ientape Brown) Removed and Replaced left Hard /A5 Passenger Seat Pan Number 2524-0i4(53CE)Senal Number 03%18-5 Foam and recovered with Townsend Leather (Flerrage &trim) Removed and replaced R.ghl Hand #7 Passenger Seat Part Number 2524.014(530A) Serial Number 030706.2 Rani and recovered weth Townsend Leather (Henlage &own) THE FOLLOWING MANUALS AND APPROVED DATA HAVE BEEN UTILIZED FOR BASIS OF REFURBISHMENT Skandia Flammabaty Test S254978 as approved by FM DER Jane Biterssein (DERY 532780-CE) on FM form 8110-3 dated 4/23/2013 Flame Out Flammability Test 4311 as approved by FM DER Herb Reed II (DERT-230293GE) on FM Form 8110.3 dared 12)2312013 Skandia FlarnmahPlY Test Report TP 22681 Rev A as approved by FM OER Jane Biberstein( DERV-032780-CE) on FM Form 81101 dated 05/022013. Thee Place Divan insueltabos Installed (3) Papa delan pan Number 32-0396(ASOPT)T123 KO2 SM 003702 In Accordance vote Aviation rabncaton STC# 5701572Mo/id Skandia Frannie/my teal report 5254978 per Jane Biterstein FM DER (DERV-832760CE) dated 4r23-2013 THE FOLLOWING INTERIOR I uts HAVE BEEN MODIFIED UR Gaily Any. Ml Galley Any. Divan Any. 1M Galley Ash and InsINI per Delta G drawing OGD-CA01.101 Rev 0. 060-CA01-101 CO E-I. UK Gale)/ Install DGD-CA01-501 Rev LO A-1. OGO-CA01-501 Rev IR as approved on FM Ohm 8110-3 per FM DER Donald Glesple (DERT•T50135SW) dated Minh 25 2013 Ml Casey Assy and Instal per Della G drawings 000-CA02-10i Rev B. OGD-CA02-501 Rev IR as approved on FM tam 81104 by FM DER Donald Galion (DERT.750155•SW) Mad March 25, 2013. Divan Any pet Della G drawings OGITCA09-10I Rev C and DGD-CA09-101 ED 0-1 as approved on FM town 5110.3 per PM DER Donald Gas» (DERT 750135•SW) dated Mardi 25, 2013. Benner KB Sidewal any drawing 25510038 Rev C. Benner Sidetedge any draWng 2592-0002 Rev C. Banner Kit Foldout Table any drawings 2553-0041 Rev C and 25510040 Rev B. Bonner /CT liner K4 Ina drawing 2553.0037 Rev C as approved on FM kern 81113 per Stephen Kenna DERT-230238-CE dated Dec 28. 2013 INSTRUCTIONS FOR CONTINUEDAIRWORTHINESS' THE REMOVAL OF THE INTERIOR IS ON THE CONDITION OF FAILURE THERE ARE NO ADDITIONAL INSPECTIONS REQUIRED. CONTINUE TO INSPECT WW MANUFACTURERS ANAL SRM. OR CAVA AS APPLICABLE AIRCRAFT EOUa4ENT LIST AND WEIGHT AND BALANCE WERE UPDATED 8Y THE CUSTOMER -END- O Additional Sheets Are Attached FM Form 337 (1006) PROT629 EFTA 00242082 PROT257 U S. DEPARTMENT OF TRANSPORTATION STATEMENT OF COMPLIANCE WIlli THE FEDERAL AVIATION REGULATIONS DATE Dee 26, 2013 MAKE Beechcrali Corporation MODEL 400A TYPE (Airplane. Ratio. Ile)leopyr. etc) AIRPLANE NAME OF APPLICANT NEXTANT Aerospace Cleveland OH. LIST OF DATA IDENTIFICAITON TITLE REPORT: BEECHJ ET 400A INTERIOR STRUCTURAL SUBSTANTIATION BEECHJET 400A XTI LINER KIT INSTL. Beech jet 400A, Aircraft Serial No. RK-244 Certification Bases for this aircraft modification is per Type Certificate Number A I6SW Revision 28 dated April 12,2013 RKG3282 Rev. IR, 8-28.2013 2553-0037 Rev C, dated 8.30.2013 PURPOSE OF DATA DESCRIBE AND SHOW VERIFICATIONS FOR NEXTANT INTERIOR INSTALLATION ON BEECHJET 400A, AIRCRAFT SERIAL NO. RK-244 APPLICABLE REQUIREMENTS ( bit specific section.p) 14 PROT890 Pan 25 §.301, 303, 305, 307a), 365, 561, 571, 601, 603, 605, 609, 613 CERTIFICATION - Under authority of appointment under Pan 183 oldie have been vesled by direction of the Administrator and in accordance with conditions rodent' Aviation Regulations, data listed above and on attached sheets examined in accordance with established procedures and found to con* Regulations. approval of these data Approve these data and limitation numbered with applicable requirements of ihe Federal Aviation I (PK) Therefore 0 Recommend SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) Stephen Farness DERT-230238-CE STRUCTURES AND DAMAGE TO FAA Farm 8110-3 in.zl surnsrm.s ptivicos minow GPO 901 PROT630 EFTA_00242083 PROT258 PROT631 EFTA 00242084 PROT259 LYE products engineering services. inc. 2946 S. Hvd rook Wilita, Kansas 67216 TI: 316.524.4466 FAX: 316.524 4455 STRUCTURAL ANALYSIS REPORT Forward Calley Cabinet Modifications - Beechcraft Model 400A, RK-244 & RK-305 Document No: 313-ST-001 Revision IR PREPARED BY: Robert F. Clossin Date: December 24, 2013 APPROVED BY: APPROVED BY: Chris Cocklin Robert F. Clossin Manager - Design Engineering President THIS DOCUMENT CONTAINS INFORMATION OF A PROPRIETARY NATURE AND SHALL NOT BE TRANSMITTED, REVEALED, OR DISCLOSED TO ANYONE WITHOUT THE EXPRESS WRITTEN PERMISSION OF LEE PRODUCTS ENGINEERING SERVICES, INC. ADDITIONALLY, USE OF THE INFORMATION IS PROHIBITED EXCEPT WHEN EXPRESSLY AUTHORIZED BY LEE PRODUCTS ENGINEERING SERVICES, INC. PROT632 EFTA 00242085 PROT260 Lee Products Engineering Services, Inc. STPIICTUPAI ANAI YSIS REPORT 313-ST-001 REV. IR PAr;F ii REVISION RECORD Revision Date Description Approval IR 12/24/13 Initial Release See Cover Sheet PROT633 EFTA 00242086 PROT261 313-ST-001 REV. IR PAGE iii 1. INTRODUCTION 1 2. REFERENCES 2 2.1 CONSTANT AVIATION DRAWINGS 2 2.2 APPLICABLE SUPPLIER DRAWINGS (AVIATION FABRICATORS) 2 2.3 APPLICABLE LPESI REPORTS 2 2.4 APPLICABLE GOVERNMENT DOCUMENTS 2 3. CERTIFICATION BASIS 2 4. DESCRIPTION 3 4.1 GENERAL 3 4.2 RH FORWARD GALLEY ASSY & INSTL 3 4.3 RH FORWARD DIVAN MODIFICATION 4 4.4 LH FORWARD GALLEY ASSY & INSTL 5 4.5 LH AFT LAVATORY EXTENSION 7 5. STRUCTURAL SUBSTANTIATION 7 5.1 LH FORWARD GALLEY ASSY & INSTL 7 6. CONCLUSION 8 APPENDIX A A.1 PROT634 EFTA 00242087 PROT262 313-5T-001 REV. IR PAGE 1 1. INTRODUCTION The purpose of this report is to demonstrate the structural substantiation to applicable 14 PROT891 Part 25 regulations as they relate to the installation and modification of various interior cabinets on Beechcraft Model 400A, S/N's RK- 244 and RK-305, for a FM Form 337 major alteration, performed by Constant Aviation at their Cleveland, OH facility. The installations consist of the replacement of new RH and LH forward galleys, and modification to the existing closet frame, an extension of the aft lavatory, and a modification to the side-facing divan with the manufacturer's approval. Everything except the new LH forward galley has been accomplished on a previous modification as documented in LPESI Report 222-5T-001. Therefore, only the new galley will be discussed and analyzed in this report. The floorplan for the two (2) Beechcraft Model 400A aircraft is as shown below. Figure 1-1 - Floorplan PROT635 EFTA_00242088 PROT263 313-ST-001 REV. IR PAGE 2 I 11 2. REFERENCES 2.1 Constant Aviation Drawings Drawing No. Rev. Title NXT0213-01 IR LH Galley Assembly NXT0213-02 IR LH Galley Installation NXT0213-05 IR Weight Placard Installation NXT0313-01 IR RH Galley Assembly NXT0313-02 IR RH Galley Installation NXT0313-03 IR Divan Assembly NXT0313-07 IR 4" Lay Ext 2.2 Applicable Supplier Drawings (Aviation Fabricators) Drawing Ni. Rev. 1 Title D-10666 A 3 Place Divan Installation (STC ST01572WI) 2.3 Applicable LPESI Reports Drawic•ig 14.1). . . ilvi 4 Title 222-ST-001 B Miscellaneous Cabinet Modifications - Beechcraft Model 400A 2.4 Applicable Government Documents Dotu nit Document ?Re'i::: ; TitIO, 14 PROT892 Part 25 See Sect. 3 Airworthiness Standards: Transport Category Airplanes ANM-115-09-017 1/28/10 Interaction of Interior Structures, Including Seats 3. CERTIFICATION BASIS The Beechcraft Model 400A certification basis is defined Type Certificate Data Sheet (TCDS) Al6SW, Rev. 28, the Certification Basis is 14 PROT893 Part 25 dated February 1, 1965, including Amendments 25-1 through 25-40. The individual 14 PROT894 Part 25 subparagraphs that will be discussed herein are: 25.301(a)(b)(c) 25.303 25.305(a)(b) 25.307(a) Loads (Amdt. 25-23) Factors of Safety (Amdt. 25-23) Strength and Deformation (25-23) Proof of Structure (Amdt. 25-23) PROT636 EFTA 00242089 PROT264 25.341(c) 25.561(a)(b)(c) 25.601 25.603(a)(b) 25.605 25.607(a)(b) 25.609(a)(b) 25.613(a-e) 25.625(a)(b)(c) 25.787(a)(b) 25.789 4. DESCRIPTION 313-ST-001 REV. IR PAGE 3 Gust Loads (No Amdt.) Emergency Landing Loads - General (Amdt 25-23) Design and Construction - General (No Amdt.) Materials and Workmanship (Amdt. 25-38) Fabrication Methods (No Amdt.) Fasteners (Amdt. 25-23) Protection of Structure (No Amdt.) Materials Strength Properties ... (No Amdt.) Fitting Factors (Amdt. 25-23) Stowage Compartments (Amdt. 25-38) Retention of Items of Mass ... (Amdt. 25-32) 4.1 General The modification of the Model 400A aircraft consists of replacing the existing RH and LH forward cabinets with new assemblies, modifying the RH forward 3- place side-facing divan by refurbing the divan, and modifying the existing LH aft lavatory cabinet by extending its cabinet structure to close out the area around it. All but the new LH galley are previously installed and certified on previous 400A aircraft, and analyzed in LPESI Report 222-ST-001. 4.2 RH Forward Galley Assy & Instl The NXT0313-01 RH forward galley assembly (installed per NXT0313-02) is the same as that previously installed on other Model 400A aircraft. An illustration of the galley in Figure 4-1. PROT637 EFTA 00242090 PROT265 313-ST-001 REV. IR PAGE 4 Figure 4-1 - RH Forward GalleyAssy (Contact Pad on Upper Area Not Shown) The galley is manufactured from strong lightweight 0.50-inch thick ATR-FP- 501F2 Nomex/fiberglass composite panels from AAR Composites, and fabricated using ATR panel pin construction. The RH forward galley is installed between the existing RH forward structural partition (which separates the flight deck with the cabin) forward of it and the 3-place side-facing divan immediately aft of it. The lower wider section of the cabinet also encloses the aircraft's air conditioning evaporator mounted separately to the floor structure underneath. 4.3 RH Forward Divan Modification The NXT0313-03 3-place side-facing divan assembly consists of new drawer and fascia door panels onto the existing structural divan frame (Aviation Fabricators D-10666 STC'd Installation Kit - STC ST01572W1). It has also been installed in previous Model 400A aircraft, and analyzed in LPESI Report 222-ST-001. An illustration of the divan assembly is provided in Figure 4-2. PROT638 EFTA_00242091 PROT266 313-5T-001 REV. IR PAGE 5 Figure 4-2 - RH Forward Divan Mod The divan closeout panels are manufactured from strong lightweight 0.50- inch thick ATR-FP-501F2 Nomex/fiberglass composite panels from MR Composites, and fabricated using ATR panel pin construction. The STC'd divan frame installation consists of a structural frame (bottom only - no seat backs, cushions form the divan backs), restraint systems consisting of lap belts and shoulder harnesses for all three (3) seated positions, and a D-106699 floorboard modification installation underneath the divan. The frame installed in eight (8) places into the existing cabinet "Brownline" seat track extrusions (inboard and outboard). 4.4 LH Forward Galley Assy & instl The NXT0213-01 LH forward galley assembly is a traditional aircraft galley and is located between the flight deck and the entry door, directly aft of the existing LH forward structural partition (bulkhead). The new galley replaces an existing galley of similar design and the same size. In fact, this new galley assembly is the same as previously installed in other Model 400A aircraft, and analyzed in LPESI Report 222-ST-001, except for a minor change to the upper forward portion of the cabinet. As can be seen in a comparison of the galley illustrations below and Fig. 4-3 of 222-ST- 001, the change consists of eliminating the small recessed condiment tray drawer and extending (down) the existing compartment to compensate. The galley is manufactured from strong lightweight 0.50-inch thick ATR-FP- 501F2 Nomex/fiberglass composite panels from AAR Composites, and fabricated using ATR panel pin construction. An illustration of the LH forward galley is provided in Figure 4-3. PROT639 EFTA_00242092 PROT267 Figure 4-3 - LH Forward Galley Assy 313-ST-001 REV. IR PAGE 6 The LH forward galley is installed per NXT0213-02 and is installed utilizing the same existing installation attachments - five (5) screw/insert attachments into the existing partition and four (4) floor attachments (2 into the existing seat track and 2 into existing floorboard mounts, and is the same as the previous NXT0313-05 installation analyzed in LPESI Report 222-ST-001. The empty cabinet weights 86.15 pounds (less than the 90.61 pound galley analyzed in LPESI Report 222-ST-001) and the total placarded content weight (Ref. NXT0213-05) of 141.0 pounds (only 1.0 pound more than the 222-ST-001 analyzed galley). Therefore, the total installation weight of the NXT0213-02 galley is 3.46 pounds lighter than that analyzed in LPESI Report 222-ST-001, and is therefore structurally substantiated by comparison. PROT640 EFTA_00242093 PROT268 313-ST-001 REV. IR PAGE 7 4.5 LH Aft Lavatory Extension The NXT0313-07 LH aft lavatory modification consists of augmenting the toilet cabinet with new panels and compartments between the existing cabinet and the RH aft partition. An illustration of the modification to the aft lavatory is shown in Figure 4-4 (new components in gray). Figure 4-4 - LH Aft Lavatory Extension This is the same as previously analyzed in LPESI Report 222-ST-001. 5. STRUCTURAL SUBSTANTIATION The structural analysis will be generated using traditional means based on conservative assumptions. In determining the Margin of Safety (MS), the resulting analytical result will be subtracted from 1.0 so that any MS greater than 0.0 is considered a positive margin. Also, MS's greater than 3.0 will be listed as "+Ample". 5.1 LH Forward Galley Assy & Intl The critical loadings for the LH forward galley are the 9.0g forward and 3.5g side load conditions. However, since the new galley weighs 3.5 pounds less than the previously analyzed galley, is of similar shape and design, includes that same installed equipment, and utilizing the same aircraft attachment points, the new galley assembly and installation is therefore structural substantiated by comparison. PROT641 EFTA_00242094 PROT269 313-ST-001 REV. IR PAGE 8 The largest placarded drawer is the top, center drawer in the lower section of the galley, which is placarded for 45.0 pounds. The drawer is restrained by a standard Actron paddle latch, P/N A23511-1S. The applied load to the latch is (the drawer itself + hardware is 5.0 pounds): Applied Load = (5.0 lbs + 45.0 Ibs) x 3.5g x 1.15ff = 201.3 pounds The minimum load rating for the A23511 paddle latch by its manufacturer is 225.0 pounds. The resulting margin of safety is: M.S. = 225.0 Ibs / 201.3 Ibs) - 1.0 = +0.12 6. CONCLUSION Based on the above structural analysis, the new cabinets and modification and their installations, listed in Sect. 2.1, into the aircraft have been shown to be compliant with the applicable 14 PROT895 Part 25 regulations, as defined in Sect. 3 with positive margins of safety. PROT642 EFTA_00242095 PROT270 APPENDIX A 313-ST-001 REV. IR PAGE A.1 O el olwratuttre L I N 0 n h e i - 'I ivqg I 1 2 O hh t II I lit AEI y4yto 5 I I N 4- n I O PROT643 EFTA_00242096 PROT271 U. S. DEPARTMENT OF TRANSPORTATION - MATE 412312013 2.MAKE Raytheon 3.MODEL NO. 400A 4,TTPEMITFIme. Ent** PeOptite. NO Airplane SRAM 0F APPLICANT Constant Aviation-CLM LIST Or DATA 6 IDENTIFICATION - tint E Design Data S254976 Rev NC Skandia, Inc. Flammability Test desalts Bunsen Burner Testing Test Specimen P/N's Cont 25 (represents main entry door trim) 27 (represents upper med surround) 28 (represents lower med, lowerMed surround, lh aft blIchcl) 29 (represents pax seat back shrouds, arms, crash pad) 30 (representsseat shrouds) 31 (represents entry Steps, cockpit ped step) 33 (represents cntri coiumn boots, rudder boots) 34 (regreSentsckpt defog Vent closeout) 35 (represents table shrouds) 36 (represents dada and street' closeout) 39 (represents crew seats) Notes: 1) Work accomplished under Skandia Inc. WO *254976-13, Ref Document ID 93650. 2) flammability lestwitnessing only, does not constitute installation approval of materials. 3) IAW Skandia Flammability Streamline Testing Test Plan 21306, Rev IR, Dated 11(03111 Page 2 8,PURPOSE OF DATA Demonstration of compliance with material flammability regtilrements for S/N TUC-244 gAPPLICPtSLE REQUIREMENTS (List sP44lEctleettbm) 14 PROT896 Part 25:853 (e) Arndt 25416 Appendix F Pant MO) Arndt 25.111 14 PROT897 P0425.853 (a) Amdt 25.116 AppeDda F Pan I (p)(1Xii) 14 PROT898 Part 25.855 (d).Amdt 25.116 Appendbc F Pert I (6) 1 °CERTIFICATION.- Under authority veiled by direction of the of appointment under 14 PROT899 Part 153, data listed above and examined in accordance with established probedures endfound Standards listed. O Recommend approval of these data (Approve these data Administratorand In accordance withikondkiona and limitations on attached sheets numbered i - ..)-have been to comply with applicable requirements of the Airworthiness 11.SIONATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE NUMBER(S) ia.GLASSIFICATION(S) (:V V1Q /lt) . (_50a0,2,119±14A - Jane Bibers in -FM DER DERY-032780-CE' Structural Special FAA Form 8110-3 (0M0)SUPERSEDES PREVIOUS EDITION PROT644 EFTA_00242097 PROT272 PROT645 EFTA _00242098 PROT273 3OLG-CON)3231)____ US. DEPARTMENT OF TRANSPORTAtiON FEDERAL AVIATION AOMMISTRATON 1. DATE March 25, 2013 AWCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2. MAKE Beechlet 3 MODEL NO. 400A t TYPE peipieni I. Reek N06:teree eft) AIRPLANE 6. NAME OF APPLICANT UST OF DATA e IDEISTINCATION 7 TILE Document No. DGD-CA08-501 REV: IR Dated: 8/13/12 DOD-CAN-101 REV; C Dated: 1125113 OGD-CA09-101 EO: 0-1 Dated: 2/28/13 CIGD-CA13-101 REV: IR Dated: 2/28/13 DGD-CA14-101 REV: IR Dated: 1131113 ARMREST RI-I INSTL DIVAN ASSY DIVAN ASSY CARD TABLE ASSY LAV CLOSET FRAME ---------• End of Data NOTES' MOD is for Beechlet model 400A (Nextant 400XT variant) S/N RK-244 only. Is for the structural design aspects only on the above listed data and an Installation approval. only for regulations specified In the "Applicable Requirements" block. with additional regulations not listed herein may be required. This form FAA approval of all engineering design data for the entire Additional 8110-3 approvals may be necessary for Damage Tolerance, Mechanical Systems, Electrical, Weight & Balance, as well as other basis, refer to TC data sheet No. A16SW Approvals are provided separately. 1. This approval 2. This approval does not constitute 3. Approval Is Compliance does not constitute alteration. Flammability, disciplines. 4. For certification 5. Structural 5. PURPOSE OF DATA To provide type data fo FAA approval of structure In support of a return to service on SIN RK-244. This approval Is for design data only on a major alteration and is not an Installation approval. 9. APPI.CAME REQUIREMENTS (Ust specific &soon) 14 PROT900 Part 25.601 Arndt 25-0, 23.60300(b). Amdt 25-3S, 25.605 Arndt 25-0, 25.609 Arndt 25-0,25.611, Arndt 25-23,25.613 (eXti)(r) Arndt 25-0, 25.619 Arndt 25-23, 25.625 Arndt 25-23, 25.785 000/XeXdXIXO Moth 25-32, 25,789 Amdt 25-32 10. CERTIFICATION - Under authOrIty Rai 163. data )sled above and rah epplcabk rearmaments of are 0 Recommend vested by Orectren of the Aeminisveicir one in eccordenCe meth condition and limitations cl apoantment tinder 14 PROT901 on aached sheets membered NM have been examined In accordant* WO astable/led procedure: and found M Camay AiwOrthlresa Starderds La: d. *Won, IR 1"16 data these data I NAM Therettve CI Approve II SIGTUREISI OF DESIGNATED ENGINEERING REPRESENTATIVE($) 12. EM-DONATIDel NUUSERS(S) 13. DASS/FICATIONS1 DEPT-7501354W STRUCTURAL Donald las& FAA Form 8110-3 (0Y10)SUPERSEDES PRDROUS ED ION SONY_GM_02755117 EFTA_00242099 PROT274 PROT646 EFTA 00242100 PROT275 13DLG-CON-0325E U.S. DEPARIMNT Of 111ANSPORTATICal FEDERAL VINTON ADWreSTRATION 1. DATE March 25.2013 ANCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 2 IMRE Beechjet 3. MODEL NO. 400A 4. TYPE (Asps, Aid.. Norco/mt. arc j AIRPLANE 5. NAME Or APPLCAta LiSTOF DATA a InENTIFICAININ 7 TRIP Document No. DGD-CA01-SS-O7 REV: IR Dated: 3/6/13 SUBSTANTIATION ANALYSIS --- End of Data NOTES• of the !Manor on en Hasler Beeetteraft 400A Aria Is for Beechjet model 400A (Nextant 400XT variant) SIN RK-244 only. is for the structural design aspects only on the above listed data and an installation approval. only for regulations specified In the "Applicable Requirements" dock. with additional regulations not listed herein may be required. This form FAA approval of all engineering design data for the entire Additional 8110.3 approvals may be necessary for Damage Tolerance, Mechanical Systems, Electrical, Weight & Balance, as well as other basis, refer to TC data sheet No. At 6SW 1. This approval 2. This approval does not constitute 3. Approval Is Compliance does not constitute alteration. Flammability, disciplines. 4. For certification B. PURPOSE OF DATA Structural substantiation In support of FM Form 337 for aircraft SIN RK-244. This approval is for design data only on a major alteration and is not an Installation approval. 9. APPLICABLE REOUIRENERTS (List werk aware) 14 PROT902 Part 25.301( Arndt. 25-23), 303lAmdt. I5-23), ..305(1)(b))Amtll 25-24 -3071Anidt 25.23I. -341]Amdt. 25-0],.561lAmdt. 25-231. .601[Ama. 25-0), 403(aXt)lAradt. 25-331, .6051Aradt. 25-0),.6091Amdt.25-0],.6111Amdt.25.231,.613(e)(bXc)(Aindl.25-0), .625 [Arndt. 25- 23), .7850IXbXsX11XeXplAindt 25-32), .787(allAmdt 2S-32),.789]Aindt. 25-32) 10. CERTIFICATION - Under authority vested by direction of me Administrate.. and In accordance dm conditions end irmations of appointment under (4 PROT903 Pan In data Isled tow and on attached vines numbered WA nave boon examines n accordance wail eget:race PeoCeOures and loins to trompb, rAt applicable requirements d the AlmultilneSS Standards Listed K Recommend approval of these data I (We) Therefore ts) Approve blew data 4004TURGEs)0F OESIONA 049INEERINDREPRESENTAINE(S) 12. OESIGNAIION nulaeRs(S) C. ORSSWICATII:70) c illi - etg-9 ( 1 tlf --4:0 -- CERT-750135-SW STRUCTURAL nald Gilles,: FAA Form 8110-3 (oma) SUPERSEDES PREVCVS EDITION PROT647 EFTA 00242101 PROT276 PROT648 EFTA_00242 I 02 PROT277 13DLG-CON-03258 U.S. DEPARTMENT OF TRANSPCRTMCN FEDERAL AVIATION ADIANISTRAMN 1. DATE March 25, 2013 2. MAKE Beechjet 3. MODEL NO. 400A 4. TYPE (Mptine. Raft. IIIM:Opler, efej AIRPLANE & NAME OF APPUCANY LIST OF DATA 6 10EIGT1GAllOal 7 TITLE Document No. DGD-CA02-101 REV: B Dated: 1125113 DGO-CA02-501 REV: IR Dated: 6/13/12 DGD-CA13-501 REV: IR Dated: 12/21/12 DGD-CA13-501 EO: A•1 baled: 2/28/12 DGD-CA04-101 REV: IR Dated: 6/13112 RH GALLEY ASSY RH GALLEY INSTL CARD TABLE INSTL CARD TABLE INSTL SIDE LEDGE ASSY -------- End of Data NOTES' is for BseeNet model 400A (Nextant 400XT variant) SRI RIC•264 only. is for the structural design aspects only on the above listed data and an Installation approval. only for regulations specified in the "Applicable Requirements" block. with additional regulations not listed herein may be required. This form FM approval of all engineering design data for the entire Additional 8110-3 approvals may be necessary for Damage Tolerance, Mechanical Systems, Electrical, Weight & Balance, as well es other basis, refer to TC data sheet No. Al flSW Approvals are provided separably. 1. This approval 2. This approval does not constitute 3. Approval Is Compliance does not constitute alteration. Flammability, disciplines. 4. For certification S. Structural & PURPOSE OF DATA To provide type data for FM approval of structure in support of a return to service on SIN RK-244. This approval is for design data only on a major alteration and Is not an Installation approval. 9. APPIXATLE REOUPEMENTS (Ust specie me m) 14 PROT904 Part 25.601 Arndt 25-0,25.60;(mXb), Arndt 25-38, 25.605 Audi 25-0,25.609 Arndt 25-0.25.611, Arndt 25-23, 25.613 (e)(b)(c) Arndt 25-0, 25.619 Arndt 25-23, 25.625 Arndt 2S-23, 25.785 (e)(bficfidfiefif) Arndt 25.32, 25.719 Arndt 25.32 10 CERTIFICATION • Undo, authonty PM 169. dale aped above and on van eteilmbia recementems of me vested by direction of the Administrator and In accordance Win condi:boos and 4n alerts of appoinienent under t4 PROT905 Daubed sheets numbered N/A have boon examined In accordance Wm eatables! premiums and found to corn* Ainvoliiness Slandada UMW. approval Of Mese data these eats Recommend I WO Therrave CO Approve 11. SIGNATUREIS)OF DESIGNATED ENGINEERING REPRESENTATIVE(SI 12 DESIGNATION NUMI5ERSIS) 11 CLASSW1CATICNIS) i ) CA/ fe d/ <24 n.4 0 DERT-750135-SW STRUCTURAL Donald Ggiespie FM Form 6110-3 (OLIO) SUPERSEDES PREVIOUS EDITION PROT649 EFTA_00242 I 03 PROT278 PROT650 EFTA 00242104 PROT279 13DLG-CON-0325A 1. DATE March 25, 2013 2 MAKE Beechjet 3. 1AOCEI. NO 400A 4. TYPE (maw*, Redo, Hatcaot atl AIRPLANE s NAN8 OF APPLICANT LIST OF DATA ti tcPtiTICCAT1ON 7 7MP Document No. DOD-CA01.101 REV: D Dated: 3/5/13 DGD-CADI.101 EO: E-1 Dated: 3/6/13 DGD-CA01.501 REV: IR Dated: 6/13/12 OG0-CA01.501 EO: A-1 Dated: 1/29/13 000-CA01.5O1 EO: A-2 Dated: 3/5/13 LH GALLEY ASSY LH GALLEY ASSY LH GALLEY INSTL Fad of Data Nons • Is for Beecidet model 400A (Nextant 400XT variant) SIN RK-244 only. Is for the structural design aspects only on the above listed data and an Installation approval. only for regulations specified in the "Applicable Requirements" block. with additional regulations not listed herein may be required. This form FAA approval of all engineering design data for the entire Additional 8110-3 approvals may be necessary for Damage Tolerance, Mechanical Systems, Electrical, Weight & Balance, as well as other basis, refer to TC data sheet No. Al 6SW Approvals are provided separately. 1. ThIs approval 2. ThIs approval does not constitute 3. Approval Is Compliance does not constitute alteration. Flammability, disciplines. 4. For certification 5. Structural e. PURPOSE OF DATA To provide type data fo FAA approval of structure in support of a return to service on SIN RK-244. This approval Is for design data only on a major alteration and is not an installation approval. (*.APPLICABLE REOUIREMENTS 11511000* swore) 14 PROT906 Pare 25.601 Made 25-0,26.6•3(a0(b),Anuft 25-31, 25.605 Arndt 25-0, 25.609 Arndt 25-0, 25.611, Amdt 25.23, 25.613 (s)(b)(e) Arndt 25-0,25.619 Ankle 25-23, 25.625 Arndt 25-23, 25.715 (aNbNeNdNeN0 Amdt 35-32, 25.789 Arndt 25-32 SO. CERTIFICATION Pan 183, data ISIS with applicable recpslrornents I tWe)Therefors - Under aulradly above and of the 0 Recommend wedded by direction on attached shags numbered AlnAorIttness Standards approver of these more data al the AdrrinIstretor WA have end b eccortlance wilh conditions and Invtainorn of appointment under 14 PROT907 been wurrined in accordance with established procedures and toted to comply Usted. dam e Approve II AlitlE(S)OF OCSIONA °ENGINEERING REPRESENTATIVE/S1 N 12 OESIONANCel lalluRERS(S) 13 CA.ASSIFCATICH(S) r., 1 5.47, i 1 DERT-750135-SW STRUCTURAL nald Gil pla FAA Form 81104 (03 re) SUPERSEDES PREVIOUS EDITION PROT651 EFTA_00242105 PROT280 PROT652 EFTA_00242 I 06 PROT281 Aviation Fabricators, Inc. 805 North Fourth Street. Clinton, Missouri 64735 Report # AF-475FTP August 09, 2010 Rev (A) Functional Test Procedure for STC # ST01572WI Hawker Beechcraft Cabin Configuration Applicable Aircraft Model: Hawker Beechcraft 400, 400A PROT653 EFTA_00242 I 07 PROT282 Aviation Fabricators, Inc. AF-475FTP 805 North Fourth Street 08-09-10 Clinton, Missouri 64735 Rev (A) Page 2 014 Revision Log Date Rev Pages Description Approved by 08.09-10 A 1 -Added model 400A G.R. Lowe W -Changed data list # to AF-475MDL PROT654 EFTA_00242 I 08 PROT283 Aviation Fabricators Inc. Clinton, MO. 64735 For Interior Cabin Configurations Document No.: AF-528 Revision "IR" Revision Date: 11121/11 Applicable to: Hawker Beechcraft model 400A Modified by FAA STC ST01572INI The Information in the Instructions for Continued Airworthiness is FM accepted material and complies with 14 PROT908 25.1529, instructions for Continued Airworthiness. It supersedes or adds to that provided in the Maintenance Manual for the Hawker Seechcraf I 400A Aircraft, only where covered in the items contained herein. For limitations and procedures not contained in the Supplement, consult the Component Maintenance Manual, or other approved airplane data. Page 1 of 15 PROT655 EFTA_00242109 PROT284 ammo (660) 8858317 (660) 885-3743 Fax www.avfab.corn e-mail: saleseavlab.com Nov 7, 2012 'gy-?,9H 5-A fi. OO3 70a CERTIFICATE OF 0NF0RMANCE l A AVIATION FABRICATORS This certifies that vlation Fabricators, Divan, 3 Place with stowage provisions, Beechjet, part number, 32-0396(A60P)T1i3.K-02, serial number, 003702, was manufactured in, or determined to be in conformity to an with approved design data and is iu a condition for safe operation for Installation on aircraft. Jeffrey Lowe Vice-President Aviation Fabricators • Central Airmotive PROT656 EFTA_00242 I 10 PROT285 1 REVISION PAGE Document Title: Instructions for Continued Airworthiness Prepared By: Todd Pogue Reviewed By: Jeffrey R. Lowe Updates to the ICA will be made by Aviation Fabricators Inc. Updates will be listed in the log of revisions and the effective pages will be listed below. Log of Revisions REV. NO. EFFECTED PAGE(S) DESCRIPTION DATE APPROVED BY IR All Initial Release 11/21/11 JRL Per the requirement of Appendix H of 14 PROT909 Part 25 paragraph H25.1 (c), the changes made to the ICA by the applicant will be distributed via mail by means of paper copy Page 2 of 15 PROT657 EFTA_00242 I I I PROT286 ICA Document No.: AF-528 Revision (IR) Dale: November 21, 2011 DESCRIPTION PAGE REVISION PAGE 2 3 ABBREVIATIONS AND DEFINITIONS 4 1.0 INTRODUCTION 5 2.0 INSPECTION REQUIREMENTS AND OVERHAUL SCHEDULE 9 3.0 DIMENSION AND ACCESS' 11 4.0 LIFTING AND SHORING 11 5.0 LEVELING AND WEIGHING 11 6.0 TOWING AND TAXIING 11 7.0 PARKING AND MOORING 11 8.0 PLACARDS AND MARKINGS 12 9.0 SERVICE INFORMATION 13 10.0 AIRWORTHINESS LIMITATIONS 15 11.0 TROUBLESHOOTING INFORMATION 15 Page 3 of 15 PROT658 EFTA_00242 I 12 PROT287 I REVISION PAGE Document Title: Instructions for Continued Airworthiness Prepared By: Todd Ponue Reviewed By: Jeffrey R. Lowe Updates to the ICA will be made by Aviation Fabricators Inc. Updates will be listed In the log of revisions and the effective pages will be listed below. Log of Revisions REV. NO. EFFECTED PAGE(S) DESCRIPTION DATE APPROVED BY IR All Initial Release 11/21/11 JRL Per the requirement of Appendix H of 14 PROT910 Part 25 paragraph H25.1 (c). the changes I made to the ICA by the applicant will be distributed via mail by means of paper copy 1 Page 2 of 15 PROT659 EFTA_00242 I 13 PROT288 Revision (IR) Clinton, MO. 84735 Date: November 21, 2011 DESCRIPTION PAGE REVISION PAGE 2 3 ABBREVIATIONS AND DEFINITIONS 4 1.0 INTRODUCTION 5 2.0 INSPECTION REQUIREMENTS AND OVERHAUL SCHEDULE 9 3.0 DIMENSION AND ACCESS• 11 4.0 LIFTING AND SHORING 11 5.0 LEVELING AND WEIGHING 11 6.0 TOWING AND TAXIING 11 7.0 PARKING AND MOORING 11 8.0 PLACARDS AND MARKINGS 12 9.0 SERVICE INFORMATION 13 10.0 AIRWORTHINESS LIMITATIONS 15 11.0 TROUBLESHOOTING INFORMATION 15 Page 3 of 15 PROT660 EFTA 00242114 PROT289 806 North Fourth Street ABBREVIATIONS AND DEFINITIONS Revision (PR) Dale: November21, 2011 Abbreviations Definitions AML FAA Approved Model List (AML) Detailed Inspection (DET) An intensive examination of a specific Item, installation or assembly to detect damage, failure or irregularity. Available lighting is normally supplemented with a direct source of good lighting at an intensity deemed appropriate. Inspection aids such as mirrors, magnifying lenses, etc. may be necessary. Surface cleaning and elaborate access procedures may be required. FM Federal Aviation Administration FM MIDO FM Manufacturing Inspection District Office General Visual Inspection (GVI) A visual examination of an interior or exterior area, installation or assembly to detect obvious damage, failure or irregularity. This level of inspection is made from within touching distance unless otherwise specified. A mirror may be necessary to enhance visual access to all exposed surfaces in the Inspection area. This level of inspection is made under normally available lighting conditions such as daylight, hangar lighting, flashlight or droplight and may require removal or opening of access panels or doors. Stands, ladders or platforms may be required to gain proemity to the area being checked. ICA Instructions for Continued Airworthiness Special Detailed Inspection (SDI) An Intensive examination of a specific item, installation , or assembly to detect damage, failure or Irregularity. The examination is likely to make extensive use of specialized Inspection Techniques and/or equipment. Intricate cleaning and substantial access or disassembly procedure may be required. STC Supplemental Type Certificate Page e of 15 SDNY_GIvl_02755193 EFTA_00242115 PROT290 1.0 INTRODUCTION Revision (IR) The purpose of this Maintenance Manual Supplement and Instructions for Continued Airworthiness (ICA) is to provide the maintenance technician with the information necessary to ensure the continued airworthiness of the Aviation Fabricators cabin configuration, per installation number 400-3, when installed in the aircraft passenger cabin in accordance with Aviation Fabricators design data included on Master Data List AF-475MDL and per Supplement Type Certificate (STC) No. ST01572W1 Modifications to an aircraft obligates the operator to include the maintenance Information provided by this document into the operators aircraft Maintenance Manual and operator's aircraft scheduled maintenance program. This document defines supplementary maintenance operations and frequencies recommended by Aviation Fabricators Inc., to ensure the aircraft's airworthiness. The information contained herein addresses the requirements specified in 14 PROT911 25.1529, Instructions for Continues Airworthiness and supplements the basic Airplane Maintenance Manual only in those areas listed as pertains to the installation of divan assemblies, as installed per the Aviation Fabricator Master Data List AF-475MDL. For limitations and procedures not contained in this supplement, consult the basic Airplane Maintenance Manual. DATA All information to support the continued airworthiness of this modification is contained in: STC ST01572WI. Master Data List: AF-475MDL. Installation: 3 Place Divan (Ref. Installation number 400-3), Installation Instructions D-10666 for P/N 32-0396K-X Parts: P/N 32-0396K-X, 3 Place Divan Installation The new divan assembly (with restraint system) is a self contained complete assembly that mounts to the existing seat track, using standard fittings, in accordance with FAA approved floor plans. The (restraint system) seat belts are attached to the seat track with typical tie down fittings and the inertia reel shoulder harness is bolted to the divan frame on the outboard side using standard aircraft hardware. Design Change Control All data and changes to the parts and assemblies will be tracked per Master Data List AF- 475MDL Rev C or later FAA approved revision. Applicable Aircraft Beechjet 400A Page 5 of 15 PROT661 EFTA_00242I 16 PROT291 ABBREVIATIONS AND DEFINITIONS ICA Document No.: AF-628 Revision (IR) Abbreviations Definitions AML FAA Approved Model List (AML) Detailed Inspection (DET) An intensive examination of a specific Item, Installation or assembly to detect damage, faiure or irregularity. Available lighting is normally supplemented with a direct source of good lighting at an Intensity deemed appropriate. Inspection aids such as mirrors, magnifying lenses, etc. may be necessary. Surface cleaning and elaborate access procedures may be required. FAA Federal Aviation Administration FM MIDO FM Manufacturing Inspection District Office General Visual Inspection (GVI) A visual examination of an interior or exterior area, installation or assembly to detect obvious damage, failure or irregularity. This level of inspection Is made from within touching distance unless otherwise specified. A mirror may be necessary to enhance visual access to all exposed surfaces in the Inspection area This level of inspection Is made under normally available lighting conditions such as daylight, hangar lighting, flashlight or droplight and may require removal or opening of access panels or doors. Stands, ladders or platforms may be required to gain proximity to the area being checked. ICA Instructions for Continued Airworthiness Special Detailed Inspection (SDI) An Intensive examination of a specific item, Installation , or assembly to detect damage, failure or irregularity. The examination is likely to make extensive use of specialized Inspection Techniques and/or equipment. Intricate cleaning and substantial access or disassembly procedure may be required. STC Supplemental Type Certificate Page 4 of 16 PROT662 EFTA_00242117 PROT292 Clinton, MO. 64736 Revision (IR) 1.0 INTRODUCTION The purpose of this Maintenance Manual Supplement and instructions for Continued Airworthiness (ICA) is to provide the maintenance technician with the information necessary to ensure the continued airworthiness of the Aviation Fabricators cabin configuration, per installation number 400-3, when installed in the aircraft passenger cabin in accordance with Aviation Fabricators design data included on Master Data List AF-475MDL and per Supplement Type Certificate (STC) No. ST01572WI. Modifications to an aircraft obligates the operator to include the maintenance Information provided by this document into the operators aircraft Maintenance Manual and operator's aircraft scheduled maintenance program. This document defines supplementary maintenance operations and frequencies recommended by Aviation Fabricators Inc., to ensure the aircraft's airworthiness. The Information contained herein addresses the requirements specified in 14 PROT912 25.1529, Instructions for Continues Airworthiness and supplements the basic Airplane Maintenance Manual only in those areas listed as pertains to the installation of divan assemblies, as installed per the Aviation Fabricator Master Data List AF-475MDL. For limitations and procedures not contained in this supplement, consult the basic Airplane Maintenance Manual. DATA All information to support the continued airworthiness of this modification is contained in: STC ST01572W1 Master Data List: AF-475MDL. Installation: 3 Place Divan (Ref. installation number 400-3), Installation Instructions D-10668 for P/N 32-0396K-X Parts: P/N 32-0396K-X, 3 Place Divan Installation The new divan assembly (with restraint system) is a self contained complete assembly that mounts to the existing seat track, using standard fittings, in accordance with FAA approved floor plans. The (restraint system) seat belts are attached to the seat track with typical tie down fittings and the inertia reel shoulder harness Is bolted to the divan frame on the outboard side using standard aircraft hardware. Design Change Control All data and changes to the parts and assemblies will be tracked per Master Data List AF- 475M0L Rev C or later FAA approved revision. Applicable Aircraft Beechjet 400A Rage 6 of 16 PROT663 EFTA_00242 I IS PROT293 3 Place Divan P/N 32-0396K-X (Top not shown for clarity) FOOT ATTCHMENT TO OWN F OOTA1TA?:/lE210 TRACK Figure 1.0A Revision (IR) "ttsurno FOOT ATIACMIT TO /TOMO' GIP Page 8 of 16 PROT664 EFTA (X1242119 PROT294 Inertia Reel Attachment DIVAN FRAME WASHER INERTIA REEL Figure 1.0B Seat Belt Attachment Figure 1.0C Revision (IR) Date: November 21. 2011 BOLT Page 7 of 15 PROT665 EFTA_00242 I 20 PROT295 3 Place Divan P/N 32-0396K-X (Top not shown for clarity) coat TOWN/01 K•011.60.0 resoisenaision tale. tiaricr4.-.. roar ATT,CHMIBIT TOT RACK Figure 1.0A Revision (IR) "far' FOOT ATTACIVSIT TO TRACKWTH COP reel - Page 6 of 16 PROT666 EFTA_00242121 PROT296 Inertia Reel Attachment Figure 1.08 Seat Belt Attachment Figure 1.0C ICA Document No.: AF•528 Revision (IR) Page 7 of 15 PROT667 EFTA_00242I 22 PROT297 SEAT BLACK ASSEMBLY SEAT BOTTOM ASSEMBLY oM CUSHION AAKFMAI V OrBOOBBY0 AMMON Figure 1.0D gam ICA Document No.: AF•526 Revision (IR) Vrtat0110C. Lou:Rower VELCROHOOK Page 8 of 16 PROT668 EFTA 00242123 PROT298 Revision (IR) 2.0 INSPECTION REQUIREMENTS AND OVERHAUL SCHEDULE 1. To comply with14 PROT913 25.1529, continue the new divan assembly (with restraint system) on the same inspection and maintenance schedule used per the Hawker Beechcraft Maintenance Manual for cabin section inspections. a. The new cabin configuration components require no service other than inspection at normal inspection interval of 200 hours. b. The safety belts require no service other than inspection at normal inspection interval of every 200 hours. c. Perform a detailed visual inspection of each passenger seat bottom and back cushions and covering of all cabin interior components to detect apparent or obvious defects or irregularities. On the cushion assembly, check for cracks and punctures within a 4" diameter circle. The cushion assembly can have no more than three defects found within the 4" diameter circle. If a cushion develops a lump", check to see if there are no more than two lumps within a 4" diameter circle. Any damage to the cushions outside of the described limits will require them to be replaced. Visually inspect the covering assemblies for holes, punctures, and tears. If the damage to the covering is holes smaller than''/? in diameter or a cut at a maximum of 2" in length then the covering is satisfactory. The sewing of the cover assemblies is not to exceed 1" tearing. Any damage to the covering assemblies outside of the described limits will require them to be replaced. d. Visually inspect the divan and seat assembly tubes and diaphragm for cracks and deformation. Damaged conditions could be detected as a crack at the edge of the tube or along the length of the tubes or as a crack, tear or cut found on the seat bottom or back diaphragm. Visually inspect all hardware for excessive wear before and after installation. Replace the seat back and bottom diaphragm if two cracks or deformations are found with a 4" diameter circle. If a tear or cut is found with a maximum of 6", replace the diaphragm. There shall be no broken tubes. There shall be no sharp corners, edges, or protrusions that may Injure passengers. Replace the tubes if they are bent in such a way that they are more than 2" off center. Replace the seat tubes if crack length is found to be .125" or greater. Replace the tube if a dent is found running longer than 3". Replace the seat tubes if deformation is greater than .25" the overall thickness of the tube diameter. Cracked or broken fasteners or fittings are to be replaced with new immediately. Page 9 of 16 PROT669 EFTA 00242124 PROT299 1 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) KOJI VELCRO NOOK VE11010 1.000 Page 8 of 16 PROT670 EFTA 0(1242125 PROT300 Clinton, MO. 84736 Revision (IR) 2.0 INSPECTION REQUIREMENTS AND OVERHAUL SCHEDULE 1. To comply with14 PROT914 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 PROT671 EFTA 00242126 PROT301 Revision (IR) For repair or replacement of damaged or broken parts or assemblies contact 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 PROT672 EFTA 00242127 PROT302 3.0 DIMENSION AND ACCESS: Revision (IR) 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 PROT673 EFTA 00242128 PROT303 Revision (IR) For repair or replacement of damaged or broken parts or assemblies contact 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 PROT674 EFTA_00242 I 29 PROT304 3.0 DIMENSION AND ACCESS: Revision (IR) 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 PROT675 EFTA_00242 I 30 PROT305 8.0 PLACARDS AND MARKINGS Revision (IR) 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 EFTA_00242 I 31 PROT306 9.0 SERVICE INFORMATION Typical Passenger Seating Service Instructions: A. Upholstery Cleaning: Service Instructions Revision (IR) 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 PROT915 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 PROT676 EFTA_00242 I 32 PROT307 8.0 PLACARDS AND MARKINGS Revision (IR) 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 PROT677 EFTA_00242 133 PROT308 1 9.0 SERVICE INFORMATION Typical Passenger Seating Service Instructions: A. Upholstery Cleaning: Service Instructions Revision (IR) 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 PROT916 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 PROT678 EFTA 00242134 PROT309 Revision (IR) 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 PROT679 EFTA 00242135 PROT310 10.0 AIRWORTHINESS LIMITATIONS ICA Document No.: AF 528 Revision (IR) 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 PROT680 EFTA 00242136 PROT311 Clinton, MO. 84736 Revision (IR) 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 PROT681 EFTA 00242137 PROT312 10.0 AIRWORTHINESS LIMITATIONS Revision (IR) 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 PROT682 EFTA_00242138 PROT313 U. S. DEPARTMENT OF TRANSPORTATION 1.DATE 5/02/2013 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 PROT917 Pert 25.853 (a) Arndt 25-116 Appendix F Part I (a)(1)(ii) 14 PROT918 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 PROT919 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 PROT683 EFTA 00242139 PROT314 PROT684 EFTA 00242140 PROT315 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 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 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 PROT920 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. . 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TIE AIRCRAFT CESCRISEOABOVE NOS MN INSPECTEOMO cotta NR Oft BY mason. ass At cni eat as c§ 3 TA PROT921 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 PROT922 an 6$ I IN CYR pen iIi OR Mi lli PROT923 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 PROT685 Q D O 0 EFTA 00242141 PROT316 PROT686 EFTA_00242 I 42 PROT317 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 PROT687 EFTA_00242143 PROT318 PROT688 EFTA_00242 I 44 PROT319 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 EFTA_00242 I 45 PROT320 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* PROT924 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 EFTA 00242146 PROT321 MATEO STATES CF AMEND DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION 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) PROT689 EFTA 00242147 PROT322 PROT690 EFTA 00242148 PROT323 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 PROT691 EFTA_00242 I 49 PROT324 PROT692 EFTA 00242150 PROT325 U.S. Department of Transportation Administration EXPERIMENTAL OPERATING LIMITATIONS PURPOSE Research and Development MAKE 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 PROT925 §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 PROT926 Part 91, and all additional limitations herein prescribed under the provisions of 14 PROT927 § 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 PROT928 §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 PROT929 § 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 PROT930 §91.9. Total Pages: 3 PROT693 EFTA_00242151 PROT326 PROT694 EFTA 00242152 PROT327 EXPERIMENTAL OPERATING LIMITATIONS PURPOSE Research and Development MAKE. 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 PROT931 § 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 PROT932 § 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 PROT933 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 PROT934 §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 PROT935 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 PROT936 Pan 43. 26) This aircraft must display the word EXPERIMENTAL in accordance with 14 PROT937 §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 PROT938 §91.205 must be inspected and maintained in accordance with the requirements. of parts 14 PROT939 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 PROT940 § 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 PROT941 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 EFTA (10242153 PROT328 PROT695 EFTA_00242 154 PROT329 EXPERIMENTAL OPERATING LIMITATIONS PURPOSE Research and Development MAKE 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 PROT696 EFTA 00242155 PROT330 PROT697 EFTA 00242156 PROT331 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 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 PROT698 EFTA_00242 157 PROT332 PROT699 EFTA 00242158 PROT333 LOG BOOK ENTRY from Designated Airworthiness Representative (DAR) REGISTRATION NUMBER AIRCRAFT MAKE/MODEL SERIAL No. TT/13N LANDINGS/CYCLES N493LX 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 PROT700 EFTA_00242159 PROT334 PROT701 EFTA_00242 I 60 PROT335 0 USDepernam el Taws. mow mem sammrstion Patina:maul cwra No 212,34020 wrXx2C07 EISCIrOnie Tracking Number 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 Model 400A Series 2. Chimer Name (AS Mow, on regraration terbfiCSM) Address (As shown on Mgisfrafion cennica(4) Address 26180 Curtiss Wright PKWY Ccy Richmond HeiohLs SUM OH 20 19.1.43-1453 County USA 4. Type 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 Minn [ADDRESS REDACTED] 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 PROT942 Pan 43 APP. El 0 Signature/Dale of Automat Indent*, A.Ockwell 4-12Lk A 05/30/2013 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" PROT702 755239 Erl'A_00242161 PROT336 PROT703 EFTA 00242162 PROT337 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. (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 DCP-5000 822-1028-011 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) PROT704 EFTA_00242 I 63 PROT338 PROT705 EFTA_00242164 PROT339 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. (If more space is required. attach additional sheets. Identify with aircraft ',shone*/ and regustrahon mark and date work completed) N493LX 5/30/2013 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 12.90 89.2 AFD-3010E 822-1753-416 12.90 89.2 AFD-3010E 822.1753-416 12.90 89.2 AFD-3010E 822-1753-416 12.90 89.2 IMT-3010 822-1140-401 4.40 85.0 IMT-3010 822-1140-401 MD Mounting Rack 4.40 85.0 IMT-3010 822-1140-401 4.40 85.0 IMT-3010 822-1140-401 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 PROT706 EFTA (X)242165 PROT340 PROT707 EFTA _00242166 PROT341 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. (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 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 [SSN REDACTED]-1 Pilot Reversion Panel 0.2 88.0 Rev. Panel 373.91.3203-3 Co-pilot Reversion Panel 0.2 88.0 9-PED [SSN REDACTED]-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 [SSN REDACTED].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. Form 337 (10-063 PROT708 EFTA 00242167 PROT342 PROT709 EFTA 00242168 PROT343 !Lida $Lnitts of ,Ponrrirn !epnrtnlent of Transportation Arbera I cAbintinn cahminiatratinn $upplentental `Type Certificate avid/€.0,4•sii.yeisele .4 71.1.,021&" STI0959SC 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. PROT710 EFTA_0024211 69 PROT344 PROT711 EFTA 00242170 PROT345 [repeated 3 times] 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. [SSN REDACTED] 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. [SSN REDACTED] 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. [SSN REDACTED] Revision IR, approved March 28,2012, or later FAA approved version, is required on board the modified aircraft. ..52tuu: Based on 14 PROT943 §§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 PROT944 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>. PROT712 EFTA_00242 I 7 I PROT346 PROT713 EFTA 00242172 PROT347 [repeated 3 times] 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 PROT945 §§ 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 PROT946 §§ 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, PROT714 EFTA 00242173 PROT348 PROT715 EFTA_00242 I 74 PROT349 e S04910.11, 1 el Trawallean reserstamme emensenism fi Porovad 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 PROT947. 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) Afteas ms shown On reeistrabon CertleCate) ACOniss 26180 Curtiss Wright PKWY cry Richmond Heights sum OH I, eil33-145.1 firu-R1 OA 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 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 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) PROT716 EFTA_00242175 PROT350 PROT717 EFTA 00242176 PROT351 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 (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 [SSN REDACTED] Rev F. End K A00610061 Sheets Are Attached FAA Form 337 0006) PROT718 EFTA_00242 I 77 PROT352 PROT719 EFTA 00242178 PROT353 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 PROT720 EFTA 00242179 PROT354 PROT721 EFTA_00242 I 80 PROT355 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 PROT722 EFTA_00242I I PROT356 PROT723 EFTA_00242182 PROT357 }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 EFTA_00242 I 83 PROT358 PROT724 EFTA 00242184 PROT359 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 PROT948 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. PROT725 EFTA_00242185 PROT360 PROT726 EFTA_00242186 PROT361 OW OW US Ceparent MAJOR REPAIR AND ALTERATION ci Tremortibm 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 PROT949 §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 PROT950. §46301(a)) 1. Aircraft 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 [ADDRESS REDACTED]atement 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 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 PROT951 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( Persons Approved by Camden Department of Transacts FAA Designee Repair Station Other (Specify Certificate er Desienatim No. DJFA 206D SapaturefDate of Authorized Individual ,R obert W. Vogt 40/2012 9. 774 20 A FAA Fonn 337 noon PROT727 EFTA 00242187 PROT362 PROT728 EFTA_00242 I 88 PROT363 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 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 PROT729 755267 EFTA_00242189 PROT364 PROT730 EFTA 00242190 PROT365 IWO SUMS OF AMEACA DEPARTMENT OF TRANSPORTATONPEDERAL AVIATION ADAW1WIRATION 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 EFTA 00242191 PROT366 \ . PROT731 EFTA_00242 I 92 PROT367 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 PROT732 EFTA_00242 I 93 PROT368 PROT733 EFTA 00242194 PROT369 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). 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 PROT734 EFTA_00242195 PROT370 PROT735 EFTA 00242196 PROT371 -:-.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 EFTA_00242197 PROT372 PROT736 EFTA 00242195 PROT373 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 PROT952 §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 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 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 [ADDRESS REDACTED]atement - B. Kind of Agency win. F ot Oeisii. VC U. S 0linafiCated Mechanic I Manuleckeer hens 27 Um (Maga a ___, _ Faaign Cars/caeca Mechanic 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 Extended range fuel per 14 PROT953 Part 43 Aft B ii Signature/Date of Authorized Individual Brian Kanya deCser A/ "reit //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 PteSOnS Approved by Canadian Pepe/anent ot Tramoal FM Designee Repair Station 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) PROT737T7 EFTA_00242 199 PROT374 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. (If more space is required, attach additional sheets. Identify with aircraft actionably and registration mark end date work completed) USA N493LX SN-244 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([REDACTED])0([REDACTED])0000(XX)00(XXX)000000([REDACTED])00C[REDACTED] PROT738 EFTA 00242200 PROT375 0 Drop-rim MAJOR REPAIR AND ALTERATION of baemmmtM, 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 PROT954 §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 PROT955. §44701). Fail re to report can result in a civil penalty for each such violation. (49 PROT956. 5463O1(a)) i. Aircraft 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 - 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 [ADDRESS REDACTED]atement 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 PROT957 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 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 EFTA_00242201 PROT376 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 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 [REDACTED]YJMO([REDACTED]J00(XXX)([REDACTED] PROT739 EFTA 00242202 PROT377 0 US Deparnern 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 PROT958 §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 PROT959. §44701). Failure to report can result in a civil penalty for each such violation. (49 PROT960. §46301(a)) 1. Aircraft 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 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 [ADDRESS REDACTED]atement Haat no% open tut U. S. CiffbfiCated MeCtene I Manufacturer Menu Mau Divs. Sias a Anti tat6catod Mechanic 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 Extended range fuel per 14 PROT961 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 Persons Approved by Callltrill °enactment or Transport FM Designee Repair Station 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 PROT740 EFTA _OO2412O3 PROT378 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 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([REDACTED]Y=XXX)0000(XXXXXJ000([REDACTED] 0 PROT741 EFTA_00242204 PROT379 0 IA Ospertnirl {Skews:4Sn '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 PROT962 §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 PROT963. §41330.1(e)) 1. Aircraft NebOrlality and Registration Mark USA N493LX Serial No. RK - 244 Make 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 4. Type 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 [ADDRESS REDACTED] 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 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 Pierian APpreved try Canaan Depertmem of TninspOt FAA Designee Repair Station CertMcale or DJFA 2060 Signature/Date of Authorized Indivklual sez57 RICHARD EVANS - A.,:0 thr dal Rio FAA Form 337 (wee) PROT742 EFTA_00242205 PROT380 PROT743 EFTA 00242206 PROT381 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 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) PROT744 EFTA_00242207 PROT382 PROT745 EFTA 00242208 PROT383 OWED MAWS OF AblEFOCA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION 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 $100.2 Ga) umIto sto Es or wee. DEPARTMENT OF TRAOSSPOTTATON - FEDERAL AVIATION ADMINISTRATION I. AATIONINJTY NC 2 WOOPACNONA Ate MOOD. 4. CATEGOON NECIAORAVONWANCE N793TA 400A RK- 244 TRANSPORT 's AvTICaTv AND SASS MA ISSUANCE TmeanorVineleCenineests issued punieem iotAttleowstAseten sag ittyiesietteste. pet nos 'se Oeie o/ essence ire *eon to elAbA WWI MI Nrr 0•0•000 an] found w cottion• to IN Nee vaislicsie weeks. to es o casco lot see *OWNS/ WO hips Nen gap pm betel IN moan "mins Crt IN aDOCIOis cationonesso• toe .Mend avo.ovisness code is • wooded t. kw. to IN Cetera. on lowneinAsi Cod ...vomiting is NA*0 feet Estegecre Na st 3 ANCRAFt VIDAL Nut4601 r (Fen MO CONOMONS Limns wow sotteneenes wawa* moo*. es • wenosion awe ts aterots• tnettisead by Pie A0"""M•10( 0" enRoll.•••• C01.1Cal• 4 elects* se boo ei we IlybeinnOt rihrtillim. Maiintieriant• NO Nene its Pinioned o KONOtoc• is4APates2 I.43 nil 44 VW Fare &neon eguisteAl. 4•00400.44e. ins IN erne 9 •024101•0 al me owl Sa -.1 i s DAVAO. ISSUANCE IDA10/01/99 r epts 0 81!. ; wRi t • i 'l.h.c.F.1,2t OEsOmoom NUMBER ACE - FWD - 07 Any earpolco teetedookel. *reseal of Mounds:eta ess be Ossien•biebv• MwneWeebq MOD a tAIVA0'.. ." 0101'.."6 3 • NNE et bah Teel CERIVICATE MUSE BE DISPUTED iN THE micamIT N ACCOMANCE WITH APPUCABLE IEOEAK WIATION AEOuuiliCe4 ram 610t.-2 sem Ud 0.010101$ SAO SDNY_GIvl_02755287 EFTA 00242209 PROT384 PROT746 EFTA 00242210 PROT385 SITITO SIAM 01 aliOeCA 0.EPARTP4 ENT OF TN OrkSPORTATION-FEOBIAL AVIATION AOSSIN16TRATCON I NATIONALITY Awl) RE.G5TAATION aaa N793TA EVJ4PACIUPER MC 1•000. 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, PROT747 15, and 17 EFTA_001411I I PROT386 Z PROT748 EFTA_00242212 PROT387 Cc-iJL12--i-faz it3-4r) O' Form us oePsmwr or (Airframe, Powerplant, Propeller, or Appliance) ripaintswition Awrissinikw Approved OMB No. 2120-0020 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 N793TA 2. Owner Name (As shown on registration certificate) NORTH CHANNEL LLC ET-AL CIO Flight Options LLC 26180 Curtiss-Wright Pkwy Richmond Heights OH 44143-1494 THE TECHN CM. DATA IDENTIFIED HEREIN HAS BEEN FOUND REQUIREMENTS AND IS HEREBY APPROVED FOR USE ONLY TO-CONFORMITY-INSPECTION-BY-KPERSON-IN-14-PROT964 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 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- 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 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 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 tcA2O6L Signal e of A thorized IndAidual a...-0 PIA roan !II emit PROT749 EFTA_00242213 PROT388 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 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 'U. S GPO 1994.568-012/00019 SONY_GM_02 755292 EFTA_00242214 PROT389 JAN 03 2005, C . (Airframe, Powerplant, Propeller, or Appliance) near Avtmon ACI ISAMISOA Form Approved OMB No. 2120-0020 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 N7937A 2 Owner Name (As shown on registration certificate) NORTH CHANNEL LLC Er-AL. CIO Flight Options LLC 26180 Curtiss-Wright Pkwy Richmond Heights OH 44143-1494 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 B Kind of Agency Lynn H. Huyen C/0 Flight Options LLC 26180 Curtiss-Wright Pkwy Richmond Heights OH 44143-1494 X U.S Certificated Mechanic ASP 278825845 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 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 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 WA AP MA PROT750 EFTA_00242215 PROT390 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. (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 PROT751 55294 EFTA_002422 I 6 PROT391 I O US Owervron, a FosUN A.,Woo Form Approved OMB Na 2120-0020 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 PROT965. 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 N793TA 2. (Now Maine (As shorn on registralion oerfilicale) FUGHTOPTIONS 26180 CURTIS WRIGHT PARKWAY RICHMOND HTS OHIO 44143 4. Unit Identification a. Type Unit Make Mode: Serial No. Repair Alteration AIRFRAME ((suited In stem 1 X (As POWERPLANT PROPELLER APPLLANCE Type Manufacturer CLASSIC INTERIOR COMPLETIONS INC. 355 RICHMOND ROAD CLEVELAND, OHIO 44143 u.S. Certificated Mechanic R4GRO31Y 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 RECEIVED FAA Designee X Repair Satoh Person Approved by Transport Oate of Approval 12or Rejection 0-2004 Certificate or R4GRO31Y DEC 16 ess_aps 2114 IAA pall/ On" SONY_GM_027 55295 EFTA_00242217 PROT392 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. 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 EFTA 00242218 PROT393 0 US Denwlmen or 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 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 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 PROT966 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 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 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 Other (Specify) OPTIONS FLIGHT SUPPORT, INC., dMa FLIGHT OPTIONS FM Designee Repair Station Person Aopeoved by Transport JUNE 10, 2003 Certificate or Designation Ni) DJFA206D Signature of nodual r za.,4:2 KEITH GAwSYS2Awsm IAA form )47 VI Ail PROT752 EFTA 00242219 PROT394 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 PROT753 EFTA 00242220 PROT395 13 y r JUN 2003 0 US 07Nrmre or FedwalArletion .74nInIstralion Form Approved OMB No. 21200O20 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 PROT967. 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 101 S WEBB ROAD WICHITA, KS 67207 3. For FAA Use On y 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME described in X (As item 1 above) POWERPLANT PROPELLER APPLIANCE Type Manufacturer Stephen J. Maiden 00 FLIGHT OPTIONS LLC 26180 CURTISS WRIGHT PARKWAY RICHMOND HEIGHTS, OH 44143 X U.S. Certificated Mechanic A297605039 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 Other (Specify) FLIGHT OPTIONS LLC AIR AGENCY CERTIFICATE FM Designee Repair Station 3 u v-e.: to, 2003 Certificate or DJFA20613 Signature of Auth ivIdual ? 4.5 c ) (6,e CAtetySTAuSei MA non nf OM. PROT754 EFTA_0024222 I PROT396 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 PROT755 EFTA 00242222 PROT397 "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. PROT756 EFTA 00242223 PROT398 I PROT757 EFTA_00242224 PROT399 AVOliCS Callenlien Center 400 Collins Road NE Mad Station 164100 Cedes Rapids. IA 52498 Tel. 319295.2185 Fax 319 295O337 Rockwell Collins May 14, 2003 W0030737.DOC Flight Options 26180 Curtiss-Wright Parkway Cleveland, 011 44143 Tel: (216) 797-3500 Attention: Subject: Mr. Jody Kremsreiter/ Mr. Richard Fine (Collins on-site) STC ST00881WI-0 Modification of Collins TCAS II System Installation with Collins TTR-920 Change 6.04a Receiver Transmitter and TPR-900 Mode S to a Collins TCAS II System Installation with Collins TTR-920, Collins TTR-921 or Collins TTR-4000 Change 7.0 TCAS II Receiver Transmitter and optional TPR-901 in Part 25 Aircraft Dear Mr. Kremsreiter: Enclosed is a compact disk with one copy each of the following FAA approved STC data: 1. STC ST00881WI-0 Certificate, dated December 1, 2000. 2. FAA Approved Model List (AML) Number ST00881WI-D, amended April 15, 2003. 3. Drawing Index 992-4358-001, Revision M. 4. One copy of each drawing listed on Drawing Index 992-4358-001. 5. Airplane Flight Manual Supplement, ACC-00-105, Revision -. This letter is our authorization for Flight Options to use this STC as basis for the installation of our equipment in your airplanes based on the following model and serial numbers provided by Mr. Richard Fine of Rockwell Collins. PROT758 EFTA_00242225 PROT400 I PROT759 EFTA_00242226 PROT401 Flight Options STC ST00881WI-D May 14, 2003 Page 2 Model 400A WO030737.DOC STC ST00881WI-D MSN MSN RK006 RK248 RK016 RK252 RK022 RK257 RK027 RK260 RK030 RK264 RK031 RK265 RK045 RK268 RK062 RK271 RK093 RK273 RK146 RK274 RK161 RK276 RK168 RK279 RK178 RK282 RK180 RK284 RK186 RK289 RK189 RK292 RK195 RK295 RK198 RK297 RK201 RK301 RK202 RK305 RK209 RK307 RK222 RK310 RK230 RK317 RK234 RK324 RK237 RK327 RK239 RK328 RK244 RK334 RK245 Please return a record of any additional aircraft serial number(s) to me for installations performed using this STC. My fax number is (319) 295-0337. Collins needs to receive this data before we can authorize additional installations. PROT760 EFTA 00242227 PROT402 i PROT761 EFTA_00242228 PROT403 is • Flight Options STC ST00881W1-D May 14, 2003 Page 3 WO030737.DOC Flight Options is responsible for the regulatory approval of any deviations from STC ST00881WI-D. Instructions explaining how to access the data on the CD have been inserted inside the jewel case. Customer satisfaction is important to us, and we would appreciate your input. Please complete and return the enclosed questionnaire or email me at nd let us know how we can best serve you. We trust this data will fulfill your installation requirements. However, if you have any questions, please call me at (319) 295-0618. Douglas W. Jessen Collins Avionics Certification Center Mail Station 164-100 /pah Enclosure PROT762 EFTA_00242229 PROT404 PROT763 EFTA_00242230 PROT405 0 US INV gamin d nearAvIsilon Form Approved OMB No. 2120-0020 41 C-le - ribt AdeMbeitrtike INSTRUCTIONS: Pnnt or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 or subsequent revision the for instructions and disposition of this form. This report is required by law (49 PROT968. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Beechjet Model 400A Serial No. RK- 2 414 USA N99374 2. Owner Name (As shone on registration corifficate) Mist A-ig TPC CT -At- Address (As sham on registration certificate) go ( 5 Loal38 a COLcr*iTYt, KS 61, 0 7 The data identified The 860e-deathbed • This Date herein complied with applicable aircraft subject to conformity approval is only for thiseircraft Approving airworthiness requirements inspection by a makermodel a vv. Inspector and is approved ri authorized elnumbez - only for in FAR 43 7 . new - EICAO P- L e-es-v,I$PECICa wolgiAlrlb`r- APR • 2 3 20O fraienie 8. Type Unit Make j Model Serial No. Repair Alteration AIRFRAME X (As described in item 1 above) POWERPtANT PROPELLER APPLIANCE Type Manufacturer IL Conformity Statement 8. Kind of Agency Keith Gawsyszawski Flight Options. Inc. 28180 Curtiss Wright Parkway Richmond Hts., OH 44143 X U.S. Certificated Mechanic AP 287603483 Certificated Repair Station i Manufacturer D. I certify hereto have information Date April that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments been made in accordance with the requirements of Part 43 of the V.S. Federal Aviation Regulations and that the furnished herein is true and cermet to the best of my knowledge. 5, 2002 Signature of Individual a l 7:14•44. -q) 7. Approval for Return To Service Pursuant Administrator BY to the authority given persons specified below. the unit identified In item 4 was impeded in the manner prescrbed by the of the Federal Aviation Administration and is 00 APPROVED LI REJECTED FM Pt Standards Inspector Manufacturer gr. Inspection Authorization Other (Sped*, FM Designee Repair Station Indy 4, Poo? nation Certificate or No. ifejt374.034,33,14 Signature ofrdividual a I MA Fa IV cow SONY_GM_02756309 EFTA_00242231 PROT406 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. 1 8. Description of Work Accomplished pf more space is required. attach additional sheets Identify with aircraft nationality and registration mark and date work completed I. Removed existing Tail Navigation Light Assembly including the rubber shock mount. 2. Installed Whelen Engineering, Inc. Model 70805-01 Tail Position Light Assembly in accordance with part number 04-0112558-00 instruction sheet to include installation procedures and drawing number 70805. 3. The light assembly will be operationally tested under Flight Options Continuous Airworthiness Maintenance Program under Phases IC, 9C and I7C. 4. Weight and Balance change found negligible. END 'Ll.S.GPO.1994-588-012100019 PROT764 EFTA 00242232 PROT407 0 U:S. Departnent (Airframe, Powerplant, Propeller, or Appliance) of bansportelon Fulani Agatha AdmIalentlan onn Approved OMB No. 21200020 Office MeMification J cc& 7 /49/ 4 - 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 PROT969. 1421). Failure to report can result in a ivil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1058). I. Aircraft Make RAYTHEON AIRCRAFT Model 400A Serial No. RIC-244 USA N793TA 2. Owner Name (As shown on registration certificate) KETTLER ROBERT, MICHELS PIPELINE CONSTRUCTION INC, SOUTHEASTERN MII,LS INC, REI AIR LLC, El-AL Maus 101 S WEBB RD WICHITA ICS 67207-1315 4. Unit Identifleadon S. Type Unit Make Model Said No. Repair Alteration AIRFRAME (As described In Item I above) X POWERPLANT PROPELLER APPLIANCE 'rape Manufacturer A. Agencts Name and Address RAYTHEON AIRCRAFT SERVICES 1115 PAUL WILIUNS ROAD SAN ANTONIO TEXAS 78216 usCaracas:a Wavle CRS-XA14605K LIMITED AIRFRAME FonaseCerdneasedMechatie X Carer:mod Repos Sienna mamaceurer 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 nude in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulatio s and that the information famished herein is true and correct to the best of my Imowledge. Date 12-10-01 Siviature of Authorized Individual MONTY CARROLL /1.---C ---9 BY Pursuant to the authority given persons specified below, the unit identified Administrator of the Federal Aviation Administration and is in item 4 was inspected 'n the manner prescribed by the 0 REJECTED El APPROVED FAA Flt. Standuds Inspector Manufacturer Other (Smelly) FAA Designee x Repair Station Canada Airworthiness Grove 12-10-01 Certificate or Daismation No. CRS-XA14605K Signature of Authorized Individual ye ir MONTY CARROLL FAA Form 337 (1248) PROT765 EFTA_00242233 PROT408 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. (If:nonspace is required attach additional skteu. Men* with aircraft nationality and registration mark and dale work completed) MAKE: RAYTHEON 400A S/N: RK-244 REG: N793TA DATE: 12-10-01 ALL SEVEN CABIN SEATS AND THE LAVATORY SEAT WERE FIREBLOCKED IN ACCORDANCE WITH FAR 25.853 (a) APPENDIX F PART I (a) (1) (ii) AND FAR 25.853 (c) APPENDIX F PART II AMENDMENT 25.83. THE FIREBLOCK1NG WAS ACCOMPLISHED IN ACCORDANCE WITH THE SKANDIA INC. TEST PLAN 48335 REV. IR DATED 12-04-01, REFERENCE THE FORM 8110-3 DATED 12-04-01 APPROVED BY DONNA J. PARRISH, DESIGNATED ENGINEERING REPRESENTATIVE, HDERY-410100-CE, STRUCTURAL SPECIAL. SEE THE FORM 8110-3 DATED 10-09-01 AS REFERENCE FOR THE FIREBLOCKING FLAMMABILITY TEST RESULTS OF THE SEATS THAT WAS PREVIOUSLY TESTED AND APPROVED ON THE SKANDIA INC TEST PLAN 48118 REV. IR. DATED 10-01-01 FOR P/N 8118-1 AND 8118-2 ONLY, APPROVED BY DONNA J. PARRISH, DESIGNATED ENGINEERING REPRESENTATIVE, IMERY-410100-CE, STRUCTURAL SPECIAL. END * US. GOVERNMENT HUNTING OFFICE: 1992-769412160157 PROT766 EFTA_00242234 PROT409 Cr 01.ficurtentl (Airframe, Powerplant, Propeller, or Appliance) ol Trutuortatint Fettraihrtatice Adminittraara Form Approved OMB No.2120-0020 For FAA We Only Office kleMificatiat Is .5-'1 9 &- INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-I (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 PROT970. 1421). Failure to report can result in a ivil penalty not to exceed 51,000 for each such violation (Section 901 Federal Aviation Act of 19581 I. Aircraft 'Make RAYIHEON AEICRAFT Model 400A Serial No. MC-244 USA N793TA 2- Owner Name (As:holm on registration certificate) RETTLER ROBERT, MICHELS PIPELINE CONSTRUCTION INC, SOUIREASTEItN MILLS INC, RE1 AIR LLC, ET-AL Address 101 S WEBB RD WICHITA KS 67207-1315 3. For FAA Uso Only 5. Type Unit Make Model Serial No. Repair Altentio-i AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Par Manufacturer A. Agency's Name and Addrest RAYTHEON AIRCRAFT SERVICES 1115 PAUL WIL1CINS ROAD SAN ANTONIO TEXAS 78216 U.S. Certificated Mechanic CRS4CA14605K LIMITED AIRFRAME RADIO CLASS 1,11, III X Certificated RegokSrafioa Mazdaceate D. I certify that the repair and/or alteration nude to the unit( ) identified in item 4 above and described on the reverse or attachments hereto have been nude in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the infomution furnished herein is Mlle and correct to the best of my knowledite. Date 12-10.01 MONTY CARROLL BY Pursuant to the authority given perso s specified below, the unit identified Administrator of the Federal Aviation Administration and is in item 4 was inspected 'n the manner prescribed by the APPROVED 0 REJECTED FAA Flt. Standards Inspector Manufactuner FAA Designee x Repair Station Canada Airworthiness Gmuo Date of Approval or Relation 12-10-01 Certificate or CRS4CA14605K MONTY CARROLL LW )e.e.r-arri FAA Form 337 OLIO PROT767 EFTA_00242235 PROT410 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. Wince space is repine; attach addifional shags. Aka* with aircraft nationality and registration nark and date work completed) MAKE: RAYTHEON 400A S/N: RK-244 REG: N793TA DATE: 12-10-01 MODIFIED THE EXISTING RIGHT HAND FORWARD GALLEY/CLOSET CABINET IN ACCORDANCE WITH THE RAYTHEON AIRCRAFT SERVICES DWG. #528-2526-001 REV. A DATED 07-27-00, REFERENCE THE FORM 8110-3 DATED 12-07-01 APPROVED KAMALA J. MEADER, DESIGNATED ENGINEERING REPRESENTATIVE, #DERT-405126-CE, STRUCTURAL. THE MODIFICATION CONSISTED OF INSTALLING ELECTRICAL PROVISIONS FOR A MAPCO, CUP HOLDERS AND LIGHTING IN THE FORWARD SECTION OF THE BAGGAGE CABINET. THE ELECTRICAL WIRING FOR THE GALLEY/CLOSET CABINET WAS INSTALLED IN ACCORDANCE WITH THE RAYTHEON AIRCRAFT SERVICES DWG. #RAS-73-0112 REV. IR DATED 12-05.01, REFERENCE THE FORM 8110-3 DATED 12-07-01 APPROVED BY ROBERT M. HURLEY, DESIGNATED ENGINEERING REPRESENTATIVE, #DERT-710137-SW, SYSTEMS AND EQUIPMENT. THE MODIFIED GALLEY/CLOSET CABINET HAS A NEW WEIGHT OF 84.5 Lbs. AND A MOMENT OF 12844.0. THE WEIGHT AND BALANCE FORM AND THE EQUIPMENT LIST HAVE BEEN REVISED AND BOTH FORMS HAVE BEEN INSERTED IN THE AIRCRAFT FLIGHT MANUAL. END Additional Sheets An Attached * US. GOVERNMENT PRINTING OFFICE: 1992.769-012/60W PROT768 EFTA_00242236 PROT411 • CO VS.Department (Airframe, Powerplant, Propeller, or Appliance) et Tonspotutlea Federal Astatba itendelstrallea orm Approved OMB Na 2120-0020 Office Ideoglication --5c-"/ 2 )42., 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 PROT971. 1421). Failure to report can result in a ivil penalty not to exceed 81,000 for each such violation (Section 901 Federal Aviation Act of 19581 1. Aircraft Make RAYTHEON AIRCRAFT Model 400A Serial No. RK-244 USA N793TA 2. Owner Name ICEITLER ROBERT, MICHELS PIPELINE CONSTRUCTION INC, SOUTHEASTERN MILLS INC, REt AIR LLC, ET-AL Address 101 S WEBB RD WICHITA KS 67207-1315 3. For FAA Use 0 ly 4. Unit Identificadon S. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described In Item I above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer A. Agencys Name and Address RAYTHEON AIRCRAFT SERVICES 1115 PAUL WILKINS ROAD SAN ANTONIO TEXAS 78216 U.S. °vacua Mechanic CRS-XA14605K LIMITED AIRFRAME Fon* Catilkated Mechanic x Califtla Rep* Sudoo mmucra set D. 1 certify that the repair and/or alteration made to the twigs) 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 Imowledge. Data 12-10-01 Signature of Authorized bidividual MONTY CARROLL 1 ce't BY Pursuant to the authority given persons specified below, the unit identified Administrator of the Federal Aviation Administration and is in item APPROVED 4 was inspected in the manner prescribed by the M REJECTED FAA FR- Standards Inspector Manufacturer FAA Designee x Repair Station Date of Approval or Medico 12-10-01 Certificate or Decimation No. CRS-XA14605K Signature of Authorized Individual " 1 .....4 40..27, MONTY CARROLL FAA Form 337 0240 SDNY_Gbl_0275531 5 EFTA_00242237 PROT412 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. (If mon space it royuirect attach additional shear. lan), with aircraft nationality and regtswation mark and dale work completed.) MAKE: RAYTHEON 400A SIN: RK-244 REG: N793TA DATE: 12-10-01 FABRICATED AND INSTALLED A NEW THE LIFE VEST CONTAINER IN THE TOILET CABINET IN ACCORDANCE WITH THE RAYTHEON AIRCRAFT SERVICES DWG. #562-3832-001 REV. M. DATED 08-22-00, REFERENCE THE FORM 8110-3 DATED 12-07-01 APPROVED BY KAMALA J. MEADER, DESIGNATED ENGINEERING REPRESENTATIVE, IIDERT-405126-CE, STRUCTURAL. THE LIFE VEST CONTAINER WAS FABRICATED USING AAR COMPOSITES FLAT NOMEX PANEL PIN ATR-FP-25 I F2, REFERENCE THE FORM 8110-3 DATED 07-01-99 APPROVED BY JUDY BOGGS, DESIGNATED ENGINEERING REPRESENTATIVE, #CHI-410, STRUCTURAL SPECIAL. THE MODIFICATION OF THE CONTAINER WAS FOR THE INSTALLATION OF A NEW EASTERN AERO MARINE LIFE VEST, P/N P01074-113. THE WEIGHT CHANGE IS NEGLIGIBLE. THE EQUIPMENT LIST HAS BEEN REVISED TO REFLECT THE NEW LIFE VEST AND HAS BEEN INSERTED IN THE AIRCRAFT FLIGHT MANUAL. ❑X Additional Sheets Are Attached * US. GOVERNMENT PRINTING OFFICE: 1992-769-012/60157 SDNY_Gtv1_02 75531 6 EFTA_00242238 PROT413 1 e US Ccpartronl of Tr-lun en (Airframe, Powerplant, Propeller, or Appliance) reden,Avation AderlMstran Form A OMB pproved No. 2120.0020'. S officeoisx.firgbo th".2. grv-2 INSTRUCTIONS: Print or typo all entries. See FAR 43.9 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 PROT972. 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 RAYTHEON Model 400A Serial No. RK-244 N793TA 2. Owner Name (As shown on registra(ion certificate) AIRCAP LLC 101 S WEBB RD WICHITA, KS 67207-1315 3. For FAA Use On y THE DATA IDENTIFIED HEREIN COMPLIES WITH APPUCAB AIRWORTHINESS REQUIREMENTS THE ABOVE DESCRIBED AIRCRAFT SU CT TQ C NFO INSPECTION BY A PERSON APR 0 4 2000 4 AND IS APPROVED ONLY FOR AUTHORIZED IN FAR 43.7 DATE FAA INSPECTOR DPA-FSDO 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Rem 1 above) X POWERPLANT PROPELLER APPLIANCE Typo Manufacturer Elliott Aviation P. O. Box 100, Quad City Airport Moline, IL 61266-0100 U.S. Certified Mechanic CGHR812C Foreign Certified Mechanic X Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit( ) 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 [truncated]