EFTA01326943.pdf

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 xtoz/tt/Aem REGISTRATION MARKS NUMBER Raytheon Aircraft N188TS Company 400A RK-244 Transport 5 AUTHORITY AND BASIS FOR ISSUANCE This airworthiness certificate is issued pursuant to 49 U.S.C. § 44704 and certifies that, as of the date of issuance, 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: -None- 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 FM REPRESENTATIVE DESIGNATION NUMBER R3/06/2014 Arnold Wolfe,(52:,s4? „ AL_. C,),V GL-25 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. 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 EFTA01326943  SDNY_GM_02754904 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 I 826 EFTA01326944  erra la 2, 204020 Ottarcedt RCN Maw Err SOWOIS 0 MAJOR REPAIR AND ALTERATION foe MA Use Only US Otooftrroft a Triespalatten (Airframe, Powerplant, Propeller, or Appliance) Federal ANSI AtiniMalereen INSTRUCTIONS: Print or type an entries. See Title 14 CFR §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 U.S.C. g44701). FaIn to repx1 can resultant:we penally lot each such violation. (49 U.S.C. 946301019 Nationality and Registration Mew Sent No. UNITED STATES / N188TS RK-244 1. Aircraft /flake Model Series RAYTHEON AIRCRAFT COMPANY 400A Name (As shoal en regatrarion csrtMcate) Address (As shown on nyistration CV:ea) Amen PO BOX 2218 2. owner THORAIR LLC 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. PAYTMONeetts./teONAWe me244 7 in AIRFRAME (As described M Item / show) POWERPLANT O nPROPELLER Typo APPLIANCE 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 355 RICHMOND ROAD Folio CellicM•11A•shanle C. Catificate No. Ph CLEVELAND as. OH 7 Crallaslad Rasa Saari a 44143 ea ," USA _ Crailuad Maintananos Oraarristion CRS#WC7R348J D. I certify DUI the repair anaor alteration made to the unas Warned In Plan 6 above and described on the reverse or attachments hereto have been made In accordance Wm the requremorks of Pad 43 al me U.S. Federal Aviation Regulatens and that the InfomiatIon furnished herein is true and correct to the best of my km i fid ar Extended TIMO0 SI Silkily I prir 14 CFR Put 43 / App. 8 Steven A. Watkins 10/04/2019 Punsuanl to the authority , vat for RMiletitillervice below. the wit in item 5 nnspected .n Inc manner prescribed by Inc Administrator of the Federal Adml end Is 1 eyed Rejected - FAA Ft Standards — Pence* Areemed by Camden Manufacturer Maintenance Organization Inspector Deporiereal al Ming:toe BY — MI Other (SPec4 FM Designee ✓ Repair Staler) neaten Authorization ._., Certi cat or SIgnaturaTM *Mud DesVation No CRS# • WC7R346J 7 / ---P---- ----- David Kerr 10/04/2019 FAA Form 337 (10/06) Page I SDNY_GM_02754905 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241827 EFTA01326945  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 SDNY_GM_02754906 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241828 EFTA01326946  U.S. DEPARTMENT OF TRANSPORTATION 1. DATE • 2. MARE FEDERAL AVIATIONPOMMSTRATION STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 1 MODEL NO. 4. TYPE Meal &pia Papaw. MO &NAME OF APPLICANT November 30, 2018 Textron Aviation N541000-004 Forebody Assy Nextant Aerospace LLC Cleveland, Ohio LIST OF DATA IL ICENTIREATION 7 TIRE NT-E0-1118-31 Engine Inlet Rivet Repair. Rev. IR November 29, 2018 ------ ---------- --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 "Appicabie Requirements." 2) This form constitutes FAA approval of as the engineering data necessary for substantiation of compliance to necessary requirements for the entire repair. • s PunPose 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) CFR 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 veMed by Senn of the AdmInIetralet end Pt manna MM co,20a4 end emtetione of spinning order 14 CM Pan la on few above end an ached inn illabtal a MVO ben eurrinod In scan:Ince et nalbtolietl teoceOns ale lowellocanolyMe nelleen teginimmla elInAlmomnies Sunders Used. o Recommend op/Novel of then dale I OW Trenrere 0 APProve then dela II. SIONATUREMICF DESIGNATED ENE4NEERND REpRESENTATNEMI 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 SDNY_GM_02754907 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241829 EFTA01326947  • • • SDNY_GM_02754908 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 I 830 EFTA01326948  • nextant aerospace //elimaaRel0 /AMU //RUJORN ENGINEERING ORDER EO t HM0.111841 I Title: Engine Inlet Rivet Repair ARTICLE DESCRIPTION fficlotWodl."401 Mast snomen:3 Team &Won 100A See Ramona —1 - 711—.....m...... Ds parpote ci lia 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 . maw •••••••••pithsoolleaan oar citeilluandllialt Oa erpaanapkid to dIatchomarim 10.6:4 let kip.* lerbibtred PeWoveliloistIsperesallos OYES ONO OYES 0 NZI OYES ONO OYES 0 PO OYES ONO Dom ON EOPpleconey Yed might. tudana. tad stremb. Writ ;stoma. Lowniant aorta ION dnledwa a Mc aempR MICR airtellisse pale OYES ONO MINOR •.....AP312 ...._ _• . Cal It El) be exargished bp:aped palm or elarbropereket? OYES O NO IMJOR MINOR Seism*? MeN,Meld INIWC9r•MONefedeinaltiness7 ta iis ONO Ones towns hiss Dap FMAlffl0VIL ION IS NAM 0 MCA 0 STC (NI STOWILA1 OYES ONO Elms O mo GENERAL IMIINIONSIO RPM I:O~RIvM Waft m RN Emise MitIM (TwINISbaw) esamstueepas IleSallainras 0 YES 0 NO 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 COa0ad By K. Ifenefripi ION/2019 , DbakInismdbyMir AWInd al P. Awhelam Pinkhas AYSIIMMOV MII..... , ION/2019 . eve 201t10010•1110 4CW Pas t 03 ram No. NT.EOOI IRIPA This Coconut Is Unconerolf*0 Ono Printed SDNY_GM_02754909 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241831 EFTA01326949  • • • SDNY_GM_02754910 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024 I 832 EFTA01326950  nextant aerospace • I Natinuato //NW //WOW E0 IfT.E0•1118-31 I Title: Engine Inlet Rivet Repair ENGINEERINGORDER PROCEDURES MN INAPUVO4 Fla Veually inspett the trgle Se! Sp and barrel la arty otw damaged, nisang et loose banners. 1 - II ao *Maw! draepandes are deteceet ecetnue MIWell IS C4101100 bib. - IIiaS36:444 descepron we rcte canted Nutt,* ABIOGDOCS ingetabIt / 1414 VisuallyAmpect ihe arra rotor a deined in Sub Task 724t-20420401 a/Inman Inlemelimel LYE MANTENAACE 144NUAL -F.144-34P III poem reaskin) 2 • IIno allialel dscrepaxies wa dettete4 COMMA at remints Sinai toot - Indto,. ones:* se MK COMMNubiaMyopia lonfospilica CO 3 Longs dareplilvatsMIMI, in Fgt., I and wornovkanplably dill cal to teak., tamale men'. makog sure not lo Sage,gin OrPIRIZIile Welt( kit pill Oit F'pacee be lidos alio wissirg Winn tor WY/ion albatrAlaxNat PR4CR3212-5.XX in lau of ncortai sold Nees MS2042104:64X 4. 4 - PinPern hobibyay 444 mop 13 IS nawbed *MO" at NOM. per Chanyt tenni CA.1015 '••tc., 4 • Disinvie be careel avie lieveiIx tie anus 13Isint slam Cheaytka cloosrent CA.1015 lag • Usip Os aianufullenea nasnandad inalahlte WIIntl tineimi 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 -80— _ LIMITATIONS Rene INSTRUCTIONS FOR CONTINUING AIRWORTHINESS RCA's) MowPt rairisike brredkepylonii MSS nulnlenence ranuat In pedal.*wis shdl Wein as iniceled in be simnel inanionwics mina °rowan 44444ofilipstkai pommel 42,4044• COMPLIANCE tIMPAR WW1 AfOVEMOIMNI)31 /MOMIOW MAIM ook4 GP aer 410 A no OTIAWalsOialla*MOESVR0ea..."0.6•100 N.1,88 7:5 itg 2.446/ OAT /i•14~' 1 CRS,WC7R346J fo/t/i1 • En Ma NT4041/R. A Paget d3 This Neuman. Uncontrolled Once Printed SDNY_GM_02754911 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241833 EFTA01326951  • • • SDNY_GM_02754912 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241834 EFTA01326952  nextant aerospace • II NSMASIID MOW //MORN EO k NT-E0-1118-31 Tttle: Ina Inlet Repair ENGINEERING ORDER I • Figure 1: Damaged Rivet Location on RH Engine Inlet Up (Typical Shown) • Form No. NT.E0-01 f Roy A P. 3 cI3 Thls Docua*nl Is Unconirollod Once Prmied SDNY_GM_02754913 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241835 EFTA01326953  • • • SDNY_GM_027.914 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241836 EFTA01326954  now, 21204020 Ibeeeee TnadneMetiew Es 501/201S 0 MAJOR REPAIR AND ALTERATION US Oen... MAIM OM/ al Tninportallon (Airframe, Powerplant, Propeller, or Appliance) foists, Avilitlaa AdministeSs INSTRUCTIONS: Print or typo all entries. See Title 14 CFR 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 U.S.C. §41701). Failure to report can result in a civil penalty for each such Nankin. (49 U.S.C. §46301(a)) Nationally and Registration Mak Serial No. UNITED STATES / N188TS RK-244 1. Aircraft !make Model Series RAYTHEON AIRCRAFT COMPANY 400A Name (As shown as registabon caracole) Address (As shown on roghbation certificate) Anus PO 80X 22i0 2. Owner THORAIR LLC VI SAPOUSXY saw OH 29 14$11 Cony VNITE0 STATES 3. For FAA Use Only 4. 5. Unit Idendfication Revak Alteration (Mt Make Model Serial No. ii pi AIRFRAME MYIIIIECOMIKOVIT CCIONIf (As Omaha in Man :above) RK-2.11 POWERPLANT PROPELLER Tee APPLIANCE Manaiaret 6. Conformity Statement A. Agency's Mane and Address B. KM of Agency Mao WOW,MAYEN U. S. Garaged Mechanic _j rasnasons, Ado.. 300110•00.1000 Foreign canelcated Mechanic C. Certificate No. oar CUEVEI/J0 Ss OH Z Centres:4 now Stinson 2* 411411 ow" WNW STATES C•finteled Mantionanca Oryanizaton CRS# WC7R346J II I codify Met the repair andlet eleretton made to In unigs bandied In MITI 5 above and described on the reverse or SttlidifTWES hereto have been made h =men* with the requirements of Pad 43 of the U.S. Federal Aviation Regttatkas and that Vie Information furnished Meath tme and eared le the ow et my ko0.04.106. Extended range bal Slonare/DetedAul .r .„,.. per 14 CFR Pad 43 ❑ App. B #4, Ryan M Landes 10/7/2019 7. proval for Return to Service Pursuant to the authority gNen person speeded below, the wit Wenrtil In hem 6 knpected In the mane( presorted by the Adrfilitistr atOr of the Federal ANation Administration and Is j Approved Relecied — FM Fe. Standards — Palmas Apiroved by Calm Manufachrer Maintenance Organization oepartmeni or Tramped Inspector —. BY — r ......., FM Designee 7 Repair Station Inspection Authorizalion (Spray) Cerlificat or SIgnatur died IndMduai Designation No. CRS# WC7R346J David Kerr 10/7/2019 FAA Form 337 (10/06) Page I SDNYGivi02754915 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241837 EFTA01326955  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 584-00-0001 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 584-00-0046 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 584-00-0050 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 584-00-0047 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 1=1Additional Sheets An Method FM Form 337 (10/06) Page 2 SDNY_GM_02754916 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024I838 EFTA01326956  athee.s.tanefistries /Department efrrampottalint I;21,11cationflivithirtrathn SupplementalType Cergficate Nailer. ST11216DS 7birenafrateivaedterBHE & Associates, Ltd. 12002 Warfield St. Suite 250 San Antonio, TX 78218 real per tbar at clap is the type juiptfintiefaffenagquad an' Me /inniations onaramennas dm:fitter specifiedSena 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 584-00-0001, 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 earnforappanniderrosoin in Oa unistsurmakrel, suspendedsnimiafrorora termination fate 4.r allientire andlisitify tendril-mi./Snuffing/tie falinnOnntion indinnairatiota Date of Application: February 9. 2018 Dam kcissucd: Daic or lase:mem Junc 24. 2018 Dow Am-acted: illy /Dinaion titfidunnistrotar 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 CFR 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 CFR 21.120). FAA Form 5110-2 (914) Page 1 o12 SDNY_GM_02754917 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241839 EFTA01326957  thuitiatatts°amnia apartment 17fransportathn FeafrativiattS/larministration Supplemental7)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): eauitraalit *mamaIrina: 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 CFR 21.1201. FAA Form 8110.2(5114) Paget Of 2 SDNY_GM_O2754918 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241840 EFTA01326958 DocuSign Envelope a CFB621313.543FE8-4C8D.A4E34461F9B213045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS FOR THE INSTALLATION OF ADS-B OUT ON PART 25 AIRCRAFT REPORT No. 584-00-0047 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 SDNY_GM_02754919 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241841 EFTA01326959 DocuSgn Envetope CFS82885-6FES4C8D-A4E3-5461F9820045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 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. 584-00-0047, Rev: D BHE & Associates, Ltd. Page 2 of 36 Red By VT.DRB. FSCM 471127. Sit 2 01 39, 201944.1a/f19 SDNY_GM_02754920 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00241842 EFTA01326960 DocuSign Envelope ID: CFI36211185-6FE8-4C8D-A4E3-5461F9820045 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS Record of Revisions , .. . . . . ... . .. . RevislOn . Approved Revision Number Description of change - . .s. • . ., .. — - . . - • , Date IR Innis] Release 5/9/18 MG Page 8, Section 1.1 revised transponder and GPS part numbers. A 6727/18 MG Page 10, Section 2 remove 'Flight Hours' horn Table 4 Page 4, Revised list of aircraft models in