EFTA01261592.pdf

cwa ne.2120402) neves Tweet wear el Ey S414011I fr US Dess-rrnm MAJOR REPAIR AND ALTERATION MA Um One of Tr systukn (Airframe, Powerplant, Propeller, or Appliance) Pram /Matron AthillnlitiliCOO INSTRUCTIONS: Mint or type as entries. See Tide 14 CFR §43.9. Part 43 Append; B, and AC 43.9-1 (or subsequent revision thereof) for instruceons and caposidon of Ws form. Ms report Is rewired by law µ9 U.S.C. §44701). Falun) to report can result in pen" for each such violation. (49U.S.C.§41001(a)) NadanalitY and Registrebon Mark Serial No. N727KB RK-260 1. Aircraft Make Model Sancta Beech 400A Name (As shown on registraton certincate) Address (As shown on registration certificate) 2. Owner PUMPJACK AVIATION LLC banns 1511 W EPA CA) Caoo. 91 Stab WY LA 026014203 Couruy USA 3. For FM Use Only 4. Type S. Unit Identification Repair Mention Unit Make Made( Serial No. both RX.410 O in AIRFRAME . (As described fn non? I above) O POWERPLANT O O O PROPELLER Type O APPLIANCE O stsmeaclunar 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency sere ShresiAter a Clones Moon 4 U. S. Ciellfirsiteci ~ado 1 Manufacturer we. Amino* ForrionCernacesso Mechanic C. Certificate No. orr SS Or KS Swoon SI 0117 convi 115A ms s; nence Organize:al 3437625 0. !entry that the repair and/or alteration made to the unit(s idenefled at tarn 5 above and described on the ravens or attachments hereto have been made in accordance with the requirements of Pan 43 c4 the U.S. Federal Aviation Regulations and that the information furnished heroin es bye and correct to ere bast of my knowledge. Extended range fuel 91 of horized Inctrvidual per t4 CFR Part 43 ❑ APP. B t -1q 4 020 7. Approval for Return to Simko Pursuant to the authority 9 ven persons specked below. the Unit identified in sera 5 wee inspected in the manner ;ascribed by the Administrator of me Federal Aviation Administration and is plApproved nitelectee FM FF. Standards Maintenance Organization Panora ApPreNed KY Canna" Manufacturer Department of Trooper Inspector BY Other (SpeCd4 FAA Designee Repair Station X Inspection AUtlailtrilial Certificate Cf 3437625 SigrultufWDEKEI of Authonzod Individual Designation No. a ff C'S I t i - 20/30 FAA Form 337 (10/06) Page I SDNY_GM_02758010 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244932 EFTA01261592  NOTICE Weight and balance or operating limitation changes shalt be entered in the appropriate aircraft Ward. An alteration must be COnwabble with all previous alterations to assure continued conformity MO the applicable airworthiness requirements. S. Descapdan of Work Accomplished (If more space is tallied. attach odoloons) 31100t3 Identify wen efroWt netiOneety end regiavellon mem end Wife *or* completed.) .4777101 •1420 Netionelty and Registration PAWS Dale Installed copilot windshield P/N: LA45AS31001-024, S/N: 10013 under STC no. ST018935WI. Weight and balance revision no factor. ClAddelonal Sheets An Attached FM Form 337 (10/06) Page 2 SDNY_GM_02758011 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244933 EFTA01261593  Fano Amend Meannic IRON Nods CAM No 2i20.4020 0 MAJOR REPAIR AND ALTERATION r30,2C07 u s Dea mmertemmintof (Airframe, Powerplant, Propeller, or Appliance Fos FAA Me Only moos *ewe Awnwaw INSTRUCTIONS. Print or type all entries Soo FAR 43.9. FAR 43 Append.% B. and AC 43.9-1 (or subsequent Rowe therocif) for mabuctions and discos/Son of tie limn. This nowt is required by ern (49 U S C 1421) Faikrra ki. report can result In CM pearly not to exceed x1.000 far tab such Waco (Section 901 Federal Anton Act 1958) Natonallty and Regisastion Mark N727KB WW1No RK-260 1. Aircraft Make Model Raytheon Aircraft Company 400A 1See. Name (Ai Mown on registration corterain) Moss, Awe) 2. Owner Flight Options .LLC Anson t PKWY Ct, wt. OH no USA 3. For FAA Use OW 4. Type E. Unit itiontincatlon Repair Maralke Unit Make MOW sone Number CI El AIRFRAME PM described In ;tern I above) POWERPLANT 0 0 0 0 PROPELLER Taw El El APPLIANCE mieuracam IL Conformity Statement A Agency's Name and Address B. KM of Arcot 0 U.S. Ceraficated Mechanic 0 IMenufacturer 0 Foreign Ceraicated Mechanc C. Certificate No. OH 0 CsnAcale0 Rose Staten Ma 0 Centime:0 MaIntonanCe OnoWitation CRS # VVC7R34SJ o made to the uni(s) Idwitlfied In Nam 5 atcre• and deleted on the reline or attaChmentS hatid0 have been made n aCCOrdatiOn wet the niquiromeras d Part 43 of Me U.S. Facet* Adam Repulsions and IoM Urbana/ion furnished herein is true and coned to the best of my ImoMedpe. Extended rano fuel MostireiDete al AtOorIzed Irdni3ual 14 CFR Pal 43 Wisea 0 Anton J. Koprivnik r 02/24/2020 7. Approval for Return ba Pursuant to the authority given persons maned below. the uM klenakid ii Rem 5 was Impacted in to manner presorted by the Admmotrator of ale Federal Aviation Adrnolinranal and is El rePROWO 0 REJECTED FM Fit Standards Parson Approwdl by Camden inspector Manutactutw Maintenance Orponitaton Department of Tranapon BY Meg SOW) FM Oesagnee X Repot staton Impecte Aultiorttabon A / Grant* or Sgricurelosto Of Author/ad Irendual oy z zz ,/' Desianatfon No CRS I VVC7R348.) An on J. Koprivnik 02/24/2020 FAA Fort 337 IOW SDNY_GIv102758012 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244934 EFTA01261594  SDNY_GM_02758013 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244935 EFTA01261595  NOTICE woof and balance or operating limitation changes shall be enteredin Me appropriate aircraft word. An alteration must be compatible with ailpievfous mentions to assure continued conformity with the applicable ainvorthiness requirements S. Description of Work Accomplished (ifmote space Is required, attach additional sheets Identity with *cab nationably and registration mark and date work completed) N727KB 02/24/2020 Nationality and Registration Mark Data This 337 is to correct the original Dated 01/04/2013. Corrected block ti I, Registration number from N746TA to N787TA and fills in the serial number to Ft/C-260. All other data is correct. Part I of 3 The Following Equipment was removed along with Associated Hardware. 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 6224189-002 Internal Compensation Unit ICU-85 622-6189-002 Internal Compensation Unit AHC-85E 622-9336.400 Attitude/Heading Computer AHC-85E 622-9336-400 Attitude/Heading Computer SDU-640B 622-9735-001 Sensor Display Unit SDU-6408 622-9735-001 Sensor Display Unit SDU-6408 622.9735-001 Sensor Display Unit DCP-5000 822-1028-011 Display Control Panel DCP-5000 822-1028-011 Display Control Panel ARP-851 622.9500-011 Altitude Reference Panel ARP-851 622.9500-011 Altitude Reference Panel AAP-851 822-0328-011 Altitude Awareness Panel AAP-851 822-0328-011 Altitude Awareness Panel CHP-850 622.7397-002 Course Heading Panel DBU-4100 822-0014-002 Data Base Unit DAU-650 622.9344.101 Data Acquisition Unit 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 (2) 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 EAdditional Sheets Are Attached Form 337 0046) SDNY_GM_02758014 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244936 EFTA01261596  SDNY_GM_02758015 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244937 EFTA01261597  NOTICE Weight end balance or operating limitation changes shag be entered In the appropriate aircraft record. An alteration must be compatible with allprevious alterations to assure continued conibmity with the applicable aimorthiness requirements S. Description of Work Accomplished (Ifmore space is required, attach additional sheets Identify with aircraft nationality and ragisfrabon mark end date work completed) N727KB 02/24/2020 Nationality and Registration Ma* Date Page 2 of 3 Installed the Following Equipment along with Associated Hardware. 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 fig IFIS) 6.5 60.83 ECU-3000 822-1200-998 File Server Unit (1st IFIS) 0.40 57.5 AFD-3010E 822-1753-416 Adaptive Flight Display 12.90 89.2 AFD-3010E 822.1753.416 Adaptive Flight Display 12.90 89.2 AFD-3010E 822-1753.416 Adaptive Flight Display 12.90 89.2 AFD-3010E 822-1753-416 Adaptive Flight Display 12.90 89.2 IMT-3010 822.1140401 AFD Mounting Rack 4.40 85.0 IMT-3010 822.1140-401 AFD Mounting Rack 4.40 85.0 IMT-3010 822-1140-401 AFD Mounting Rack 4.40 85.0 IMT-3010 822-1140-401 AFD Mounting Rack 4.40 85.0 10852301700 Fuel Quantity Conditioner 0.90 324 PC920-2A2000PH-2A1 Fuel Flow Conditioner 1.10 325 GPS-40005 822-2189-004 GPS 6.0 37 CI 429.200 GPS/XW Antenna 1.0 166.14 Amp Cluster N241100-002 DC Voltmeter 1.5 97.4 373.93.1501-1 Speed Switch x2 0.25 89.2 D8U-5010E 822-2215-202 Data ease Unit 1.60 134.5 PS-835D 501-1228-004 Power Supply 12.5 52.9 MMT•5000 822-1811-003 File Server Unit Rack 0.30 57.5 MMT-3010 822-1290-003 AHS Mounting Rack 1.80 57.5 MMT-3010 822.1290-003 AHS Mounting Rack 1.80 57.5 CHP-3010 822-1280-002 Course Heading Panel 1.30 92.5 Options Configuration Module OCM-4103 822.1463.228 0.30 57.5 WAAS/I.PV OCM4100 822.1463.228 Options Configuration Module 0.30 57.5 WAAS/tPV El AddlilOnil Shuts Ni Attar:hart Form 337 (won SDNY_GM_02758016 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00244938 EFTA01261598  SDNY_GM_02758017 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244939 EFTA01261599  NOTICE Weight and balance or operating Amitatlon changes shall be enteredin the vampish, airtualt record. M alteration must be canoe:Age wait at previous alterations ro assure continued calamity with the applicable einvorthiness requirements. 8. Description of Work Accomplished Ofmore specs is required, attach additional sheets, identify with aircraft natbnally and registration ma* and date yak completed.) N727KB 02/24/2020 Nationmay and Registration mark Date Page 3 of 3 Model Part Number Description Weight Arm CSU-4100 (2) 822-1364-002 Configuration Strapping Unit 1.60 55.7 MDC-3110 822.1987-006 Maintenance Data Computer 0.80 55.7 FMC-6000 (2) 822-0868-123 Flight Management Computer 1.90 55.7 ADC-850D (2) 822-0389-468 Air Data Computer 5.30 60.83 AMC-3000A (2) 822.1378-001 Attitude Heading Computer 4.80 57.5 DCP-3030 (2) 822.1828-002 Display Control Panel 1.90 89.96 PWR-4000 (4) 622-9945-022 IAPS Power Card 1.3 55.0 IOC-4100(4) 822.1362.511 Input/output Concentrator 0.8 55.0 XM WR-1000 822-2031-002 XM Weather 41.0 LT-4001-010 Master Caution Panel 1.3 87.0 Rev. Panel 373-91.3203-1 Pilot Reversion Panel 0.2 88.0 Rev. Panel 373.91.3203.3 Co-pilot Reversion Panel 0.2 88.0 9-PEG 373-91-3203-9 9-Pedestal Panel 1.8 92.89 345-6169 ELT Switch 0.2 88.0 Annunciator 2-F840233-I AUX BATT (1/2) Annunciator 0.05 88.0 Annunciator (2) 2-F840232-I Pull Up/ Terrain Annunciator 0.05 88.0 Annunciator 2-F840231-I TERR INHBT/ TERR Fall 0.05 88.0 In Accordance with SIC ST10959SC. See Attached Copy AFM Supplement, Nextant Aerospace Doc. No. 373-00-0023 Rev IR Dated 09/02/2011 or later FM approved revision, Installed on Aircraft. Equipment Pilot Guides are Installed in the Aircraft as Portable Document Format (.pdf) via supplied I-Pad. NOTE: Portable electronic devices used to store required aircraft records required by Part 91.9 are considered Electronic Flight Bags (EFB) per FAA Advisory Circular AC 120-768 par 4-g. Commercial operators are required to obtain authorization for their use from their managing Flight Standards District Office. Instructions for Continued Airworthiness (ICA) Ref Nextant Aerospace Document 373-00-0002.Rev C or Later are Included in the Aircraft Maintenance Records Carried out System Ground Test Plan 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. Aircraft Weighed see Report Dated 12/21/2012 ❑ Additonal Sheets Are Attached town 337 hoes) SDNY_GM_02758018 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00244940 EFTA01261600  SDNY_GM_02758019 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244941 EFTA01261601  Fan /wares (Yawn 'wiry Naas ONO PO 2, 10490 Metal MAJOR REPAIR AND ALTERATION 0 Fee MAIM 0.1. Js : v.:m.3,n cl "rvdp:cisi.., (Airframe, Powerplant, Propeller, or Appliance) Nam! anon Adrileilaatlen eNSTRUCTiCtiS: Pala w tyre all entnes See Tee 74 CFR 1.3.0. Pan 43 Appendix S. IS AC 13.91 (or subtentinni tensing' Pew!) be inStilietan and dillmalllon of Ws fern This report la required by law (49 U.S.C. §44701). Failure lo report can resutt in a civil penalty for OaCh such Vidalia,. (49 U.S.C. 946301(1)) Nationality and ReptilitIon Mark Serial No. USA N727KS RK-2S0 1. Micron Make uaaa Saes Raytheon Aircraft Company 4 Name (As shown on rep/groom contecale) Ad 2. Corner Co Nan MN. XT Leasing CO. LLC as 3. For FAA Use Only I The data identified herein complies with the applicable DALE E ••••••••••••••••••pos sinvoithiness requiremenu and ts approved for the above an desenbed aircraft, subject to oonfomilty Inspection by a person DRENCKHAHN """aa authorised in I4CFR 13.7 FAA Inspector MSP-FSDO•GLI5 4- WM & UMIldentlflealon Repair Minion Urn Make Model Serial No • RI AIRFRAME (4.5 deserts:f in kern 1above) 0 0 POIM1ERPtANT 0 0 PROPELLER Tape O APPLIANCE CI wanutaawar 4. Confonwity 91altenteril I 0 Kind of Agency U. S. Canes knorwrie I Menufedurin Falign Canicard Mahe* C. Catibleale NO. / CankaMORaork Simon I cartileand Malnwenos OrganiaMlon KX5R005N I ( ) Centime in awn el above antleemotied on ma reverse orattadtrnents hereto have been made in accordance with the repukemenla of Pert 43 of Me U.S. Federal Analog, Regulannte and that the information lurnnhed Wain Is bee and coned to Me best of my knowledge. Extended range Net Signature/Dele orMed Intivkluil pee 14 CFR Pan 43 O APO a /1-.2o ( f-^ l e .5- 7. Approval for Return to Service Pursuard to the eugmnty Yuen persons spec-Fed below. Me unit Identified in nem 5 was impeded in Ma manner pretabged by Admenstralor of me Federal Aviation Acknostiaten and is 2 Appienied 0 Rejected FAA Mt Standards Parkin AppeNed by tannin Manufacturer Maintenance COMnizabon Demotion ce Troweat Inspector SY OthW (SPonF)7 FAA Designee / Reba, Sleben Inspection Audit:enamel Ceatificalo or Sigratunut of Aulbeetzed tridrenualz , Designation NO KX5R005N --e---g-7..--dezn .... S^I )- 2o /i.-- FAA Form 337 rrcm. SDNY_GM_02758020 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244942 EFTA01261602  SDNY_GM_02758021 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244943 EFTA01261603  NOTICE Weight end balance or operating Mutation changes Shea be entered in the appropnale aircraft record An alteration must be COmpebblit with el previous *Aerations to assure continued conlomety whir the applicable airworthiness requirements. IL DewSart of Work Accomplished (Ifma were re reaaed each actitaned sheets leen* rani entre natfoneity end movie:Kra malt and date tarkCariplered) USA 14727 KI3 [ Nakielity and Realltretren Mark Date 1. Installed Gamin Automatic Dependant Surveillance-Broadcast (ADS-6) system referencing Elliott Aviation Technica Products Development Inc. drawings 121.3761-M0560.60 revision IR, and 121-4070-E0560-000 revision PA. A satisfactory ground test of the ADS-8 Out system was completed using a Aerofiek IFR-6000. checking for proper configuration and equipment performance requirements. The Installed ADS-B Out system has been shown to meet the equipment requirements of 14CFR 91.227. 2. The following LRU's are installed and interfaced referencing the previously approved equipment pairing of the GTX-3000 Mode '5' transponders and the GDL-88 Universal Access Transceiver by STC ST04214CH. a) Removed existing Rockwell Collins TOR-94D Mode "S" Transponders pin 622.9210-004. sin's 3MPD. and 6053 from right hand upper avionics shelf at sta 48. Installed two Gamin GTX-3000 Mode "S. Transponders (TSO-C112d), pin 011-01997-00, on right hand upper avionics shelf, s/n 20S008042 at sta. 49.7. and s/n 20S008050 at ste. 52.95. b) Installed a Garmin GDL-88 Universal Access Transceiver (TSO-C154c), p/n 010-00860-30. s/n 22U000700 on right hand upper avionics shelf at sta 46.95. The G0L-88 is connected to a GA-36 Antenna (TSO-C144), p/n 013-00244-00 s/n 14145 at sta. 128.7 through the GPS port and a UAT Antenna (TSO-C86c) p/n CI710.40.30. s/n 522354 at Ma. 35.1 for the FIS-B weather function. c) Installed a Garmin Flight Stream 110 (TSO-C157), p/n 010-01194-01. s/n 3G0000731 on the co-pilots manual holder at sta 136, interfaced to the GDL-88 UAT. The Flight Stream 110 provides FIS-B weather, ADS-B traffic, and GPS position data. 3. The FAA Approved Airplane Flight Manual Supplement for the Garmin Automatic Dependant Surveillance (ADS-B) Transponder installation ReporNumber FMS-4079-560 Revision IR, dated was placed in the Aircraft Flight Manual and must be available to the pilot at all times. 4. Structural work performed referencing the following: Elliott Aviation Technical Products Development Inc. drawing 121-3761-M0560-60 revision IR. Beechcraft Corporation Model 400/400A Maintenance Manual p/n 128-590001.9 Revision C29, Beechcraft Corporation Structural Repair Manual phi 128590001.17 Revision C16. and acceptable methods contained in AC43.13-1B. chapter 4, si.c.uon 4, and AC43.13-28, chapters 1,2,and 3. 5. The electrical interface of the Garmin Automatic Dependant Surveillance (ADS-8) Transponders was performed referencing Elliott Aviation Technical Products Development Inc. drawing 121-4070-E0560-000 revision PA. Wiring fabrication and interface performed in accordance with Beechcraft Corporation Beechjet 400/400A series wiring manual pin 128-590001-79 Revision 0, and acceptable practices contained in AC43.13.18, change 1, chapter 11. I 6. Weight and balance and equipment list have been revised to reflect this installation. 7. Instructions for Continued Airworthiness, Elliott Aviation Technical Products Development Inc Report ICA-4079-560 Revision IR , provided in aircraft records. END AOrlibcoad Sheets Are Attached FAA Form 337 imam SDNY_GM_02758022 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244944 EFTA01261604  SDNY_GM_02758023 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244945 EFTA01261605 41; Elliott Aviation Technical Products Development, Inc. el Report No.: ICA-4079- 60 6601 74m Ave Building A Revision IR Milan. IL 61264 ELLKYIT AVIATION Dated 05/01121 18 1 01 19 Instructions for Continued Airworthiness For Garmin ADS-8 System Installation Instructions for Continued Airworthiness For Garmin ADS-B Out System Installation (Type Certificate A16SW) 0 Z018 ELUOTT AVIATION TECHNICAL PRODUCTS DEVELOPMENT. INC. Elliott Aviation Technical Products Development. Inc. reserves the copyright of all information and illustrations in this publication which is provided in confidence and which may not be used for any purpose other than for which it was onginally supplied. The pubica - may not be reproduced in part or in whole without the consent in writing of Elliott Aviation Technical Products Development. Inc II SDNY_GM_02758024 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244946 EFTA01261606  SDNY_GM_02758025 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244947 EFTA01261607  • Elliott Aviation Technical Products Development Inc. Report No.: ICA-4079-660 6601 74" Ave Building A Revisi• : IR Milan, IL 61264 EWOT T AVIATION Dated 05/0112 8 2. 19 Instructions for Continued Airworthiness for Garin ADS•8 S tem Installation REVISIONS PAGE Rev Description Page (S) Date Approved By IR Initial Release ALL SDNY_GM_02758026 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244948 EFTA01261608  SDNY_GM_02758027 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244949 EFTA01261609  Elliott Aviation Technical Products Development. Inc. C7, Report No.: ICA-4079-560 6601 74m Ave Building A Revision: IR Milan, IL 61264 ELLIOTT AVIATION Dated 05/01/2018 3 of 19 Instructions for Continued Airworthiness For Garmin ADS-B System Installation TABLE OF CONTENTS COVER PAGE 1 REVISIONS PAGE 2 TABLE OF CONTENTS 3 Chapter 1 Introduction 4 Chapter 2 Maintenance Instructions and Shedules 6 Chapter 3 Access 13 Chapter 4 Lifting and Shoring 14 Chapter 5 Loving and Weighing 14 Chapter 6 Towing and Taxing 14 Chapter 7 Parking and Mooing 14 Chapter 8 Placards and Markings 14 Chapter 9 Servicing 14 Chapter 10 Air worthiness Limitations 15 Appendix A Al SDNY_GM_02758028 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00244950 EFTA01261610  SDNY_GM_02758029 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00244951 EFTA01261611  t:t 7 Elliott Aviation Technical Products Development. Inc. C=J Report No.: ICA-4079-i 60 6601 74" Ave Building A Revision IR Milan. IL 61264 ELLIOT T AVIATION Dated 05/01/2 18 4019 Instructions for Continued Airworthiness For Garmin ADS-B System Installation Chapter 1 INTRODUCTION 1.1 Scope/Purpose/Applicability/Distribution The Instructions for Continued Airworthiness (ICA) described herein are applicable only to RK-260 modified with Gamin ADS-8 System. These ICA desc