# N8653A: 2014 Boeing 737-8H4 - Status: Valid registration - Airframe: [Boeing 737-8H4](https://openairdocs.org/model/boeing-737-8h4) (registry code 138440A, 143 seats) - Engine: [CFM International CFM56-7B27E series](https://openairdocs.org/engine/cfm-international-cfm56-7b27e-series) (registry code 13078) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (The Boeing Company) (OpenAirDocs) - Serial number: 37037 - Year built: 2014 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 13, 2014 - Certificate issued: January 12, 2015 - Expires: January 31, 2028 - Mode S code: ABE42C - Registered owner: [Southwest Airlines Co](https://openairdocs.org/faa-owner/SOUTHWEST%20AIRLINES%20CO) - Location: [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas) - Owner type: Corporation - Owner's area on the map: 32.8326° N, 96.8491° W: Placed by OpenAirDocs at the center of ZIP code 75235, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8653A - Page: https://openairdocs.org/aircraft/N8653A From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every CFM International CFM56-7B27E model are included. ## ADs that may apply (OpenAirDocs): 6 in force ### Matched by airframe (Boeing 737-8H4) None in force. ### Matched by engine (CFM International CFM56-7B27E series) - [AD 2023-05-05](https://openairdocs.org/ad/2023-05-05): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 98 more. Effective May 10, 2023 - [AD 2018-26-01](https://openairdocs.org/ad/2018-26-01): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jan 10, 2019 - [AD 2018-09-51](https://openairdocs.org/ad/2018-09-51): Engine · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 7, 2018 - [AD 2015-18-04](https://openairdocs.org/ad/2015-18-04): 73-tooth gearshaft located in the engine accessory gearbox (AGB) · CFM International CFM56-3, CFM56-7B20, CFM56-7B20/2 and 47 more. Effective Oct 20, 2015 - [AD 2015-04-02](https://openairdocs.org/ad/2015-04-02): Dual engine thrust instability event · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Mar 31, 2015 - [AD 2009-11-02](https://openairdocs.org/ad/2009-11-02): HPC 4-9 spools · CFM International CFM56-2, CFM56-2A, CFM56-2B and 109 more. Effective Jun 23, 2009 ### Historical (superseded or no longer in force) - [AD 2021-10-09](https://openairdocs.org/ad/2021-10-09) (historical): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 82 more. Effective Jun 24, 2021 - [AD 2018-18-01](https://openairdocs.org/ad/2018-18-01) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Oct 16, 2018 - [AD 2018-10-11](https://openairdocs.org/ad/2018-10-11) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 1, 2018 - [AD 2018-09-10](https://openairdocs.org/ad/2018-09-10) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective May 14, 2018 - [AD 2013-26-01](https://openairdocs.org/ad/2013-26-01) (historical): Oil dynamic seal assembly · CFM International CFM56-3, CFM56-3B, CFM56-3C and 52 more. Effective Feb 3, 2014 ## Information bulletins (advisory) (1 in force) - [SAIB NE-08-17R3](https://openairdocs.org/saib/NE-08-17R3): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued May 28, 2014 - [SAIB NE-08-17R2](https://openairdocs.org/saib/NE-08-17R2) (historical): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued Mar 7, 2011 ## NTSB investigations None matched to N8653A. ## FAA accident and incident reports None matched to N8653A. ## Service difficulty reports (160, newest 50) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SWAA2026092916162](https://openairdocs.org/sdr/SWAA2026092916162), Sep 25, 2026: SIGN. UNSECURE. PASSENGER CABIN, CEILING EXIT SIGN UNSECURE. SECURED THE SIGN IAW AMM 33-51-01-960-802, STEP 3.C. (6) (E). - [SDR SWAA2026092988170](https://openairdocs.org/sdr/SWAA2026092988170), Sep 25, 2026: BATTERY PACK. INOPERATIVE. RIGHT AFT EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805, 21-23-03-000-801, & 21-23-03-400-802. - [SDR SWAA2026092907824](https://openairdocs.org/sdr/SWAA2026092907824), Sep 25, 2026: BATTERY PACK. INOPERATIVE. LEFT EMERGENCY EXIT LIGHT WAS INOPERATIVE. REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805, 21-23-03-000-801, & 21-23-03-400-802. - [SDR SWAA2026092935990](https://openairdocs.org/sdr/SWAA2026092935990), Sep 25, 2026: LIGHT. INOPERATIVE. EMERGENCY LIGHT AFT OF RT WTB FAIRING WAS INOPERATIVE. REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-00-710-801. TESTED OK. - [SDR SWAA2026092491186](https://openairdocs.org/sdr/SWAA2026092491186), Sep 10, 2026: BALANCE WEIGHT. OUT OF SEQUENCE. DURING WEIGHT AND BALANCE PROCEDURE OF ELEVATOR RT FOUND BALANCE, 1 EA ON BAY 2, 1 EA, 3 EA ON BAY 3, & 1 EA ON BAY 4. TASK CARD ACCOMPLISHED ON MULTI EA M-22-1 - [SDR SWAA2026092486702](https://openairdocs.org/sdr/SWAA2026092486702), Sep 10, 2026: BALANCE WEIGHT. OUT OF SEQUENCE. DURING WEIGHT AND BALANCE PROCEDURE OF ELEVATOR LT FOUND BALANCE WEIGHT 183A0210-15 (1 EA) ON BAY 4, 183A0210-14 (1 EA) AND 6953211-2 (2 EA) ON BAY 3, 183A0210- - [SDR SWAA2026092957301](https://openairdocs.org/sdr/SWAA2026092957301), Sep 4, 2026: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL BTWN BS 400 - 420, STR 26L. REPLACED THE INTERCOSTAL IAW SRM 51-10-02, ITEM 9, AND FASTENERS IAW SRM 51-40-02, & DWG 143A7505, SHEET 151, RE - [SDR SWAA2026092999840](https://openairdocs.org/sdr/SWAA2026092999840), Aug 27, 2026: ANGLE. CORRODED. CORROSION ON LOWER ANGLE, BS 767 - 787, RBL 21, WL 155.3. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 146A8123, SHEET 16, REV-. - [SDR SWAA2026092440445](https://openairdocs.org/sdr/SWAA2026092440445), Aug 27, 2026: PLATE. CRACKED. CRACKED CORRUGATED PLATE, IRSS 216 RT WING T/R. REPLACED THE CORRUGATED PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 115A2781, SHEET 2, REV B. - [SDR SWAA2026092488382](https://openairdocs.org/sdr/SWAA2026092488382), Aug 27, 2026: PLATE. DAMAGED. ELONGATED HOLE ON CORRUGATED PLATE LOCATED ORSS 320 TRAILING EDGE, RT WING. REPLACED CORRUGATED PLATE, DID NOT FIND ALLOWABLE DAMAGE LIMITS IN SRM 57-51-02-1A-1 - [SDR SWAA2026092917117](https://openairdocs.org/sdr/SWAA2026092917117), Aug 26, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 500I, STR 28L. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7902, SHEET 320, REV-. - [SDR SWAA2026092973065](https://openairdocs.org/sdr/SWAA2026092973065), Aug 26, 2026: WEB. CRACKED. CRACKED WEB TRAILING EDGE PANEL, RT WING, ORSS 266. REPLACED THE WEB AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 115A2512, SHEET 16, REV-. - [SDR SWAA2026092956153](https://openairdocs.org/sdr/SWAA2026092956153), Aug 26, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, RT WING, ORSS 261. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 115A2512, SHEET 13, REV- . - [SDR SWAA2026092933487](https://openairdocs.org/sdr/SWAA2026092933487), Aug 26, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, ORSS 271, RT WING. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, AND DWG 115A6200, SHEET 17, REV A. - [SDR SWAA2026092956067](https://openairdocs.org/sdr/SWAA2026092956067), Aug 26, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE AT THE FIXED TRAILING EDGE PANEL, ORSS 261, LT WING. REPLACED THE SUPPORT ANGLE IAW RM 51-10-02, PARAGRAPH 9, SRM 51-40-02, DWG 115A2512, - [SDR SWAA2026092959991](https://openairdocs.org/sdr/SWAA2026092959991), Aug 25, 2026: ACCESS PANEL. CRACKED. CRACKED HORIZONTAL STAB ACCESS PANEL 343CB. REPLACED THE ACCESS PANEL IAW SRM 51-10-02, ITEM 9, 51-40-02, & DWG 185A1702, SHEET 19, REV F. - [SDR SWAA2026092431706](https://openairdocs.org/sdr/SWAA2026092431706), Aug 25, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE ON ACCESS PANELS 834DZ AT THE AFT ENTRY DOOR. REPLACED THE SUPPORT ANGLE ON ACCESS PANELS 834DZ IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DR - [SDR SWAA2026092490877](https://openairdocs.org/sdr/SWAA2026092490877), Aug 25, 2026: SUPPORT WEB. CRACKED. CRACKED SUPPORT WEB INBD FAN COWL, LT ENGINE. REPLACED FASTENERS & SUPPORT WEB ON THE INBOARD FAN COWL IAW SRM 51-40-02, SRM 51-10-02, & 71-13-30, PAGE 10094. - [SDR SWAA2026092457388](https://openairdocs.org/sdr/SWAA2026092457388), Aug 25, 2026: PLATE. DAMAGED. ELONGATED HOLE ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 282 AT LT WING. EVALUATED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 282 LT WING AND DID NOT FIND - [SDR SWAA2026092432884](https://openairdocs.org/sdr/SWAA2026092432884), Aug 25, 2026: PLATE. DAMAGED. ELONGATED HOLE ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 226 AT LT WING. EVALUATED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 226 AT LT WING AND NOT FOUND - [SDR SWAA2026092996069](https://openairdocs.org/sdr/SWAA2026092996069), Aug 24, 2026: WEB. CRACKED. CRACKED SHIELD WEB, BTWN BS 767 - 787, STR 25R. REPLACED THE SHIELD WEB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 146A0081, SHEET 49, REV A. - [SDR SWAA2026092919174](https://openairdocs.org/sdr/SWAA2026092919174), Aug 24, 2026: FITTING. CRACKED. CRACKED FITTING, BS 947.5, STR 26L. REPLACED THE FITTING IAW SRM 51-40-02, AND DWG 149A8103, SHEET 8, REV- . - [SDR SWAA2026092411897](https://openairdocs.org/sdr/SWAA2026092411897), Aug 24, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BTWN BS 380 - 400, RBL 40, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A5400, SHEETS 140,& - [SDR SWAA2026092434571](https://openairdocs.org/sdr/SWAA2026092434571), Aug 24, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BTWN BS 380 - 400, LBL 13, WL 208.1. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 143A5400, SHE - [SDR SWAA2026092415163](https://openairdocs.org/sdr/SWAA2026092415163), Aug 24, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BTWN BS 380 - 400, LBL 50, WL 208.1. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02, 51-10-02, ITEM 9, & DWG 143A5400, SHEET 1 - [SDR SWAA2026092459556](https://openairdocs.org/sdr/SWAA2026092459556), Aug 24, 2026: SUPPORT BRACKET. CRACKED. CRACKED SUPPORT BRACKET, BS 540 AIR CONDITIONING DUCT AT LOWER FUSELAGE LT SIDE. REPLACED THE SUPPORT BRACKET FOR AIR CONDITIONING DUCT AT LOWER FUSELAGE LT SID - [SDR SWAA2026092974826](https://openairdocs.org/sdr/SWAA2026092974826), Aug 23, 2026: ACCESS PANEL. ELONGATED. ELONGATED HOLE ON ACCESS PANEL 542EB, FLAP SUPPORT FAIRING 3, LT WING. REPAIRED THE ACCESS PANEL 542EB ON FLAP SUPPORT FAIRING 3 IAW SRM 51-70-04-2R-9, REPAIR 9 - [SDR SWAA2026092947026](https://openairdocs.org/sdr/SWAA2026092947026), Aug 21, 2026: WEB. CRACKED. CRACKED WEB, BTWN BS 927 - 947.5, STR 26R. REPLACED THE WEB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 147A7500, SHEET 36, & 37, REV-. - [SDR SWAA2026092992864](https://openairdocs.org/sdr/SWAA2026092992864), Aug 21, 2026: FLOORBEAM. CRACKED. CRACKED FLOORBEAM, BS 270, BTWN BL 0 - LBL 1, WL 208.1. REPAIRED THE TRANSVERSAL BEAM IN THE FLT COMPARTMENT IAW EA 26-153-02313, EA 26-153-02313-WIP1, AND EA 2 - [SDR SWAA2026092916099](https://openairdocs.org/sdr/SWAA2026092916099), Aug 21, 2026: SUPPORT BRACKET. CRACKED. CRACKED SUPPORT BRACKET, BS 727, BL 0, WL 163. REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 144A2600, SHEET 1084, REV-. - [SDR SWAA2026092915974](https://openairdocs.org/sdr/SWAA2026092915974), Aug 21, 2026: TIE CLIP. CRACKED. CRACKED TIE CLIP, BS 277, STR 10R. REPLACED THE TIE CLIP IAW SRM 51-40-02, AND DWG 141A1110, SHEET 55, REV -. - [SDR SWAA2026092995959](https://openairdocs.org/sdr/SWAA2026092995959), Aug 21, 2026: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BS 867 AT LEVEL STR 27L AT AFT CARGO COMPARTMENT. REPLACED SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 149A8102, - [SDR SWAA2026092491395](https://openairdocs.org/sdr/SWAA2026092491395), Aug 21, 2026: ACCESS PANEL. DELAMINATED. DELAMINATED EXTERNAL SKIN ACCESS PANEL 191CL. REPAIRED EXTERNAL SKIN ACCESS PANEL 191CL IAW SRM 51-70-04-2R-1 REPAIR 1. - [SDR SWAA2026092433515](https://openairdocs.org/sdr/SWAA2026092433515), Aug 21, 2026: FRAME. CRACKED. CRACKED FRAME, BS 312, BTWN STR 5L - 6L. REPAIRED THE FRAME IAW M-22-153-01244. - [SDR SWAA2026092491559](https://openairdocs.org/sdr/SWAA2026092491559), Aug 20, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, FWD FACE, BS 695, LBL 1, WL 208.1. REPLACED THE SUPPORT ANGLE LOCATED FWD FACE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 273A9111, SH - [SDR SWAA2026092429167](https://openairdocs.org/sdr/SWAA2026092429167), Aug 20, 2026: SEAT TRACK. CORRODED. CORRODED SEAT TRACK, BOTTOM SURFACE, BS 727F + 13 INCHES, RBL 24.75, WL 208.1. REMOVED THE DAMAGE & EVALUATED REWORK ON SEAT TRACK IAW SRM 53-00-52-1A-1, STEP 4 - [SDR SWAA2026092411677](https://openairdocs.org/sdr/SWAA2026092411677), Aug 20, 2026: FLOOR PANEL. DELAMINATED. DELAMINATION ON TOP SKIN OF FLOOR PANEL 231KF. REPAIRED THE FLOOR PANEL 231KF IAW SRM 53-00-50-2R-7, REPAIR 7. - [SDR SWAA2026092472284](https://openairdocs.org/sdr/SWAA2026092472284), Aug 20, 2026: CROSSBEAM. CRACKED. CRACKED BRAKE PANEL LOCATED BS 540 BTW BL 0 - LBL 24.75, WL 208.1. REPLACED THE BRAKE PANEL IAW SRM 51-40-02, AND DWG 143A0060, SHEET 64, REV- . - [SDR SWAA2026092407246](https://openairdocs.org/sdr/SWAA2026092407246), Aug 20, 2026: SEAT TRACK. CORRODED. CORROSION SEAT TRACK LOCATED BTW BS 540 - 727B, WL 208, LBL 45.5, CROWN AREA BOTTOM SURFACE (4 E/A). REMOVED DAMAGE AND EVALUATED REWORK AREA IAW SRM 53-00-52-1 - [SDR SWAA2026092476359](https://openairdocs.org/sdr/SWAA2026092476359), Aug 20, 2026: FLOORBEAM. CORRODED. CORRODED FLOORBEAM, BS 986.5, RBL 43, WL 208.1 IN THE AFT GALLEY AREA. REPAIRED THE FLOORBEAM, IAW SRM 53-70-51-2R-6, REPAIR 6. - [SDR SWAA2026092455644](https://openairdocs.org/sdr/SWAA2026092455644), Aug 20, 2026: SEAT TRACK. CORRODED. CORRODED SEAT TRACK, BOTTOM SURFACE, BS 727 + 13 INCHES, RBL 24.75, WL 208.1. REMOVED DAMAGE AND EVALUATED REWORK AREA BOTTOM SURFACE LOCATED BS 727 + 13 INCHES - [SDR SWAA2026092415985](https://openairdocs.org/sdr/SWAA2026092415985), Aug 20, 2026: SEAT TRACK. CORRODED. CORRODED SEAT TRACK BTW BS 727B - 887, WL 208, RBL45.5 CROWN AREA BOTTOM SURFACE, (5 EA). REMOVED DAMAGE AND EVALUATED SEAT TRACK LOCATED BTW BS 727B - 887, WL - [SDR SWAA2026092416069](https://openairdocs.org/sdr/SWAA2026092416069), Aug 20, 2026: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK BOTTOM SURFACE LOCATED BS 500F PLUS 10 INCHES RBL 24.75 WL 208.1 AT PASSENGER CABIN. REMOVED DAMAGE AND EVALUATED REWORK AREA BOTTOM SUR - [SDR SWAA2026092916176](https://openairdocs.org/sdr/SWAA2026092916176), Aug 19, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 440, STR 26L. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A7505, SHEET 152, REV-. - [SDR SWAA2026092935972](https://openairdocs.org/sdr/SWAA2026092935972), Aug 19, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 400, STR 26L. REPLACED THE ANGLE & FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DRAWING 143A7505, SHEET 151, REV A. - [SDR SWAA2026092451667](https://openairdocs.org/sdr/SWAA2026092451667), Aug 19, 2026: ACCESS PANEL. ELONGATED. ELONGATED HOLES ON ACCESS PANEL 561BB, LT WING. REPAIRED THE ACCESS PANEL 561BB IAW SRM 51-70-04-2R-10, REPAIR 10. - [SDR SWAA2026092411625](https://openairdocs.org/sdr/SWAA2026092411625), Aug 19, 2026: SKIN. CRACKED. CRACKED INNER CHORD, BS 303.9, STR 17L. REPLACED BTWN BS 270 - 360, STR 17L IAW SRM 51-10-02, ITEM 9, INSTALLED FASTENERS IAW SRM 51-40-02 & DWG 142A0050, SHEET - [SDR SWAA2026092451051](https://openairdocs.org/sdr/SWAA2026092451051), Aug 19, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BTWN BS 291.5 - 294.5, STR 17R IN FWD GALLEY. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND 141A8310, SHEET 33, - [SDR SWAA2026092472212](https://openairdocs.org/sdr/SWAA2026092472212), Aug 19, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 661CB T / E, RT WING. REMOVED AND REPLACED THE ACCESS PANEL 661CB IAW SRM 51-70-04-2R-10, REPAIR 10. - [SDR SWAA2026092471077](https://openairdocs.org/sdr/SWAA2026092471077), Aug 19, 2026: PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 561AB AT LT WING. REPAIRED THE ACCESS PANEL 561AB IAW SRM 51-70-04-2R-10, REPAIR 10. All 160: https://openairdocs.org/aircraft/N8653A/reports.md ## STCs that may be installed (OpenAirDocs) (31) Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do. ### Approved for the airframe (Boeing 737-8H4) - [STC ST00555AT](https://openairdocs.org/stc/ST00555AT): Installation of Airshow 210 system. AIRCRAFT RECONFIG TECHNOLOGIES, LLC. Lists 737 Series - [STC SA4842SW](https://openairdocs.org/stc/SA4842SW): Modification of air to air heat exchanger (P/N 182820-2 Series 2). Honeywell International Inc. Lists 737 Series - [STC SA270NW](https://openairdocs.org/stc/SA270NW): Installation of modified seat. Aviation Technical Services. Lists 737 Series - [STC ST01162NY](https://openairdocs.org/stc/ST01162NY): Installation of Literature Pockets. Magee Plastics Company. Lists 737 Series - [STC SA2607SO](https://openairdocs.org/stc/SA2607SO): Installation of coffee maker P/N 416-1001-29. B/E Aerospace Inc. Lists 737 Series - [STC SA2608SO](https://openairdocs.org/stc/SA2608SO): Installation of rail assembly, P/N 416-0201-15. B/E Aerospace Inc. Lists 737 Series - [STC SA3058SO](https://openairdocs.org/stc/SA3058SO): Installation of coffee maker 416-0001-23 and rail assembly 416-0201-5. B/E Aerospace Inc. Lists 737 Series - [STC ST01476AT](https://openairdocs.org/stc/ST01476AT): Installation of coffee maker. B/E Aerospace Inc. Lists 737 Series - [STC ST01778AT](https://openairdocs.org/stc/ST01778AT): Installation of espresso maker p/n 3510-0066-01. B/E Aerospace Inc. Lists 737 Series - [STC SA629GL](https://openairdocs.org/stc/SA629GL): Installation of Grimes galley, Model 1545LW unit 2 and unit 4. B/E Aerospace. Lists 737 Series - [STC ST01332AT](https://openairdocs.org/stc/ST01332AT): Installation of Galley Service Carts. Champ International, Inc. Lists 737 Series - [STC ST09870SC](https://openairdocs.org/stc/ST09870SC): Installation of Mechanical Window Shades. Lou Martin & Associates. Lists 737 Series - [STC ST00033AT](https://openairdocs.org/stc/ST00033AT): Installation of a single Mode S system and provisions for a TCAS II system. General Aerospace, Inc. Lists 737 Series - [STC SA4532NM](https://openairdocs.org/stc/SA4532NM): Installation of Coltech, CTD-80 ATSCALL, enabling company calling of selected aircraft via company selected radio. Avtech Corporation. Lists 737 Series - [STC ST4532NM](https://openairdocs.org/stc/ST4532NM): Installation of Coltech CTD-80 ATSCALL, enabling company calling of selected aircraft via company selected radio. Avtech Corporation. Lists 737 Series - [STC ST00774NY](https://openairdocs.org/stc/ST00774NY): Installation of a passenger cabin Liquor/beverage service cart P/N E500170. (757-222) (767-222) (727-222) (737 SERIES 222, 291, 322, 522) (747-100 SERIES 238B). Driessen Aircraft Interior Systems USA, Inc. Lists 737 Series - [STC ST02052AT](https://openairdocs.org/stc/ST02052AT): Installation of a single Collins GNLU910A flight management system, along with global navigation satellite system sensor. General Aerospace, Inc. Lists 737 Series - [STC SA02034AT](https://openairdocs.org/stc/SA02034AT): Manufacture of tray carrier, P/N 2282-506. BFE Services. Lists 737 Series - [STC ST01968AT](https://openairdocs.org/stc/ST01968AT): Manufacture of inserts for galley stowage. JK Aerospace, Inc. Lists 737 Series - [STC SA01916AT](https://openairdocs.org/stc/SA01916AT): Manufacture of Tray Carrier P/N 1839-501. BFE Services. Lists 737 Series - [STC SA2534SO](https://openairdocs.org/stc/SA2534SO): Installation of window shades, acoustic panes and reveals. Magee Plastics Company. Lists 737 Series - [STC ST179CH](https://openairdocs.org/stc/ST179CH): Installation of cargo container curtain. Plastic Composites Corp. Lists 737 Series - [STC SA00056LA](https://openairdocs.org/stc/SA00056LA): Installation of Weber Coffeemaker, P/N 870130-415. Monogram Systems. Lists 737 Series - [STC SA6090NM](https://openairdocs.org/stc/SA6090NM): Installation of emergency vision assurance system (EVAS). VisionSafe Corporation. Lists 737 Series - [STC SA370NW](https://openairdocs.org/stc/SA370NW): Removal of passenger interior, installation of cargo compartment liners and cargo tie down equipment. Western Metal Products. Lists 737 Series - [STC SA2589CE](https://openairdocs.org/stc/SA2589CE): Install Bennetts Seat Converter Stowage Compartment on passenger seat(s). John's Aircraft and Upholstery. Lists 737 Series - [STC SA1029NW](https://openairdocs.org/stc/SA1029NW): Installation of a cargo system. Western Metal Products. Lists 737 Series - [STC SA1258EA](https://openairdocs.org/stc/SA1258EA): Installation of Cosco model78-( ) child restraint system. (172M S/N 17263459 - 17267584). Miller Stuart R. Lists 737 Series - [STC SA1052SO](https://openairdocs.org/stc/SA1052SO): Installation of GE battery P/N43B022RB36 in place of Marathon P/N CA-727-7, CA-727-20, or CA-27-20 batteries or SAFT P/N23180 batteries; or installation of GE battery P/N 43B020RB10 replacing Marathon P/N CA-727-7, CA-727-20 or CA-27-20 or SAFT P/N 23186 or 23180 batteries. General Electric Company. Lists 737 Series - [STC SA1082NW](https://openairdocs.org/stc/SA1082NW) (historical): Installation of auxiliary fuel tanks in the aft cargo compartment. (737 series -2K9A). Rogerson ATS. Lists 737 Series ### Approved for the engine (CFM International CFM56-7B27E series) - [STC SE04840NY](https://openairdocs.org/stc/SE04840NY): Installation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engine. Kilroy Aviation LLC ## Earlier aircraft with N8653A The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N8653A before. - [Cancelled 1953-08-04](https://openairdocs.org/deregistered/N8653A-1953-08-04): Beech A35, S/N D-2063. Owner: [Cummings A L M D](https://openairdocs.org/faa-owner/CUMMINGS%20A%20L%20M%20D), [Burbank, CA](https://openairdocs.org/faa-place/CA/Burbank) ## Related - Other Boeing 737-8H4 aircraft: https://openairdocs.org/model/boeing-737-8h4/aircraft.md - The CFM International CFM56-7B27E series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b27e-series.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.