# N8629A: 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: 36897 - Year built: 2014 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 6, 2014 - Certificate issued: May 28, 2014 - Expires: May 31, 2027 - Mode S code: ABD9D9 - 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=8629A - Page: https://openairdocs.org/aircraft/N8629A 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 N8629A. ## FAA accident and incident reports None matched to N8629A. ## Service difficulty reports (174, 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 SWAA2026100722692](https://openairdocs.org/sdr/SWAA2026100722692), Oct 3, 2026: LIGHT. UNSECURE. EXIT ROW LIGHT STRIP PULLED UP FROM CARPET ABEAM ROW 12ABC. SECURED THE FLOOR PROXIMITY PHOTO LUMINESCENT IAW AMM 33-51-15. - [SDR SWAA2026042391053](https://openairdocs.org/sdr/SWAA2026042391053), Apr 20, 2026: SIGN. LOOSE. OVERWING EXIT ROW EXIT SIGN LOOSE. RESECURED EMER EXIT SIGN IN REF TO AMM 33-51-01. - [SDR SWAA2026040183895](https://openairdocs.org/sdr/SWAA2026040183895), Mar 28, 2026: LIGHT. INTERMITTENT. MID-CABIN CEILING EXIT SIGNAGE LIGHT FLASHES INTERMITTENTLY. INSPECTED MID CABIN EMERGENCY EXIT LIGHT ASSY. AND FOUND OPERATION TO BE NORMAL IAW AMM 33-51-00. F - [SDR SWAA2026031270649](https://openairdocs.org/sdr/SWAA2026031270649), Feb 13, 2026: HANDLE. BROKEN. BROKEN ASSIST HANDLE DOOR LINING FWD ENTRY DOOR AT FWD GALLEY AREA 2EA. REPLACED ASSIST HANDLE DOOR LINING FWD ENTRY DOOR AT FWD GALLEY AREA 2EA IAW AMM-52-11-3 - [SDR SWAA2026031269986](https://openairdocs.org/sdr/SWAA2026031269986), Feb 12, 2026: BATTERY PACK. INOPERATIVE. BATTERY PACK LOCATED BETWEEN BS 559 & 578, RT SIDE IN PAX CABIN. REPLACED THE BATTERY PACK LOCATED BETWEEN BS 559 & 578 IAW AMM 33-51-06-960-805, STEP 4.E.(4) T - [SDR SWAA2026031269985](https://openairdocs.org/sdr/SWAA2026031269985), Feb 12, 2026: BATTERY PACK. INOPERATIVE. BATTERY PACK LOCATED BETWEEN STA 500C AND STA 500D RH SIDE IN PAX CABIN INOPERATIVE. REPLACED BATTERY PACK LOCATED BETWEEN BS 500C & 500D RT SIDE IN PAX CABIN I - [SDR SWAA2026031669862](https://openairdocs.org/sdr/SWAA2026031669862), Feb 11, 2026: ACCESS PANEL. CRACKED. CRACK SEAL PLATE ACCESS PANEL 441AT INBOARD POSITION RT PYLON. REPLACED SEAL PLATE ACCESS PANEL 441AT INBOARD POSITION RT PYLON IAW SRM 51-40-02 AND SRM 51-10-0 - [SDR SWAA2026031269861](https://openairdocs.org/sdr/SWAA2026031269861), Feb 11, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, ACCESS PANEL 551FB, LT WING. REPLACED THE SUPPORT ANGLE FOR ACCESS PANEL 551FB, LT WING IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 115 - [SDR SWAA2026031669457](https://openairdocs.org/sdr/SWAA2026031669457), Feb 10, 2026: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET LOCATED ON PNEUMATIC DUCT BS 540, LBL 6 IN AIR CONDITIONING BAY. PERFORMED INSPECTION OF DAMAGE ON SUPPORT BRACKET LOCATED BS 540 LBL 6 AT - [SDR SWAA2026031669622](https://openairdocs.org/sdr/SWAA2026031669622), Feb 10, 2026: NUT PLATE. CORRODED. CORROSION ON RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS548 AT LT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS548 AT L - [SDR SWAA2026031669455](https://openairdocs.org/sdr/SWAA2026031669455), Feb 10, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 500I, STR 28R. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02 ITEM 9; SRM 51-40-02, AND DWG 143A7902 SHEET 320, REV -. - [SDR SWAA2026031669623](https://openairdocs.org/sdr/SWAA2026031669623), Feb 10, 2026: NUT PLATE. CORRODED. CORROSION ON RAIL NUT PLATE INTERNAL CAVITY LEADING EDGE LOCATED OFSS421 AT LT WING. REPLACED RAIL NUT PLATE INTERNAL CAVITY LEADING EDGE LOCATED OFSS421 AT LT - [SDR SWAA2026031669620](https://openairdocs.org/sdr/SWAA2026031669620), Feb 10, 2026: NUT PLATE. CORRODED. CORROSION ON RAIL NUT PLATE INTERNAL CAVITY LEADING EDGE LOCATED OFSS541 AT LT WING. REPLACED RAIL NUT PLATE INTERNAL CAVITY LEADING EDGE LOCATED OFSS541 AT LT - [SDR SWAA2026031669618](https://openairdocs.org/sdr/SWAA2026031669618), Feb 10, 2026: NUT PLATE. CORRODED. CORROSION ON RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS761 AT LT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS761 AT L - [SDR SWAA2026031669624](https://openairdocs.org/sdr/SWAA2026031669624), Feb 10, 2026: NUT PLATE. CORRODED. CORROSION ON RAIL NUT PLATE INTERNAL CAVITY LEADING EDGE LOCATED OFSS416 AT LT WING. REPLACED RAIL NUT PLATE INTERNAL CAVITY LEADING EDGE LOCATED OFSS416 AT LT - [SDR SWAA2026031669627](https://openairdocs.org/sdr/SWAA2026031669627), Feb 10, 2026: NUT PLATE. CORRODED. CORROSION ON RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS287 AT LT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS287 AT L - [SDR SWAA2026031669626](https://openairdocs.org/sdr/SWAA2026031669626), Feb 10, 2026: NUT PLATE. CORRODED. CORROSION ON RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS303 AT LT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS303 AT L - [SDR SWAA2026031369454](https://openairdocs.org/sdr/SWAA2026031369454), Feb 10, 2026: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 - 400, BL 0, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, AND DWG 143A5400, SHEET 154, REV-. - [SDR SWAA2026031369625](https://openairdocs.org/sdr/SWAA2026031369625), Feb 10, 2026: RAIL. CORRODED. CORROSION ON RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS411 AT LT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE IAW SRM 51-40-02-0G, - [SDR SWAA2026031369621](https://openairdocs.org/sdr/SWAA2026031369621), Feb 10, 2026: RAIL. CORRODED. CORROSION ON RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE, OFSS 578, LT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE IAW SRM 51-40-02-0G, & DWG 1 - [SDR SWAA2026031369461](https://openairdocs.org/sdr/SWAA2026031369461), Feb 10, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 663 RBL 36. REPLACED THE ANGLE IAW SRM 51-10-02-0G-0, ITEM 9, AND DWG 111A1000, SHEET 331, REV A . - [SDR SWAA2026031669325](https://openairdocs.org/sdr/SWAA2026031669325), Feb 9, 2026: PLATE. CRACKED. CRACK CORRUGATED PLATE LOCATED TRAILING EDGE IRSS 217 AT RT WING. REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE IRSS 217 AT RT WING IAW SRM 51-40-02-0G-0, SRM - [SDR SWAA2026031669319](https://openairdocs.org/sdr/SWAA2026031669319), Feb 9, 2026: SUPPORT BRACKET. CRACKED. CRACK ON SUPPORT BRACKET LOCATED TRAILING EDGE ORSS 273 AT RIGHT. REPLACED SUPPORT BRACKET LOCATED TRAILING EDGE ORSS 273 AT RT WING. IAW SRM 51-40-02, SRM-51-1 - [SDR SWAA2026031369055](https://openairdocs.org/sdr/SWAA2026031369055), Feb 9, 2026: BRACKET. CRACKED. CRACKED BRACKET FOR ACCESS PANEL 834DZ, ON AFT ENTRY DOORS. REPLACED THE BRACKET IAW SRM 51-40-02, SRM 51-10-02, ITEM 9,0 & DWG 411A2119, SHEET 72, REV -. - [SDR SWAA2026031369326](https://openairdocs.org/sdr/SWAA2026031369326), Feb 9, 2026: ANGLE. CORRODED. CORRODED ANGLE, BS 500I, LBL 22 - RBL 22, WL156. REPLACED THE ANGLE IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02, DWG 143A9481, SHEET 14, REV -, & DWG 143A7902, - [SDR SWAA2026031369324](https://openairdocs.org/sdr/SWAA2026031369324), Feb 9, 2026: TIE CLIP. CRACKED. CRACK TIE CLIP, BS 500I, STR 26R. REPLACED THE TIE CLIP AND FASTENERS IAW SRM 51-40-02-0G-0, & DWG 143A1234, SHEET 14, REV A. - [SDR SWAA2026031369057](https://openairdocs.org/sdr/SWAA2026031369057), Feb 9, 2026: RAIL. CORRODED. CORROSION ON RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS571 AT RT WING. RE-INSTALLED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE IAW SRM 51-40-02 - [SDR SWAA2026031269322](https://openairdocs.org/sdr/SWAA2026031269322), Feb 9, 2026: SHIELD. CORRODED. CORROSION SHIELD WEB LOCATED BETWEEN BS 492 - 500A, RBL 22, WL156. FWD CARGO BAY. REPLACED SHIELD WEB AND FASTENERS IAW SRM 51-40-02-0G AND DWG 143A0080 SHEET 3 - [SDR SWAA2026031668956](https://openairdocs.org/sdr/SWAA2026031668956), Feb 8, 2026: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA. REPLACED SUPPORT ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL ST - [SDR SWAA2026031668954](https://openairdocs.org/sdr/SWAA2026031668954), Feb 8, 2026: FRAME. CRACKED. CRACKED FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA. REPAIRED THE FRAME IAW EA M-22-153-01244. - [SDR SWAA2026031368955](https://openairdocs.org/sdr/SWAA2026031368955), Feb 8, 2026: TIE CLIP. CRACKED. CRACKED TIE CLIP, BS 277, STR 10R. REPLACED THE TIE CLIP AND FASTENERS IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, DRAWING 141A1110, SHEET 55, REV-, - [SDR SWAA2026031369046](https://openairdocs.org/sdr/SWAA2026031369046), Feb 8, 2026: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE, BS 380 - 400, LBL 13, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, SRM 51-10-02, ITEM 9, & DWG 143A5400, SHEET 184, REV-. - [SDR SWAA2026031369052](https://openairdocs.org/sdr/SWAA2026031369052), Feb 8, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 867, LBL 10. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, PARAGRAPH 9, & DWG 149A8102, SHEET 19, REV A. - [SDR SWAA2026031369047](https://openairdocs.org/sdr/SWAA2026031369047), Feb 8, 2026: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 - 400, LBL 52, WL 208.1. REPLACED SUPPORT ANGLE IAW SRM 51-40-02-0G-0, SRM 51-10-02, ITEM 9, AND DWG 143A5400 SHEET 18 - [SDR SWAA2026031269045](https://openairdocs.org/sdr/SWAA2026031269045), Feb 8, 2026: ACCESS PANEL. CRACKED. CRACKED ACCESS PANEL 544BB, LT WING. REPAIRED THE ACCESS PANEL 544BB IAW EA 26-157-00484. - [SDR SWAA2026031269050](https://openairdocs.org/sdr/SWAA2026031269050), Feb 8, 2026: SHIELD. CORRODED. CORRODED SHIELD WEB BETWEEN BS 767 - 794.3, RBL 22, WL 156. REPLACED SHIELD WEB IAW SRM 51-40-02-0G-0, & DWG 146A0081, SHEET 49, REV A. . - [SDR SWAA2026031268957](https://openairdocs.org/sdr/SWAA2026031268957), Feb 8, 2026: SUPPORT BEAM. CRACKED. CRACKED SUPPORT BEAM NR 4, FWD GALLEY DOOR. REPLACED SUPPORT BEAM IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DRAWING 141A6516, SHEET 142, REV-. - [SDR SWAA2026031269051](https://openairdocs.org/sdr/SWAA2026031269051), Feb 8, 2026: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BETWEEN BS 727C - 747, RBL 21, WL156 IN THE AFT CARGO BAY. REPAIRED SUPPORT ZEE IAW SRM 51-40-02, SRM 53-00-53-2R-6, REPAIR 6, FIG - [SDR SWAA2026031169049](https://openairdocs.org/sdr/SWAA2026031169049), Feb 8, 2026: KEELBEAM. CRACKED. CRACKED KEELBEAM BETWEEN BS 727 - 727A, STR 27R, AFT CARGO BAY. PERFORMED REPAIR ON KEELBEAM BTWN BS 727 - 727A, STR 27R IAW EA 26-153-00444 AND 26-153-00444 WI - [SDR SWAA2026031668572](https://openairdocs.org/sdr/SWAA2026031668572), Feb 7, 2026: NUT. CORRODED. CORROSION ON RAIL NUT LOCATED OSS 146.43 BETWEEN OSS 160.30 ON LH WING. REPLACED NEW RAIL NUT LOCATED OSS 146.43 BETWEEN OSS 160.30 ON LH WING. - [SDR SWAA2026031668573](https://openairdocs.org/sdr/SWAA2026031668573), Feb 7, 2026: NUT. CORRODED. CORROSION ON RAIL NUT LOCATED OSS 126.72 BETWEEN OSS 140.92 AT LH WING. REPLACED NEW RAIL NUT IAW SRM 51-40-02-0G. - [SDR SWAA2026031668579](https://openairdocs.org/sdr/SWAA2026031668579), Feb 7, 2026: NUT PLATE. CORRODED. CORROSION ON RAIL NUT LOC OSS 93.30 BETWEEN OSS 106.65, LT WING. REPLACED NEW RAIL NUT LOC APROX OSS 93.30 BETWEEN OSS 106.65 ON LH WING SEE TTG8Q01A8AB5 STEP 5 - [SDR SWAA2026031668580](https://openairdocs.org/sdr/SWAA2026031668580), Feb 7, 2026: NUT PLATE. CORRODED. CORROSION ON RAIL NUT LOCATED OSS113.18 BETWEEN OSS 118.65 AT LT WING. REPLACED NEW RAIL NUT LOCATED OSS113.18 BETWEEN OSS 118.65 AT LH. WING SEE TTG8Q01A8AB5. - [SDR SWAA2026031668753](https://openairdocs.org/sdr/SWAA2026031668753), Feb 7, 2026: WEB. CRACKED. CRACK ON WEB INBD FAN COWL ON ENGINE 1 2026-112370<[01] REPLACED WEB ON INBD FAN COWL ON ENGINE 1 IAW SRM 51-40-02-0G-0 AND CMM 71-13-30, REV 32, PAGE 10092. - [SDR SWAA2026031268587](https://openairdocs.org/sdr/SWAA2026031268587), Feb 7, 2026: SCUFF PLATE. CRACKED. CRACKED FWD CORNER SCUFF PLATE, IN THE AFT CARGO BAY. REPAIRED THE FWD CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975. - [SDR SWAA2026031268586](https://openairdocs.org/sdr/SWAA2026031268586), Feb 7, 2026: SCUFF PLATE. CRACKED. CRACK ON AFT CORNER SCUFF PLATE LOC AFT CARGO BAY. REPAIRED THE AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975. - [SDR SWAA2026031668561](https://openairdocs.org/sdr/SWAA2026031668561), Feb 6, 2026: CROSSBEAM. CRACKED. CRACK ON BRAKE PANEL LOCATED BS 540 BTW BL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN. REPLACED BRAKE PANEL LOCATED BS 540 BTW BL 0 TO LBL 24.75 WL 208.1 AT PAS - [SDR SWAA2026031668560](https://openairdocs.org/sdr/SWAA2026031668560), Feb 6, 2026: CROSSBEAM. CRACKED. CRACK ON BRAKE PANEL LOCATED BS 540 BTW BL 0 TO RBL 24.75 WL 208.1 AT PASSENGER CABIN. REPLACED BRAKE PANEL LOCATED BS 540 BTW BL 0 TO RBL 24.75 WL 208.1 AT PAS - [SDR SWAA2026031668427](https://openairdocs.org/sdr/SWAA2026031668427), Feb 6, 2026: FLOORBEAM. CORRODED. CORROSION ON FLOOR BEAM, BS 947.5 LBL 24 WL 208.1. REPAIRED IAW SRM 53-70-51-2R-5, REPAIR 5, AND EA 26-153-00448 AND EA M-24-153-02022. - [SDR SWAA2026031668205](https://openairdocs.org/sdr/SWAA2026031668205), Feb 6, 2026: SEAT TRACK. CRACKED. CRACK ON SEAT TRACK FWD INBOARD OF CAPTAIN SEAT IN COCKPIT. REPLACED SEAT TRACK FWD INBOARD OF CAPTAIN SEAT IN COCKPIT IAW AMM 25-11-11-400-801 INSTALLATION WIL All 174: https://openairdocs.org/aircraft/N8629A/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 N8629A The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N8629A before. - [Cancelled 1998-02-18](https://openairdocs.org/deregistered/N8629A-1998-02-18): Enstrom Helicopter 480, S/N 5023. Owner: [Enstrom Helicopter Corporation](https://openairdocs.org/faa-owner/ENSTROM%20HELICOPTER%20CORPORATION), [Menominee, MI](https://openairdocs.org/faa-place/MI/Menominee) ## 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.