# N8632A: 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: 60082
- Year built: 2014
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 1, 2014
- Certificate issued: June 26, 2014
- Expires: June 30, 2027
- Mode S code: ABDC9B
- 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=8632A
- Page: https://openairdocs.org/aircraft/N8632A

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 N8632A.

## FAA accident and incident reports

None matched to N8632A.

## Service difficulty reports (163, 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 SWAA2026091706067](https://openairdocs.org/sdr/SWAA2026091706067), Sep 13, 2026: INLET. CRACKED. OTS-#2 ENGINE INLET COWL CRACKED_ VERIFIED CRACK AND MARKED ENDS. CRACK MEASURES 3.0IN LONG. REF NDT PART 6 51-00-00. PROCEDURE 23. REMOVED AND REPLACED #2 ENG 
- [SDR SWAA2026082410417](https://openairdocs.org/sdr/SWAA2026082410417), Aug 18, 2026: LIGHT. DAMAGED. PHOTOLUMINESCENT STRIP HAS INTERNAL MOISTURE AT CENTER ISLE R/H ROW 1-2. PHOTOLUMINESCENT STRIP REMOVED AT RT CENTER ISLE AND DRIED MOISTURE IAW AMM 33-51-15.
- [SDR SWAA2026050494009](https://openairdocs.org/sdr/SWAA2026050494009), Apr 30, 2026: FLOORBEAM. CRACKED. CRACK SUPPORT ANGLE FLOOR STRUCTURE BS 695 AND RBL 1. REPLACED SUPPORT ANGLE FLOOR STRUCTURE BS 695 AND RBL 1 AT PASSENGER CABIN IAW SRM 51-40-02; SRM 51-10-02 
- [SDR SWAA2026050489288](https://openairdocs.org/sdr/SWAA2026050489288), Apr 15, 2026: WEB. CRACKED. CRACK ON WEB LOC. ON FWD CARGO COMPARTMENT BTW STA 500G TO 500H STRING ER 26L. REPLACED WEB LOC. ON FWD CARGO COMPARTMENT BTW STA 500G TO 500H STRING ER 26L IAW
- [SDR SWAA2026050487670](https://openairdocs.org/sdr/SWAA2026050487670), Apr 8, 2026: FLOORBEAM. DAMAGED. ELONGATED HOLE ON CLIP LOC. ON FLOORBEAM WEB 947.5 LBL 24.5 WL 208.1 AFT GALLEY AREA AT PASSENGER CABIN. REPLACED CLIP AND FASTENERS LOC. ON FLOOR BEAM WEB 947.
- [SDR SWAA2026050495355](https://openairdocs.org/sdr/SWAA2026050495355), Apr 8, 2026: FLOORBEAM. DAMAGED. ELONGATED HOLE ON CLIP LOC. ON FLOORBEAM WEB 947.5 LBL 24.5 WL 208.1 AFT GALLEY AREA. REPLACED CLIP AND FASTENERS LOC. ON FLOOR BEAM WEB 947.5 LBL 24.5 WL 208.1
- [SDR SWAA2026050485195](https://openairdocs.org/sdr/SWAA2026050485195), Mar 31, 2026: ACCESS PANEL. CRACKED. CRACK LEADING EDGE RIB ACCESS PANEL 331B LOCATED LE STA 123.85 AT LT HORIZONTAL STABILIZER. REPLACED RIB ACCESS PANEL 331B LOCATED LE STA 123.85 AT LT HORIZONTA
- [SDR SWAA2026050485070](https://openairdocs.org/sdr/SWAA2026050485070), Mar 31, 2026: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED AT LEVEL ORSS 270 DEFLECTION CONTROL RIB AREA RT WING. REPLACED SUPPORT ANGLE LOCATED AT LEVEL ORSS 270 DEFLECTION CONTROL RIB AR
- [SDR SWAA2026050484620](https://openairdocs.org/sdr/SWAA2026050484620), Mar 30, 2026: ANGLE. CRACKED. CRACK ON ANGLE LOCATED AFT FACE BS 500I AT LEVEL STR 28L AT FWD CARGO COMPARTMENT. REPLACED ANGLE AND FASTENERS LOC. AFT FACE BS 500I AT LEVEL STR 28L AT FWD CA
- [SDR SWAA2026050495351](https://openairdocs.org/sdr/SWAA2026050495351), Mar 30, 2026: ANGLE. CRACKED. CRACK ON ANGLE LOCATED AFT FACE BS 500I AT LEVEL STR 28L AT FWD CARGO COMPARTMENT. REPLACED ANGLE AND FASTENERS LOC. AFT FACE BS 500I AT LEVEL STR 28L AT FWD CA
- [SDR SWAA2026050484621](https://openairdocs.org/sdr/SWAA2026050484621), Mar 30, 2026: ANGLE. CRACKED. CRACK ON ANGLE LOCATED AFT FACE BS 500I AT LEVEL STR 28R AT FWD CARGO COMPARTMENT. REPLACED ANGLE LOCATED AFT FACE BS 500I AT LEVEL STR 28R AT FWD CARGO COMPART
- [SDR SWAA2026050484747](https://openairdocs.org/sdr/SWAA2026050484747), Mar 30, 2026: PLATE. CRACKED. CRACK ON CORRUGATED PLATE AT LEVEL ORSS 295 TRAILING EDGE AT LT WING. REPLACED CORRUGATED PLATE AT LEVEL ORSS 295 TRAILING EDGE AT LT WING IAW SRM 51-40-02; SRM
- [SDR SWAA2026050484380](https://openairdocs.org/sdr/SWAA2026050484380), Mar 29, 2026: SUPPORT. CORRODED. CORROSION LOWER SILL, BS 440 TO 492.4 RBL 20 TO RBL 28 WL156 FWD CARGO BAY. REPLACED LOWER SILL LOC. BTW STA 440 TO 492.4 RBL 20 TO RBL 28 WL156 FWD CARGO COMPA
- [SDR SWAA2026050495350](https://openairdocs.org/sdr/SWAA2026050495350), Mar 29, 2026: ANGLE. CRACKED. CRACK ON ANGLE LOCATED BS867 AND LBL11 WL156 AT AFT CARGO COMPARTMENT. REPLACED ANGLE AND FASTENERS LOCATED BS867 AND LBL11 WL156 AT AFT CARGO COMPARTMENT I.A.W
- [SDR SWAA2026050484475](https://openairdocs.org/sdr/SWAA2026050484475), Mar 29, 2026: ANGLE. CRACKED. CRACK ON ANGLE LOCATED BS867 AND LBL11 WL156 AT AFT CARGO COMPARTMENT. REPLACED ANGLE AND FASTENERS LOCATED BS867 AND LBL11 WL156 AT AFT CARGO COMPARTMENT I.A.W
- [SDR SWAA2026050484478](https://openairdocs.org/sdr/SWAA2026050484478), Mar 29, 2026: INTERCOSTAL. CORRODED. CORROSION ON WEB INTERCOSTAL LOCATED BETWEEN BS 747 TO 767 AND RBL 23 WL156 AT AFT CARGO COMPARTMENT FAULT RESOLVED ON OTHER FAULT TTG8Q01BATYS.
- [SDR SWAA2026050184379](https://openairdocs.org/sdr/SWAA2026050184379), Mar 29, 2026: WEB. CORRODED. CORRODED SHIELD WEB, BETWEEN BS 767 - 787, RBL 23, WL 156 IN THE AFT CARGO BAY. REPLACED THE SHIELD WEB AND FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 146A0081, S
- [SDR SWAA2026050184477](https://openairdocs.org/sdr/SWAA2026050184477), Mar 29, 2026: WEB. CRACKED. CRACKED WEB, BETWEEN BS 927 - 947, RBL 21, WL 156 IN THE AFT CARGO BAY. REPLACED THE WEB IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, STEP 9, AND DWG 147A7500, SHE
- [SDR SWAA2026043084377](https://openairdocs.org/sdr/SWAA2026043084377), Mar 29, 2026: SUPPORT. CORRODED. CORRODED SUPPORT ZEE, BTWN BS 727I - 767, RBL 23, WL 156 IN THE AFT CARGO BAY. REPLACED ZEE CHANNEL SIDEPLATE, SPLICE SIDEPLATE, STRAP SPLICE AND FASTENERS BTWN
- [SDR SWAA2026043084386](https://openairdocs.org/sdr/SWAA2026043084386), Mar 29, 2026: SUPPORT. CORRODED. CORRODED SUPPORT ZEE BTWN BS 727G - 787, LBL 23, WL 156 IN THE AFT CARGO BAY. REPAIRED THE SUPPORT ZEE SECTION BTWN BS 727E + 10 INCHES - 847, LBL 23, WL 156. I
- [SDR SWAA2026050484107](https://openairdocs.org/sdr/SWAA2026050484107), Mar 28, 2026: TIE CLIP. CRACKED. CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA. REPLACED TIE CLIP LOC. BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B737-800 SRM 51-40-0
- [SDR SWAA2026050484102](https://openairdocs.org/sdr/SWAA2026050484102), Mar 28, 2026: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13 WL 208.1. REPLACED SUPPORT ANGLE AND FASTENER LOCATED BTW BS 380 TO BS 400 LBL 13 WL 208.1 AT PASSENG
- [SDR SWAA2026050495353](https://openairdocs.org/sdr/SWAA2026050495353), Mar 28, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13 WL 208.1. REPLACED SUPPORT ANGLE AND FASTENER LOCATED BTW BS 380 TO BS 400 LBL 13 WL 208.1 AT PASSENGE
- [SDR SWAA2026050484103](https://openairdocs.org/sdr/SWAA2026050484103), Mar 28, 2026: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 41 WL 208.1. REPLACED SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 41 APPROX WL 208.1 AT PASSENGER CAB
- [SDR SWAA2026050484106](https://openairdocs.org/sdr/SWAA2026050484106), Mar 28, 2026: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 51 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENER LOCATED BTW BS 380 TO BS 400 LBL 51 
- [SDR SWAA2026050495354](https://openairdocs.org/sdr/SWAA2026050495354), Mar 28, 2026: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 51 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENER LOCATED BTW BS 380 TO BS 400 LBL 51 
- [SDR SWAA2026050484110](https://openairdocs.org/sdr/SWAA2026050484110), Mar 28, 2026: FRAME. CRACKED. CRACKED FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA . PERFORMED REPAIR ON FRAME ON BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA IAW EA# M-22-
- [SDR SWAA2026043084212](https://openairdocs.org/sdr/SWAA2026043084212), Mar 28, 2026: STRAP. CORRODED. CORROSION ON LOWER STRAP, BTWN BS 787 - 794.3, RBL 19, WL 156 IN THE AFT CARGO BAY. REPLACED THE LOWER STRAP IAW SRM 51-10-02-0G-0, AND DWG 146A0081, SHEET 49, 
- [SDR SWAA2026050483937](https://openairdocs.org/sdr/SWAA2026050483937), Mar 27, 2026: WEB. CORRODED. CORRODED SHIELD WEB LOCATED BETWEEN STA 492.4 TO STA 500A AND RBL21 WL156 AT FWD CARGO COMPARTMENT. REPLACED SHIELD WEB AND FASTENERS AND RBL21 WL156 AT FWD CAR
- [SDR SWAA2026050495348](https://openairdocs.org/sdr/SWAA2026050495348), Mar 27, 2026: SHIELD. CORRODED. CORROSION SHIELD WEB LOCATED BETWEEN STA492.4 TO STA500A AND RBL21 WL156 AT FWD CARGO COMPARTMENT. REPLACED SHIELD WEB AND FASTENERS LOCATED BETWEEN BS 492.4 TO
- [SDR SWAA2026050483938](https://openairdocs.org/sdr/SWAA2026050483938), Mar 27, 2026: ANGLE. CRACKED. CRACKED ANGLE, STA500G AND STR26R FWD CARGO COMPARTMENT. REPLACED ANGLE CLIP AND FASTENERS LOCATED STA 500G AND STR26R FWD CARGO COMPARTMENT IAW SRM 51-10-02 IT
- [SDR SWAA2026050495349](https://openairdocs.org/sdr/SWAA2026050495349), Mar 27, 2026: ANGLE. CRACKED. CRACKED ANGLE, STA500G AND STR26R FWD CARGO COMPARTMENT. REPLACED ANGLE CLIP AND FASTENERS LOCATED STA 500G AND STR26R FWD CARGO COMPARTMENT IAW SRM 51-10-02 IT
- [SDR SWAA2026050483933](https://openairdocs.org/sdr/SWAA2026050483933), Mar 27, 2026: TIE CLIP. CRACKED. CRACK TIE CLIP LOCATED BS 500I AND STR26R FWD CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED STA500I AND STR26R FWD CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9; SRM
- [SDR SWAA2026050483940](https://openairdocs.org/sdr/SWAA2026050483940), Mar 27, 2026: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET LOCATED BS540 AT LEVEL LBL 6 AT LT AIR CONDITIONING BAYS. REPLACED SUPPORT BRACKET LOCATED BS 540 AT LEVEL LBL 6 AT LT AIR CONDITIONING BA
- [SDR SWAA2026050483935](https://openairdocs.org/sdr/SWAA2026050483935), Mar 27, 2026: SUPPORT. CRACKED. CRACK SUPPORT ZEE LOCATED BETWEEN STA500C TO STA500D AND LBL21 WL156 AT FWD CARGO COMPARTMENT. THE DAMAGE WAS REPAIRED PER SRM 53-00-53-2R-5 (REPAIR 5) AND EA M
- [SDR SWAA2026043083934](https://openairdocs.org/sdr/SWAA2026043083934), Mar 27, 2026: TIE CLIP. CRACKED. CRACKED TIE CLIP, BS 500I, S26L IN THE FWD CARGO BAY. REPLACED TIE CLIP LOCATED BS 500I, S26L IAW SRM 51-40-02, & DWG 143A1215, SHEET 157 - 158, REV - .
- [SDR SWAA2026043083936](https://openairdocs.org/sdr/SWAA2026043083936), Mar 27, 2026: SUPPORT. CORRODED. CORRODED SUPPORT ZEE, BTWN BS 500A - 500C, RBL 21, WL 156 IN THE FWD CARGO BAY. REPAIRED IAW SRM 53-00-53-2R-5, REPAIR 5, & EA M-22-153-01550.
- [SDR SWAA2026050483697](https://openairdocs.org/sdr/SWAA2026050483697), Mar 26, 2026: ACCESS PANEL. ELONGATED. ELONGATED HOLES ON ACCESS PANEL 193CR WING TO BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 193CR WING TO BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 5
- [SDR SWAA2026050483698](https://openairdocs.org/sdr/SWAA2026050483698), Mar 26, 2026: ACCESS PANEL. ELONGATED. ELONGATED HOLE ACCESS PANEL 194CR BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 194CR BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-04-2R-9 REPAIR 
- [SDR SWAA2026050483702](https://openairdocs.org/sdr/SWAA2026050483702), Mar 26, 2026: ACCESS PANEL. CRACKED. CRACKED SEAL BLADE ACCESS PANEL 333AB AT LT HORIZONTAL STAB. REPLACED SEAL BLADE ACCESS PANEL 333AB AT LT HORIZONTAL STAB IAW SRM 51-40-02-0G-0 AND SRM 51-10-02
- [SDR SWAA2026050483703](https://openairdocs.org/sdr/SWAA2026050483703), Mar 26, 2026: ACCESS PANEL. CRACKED. CRACKED SEAL BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STABILIZER. REPLACED SEAL BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STABILIZER IAW SRM 51-40-02 AND SRM 5
- [SDR SWAA2026050483699](https://openairdocs.org/sdr/SWAA2026050483699), Mar 26, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 561CB AT LT WING. REPAIRED ACCESS PANEL 561CB AT LT WING IAW SRM 51-70-04-2R-10 REPAIR 10.
- [SDR SWAA2026050483294](https://openairdocs.org/sdr/SWAA2026050483294), Mar 25, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLE ON ACCESS PANEL 192K AT LOWER. REPAIRED ACCESS PANEL 192K AT LOWER IAW SRM 51-70-04-2R-10 REPAIR 10.
- [SDR SWAA2026050483121](https://openairdocs.org/sdr/SWAA2026050483121), Mar 25, 2026: ANGLE. CRACKED. CRACK ANGLE, BS500G AT LEVEL STR26L FWD POSITION AT FWD CARGO COMPARTMENT. REPLACED ANGLE AND FASTENERS IAW SRM 51-10-02-0G-0 PARAGRAPH 9 SRM 51-40-02-0G-0 AND 
- [SDR SWAA2026050495343](https://openairdocs.org/sdr/SWAA2026050495343), Mar 25, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS500G AT LEVEL STR26L FWD POSITION AT FWD CARGO COMPARTMENT. REPLACED ANGLE CLIP AND FASTENERS LOC BS 500G AT LEVEL STR26L FWD POSITION AT FWD C
- [SDR SWAA2026050483122](https://openairdocs.org/sdr/SWAA2026050483122), Mar 25, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS500G AT LEVEL STR26L AFT POSITION AT FWD CARGO . REPLACED ANGLE - CLIP LOCATED BS500G AT LEVEL STR26L AFT POSITION AT FWD CARGO IAW SRM 51-10-0
- [SDR SWAA2026050483131](https://openairdocs.org/sdr/SWAA2026050483131), Mar 25, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS500H AT LEVEL STR26L AFT POSITION AT FWD CARGO COMPARTMENT. REPLACED ANGLE IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 143A7505; SHEET: 138;
- [SDR SWAA2026050483132](https://openairdocs.org/sdr/SWAA2026050483132), Mar 25, 2026: ANGLE. CRACKED. CRACKED GUSSET ANGLE LOCATED BS 500I AT LEVEL STR 21L AT FWD CARGO COMPARTMENT. REPLACED GUSSET ANGLE LOCATED BS 500I AT LEVEL STR 21L AT FWD CARGO COMPARTMENT 
- [SDR SWAA2026050483124](https://openairdocs.org/sdr/SWAA2026050483124), Mar 25, 2026: GUSSET. CRACKED. CRACK GUSSET LOCATED STA500I AND STR19R AT FWD CARGO COMPARTMENT. REPLACED GUSSET AND FASTENERS LOCATED BS 500I AND STR19R IAW SRM 51-10-02-0G-0 AND DWG 143A790
- [SDR SWAA2026050495344](https://openairdocs.org/sdr/SWAA2026050495344), Mar 25, 2026: GUSSET. CRACKED. CRACK GUSSET LOCATED STA500I AND STR19R AT FWD CARGO COMPARTMENT. REPLACED GUSSET AND FASTENERS LOCATED STA500I AND STR19R AT FWD CARGO COMPARTMENT IAW SRM 51-1

All 163: https://openairdocs.org/aircraft/N8632A/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 N8632A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N8632A before.

- [Cancelled 1953-10-28](https://openairdocs.org/deregistered/N8632A-1953-10-28): Beech A35, S/N D-2042. Owner: [Martin School Of Aviation](https://openairdocs.org/faa-owner/MARTIN%20SCHOOL%20OF%20AVIATION), [Santa Ana, CA](https://openairdocs.org/faa-place/CA/Santa%20Ana)

## 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

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