# N8624J: 2014 Boeing 737-8H4, registration cancelled 2026-02-09 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 9, 2026 - Exported to: Israel - Status when cancelled: Valid registration - Airframe: [Boeing 737-8H4](https://openairdocs.org/model/boeing-737-8h4) (registry code 138440A) - 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) (OpenAirDocs) - Serial number: 37004 - Year built: 2014 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 25, 2014 - Certificate issued: April 21, 2014 - Last registry action: January 22, 2023 - Mode S code: ABD932 - Owner when cancelled: [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 was based - The mark today: https://openairdocs.org/aircraft/N8624J - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8624J - Page: https://openairdocs.org/deregistered/N8624J-2026-02-09 From the FAA registry file of November 7, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Boeing 737-8H4: https://openairdocs.org/model/boeing-737-8h4.md ## Service difficulty reports (190, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SWAA2026020660566](https://openairdocs.org/sdr/SWAA2026020660566), Jan 12, 2026: BULB. BURNED OUT. CABIN OVERWING EMERGENCY LIGHTS HAVE BURNED OUT LIGHT BULBS. PERFORMED OPS TEST OF CABIN OVERWING EMERGENCY LIGHTS IAW AMM 33-51-00-710-801, TEST PASSED. - [SDR SWAA2026020660197](https://openairdocs.org/sdr/SWAA2026020660197), Jan 10, 2026: LIGHT. INOPERATIVE. EMERGENCY WINDOW LT SIDEWALL LIGHT INOPERATIVE. PERFORMED EXIT SIGNAL EMERGENCY WINDOWS LT SIDEWALL LIGHT OPS TEST IAW AMM 33-51-00-710-801, TEST PASSED. - [SDR SWAA2025123040480](https://openairdocs.org/sdr/SWAA2025123040480), Nov 28, 2025: TIE CLIP. CRACKED. CRACKED TIE CLIP, FWD FACE BS 500I, STRINGER 26L IN THE FWD CARGO BAY. REPLACED THE TIE CLIP IAW SRM 51-40-02, AND DWG 143A1234, SHEET 14, REV A. - [SDR SWAA2025122946834](https://openairdocs.org/sdr/SWAA2025122946834), Nov 28, 2025: TIE CLIP. CRACKED. CRACKED TIE CLIP, BS 500I, STRINGER 26L IN THE FWD CARGO BAY. REPLACED THE TIE CLIP IAW SRM 51-40-02, AND DWG 143A1234, SHEET 14, REV A. - [SDR SWAA2025123040382](https://openairdocs.org/sdr/SWAA2025123040382), Nov 27, 2025: TIE CLIP. CRACKED. CRACKED TIE CLIP FWD FACE BS 500I, STR 26R AT FWD CARGO BAY. REPLACED THE TIE CLIP AND FASTENERS IAW SRM 51-40-02, AND DWG 143A1234, SHEET 14, REV A. - [SDR SWAA2025123040385](https://openairdocs.org/sdr/SWAA2025123040385), Nov 27, 2025: ANGLE. CRACKED. CRACKED ANGLE AFT FACE BS 500H, STRINGER 26L IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02-OG-0, PARAGRAPH 9, AND DWG 143A7505, SHEET 137, REV -. - [SDR SWAA2025122940347](https://openairdocs.org/sdr/SWAA2025122940347), Nov 27, 2025: SHIELD. CORRODED. CORROSION ON SHIELD WEB LOCATED BTW BS 492.4 TO BS 500A RBL 23 WL 156.1 AT FWD CARGO COMPARTMENT. REPLACED SHIELD WEB AND FASTENERS LOCATED AT FORWARD CARGO COM - [SDR SWAA2025122946832](https://openairdocs.org/sdr/SWAA2025122946832), Nov 27, 2025: TIE CLIP. CRACKED. CRACK ON TIE CLIP LOCATED FWD FACE BS 500I AT LEVEL STR 26R AT FWD CARGO COMPARTMENT. REPLACED TIE CLIP AND FASTENERS LOCATED FWD FACE BS 500I AT LEVEL STR 26R - [SDR SWAA2025122940344](https://openairdocs.org/sdr/SWAA2025122940344), Nov 27, 2025: ANGLE. CRACKED. CRACKED ANGLE, BS 500I, STRINGER 28L IN THE FWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7902, SHEET 320, - [SDR SWAA2025122940384](https://openairdocs.org/sdr/SWAA2025122940384), Nov 27, 2025: ANGLE. CRACKED. CRACKED ANGLE, BS 500H, STRINGER 26R IN THE FWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, PARAGRAPH 9, AND DWG 143A7505, SHEET - [SDR SWAA2025122940386](https://openairdocs.org/sdr/SWAA2025122940386), Nov 27, 2025: ANGLE. CRACKED. CRACKED ANGLE, BS 500G, STRINGER 26L IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02-0G-0, AND DWG 143A7505, SHEET 137, REV -. - [SDR SWAA2025122946833](https://openairdocs.org/sdr/SWAA2025122946833), Nov 27, 2025: ANGLE. CRACKED. CRACKED ANGLE, BS 500H, STRINGER 26L IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02-OG-0, PARAGRAPH 9, AND DWG 143A7505, SHEET 137, REV -. - [SDR SWAA2025122940346](https://openairdocs.org/sdr/SWAA2025122940346), Nov 27, 2025: SUPPORT ANGLE. CORRODED. CORROSION ON SUPPORT ANGLE LOCATED BS 500I, STRINGERS 26L - 26R, WL 156.1. REPLACED SUPPORT ANGLE & FASTENERS IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0 - [SDR SWAA2025123040076](https://openairdocs.org/sdr/SWAA2025123040076), Nov 26, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 14 WL 208.1. REPLACED SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 14 WL 208.1 AT PASSENGER CABIN SRM - [SDR SWAA2025123040190](https://openairdocs.org/sdr/SWAA2025123040190), Nov 26, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BTW BS 294.5, STR 13L AT FWD GALLEY AREA. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 294.5 AT LEVEL STR 13L AT FWD GALLE - [SDR SWAA2025122940078](https://openairdocs.org/sdr/SWAA2025122940078), Nov 26, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE BTW BS 380 - 400, RBL 10, WL 208.1. REPLACED SUPPORT ANGLE IAW SRM 51-40-02, DRAWING 143A5400, SHEET 38, REV A. - [SDR SWAA2025122940079](https://openairdocs.org/sdr/SWAA2025122940079), Nov 26, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE BTW BS 380 - 400, LBL 52, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DRAWING 143A5400, SHEET 38, RE - [SDR SWAA2025122946830](https://openairdocs.org/sdr/SWAA2025122946830), Nov 26, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE BTW BS 380 - 400, LBL 14, WL 208.1 IN PASSENGER CABIN. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, DRAWING 143A5400, SHEET 38, REV A. - [SDR SWAA2025122940186](https://openairdocs.org/sdr/SWAA2025122940186), Nov 26, 2025: RIB. CRACKED. CRACKED ACCESS PANEL 341B RIB, LE STA 105.26 ON RT HORIZONTAL STAB. REPLACED THE RIB AND FASTENERS IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, & DWG - [SDR SWAA2025122940187](https://openairdocs.org/sdr/SWAA2025122940187), Nov 26, 2025: RIB. CRACKED. CRACK ACCESS PANEL 341B RIB, LE STA 114.55 ON THE RT HORIZONTAL STAB. REPLACED RIB AND FASTENERS ON ACCESS PANEL 341B IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, - [SDR SWAA2025122940081](https://openairdocs.org/sdr/SWAA2025122940081), Nov 26, 2025: FRAME. CRACKED. CRACKED FRAME, BS 312, BTW S5 - 6L AT FWD GALLEY AREA. PERFORMED REPAIR AT FRAME BS 312 AND BETWEEN S5 - 6L IAW M-22-153-01244. - [SDR SWAA2025122940077](https://openairdocs.org/sdr/SWAA2025122940077), Nov 26, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 - 400, BL 0, WL 208.1. REPLACED SUPPORT ANGLE IAW SRM 51-40-02, DRAWING 143A5400, SHEET 38, REV A. - [SDR SWAA2025122946831](https://openairdocs.org/sdr/SWAA2025122946831), Nov 26, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED AT BS 294.5, STRINGER 13L IN FWD GALLEY AREA. REPLACED SUPPORT ANGLE AND FASTENERS BS 294.5, STRINGER 13L IAW SRM 51-40-02, SRM 5 - [SDR SWAA2025122939647](https://openairdocs.org/sdr/SWAA2025122939647), Nov 25, 2025: TIE CLIP. CRACKED. CRACKED TIE CLIP, BS 277, STRINGER 10R. REPLACED THE TIE CLIP AND FASTENERS IAW SRM 51-40-02, AND DRAWING 141A1110, SHEET 55, REV -. - [SDR SWAA2025122939106](https://openairdocs.org/sdr/SWAA2025122939106), Nov 23, 2025: SUPPORT BRACKET. CRACKED. CRACK INBD TRAILING EDGE SUPPORT BRACKET IRSS 212, RT WING. REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02-0G-0, AND SRM 51-10-02-0G-0, ITEM 9, AND DWG 115A2001, - [SDR SWAA2025122939104](https://openairdocs.org/sdr/SWAA2025122939104), Nov 23, 2025: WEB. CRACKED. CRACK WEB TRAILING EDGE FIXED PANEL ORSS 271 ON RT WING. REMOVED AND REPLACED THE WEB T/E FIXED PANEL IAW SRM 51-40-02; SRM 51-10-02, ITEM 9, AND DWG 115A2512, - [SDR SWAA2025122939105](https://openairdocs.org/sdr/SWAA2025122939105), Nov 23, 2025: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE ORSS 297 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE ORSS 297 AT RT WING IAW SRM 51-40-02-0G-0, AND DWG 115A3700, S - [SDR SWAA2025123038594](https://openairdocs.org/sdr/SWAA2025123038594), Nov 22, 2025: STRIP. DETERIORATED. DETERIORATED PHOTOLUMINESCENT STRIP ALONG PAX CABIN. REPLACED PHOTOLUMINESCENT STRIP ALONG PAX CABIN IAW DWG 417A5775, REV-, SHEET 2, AND SOPM 20-50-12, REV 58. - [SDR SWAA2025123038777](https://openairdocs.org/sdr/SWAA2025123038777), Nov 22, 2025: SUPPORT ANGLE. CORRODED. CORROSION ON SUPPORT ANGLE LOCATED BTW BS 312 - 344, LBL 56, WL 208.1 AT FWD GALLEY AREA. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, P - [SDR SWAA2025122946814](https://openairdocs.org/sdr/SWAA2025122946814), Nov 22, 2025: LIGHT. DETERIORATED. DETERIORATED PHOTOLUMINESCENT STRIP ALONG PAX CABIN. REPLACED PHOTOLUMINESCENT STRIP ALONG PAX CABIN IAW DWG 417A5775 REV.- SHEET 2 AND SOPM 20-50-12 REV. 58. - [SDR SWAA2025122938770](https://openairdocs.org/sdr/SWAA2025122938770), Nov 22, 2025: WEB. CRACKED. CRACKED WEB, BS 277 - 294.5, RBL 1, WL 208.1 REPLACED THE WEB AND FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 141A5400, SHEET 20, REV-. - [SDR SWAA2025122938920](https://openairdocs.org/sdr/SWAA2025122938920), Nov 22, 2025: FLOORBEAM. CRACKED. CRACKED FLOORBEAM BS 540, BL 0 - LBL 24.75, WL 208.1. REPLACED THE FLOORBEAM IAW SRM 51-10-02-0G, SRM 51-40-02-0G, AND DWG 143A0060, SHEET 64, REV-. - [SDR SWAA2025122938776](https://openairdocs.org/sdr/SWAA2025122938776), Nov 22, 2025: INTERCOSTAL. CRACKED. CRACK ON WEB INTERCOSTAL BTW BS 344 - 360, RBL 13, WL 208.1 IN FWD GALLEY AREA. REPLACED WEB INTERCOSTAL AND FASTENERS IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 5 - [SDR SWAA2025122938771](https://openairdocs.org/sdr/SWAA2025122938771), Nov 22, 2025: SUPPORT ANGLE. CORRODED. CORROSION ON SUPPORT ANGLE, BTW BS 312 - 344, RBL 56, WL 208.1 IN FWD GALLEY AREA. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02- - [SDR SWAA2025122938919](https://openairdocs.org/sdr/SWAA2025122938919), Nov 22, 2025: FLOORBEAM. CRACKED. CRACK ON FLOORBEAM BS 540, BTW BL 0 TO RBL 24.75, WL 208.1 IN PASSENGER CABIN. REPLACED FLOORBEAM IAW SRM 51-40-02-0G-0, AND DWG 143A0060, SHEET 64, REV-. - [SDR SWAA2025122946817](https://openairdocs.org/sdr/SWAA2025122946817), Nov 22, 2025: SUPPORT ANGLE. CORRODED. CORROSION ON SUPPORT ANGLE, BTW BS 312 - 344, LBL 56, WL 208.1 IN THE FWD GALLEY AREA. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, PARA - [SDR SWAA2025122938780](https://openairdocs.org/sdr/SWAA2025122938780), Nov 22, 2025: NUT PLATE. CORRODED. CORROSION OTBD FRONT SPAR RAIL NUT PLATE OFSS 572 ON RT WING. REPLACED OUTBOARD FRONT SPAR RAIL NUT PLATE LOCATED OFSS 572 IAW SRM 51-40-02, SRM 51-40-03, AND D - [SDR SWAA2025122938773](https://openairdocs.org/sdr/SWAA2025122938773), Nov 22, 2025: NUT PLATE. CORRODED. CORROSION OTBD FRONT SPAR RAIL NUT PLATE OFSS 426 ON RT WING. REPLACED OTBD FRONT SPAR RAIL NUT PLATE LOCATED OFSS 426 IAW SRM 51-40-02, SRM 51-40-03, AND DWG 1 - [SDR SWAA2025123038436](https://openairdocs.org/sdr/SWAA2025123038436), Nov 21, 2025: SHIELD. CORRODED. CORRODED SHIELD WEB BTW BS 767 - 794.3, RBL 22, WL 156.1 IN THE AFT CARGO BAY. REPLACED THE SHIELD WEB IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, PARAGRAPH 9, AN - [SDR SWAA2025123038582](https://openairdocs.org/sdr/SWAA2025123038582), Nov 21, 2025: SUPPORT ANGLE. CRACKED. CRACK ON CARGO LINER SUPPORT ANGLE, BS 727I, LBL 51, WL 202 IN THE AFT CARGO BAY. REPAIRED THE SUPPORT ANGLE IAW SRM 51-70-11-2R-0, AND DWG 149A9490, SHEET 24, - [SDR SWAA2025123038586](https://openairdocs.org/sdr/SWAA2025123038586), Nov 21, 2025: SUPPORT ANGLE. CRACKED. CRACKED CARGO LINER SUPPORT ANGLE, BS 727B, LBL 51 IN THE AFT CARGO BAY. REPAIRED THE SUPPORT ANGLE IAW SRM 51-70-11-2R-0, AND DWG 149A9490, SHEET 24, REV -. - [SDR SWAA2025123038431](https://openairdocs.org/sdr/SWAA2025123038431), Nov 21, 2025: WEB. CORRODED. CORROSION ON SHIELD WEB, BS 847 - 867, RBL 19, WL 156.1 IN THE AFT CARGO BAY. REPLACED SHIELD WEB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 146A0081, SHEE - [SDR SWAA2025123038435](https://openairdocs.org/sdr/SWAA2025123038435), Nov 21, 2025: SUPPORT ANGLE. CORRODED. CORRODED SUPPORT ANGLE BTW BS 767 TO 787, RBL 21 AND WL156 IN AFT CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, PARAGRAPH 9, A - [SDR SWAA2025122946809](https://openairdocs.org/sdr/SWAA2025122946809), Nov 21, 2025: SUPPORT ANGLE. CRACKED. CRACK ON CARGO LINER SUPPORT ANGLE LOCATED BS 727I LBL 51 WL 202 AT AFT CARGO COMPARTMENT. REPAIRED CARGO LINER SUPPORT ANGLE LOCATED BS 727I LBL 51 WL 202 AT A - [SDR SWAA2025122946810](https://openairdocs.org/sdr/SWAA2025122946810), Nov 21, 2025: SUPPORT ANGLE. CRACKED. CRACK CARGO LINER SUPPORT ANGLE LOCATED BS727B LBL51 AT AFT CARGO COMPARTMENT. REPAIRED CARGO LINER SUPPORT ANGLE LOCATED BS727B LBL51 AT AFT CARGO COMPARTMENT - [SDR SWAA2025122946805](https://openairdocs.org/sdr/SWAA2025122946805), Nov 21, 2025: SHIELD. CORRODED. CORROSION ON SHIELD WEB LOCATED TW BS 847 TO BS 867 RBL 19 WL 156.1 AT AFT CARGO COMPARTMENT. REPLACED SHIELD WEB LOCATED BTW BS 847 TO BS 867 RBL 19 WL 156.1 A - [SDR SWAA2025122946807](https://openairdocs.org/sdr/SWAA2025122946807), Nov 21, 2025: SHIELD. CORRODED. CORROSION ON SHIELD WEB LOCATED BTW BS 767 TO BS 794.3 RBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2025-714110<[01] REPLACED SHIELD WEB LOCATED BTW BS 767 TO BS 79 - [SDR SWAA2025122938432](https://openairdocs.org/sdr/SWAA2025122938432), Nov 21, 2025: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE AT BULKHEAD BS 663.75, RBL 36. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02-0G-0, ITEM 9, DWG 111A1000, SHEET 330, SHEET 331, AND SHEET 329 - [SDR SWAA2025122946806](https://openairdocs.org/sdr/SWAA2025122946806), Nov 21, 2025: SUPPORT ANGLE. CORRODED. CORRODED SUPPORT ANGLE, BS 767 - 787, RBL 21, WL 156 IN THE AFT CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, PARAGRAPH 9, DWG - [SDR SWAA2025122938434](https://openairdocs.org/sdr/SWAA2025122938434), Nov 21, 2025: FITTING. CRACKED. CRACKED FITTING, BS 947.5, STRINGER 26L THE AFT CARGO BAY. REPLACED THE FITTING IAW SRM 51-40-02, AND DRAWING 149A8103, SHEET 8, REV-. All 190: https://openairdocs.org/deregistered/N8624J-2026-02-09/reports.md ## Other aircraft with N8624J - [Cancelled 1995-05-23](https://openairdocs.org/deregistered/N8624J-1995-05-23): Cessna 150G, S/N 15066524. Triennial form not returned. Owner: [Koenig Henry T DBA](https://openairdocs.org/faa-owner/KOENIG%20HENRY%20T%20DBA), [Almogordo, NM](https://openairdocs.org/faa-place/NM/Almogordo) --- 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.