# N8625A: 2014 Boeing 737-8H4, registration cancelled 2026-03-06 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 6, 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: 36896 - Year built: 2014 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 28, 2014 - Certificate issued: April 22, 2014 - Last registry action: January 22, 2023 - Mode S code: ABD94D - 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/N8625A - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8625A - Page: https://openairdocs.org/deregistered/N8625A-2026-03-06 From the FAA registry file of November 5, 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 (188, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SWAA2026021962632](https://openairdocs.org/sdr/SWAA2026021962632), Jan 19, 2026: BULB. BURNED OUT. EXIT SIGNS AT 14ABC; 14DEF AND 15BC HAS BULBS BURNED OUT<[01] REPLACED THE EXIT SIGN LAMPS, 14ABC;14DEF AND 15BC IAW AMM 33-51-01-960-801 PERFORMED OPERATIONAL - [SDR SWAA2026011343848](https://openairdocs.org/sdr/SWAA2026011343848), Dec 8, 2025: ANGLE. CRACKED. CRACKED ANGLE, BS 500H, LBL 21 IN THE FWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, AND DWG 143A7505, SHEET 138, REV -. - [SDR SWAA2026011343849](https://openairdocs.org/sdr/SWAA2026011343849), Dec 8, 2025: ANGLE. CRACKED. CRACKED ANGLE, BS 500G, RBL 21 IN FWD FWD CARGO. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, 51-40-02, AND DWG 143A7505, SHEET 138, REV -. - [SDR SWAA2026011343850](https://openairdocs.org/sdr/SWAA2026011343850), Dec 8, 2025: ANGLE. CRACKED. CRACKED ANGLE, BS 500H, RBL 21 IN THE AFT CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, 51-40-02, AND DWG 143A7505, SHEET 138, REV -. - [SDR SWAA2026011343855](https://openairdocs.org/sdr/SWAA2026011343855), Dec 8, 2025: ANGLE. CRACKED. CRACKED ANGLE, BS 500H, LBL 21. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, 51-40-02, AND DWG 143A7505, SHEET 138, REV -. - [SDR SWAA2026011343856](https://openairdocs.org/sdr/SWAA2026011343856), Dec 8, 2025: ANGLE. CRACKED. CRACKED ANGLE, BS 500H, RBL 21. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, 51-40-02, AND DWG 143A7505, SHEET 138, REV -. - [SDR SWAA2026011343852](https://openairdocs.org/sdr/SWAA2026011343852), Dec 8, 2025: ANGLE. CRACKED. CRACKED ANGLE, BS 400, LBL 21, FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02-0G, AND DWG 143A7505, SHEET 137, REV -. - [SDR SWAA2026011343851](https://openairdocs.org/sdr/SWAA2026011343851), Dec 8, 2025: SHIELD. CRACKED. CRACK SHIELD WEB, BTW BS492.4 - 500A, RBL 21 IN THE FWD CARGO BAY. REPLACED SHIELD WEB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A0080, SHEET 39, REV - - [SDR SWAA2026011243857](https://openairdocs.org/sdr/SWAA2026011243857), Dec 8, 2025: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BTW BS 500A TO BS 500I RBL 21 AND WL 156 AT FWD CARGO COMPARTMENT, THE DAMAGE WAS REPAIR IAW SRM 53-00-53-2R-5 AND EA M-22-153-015 - [SDR SWAA2026010943624](https://openairdocs.org/sdr/SWAA2026010943624), Dec 7, 2025: SUPPORT BRACKET. CRACKED. CRACK ON SUPPORT BRACKET PNEUMATIC DUCT LOCATED BS 540, LBL 6 IN THE AIR CONDITIONING BAY. - [SDR SWAA2026011343419](https://openairdocs.org/sdr/SWAA2026011343419), Dec 6, 2025: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE BTW BS 380 - 400, BL 0, WL 208.1. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SHEET - [SDR SWAA2026011343429](https://openairdocs.org/sdr/SWAA2026011343429), Dec 6, 2025: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BTW BS 380 - 400, RBL 40, WL 208.1. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SH - [SDR SWAA2026011343432](https://openairdocs.org/sdr/SWAA2026011343432), Dec 6, 2025: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BTW BS 380 - 400, LBL 53, WL 208.1. REPLACED THE SUPPORT ANGLE & FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SHEE - [SDR SWAA2026011343427](https://openairdocs.org/sdr/SWAA2026011343427), Dec 6, 2025: TIE CLIP. CRACKED. CRACKED TIE CLIP, BS 277, S10R IN FWD GALLEY. MEASUREMENT OF CRACK: L: 0.416 INCHES. REPLACED TIE CLIP IAW SRM 51-10-02-0G, SRM 51-40-02-0G, AND DWG 141A1110, S - [SDR SWAA2026011343428](https://openairdocs.org/sdr/SWAA2026011343428), Dec 6, 2025: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BTW BS 380 - 400, LBL 13, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SHEET 184, REV - - [SDR SWAA2026011343426](https://openairdocs.org/sdr/SWAA2026011343426), Dec 6, 2025: FRAME. CRACKED. CRACK ON FRAME, BS 312 BTW S5 - 6L. PERFORMED PERMANENT REPAIR TO THE FRAME IAW EA M-22-153-01244, REV B. - [SDR SWAA2026011343508](https://openairdocs.org/sdr/SWAA2026011343508), Dec 6, 2025: SUPPORT BRACKET. CRACKED. CRACK ON SUPPORT BRACKET, BS 867 BTW S2 & 3R. REPLACED THE SUPPORT BRACKET IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 146A7901, SHEET 66, REV A. - [SDR SWAA2026011343155](https://openairdocs.org/sdr/SWAA2026011343155), Dec 5, 2025: SUPPORT ANGLE. CORRODED. CORRODED SUPPORT ANGLE, BTW BS 767 - 887, WL156, AND RBL 21 IN THE AFT CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 146 - [SDR SWAA2026011343141](https://openairdocs.org/sdr/SWAA2026011343141), Dec 5, 2025: INTERCOSTAL. CRACKED. CRACK ON INTERCOSTAL WEB, BTW BS 344 - 360, RBL 12, WL 208.1. PERFORMED A PERMANENT REPAIR ON WEB INTERCOSTAL IAW SRM 53-10-51-2R-20, REPAIR 20. - [SDR SWAA2026011343145](https://openairdocs.org/sdr/SWAA2026011343145), Dec 5, 2025: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL WEB, BTW BS 344 - 360, BL 0, WL 208.1. REPLACED NEW INTERCOSTAL WEB AND FASTENERS IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G, AND DRAWING 141A54 - [SDR SWAA2026011343146](https://openairdocs.org/sdr/SWAA2026011343146), Dec 5, 2025: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL WEB, BTW BS 344 - 360, LBL 12, WL 208.1. REPLACED THE INTERCOSTAL WEB AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 141A5400, - [SDR SWAA2026011343160](https://openairdocs.org/sdr/SWAA2026011343160), Dec 5, 2025: PLATE. CRACKED. CRACKED CORRUGATED PLATE TRAILING EDGE LOCATED BETWEEN ORSS290 TO ORSS297, LT WING. REPLACED CORRUGATED PLATE AND FASTENERS TRAILING EDGE, LT WING IAW SRM 51-40 - [SDR SWAA2026011347409](https://openairdocs.org/sdr/SWAA2026011347409), Dec 5, 2025: STRUCTURE. CRACKED. CRACK INNER CHORD LOCATED BS 303.9, S17L. REPLACED INNER CHORD BTW BS 270 - 370, S17L IAW SRM 51-40-02-0G-0, DWG 141A8110, SHEET 3, REV E, DWG 141A8110, SHEET 1 - [SDR SWAA2026011343149](https://openairdocs.org/sdr/SWAA2026011343149), Dec 5, 2025: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE ORSS 297 RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 297 RT WING IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, - [SDR SWAA2026011343150](https://openairdocs.org/sdr/SWAA2026011343150), Dec 5, 2025: PLATE. CRACKED. CRACK CORRUGATED PLATE T/E IRSS 215 ON RT WING. REPLACED CORRUGATED PLATE LOCATED ON RT WING TRAILING EDGE IAW SRM 51-40-02, AND DWG 115A2001, SHEET 67, AND REV - [SDR SWAA2026011343148](https://openairdocs.org/sdr/SWAA2026011343148), Dec 5, 2025: WEB. CRACKED. CRACK WEB T/E FIXED PANEL ORSS 271 ON RT WING. REPLACED WEB IAW SRM 51-40-02, AND DWG 115A2512, SHEET 16, REV -. - [SDR SWAA2026011343142](https://openairdocs.org/sdr/SWAA2026011343142), Dec 5, 2025: WEB. CRACKED. CRACK WEB FAN COWL INBOARD LOC. INTERNAL AREA ACCESS DOOR 414AR ON NR 1 ENGINE. REPLACED WEB FAN COWL INBD INTERNAL AREA ACCESS DOOR 414AR IAW SRM 51-10-02, ITE - [SDR SWAA2026011343151](https://openairdocs.org/sdr/SWAA2026011343151), Dec 5, 2025: WEB. CRACKED. CRACKED OUTBOARD FAN COWL WEB, INTERNAL AREA ACCESS DOOR 424AR ON NR 2 ENGINE. REPLACED WEB LOCATED ON OTBD FAN COWL INTERNAL AREA ACCESS DOOR 424AR IAW SRM 51- - [SDR SWAA2026011243152](https://openairdocs.org/sdr/SWAA2026011243152), Dec 5, 2025: INTERCOSTAL. CRACKED. CRACK ON WEB - INTERCOSTAL LOCATED BTW BS927 TO BS947.5 AND RBL21 AFT CARGO COMPARTMENT. REPLACED WEB - INTERCOSTAL LOCATED BTW BS927 TO BS947.5 AND RBL21 AFT C - [SDR SWAA2026011243153](https://openairdocs.org/sdr/SWAA2026011243153), Dec 5, 2025: SUPPORT ANGLE. CRACKED. CRACK ON ANGLE - SUPPORT LOCATED BS867 AND LBL 10 AFT CARGO COMPARTMENT. REPLACED ANGLE - SUPPORT LOCATED BS867 AND LBL 10 AFT CARGO COMPARTMENT IAW SRM 51-10-0 - [SDR SWAA2026011243154](https://openairdocs.org/sdr/SWAA2026011243154), Dec 5, 2025: WEB. CORRODED. CORROSION ON SHIELD WEB LOCATED BTW BS767 TO BS794.3 WL156 AND RBL21 AT AFT CARGO COMPARTMENT. REPLACED SHIELD WEB LOCATED BTW BS767 TO BS794.3 WL156 AND RBL21 - [SDR SWAA2026011243156](https://openairdocs.org/sdr/SWAA2026011243156), Dec 5, 2025: SUPPORT. CORRODED. CORROSION ON SUPPORT ZEE LOCATED BTW BS727E PLUS 10INCH TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT. REPAIRED SUPPORT ZEE LOCATED BTW 727 TO 767 AT AFT CARGO - [SDR SWAA2026011243159](https://openairdocs.org/sdr/SWAA2026011243159), Dec 5, 2025: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BTW BS 727G PLUS 10INCH TO BS807 PLUS 10INCH WL156 AND LBL21 AFT CARGO COMPARTMENT. REPAIRED SUPPORT ZEE CHANNEL LOCATED BTW BS 72 - [SDR SWAA2026010843144](https://openairdocs.org/sdr/SWAA2026010843144), Dec 5, 2025: FRAME. CRACKED. CRACK INNER CHORD LOCATED BS 303.9 AT LEVEL OF STR 17L AT FWD GALLEY AREA. - [SDR SWAA2026011342430](https://openairdocs.org/sdr/SWAA2026011342430), Dec 4, 2025: INTERCOSTAL. CORRODED. CORROSION ON INTERCOSTAL BTW BS 947 - 967, LBL 50, WL 208.1. REPLACED THE INTERCOSTAL IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 147A5650, SHEET 54, REV A. - [SDR SWAA2026011342674](https://openairdocs.org/sdr/SWAA2026011342674), Dec 4, 2025: NUT PLATE. CORRODED. CORROSION OTBD FRONT SPAR RAIL NUT PLATE OFSS 548 ON LT WING. REPLACED THE SPAR RAIL NUT PLATE OFSS 548, FASTENERS IAW SRM 51-40-02, AND DWG 112A4402, SHEET 40, - [SDR SWAA2026011342675](https://openairdocs.org/sdr/SWAA2026011342675), Dec 4, 2025: NUT PLATE. CORRODED. CORROSION OTBD FRONT SPAR RAIL NUT PLATE OFSS 449 LT WING. REPLACED RAIL NUT PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 112A4402, SHEET 40, REV A. - [SDR SWAA2026011342673](https://openairdocs.org/sdr/SWAA2026011342673), Dec 4, 2025: NUT PLATE. CORRODED. CORROSION OTBD FRONT SPAR RAIL NUT PLATE OFSS 652 ON LT WING. REPLACED OTBD FRONT SPAR RAIL NUT PLATE IAW SRM 51-40-02, 51-10-02, ITEM 9, AND DWG 112A4402, SHEE - [SDR SWAA2026011342676](https://openairdocs.org/sdr/SWAA2026011342676), Dec 4, 2025: NUT PLATE. CORRODED. CORROSION OTBD FRONT SPAR RAIL NUT PLATE OFSS 421 ON LT WING. REPLACED THE RAIL NUT PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 112A4402, SHEET 40, RE - [SDR SWAA2026011342677](https://openairdocs.org/sdr/SWAA2026011342677), Dec 4, 2025: NUT PLATE. CORRODED. CORROSION OTBD FRONT SPAR RAIL NUT PLATE OFSS 527 ON LT WING. REPLACED RAIL NUT PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02 AND DWG: 112A4402, SHEET 40, REV A. - [SDR SWAA2026011242863](https://openairdocs.org/sdr/SWAA2026011242863), Dec 4, 2025: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE AT BULKHEAD BS 663.75 AND LBL 10 CENTER SECTION. PERFORMED PERMANENT REPAIR ON ANGLE LOCATED AT BS 663 BTW LBL 6 TO LBL 25 IAW B737-800 SRM - [SDR SWAA2026011242864](https://openairdocs.org/sdr/SWAA2026011242864), Dec 4, 2025: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE AT BULKHEAD BS 663.75 AND RBL 10 CENTER SECTION. PERFORMED PERMANENT REPAIR ON ANGLE LOCATED AT BS 663 BTW RBL 6 TO RBL 25 IAW SRM 57-10-10- - [SDR SWAA2026011342262](https://openairdocs.org/sdr/SWAA2026011342262), Dec 3, 2025: ANGLE. CRACKED. CRACKED GUSSET ANGLE, BS 500I, S19R. REPLACED THE GUSSET ANGLE AND FASTENERS IAW SRM 51-40-02-0G, & DWG 143A7902, SHEET 256, REV B. - [SDR SWAA2026011242260](https://openairdocs.org/sdr/SWAA2026011242260), Dec 3, 2025: BALANCE WEIGHT. OUT OF BALANCE. DURING WEIGHT AND BALANCE PROCEDURE OF RT ELEVATOR FOUND BALANCE WEIGHTS (1EA) ON BAY 2; P/N: 183A0210-14 (1EA) AND P/N: 69-53211-2 (2EA) ON BAY 3; P/N: 183A021 - [SDR SWAA2026011241571](https://openairdocs.org/sdr/SWAA2026011241571), Dec 2, 2025: FLOOR PANEL. DAMAGED. ELONGATED HOLES ON FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT. REPLACED FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT IAW SRM 51-10-02 TEM 9 AND DWG 453A2610, SHEE - [SDR SWAA2026011341570](https://openairdocs.org/sdr/SWAA2026011341570), Dec 1, 2025: STUB FRAME. CRACKED. CRACK INDICATION ON STUB FRAME BTWN BS 294.5 - 296.5, S8-9R. CRACK LENGTH: 0.375 IN. REPLACED THE STUB FRAME IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 141A8 - [SDR SWAA2026011341328](https://openairdocs.org/sdr/SWAA2026011341328), Dec 1, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BS 500I, S19R BELLY FAIRING. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, DWG 116A3110, SHEET 8, REV -, AND DWG 149A7101, SHEET 1 - [SDR SWAA2026011341330](https://openairdocs.org/sdr/SWAA2026011341330), Dec 1, 2025: ACCESS PANEL. ELONGATED. ELONGATED HOLES ON ACCESS PANEL 661CB T/E, RT WING. REPAIRED THE ACCESS PANEL 661CB IAW SRM 51-70-04-2R-10, REPAIR 10. - [SDR SWAA2026011341029](https://openairdocs.org/sdr/SWAA2026011341029), Nov 30, 2025: ADAPTER. DETERIORATED. DETERIORATED ADAPTER PLATE AND SHIM ON GIRT BAR FITTING, FWD ENTRY, & SERVICE DOORS. REPLACED THE ADAPTER PLATE AND SHIM IAW AMM 25-66-02-400-801, STEP 3 D, 1, - [SDR SWAA2026011341036](https://openairdocs.org/sdr/SWAA2026011341036), Nov 30, 2025: ADAPTER. DETERIORATED. DETERIORATED ADAPTER PLATE AND SHIM ON THE GIRT BAR FITTING ON THE AFT ENTRY AND SERVICE DOORS. REPLACED THE ADAPTER PLATE AND SHIM IAW AMM 25-66-02-400-801, ST All 188: https://openairdocs.org/deregistered/N8625A-2026-03-06/reports.md ## Other aircraft with N8625A - [Cancelled 1991-06-17](https://openairdocs.org/deregistered/N8625A-1991-06-17): Enstrom F-28F, S/N 759. Exported to Italy. Owner: [Enstrom Helicopter Corp](https://openairdocs.org/faa-owner/ENSTROM%20HELICOPTER%20CORP), [Menominee, MI](https://openairdocs.org/faa-place/MI/Menominee) --- 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.