# N8634A: 2014 Boeing 737-8H4, registration cancelled 2026-09-03 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 3, 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 CFM56-7B24E series](https://openairdocs.org/engine/cfm-international-cfm56-7b24e-series) (registry code 13804) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 42522 - Year built: 2014 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 13, 2014 - Certificate issued: July 8, 2014 - Last registry action: March 4, 2023 - Mode S code: ABDCE1 - 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/N8634A - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8634A - Page: https://openairdocs.org/deregistered/N8634A-2026-09-03 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 (155, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SWAA2026070711868](https://openairdocs.org/sdr/SWAA2026070711868), Jun 13, 2026: SIGN. INOPERATIVE. EMERGENCY EXIT SIGN HAS 1 BULB INOP AT THE R1 DOOR. REPLACED EMERGENCY EXIT SIGN ASSEMBLY IAW AMM 33-51-01-960-802; TEST PASSED. VERIFIED REPLACED EMERGENCY EXI - [SDR SWAA2026061110186](https://openairdocs.org/sdr/SWAA2026061110186), Jun 8, 2026: LIGHT. INOPERATIVE. RIGHT OVERWING EXIT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RT OVERWING EMERGENCY LIGHT (FWD) IAW AMM 33-51-04-960-801. OPS TESTED GOOD. - [SDR SWAA2026030369239](https://openairdocs.org/sdr/SWAA2026030369239), Feb 10, 2026: FLOOR PANEL. CRACKED. CRACKED FLOOR PANEL 231AF. REPAIRED THE FLOOR PANEL 231AF IAW SRM 53-00-50-2R-1, REPAIR 1. - [SDR SWAA2026030568401](https://openairdocs.org/sdr/SWAA2026030568401), Feb 6, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 360, STRINGERS 27R - 28R. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, PARAGRAPH 9, & SRM 51-40-02. - [SDR SWAA2026030567342](https://openairdocs.org/sdr/SWAA2026030567342), Feb 3, 2026: FRAME. CRACKED. CRACKED FRAME, BS 312, STRINGERS 5L - 6L, LBL 33. PERFORMED A TRIM OUT OF FRAME IAW EA M-22-153-01244, REV B. - [SDR SWAA2026030566956](https://openairdocs.org/sdr/SWAA2026030566956), Feb 2, 2026: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET LOCATED BS 540 AT LEVEL LBL 6 AT LT & RT AIR CONDITIONING BAYS. REPLACED SUPPORT BRACKET LOCATED BS 540 AT LEVEL LBL 6 AT LT/RT AIR CONDIT - [SDR SWAA2026030566957](https://openairdocs.org/sdr/SWAA2026030566957), Feb 2, 2026: SUPPORT BRACKET. CRACKED. CRACKED SUPPORT BRACKET, BS 540, RBL 6 IN THE LT & RT AIR CONDITIONING BAYS. REPLACED THE SUPPORT BRACKET IAW SRM 51-10-02-0G, & DWG 212A1101, SHEET 11, REV -, - [SDR SWAA2026030566754](https://openairdocs.org/sdr/SWAA2026030566754), Feb 2, 2026: WEB. CRACKED. CRACKED WEB, ORSS269, RT WING T/E. REPLACED THE WEB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 115A2512, SHEET 16, REV-. - [SDR SWAA2026030566752](https://openairdocs.org/sdr/SWAA2026030566752), Feb 2, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, ORSS 288, RT WING T/E. REMOVED AND REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02. AND DWG 115A3761 - [SDR SWAA2026030566543](https://openairdocs.org/sdr/SWAA2026030566543), Jan 31, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 400, STRINGER 26L. REPLACED THE ANGLE IAW SRM 51-40-02, & DWG 143A7505, SHEET 137, REV -. THE ANGLE WAS REPLACED DUE TO NO ALLOWABLE DAMAGE LI - [SDR SWAA2026030566537](https://openairdocs.org/sdr/SWAA2026030566537), Jan 31, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500G, STRINGER 26L FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02, & DWG 143A7505, SHEET 138, REV -. - [SDR SWAA2026030566548](https://openairdocs.org/sdr/SWAA2026030566548), Jan 31, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500H, STRINGER 26R, FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02, & DWG 143A7505, SHEET 139, REV -. - [SDR SWAA2026030566544](https://openairdocs.org/sdr/SWAA2026030566544), Jan 31, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500G, STRINGER 26L, REPLACED THE ANGLE IAW SRM 51-40-02, & DWG 143A7505, SHEET 138, REV -. - [SDR SWAA2026030566545](https://openairdocs.org/sdr/SWAA2026030566545), Jan 31, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500G, STRINGER 26R. REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 143A7505, SHEET 138, REV -. - [SDR SWAA2026030566546](https://openairdocs.org/sdr/SWAA2026030566546), Jan 31, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500H, STRINGER 26L. REPLACED THE ANGLE IAW SRM 51-40-02, & DWG 143A7505, SHEET 139, REV -. - [SDR SWAA2026030566549](https://openairdocs.org/sdr/SWAA2026030566549), Jan 31, 2026: SUPPORT BRACKET. CRACKED. CRACKED SUPPORT BRACKET, BS 727. REPLACED THE SUPPORT BRACKET IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, AND DWG 144A2600, SHEET 1084, REV-. - [SDR SWAA2026030566538](https://openairdocs.org/sdr/SWAA2026030566538), Jan 31, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500H, STRINGER 26R. REPLACED THE ANGLE, IAW FASTENERS IAW SRM 51-40-02-0G, SRM-51-10-02-0G-0, ITEM 9, & DWG 143A7505, SHEET 138, REV-. - [SDR SWAA2026030566547](https://openairdocs.org/sdr/SWAA2026030566547), Jan 31, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500H, STRINGER 26L. REPLACED THE ANGLE & FASTENERS IAW SRM 51-40-02, & DWG 143A7505, SHEET 139, REV -. - [SDR SWAA2026030566536](https://openairdocs.org/sdr/SWAA2026030566536), Jan 31, 2026: SILL DRAIN. CORRODED. CORRODED LOWER SILL DRAIN, BS 440 - 492.4, RBL 21, WL 156. REPLACED THE SILL DRAIN AND FASTENERS IAW SRM 51-40-02, AND DWG 143A8330, SHEET 30, REV -. - [SDR SWAA2026030566540](https://openairdocs.org/sdr/SWAA2026030566540), Jan 31, 2026: GUSSET. CRACKED. CRACKED GUSSET ANGLE, BS 500I, STRINGER 19R. REPLACED THE GUSSET ANGLE IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, AND DWG 143A7902, SHEET 256, REV B. - [SDR SWAA2026030566539](https://openairdocs.org/sdr/SWAA2026030566539), Jan 31, 2026: GUSSET. CRACKED. CRACKED GUSSET ANGLE, BS 500I, STRINGER 21R, FWD CARGO BAY. REPLACED THE GUSSET ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7902, SHEET 257, REV B - [SDR SWAA2026030566414](https://openairdocs.org/sdr/SWAA2026030566414), Jan 31, 2026: PLATE. CRACKED. CRACKED CORRUGATED PLATE IRSS 216, LT WING T/E. REPLACED THE CORRUGATED PLATE IAW SRM 51-10-02-0G, ITEM 9, SRM 51-40-02-0G, AND DWG 115A2001, SHEET 78, REV: A. - [SDR SWAA2026030566417](https://openairdocs.org/sdr/SWAA2026030566417), Jan 31, 2026: ANGLE. CRACKED. CRACKED ANGLE ON ACCESS PANEL 551GB, LT WING. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, & SRM 51-40-02. - [SDR SWAA2026030566418](https://openairdocs.org/sdr/SWAA2026030566418), Jan 31, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLE ON ACCESS PANEL 561AB, LT WING. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-9, REPAIR 9. - [SDR SWAA2026030566419](https://openairdocs.org/sdr/SWAA2026030566419), Jan 31, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLE ON ACCESS PANEL 561CB, LT WING. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-9, REPAIR 9. - [SDR SWAA2026030566060](https://openairdocs.org/sdr/SWAA2026030566060), Jan 30, 2026: FLOOR SUPPORT. CORRODED. CORRODED FLOOR SUPPORT, BS 947 - 967, LBL 49, WL 208.1. REPLACED THE FLOOR SUPPORT & FASTENERS IAW SRM 51-40-02, AND DWG 1475650, SHEET 55, REV A. - [SDR SWAA2026030566062](https://openairdocs.org/sdr/SWAA2026030566062), Jan 30, 2026: ANGLE. CORRODED. CORRODED ANGLE, BS 986.5 - 1016, RBL 32, WL 208.5. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, & DWG 147A5700, SHEET 121, REV A. - [SDR SWAA2026030566061](https://openairdocs.org/sdr/SWAA2026030566061), Jan 30, 2026: FLOORBEAM. CORRODED. CORRODED FLOORBEAM, BS 986.5, LBL 43, WL 208.1. PERFORMED A PERMANENT REPAIR ON THE FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6. - [SDR SWAA2026030566069](https://openairdocs.org/sdr/SWAA2026030566069), Jan 30, 2026: SKIN. CORRODED. CORRODED SKIN, BS 807 - 827, STRINGERS 27R - 27L, WL 148. PERFORMED A REPAIR IAW EA 26-153-00408-WIP1, EA 26-153-00408-WIP2, EA 26-153-00408-WIP3, EA 26-153-004 - [SDR SWAA2026030566067](https://openairdocs.org/sdr/SWAA2026030566067), Jan 30, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 380 - 400, LBL 13. REPLACED THE ANGLE IAW SRM 51-40-02, SRM-51-10-02-0G-0, ITEM 9, & DWG 143A5400, SHEET 38, REV A. - [SDR SWAA2026030566070](https://openairdocs.org/sdr/SWAA2026030566070), Jan 30, 2026: ANGLE. CORRODED. CORRODED ANGLE, BS 767 - 787, RBL 21, WL 156., REPLACED THE ANGLE & FASTENERS IAW SRM 51-40-02, & DWG 146A8123, SHEET 16, REV -. - [SDR SWAA2026030566188](https://openairdocs.org/sdr/SWAA2026030566188), Jan 30, 2026: STRAP. CORRODED. CORRODED STRAP, BS 787 - 807, RBL 21, WL156. REPLACED THE STRAP AND FASTENERS IAW SRM 51-40-02-0G-0, DWG 146A0081, SHEET 49, REV A, & DWG 146A8340, SHEET 28, RE - [SDR SWAA2026030566063](https://openairdocs.org/sdr/SWAA2026030566063), Jan 30, 2026: FLOOR SUPPORT. CORRODED. CORRODED FLOOR SUPPORT, BS 947 - 967, RBL 24, WL 208.1. REPLACED THE FLOOR SUPPORT AND FASTENERS IAW SRM 51-40-02, AND DWG 47A5650, SHEET 70, REV A. - [SDR SWAA2026030566064](https://openairdocs.org/sdr/SWAA2026030566064), Jan 30, 2026: FLOOR SUPPORT. CORRODED. CORRODED FLOOR SUPPORT, BS 947 - 967, RBL 50, WL 208.1. REPLACED THE FLOOR SUPPORT AND FASTENERS IAW SRM 51-40-02, & DWG 47A5650, SHEET 70, REV A. - [SDR SWAA2026030565868](https://openairdocs.org/sdr/SWAA2026030565868), Jan 30, 2026: FLOORBEAM. CORRODED. FOUR AREAS, CORRODED FLOORBEAM UPPER TEE, BS 947.5, LBL 53, LBL 24, RBL 24, & RBL 50. REPAIRED THE FLOORBEAM IAW EA 26-153-00376-WIP1, EA 26-153-00376-WIP2, EA - [SDR SWAA2026030566071](https://openairdocs.org/sdr/SWAA2026030566071), Jan 30, 2026: CARGO TRACK. CRACKED. CRACKED TRACK RBL 13.84, BS 727I IN THE AFT CARGO BAY. REPAIRED THE CARGO TRACK IAW SRM 53-00-53-2R-3, REPAIR 3, ALTERNATIVE 1, & 2, FIGURE 203, SHEETS 1 & 2. - [SDR SWAA2026030366065](https://openairdocs.org/sdr/SWAA2026030366065), Jan 30, 2026: CHANNEL. DAMAGED. ELONGATED HOLE ON SUPPORT ZEE, BS 727J - 747, RBL 21. REPLACED THE ZEE CHANNEL SIDEPLATE, SPLICE SIDEPLATE, & FASTENERS. IAW SRM 51-40-02-0G, SRM 53-00-53-2R-5, - [SDR SWAA2026030366066](https://openairdocs.org/sdr/SWAA2026030366066), Jan 30, 2026: SHIELD. CORRODED. CORRODED SHIELD WEB, BS 767 - 794.3, RBL21, WL 156. REPLACED SHIELD IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 146A0081, SHEET 49, REV A . - [SDR SWAA2026030366187](https://openairdocs.org/sdr/SWAA2026030366187), Jan 30, 2026: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL, BS 927 - 947.5, STRINGER 25R. REPLACED THE INTERCOSTAL & FASTENERS IAW SRM 51-40-02, & DWG147A7500, SHEET 37, REV-. - [SDR SWAA2026030565866](https://openairdocs.org/sdr/SWAA2026030565866), Jan 29, 2026: WEB. CRACKED. CRACKED WEB, BS 344 - 360, BL 0. REPLACED THE WEB IAW SRM 51-10-02, ITEM 9, & DWG 141A5400, SHEET 32, REV -. - [SDR SWAA2026030564765](https://openairdocs.org/sdr/SWAA2026030564765), Jan 27, 2026: SCUFF PLATE. CRACKED. CRACKED AFT CORNER OF SCUFF PLATE, AT THE AFT CARGO DOOR CUT-OUT. REPAIRED AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, & BAC 5975. - [SDR SWAA2026030565108](https://openairdocs.org/sdr/SWAA2026030565108), Jan 27, 2026: FLOORBEAM. CRACKED. CRACKED FLOORBEAM, BS 540, BL 0 - RBL 24.75. REPLACED THE FLOORBEAM IAW SRM 51-40-02, AND SRM-51-10-02-0G-0, ITEM 9, & DWG 143A0060; SHEET 64, REV-. - [SDR SWAA2026030564766](https://openairdocs.org/sdr/SWAA2026030564766), Jan 27, 2026: SCUFF PLATE. CRACKED. CRACKED AFT CORNER OF THE SCUFF PLATE AT THE FWD CARGO DOOR CUT-OUT. REPAIRED THE SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, AND BAC 5975. - [SDR SWAA2026030565109](https://openairdocs.org/sdr/SWAA2026030565109), Jan 27, 2026: LIGHT. DETERIORATED. DETERIORATED PHOTOLUMINESCENT STRIP IN THE CABIN. REPLACED PHOTOLUMINESCENT STRIP IAW AMM 33-51-15-960-801. - [SDR SWAA2026030365106](https://openairdocs.org/sdr/SWAA2026030365106), Jan 27, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 727B. PERFORMED A REPAIR ON THE SUPPORT ANGLE IAW SRM 51-70-11-2R-0. - [SDR SWAA2026030365107](https://openairdocs.org/sdr/SWAA2026030365107), Jan 27, 2026: SUPPORT ANGLE. CRACKED. CRACKED LINER SUPPORT ANGLE, BS 727I, LBL 65. PERFORMED A REPAIR ON THE SUPPORT ANGLE BS 727I IAW SRM 51-70-11-2R-0, - [SDR SWAA2026012664072](https://openairdocs.org/sdr/SWAA2026012664072), Jan 23, 2026: SLIDE. OUT OF POSITION. FORWARD ENTRY SLIDE COVER MISSING. REPOSITIONED SLIDE ASSY INTO DOOR IAW MT 725-61-06. - [SDR SWAA2025122354238](https://openairdocs.org/sdr/SWAA2025122354238), Dec 20, 2025: FITTING. DAMAGED. ROW 29ABC AFT INBD SEAT TRACK FITTING ASSY. ROUNDED OUT. - [SDR SWAA2025122254268](https://openairdocs.org/sdr/SWAA2025122254268), Dec 19, 2025: SLIDE. PARTIAL DEPLOY. L1 DOOR EMERGENCY SLIDE PARTIALLY DEPLOYED. SLIDE DID NOT DEPLOY. SECURED L1 SLIDE IN TH CASE REF MT 725-61-06. NO DEFECTS - [SDR SWAA2025040721814](https://openairdocs.org/sdr/SWAA2025040721814), Apr 4, 2025: LENS. DAMAGED. MID CABIN OVERHEAD SIGN DAMAGED.<[01] SECURED MID CABIN EMERGENCY EXIT SIGN LENS IAW AMM 33-51-01 All 155: https://openairdocs.org/deregistered/N8634A-2026-09-03/reports.md ## Other aircraft with N8634A - [Cancelled 1951-02-13](https://openairdocs.org/deregistered/N8634A-1951-02-13): Beech A35, S/N D-2044. Owner: [Western Engineering Co](https://openairdocs.org/faa-owner/WESTERN%20ENGINEERING%20CO), [Harlan, IA](https://openairdocs.org/faa-place/IA/Harlan) --- 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.