# N8638A: 2014 Boeing 737-8H4, registration cancelled 2026-06-25 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 25, 2026 - Exported to: Nigeria - 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: 36911 - Year built: 2014 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 20, 2014 - Certificate issued: August 8, 2014 - Last registry action: March 10, 2023 - Mode S code: ABDD6D - 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/N8638A - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8638A - Page: https://openairdocs.org/deregistered/N8638A-2026-06-25 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 (133, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SWAA2026041689278](https://openairdocs.org/sdr/SWAA2026041689278), Apr 14, 2026: SEAT. OUT OF ADJUST. EXIT ROW SEAT 14F RECLINES. PERFORMED SEAT RECLINE LOCKED 14F IAW CMM 25-22-46-3500 REV.9 FIGURE 5 ITEM 10 PAGE 10102 AND PAGE 7014 STEP Y.(4) TO (7). TESTED OK - [SDR SWAA2026041480751](https://openairdocs.org/sdr/SWAA2026041480751), Mar 17, 2026: ANGLE. CRACKED. CRACK ANGLE LOCATED STA500I AND RBL 7 AT FWD CARGO COMPARTMENT. REPLACED ANGLE IAW SRM 51-40-02, 51-10-02, ITEM 9, & DWG 143A7902, SHEET 320, REV -, & SRM 53-00 - [SDR SWAA2026041780404](https://openairdocs.org/sdr/SWAA2026041780404), Mar 16, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 333CB AT LT HORIZONTAL STABILIZER. REPAIRED ACCESS PANEL 333CB AT LT HORIZONTAL STABILIZERIAW SRM 51-70-04-2R-10 REPAIR 10. - [SDR SWAA2026042080023](https://openairdocs.org/sdr/SWAA2026042080023), Mar 15, 2026: SUPPORT ANGLE. CRACKED. CRACKED OXYGEN BOTTLE SUPPORT ANGLE, BS 360, STR 27R - 28R. REPLACED OXYGEN BOTTLE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, SRM 51-10-02, ITEM 9; MEASUREMENT OF CRA - [SDR SWAA2026042080120](https://openairdocs.org/sdr/SWAA2026042080120), Mar 15, 2026: ACCESS PANEL. CRACKED. CRACKED ANGLE ON ACCESS PANEL 844DZ ON THE AFT SERVICE DOOR. REPLACED THE ANGLE OF THE ACCESS PANEL 844DZ IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 411A21 - [SDR SWAA2026042080022](https://openairdocs.org/sdr/SWAA2026042080022), Mar 15, 2026: TIE CLIP. CRACKED. CRACKED TIE CLIP, BS 277, STR 10R. REPLACED THE TIE CLIP IAW SRM 51-10-02, ITEM 9, AND FASTENERS IAW SRM 51-40-02 AND DRAWING 141A1110, SHEET 55, REV -. - [SDR SWAA2026042080118](https://openairdocs.org/sdr/SWAA2026042080118), Mar 15, 2026: ACCESS PANEL. CRACKED. CRACK ACCESS PANEL 333AT BLADE ANGLE AT LT HORIZONTAL STABILIZER 2026-182072<[01] REPLACED ACCESS PANEL 333AT BLADE ANGLE AT LT HORIZONTAL STABILIZER IAW B737-8 - [SDR SWAA2026042079836](https://openairdocs.org/sdr/SWAA2026042079836), Mar 14, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 867, LBL 10. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, DWG 149A8102, SHEET 19, REV A. MEASUREMENT OF CRACK IS L= 0.602. - [SDR SWAA2026042079837](https://openairdocs.org/sdr/SWAA2026042079837), Mar 14, 2026: FITTING. CRACKED. CRACKED FITTING, BS 947.5 AND LBL10. REPLACED THE FITTING IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G, AND DWG 149A8103, SHEET 8, REV -. - [SDR SWAA2026041779834](https://openairdocs.org/sdr/SWAA2026041779834), Mar 14, 2026: HOOK AND LOOP. OUT OF ADJUST. VELCRO STRIP ON THE GIRT ARE NOT ATTACHED TO THE VELCRO STRIP ON THE BACKING PAN SHELF LOCATED AFT SERVICE DOOR AT PASSENGER CABIN. INSTALLED CORRECTLY GIRT VEL - [SDR SWAA2026041679842](https://openairdocs.org/sdr/SWAA2026041679842), Mar 14, 2026: SUPPORT ANGLE. CORRODED. CORROSION ON SUPPORT ANGLE BTW BS 767 - 787, WL 156 AND RBL 21 AFT CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, DWG 146A8123, S - [SDR SWAA2026041679835](https://openairdocs.org/sdr/SWAA2026041679835), Mar 14, 2026: WEB. CORRODED. CORROSION ON SHIELD WEB, BETWEEN BS 767 - 787, WL 156, & RBL 21 IN THE AFT CARGO BAY. REPLACED SHIELD WEB AND FASTENERS LOCATED BETWEEN BS767 TO BS787 WL156 AND - [SDR SWAA2026041679838](https://openairdocs.org/sdr/SWAA2026041679838), Mar 14, 2026: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL BTW BS 927 - 947, RBL 21 IN THE AFT CARGO BAY. REPLACED THE INTERCOSTAL, NUTPLATE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND - [SDR SWAA2026041779510](https://openairdocs.org/sdr/SWAA2026041779510), Mar 13, 2026: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE AT IRSS217 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE AT IRSS217 AT RT WING IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 - [SDR SWAA2026041779078](https://openairdocs.org/sdr/SWAA2026041779078), Mar 12, 2026: SUPPORT BRACKET. CRACKED. CRACKED SUPPORT BRACKET AT ORSS277 TRAILING EDGE AT RT WING. REPLACED SUPPORT BRACKET AT ORSS277 TRAILING EDGE AT RT WING IAW SRM 51-10-02, ITEM 9, SRM 51-40-02 - [SDR SWAA2026042078900](https://openairdocs.org/sdr/SWAA2026042078900), Mar 11, 2026: TIE CLIP. CRACKED. CRACKED TIE CLIP, BS 500I, STR 26R. REPLACED TIE CLIP AND FASTENERS IAW SRM 51-40-02; SRM 51-10-02, ITEM 9 AND DWG 143A1234, SHEET 14, REV A. - [SDR SWAA2026042078736](https://openairdocs.org/sdr/SWAA2026042078736), Mar 11, 2026: ANGLE. CRACKED. CRACKED UPPER CHORD LOCATED INTERNAL AREA RT SIDE BS 663.75 AND RBL 34 AT AIR CONDITIONING BAY. REPLACED UPPER CHORD LOCATED INTERNAL AREA RT SIDE BODY STA 663. - [SDR SWAA2026041678902](https://openairdocs.org/sdr/SWAA2026041678902), Mar 11, 2026: TIE CLIP. CRACKED. CRACK ON TIE CLIP LOCATED FWD FACE BS 500I AT LEVEL STR 26L AT FWD CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED FWD FACE BS 500I AT LEVEL STR 26L AT FWD CARGO C - [SDR SWAA2026041678903](https://openairdocs.org/sdr/SWAA2026041678903), Mar 11, 2026: TIE CLIP. CRACKED. CRACK ON TIE CLIP LOCATED FWD FACE BS 500H AT LEVEL STR 26L AT FWD CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED FWD FACE BS 500H AT LEVEL STR 26L AT FWD CARGO C - [SDR SWAA2026041678735](https://openairdocs.org/sdr/SWAA2026041678735), Mar 11, 2026: WEB. CORRODED. CORROSION ON SHIELD WEB LOCATED BTW BS 492.4 TO BS 500A RBL 22 WL 156.1 AT FWD CARGO COMPARTMENT. REPLACED SHIELD WEB LOCATED BTW BS 492.4 TO BS 500A RBL 22 WL - [SDR SWAA2026042078330](https://openairdocs.org/sdr/SWAA2026042078330), Mar 10, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500H, STR 26R. REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 143A7505, SHEET 138, REV -. - [SDR SWAA2026042078333](https://openairdocs.org/sdr/SWAA2026042078333), Mar 10, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500G, STR 26R. REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 143A7505, SHEET 138, REV-. - [SDR SWAA2026042078328](https://openairdocs.org/sdr/SWAA2026042078328), Mar 10, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500H, STR 26L. REPLACED ANGLE IAW SRM 51-40-02-0G, AND DWG 143A7505, SHEET 138, REV -. - [SDR SWAA2026042078329](https://openairdocs.org/sdr/SWAA2026042078329), Mar 10, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500H, STR 26R. REPLACED ANGLE AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 137, REV-. - [SDR SWAA2026042091107](https://openairdocs.org/sdr/SWAA2026042091107), Mar 10, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500H, STR 26R. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 137, REV-. - [SDR SWAA2026042078331](https://openairdocs.org/sdr/SWAA2026042078331), Mar 10, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500G, STR 26R. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7505, SHEET 137, REV-. - [SDR SWAA2026042091108](https://openairdocs.org/sdr/SWAA2026042091108), Mar 10, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500G, STR 26R. REPLACED THE CLIP AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7505, SHEET 137, REV-. - [SDR SWAA2026042078334](https://openairdocs.org/sdr/SWAA2026042078334), Mar 10, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 500H, STR 26L. REPLACED ANGLE IAW SRM 51-40-02, SRM 51-10-02, PARAGRAPH 9, & DWG 143A7505, SHEET 138, REV- . - [SDR SWAA2026042078567](https://openairdocs.org/sdr/SWAA2026042078567), Mar 10, 2026: ANGLE. CRACKED. CRACKED ANGLE, BS 440, STR 26L. REPLACED THE ANGLE IAW SRM 51-40-02; 51-10-02, ITEM 9, AND DWG 143A7505, SHEET 137, REV -. - [SDR SWAA2026042078327](https://openairdocs.org/sdr/SWAA2026042078327), Mar 10, 2026: ANGLE. CRACKED. CRACK GUSSET ANGLE LOCATED BS 500I AT LEVEL STR 19R. REPLACED GUSSET ANGLE LOCATED BS 500I AT LEVEL STR 19R IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A - [SDR SWAA2026042078568](https://openairdocs.org/sdr/SWAA2026042078568), Mar 10, 2026: SUPPORT. CORRODED. CORRODED LOWER SILL LOCATED BTW BS 440 TO BS 492. 4 RBL 29 WL 208.1. REPLACED LOWER SILL LOCATED BTW BS 440 TO BS 492. 4 RBL 29 WL 208.1 IAW SRM 51-10-02 ITEM 9 - [SDR SWAA2026041778570](https://openairdocs.org/sdr/SWAA2026041778570), Mar 10, 2026: BRACKET. DETERIORATED. DETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS SERVICE DOOR AT FWD GALLEY AREA. REPLACED HARDWARE GIRT BAR FLOOR BRACKETS SERVICE DOOR AT FWD GALLEY AREA IAW AMM - [SDR SWAA2026041778571](https://openairdocs.org/sdr/SWAA2026041778571), Mar 10, 2026: BRACKET. DETERIORATED. DETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY DOOR AT FWD GALLEY AREA. REPLACED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY DOOR AT FWD GALLEY AREA IAW AMM 25- - [SDR SWAA2026041778572](https://openairdocs.org/sdr/SWAA2026041778572), Mar 10, 2026: BRACKET. DETERIORATED. DETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY DOOR AT AFT GALLEY AREA. REPLACED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY DOOR AT AFT GALLEY AREA IAW AMM 25- - [SDR SWAA2026041778573](https://openairdocs.org/sdr/SWAA2026041778573), Mar 10, 2026: BRACKET. DETERIORATED. DETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS SERVICE DOOR AT AFT GALLEY AREA. REPLACED HARDWARE GIRT BAR FLOOR BRACKETS SERVICE DOOR AT AFT GALLEY AREA IAW AMM - [SDR SWAA2026041678332](https://openairdocs.org/sdr/SWAA2026041678332), Mar 10, 2026: SCUFF PLATE. CRACKED. CRACKED SCUFF PLATE, AFT ENTRY DOOR. REPAIRED THE SCUFF PLATE IAW SRM 53-70-15-2R-1, REPAIR 1, PARAGRAPH 4. B, FIGURE 203. - [SDR SWAA2026041678566](https://openairdocs.org/sdr/SWAA2026041678566), Mar 10, 2026: ANGLE. CRACKED. CRACKED ANGLE, LOCATED AFT FACE BS 400 AT LEVEL STR 26L FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02, 51-10-02, ITEM 9, AND DWG 143A7505, SHEET 137, REV - - [SDR SWAA2026042077958](https://openairdocs.org/sdr/SWAA2026042077958), Mar 9, 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 FASTENERS IAW SRM 51-40-02 SRM 51-10-02 ITEM - [SDR SWAA2026042077953](https://openairdocs.org/sdr/SWAA2026042077953), Mar 9, 2026: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 41 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE IAW SRM 51-40-02 ;SRM 51-10-02 PARAGRAPH 9 ;DWG 1 - [SDR SWAA2026042077959](https://openairdocs.org/sdr/SWAA2026042077959), Mar 9, 2026: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET LOCATED BS540 AT LEVEL LBL 6 AT LT AIR CONDITIONING BAYS. REPLACED SUPPORT BRACKET LOCATED BS540 AT LEVEL LBL 6 AT LT AIR CONDITIONING BAY - [SDR SWAA2026041778156](https://openairdocs.org/sdr/SWAA2026041778156), Mar 9, 2026: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE FIXED TRAILING EDGE AT LEVEL ORSS274 RT WING. REPLACED SUPPORT ANGLE FIXED TRAILING EDGE AT LEVEL ORSS274 RT IAW B737-800 SRM 51-40-02; SRM - [SDR SWAA2026041677956](https://openairdocs.org/sdr/SWAA2026041677956), Mar 9, 2026: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM, BS 947.5, RBL 51, WL 208.1. REPAIRED THE FLOORBEAM IAW SRM 53-70-51-2R-5, REPAIR 5, ALTERNATIVE 2, AND EA 26-153-00786. - [SDR SWAA2026042077659](https://openairdocs.org/sdr/SWAA2026042077659), Mar 8, 2026: WEB. CRACKED. CRACKED WEB, BS 344 - 360, RBL 33, WL 208.1 REPLACED THE WEB LOCATED IAW SRM 51-40-02, AND DRAWING 141A5400, SHEET 33, REV -. - [SDR SWAA2026042077658](https://openairdocs.org/sdr/SWAA2026042077658), Mar 8, 2026: WEB. CRACKED. CRACKED WEB, BS 277 TO 294.5, RBL 1, WL 208.1. REPLACED WEB LOCATED BTW BS 277 TO BS 294.5 RBL 1 WL 208.1 AT FWD GALLEY AREA IAW SRM B737-800 SRM 51-10-02 ITEM - [SDR SWAA2026042077809](https://openairdocs.org/sdr/SWAA2026042077809), Mar 8, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE LOCATED BS 695 BL 0 WL 208.1 RT SIDE AT PASSENGER CABIN. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 273A9111 - [SDR SWAA2026042077660](https://openairdocs.org/sdr/SWAA2026042077660), Mar 8, 2026: WEB. CRACKED. CRACK INTERCOSTAL WEB LOCATED BTW BS 344 TO BS 360 LBL 11 WL 208.1 AT FWD GALLEY AREA. REPLACED THE INTERCOSTAL WEB LOCATED BTW BS 344 TO BS 360 LBL 11 WL 208.1 - [SDR SWAA2026042077655](https://openairdocs.org/sdr/SWAA2026042077655), Mar 8, 2026: ANGLE. CRACKED. CRACK ON ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA. REPLACED ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GAL - [SDR SWAA2026042077656](https://openairdocs.org/sdr/SWAA2026042077656), Mar 8, 2026: ANGLE. CRACKED. CRACK ON ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA. FAULT RESOLVED ON OTHER FAULT SEE TTG8Q01AV4EG. - [SDR SWAA2026042077657](https://openairdocs.org/sdr/SWAA2026042077657), Mar 8, 2026: ANGLE. CRACKED. CRACK ON INNER CHORD LOCATED BS 303.9 AT LEVEL STR 17L AT FWD GALLEY AREA. REPLACED INNER CHORD AND FASTENERS LOCATED BTW BS270 TO BS360 AT LEVEL STR 17L IAW SR - [SDR SWAA2026041677654](https://openairdocs.org/sdr/SWAA2026041677654), Mar 8, 2026: FLOORBEAM. CORRODED. CORRODED FLOORBEAM, BS 344, LBL 7, WL 208.1. REPAIRED THE FLOORBEAM IAW EA 26-153-00771. 26-153-00771-WIP1, 26-153-00771-WIP2, AND 26-153-00771-WIP3. All 133: https://openairdocs.org/deregistered/N8638A-2026-06-25/reports.md ## Other aircraft with N8638A - [Cancelled 1965-05-20](https://openairdocs.org/deregistered/N8638A-1965-05-20): Beech A35, S/N D-2048. Owner: [Henery A Smith](https://openairdocs.org/faa-owner/HENERY%20A%20SMITH), [Richmond, CA](https://openairdocs.org/faa-place/CA/Richmond) --- 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.