# N419WN: 2001 Boeing 737-7H4, registration cancelled 2025-10-01 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 1, 2025 - Status when cancelled: Valid registration - Airframe: [Boeing 737-7H4](https://openairdocs.org/model/boeing-737-7h4) (registry code 1384404) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 29824 - Year built: 2001 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 3, 2001 - Certificate issued: May 10, 2002 - Last registry action: January 22, 2023 - Mode S code: A4F790 - 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/N419WN - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=419WN - Page: https://openairdocs.org/deregistered/N419WN-2025-10-01 From the FAA registry file of October 29, 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 737-7H4: https://openairdocs.org/model/boeing-737-7h4.md ## Service difficulty reports (305, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SWAA2025061782241](https://openairdocs.org/sdr/SWAA2025061782241), Jun 16, 2025: BATTERY PACK. INOPERATIVE. RIGHT OVERWING EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED R/H SIDEWALL BATTERY PACK PER AMM 33-51-06. - [SDR SWAA2025050565418](https://openairdocs.org/sdr/SWAA2025050565418), Apr 29, 2025: POWER SUPPLY. DAMAGED. DURING EMERGENCY EXIT LIGHT TROUBLESHOOTING FOUND DAMAGED POWER SUPPLY (M1670)<[01] REMOVED AND REPLACED DAMAGED POWER SUPPLY (M1670) REF AMM 33-51-06. OPS CHEC - [SDR SWAA2025050565417](https://openairdocs.org/sdr/SWAA2025050565417), Apr 29, 2025: BATTERY PACK. INOPERATIVE. OVER-WING EMERGENCY EXIT AISLE LIGHTS AND GROUND ILLUMINATION LIGHTS INOPS<[01] REMOVED AND REPLACED EMERGENCY EXIT POWER SUPPLY BATTERY PACK (M1670) REF AMM 33 - [SDR SWAA2025041524566](https://openairdocs.org/sdr/SWAA2025041524566), Apr 14, 2025: SIGN. LOOSE. CAPT SIDE OVER WING EXIT SIGN PANEL LOOSE <[01]. RESECURED EXIT SIGN PANEL IAW AMM 33-51-01. - [SDR SWAA2025011586135](https://openairdocs.org/sdr/SWAA2025011586135), Jan 15, 2025: LAMP. INOPERATIVE. LEFT AND RIGHT AFT OVERWING EMERGENCY EXIT LIGHTS INOP<[01] REMOVED AND REPLACED LEFT AND RIGHT AFT OVERWING EMERGENCY EXIT LAMPS AS REQUIRED PER AMM 33-51-04; - [SDR SWAA2024121777330](https://openairdocs.org/sdr/SWAA2024121777330), Dec 14, 2024: SIGN. LOOSE. FWD EMERGENCY EXIT SIGN CAME LOOSE.<[01] RESECURED FWD EMERGENCY EXIT SIGN PER SIP. - [SDR SWAA2024091637915](https://openairdocs.org/sdr/SWAA2024091637915), Sep 14, 2024: HANDLE. LOOSE. PLASTIC ASSIST HANDLE ON INSIDE OF FWD ENTRY DOOR LOOSE<[01] RESECURED DOOR ASSIST HANDLE ON FWD ENTRY DOOR PER AMM 52-11-31 OPS CHECK NORMAL - [SDR SWAA2024061401165](https://openairdocs.org/sdr/SWAA2024061401165), Jun 13, 2024: SLIDER. CRACKED. LH HORIZONTAL STABLIZER; UPPER FWD SLIDER CRACKED<[01] REMOVED AND REPLACED WITH NEW; L/H HORIZONTAL STABILIZER; UPPER FWD SLIDER REF AMM 53-31-31 - [SDR SWAA2024061401162](https://openairdocs.org/sdr/SWAA2024061401162), Jun 13, 2024: SEAL. CRACKED. RH HORIZONTAL UPPER FWD SLIDER CRACKED<[01] REPLACED RH HORIZONTAL UPPER FWD SLIDER REF MM 53-31-31.
01 - REMOVED AND REPLACED PER [AMM 53-31-31-000-802-NG ( - [SDR SWAA2024061401167](https://openairdocs.org/sdr/SWAA2024061401167), Jun 13, 2024: SKIN. CRACKED. POSSIBLE CRACK ON RH HORIZONTAL STABILIZER LOWER SKIN; JUST FWD OF REAR SPAR; APROX. LE STA 221. VERIFIED CRACK AND ITS ENDS PER NDT PART 6; 51-00-00; PROCEDURE - [SDR SWAA2023103116409](https://openairdocs.org/sdr/SWAA2023103116409), Oct 30, 2023: SLIDE. LOOSE. MAIN CABIN DOOR SLIDE LOOSE<[01] REINSTALLLED L1 DOOR SLIDE. REF MT 725-61-06. - [SDR SWAA2023091198607](https://openairdocs.org/sdr/SWAA2023091198607), Sep 9, 2023: SLIDE. LOOSE. AFT ENTRY SLIDE IS LOOSE<[01] RESECURED AFT ENTRY DOOR SLIDE IAW MT 725-61-06. A/C OK FOR SERVICE. - [SDR SWAA2023081086401](https://openairdocs.org/sdr/SWAA2023081086401), Aug 7, 2023: BRACKET. CRACKED. BRACKET CRACKED UNDER 193B PANEL AT APPROXIMATELY RBL15 STA.663 COMMON TO THE RH ACM EXHAUST DUCT SEAL ON THE I/B SIDE.<[01] CW;[02] C/W;[03] CW - [SDR SWAA2023080284878](https://openairdocs.org/sdr/SWAA2023080284878), Aug 1, 2023: SIGN. BROKEN. CENTER CABIN OVERHEAD EMERGENCY LIGHT BROKEN<[01] REMOVED AND REPLACED OVERHEAD EMERGENCY EXIT SIGN IAW M/M 33-51-03 - [SDR SWAA2023072073668](https://openairdocs.org/sdr/SWAA2023072073668), Jul 1, 2023: ANGLE. CRACKED. L/H WING FWD BOOST POMP AREA UPPER ANGLE CRACK<[01] REMOVED AND REPLACED DAMAGE ANGLE UPPER OF BOOST POMP ;PER REF. SRM 51-40-02-0G-0 AND DRAWING # 112A2004;[02 - [SDR SWAA2023072073221](https://openairdocs.org/sdr/SWAA2023072073221), Jun 30, 2023: ANGLE. CRACKED. L/H FUS WTB STA. 540 STR 23 ANGLE CRACKED<[01] REMOVED AND REPLACED NEW ANGLE [CLIP] AT L/H FUS WTB STA540 STR 23 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1 - [SDR SWAA2023072073011](https://openairdocs.org/sdr/SWAA2023072073011), Jun 29, 2023: BATTERY PACK. INOPERATIVE. CABIN EMERGENCY LIGHTS ARE INOPERATIVE AT 9ABC;12ABC AND 13DEF<[01] REPLACED BATTERY PACK (M7670) AS PER REF AMM 33-51-06-960-805 AND RELAMPED 13DEF TEST NORMAL - [SDR SWAA2023072472687](https://openairdocs.org/sdr/SWAA2023072472687), Jun 28, 2023: SPAR. BROKEN. LT WING REAR SPAR LOWER CORD AT IRSS 211 SUPPORT BRACKET IS BROKEN. 124-008<[01] REMOVED AND REPLACED CLIP AT LT/WING REAR SPAR LOWER CORD AT IRSS 211 REF SRM 5 - [SDR SWAA2023072472683](https://openairdocs.org/sdr/SWAA2023072472683), Jun 28, 2023: FITTING. CRACKED. RT WING RIB CONTROL PANEL LOWER FWD SUPPORT SEALIS CRACKED.<[01] REMOVED AND REPLACED RT. WING T/E FITTING PER SRM 51-40-02-0G-0;[02] VERIFIED STEP#1 - [SDR SWAA2023072073665](https://openairdocs.org/sdr/SWAA2023072073665), Jun 28, 2023: VAPOR BARRIER. CRACKED. LT VAPOR BARRIER IS CRACKED AT KEEL BEAM STA 663 LBL 5'<[01] REPAIRED DAMAGED AREA AT LT VAPOR BARRIER PER B737 SRM 51-70-04-2R-0 PARAGRAPH(4.L.7) MATERIAL USED - [SDR SWAA2023072072693](https://openairdocs.org/sdr/SWAA2023072072693), Jun 28, 2023: PANEL. CRACKED. R/H WING T/E ACCESS PANEL 661BB LOWER SKIN SURFACE HAS CRACKS AROUND FASTENER HOLES.<[01] APPLIED REPAIR IN DAMAGED AREA ( FASTENER HOLES.) AS PER B737 SRM 51-7 - [SDR SWAA2023072072054](https://openairdocs.org/sdr/SWAA2023072072054), Jun 27, 2023: FASTENER. PULLED. L/E TO FRONT SPAR I/B OF NACELLE STRUT AT AFT OF NACELLE STRUT I/B POSITION HAS ONE FASTENER PULLED OUT ON REPAIRED AREA.<[01] REMOVED AND REPLACED FASTENER AT - [SDR SWAA2023062771700](https://openairdocs.org/sdr/SWAA2023062771700), Jun 26, 2023: LIGHT. INOPERATIVE. RH OVER-WING EMER LIGHT INOP.<[01] R/R RH OVER-WING EMER LIGHT PER AMM 33-51-04. OPS CHECK GOOD. - [SDR SWAA2023032117898](https://openairdocs.org/sdr/SWAA2023032117898), Mar 17, 2023: LIGHT. INOPERATIVE. FORWARD ENTRY DOOR EXIT ASSEMBLY BROKEN<[01] R/R L1 DOOR EMERGENCY EXIT DOOR LIGHT CONNECTORS D3662; D3664 REF SWPM 20-30-12; WDM 33-51-21; NO HELP; R/R M1675 P - [SDR SWAA2023021502860](https://openairdocs.org/sdr/SWAA2023021502860), Feb 14, 2023: SLIDE. OUT OF POSITION. FWD FLIGHT ATTENDANT REPORTS: FWD SERVICE DOOR SLIDE; DROOPING.<[01] REPOSITIONED SLIDE ASSY IAWMM 25-66-01 REF MT 725-66-01 - [SDR SWAA2023020900919](https://openairdocs.org/sdr/SWAA2023020900919), Feb 9, 2023: BATTERY. INOPERATIVE. BOTH FORWARD EMERGENCY LIGHT POWER SUPPLIES INOP<[01] R&R BATTERY PACKS REF AMM 33-51-06 OPS CHECK GOOD NO OTHER DEFECTS NOTED AT THIS TIME - [SDR SWAA2022122184039](https://openairdocs.org/sdr/SWAA2022122184039), Dec 21, 2022: LIGHT. INOPERATIVE. ALL EMERGENCY LIGHTS IN FWD PART OF AIRCRAFT; BOTH INTERNAL AND EXTERNAL INOP<[01] CHARGED EMERGENCY LIGHTS BATTERY PACKS PER AMM 33-51-06. OPS CHECK GOOD. - [SDR SWAA2022112172677](https://openairdocs.org/sdr/SWAA2022112172677), Nov 18, 2022: BATTERY PACK. INOPERATIVE. AFT L/H BATTERY PACK WILL NOT CHARGE AFT L/H BATTERY PACK WILL NOT CHARGE. / [01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06. - [SDR SWAA2022101459422](https://openairdocs.org/sdr/SWAA2022101459422), Oct 13, 2022: ENGINE. FAILED. ENGINE FAILURE #1 ENGINE WHILE CLIMBING THROUGH FL 290. ENGINE EGT LIMITS EXCEEDED. ENGINE REPLACEMENT WAS PREVIOUSLY COMPLIED WITH. - [SDR SWAA2022072532038](https://openairdocs.org/sdr/SWAA2022072532038), Jul 21, 2022: FIRE BOTTLE. LOW. FLIGHT DECK FIRE EXTINGUISHER SHOW LOW PRESSURE / [01] R/R'D F/D HALON FIRE EXTINGUISHER PER AMM 26-26-01. - [SDR SWAA2022011259533](https://openairdocs.org/sdr/SWAA2022011259533), Jan 9, 2022: LIGHT. MISSING. OVERWING EMERGENCY EXIT SIGN (AIRCRAFT LEFT/FLOOR) MISSING ; OVERWING EMERGENCY EXIT SIGN (AIRCRAFT LEFTFLOOR) MISSING / [01] INSTALLED EMERG EXIT SIGN COVER CA - [SDR SWAA2021110540183](https://openairdocs.org/sdr/SWAA2021110540183), Nov 3, 2021: FLOOR PANEL. ELONGATED. WING TO BODY PANEL 193D HAS 5(EA) FASTENER HOLES ELONGATED. ; / [01] EA 21-153-03253 ADDED AS SUBTASK.; [02] CW - [SDR SWAA2021110540184](https://openairdocs.org/sdr/SWAA2021110540184), Nov 3, 2021: FLOOR PANEL. ELONGATED. WING TO BODY PANEL 194E HAS 2(EA) FASTENER HOLES ELONGATED ; / [01] CW; [02] REFERENCE FAULT TTG8Q0093H6G AND EA 21-153-03253; [03] ADDED REFERENCE FOR COMPLIAN - [SDR SWAA2021080289654](https://openairdocs.org/sdr/SWAA2021080289654), Jun 30, 2021: STRINGER. CRACKED. CRACK STRINGER 23L LOCATED BS 540 FWD CARGO COMPARTMENT ; 2021-295482 / REPAIRED STRINGER 23L LOCATED BS 500D + 10 TO BS 540 FWD CARGO COMPARTMENT IAW B737-700 - [SDR SWAA2021080289656](https://openairdocs.org/sdr/SWAA2021080289656), Jun 30, 2021: STRINGER. CRACKED. CRACK STRINGER 27L LOCATED BS 540 FWD CARGO COMPARTMENT ; 2021-295486 / REPAIRED STRINGER 27L LOCATED BTW 500D + 10 TO BS 540 FWD CARGO COMPARTMENT IAW B737-700 - [SDR SWAA2021080289655](https://openairdocs.org/sdr/SWAA2021080289655), Jun 30, 2021: STRINGER. CRACKED. CRACK STRINGER 26L LOCATED BS 540 FWD CARGO COMPARTMENT ; 2021-295485 / [01] TOOL USED: CALIPER P/N 500-197-30; S/N A 18234369; DUE DATE 19-AUG-21.; [02] TOOL U - [SDR SWAA2021080288509](https://openairdocs.org/sdr/SWAA2021080288509), Jun 27, 2021: SPAR. CRACKED. CRACK FRONT SPAR ANGLE LOCATED ABOVE FUEL BOOST PUMP IFSS 120 APROX AT RT WING ; 2021-295513 / [01] TOOL USED: DIGITAL CALIPER P/N: 500-464; D/N: 15331926; DUE - [SDR SWAA2021080287855](https://openairdocs.org/sdr/SWAA2021080287855), Jun 25, 2021: STRINGER CLIP. CRACKED. CRACK TIE CLIP LOCATED ST BS 277 STRINGER 10R AT PASSENGER CABIN ; 2021-295473 / [01] REMOVED TIE CLIP LOCATED BS 277 STR 10R AT PASSENGER CABIN I.A.W. B737-700 - [SDR SWAA2021080287856](https://openairdocs.org/sdr/SWAA2021080287856), Jun 25, 2021: CARGO TRACK. CRACKED. CRACK BILGE AREA ON CARGO TRACK AT LEVEL BS 500 AND STR 27R RBL 13.84 AT FWD CARGO COMPARTMENT ; 2021-295474 / [01] TOOL USED DIGITAL CALIPER P/N:500-197-30; S/ - [SDR SWAA2021080287854](https://openairdocs.org/sdr/SWAA2021080287854), Jun 25, 2021: FRAME. CRACKED. CRACK FRAME ON BS 312 AT UPPER FWD CORNER CUT OUT FWD ENTRY DOOR FWD GALLEY AND LAV ; 2021-295472 / [01] TOOL USED: PRECISION RADIUS GAUGE: PN S167C; SN:AE-3594 - [SDR SWAA2021080287862](https://openairdocs.org/sdr/SWAA2021080287862), Jun 25, 2021: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED BETWEEN BS 380 AND BS 400 BL 0 AT PASSENGER CABIN ; 2021-295488 / [01] REPLACED NEW SUPPORT ANGLE LOCATED BETWEEN BS 380 AND BS 400 - [SDR SWAA2021080287863](https://openairdocs.org/sdr/SWAA2021080287863), Jun 25, 2021: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED BETWEEN BS 380 AND BS 400 RBL 10 AT PASSENGER CABIN ; 2021-295483 / [01] REPLACED ANGLE AND FASTENERS LOC BETWEEN BS380 TO BS400 RBL - [SDR SWAA2021080287868](https://openairdocs.org/sdr/SWAA2021080287868), Jun 25, 2021: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED BETWEEN BS 380 AND BS 400 LBL 14 AT PASSENGER CABIN ; 2021-295489 / [01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: - [SDR SWAA2021080287859](https://openairdocs.org/sdr/SWAA2021080287859), Jun 25, 2021: WEB. CRACKED. CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 328 TO BS 344 AT LEVEL LBL 47 FWD GALLEY AND LAV ; 2021-295487 / [01] REPLACED WEB-INTERCOSTAL FLOOR - [SDR SWAA2021080287867](https://openairdocs.org/sdr/SWAA2021080287867), Jun 25, 2021: WEB. CRACKED. CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 RBBL 34 FWD GALLEY AND LAV ; 2021-295490 / [01] REPLACED WEB-INTERCOSTAL LOC. FLOOR ST - [SDR SWAA2021080287865](https://openairdocs.org/sdr/SWAA2021080287865), Jun 25, 2021: WEB. CRACKED. CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 294.5 TO BS 312 AT LEVEL BL0 FWD GALLEY AND LAV ; 2021-295484 / [01] REMOVED WEB-INTERCOSTAL LOCATED - [SDR SWAA2021080287864](https://openairdocs.org/sdr/SWAA2021080287864), Jun 25, 2021: FRAME. CRACKED. CRACK FRAME BS 400 AT LEVEL STRINGER 8L AT PASSENGER CABIN ; 2021-295478 / [01] TOOL USED: CALIPER P/N 500-197-30; S/N A18234369; DUE DATE 19-AUG-21; [02] INSTA - [SDR SWAA2021080287858](https://openairdocs.org/sdr/SWAA2021080287858), Jun 25, 2021: FRAME. CRACKED. CRACK FRAME BS 440 AT LEVEL S-8L AT PASSENGER CABIN ; 2021-295477 / [01] TOOL USED: CALIPER P/N 500-197-30; S/N A18234369; DUE DATE 19-AUG-21.; [02] INSTALLED R - [SDR SWAA2021080287857](https://openairdocs.org/sdr/SWAA2021080287857), Jun 25, 2021: FRAME. CRACKED. CRACK FRAME BS 380 AT LEVEL S-8L AT PASSENGER CABIN ; 2021-295479G / [01] TOOL USED: CALIPER P/N 500-197-30; S/N A18234369; DUE DATE 19-AUG-21; [02] INSTALLED R - [SDR SWAA2021080287866](https://openairdocs.org/sdr/SWAA2021080287866), Jun 25, 2021: STIFFENER. CRACKED. CRACK FLOOR STRUCTURE STIFFENER BS 540 BETWEEN LBL 24.5 AND BL 0 AT PASSENGER CABIN ; 2021-295460 / [01] REPLACED NEW STIFFENER AND FASTENERS LOC. FLOOR STRUCTU All 305: https://openairdocs.org/deregistered/N419WN-2025-10-01/reports.md --- 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.