# N413WN: 2001 Boeing 737-7H4, registration cancelled 2026-06-05

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 5, 2026
- 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: 29819
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 3, 2001
- Certificate issued: March 22, 2002
- Last registry action: September 22, 2023
- Mode S code: A4E146
- 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/N413WN
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=413WN
- Page: https://openairdocs.org/deregistered/N413WN-2026-06-05

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 (307, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR SWAA2025072393464](https://openairdocs.org/sdr/SWAA2025072393464), Jul 20, 2025: LENS. LOOSE. EMERGENCY EXIT LIGHT LENS LOOSE ROW 3 DEF, SECURED LENS WITH TAPE. OK TO CONTINUE PER MEL 3-15-02 SP-1B . REINSTALLED EMERGENCY LIGHT LENS AT ROW 3DEF PER AMM 3
- [SDR SWAA2025063086111](https://openairdocs.org/sdr/SWAA2025063086111), Jun 27, 2025: FLOOR PANEL. CRACKED. FWD CARGO BIN HAS FWD CRACK ON FLOOR<[01] PREFORMED REPAIR OF FWD CARGO AFT FLOOR PANEL (120CF) PER SRM 53-00-53-1A-1 TO BE REINSPECTED EVERY 400 CYCLE MUST REP
- [SDR SWAA2025063085969](https://openairdocs.org/sdr/SWAA2025063085969), Jun 26, 2025: FLOOR PANEL. CRACKED. FWD CARGO BIN HAS FWD CRACK ON FLOOR <[01]. OK TO CONTINUE AS PER MEL 25-16-01 SP1B AUTH NO 263657; [02] PERFORMED REPAIR ON FWD CARGO PIT AFT FLOOR PANEL 120CF
- [SDR SWAA2025050767579](https://openairdocs.org/sdr/SWAA2025050767579), May 5, 2025: GIRT BAR. OUT OF ADJUST. AFT FLT ATT NDT REPORTS CAPT SIDE GIRT BAR CATCHING ON DOOR FRAME. ADJUSTED GIRT BAR IAW AMM 25-66-01.
- [SDR SWAA2025041725075](https://openairdocs.org/sdr/SWAA2025041725075), Apr 16, 2025: SEAT. LOOSE. PASSENGER CABIN SEAT ROWS 1DEF; 2DEF; 3DEF; 5ABC; 8ABC AND 11DEF LOOSE IN SEAT TRACKS <[01]. ADJUSTED SEAT ROWS 1DEF; 2DEF; 3DEF; 5ABC; 8ABC; & 11DEF IN REF TO 
- [SDR SWAA2024121878927](https://openairdocs.org/sdr/SWAA2024121878927), Dec 17, 2024: GIRT BAR. OUT OF ADJUST. CAPT AFT DOOR OPENED FROM OUTSIDE WITH GIRT BAR ATTACHED<[01] INSPECTED AFT DOOR SLIDE ON CAPT SIDE IN REFERENCE TO AMM 25-66-00 NO FAULTS NOTED
- [SDR SWAA2024090934916](https://openairdocs.org/sdr/SWAA2024090934916), Sep 6, 2024: COVER. OUT OF ADJUST. AFT GALLEY SLIDE DOES NOT STOW PROPERLY<[01] READJUSTED AFT ENTRY DOOR SLIDE COVER PER SIP. NO OTHER DEFECTS NOTED.
- [SDR SWAA2024072516217](https://openairdocs.org/sdr/SWAA2024072516217), Jul 24, 2024: SLIDE. DISLODGED. FLIGHT CREW LEFT GIRT BAR ARMED ON FWD SERVICE DOOR AND SLIDE CAME OUT AND PARTLY UNPACKED.<[01] REMOVED AND REPLACED FWD SERVICE DOOR SLIDE IAW AMM 25-66-01 AN
- [SDR SWAA2024050783114](https://openairdocs.org/sdr/SWAA2024050783114), May 6, 2024: GIRT BAR. LOOSE. AFT ENTRY SLIDE GIRT BAR LOOSE<[01] RE-ADJUSTED GIRT BAR AND AFT ENTRY SLIDE REF MT 725-61-06
- [SDR SWAA2023082490844](https://openairdocs.org/sdr/SWAA2023082490844), Aug 17, 2023: RIB. CRACKED. L/H HORIZONTAL STABILIZER REMOVABLE L/E; #4 (FROM I/B) UPPER RIB CRACKED. (MARKED)<[01] SRM 55-10-09-0I-1 IDENTIFICATION AND SRM 53-10-09-1A-1 ALLOWABLE DAMAGE 
- [SDR SWAA2023082490845](https://openairdocs.org/sdr/SWAA2023082490845), Aug 17, 2023: RIB. CRACKED. R/H HORIZONTAL STABILIZER REMOVABLE L/E; #2 (FROM I/B) LOWER RIB CRACKED. (MARKED)<[01] SRM 55-10-09-0I-1 IDENTIFICATION AND SRM 53-10-09-1A-1 ALLOWABLE DAMAGE 
- [SDR SWAA2023082489571](https://openairdocs.org/sdr/SWAA2023082489571), Aug 14, 2023: STIFFENER. CRACKED. REJECTED: L/H H-STAB RIB #7 STIFFENER #4 UPPER RADIUS CRACKED: SRM APPLICABILITY VALIDATION FOR REPAIR; AND NDT/VISUAL INSPECTIONS NOT PERFORMED AFTER DAMAGE RE
- [SDR SWAA2023082487322](https://openairdocs.org/sdr/SWAA2023082487322), Aug 9, 2023: SUPPORT BRACKET. CRACKED. RT WING T/E PANEL 651FB FWD CENTER SUPPORT BRACKET IS CRACKED<[01] REMOVED AND REPLACED CRACKED FWD SUPPORT BRACKET ON PNL 651FB PER SRM 51-40-02-0G-0;[02] ADD 
- [SDR SWAA2023082487069](https://openairdocs.org/sdr/SWAA2023082487069), Aug 8, 2023: STRINGER. CRACKED. AREA AFT OF FORWARD CARGO BAY; STR 23R IS CRACKED AT AFT FASTENER BS 520+18<[01] PARTIAL STEP 1;[02] THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-00-03-2R-1 (REPA
- [SDR SWAA2023082487068](https://openairdocs.org/sdr/SWAA2023082487068), Aug 8, 2023: STRINGER. CRACKED. AREA AFT OF FORWARD CARGO BAY; STR 26R IS CRACKED AT AFT FASTENER BS 520+18<[01] PARTIAL STEP 1;[02] REPAIRED AREA AFT OF FORWARD CARGO BAY; STR 26R FROM BS 500
- [SDR SWAA2023082487066](https://openairdocs.org/sdr/SWAA2023082487066), Aug 8, 2023: STRINGER. CRACKED. AREA AFT OF FORWARD CARGO BAY; STR 23L IS CRACKED AT AFT FASTENER BS 520+18<[01] COMPLETED STEPS 1;2;3 AND 5;[02] THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-00-
- [SDR SWAA2023082486832](https://openairdocs.org/sdr/SWAA2023082486832), Aug 8, 2023: STIFFENER. CRACKED. L/H H-STAB RIB #5 STIFFENERS 2 & 3 LOWER RADII ARE CRACKED.<[01] REMOVED THE DAMAGED PART AT LH HORIZONTAL STABILIZER STA 129.50 RIB 2ND AND 3RD VERTICAL STIFFE
- [SDR SWAA2023082486834](https://openairdocs.org/sdr/SWAA2023082486834), Aug 8, 2023: STIFFENER. CRACKED. CRACK INDICATION ON L/H H-STAB RIB #7 STIFFENER #4 UPPER RADIUS.<[01] REJECTED: L/H H-STAB RIB #7 STIFFENER #4 UPPER RADIUS CRACKED: THE SRM APPLICABILITY VALID
- [SDR SWAA2023082486833](https://openairdocs.org/sdr/SWAA2023082486833), Aug 8, 2023: STIFFENER. CRACKED. R/H H-STAB RIB 4 #3 STIFFENER LOWER RADIUS IS CRACKED.<[01] REMOVED THE DAMAGED PART AT RH HORIZONTAL STABILIZER STA 120.30 RIB 3RD VERTICAL STIFFENER IAW SRM 5
- [SDR SWAA2023082387321](https://openairdocs.org/sdr/SWAA2023082387321), Aug 8, 2023: SCUFF PLATE. CRACKED. AFT CARGO BAY FORWARD CORNER SCUFF PLATE IS CRACKED<[01] WELDED CRACK ON AFT CARGO BAY FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM
- [SDR SWAA2023082387067](https://openairdocs.org/sdr/SWAA2023082387067), Aug 8, 2023: STRINGER. CRACKED. AREA AFT OF FORWARD CARGO BAY; STR 27R IS CRACKED AT AFT FASTENER BS 520+18<[01] PARTIAL STEP 1;[02] REPAIRED AREA AFT OF FORWARD CARGO BAY; STR 27R FROM BS 500
- [SDR SWAA2023082387065](https://openairdocs.org/sdr/SWAA2023082387065), Aug 8, 2023: STRINGER. CRACKED. AREA AFT OF FORWARD CARGO BAY; STR 24L IS CRACKED AT AFT FASTENER BS 520+18<[01] COMPLETED STEPS 1;2;3 AND 5;[02] REPAIRED AREA AFT OF FORWARD CARGO BAY; STR 24
- [SDR SWAA2023082387064](https://openairdocs.org/sdr/SWAA2023082387064), Aug 8, 2023: STRINGER. CRACKED. AREA AFT OF FORWARD CARGO BAY; STR 26L IS CRACKED AT AFT FASTENER BS 520+18<[01] COMPLETED STEPS 1;2;3 AND 7;[02] REMOVED DAMAGED SECTION OF STR 26L BETWEEN BS 
- [SDR SWAA2023082486619](https://openairdocs.org/sdr/SWAA2023082486619), Aug 7, 2023: PANEL. CRACKED. WING CENTER SECTION BREAK PANEL IS CRACKED AT BS 540; RBL 1; WL 208<[01] REMOVED AND INSTALLED NEW BREAK PANEL AT WING CENTER SECTION BS 540; PER SRM 51-40-02 A
- [SDR SWAA2023082486620](https://openairdocs.org/sdr/SWAA2023082486620), Aug 7, 2023: ATTACH ANGLE. CRACKED. WING CENTER SECTION CABLE INTERCOSTAL LOWER ATTACH ANGLE IS CRACKED AT BS 685+7; RBL 24; WL 203<[01] VERIFIED CORRECTIVE ACTION PARTIAL ITEMS AND MEASUREMENT FI
- [SDR SWAA2023082486621](https://openairdocs.org/sdr/SWAA2023082486621), Aug 7, 2023: ATTACH ANGLE. CRACKED. WING CENTER SECTION CABLE INTERCOSTAL LOWER ATTACH ANGLE IS CRACKED AT BS 685+7; LBL 24; WL 203<[01] VERIFIED CORRECTIVE ACTION PARTIAL ITEMS AND MEASUREMENT FI
- [SDR SWAA2023082386622](https://openairdocs.org/sdr/SWAA2023082386622), Aug 7, 2023: FRAME. CRACKED. BS 312 FRAME IS CRACKED IN THE LOWER RADIUS AT FED HEADER SUPPORT<[01] REPAIRED BS 312 FRAME LOWER RADIUS IAW EA # M-22-153-01244;[02] VERIFIED MEASUREMENT TABL
- [SDR SWAA2023082886355](https://openairdocs.org/sdr/SWAA2023082886355), Aug 6, 2023: PANEL. PULLED. /R/W T/E PANEL 661CB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<[01] R/W T/E PANEL 661CB WITH SEVERAL PULLED FASTENER HOLE ON AFT END WAS REPAIRED IAW
- [SDR SWAA2023082886356](https://openairdocs.org/sdr/SWAA2023082886356), Aug 6, 2023: PANEL. PULLED. R/W T/E PANEL 661BB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<[01] CONDUCTIVE COATED THE TOOLSIDE REPAIR SURFACE; CURED CONDUCTIVE COATING; AND PERFO
- [SDR SWAA2023082886357](https://openairdocs.org/sdr/SWAA2023082886357), Aug 6, 2023: PANEL. PULLED. R/W T/E PANEL 661AB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<[01] R/W T/E PANEL 661AB WITH SEVERAL PULLED FASTENER HOLE ON AFT ENDWAS REPAIRED IAW S
- [SDR SWAA2023082486362](https://openairdocs.org/sdr/SWAA2023082486362), Aug 6, 2023: TRACK. BROKEN. L/H HORIZ STAB UPPER AFT SLIDE SEAL TRACK FOR IS BROKEN<[01] VERIFIED OK TO INSTALL L/H HORIZ STAB UPPER AFT SLIDE SEAL TRACK.;[02] REMOVED AND REPLACE L/H HORI
- [SDR SWAA2023082385853](https://openairdocs.org/sdr/SWAA2023082385853), Aug 4, 2023: BATTERY PACK. UNKNOWN. REMOVE AND REPLACE EMERGENCY EXIT LIGHT BATTERIES PRIOR TO AIRCRAFT DEPARTURE<[01] DOCUMENTATION OF INSTALLED PARTS;[02] ALL STEPS COMPLETE;[03] VERIFIED ALL PA
- [SDR SWAA2022093049110](https://openairdocs.org/sdr/SWAA2022093049110), Sep 29, 2022: PANEL. DAMAGED. 193B MOUNTING HOLE LOCATIONS 1; 14 ; AND 19 HAVE ELONGATED OVERSIZED HOLES / [01] INSTALLED WASHERS AT HOLE LOCATIONS 1; 14; AND 19 PER EA 22-153-02942.
- [SDR SWAA2022051908866](https://openairdocs.org/sdr/SWAA2022051908866), May 17, 2022: LENS. LOOSE. 17ABC CLEAR LENS AT BULLNOSE LOOSE / [01] SECURED LENS IN PLACE WITH BIN TAPE <BR>OK TO CONTINUE PER MEL 25-10-01 SP1B<BR>AUTH 66639;[02] REINSTALLED AREA IGHT 
- [SDR SWAA2022010357368](https://openairdocs.org/sdr/SWAA2022010357368), Dec 31, 2021: BALLAST. INOPERATIVE. RH EMERGENCY OVER WING EXIT SIDE WALL LIGHT OUT ; FLORESCENT LIGHT ON THE EMERG DOOR. OK TO CONTINUE PER MEL 33-2-03 SP1B. R & R BALLAST IAW MM 33-21-00.
- [SDR SWAA2021122254435](https://openairdocs.org/sdr/SWAA2021122254435), Dec 18, 2021: COVER. LOOSE. EMERGENCY LIGHT COVER AT 5DEF FELL OFF ; / [01] SECURED LIGHT COVER AT 5DEF IAW AMM 33-51-03 OPS CHECK GOOD
- [SDR SWAA2021121452162](https://openairdocs.org/sdr/SWAA2021121452162), Dec 12, 2021: TIE ROD. BROKEN. SUPPLEMENTAL INFORMATION: L/H FIXED LOWER TE PANEL 551FB HAS BROKEN SUPPORT STUTS AT LEADING EDGE INBOARD SIDE. ; / [01] R/R TWO BROKEN TIE RODS ON INBOARD FIXE
- [SDR SWAA2021112446110](https://openairdocs.org/sdr/SWAA2021112446110), Nov 21, 2021: LIGHT. INOPERATIVE. SUPPLEMENTAL INFORMATION: LEFT WING EMERGENCY EXIT DOOR OUTSIDE EMERGENCY LIGHT INOP ; / [01] RELAMPED LEFT OVERWING EMERGENCY LIGHT IAW AMM 33-51-04
- [SDR SWAA2021102232413](https://openairdocs.org/sdr/SWAA2021102232413), Sep 27, 2021: NONE. CRACKED. GIRT TUBE END CRACKED OUT / [01] R&R GIRT TUBE IAW CMM 25-66-17.; [02] C/W
- [SDR SWAA2021092018033](https://openairdocs.org/sdr/SWAA2021092018033), Sep 16, 2021: DOOR. OUT OF ADJUST. ON LANDING FWD ENTRY DOOR HANDLE POPPED UP A LITTLE AND FWD ENTRY LIGHT CAME ON. 2 OUT OF 3 LANDINGS. / [01] ADJUSTED FWD ENTRY DOOR OPS CHECK GOOD PER AMM 52-1
- [SDR SWAA2021091616781](https://openairdocs.org/sdr/SWAA2021091616781), Sep 12, 2021: LAMP. INOPERATIVE. EMERGENCY LIGHT ROW 4ABL INOP. ; / [01] RELAMPED EMERGENCY LIGHT AT ROW 4ABC PER B7373 AMM 33-51-03-960-801. INSTALLATION TEST; TESTED NORMAL.; [02] VERIFIED
- [SDR SWAA2021091615326](https://openairdocs.org/sdr/SWAA2021091615326), Sep 8, 2021: SCUFF PLATE. CRACKED. AFT CARGO DOOR FORWARD CORNER SCUFF PLATE FOUND CRACKED. ; / [01] LOCATED AND DRILLED NEW AFT CARGO DOOR FORWARD SCUFF PLATE IAW SRM 51-40-05-0G-0. SCUFF PLATE 
- [SDR SWAA2021091614807](https://openairdocs.org/sdr/SWAA2021091614807), Sep 4, 2021: BATTERY PACK. INOPERATIVE. ASSOCIATED EMERGENCY LIGHTS BY LH OVER WING EXIT DOOR WITH BATTERY PACK M1668 ARE INOP. ; OCIATED EMERGENCY LIGHTS BY LH OVER WING EXIT DOOR WITH BATTERY PACK M
- [SDR SWAA2021091613659](https://openairdocs.org/sdr/SWAA2021091613659), Aug 31, 2021: SUPPORT BRACKET. BROKEN. RT WING AT LWR REAR SPAR NEAR OB FWD CORNER OF PNL 651BD HAS PNL SUPPORT BRKT BROKEN 8-98 ; / [01] REMOVED AND REPLACED SUPPORT BRACKET AT RT WING AT LOWER REAR
- [SDR SWAA2021091610592](https://openairdocs.org/sdr/SWAA2021091610592), Aug 23, 2021: LUG. CORRODED. CORROSION-- RH HORIZONTALSTABILIZER CENTER SECTION REAR SPAR LOWER CLEVIS E FWD LUG HAS CORROSION IN BORE. ; / [01] ''PERFORMED EA 21-155-02335. REFER TO FAULT 
- [SDR SWAA2021091610591](https://openairdocs.org/sdr/SWAA2021091610591), Aug 23, 2021: LUG. CORRODED. CORROSION-- RH HORIZONTAL STABILIZER CENTER SECTION REAR SPAR LOWER CLEVIS E AFT LUG HAS CORROSION ON FWD FACE. ; / [01] ''PERFORMED EA 21-155-02335. REFER TO F
- [SDR SWAA2021091609154](https://openairdocs.org/sdr/SWAA2021091609154), Aug 20, 2021: SPAR. CORRODED. CORROSION FOUND ON RH REAR SPAR LOWER LUG K HAS CORROSION ON BOTH FACE OF THE LUG. ; / [01] REPAIR ACCOMPLISHED PER EA 21-155-02337. REFER TO FAULT TTG8Q0065LLA
- [SDR SWAA2021091608697](https://openairdocs.org/sdr/SWAA2021091608697), Aug 19, 2021: BAFFLE. CRACKED. FWD CARGO RT SIDE PLATE BAFFLE CRACKED BTW STA 400 AND 420 ; / [01] REMOVED CRACKED BAFFLE OF FWD. CARGO COMP. STA. 400 TO 420. R/H.; [02] LOCATED AND DRILL NEW
- [SDR SWAA2021091607868](https://openairdocs.org/sdr/SWAA2021091607868), Aug 16, 2021: FITTING. CORRODED. LH O/B REAR SPAR FITTING OF VERTICAL STABILIZER(FTG-LH FWD MAIN)HAS PITTING CORROSION. ; / [01] REMOVED LH O/B REAR SPAR FITTING OF VERTICAL STABILIZER - LH FWD
- [SDR SWAA2021091606993](https://openairdocs.org/sdr/SWAA2021091606993), Aug 14, 2021: CLEVIS. CORRODED. **CORROSION** R/H HORIZONTAL STABILIZER REAR SPAR LOWER AFT CLEVIS 'E'; HAS CORROSION. DOT # 208-151 ; / [01] COMPLETED REPAIR OF RIGHT HORIZONTAL STABILIZER RE

All 307: https://openairdocs.org/deregistered/N413WN-2026-06-05/reports.md

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