# N412WN: 2001 Boeing 737-7H4, registration cancelled 2025-09-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 30, 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: 29818
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 1, 2001
- Certificate issued: March 5, 2002
- Last registry action: September 22, 2023
- Mode S code: A4DD8F
- 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/N412WN
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=412WN
- Page: https://openairdocs.org/deregistered/N412WN-2025-09-30

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 (359, newest 50)

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

- [SDR SWAA2025041524221](https://openairdocs.org/sdr/SWAA2025041524221), Apr 13, 2025: LIGHT. INOPERATIVE. LH AFT EXTERIOR EMERGENCY LIGHT INOP <[01]. RELAMPED LH AFT EXTERIOR EMERGENCY LIGHT REF AMM 33-51-04. OPS CHECK GOOD.
- [SDR SWAA2025031704756](https://openairdocs.org/sdr/SWAA2025031704756), Mar 13, 2025: HANDLE. LOOSE. L1 DOOR INTERIOR HANDLE LOOSE <[01.] TIGHTENED L1 DOOR INTERIOR HANDLE PER AMM 53-13-11.
- [SDR SWAA2025031704755](https://openairdocs.org/sdr/SWAA2025031704755), Mar 13, 2025: HANDLE. LOOSE. R1 DOOR INTERIOR HANDLE LOOSE<[01] TIGHTENED R1 DOOR INTERIOR HANDLE PER AMM 52-41-11.
- [SDR SWAA2024071010270](https://openairdocs.org/sdr/SWAA2024071010270), Jul 7, 2024: SIGN. MISSING. OVERWING EXIT SIGN COVER MISSING RT SIDE<[01] INSTALLED MISSING EXIT SIGN IN REFERENCE TO AMM 33-51-01
- [SDR SWAA2024062002980](https://openairdocs.org/sdr/SWAA2024062002980), Jun 18, 2024: SENSOR. FAULTED. AFTER TAKEOFF GEAR HANDLE IN THE UP POSITION; NOSE GEAR DISAGREE LIGHT ILLUMINATED ON FORWARD PANEL WITH GREEN NOSE GEAR LIGHT ILLUMINATED ON OVERHEAD PANEL. AF
- [SDR SWAA2024052889482](https://openairdocs.org/sdr/SWAA2024052889482), May 24, 2024: BATTERY PACK. INOPERATIVE. FOUND 5 EACH EMERGENCY LIGHT IN AFT LEFT CABIN WONT TURN ON.<[01] R/R AFT L/H EMERGENCY BATTERY PACK PER AMM 33-51-06 AND OPS CHECK GOOD.
- [SDR SWAA2024050983337](https://openairdocs.org/sdr/SWAA2024050983337), May 7, 2024: SLIDE. UNSECURE. FLIGHT ATTENDANT REPORTS L1 DOOR SLIDE NOT SECURED IN CONTAINER<[01] RE-INSTALLED L1 DOOR SLIDE IN THE CONTAINER IAW AMM 25-66-01 AND MT 725-61-06
- [SDR SWAA2024040971555](https://openairdocs.org/sdr/SWAA2024040971555), Apr 6, 2024: GLOWSTRIP. UNSECURE. GLOW STRIP NEAR FWD GALLEY; FO SIDE PULLING UP FROM FLOOR.<[01] RESECURED PHOTOLUMINESCENT STRIP; NEAR FWD GALLEY FO SIDE REF AMM 33-51-15.
- [SDR SWAA2024032567050](https://openairdocs.org/sdr/SWAA2024032567050), Mar 23, 2024: TRANSMITTER. SPLIT. ON APPROACH FLAP SPLIT BETWEEN UP AND 1.<[01] REMOVED AND REPLACED LH FLAP POSITION TRANSMITTER PER AMM 27-58-01. OPS CHECK GOOD AT THIS TIME.
- [SDR SWAA2024032166259](https://openairdocs.org/sdr/SWAA2024032166259), Mar 21, 2024: SLIDE. OUT OF ADJUST. EMERGENCY SLIDE F/O'S SIDE REAR IS HANGING INCORRECTLY<[01] ACCOMPLISHED MT# 725-61-06; SLIDE REMOVAL AND INSTALLATION; FOR POSITION AND SECURITY VERIFICATION.
- [SDR SWAA2024012242687](https://openairdocs.org/sdr/SWAA2024012242687), Jan 19, 2024: SEAL. CRACKED. R/H HORIZONTAL STABILIZER UPPER FORWARD SLIDING SEAL HAS A 3' CRACK ON THE FORWARD LOWER SIDE WHERE IT MEETS THE SLIDING SEAL TRACK.<[01] R&R RH HORIZONTAL STAB
- [SDR SWAA2023103015901](https://openairdocs.org/sdr/SWAA2023103015901), Oct 28, 2023: SLIDE. OUT OF ADJUST. FWD ENTRY DOOR SLIDE IS HANGING DOWN<[01] ADJUSTED FWD ENTRY DOOR SLIDE PER MT 725-61-06. OK TO CONTINUE
- [SDR SWAA2023092002544](https://openairdocs.org/sdr/SWAA2023092002544), Sep 19, 2023: MODULE. FAULTY. AFTER TAKEOFF CAME ON THREE DIFFERENT TIMES. 20KTS SPLIT BETWEEN CA AND F.O. INDICATORS. AFTER VERIFYING AIRSPEED WITH STAY IT WAS THE CAPTAINS SIDE THAT WAS OF
- [SDR SWAA2023061558608](https://openairdocs.org/sdr/SWAA2023061558608), Jun 13, 2023: SIGN. DETACHED. THE EMERGENCY EXIT ROW SIGN IS DETACHED FROM THE CEILING<[01] R/R EMERGENCY EXIT OVERHEAD SIGN IAW MM 33-51-03. OP?S CK NORMAL
- [SDR SWAA2023052451656](https://openairdocs.org/sdr/SWAA2023052451656), May 24, 2023: BATTERY PACK. FAILED. CABIN FWD GALLEY AREA; ONE EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST<[01] REMOVED & REPLACED ONE EMERGENCY BATTERY PACK (M01675); AT FWD GALLEY AREA;
- [SDR SWAA2023042730902](https://openairdocs.org/sdr/SWAA2023042730902), Apr 24, 2023: GIRT BAR. LOOSE. FED AFT GIRT BAR FITTING IS LOOSE<[01] TIGHTENED FED AFT GIRT BAR FITTING; PERFORMED INSTALLATION TEST CHECKS GOOD PER AMM 25-66-02-400-801;[02] INSPECTED AND V
- [SDR SWAA2023042827531](https://openairdocs.org/sdr/SWAA2023042827531), Apr 14, 2023: RIB. CRACKED. CRACK FOUND ON THE RH HORIZONTAL RIB LOWER FLANGE AT STAB STA 193.9; 25' FROM THE LE.<REMOVED DAMAGED IN AN AREA OF 1.8' X 0.8' PER SRM 55-10-09-2R-5 REP 5.; FA
- [SDR SWAA2023042725491](https://openairdocs.org/sdr/SWAA2023042725491), Apr 10, 2023: LIGHT. INOPERATIVE. FWD EMERGENCY EXIT LIGHT AT LEFT OVERWING EXIT IS INOP<[01] RELAMPED IAW AMM 33-51-01-960-801;[02] RELAMPED AND GOOD OP-CHECK IAW AMM 33-51-01-960-801 AND AMM 3
- [SDR SWAA2023042824466](https://openairdocs.org/sdr/SWAA2023042824466), Apr 6, 2023: SKIN. CRACKED. CRACK FOUND RH STAB STA 193.9 25' FROM FWD EDGE 0.4'L<REMOVED DAMAGED SKIN ON R/H HORZ STAB LOWER SKIN STA 193.9 25' FROM FWD EDGE IN AN AREA OF 2.6' X 1.7' IAW
- [SDR SWAA2023042824467](https://openairdocs.org/sdr/SWAA2023042824467), Apr 6, 2023: SKIN. CRACKED. CRACK FOUND LH HORZ STAB LOWER SKIN STA 193.9 17' FROM FWD EDGE .8'L<REMOVED DAMAGED SKIN ON LH HORZ STAB LOWER SKIN STA 193.9 17' FROM FWD EDGE IAW SRM 55-10-0
- [SDR SWAA2023042724461](https://openairdocs.org/sdr/SWAA2023042724461), Apr 6, 2023: STRINGER CLIP. CRACKED. CRACK ON PASSENGER CABIN STRINGER CLIP AT BS 727D STRINGER 4R.<[01] DISPLACED INSULATION BLANKETS AT STRINGER CLIP AT BS 727D STR 4R TO FOM AS PER M/M 25-80-00-
- [SDR SWAA2023042823693](https://openairdocs.org/sdr/SWAA2023042823693), Apr 4, 2023: ANGLE. CORRODED. CORROSION ON ANGLE AT MID CABIN BS663+29 RBL66 WL203.<[01] NO ALLOWABLE LIMITS FOUND DAMAGE TO BE REMOVED I.A.W SRM 51-10-02-0G-0 AND SUBMITTED ENGINEERING FOR 
- [SDR SWAA2023042823696](https://openairdocs.org/sdr/SWAA2023042823696), Apr 4, 2023: ATTACH ANGLE. CRACKED. CRACKED ATTACH ANGLE AT MID CABIN BS663+28 LBL1 WL206.<[01] REMOVED CRACK DAMAGED ATTACH ANGLE AT BS 663+28 LBL 1 WL 206 IAW SRM 51-40-02-0G-0 NO SRM DAMAGE LIM
- [SDR SWAA2023042823697](https://openairdocs.org/sdr/SWAA2023042823697), Apr 4, 2023: ATTACH ANGLE. CRACKED. CRACKED ATTACH ANGLE AT MID CABIN BS663+28 RBL1 WL206.<[01] REMOVED CRACK DAMAGED ATTACH ANGLE AT BS 663+28 RBL 1 WL 206 IAW SRM 51-40-02-0G-0 NO SRM DAMAGE LIM
- [SDR SWAA2023042823699](https://openairdocs.org/sdr/SWAA2023042823699), Apr 4, 2023: ATTACH ANGLE. CRACKED. CRACKED ATTACH ANGLE AT MID CABIN BS663+29 LBL23 WL203.<[01] REMOVED CRACK DAMAGED ATTACH ANGEL AT MID CABIN BS 663+29 LBL 23 WL 203 IAW SRM 51-40-02-0G-0 NO DA
- [SDR SWAA2023042823552](https://openairdocs.org/sdr/SWAA2023042823552), Apr 4, 2023: ANGLE. CORRODED. CORROSION ON ANGLE AT MID CABIN BS719 LBL67 WL203.<[01] NO ALLOWABLE LIMITS FOUND DAMAGE TO BE REMOVED I.A.W SRM 51-10-02-0G-0 AND SUBMITTED ENGINEERING FOR FUR
- [SDR SWAA2023042823553](https://openairdocs.org/sdr/SWAA2023042823553), Apr 4, 2023: ANGLE. CORRODED. CORROSION ON ANGLE AT MID CABIN BS713 LBL63; LBL65 WL203.< REMOVED FOR ACCESS 2EA RIVET AT MID CABIN BS713 LBL63; LBL65 TO REMOVED CORROSION ON ANGLE SURFACE I.
- [SDR SWAA2023042823698](https://openairdocs.org/sdr/SWAA2023042823698), Apr 4, 2023: ATTACH ANGLE. CRACKED. CRACKED ATTACH ANGLE AT MID CABIN BS663+29 RBL23 WL203.<[01] REMOVED CRACK DAMAGED ATTACH ANGLE AT MID CABIN BS 663+29 RBL 23 WL 203 IAW SRM 51-40-02-0G-0 NO SR
- [SDR SWAA2023042823700](https://openairdocs.org/sdr/SWAA2023042823700), Apr 4, 2023: FLOOR SUPPORT. CRACKED. PASSENGER CABIN FLOOR SUPPORT IS CRACKED BS540 LBL1 WL208.<[01] NO ALLOWABLE DAMAGE FOUND ON SRM PART TO BE REMOVED AND REPLACED I.A.W SRM 51-10-02-0G-0 PAR 9.C
- [SDR SWAA2023042823701](https://openairdocs.org/sdr/SWAA2023042823701), Apr 4, 2023: FLOOR SUPPORT. CRACKED. PASSENGER CABIN FLOOR SUPPORT IS CRACKED BS540 RBL1 WL208.<[01] NO ALLOWABLE DAMAGE FOUND ON SRM PART TO BE REMOVED AND REPLACED I.A.W SRM 51-10-02-0G-0 PAR 9.C
- [SDR SWAA2023042823364](https://openairdocs.org/sdr/SWAA2023042823364), Apr 3, 2023: STRINGER. CRACKED. CRACKED STRINGER AT AREA AFT OF FCB BS535 S-23R WL164. MARKED<REMOVED DAMAGED SECTION OF S-23R BETWEEN BS 500D TO 540; RECEIVED STRINGER SECTION FROM OSS R.O # 
- [SDR SWAA2023042823363](https://openairdocs.org/sdr/SWAA2023042823363), Apr 3, 2023: STRINGER. CRACKED. CRACKED STRINGER AT AREA AFT OF FCB BS535 S-26L WL153. MARKED<REMOVED DAMAGED SECTION OF S-26L BETWEEN BS 500D TO 540 RECEIVED STRINGER SECTION FROM OSS R.O # 9
- [SDR SWAA2023042823360](https://openairdocs.org/sdr/SWAA2023042823360), Apr 3, 2023: STRINGER. CRACKED. CRACKED STRINGER AT AREA AFT OF FCB BS535 S-23L WL164. MARKED<REMOVED DAMAGED SECTION OF S-23L BETWEEN BS 500D TO 540 RECEIVED STRINGER SECTION FROM OSS R.O # 9
- [SDR SWAA2023042823365](https://openairdocs.org/sdr/SWAA2023042823365), Apr 3, 2023: STRINGER. CRACKED. CRACKED STRINGER AT AREA AFT OF FCB BS535 S-26R WL153. MARKED<REMOVED DAMAGED SECTION OF S-26R BETWEEN BS 500D TO 540; PERFORMED DVI ON REPAIR AREA AND NO ADDIT
- [SDR SWAA2023042823366](https://openairdocs.org/sdr/SWAA2023042823366), Apr 3, 2023: STRINGER. CRACKED. CRACKED STRINGER AT AREA AFT OF FCB BS535 S-27R WL150. MARKED<REMOVED DAMAGED SECTION OF S-27R BETWEEN BS 500D TO 540; PERFORMED DVI ON REPAIR AREA AND NO ADDIT
- [SDR SWAA2023042823223](https://openairdocs.org/sdr/SWAA2023042823223), Apr 3, 2023: SPAR. CORRODED. ***CORROSION*** ON LEFT WING REAR SPAR AROUND BOOST PUMP UPPER BONDING JUMPER IRSS145.<REMOVED CORROSION ON LEFT WING REAR SPAR WEB AROUND BOOST PUMP UPPER BOND
- [SDR SWAA2023042823224](https://openairdocs.org/sdr/SWAA2023042823224), Apr 3, 2023: SPAR. CORRODED. ***CORROSION*** ON LEFT WING REAR SPAR AROUND BOOST PUMP LOWER BONDING JUMPER IRSS145.<REMOVED CORROSION ON LEFT WING REAR SPAR WEB AROUND BOOST PUMP LOWER BOND
- [SDR SWAA2023042723362](https://openairdocs.org/sdr/SWAA2023042723362), Apr 3, 2023: STRINGER. CRACKED. CRACKED STRINGER AT AREA AFT OF FCB BS535 S-25L WL155. MARKED<[01] NO ALLOWABLE DAMAGED FOUND ON SRM FOR CRACK ON FCB BS535 S-25L WL164; VERIFIED APPLICABILITY 
- [SDR SWAA2023010386699](https://openairdocs.org/sdr/SWAA2023010386699), Dec 31, 2022: POWER SUPPLY. INOPERATIVE. LH EMERGENCY EXIT LIGHTS ARE ALL OUT. REPLACED LH EMERGENCY EXIT POWER SUPPLY PER AMM 33-51-06 OPS CHECK GOOD FOR ALL APPLICABLE LIGHTS
- [SDR SWAA2022102863757](https://openairdocs.org/sdr/SWAA2022102863757), Oct 25, 2022: SEAL. CRACKED. R/H HORIZONTAL STAB FORWARD UPPER SLIDING SEAL IS CRACKED / [01] R&R R/H HORIZONTAL STAB FORWARD UPPER SLIDING SEAL. IAW AMM 53-31-31
- [SDR SWAA2022102763766](https://openairdocs.org/sdr/SWAA2022102763766), Oct 25, 2022: ANGLE. CRACKED. AFT GALLEY DOOR LINER LOWER SUPPORT ASSY ANGLE CRACKED AFT SIDE / [01] R&R AFT GALLEY DOOR LINER LOWER SUPPORT ASSY ANGLE PER AMM 52-41-31
- [SDR SWAA2022031481351](https://openairdocs.org/sdr/SWAA2022031481351), Mar 9, 2022: PLATE. CRACKED. R/H WING LOWER TRAILING EDGE SHELF PANEL; JUST OUTBOARD OF THE #6 FLAP TRACK FAIRING HAS A WAFFLE PLATE CRACKED OUT WITH A MISSING NUT PLATE AT ORSS 263; JUST A
- [SDR SWAA2022022275459](https://openairdocs.org/sdr/SWAA2022022275459), Feb 19, 2022: LIGHT. INOPERATIVE. LEFT OVER WING EXIT LIGHT INOP. / [01] RE-LAMPED L/H OVER WING EMERGENCY EXIT LIGHT PER AMM 33-51-04. OPS CHECKED GOOD.
- [SDR SWAA2022022173744](https://openairdocs.org/sdr/SWAA2022022173744), Feb 17, 2022: SIGN. LOOSE. EMERGENCY EXIT SIGN IN AFT GALLET NEAR SERVICE DOOR LOOSE / [01] R/R'D AFT GALLEY SERVICE DOOR EMERGENCY EXIT ASSY AS PER AMM 33-51-01
- [SDR SWAA2022012562987](https://openairdocs.org/sdr/SWAA2022012562987), Jan 21, 2022: LIGHT. BROKEN. R/H OVERWING EXIT SIGN COVER BROKEN ; / [01] R AND R'D EXIT SIGN ASSY PER AMM-33-51-01<BR>OPS NORMAL.
- [SDR SWAA2022010557434](https://openairdocs.org/sdr/SWAA2022010557434), Jan 1, 2022: DOME. DELAMINATED. SUPPLEMENTAL INFORMATION: 4 HOLE AND DELAMINATION ON RADAR DOME ; NOTED 4 HOLES AND DELAMINATION ON RADAR DOME / [01] TEMP REPAIRED PER SRM53-10-72; [02] CONFIR
- [SDR SWAA2021121351544](https://openairdocs.org/sdr/SWAA2021121351544), Dec 9, 2021: SIGN. LOOSE. SUPPLEMENTAL INFORMATION: R/H OVERWING EXIT SIGN FELL OFF ; / [01] RESECURED R/H OVERWING EXIT SIGN IAW AMM 33-51-01. A/C OK FOR SERVICE
- [SDR SWAA2021110133339](https://openairdocs.org/sdr/SWAA2021110133339), Oct 26, 2021: PANEL. ELONGATED. PANEL 193D HAS SEVERAL ELONGATED FASTENER HOLES. ; / [01] LOCATED HOLE IN NEW PANEL PER EO 5351-I-14642-NG; [02] REMOVED AND REPLACED PANEL PER SRM 51-10-02 AND
- [SDR SWAA2021091316281](https://openairdocs.org/sdr/SWAA2021091316281), Sep 9, 2021: HANDLE. INOPERATIVE. COVER FOR AFT SERVICE DOOR SLIDE MANUAL INFLATION HANDLE NOT INSTALLED ; / [01] UNTUCKED MANUAL SLIDE INFLATION HANDLE COVER IAW SIP ON AFT SERVICE DOOR (R2)
- [SDR SWAA2021082409132](https://openairdocs.org/sdr/SWAA2021082409132), Aug 22, 2021: SLIDE. OUT OF POSITION. AFT ENTRY DOOR SLIDE FELL OUT OF THE COVER. ; / [01] REINSTALLED/REPOSITIONED AFT ENTRY DOOR SIDE IN THE COVER PER AMM 25-66-01. A/C OK FOR SERIVCE.

All 359: https://openairdocs.org/deregistered/N412WN-2025-09-30/reports.md

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