# N235WN: 2006 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: 34630
- Year built: 2006
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 10, 2006
- Certificate issued: May 12, 2006
- Last registry action: January 22, 2023
- Mode S code: A21D14
- 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/N235WN
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=235WN
- Page: https://openairdocs.org/deregistered/N235WN-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 (280, newest 50)

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

- [SDR SWAA2025120441472](https://openairdocs.org/sdr/SWAA2025120441472), Dec 2, 2025: BATTERY. NO TEST. AFT RIGHT EMERGENCY LIGHTING BATTERY PACK FAILED A CAPACITY CHECK. REMOVED & REPLACED THE BATTERY IAW MM 33-51-06.
- [SDR SWAA2025070387876](https://openairdocs.org/sdr/SWAA2025070387876), Jul 3, 2025: LAMP. INOPERATIVE. FWD SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED IAW MM 33-51-04.
- [SDR SWAA2025062785436](https://openairdocs.org/sdr/SWAA2025062785436), Jun 25, 2025: LAMP. INOPERATIVE. LEFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] RELAMPED IAW AMM 33-51-03
- [SDR SWAA2025041122644](https://openairdocs.org/sdr/SWAA2025041122644), Apr 8, 2025: HANDLE. BROKEN. F/O PILOT ASSIST HANDLE BROKEN<[01] R&R F/O SEAT ASSIST HANDLE PER AMM 20-50-11
- [SDR SWAA2025020492495](https://openairdocs.org/sdr/SWAA2025020492495), Feb 3, 2025: COVER. OUT OF ADJUST. PLASTIC EXIT ROW COVER FELL OFF AFTER LANDING<[01] RE-INSTALL PLASTIC EXIT ROW I.A.W AMM 11-32-01.
- [SDR SWAA2024080822699](https://openairdocs.org/sdr/SWAA2024080822699), Aug 5, 2024: WIRE HARNESS. DISCONNECTED. RED BOX ON SHUTDOWN IN #2 ENG. EGT REDLINE LIMIT EXCEEDED ON TAKEOFF. DISCONNECTED A/T AND REDUCED THRUST; NO FURTHER INDICATIONS.<[01] T/S PER FIM 71-06 TASK 8
- [SDR SWAA2024080823958](https://openairdocs.org/sdr/SWAA2024080823958), Aug 5, 2024: PROBE. FAILED. RED BOX ON SHUTDOWN IN #2 ENG. EGT REDLINE LIMIT EXCEEDED ON TAKEOFF. DISCONNECTED A/T AND REDUCED THRUST; NO FURTHER INDICATIONS.<[01] T/S PER FIM 71-06 TASK 8
- [SDR SWAA2024062505471](https://openairdocs.org/sdr/SWAA2024062505471), Jun 24, 2024: EGT INDICATION. ACTIVATED. ON T/O #2 ENGINE EGT HAD AN EXCEEDENCE; EGT OF 960 FOR 5 SEC'S EGT GAUGE TURNED RED. PULLED POWER BACK & EGT RETURNED TO LIMITS. PER THE ENGINE EXCEEDENCE PAGE 
- [SDR SWAA2024061801469](https://openairdocs.org/sdr/SWAA2024061801469), Jun 14, 2024: HANDLE. LOOSE. FWD ENTRY DOOR HANDLE RATTLES WHEN DOOR IS CLOSED<[01] RETIGHTEN FWD ENTRY DOOR HANDLE AS REQUIRED REF. AMM 52-11-31.
- [SDR SWAA2024061801470](https://openairdocs.org/sdr/SWAA2024061801470), Jun 14, 2024: GIRT BAR. OUT OF ADJUST. FWD GALLEY SERVICE DOOR; SLIDE GIRT IS NOT PROPERLY PACKED<[01] REPACKED FWD SERVICE DOOR SLIDE GIRT PROPERLY REF. AMM 25-66-00.;[02] REPACKED FWD SERVICE DOOR 
- [SDR SWAA2024011639815](https://openairdocs.org/sdr/SWAA2024011639815), Jan 10, 2024: LIGHT. INOPERATIVE. RIGHT HAND EMERGENCY EXIT GROUND ILLUMINATION LIGHT IS INOP<[01] RELAMPED R/H EMERGENCY EXIT GROUND ILLUMINATION LIGHT AND PERFORMED GOOD INSTALLATION TEST PER 
- [SDR SWAA2024011639220](https://openairdocs.org/sdr/SWAA2024011639220), Jan 9, 2024: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS ASSOCIATED WITH EMERGENCY BATTERY PACK M1669 INOP<[01] REPLACED EMERGENCY EXIT BATTERY PACK M1669 AND PERFORMED GOOD TEST PER AMM 33-51-06
- [SDR SWAA2024011639217](https://openairdocs.org/sdr/SWAA2024011639217), Jan 9, 2024: BATTERY PACK. INOPERATIVE. MULTIPLE EMERGENCY EXIT LIGHTS ASSOCIATED WITH EMERGENCY BATTERY PACK M1674 INOP<[01] REPLACED BATTERY PACK M1674 AND PERFORMED GOOD TEST PER AMM 33-51-06-960-8
- [SDR SWAA2024011639219](https://openairdocs.org/sdr/SWAA2024011639219), Jan 9, 2024: LIGHT. INOPERATIVE. AFT SERVICE DOOR SLIDE LIGHT IS INOP<[01] RELAMPED AFT SERVICE DOOR SLIDE LIGHT AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-04-960-801.;[02] VERIFIED COR
- [SDR SWAA2024011737606](https://openairdocs.org/sdr/SWAA2024011737606), Jan 3, 2024: SHIELD. CORRODED. PERFORM RII BUYBACK OF FWD CARGO AFT SHIELD HAS CORROSION AT BS 500+5 - 500+16; RBL 24; WL 208 [TTG8Q00QAH7R]<[01] UPDATED MEASUREMENTS;[02] PERFORMED RII BUYBA
- [SDR SWAA2024011636727](https://openairdocs.org/sdr/SWAA2024011636727), Dec 31, 2023: INTERCOSTAL. CORRODED. CORROSION ON AFT CARGO BAY WEB AT BS 827-847 STRINGER 27 R/H<[01] REMOVED AND REPLACED ACB INTERCOSTAL FROM BS 827 TO BS 847 RBL 6 WL 156 IAW SRM 51-40-02-0G-0 
- [SDR SWAA2024011633879](https://openairdocs.org/sdr/SWAA2024011633879), Dec 19, 2023: SCUFF PLATE. CRACKED. AFT CARGO BAY FORWARD CORNER SCUFF PLATE IS CRACKED<[01] AFT CARGO BAY FORWARD CORNER SCUFF PLATE REPAIRED PER SRM 53-60-15-2R-1.;[02] CORRECTED MEASUREMENT LIN
- [SDR SWAA2024011633670](https://openairdocs.org/sdr/SWAA2024011633670), Dec 19, 2023: FLOOR PANEL. PULLED. FWD FLOOR PANEL 221CF UPPER SURFACE HAS PULLED STRAND OF FIBERGLASS.<[01] REPAIRED FWD FLOOR PANEL 221CF UPPER SURFACE PULLED STRAND OF FIBERGLASS IAW SRM 53-00
- [SDR SWAA2024011633671](https://openairdocs.org/sdr/SWAA2024011633671), Dec 19, 2023: FLOOR PANEL. DELAMINATED. FWD FLOOR PANEL 221CF LOWER SURFACE HAS AREAS OF DELAMINATION.<[01] REPAIRED FWD FLOOR PANEL 221CF LOWER SURFACE DELAMINATION IAW SRM 53-00-50-2R-1.;[02] VERIFI
- [SDR SWAA2024011633672](https://openairdocs.org/sdr/SWAA2024011633672), Dec 19, 2023: FLOOR PANEL. DELAMINATED. FWD FLOOR PANEL 222AF UPPER SURFACE HAS AREAS OF DELAMINATION.<[01] REPAIRED FWD FLOOR PANEL 222AF UPPER SURFACE DELAMINATION IAW SRM 53-00-50-2R-1.;[02] VERIFI
- [SDR SWAA2024011633673](https://openairdocs.org/sdr/SWAA2024011633673), Dec 19, 2023: FLOOR PANEL. DELAMINATED. FWD FLOOR PANEL 222AF LOWER SURFACE HAS AREAS OF DELAMINATION.<[01] REPAIRED FWD FLOOR PANEL 222AF LOWER SURFACE DELAMINATION IAW SRM 53-00-50-2R-1.;[02] VERIFI
- [SDR SWAA2024011633476](https://openairdocs.org/sdr/SWAA2024011633476), Dec 19, 2023: FRAME. CRACKED. STATION 312 FRAME IS CRACKED IN RADIUS ABOVE L1 DOOR CUT-OUT.<[01] THE UPPER CORD OF THE BS312 FRAME WAS REPAIRED PER REF EA M-22-153-01244;[02] VERIFIED CORREC
- [SDR SWAA2024011633439](https://openairdocs.org/sdr/SWAA2024011633439), Dec 18, 2023: SUPPORT ANGLE. CRACKED. LEFT WING; T/E COVE SEAL SUPPORT ANGLE CRACKED ABOVE #1 PYLON AFT TIP<[01] REMOVED AND REPLACED LEFT WING; T/E COVE SEAL SUPPORT ANGLE ABOVE #1 PYLON AFT TIP IA
- [SDR SWAA2024011633454](https://openairdocs.org/sdr/SWAA2024011633454), Dec 18, 2023: SCUFF PLATE. CRACKED. AFT CARGO DOOR AFT CORNER SCUFF PLATE IS CRACKED<[01] AFT CARGO DOOR AFT CORNER SCUFF PLATE REPAIRED PER SRM 53-60-15-2R-1.;[02] CORRECTED MEASUREMENT LINE ITEM
- [SDR SWAA2024011632520](https://openairdocs.org/sdr/SWAA2024011632520), Dec 16, 2023: FLOOR PANEL. PULLED. FLOOR PANEL 231FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231FF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR P
- [SDR SWAA2024011632521](https://openairdocs.org/sdr/SWAA2024011632521), Dec 16, 2023: FLOOR PANEL. PULLED. FLOOR PANEL 231MF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231MF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR P
- [SDR SWAA2024011632522](https://openairdocs.org/sdr/SWAA2024011632522), Dec 16, 2023: FLOOR PANEL. PULLED. FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241UF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR P
- [SDR SWAA2024011632518](https://openairdocs.org/sdr/SWAA2024011632518), Dec 15, 2023: BRACKET. CRACKED. PULLEY SUPPORT BEAM CRACKED ON L-BRACKET AT BS 697; LBL 0.5; WL 207. (MARKED)<[01] STEP 2 COMPLETE OK TO APPLY CONVERSION COAT AND PRIME;[02] STEP 3 COMPLETE;[0
- [SDR SWAA2024011632253](https://openairdocs.org/sdr/SWAA2024011632253), Dec 15, 2023: FLANGE. CORRODED. CORROSION ON FWD R/H MOP SILL VERTICAL FLANGE FROM STA 294 TO STA 330; RBL 54 TO RBL 59; WL 208.9.<[01] REMOVED AND REPLACED ON FWD R/H MOPSILL BS 260 TO BS 360
- [SDR SWAA2024011632251](https://openairdocs.org/sdr/SWAA2024011632251), Dec 15, 2023: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL AT STA 277+10; BL 0; WL 208.1.<[01] REMOVED AND REPLACED NEW INTERCOSTAL ITEM 141A5410-3 IAW SRM 51-40-02 AND DWG 141A5400;[02] VERIFIED COR
- [SDR SWAA2024011632393](https://openairdocs.org/sdr/SWAA2024011632393), Dec 15, 2023: SCUFF PLATE. CRACKED. FCB AFT CORNER SCUFF PLATE IS CRACKED<[01] APPLIED A CHEMICAL CONVERSION COATING TO THE BARE ALUMINUM SURFACES PER SOPM 20-43-03; TYPE 2; CLASS A OR C AND SRM 5
- [SDR SWAA2024011631806](https://openairdocs.org/sdr/SWAA2024011631806), Dec 14, 2023: FLOOR PANEL. PULLED. FWD FLOOR PANEL 221AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221AF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE
- [SDR SWAA2024011631807](https://openairdocs.org/sdr/SWAA2024011631807), Dec 14, 2023: FLOOR PANEL. PULLED. FWD FLOOR PANEL 221BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE
- [SDR SWAA2024011631815](https://openairdocs.org/sdr/SWAA2024011631815), Dec 14, 2023: FLOOR PANEL. PULLED. FWD FLOOR PANEL 221GF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221GF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE
- [SDR SWAA2024011631812](https://openairdocs.org/sdr/SWAA2024011631812), Dec 14, 2023: FLOOR PANEL. PULLED. FWD FLOOR PANEL 222CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AREAS OF PULLED STRANDS ON UPPER SKIN OF FWD FLOOR PANEL 222CF WERE REPAIRED IAW SRM 53-00-50
- [SDR SWAA2024011631816](https://openairdocs.org/sdr/SWAA2024011631816), Dec 14, 2023: FLOOR PANEL. PULLED. PASSENGER CABIN FLOOR PANEL 241DF HAS PULLED STRANDS.<[01] DUE TO EXTENT OF THE DAMAGE ON PASSENGER CABIN FLOOR PANEL 241DF FABRICATED NEW PANEL FROM BMS4-17 TY
- [SDR SWAA2024011631820](https://openairdocs.org/sdr/SWAA2024011631820), Dec 14, 2023: FLOOR PANEL. PULLED. PASSENGER CABIN FLOOR PANEL 241FF HAS PULLED STRANDS.<[01] VERIFIED STEP 1;2 AND THE MEASUREMENT TABLE.;[02] PASSENGER CABIN FLOOR PANEL 241FF WITH PULLED STRAN
- [SDR SWAA2024011631818](https://openairdocs.org/sdr/SWAA2024011631818), Dec 14, 2023: FLOOR PANEL. PULLED. PASSENGER CABIN FLOOR PANEL 242CF HAS PULLED INSERT.<[01] VERIFIED STEP 1;2 AND THE MEASUREMENT TABLE.;[02] PASSENGER CABIN FLOOR PANEL 242CF WITH A PULLED INSE
- [SDR SWAA2024011631821](https://openairdocs.org/sdr/SWAA2024011631821), Dec 14, 2023: FLOOR PANEL. PULLED. AFT FLOOR PANEL 241AAF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241AAF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS BEYOND ECONOMICAL REPAIR.
- [SDR SWAA2024011631823](https://openairdocs.org/sdr/SWAA2024011631823), Dec 14, 2023: FLOOR PANEL. PULLED. AFT FLOOR PANEL 241ADF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ADF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50
- [SDR SWAA2024011631824](https://openairdocs.org/sdr/SWAA2024011631824), Dec 14, 2023: FLOOR PANEL. PULLED. AFT FLOOR PANEL 242TF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242TF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2
- [SDR SWAA2024011631827](https://openairdocs.org/sdr/SWAA2024011631827), Dec 14, 2023: FLOOR PANEL. PULLED. AFT FLOOR PANEL 242UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242UF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2
- [SDR SWAA2024011631828](https://openairdocs.org/sdr/SWAA2024011631828), Dec 14, 2023: FLOOR PANEL. PULLED. AFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242VF UPPER SKIN; AREAS OF PULLED STRANDS; WAS REPAIRED IAW SRM 53-00-50-2R-1
- [SDR SWAA2024011632239](https://openairdocs.org/sdr/SWAA2024011632239), Dec 14, 2023: FRAME. CORRODED. AFT CABIN WET AREA FRAME HAS CORROSION AT FASTENER HOLE; BS 986; LBL 44; WL 208<[01] REMOVED AND REPLACED REPAIR PARTS PER SEM 51-40-02 AS SHOW IN SWA EA#1-753-
- [SDR SWAA2024011632244](https://openairdocs.org/sdr/SWAA2024011632244), Dec 14, 2023: WEB. CORRODED. FWD CARGO DOOR CENTER THRESHOLD HAS CORROSION AT BS 440+10 - 480+4; RBL 28; WL 208<[01] REMOVED AND REPLACED THRESHOLD WEB AT FCB BS 440- 492.4; RBL 28; WL 156.
- [SDR SWAA2024011632245](https://openairdocs.org/sdr/SWAA2024011632245), Dec 14, 2023: SHIELD. CORRODED. FWD CARGO AFT SHIELD HAS CORROSION AT BS 500+5 - 500+16; RBL 24; WL 208<[01] REMOVED AND REPLACED AFT SHIELD;IAW DWG#143A0080 AND SRM 51-40-02.;[02] VERIFIED CO
- [SDR SWAA2024011632246](https://openairdocs.org/sdr/SWAA2024011632246), Dec 14, 2023: SIDEWALL SUPPORT. CORRODED. AFT CARGO FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 767-727E; RBL 22; WL 156<[01] REMOVED AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02 AN DW
- [SDR SWAA2024011632243](https://openairdocs.org/sdr/SWAA2024011632243), Dec 14, 2023: SIDEWALL SUPPORT. CORRODED. AFT CARGO FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 727D - 744; LBL 22; WL 156<[01] CORRECTION TOM MEASUREMENT #1;[02] REMOVED AND REPLACED LH SIDEWALL SUPP
- [SDR SWAA2024011632247](https://openairdocs.org/sdr/SWAA2024011632247), Dec 14, 2023: SIDEWALL SUPPORT. CORRODED. AFT CARGO FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 747+9 - 787; LBL 22; WL 157<[01] THIS TASK CARD WILL BE COMPLETED WITH CARD #TTG8Q00QAFFY.;[02] VERIFIED
- [SDR SWAA2024011632003](https://openairdocs.org/sdr/SWAA2024011632003), Dec 14, 2023: FRAME. CORRODED. FWD CABIN WET AREA FRAME HAS CORROSION AT FASTENER HOLES; BS 294.5; RBL 7; WL 208 CLARIFICATION THIS IS THE BS 294 FLOOR BEAM=FWD CABIN WET AREA FRAME HAS CORRO

All 280: https://openairdocs.org/deregistered/N235WN-2026-06-05/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.