# N467WN: 2004 Boeing 737-7H4

- Status: Valid registration
- Airframe: [Boeing 737-7H4](https://openairdocs.org/model/boeing-737-7h4) (registry code 1384404, 143 seats)
- 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) (The Boeing Company) (OpenAirDocs)
- Serial number: 33830
- Year built: 2004
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 14, 2004
- Certificate issued: July 21, 2004
- Expires: October 31, 2027
- Mode S code: A5B59D
- Registered owner: [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 is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=467WN
- Page: https://openairdocs.org/aircraft/N467WN

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every CFM International CFM56 model are included.

## ADs that may apply (OpenAirDocs): 55 in force

### Matched by airframe (Boeing 737-7H4)

None in force.

### Matched by engine (CFM International CFM56 series)

- [AD 2023-05-05](https://openairdocs.org/ad/2023-05-05): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 98 more. Effective May 10, 2023
- [AD 2022-02-03](https://openairdocs.org/ad/2022-02-03): Turbine Engine Accessory Drive · CFM International CFM56-3, CFM56-3B, CFM56-3C and 34 more. Effective Mar 22, 2022
- [AD 2021-16-08](https://openairdocs.org/ad/2021-16-08): Turbine Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 55 more. Effective Sep 28, 2021
- [AD 2018-26-01](https://openairdocs.org/ad/2018-26-01): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jan 10, 2019
- [AD 2018-09-51](https://openairdocs.org/ad/2018-09-51): Engine · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 7, 2018
- [AD 2017-14-08](https://openairdocs.org/ad/2017-14-08): Turbine Engine Compressor Section · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Aug 18, 2017
- [AD 2017-05-09](https://openairdocs.org/ad/2017-05-09): Accessory Gearboxes · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 33 more. Effective Apr 13, 2017
- [AD 2016-14-10](https://openairdocs.org/ad/2016-14-10): High-pressure turbine (HPT) disks · CFM International CFM56-3, CFM56-3B and CFM56-3C with STC SE00034EN. Effective Aug 9, 2016
- [AD 2016-02-04](https://openairdocs.org/ad/2016-02-04): Turbine rear frames (TRFs) · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 33 more. Effective Mar 1, 2016
- [AD 2015-18-04](https://openairdocs.org/ad/2015-18-04): 73-tooth gearshaft located in the engine accessory gearbox (AGB) · CFM International CFM56-3, CFM56-7B20, CFM56-7B20/2 and 47 more. Effective Oct 20, 2015
- [AD 2015-04-02](https://openairdocs.org/ad/2015-04-02): Dual engine thrust instability event · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Mar 31, 2015
- [AD 2013-14-06](https://openairdocs.org/ad/2013-14-06): Hydro-mechanical unit (HMU) fuel control · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 34 more. Effective Sep 3, 2013
- [AD 2012-02-03](https://openairdocs.org/ad/2012-02-03): Engine · CFM International CFM56-5B1/3, CFM56-5B2/3, CFM56-5B3/3 and 8 more. Effective Mar 15, 2012
- [AD 2010-13-09](https://openairdocs.org/ad/2010-13-09): Stage 3 low-pressure turbine (LPT) · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 88 more. Effective Jul 26, 2010
- [AD 2010-12-03](https://openairdocs.org/ad/2010-12-03): Fan blades · CFM International CFM56-3 and CFM56-3B. Effective Jul 13, 2010
- [AD 2010-09-14](https://openairdocs.org/ad/2010-09-14): Exhaust gas temperature (EGT) · CFM International CFM56-5B1/2P, CFM56-5B1/P, CFM56-5B2/2P and 16 more. Effective Jun 8, 2010
- [AD 2010-01-05](https://openairdocs.org/ad/2010-01-05): LP turbine rear frames · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 25 more. Effective Feb 18, 2010
- [AD 2009-18-01](https://openairdocs.org/ad/2009-18-01): LP turbine rear frames · CFM International CFM56-5B1/3, CFM56-5B1/P, CFM56-5B2/3 and 19 more. Effective Oct 1, 2009
- [AD 2009-11-02](https://openairdocs.org/ad/2009-11-02): HPC 4-9 spools · CFM International CFM56-2, CFM56-2A, CFM56-2B and 109 more. Effective Jun 23, 2009
- [AD 2008-03-09](https://openairdocs.org/ad/2008-03-09): Low pressure turbine rear frames (TRFs) · CFM International CFM56-7B18, CFM56-7B20, CFM56-7B22 and 10 more. Effective Mar 10, 2008
- [AD 2007-24-04](https://openairdocs.org/ad/2007-24-04): Low pressure turbine (LPT) · CFM International CFM56-5C4/1. Effective Dec 6, 2007
- [AD 2007-03-15](https://openairdocs.org/ad/2007-03-15): Exhaust gas temperature (EGT) harness · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 34 more. Effective Mar 19, 2007
- [AD 2006-26-01](https://openairdocs.org/ad/2006-26-01): Fuel filters · CFM International CFM56-2, CFM56-2A, CFM56-2B and 93 more. Effective Jan 3, 2007
- [AD 2005-10-05](https://openairdocs.org/ad/2005-10-05): Air turbine starters · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 50 more. Effective Jun 14, 2005
- [AD 97-09-02 R3](https://openairdocs.org/ad/97-09-02-R3): High pressure turbine rotor (HPTR) front shafts · CFM International CFM56-5C2, CFM56-5C3/G and CFM56-5C4. Effective Oct 14, 2004
- [AD 2004-10-13](https://openairdocs.org/ad/2004-10-13): Service main fuel pumps · CFM International CFM56-3, CFM56-5, CFM56-5-A1/F and 4 more. Effective Jun 24, 2004
- [AD 2002-22-12](https://openairdocs.org/ad/2002-22-12): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more. Effective Dec 13, 2002
- [AD 2002-16-18](https://openairdocs.org/ad/2002-16-18): Low pressure turbine (LPT) nozzle segments · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 33 more. Effective Sep 18, 2002
- [AD 2002-13-03](https://openairdocs.org/ad/2002-13-03): Turbofan Engines · CFM International CFM56-2, CFM56-2A, CFM56-2B and 55 more. Effective Aug 1, 2002
- [AD 2002-02-13](https://openairdocs.org/ad/2002-02-13): Magnetic Drain Plug · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 33 more. Effective Mar 21, 2002
- [AD 2001-11-05](https://openairdocs.org/ad/2001-11-05): No. 4 Bearings · CFM International CFM56-2, CFM56-2B, CFM56-3 and 45 more. Effective Jun 11, 2001
- [AD 2001-09-17](https://openairdocs.org/ad/2001-09-17): Fuel Manifold and CJ9L Harness · CFM International CFM56-5C2, CFM56-5C2/4, CFM56-5C2/F and 13 more. Effective May 14, 2001
- [AD 2001-04-06](https://openairdocs.org/ad/2001-04-06): Fan Disk · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Apr 4, 2001
- [AD 2001-02-12](https://openairdocs.org/ad/2001-02-12): On-Wing Torque Inspection · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 11 more. Effective Feb 14, 2001
- [AD 2000-15-01](https://openairdocs.org/ad/2000-15-01): Fuel Leakage · CFM International CFM56-2, CFM56-2A, CFM56-2B and 39 more. Effective Oct 2, 2000
- [AD 2000-05-22](https://openairdocs.org/ad/2000-05-22): CFM International CFM56-2, CFM56-2A, CFM56-2B and 3 more. Effective May 2, 2000
- [AD 99-06-16](https://openairdocs.org/ad/99-06-16): High Pressure Turbine Rotor (HPTR) Front Air Seal · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 3 more. Effective Apr 21, 1999
- [AD 98-21-23](https://openairdocs.org/ad/98-21-23): Electronic Engine Control · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 10 more. Effective Nov 2, 1998
- [AD 98-19-20](https://openairdocs.org/ad/98-19-20): Hydromechanical Unit · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 7 more. Effective Oct 7, 1998
- [AD 98-14-51](https://openairdocs.org/ad/98-14-51): Accessory Gearbox · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 10 more. Effective Oct 1, 1998
- [AD 98-19-10](https://openairdocs.org/ad/98-19-10): Accessory Gearbox · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Sep 28, 1998
- [AD 98-12-32](https://openairdocs.org/ad/98-12-32): High Pressure Turbine Rotor Disks · CFM International CFM56-2, CFM56-2A, CFM56-2B and 3 more. Effective Jul 20, 1998
- [AD 98-10-11](https://openairdocs.org/ad/98-10-11): Accessory Gearbox · CFM International CFM56-3, CFM56-3B, CFM56-3C and 31 more. Effective Jun 3, 1998
- [AD 98-07-02](https://openairdocs.org/ad/98-07-02): Air/oil Seal · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Mar 30, 1998
- [AD 98-02-04](https://openairdocs.org/ad/98-02-04): Low Pressure Turbine Case · CFM International CFM56-5B1/2P, CFM56-5B2/2P, CFM56-5B3/2P and 1 more. Effective Mar 23, 1998
- [AD 89-23-06 R1](https://openairdocs.org/ad/89-23-06-R1): Magnetic Chip Detector · CFM International CFM56-2, CFM56-2A, CFM56-3 and 8 more. Effective Jan 28, 1998
- [AD 97-08-01](https://openairdocs.org/ad/97-08-01): Fan Disks · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Jun 23, 1997
- [AD 97-06-01](https://openairdocs.org/ad/97-06-01): High Pressure Compressor Rotor (HPCR) Stage 1-2 Spool · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 28 more. Effective Jun 3, 1997
- [AD 97-05-13](https://openairdocs.org/ad/97-05-13): Air Turbine Engine Starter · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 3 more. Effective Jun 3, 1997
- [AD 96-25-11](https://openairdocs.org/ad/96-25-11): Redesigned Fan Blades · CFM International CFM56-3B and CFM56-3C. Effective Jan 29, 1997

### Historical (superseded or no longer in force)

- [AD 2021-10-09](https://openairdocs.org/ad/2021-10-09) (historical): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 82 more. Effective Jun 24, 2021
- [AD 2019-12-05](https://openairdocs.org/ad/2019-12-05) (historical): Turbine Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 39 more. Effective Jul 5, 2019
- [AD 2018-18-01](https://openairdocs.org/ad/2018-18-01) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Oct 16, 2018
- [AD 2018-10-11](https://openairdocs.org/ad/2018-10-11) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 1, 2018
- [AD 2018-09-10](https://openairdocs.org/ad/2018-09-10) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective May 14, 2018
- [AD 2013-26-01](https://openairdocs.org/ad/2013-26-01) (historical): Oil dynamic seal assembly · CFM International CFM56-3, CFM56-3B, CFM56-3C and 52 more. Effective Feb 3, 2014
- [AD 2013-02-02](https://openairdocs.org/ad/2013-02-02) (historical): High-pressure turbine (HPT) disks · CFM International CFM56-3, CFM56-3B and CFM56-3C with STC SE00034EN. Effective Jan 28, 2013
- [AD 2009-01-01](https://openairdocs.org/ad/2009-01-01) (historical): Exhaust gas temperature (EGT) · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 22 more. Effective Dec 31, 2008
- [AD 97-09-02 R2](https://openairdocs.org/ad/97-09-02-R2) (historical): Low pressure turbine rotor (LPTR) · CFM International CFM56-5C2, CFM56-5C2/4, CFM56-5C2/F and 9 more. Effective Apr 29, 2003
- [AD 2003-02-04](https://openairdocs.org/ad/2003-02-04) (historical): Exhaust gas temperature (EGT) · CFM International CFM56-5 Series (all). Effective Feb 27, 2003
- [AD 97-09-02 R1](https://openairdocs.org/ad/97-09-02-R1) (historical): High Pressure Turbine rotor (HPTR) front shaft · CFM International CFM56-5C2/G, CFM56-5C2/G4, CFM56-5C3/G and 3 more. Effective Sep 24, 2002
- [AD 2001-17-14](https://openairdocs.org/ad/2001-17-14) (historical): LPT Conical Supports · CFM International CFM56-5C4/1. Effective Sep 7, 2001
- [AD 2001-08-51](https://openairdocs.org/ad/2001-08-51) (historical): Fuel leakage · CFM International CFM56-5 Series (all)
- [AD 2000-12-01](https://openairdocs.org/ad/2000-12-01) (historical): Critical Life-Limited Parts · CFM International CFM56-2, CFM56-2A, CFM56-2B and 54 more. Effective Dec 11, 2000
- [AD 99-08-16](https://openairdocs.org/ad/99-08-16) (historical): CFM International CFM56-2, CFM56-2A, CFM56-2B and 3 more. Effective May 13, 1999
- [AD 97-09-02](https://openairdocs.org/ad/97-09-02) (historical): High/Low Pressure Turbine Rotor · CFM International CFM56-5C2/G, CFM56-5C2/G4, CFM56-5C3/G and 3 more. Effective Jun 30, 1997

All 71: https://openairdocs.org/aircraft/N467WN/ads.md

## Information bulletins (advisory) (4 in force)

- [SAIB NE-08-17R3](https://openairdocs.org/saib/NE-08-17R3): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued May 28, 2014
- [SAIB NE-13-33R2](https://openairdocs.org/saib/NE-13-33R2): Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes. Issued Jan 28, 2014
- [SAIB NE-12-29](https://openairdocs.org/saib/NE-12-29): Engine Fuel Distribution  CFM56-5B LPTACC Fuel Manifold. Issued Apr 27, 2012
- [SAIB NE-06-02](https://openairdocs.org/saib/NE-06-02): . Issued Oct 18, 2005
- [SAIB NE-13-33R1](https://openairdocs.org/saib/NE-13-33R1) (historical): Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes. Issued Jun 24, 2013
- [SAIB NE-13-33](https://openairdocs.org/saib/NE-13-33) (historical): Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes. Issued May 13, 2013
- [SAIB NE-08-17R2](https://openairdocs.org/saib/NE-08-17R2) (historical): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued Mar 7, 2011
- [SAIB NE-08-17R1](https://openairdocs.org/saib/NE-08-17R1) (historical): Propulsion Technology LLC Unapproved Repair. Issued May 22, 2008
- [SAIB NE-08-17](https://openairdocs.org/saib/NE-08-17) (historical): Propulsion Technologies International Unapproved Repair. Issued May 14, 2008

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA16CA026](https://openairdocs.org/ntsb/DCA16CA026), Nov 29, 2015: Boeing 737 7H4 (N467WN), St Louis, MO, no damage. Probable cause: an inadvertent encounter with clear air turbulence.

## FAA accident and incident reports

None matched to N467WN.

## Service difficulty reports (359, newest 50)

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

- [SDR SWAA2026092865075](https://openairdocs.org/sdr/SWAA2026092865075), Sep 26, 2026: LENS. MISSING. RIGHT OVERWING EXIT LOWER LEFT EMERGENCY LIGHT LENS MISSING. INSTALLED EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-01. ACFT OK FOR SERVICE.
- [SDR SWAA2026081739045](https://openairdocs.org/sdr/SWAA2026081739045), Aug 11, 2026: SLIDE. UNSECURE. FWD ENTRY DOOR SLIDE NOT SECURE REINSTALLED L1 DOOR SLIDE REF MT 72561-06 NO DEFECTS NOTED.
- [SDR SWAA2026073102234](https://openairdocs.org/sdr/SWAA2026073102234), Jul 27, 2026: FLASHLIGHT. NO TEST. ONE OF FWD GALLEY EMERGENCY FLASHLIGHTS TEST LIGHT NOT FLASHING. R & R FWD GALLEY EMERGENCY FLASHLIGHT IAW AMM 25-64-00. OPS CHECKED GOOD.
- [SDR SWAA2026072854375](https://openairdocs.org/sdr/SWAA2026072854375), Jul 24, 2026: SLIDE. DISLODGED. L1 SLIDE FELL OUT OF BUSTLE. REPACKED FWD ENTRY EMERGENCY SLIDE REF MT 72561-06.
- [SDR SWAA2026061611895](https://openairdocs.org/sdr/SWAA2026061611895), Jun 12, 2026: ENGINE. POWER LOSS. NR 2 ENGINE ROLLED BACK ON ITS OWN WITH WHITE FLASHING BOX. NO EXCEEDANCE OF EGT. RAN NR 2 ENGINE IAW AMM 71-00-00. NO DEFECTS NOTED.
- [SDR SWAA2026060107415](https://openairdocs.org/sdr/SWAA2026060107415), May 28, 2026: BATTERY PACK. NO TEST. FWD ENTRY LT EMERGENCY BATTERY PACK M1675 FAILED CAPACITY CHECK. R&R CABIN EMERGENCY BATTERY PACK PER AMM 33-51-06.
- [SDR SWAA2026050694972](https://openairdocs.org/sdr/SWAA2026050694972), May 3, 2026: BATTERY PACK. INOPERATIVE. INOPERATIVE BATTERY PACK M1673 AT BS 952, WL 290, LBL 13. REMOVED AND REPLACED THE BATTERY PACK M1673 IAW AMM 33-51-06-960-805. TESTED OK.
- [SDR SWAA2026050691337](https://openairdocs.org/sdr/SWAA2026050691337), Apr 21, 2026: LENS. BROKEN. BROKEN EMERGENCY EXIT LIGHT LENS ON SIDEWALL PANEL 232YHW AT PASSENGER CABIN. REPLACED EMERGENCY EXIT LIGHT LENS ON SIDEWALL PANEL 232YHW AT PASSENGER CABIN IAW
- [SDR SWAA2026050790982](https://openairdocs.org/sdr/SWAA2026050790982), Apr 19, 2026: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE LOC. ORSS 270 APPROX AT LT WING 2026-255674<[01] REPLACED ANGLE AND FASTENERS ON TRAILING EDGE LOC. ORSS 270 APPROX AT LT WING; MEASUR
- [SDR SWAA2026050690984](https://openairdocs.org/sdr/SWAA2026050690984), Apr 19, 2026: LIGHT. DETERIORATED. DETERIORATED PHOTOLUMINESCENT STRIP A LONG PASSENGER CABIN. REPLACED PHOTOLUMINESCENT STRIP A LONG PASSENGER CABIN IAW AMM 33-51-15-400-802.
- [SDR SWAA2026050690771](https://openairdocs.org/sdr/SWAA2026050690771), Apr 18, 2026: ANGLE. CRACKED. CRACK ANGLE LOCATED BS 695 RBL1 AT CENTER WING BOX . REPLACED ANGLE AND FASTENERS LOCATED BS 695 RBL1 AT CENTER WING BOX IAW SRM 51-10-02 ITEM 9, SRM 51-40-02 A
- [SDR SWAA2026050690234](https://openairdocs.org/sdr/SWAA2026050690234), Apr 17, 2026: SCUFF PLATE. CRACKED. CRACK FWD CORNER SCUFF PLATE AT AFT CARGO DOOR CUT-OUT. REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO DOOR CUT OUT IAW SRM 53-60-15-2R-1, REPAIR 1, & BAC 5975.
- [SDR SWAA2026050690438](https://openairdocs.org/sdr/SWAA2026050690438), Apr 17, 2026: RIB. CRACKED. CRACKED INSPAR RIB 111.10 LOCATED AT 20 INCHES OF FRONT SPAR AT RT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON RIB 111.10 LOCATED AT 20 INCHES OF FRONT SPAR 
- [SDR SWAA2026050690439](https://openairdocs.org/sdr/SWAA2026050690439), Apr 17, 2026: RIB. CRACKED. CRACKED INSPAR RIB 111.10 LOCATED AT 28 INCHES OF FRONT SPAR AT RT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR INSPAR RIB 111.10 LOCATED AT 28 INCHES OF FRONT S
- [SDR SWAA2026050690440](https://openairdocs.org/sdr/SWAA2026050690440), Apr 17, 2026: RIB. CRACKED. CRACKED INSPAR RIB 111.10 LOCATED AT 37 INCHES OF FRONT SPAR AT RT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON RIB 111.10<BR>AT 37 INCHES OF FRONT SPAR AT RT
- [SDR SWAA2026050690441](https://openairdocs.org/sdr/SWAA2026050690441), Apr 17, 2026: RIB. CRACKED. CRACKED INSPAR RIB 129.50 LOCATED 18 INCHES OF FRONT SPAR AT LT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR LOC. INSPAR RIB 129.50 LOCATED 18 INCHES OF FRONT SP
- [SDR SWAA2026050690233](https://openairdocs.org/sdr/SWAA2026050690233), Apr 17, 2026: SCUFF PLATE. CRACKED. CRACK AFT CORNER SCUFF PLATE AT AFT CARGO DOOR CUT-OUT. REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO DOOR CUT OUT IAW B737-700 SRM 53-60-15-2R-1 REPAIR 1. AND B
- [SDR SWAA2026050790230](https://openairdocs.org/sdr/SWAA2026050790230), Apr 16, 2026: ACCESS DOOR. CORRODED. CORROSION ACCESS DOOR 311BL INERNAL DOUBLER AT TAIL CONE 2026-255586<[01] TOOL USED P/N: NORTEC 500D; S/N: N500X1693P030456; CAL DUE: 25-MAY-26.;[02] TOOL USED 
- [SDR SWAA2026050790045](https://openairdocs.org/sdr/SWAA2026050790045), Apr 16, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLE ACCESS PANEL 561BB AT LT WING. REPAIRED ACCESS PANEL 561BB AT LT WING IAW SRM 51-70-04-2R-10 REPAIR 10.
- [SDR SWAA2026050690231](https://openairdocs.org/sdr/SWAA2026050690231), Apr 16, 2026: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANEL 242BF AT PASSENGER CABIN. REPAIRED FLOOR PANEL 242BF AT PASSENGER CABIN IAW SRM 53-00-50-2R-7, REPAIR 7.
- [SDR SWAA2025121953741](https://openairdocs.org/sdr/SWAA2025121953741), Dec 18, 2025: GIRT BAR. LOOSE. FWD GALLEY FO SIDE HOLDING BRACKET FOR GIRT BAR LOOSE. REMOVED AND REPLACED THE RIVETS FOR THE FWD SERVICE DOOR AFT GIRT BAR RETAINER CLIP IAW SRM 51-40-02.
- [SDR SWAA2025092517849](https://openairdocs.org/sdr/SWAA2025092517849), Sep 24, 2025: NUT. BROKEN. AFT FO SIDE SERVICE DOOR GRIP HANDLE BROKEN<[01] R/R AFT SERVICE DOOR ASSIST HANDLE NUT REF. AMM 52-41-31.
- [SDR SWAA2025092617330](https://openairdocs.org/sdr/SWAA2025092617330), Sep 23, 2025: SEAL. CRACKED. RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED. R & R RT HORIZONTAL STAB FWD UPPER SLIDING SEAL. IAW AMM 53-31-31.
- [SDR SWAA2025071590368](https://openairdocs.org/sdr/SWAA2025071590368), Jul 11, 2025: PITOT TUBE. CLOGGED. ON TAKEOFF ROLL ABOVE 80KTS CAPT AND F/O AIRSPEED INDICATIONS DISAGREED. F/O AIRSPEED AND ALTITUDE WERE RELIABLE. EEC'S SWITCHED TO ALTERNATE.<[01] FOUND INSECT
- [SDR SWAA2025050967786](https://openairdocs.org/sdr/SWAA2025050967786), May 6, 2025: SLIDE. OUT OF ADJUST. R2 DOOR SLIDE GIRT DRAGS<[01] REPACKED R2 DOOR SLIDE GIRT PER AMM 25-66-01.
- [SDR SWAA2025030300676](https://openairdocs.org/sdr/SWAA2025030300676), Feb 28, 2025: LIGHT. INOPERATIVE. CAPTAIN SIDE LWR EMERGENCY LIGHT (BEHIND TRAILING EDGE FLAPS) INOP <[01]. 01 - REMOVED AND REPLACED PER [AMM 33-51-04-960-801-NG (SLIDE/OVERWING LIGHT - LAMP RE
- [SDR SWAA2025021295239](https://openairdocs.org/sdr/SWAA2025021295239), Feb 11, 2025: HYDRAULIC LINE. LEAKING. HYDRAULIC SYSTEM A LOSS ALL FLUID<[01] REMOVED AND REPLACED A SYSTEM SPOILER ACTUATOR TUBE BY #7 GROUND SPOILER 1EA LEAK CHECK GOOD PER AMM 20-10-51.;[02] SEE C
- [SDR SWAA2025012789831](https://openairdocs.org/sdr/SWAA2025012789831), Jan 26, 2025: HANDLE. UNSECURE. WALK ITEM: R2 DOOR ASSIST HANDLE NEEDS SECURED<[01] SECURED R2 DOOR ASSIST HANDLE IAW B737NG AMM 52-41-31-401-NG (GALLEY SERVICE DOOR LINING - REMOVAL/INSTALLAT
- [SDR SWAA2025012788965](https://openairdocs.org/sdr/SWAA2025012788965), Jan 23, 2025: HANDLE. CRACKED. R1 DOOR ASSIST HANDLE IS CRACKED<[01] RECEIVED DOOR HANDLE PO# 1112200.1 AND RECEIVED NUTS PO# 1112200.2 REMOVED AND REPLACED DOOR HANDLE PER B737-700 AMM 52--1
- [SDR SWAA2024081224214](https://openairdocs.org/sdr/SWAA2024081224214), Aug 9, 2024: LENS. MISSING. FWD ENTRY DOOR EMERGENCY EXIT LOWER LIGHT LENS MISSING DIRECTIONAL ARROW<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-01-201-NG (EXIT SIGNS - MAINTENANCE PRACT
- [SDR SWAA2024081224206](https://openairdocs.org/sdr/SWAA2024081224206), Aug 9, 2024: LENS. MISSING. LEFT WING EMERGENCY EXIT LOWER LIGHT LEN MISSING DIRECTIONAL ARROW LEFT WING EMERGENCY EXIT LOWER LIGHT LEN MISSING DIRECTIONAL ARROW<[01] 01 - REMOVED AND REPL
- [SDR SWAA2024081224205](https://openairdocs.org/sdr/SWAA2024081224205), Aug 9, 2024: LENS. MISSING. RIGHT WING EMERGENCY EXIT LOWER LIGHT LEN MISSING DIRECTIONAL ARROW<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-01-201-NG (EXIT SIGNS - MAINTENANCE PRACTICES 
- [SDR SWAA2024080522145](https://openairdocs.org/sdr/SWAA2024080522145), Aug 2, 2024: MEGAPHONE. BROKEN. MEGAPHONE BROKEN<[01] R&R MEGAPHONE PER AMM 25-64-00
- [SDR SWAA2024072515890](https://openairdocs.org/sdr/SWAA2024072515890), Jul 23, 2024: SLIDE. OUT OF POSITION. FWD ENTRY SLIDE BOTTLE PRESSURE NOT IN VIEW<[01] REPOSITION SLIDE PER MT725-61-06
- [SDR SWAA2024061702001](https://openairdocs.org/sdr/SWAA2024061702001), Jun 15, 2024: GIRT BAR. NOT SEATED. FWD SERVICE DOOR GIRT BAR GIRT IS NOT PROPERLY STORED 2024-295623<[01] INSTALLED PROPERLY THE GIRT AND THE GIRT BAR AT ESCAPE SLIDE SERVICE DOOR IAW B737-700-AM
- [SDR SWAA2024061789280](https://openairdocs.org/sdr/SWAA2024061789280), May 24, 2024: LIGHT. BROKEN. BROKEN PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RT SIDE AT PASSENGER CABIN (1 EA) 2024-295581<[01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RT SIDE A
- [SDR SWAA2024061789279](https://openairdocs.org/sdr/SWAA2024061789279), May 24, 2024: LIGHT. BROKEN. BROKEN PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LT SIDE AT PASSENGER CABIN (2 EA) 2024-295580<[01] REPLACED BROKEN PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LT
- [SDR SWAA2024061702568](https://openairdocs.org/sdr/SWAA2024061702568), May 15, 2024: INTERCOSTAL. CRACKED. CRACK WEB - INTERCOSTAL BTW BS 500B TO BS 500C AND BTW STRINGER 26L TO STRINGER 25L AT FWD CARGO COMPARTMENT 2024-295571<[01] REPLACED WEB - INTERCOSTAL LOCATED
- [SDR SWAA2024061785641](https://openairdocs.org/sdr/SWAA2024061785641), May 15, 2024: INTERCOSTAL. CRACKED. CRACK WEB - INTERCOSTAL BTW BS 500B TO BS 500C AND BTW STRINGER 26L TO STRINGER 25L AT FWD CARGO COMPARTMENT 2024-295571<[01] REPLACED WEB - INTERCOSTAL LOCATED
- [SDR SWAA2024061783528](https://openairdocs.org/sdr/SWAA2024061783528), May 7, 2024: BRACKET. CRACKED. CRACK SUPPORT BRACKET BS 540 AND LBL 6 AT AIR CONDITIONING BAY. REPLACED SUPPORT BRACKET LOCATED BS 540 AND LBL 6 AT AIR CONDITIONING BAY DUE TO NOT FOUND ALLOW
- [SDR SWAA2024061783527](https://openairdocs.org/sdr/SWAA2024061783527), May 7, 2024: SPAR. CORRODED. CORROSION OUTBOARD FRONT SPAR LOWER CHORD OFSS 299 AT RT WING. PERFORMED REPAIR CORROSION OUTBOARD FRONT SPAR LOWER CHORD OFSS 299 AT RT WING IAW EA# 24-157-014
- [SDR SWAA2024061782256](https://openairdocs.org/sdr/SWAA2024061782256), May 4, 2024: FRAME. CRACKED. CRACK ON FRAME LOCATED STA259.5 BETWEEN STR 8L TO STR 9L AT PASSENGER CABIN 2024-295396<[01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC600D; S/N: 6000916163
- [SDR SWAA2024061782257](https://openairdocs.org/sdr/SWAA2024061782257), May 4, 2024: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE AFT POSITION LOCATED BTW BS 907 TO BS 927 AND BTW STR 25R TO STR 27R AT AFT CARGO COMPARTMENT 2024-295399<[01] REPLACED SUPPORT ANGLE AFT
- [SDR SWAA2024061782258](https://openairdocs.org/sdr/SWAA2024061782258), May 4, 2024: WEB. CRACKED. CRACK ON WEB LOCATED BTW BS 927 TO BS 947.5 AT LEVEL STR 25R AT CARGO COMPARTMENT 2024-295400<[01] REPLACED WEB LOCATED BTW BS 927 TO BS 947.5 AT LEVEL STR 25R 
- [SDR SWAA2024061782254](https://openairdocs.org/sdr/SWAA2024061782254), May 4, 2024: FITTING. CRACKED. CRACK ON FITTING LOCATED 947.5 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT 2024-295401<[01] REPLACED FITTING AND FASTENERS LOCATED 947.5 AT LEVEL STR 26L AT AFT C
- [SDR SWAA2024061782259](https://openairdocs.org/sdr/SWAA2024061782259), May 4, 2024: ANGLE. CRACKED. CRACK ON ANGLE LOCATED BS 867 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT 2024-295402<[01] REPLACED ANGLE LOCATED BS 867 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT
- [SDR SWAA2024061782260](https://openairdocs.org/sdr/SWAA2024061782260), May 4, 2024: WEB. CORRODED. CORROSION ON SHEILD WEB LOCATED BTW BS 847 TO BS 867 AT LEVEL STR 25R WL 156.1 AT AFT CARGO COMPARTMENT 2024-295403 CORROSION ON SHIELD WEB LOCATED BTW BS 847 T
- [SDR SWAA2024061702569](https://openairdocs.org/sdr/SWAA2024061702569), May 4, 2024: FITTING. CRACKED. CRACK ON FITTING LOCATED 947.5 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT 2024-295401<[01] REPLACED FITTING AND FASTENERS LOCATED 947.5 AT LEVEL STR 26L AT AFT C
- [SDR SWAA2024061782255](https://openairdocs.org/sdr/SWAA2024061782255), May 4, 2024: WEB. CORRODED. CORROSION ON SHEILD WEB LOCATED BTW BS 787 TO BS 767 AT LEVEL STR 25R WL 156.1 AT AFT CARGO COMPARTMENT 2024-295404<[01] REPLACED SHEILD WEB AND FASTENERS LOCAT
- [SDR SWAA2024061702571](https://openairdocs.org/sdr/SWAA2024061702571), May 4, 2024: FASTENER. CORRODED. CORROSION ON SHEILD WEB LOCATED BTW BS 787 TO BS 767 AT LEVEL STR 25R WL 156.1 AT AFT CARGO COMPARTMENT 2024-295404<[01] REPLACED SHEILD WEB AND FASTENERS LOCAT

All 359: https://openairdocs.org/aircraft/N467WN/reports.md

## STCs that may be installed (OpenAirDocs) (37)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Boeing 737-7H4)

- [STC ST00555AT](https://openairdocs.org/stc/ST00555AT): Installation of Airshow 210 system. AIRCRAFT RECONFIG TECHNOLOGIES, LLC. Lists 737 Series
- [STC SA4842SW](https://openairdocs.org/stc/SA4842SW): Modification of air to air heat exchanger (P/N 182820-2 Series 2). Honeywell International Inc. Lists 737 Series
- [STC SA270NW](https://openairdocs.org/stc/SA270NW): Installation of modified seat. Aviation Technical Services. Lists 737 Series
- [STC ST01162NY](https://openairdocs.org/stc/ST01162NY): Installation of Literature Pockets. Magee Plastics Company. Lists 737 Series
- [STC SA2607SO](https://openairdocs.org/stc/SA2607SO): Installation of coffee maker P/N 416-1001-29. B/E Aerospace Inc. Lists 737 Series
- [STC SA2608SO](https://openairdocs.org/stc/SA2608SO): Installation of rail assembly, P/N 416-0201-15. B/E Aerospace Inc. Lists 737 Series
- [STC SA3058SO](https://openairdocs.org/stc/SA3058SO): Installation of coffee maker 416-0001-23 and rail assembly 416-0201-5. B/E Aerospace Inc. Lists 737 Series
- [STC ST01476AT](https://openairdocs.org/stc/ST01476AT): Installation of coffee maker. B/E Aerospace Inc. Lists 737 Series
- [STC ST01778AT](https://openairdocs.org/stc/ST01778AT): Installation of espresso maker p/n 3510-0066-01. B/E Aerospace Inc. Lists 737 Series
- [STC SA629GL](https://openairdocs.org/stc/SA629GL): Installation of Grimes galley, Model 1545LW unit 2 and unit 4. B/E Aerospace. Lists 737 Series
- [STC ST01332AT](https://openairdocs.org/stc/ST01332AT): Installation of Galley Service Carts. Champ International, Inc. Lists 737 Series
- [STC ST09870SC](https://openairdocs.org/stc/ST09870SC): Installation of Mechanical Window Shades. Lou Martin & Associates. Lists 737 Series
- [STC ST00033AT](https://openairdocs.org/stc/ST00033AT): Installation of a single Mode S system and provisions for a TCAS II system. General Aerospace, Inc. Lists 737 Series
- [STC SA4532NM](https://openairdocs.org/stc/SA4532NM): Installation of Coltech, CTD-80 ATSCALL, enabling company calling of selected aircraft via company selected radio. Avtech Corporation. Lists 737 Series
- [STC ST4532NM](https://openairdocs.org/stc/ST4532NM): Installation of Coltech CTD-80 ATSCALL, enabling company calling of selected aircraft via company selected radio. Avtech Corporation. Lists 737 Series
- [STC ST00774NY](https://openairdocs.org/stc/ST00774NY): Installation of a passenger cabin Liquor/beverage service cart P/N E500170. (757-222) (767-222) (727-222) (737 SERIES 222, 291, 322, 522) (747-100 SERIES 238B). Driessen Aircraft Interior Systems USA, Inc. Lists 737 Series
- [STC ST02052AT](https://openairdocs.org/stc/ST02052AT): Installation of a single Collins GNLU910A flight management system, along with global navigation satellite system sensor. General Aerospace, Inc. Lists 737 Series
- [STC SA02034AT](https://openairdocs.org/stc/SA02034AT): Manufacture of tray carrier, P/N 2282-506. BFE Services. Lists 737 Series
- [STC ST01968AT](https://openairdocs.org/stc/ST01968AT): Manufacture of inserts for galley stowage. JK Aerospace, Inc. Lists 737 Series
- [STC SA01916AT](https://openairdocs.org/stc/SA01916AT): Manufacture of Tray Carrier P/N 1839-501. BFE Services. Lists 737 Series
- [STC SA2534SO](https://openairdocs.org/stc/SA2534SO): Installation of window shades, acoustic panes and reveals. Magee Plastics Company. Lists 737 Series
- [STC ST179CH](https://openairdocs.org/stc/ST179CH): Installation of cargo container curtain. Plastic Composites Corp. Lists 737 Series
- [STC SA00056LA](https://openairdocs.org/stc/SA00056LA): Installation of Weber Coffeemaker, P/N 870130-415. Monogram Systems. Lists 737 Series
- [STC SA6090NM](https://openairdocs.org/stc/SA6090NM): Installation of emergency vision assurance system (EVAS). VisionSafe Corporation. Lists 737 Series
- [STC SA370NW](https://openairdocs.org/stc/SA370NW): Removal of passenger interior, installation of cargo compartment liners and cargo tie down equipment. Western Metal Products. Lists 737 Series
- [STC SA2589CE](https://openairdocs.org/stc/SA2589CE): Install Bennetts Seat Converter Stowage Compartment on passenger seat(s). John's Aircraft and Upholstery. Lists 737 Series
- [STC SA1029NW](https://openairdocs.org/stc/SA1029NW): Installation of a cargo system. Western Metal Products. Lists 737 Series
- [STC SA1258EA](https://openairdocs.org/stc/SA1258EA): Installation of Cosco model78-( ) child restraint system. (172M S/N 17263459 - 17267584). Miller Stuart R. Lists 737 Series
- [STC SA1052SO](https://openairdocs.org/stc/SA1052SO): Installation of GE battery P/N43B022RB36 in place of Marathon P/N CA-727-7, CA-727-20, or CA-27-20 batteries or SAFT P/N23180 batteries; or installation of GE battery P/N 43B020RB10 replacing Marathon P/N CA-727-7, CA-727-20 or CA-27-20 or SAFT P/N 23186 or 23180 batteries. General Electric Company. Lists 737 Series
- [STC SA1082NW](https://openairdocs.org/stc/SA1082NW) (historical): Installation of auxiliary fuel tanks in the aft cargo compartment. (737 series -2K9A). Rogerson ATS. Lists 737 Series

### Approved for the engine (CFM International CFM56 series)

- [STC SE04840NY](https://openairdocs.org/stc/SE04840NY): Installation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engine. Kilroy Aviation LLC. Lists CFM56-7B20
- [STC SE03036CH](https://openairdocs.org/stc/SE03036CH): Application of a deep compressive stress layer using a Low Plasticity Burnishing (LPB) process on CFM56-7 Series Engines Stage 1 High Pressure Compressor (HPC) Blade Dovetails in accordance with Delta Air Lines Inc. Drawing No. 72-0396, Revision B, dated November 3, 2011, or later FAA Approved revision. Delta Air Lines Inc. Lists CFM56-7B20
- [STC SE00032EN](https://openairdocs.org/stc/SE00032EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 Fan/Booster Module. Pratt & Whitney. Lists CFM56-3
- [STC SE00033EN](https://openairdocs.org/stc/SE00033EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 High Pressure Compressor Module. Pratt & Whitney. Lists CFM56-3
- [STC SE00034EN](https://openairdocs.org/stc/SE00034EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 High Pressure Turbine Module. Pratt & Whitney. Lists CFM56-3
- [STC SE00035EN](https://openairdocs.org/stc/SE00035EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 Low Pressure Turbine Module. Pratt & Whitney. Lists CFM56-3
- [STC SE00822CH](https://openairdocs.org/stc/SE00822CH): Install AeroControlex P/N 2604880-001 variable stator feedback control cable and P/N 2604880-002 variable bleed valve feedback control cable on CFM International engines. AeroControlex Group TransDigm Inc. Lists CFM56-2

## Related

- Other Boeing 737-7H4 aircraft: https://openairdocs.org/model/boeing-737-7h4/aircraft.md
- The CFM International CFM56 series engine: https://openairdocs.org/engine/cfm-international-cfm56-series.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.