# N465WN: 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: 33829
- Year built: 2004
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 11, 2004
- Certificate issued: July 15, 2004
- Expires: October 31, 2027
- Mode S code: A5AE2F
- 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=465WN
- Page: https://openairdocs.org/aircraft/N465WN

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/N465WN/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

None matched to N465WN.

## FAA accident and incident reports

None matched to N465WN.

## Service difficulty reports (285, 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 SWAA2026101274296](https://openairdocs.org/sdr/SWAA2026101274296), Oct 7, 2026: ASSIST HANDLE. BROKEN. PASSENGER ENTRY DOOR ASSIST HANDLE BROKEN. REMOVED AND REPLACED IAW AMM INTRODUCTION-NG (USE OF STANDARD INDUSTRY PRACTICES - SIP - PERMANENT)]
- [SDR SWAA2026031678273](https://openairdocs.org/sdr/SWAA2026031678273), Mar 10, 2026: ENGINE. POWER LOSS. AT TOP OF CLIMB NR 1 ENGINE REDUCED TO 60% N1 UN-COMMANDED WITH NO THRUST LEVER SPLIT, NR 2 ENGINE REDUCED TO 85% N1 AS EXPECTED. AUTO-THROTTLES WERE ON. ALL OT
- [SDR SWAA2026012859175](https://openairdocs.org/sdr/SWAA2026012859175), Jan 7, 2026: PLATE. CRACKED. CRACKED CORRUGATED PLATE ORSS 261, RT WING T/E. REPLACED THE CORRUGATED PLATE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 115A2001, SHEET 29, RE
- [SDR SWAA2026012859177](https://openairdocs.org/sdr/SWAA2026012859177), Jan 7, 2026: ANGLE. CRACKED. CRACKED ANGLE, ORSS 271, RT WING T/E. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, & DWG 115A2900, SHEET 2, REV E. MEASUREMENT OF CRACK: L= 0.320.
- [SDR SWAA2026012859176](https://openairdocs.org/sdr/SWAA2026012859176), Jan 7, 2026: PLATE. CRACKED. CRACKED CORRUGATED PLATE ORSS 241, RT WING T/E. REPLACED THE CORRUGATED PLATE IAW SRM 51-40-02-0G, & DWG 115A2001, SHEET 30, REV A.
- [SDR SWAA2026012858919](https://openairdocs.org/sdr/SWAA2026012858919), Jan 6, 2026: SUPPORT BRACKET. CRACKED. CRACKED SUPPORT BRACKET ON THE VAPOR BARRIER, RBL 15.54 - RBL 25. REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 111A1000, SHEET 1
- [SDR SWAA2026012858801](https://openairdocs.org/sdr/SWAA2026012858801), Jan 6, 2026: VAPOR BARRIER. CRACKED. CRACKED VAPOR BARRIER RT SIDE BETWEEN RBL 15 & 25. REPAIRED THE VAPOR BARRIER IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026012858916](https://openairdocs.org/sdr/SWAA2026012858916), Jan 6, 2026: RIB. CRACKED. CRACKED RIB, LE STA 142.45 ACCESS PANEL 341B, RT HORIZONTAL STAB REPLACED THE RIB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 186A1001, SHEET 10, REV A.
- [SDR SWAA2026012858310](https://openairdocs.org/sdr/SWAA2026012858310), Jan 5, 2026: LANDING. CRACKED. CRACKED ACCESS PANEL 343AT LANDING AT RT HORIZONTAL STAB. REPLACED THE LANDING AND FASTENER IAW SRM 51-40-02, & 51-10-02 ITEM 9. MEASURE OF CRACK IS L: 0.249?.<
- [SDR SWAA2026012857873](https://openairdocs.org/sdr/SWAA2026012857873), Jan 3, 2026: CROSSBEAM. CRACKED. CRACKED CROSSBEAM, BS 540, BL 0 - RBL 24.75. REPLACED CROSSBEAM IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A0060, SHEET 36, REV A.
- [SDR SWAA2026012857874](https://openairdocs.org/sdr/SWAA2026012857874), Jan 3, 2026: CROSSBEAM. CRACKED. CRACKED CROSSBEAM BS 540, BL 0 - LBL 24.75. REPLACED CROSSBEAM IAW SRM 51-40-02, AND DWG 143A0060, SHEET 36, REV A.
- [SDR SWAA2026012857876](https://openairdocs.org/sdr/SWAA2026012857876), Jan 3, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE BS 695, RBL 24.75. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 273A9110, SHEET 6, REV A.
- [SDR SWAA2026012857983](https://openairdocs.org/sdr/SWAA2026012857983), Jan 3, 2026: ACCESS PANEL. ELONGATED. ELONGATED HOLES ON ACCESS PANEL 561CB, T/E, LT WING. REPAIRED THE ACCESS PANEL 561CB IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026012757877](https://openairdocs.org/sdr/SWAA2026012757877), Jan 3, 2026: FLOOR SUPPORT. CRACKED. CRACKED FLOOR SUPPORT, OTBD SIDE, BS 695 BL 0. REPLACED FLOOR SUPPORT AND FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 273A9110, SHEET 6, REV A.
- [SDR SWAA2026012757879](https://openairdocs.org/sdr/SWAA2026012757879), Jan 3, 2026: FLOOR SUPPORT. CRACKED. CRACKED FLOOR SUPPORT, BS 695, BL 0. REPLACED THE FLOOR SUPPORT AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 273A9110, SHEET 6, REV A.
- [SDR SWAA2026012757880](https://openairdocs.org/sdr/SWAA2026012757880), Jan 3, 2026: FLOOR SUPPORT. CRACKED. CRACKED FLOOR SUPPORT OTBD SIDE, BS 695, BL 0. REPLACED FLOOR SUPPORT IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DRAWING 273A9110, SHEET 6, REV A.
- [SDR SWAA2026012757741](https://openairdocs.org/sdr/SWAA2026012757741), Jan 2, 2026: SKIN. CRACKED. CRACKED SLAT 2, SS 322.71, LT WING. PERFORMED PERMANENT REPAIR IAW SRM 57-42-01-2R-8, REPAIR 8.
- [SDR SWAA2025123156725](https://openairdocs.org/sdr/SWAA2025123156725), Dec 29, 2025: SLIDE. OUT OF ADJUST. FWD GALLEY DOOR SLIDE PARTIALLY OUT OF BOX. INSTALLED THE FWD SERVICE DOOR SLIDE ASSEMBLY IAW MT 725-61-06.
- [SDR SWAA2025121953161](https://openairdocs.org/sdr/SWAA2025121953161), Dec 17, 2025: BATTERY PACK. INOPERATIVE. FOUND ROW 6 ABC EMERGENCY LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM 33-51-06. OPS CHECKED GOOD.
- [SDR SWAA2025121651934](https://openairdocs.org/sdr/SWAA2025121651934), Dec 13, 2025: HANDLE. BROKEN. R1 DOOR ASSIST HANDLE BROKEN. INSTALLED A SERVICEABLE ASSIST HANDLE ONTO THE R1 DOOR FROM FWD LAVATORY IAW AMM 52-11-31. OK TO CONTINUE IAW MEL 25-10-01, SP1B A
- [SDR SWAA2025091715500](https://openairdocs.org/sdr/SWAA2025091715500), Sep 16, 2025: TRANSFER SYS. NO DISCREPANCY. AFTER LEVEL OFF AT 10;000 ABOUT 12 MINUTES INTO FLIGHT WE RECEIVED A MASTER CAUTION FOR FUEL W/FUEL IMBALANCE ON NR 1 TANK. COMPLIED WITH QRH TO BALANCE FUEL. F
- [SDR SWAA2025091513812](https://openairdocs.org/sdr/SWAA2025091513812), Sep 11, 2025: ENGINE. FAILED. NUMBER 1 ENGINE FAILED AFTER TAKEOFF, LOUD BANG, N1 DROPPED TO APPROX 16%, EGT REMAINED IN THE YELLOW. NO NOTICEABLE SMELL OF SMOKE R & R NR 1 ENGINE IAW MT 771
- [SDR SWAA2025090811786](https://openairdocs.org/sdr/SWAA2025090811786), Sep 5, 2025: CHARGER. INOPERATIVE. EMERGENCY EXIT LIGHT OVERHEAD AILSE AT MID CABIN AND LIGHT ON OVERWING EXIT CAPT SIDE WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERY CHARGER AND BATTERY AMM 
- [SDR SWAA2025090812316](https://openairdocs.org/sdr/SWAA2025090812316), Sep 5, 2025: BATTERY. INOPERATIVE. EMERGENCY EXIT LIGHT OVERHEAD AILSE AT MID CABIN AND LIGHT ON OVERWING EXIT CAPT SIDE WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERY CHARGER AND BATTERY AMM 
- [SDR SWAA2025061079046](https://openairdocs.org/sdr/SWAA2025061079046), Jun 7, 2025: COVER. MISSING. CABIN R/H EMERGENCY EXIT DOOR FWD EMERGENCY LIGHT COVER IS MISSING.<[01] INSTALLED NEW LIGHT COVER ON EXIT SIGN FOR R/H EMERGENCY EXIT DOOR FWD LIGHT PER AMM 33
- [SDR SWAA2025021795502](https://openairdocs.org/sdr/SWAA2025021795502), Feb 13, 2025: GIRT BAR. UNPACKED. L1 DOOR ESCAPE SLIDE GIRT REPACKED REQUIRED.<[01] REPACKED L1 DOOR SLIDE GIRT PER AMM 25-66-01.
- [SDR SWAA2025021395501](https://openairdocs.org/sdr/SWAA2025021395501), Feb 13, 2025: GIRT BAR. DEBONDED. AFT SERVICE DOOR R2 DOOR SLIDE GIRT BONDED BLACK LINER DISBONDED & SEPERATED.<[01] REMOVED AND REPLACED R2 DOOR SLIDE PER AMM 25-66-01. REF BARCODE TTG8Q004QAHQ
- [SDR SWAA2025012388881](https://openairdocs.org/sdr/SWAA2025012388881), Jan 23, 2025: BUSHING. LOOSE. PLASTIC BUSHING FELL OFF FWD SERVICE DOOR GIRT BAR<[01] REPLACED BUSHING IAW MM 25-66-01.
- [SDR SWAA2024100745252](https://openairdocs.org/sdr/SWAA2024100745252), Oct 4, 2024: COVER. MISSING. L1 DOOR EMERG EXIT SING COVER MISSING<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-01-960-802-NG (EXIT SIGN - LIGHT ASSEMBLY REPLACEMENT - PERMANENT)]
- [SDR SWAA2024091638147](https://openairdocs.org/sdr/SWAA2024091638147), Sep 16, 2024: SLIDE. DETACHED. FWD ENTRY DOOR SLIDE PARTIALLY FELL OUT OF COVER<[01] REINSTALLED SLIDE IN COVER PER MT 725-61-06. A/C OK FOR SERVICE.
- [SDR SWAA2024030753243](https://openairdocs.org/sdr/SWAA2024030753243), Feb 17, 2024: SCUFF PLATE. CRACKED. REJECT: CRACK FOUND AT FWD CORNER SCUFF PLATE ACB<[01] UPDATED MEASUREMENT TABLE;[02] IT WAS REMOVED AND WELDED FWD CORNER SCUFF PLATE;APPLIED CHEMICAL CONVERSI
- [SDR SWAA2024030652468](https://openairdocs.org/sdr/SWAA2024030652468), Feb 14, 2024: FAIRING. DELAMINATED. #1 CANOE FAIRING AFT FAIRING HAS DELAMINATION ON AFT END.<[01] REMOVED AND REPLACED #1 CANOE FAIRING AFT FAIRING IAW AIPC 27-51-28-01 AND AMM 20-50-11-910-801<B
- [SDR SWAA2024030850539](https://openairdocs.org/sdr/SWAA2024030850539), Feb 9, 2024: SKIN. CORRODED. REJECT: CORROSION AT FUSELAGE SKIN AROUND RADIO ALTIMETER ANTENNA STA-450 BTW STR-27L TO STR-28L<[01] REMOVED CORROSION AND REWORKED AREA AROUND RADIO ALTIMETER
- [SDR SWAA2024030850538](https://openairdocs.org/sdr/SWAA2024030850538), Feb 9, 2024: SKIN. CORRODED. REJECT: CORROSION AT FUSELAGE SKIN AROUND RADIO ALTIMETER ANTENNA STA-410 BTW STR-27L TO STR-28L<[01] VERIFIED STEP 3 COMPLETED;[02] 'REFER TO FAULT TTG8Q00RFUS
- [SDR SWAA2024030849681](https://openairdocs.org/sdr/SWAA2024030849681), Feb 6, 2024: PANEL. CORRODED. RIGHT WING FUELING PANEL (621GB) FUEL GAUGE PANEL IS CORRODED<[01] REPLACED WING REFUEL PANEL (P15) PER AMM 28-21-00-000-801; INSTALLED PER AMM 28-21-00-400-801
- [SDR SWAA2024030749685](https://openairdocs.org/sdr/SWAA2024030749685), Feb 6, 2024: DRIP TRAY. CRACKED. FLIGHT COMPARTMENT FLOOR STRUCTURE - CRACKED DRIPSHIELD BS 211.8 LBL 38 WL 208 (MARKED)<[01] REMOVED AND REPLACED FLIGHT COMPARTMENT FLOOR STRUCTURE DRIP SHIELD
- [SDR SWAA2024030749684](https://openairdocs.org/sdr/SWAA2024030749684), Feb 6, 2024: BRACKET. CRACKED. FLIGHT COMPARTMENT OVERHEAD - CRACKED BRACKET ASSY ON DRIP SHIELD OVHD BS 211.8 S-3R (MARKED)<[01] REMOVED AND REPLACED FLIGHT COMPARTMENT OVERHEAD RECEPTICLE O
- [SDR SWAA2024030749683](https://openairdocs.org/sdr/SWAA2024030749683), Feb 6, 2024: BRACKET. CRACKED. FLIGHT COMPARTMENT OVERHEAD - CRACKED BRACKET ASSY ON DRIP SHIELD OVHD BS 211.8 S-3L (MARKED)<[01] REMOVED AND REPLACED FLIGHT COMPARTMENT OVERHEAD RECEPTICLE O
- [SDR SWAA2024030749673](https://openairdocs.org/sdr/SWAA2024030749673), Feb 6, 2024: BRACKET. CRACKED. WING CENTER SECTION - CRACK ON SUPPORT AIR DUCT BS 540+7 RBL 6.30 WL 170.65 (MARKED)<[01] REMOVED AND REPLACED RH AIR DUCT SUPPORT BRACKET IAW SRM 51-40-02 AND 
- [SDR SWAA2024030749674](https://openairdocs.org/sdr/SWAA2024030749674), Feb 6, 2024: BRACKET. CRACKED. WING CENTER SECTION - CRACK ON SUPPORT AIR DUCT BS 540+7 LBL 6.30 WL 170.65 (MARKED)<[01] REMOVED AND REPLACED LH AIR DUCT SUPPORT BRACKET IAW SRM 51-40-02 AND 
- [SDR SWAA2024030749416](https://openairdocs.org/sdr/SWAA2024030749416), Feb 6, 2024: BRACKET. CRACKED. MAIN E-BAY O2 BOTTLE FWD SUPPORT BRACKET; LOWER ATTACH ANGLE IS CRACKED AT O/B FASTENER (MARKED)<[01] VERIFIED DAMAGE EVALUATION;[02] REMOVED AND INSTALLED NEW 
- [SDR SWAA2024030749409](https://openairdocs.org/sdr/SWAA2024030749409), Feb 6, 2024: ANGLE. CRACKED. SKIN SPLICES CRACKED AROUND HARDWARES AFT CARGO BS 907-927; WL 150; RBL 15.0.<[01] REMOVED AND REPLACED 2EA SUPPORT ANGLES FROM AFT CARGO BAY BETWEEN BS 907 TO 
- [SDR SWAA2024030848716](https://openairdocs.org/sdr/SWAA2024030848716), Feb 4, 2024: PANEL. PULLED. R/W T/E PANEL 661BB HAS SEVERAL PULLED FASTENER HOLES UNDER THE T/E SEAL (MARKED)<[01] R/W T/ E PANEL 661BB FASTENER HOLES HAVE BEEN REPAIRED IAW SRM 51-70-04-2
- [SDR SWAA2024030748722](https://openairdocs.org/sdr/SWAA2024030748722), Feb 4, 2024: SHIELD. CORRODED. FWD SHIELD CORRODED AROUND NUTPLATE HOLES LBL 21; 787-807; WL 150 FWD SHIELD CORRODEDN AROUND NUTE PLATES RBL 21 BS787-807 WL 150.<[01] REMOVED AND REPLACED ON 
- [SDR SWAA2024030748503](https://openairdocs.org/sdr/SWAA2024030748503), Feb 4, 2024: SIDEWALL SUPPORT. CORRODED. CORROSION FOUND AT SECTION 1; LBL 21; BS 440-500; WL 150 FAULT CORRECTION-CORROSION FOUND AT SECTION 1 AROUND NUTPLATE HOLES AT FLOOR TO SIDEWALL SUPPORT<[01] E
- [SDR SWAA2024030748720](https://openairdocs.org/sdr/SWAA2024030748720), Feb 4, 2024: SUPPORT. CORRODED. CORROSION ON FLOOR TO SIDEWALL SUPPORT RBL 21; BS 727 TO BS 787; WL 150<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT RBL 21; BS 727 TO BS 787; WL 150 I.A
- [SDR SWAA2024030748719](https://openairdocs.org/sdr/SWAA2024030748719), Feb 4, 2024: SUPPORT. CORRODED. CORROSION ON FLOOR TO SIDEWALL SUPPORT LBL 21; BS 727C TO BS 807; WL 150.<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT LBL 21; BS 727C TO BS 807; WL150 I
- [SDR SWAA2024030748717](https://openairdocs.org/sdr/SWAA2024030748717), Feb 4, 2024: SHIELD. CORRODED. AFT DOOR SHIELD CORRODED MULTIPLE AREAS BS 867-887; RBL 21; WL 150 AFT DOOR SHIELD CORROEDED MULTIPLE AREAS BS 847-867 RBL 21 WL 150.<[01] REMOVED AND REPLACED 
- [SDR SWAA2024030748509](https://openairdocs.org/sdr/SWAA2024030748509), Feb 4, 2024: RAIL. CORRODED. CORROSION FOUND AROUND NUTPLATES AROUND NUTPLATES BS 500 D; WL 150; LBL 8.1 AND 12.5<[01] VERIFIED STEP 7 IN PARTIAL.;[02] REMOVED AND REINSTALLED AFT BULKHEAD 
- [SDR SWAA2024030748507](https://openairdocs.org/sdr/SWAA2024030748507), Feb 4, 2024: SHIELD. CORRODED. AFT FWD CARGO DOOR FLOOR SHIELD HAS CORROSION AROUND NUTPLATE HOLES FAULT CORRECTION-AFT FWD CARGO DOOR FLOOR SHIELD HAS CORROSION AROUND NUTPLATE HOLES RBL 21 

All 285: https://openairdocs.org/aircraft/N465WN/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

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