# N445WN: 2003 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: 29841
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 3, 2003
- Certificate issued: January 23, 2004
- Expires: June 30, 2029
- Mode S code: A55F31
- 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=445WN
- Page: https://openairdocs.org/aircraft/N445WN

From the FAA registry file of October 21, 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/N445WN/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 N445WN.

## FAA accident and incident reports

None matched to N445WN.

## Service difficulty reports (289, newest 50)

As reported by operators and repair stations.

- [SDR SWAA2026081787426](https://openairdocs.org/sdr/SWAA2026081787426), Aug 13, 2026: LIGHT. INOPERATIVE. LEFT FWD EXTERNAL EMERGENCY LIGHT IS INOPERATIVE. R & R EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-04-960-801, OPS CHKD GOOD.
- [SDR SWAA2026022573053](https://openairdocs.org/sdr/SWAA2026022573053), Feb 21, 2026: COMPRESSOR. STALLED. 10-15 COMPRESSOR STALLS RIGHT ENGINE = 89% N1 @ 31;000 FT. RETARDED ENGINE TO 40% N1 & ENGINE STABILIZED. WAS ABLE TO GET ENGINE BACK TO NORMAL OPS PER QRH.<
- [SDR SWAA2026022372611](https://openairdocs.org/sdr/SWAA2026022372611), Feb 19, 2026: CHECK VALVE. FAULTED. RIGHT ENGINE COMPRESSOR STALLED AT FL 290. ACCOMPLISHED BORESCOPE INSPECTIONS IAW AMM 71-00-00-210-801-F00, NO FINDINGS TIME LIMITING OR BEYOND AMM LIMITS. REMO
- [SDR SWAA2026011259836](https://openairdocs.org/sdr/SWAA2026011259836), Jan 8, 2026: CHECK VALVE. FAULTED. SUSPECTED COMPRESSOR STALLS (X3) ON NR 1 ENG UPON LEVEL OFF. ACCOMP BY FLUCTUATING EGT MOMENTARILY. STABILIZED WITHOUT REPEAT FOR DURATION OF FLT. CREW NOTED EV
- [SDR SWAA2026010555813](https://openairdocs.org/sdr/SWAA2026010555813), Dec 27, 2025: PRESSURE BLKHD. CRACKED. CRACK INDICATION AT BS 1016 APB DOME APEX UPPER LEFT FASTENER ON THE GORE WEB LAP SPLICE AT S-23R MEASURING 0.0625 INCH IN LENGTH FROM FASTENER HEAD. REPAIRED B
- [SDR SWAA2025122955665](https://openairdocs.org/sdr/SWAA2025122955665), Dec 25, 2025: SIGN. DETACHED. EXIT/SALIDA SIGN FELL FROM FORWARD CABIN ON TAKEOFF. R & R FWD EXIT SIGN LIGHT ASSY IAW AMM 33-51-01.
- [SDR SWAA2025102721975](https://openairdocs.org/sdr/SWAA2025102721975), Oct 6, 2025: WEB. CORRODED. CORROSION UPPER MAIN SILL WEB LOCATED BETWEEN BS440 TO BS492 AT LEVEL STR 18R AND WL 198.5. REPLACED WEB AND FASTENERS LOCATED BTW BS440 TO BS492 AT LEVEL STR18
- [SDR SWAA2025102721977](https://openairdocs.org/sdr/SWAA2025102721977), Oct 6, 2025: NUT PLATE. CORRODED. CORROSION ON RAIL NUT-PLATE LOCATED ORSS 404 INTERNAL CAVITY UPPER AREA TRAILING EDGE AT RT WING. REPLACED RAIL NUT-PLATE LOCATED ORSS 404 INTERNAL CAVITY UPPER
- [SDR SWAA2025102721832](https://openairdocs.org/sdr/SWAA2025102721832), Oct 6, 2025: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 265 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 265 AT LT WING IAW SRM 51-40-02 AND SRM 5
- [SDR SWAA2025102721978](https://openairdocs.org/sdr/SWAA2025102721978), Oct 6, 2025: NUT PLATE. CORRODED. CORROSION ON RAIL NUT-PLATE LOCATED ORSS 297 INTERNAL CAVITY TRAILING EDGE AT RT WING. REPLACED RAIL NUT-PLATE LOCATED ORSS 297 INTERNAL CAVITY TRAILING EDGE AT
- [SDR SWAA2025102721833](https://openairdocs.org/sdr/SWAA2025102721833), Oct 6, 2025: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 216 AT LT WING . REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 216 AT LT WING IAW SRM 51-10-02 ITEM 9 A
- [SDR SWAA2025102721831](https://openairdocs.org/sdr/SWAA2025102721831), Oct 6, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE TRAILING EDGE LOCATED IRSS 212 AT LT WING. REPLACED SUPPORT ANGLE AND FASTENERS TRAILING EDGE LOCATED IRSS 212 AT LT WING IAW SRM 51-40-0
- [SDR SWAA2025102721976](https://openairdocs.org/sdr/SWAA2025102721976), Oct 6, 2025: NUT PLATE. CORRODED. CORROSION ON RAIL NUT-PLATE LOCATED ORSS 376 INTERNAL CAVITY TRAILING EDGE AT RT WING.
- [SDR SWAA2025102721683](https://openairdocs.org/sdr/SWAA2025102721683), Oct 5, 2025: STRAP. CORRODED. CORROSION STRAP LOCATED BETWEEN BS 794.5 TO 807, S26R, WL 153 IN AFT CARGO BAY. REPLACED STRAP & FASTENERS IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, AND DWG 146A83
- [SDR SWAA2025102721684](https://openairdocs.org/sdr/SWAA2025102721684), Oct 5, 2025: WEB. CORRODED. CORROSION LOWER SILL LOCATED BETWEEN BS 794.5 TO 847, STR 25R, WL156 IN AFT CARGO BAY. REPLACED LOWER SILL AND FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 146A8340
- [SDR SWAA2025102721477](https://openairdocs.org/sdr/SWAA2025102721477), Oct 4, 2025: FLOORBEAM. CRACKED. CRACKED BRAKE PANEL FLOORBEAM LOCATED BS 540, BL 0 TO RBL 24.75 AT PASSENGER CABIN REPLACED FLOORBEAM AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND 
- [SDR SWAA2025102721110](https://openairdocs.org/sdr/SWAA2025102721110), Oct 4, 2025: SUPPORT ANGLE. CRACKED. CRACK ANGLE FLOOR STRUCTURE LOCATED STA695 AND RBL24.75 PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED ON FLOOR STRUCTURE AT STA695 AND RBL24.75 
- [SDR SWAA2025102721479](https://openairdocs.org/sdr/SWAA2025102721479), Oct 4, 2025: TAIL CONE. DELAMINATED. DELAMINATED TAIL CONE ON EXTERNAL SKIN. REPAIRED TAIL CONE ON EXTERNAL SKIN IAW SRM 51-70-04-2R-1 REPAIR 1.
- [SDR SWAA2025102721109](https://openairdocs.org/sdr/SWAA2025102721109), Oct 3, 2025: SUPPORT ANGLE. CRACKED. CRACK ANGLE FLOOR STRUCTURE LOCATED STA695 AND LBL24.75 PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED ON FLOOR STRUCTURE IAW SRM 51-40-02-0G-0, 
- [SDR SWAA2025102721106](https://openairdocs.org/sdr/SWAA2025102721106), Oct 3, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 571FB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 571FB TRAILING EDGE AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.
- [SDR SWAA2025102720583](https://openairdocs.org/sdr/SWAA2025102720583), Oct 2, 2025: SCUFF PLATE. CRACKED. CRACK ON AFT CORNER SCUFF PLATE AT AFT CARGO BAY. REPAIRED THE AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.
- [SDR SWAA2025102720580](https://openairdocs.org/sdr/SWAA2025102720580), Oct 2, 2025: SUPPORT ANGLE. CRACKED. CRACK TRAILING EDGE SUPPORT ANGLE LOCATED INTERNAL CAVITY AT LEVEL ORSS 285 AT LT WING. REPLACED TRAILING EDGE SUPPORT ANGLE LOCATED INTERNAL CAVITY AT LEVEL OR
- [SDR SWAA2025102720581](https://openairdocs.org/sdr/SWAA2025102720581), Oct 2, 2025: SUPPORT ANGLE. CRACKED. CRACK TRAILING EDGE SUPPORT ANGLE LOCATED INTERNAL CAVITY AT LEVEL ORSS 270 AT LT WING. REPLACED TRAILING EDGE SUPPORT ANGLE LOCATED INTERNAL CAVITY AT LEVEL OR
- [SDR SWAA2025102720741](https://openairdocs.org/sdr/SWAA2025102720741), Oct 2, 2025: RIB. CRACKED. CRACK INSPAR RIB LOCATED STAB STA 120.30 AND 9 INCHES OF REAR SPAR AT RT HORIZONTAL STABILIZER. PERFORMED REPAIR LOCATED STAB STA 120.30 AND 9 INCHES OF REAR SP
- [SDR SWAA2025102719923](https://openairdocs.org/sdr/SWAA2025102719923), Sep 30, 2025: LIGHT. BROKEN. BROKEN PHOTOLUMINESCENT STRIP ON LH SIDE (7EA) AT PASSENGER CABIN 2025-611549<[01] REPLACED PHOTOLUMINESCENT STRIP ON LH SIDE (7EA) AT PASSENGER CABIN IAW B737-
- [SDR SWAA2025102719924](https://openairdocs.org/sdr/SWAA2025102719924), Sep 30, 2025: LIGHT. BROKEN. BROKEN PHOTOLUMINESCENT STRIP RH SIDE (7EA) AT PASSENGER CABIN. REPLACED PHOTOLUMINESCENT STRIP RH SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-15-400-802;[02
- [SDR SWAA2025092918571](https://openairdocs.org/sdr/SWAA2025092918571), Sep 26, 2025: SLIDE. DISLODGED. FWD PAX DOOR DISLODGED AIR SLIDE FROM GIRT BAR, DID NOT INFLATE. RE-INSTALLED SLIDE PER MT 725-61-06
- [SDR SWAA2025063085795](https://openairdocs.org/sdr/SWAA2025063085795), Jun 27, 2025: HANDLE. UNSECURE. INSIDE ASSIST HANDLE NEXT TO AFT SERVICE DOOR NOT SECURE.<[01] SECURED IAW SIP.
- [SDR SWAA2025060377046](https://openairdocs.org/sdr/SWAA2025060377046), May 31, 2025: SEAT BACK. OUT OF ADJUST. SEAT 12F WILL NOT STAY UP. SECURED UPRIGHT. <[01] SECURED SEAT UPRIGHT. REFER LP# 2258629 FOR NEW MEL.; [02] SIGNED OFF AS FACT IN MAINTENIX IN ERROR. CREATED N
- [SDR SWAA2025040721623](https://openairdocs.org/sdr/SWAA2025040721623), Apr 3, 2025: TRANSMITTER. LOCKED. FLAPS LOCK OUT AT 9 DEGREES; TRAILING EDGE DISAGREE LIGHT; WE DROVE THE FLAPS TO 15 DEGREES PER THE QRH. ALL INDICATIONS NORMAL.<[01] R&R R/H FLAP POSITION TRAN
- [SDR SWAA2025021796397](https://openairdocs.org/sdr/SWAA2025021796397), Feb 15, 2025: WINDSHIELD. CRACKED. R1 WINDSHIELD CRACKED IN FLIGHT<[01] REMOVED AND REPLACED R1 WINDSHIELD AND R1 WHCU IAW AMM 56-11-11 AND AMM 30-41-11. AIRCRAFT RECERTIFED TO CAT III STATUS PER
- [SDR SWAA2025021796899](https://openairdocs.org/sdr/SWAA2025021796899), Feb 15, 2025: CONTROL UNIT. FAULTED. R1 WINDSHIELD CRACKED IN FLIGHT<[01] REMOVED AND REPLACED R1 WINDSHIELD AND R1 WHCU IAW AMM 56-11-11 AND AMM 30-41-11. AIRCRAFT RECERTIFED TO CAT III STATUS PER
- [SDR SWAA2024091636149](https://openairdocs.org/sdr/SWAA2024091636149), Sep 11, 2024: WEB. CRACKED. LMLG CENTER DOOR CRACKED AT WEB- MARKED<[01] REMOVED L/H MLG CTR & INNER DOOR ASSEMBLY. I.A.W. AMM 32-13-11. OK FOR CONTINUED SERVICE PER CDL 32-10-3XC
- [SDR SWAA2024082629290](https://openairdocs.org/sdr/SWAA2024082629290), Aug 22, 2024: STARTER. OVERHEATED. ON #1 ENGINE START HAD ENGINE 1 OVERHEAT FOLLOWED BY #1 ENGINE FIRE INDICATION; COMPLIED WITH QRC AND QRH PROCEDURES.<[01] REF BAR CODE TTG8Q00VE9LA FOR STARTER
- [SDR SWAA2024070106898](https://openairdocs.org/sdr/SWAA2024070106898), Jun 27, 2024: LENS. DISLODGED. EMERGENCY EXIT LENS DISLODGED FROM ABOVE FWD SERVICE DOOR LOCKING PIN MISSING FROM LIGHT ASSY FWD SIDE<[01] C/W EA M21-133-00720
- [SDR SWAA2024060597715](https://openairdocs.org/sdr/SWAA2024060597715), Jun 3, 2024: LIGHT. INOPERATIVE. EXTERIOR AFT MOST LEFT EMERGENCY LIGHT INOP<[01] RELAMPED EXTERIOR AFT MOST EMERGENCY LIGHT REF AMM 33-51-00 OPS CHECK GOOD
- [SDR SWAA2024020246984](https://openairdocs.org/sdr/SWAA2024020246984), Jan 31, 2024: LAMP. INOPERATIVE. EXTERIOR EMERGENCY LIGHT AFT OF AFT ENTRY DOOR INOP<[01] RE-LAMPED THE EXTERIOR EMERGENCY LIGHT AFT OF THE AFT ENTRY DOOR IAW AMM 33-51-04. OPS CHECK GOOD
- [SDR SWAA2024012243019](https://openairdocs.org/sdr/SWAA2024012243019), Jan 18, 2024: GIRT BAR. OUT OF ADJUST. DOOR 1R FLOOR CLIPS FPR SLIDE GIRT BAR MIGHT BE FACING WRONG DIRECTION; AS NOTICED BY FLIGHT ATTENDANTS.<[01] REMOVED AND REINSTALLED FORWARD SERVICE DOOR FLOOR
- [SDR SWAA2024010432957](https://openairdocs.org/sdr/SWAA2024010432957), Dec 17, 2023: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT BATTERY PACKS FOR POWER SUPPLY'S M1672; M1673; M1674 FAILED CAPACITY CHECK EMERGENCY LIGHTS INOP AND DID STAY ON.<[01] REMOVED AND REPLACED BATT
- [SDR SWAA2024010426504](https://openairdocs.org/sdr/SWAA2024010426504), Nov 30, 2023: SCUFF PLATE. CRACKED. R1 DOOR ; SCUFF PLATE FOUND CRACK AT FWD CORNER<[01] ACCOMPLISHED WELD REPAIR OF CRACK FOUND AT R1 DOOR SCUFF PLATE FWD CORNER PER REF B737 SRM 53-70-15-2R-1;[0
- [SDR SWAA2024010425465](https://openairdocs.org/sdr/SWAA2024010425465), Nov 27, 2023: RIB. CRACKED. LEFT HORIZONTAL STABILIZER LE (PANEL 331B)HAS CRAKED RIB # 19 DOT# 223<[01] REMOVED AND REPLACED RIB# 19 AT LEFT HORIZONTAL STABILIZER LE PANEL 331 B AS PER B 7
- [SDR SWAA2024010425462](https://openairdocs.org/sdr/SWAA2024010425462), Nov 27, 2023: INTERCOSTAL. CRACKED. AFT OF FWD CARGO COMPARTMENT; RIGHT SIDE STG 25 BS 500D TO BS 520 INTERCOSTAL CRACK NOTED (P/N: 143A9803-58).<[01] REMOVED AND REPLACED INTERCOSTAL AT FWD CARGO
- [SDR SWAA2023122924006](https://openairdocs.org/sdr/SWAA2023122924006), Nov 22, 2023: PANEL. CRACKED. R2 DOOR LOWER PANEL 844DZ FOUND CRACKED AND BENT IN SEVERAL PLACES.<[01] RECEIVED NEW R2 DOOR LOWER PANEL 844DZ FROM STOCK. ITEM TO BE INSTALLED ON TTG8Q00PRE1S
- [SDR SWAA2024010527539](https://openairdocs.org/sdr/SWAA2024010527539), Nov 20, 2023: THRUST REVERSER. CORRODED. CORROSION AT NO-2 ENGINE INB THRUST REVERSER AFT TRAILING EDGE<[01] EVALUATED DAMAGE AREA AT NO2 ENG I/B T/R AFT T/E SKIN; FOUND DEEP PITTING CORROSION OUT OF L
- [SDR SWAA2024010527540](https://openairdocs.org/sdr/SWAA2024010527540), Nov 20, 2023: THRUST REVERSER. CORRODED. CORROSION AT NO-2 ENGINE OUB THRUST REVERSER AFT TRAILING EDGE<[01] EVALUATED DAMAGE AREA AT NO2 ENG O/B T/R AFT T/E SKIN; FOUND DEEP PITTING CORROSION OUT OF L
- [SDR SWAA2024010323500](https://openairdocs.org/sdr/SWAA2024010323500), Nov 20, 2023: PANEL. CRACKED. AFT CARGO COMPARTMENT PANEL #142YAC; WAVY SURFACE AND CRACKED EDGES.<[01] FABRICATED NEW AFT CARGO PANEL #142YAC PER REF AMM 25-52-01-201-801;[02] FINAL INSPECT
- [SDR SWAA2024010523222](https://openairdocs.org/sdr/SWAA2024010523222), Nov 19, 2023: PANEL. CORRODED. CORROSION SPOT AT R/W FRONT SPAR L/E FUEL QTY INDICATORS SUPPORT PANEL MKD DOT<[01] REMOVED REFUEL PANEL (P15) PER TASK 28-21-00-000-801; INSTALLED EWIS PROTECT
- [SDR SWAA2024010422609](https://openairdocs.org/sdr/SWAA2024010422609), Nov 17, 2023: SUPPORT BRACKET. CORRODED. CORROSION ** MAIN CABIN CENTER WING BOX HORIZONTAL BEAM SUPPORT BRACKET @ LBL-64 STA 706 MKD DOT<[01] REMOVED AND REPLACED SUPPORT BRACKET AT MAIN CABIN CENTER 
- [SDR SWAA2024010422610](https://openairdocs.org/sdr/SWAA2024010422610), Nov 17, 2023: SUPPORT BRACKET. CORRODED. CORROSION ** MAIN CABIN CENTER WING BOX HORIZONTAL BEAM SUPPORT BRACKET @ LBL-64 STA 706+10' MKD DOT<[01] REMOVED AND REPLACED SUPPORT BRACKET AT MAIN CABIN CEN
- [SDR SWAA2024010422612](https://openairdocs.org/sdr/SWAA2024010422612), Nov 17, 2023: SUPPORT BRACKET. CORRODED. CORROSION ** MAIN CABIN CENTER WING BOX HORIZONTAL BEAM SUPPORT BRACKET @ LBL-65 STA 727 MKD DOT<[01] REMOVED AND REPLACED SUPPORT BRACKET AT MAIN CABIN LBL 65 

All 289: https://openairdocs.org/aircraft/N445WN/reports.md

## Related

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

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