# N482WN: 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: 29852
- Year built: 2004
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 8, 2004
- Certificate issued: October 4, 2004
- Expires: August 31, 2028
- Mode S code: A5F208
- 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=482WN
- Page: https://openairdocs.org/aircraft/N482WN

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/N482WN/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 N482WN.

## FAA accident and incident reports

None matched to N482WN.

## Service difficulty reports (301, newest 50)

As reported by operators and repair stations.

- [SDR SWAA2026100741317](https://openairdocs.org/sdr/SWAA2026100741317), Oct 3, 2026: PUMP. LOW PRESSURE. ENG 1 HYD PUMP LOW PRESSURE LIGHT CAME ON IN FLIGHT. HYDRAULIC SYSTEM A QTY: 13% PRESS: 3080.
- [SDR SWAA2026071420114](https://openairdocs.org/sdr/SWAA2026071420114), Jul 10, 2026: ATTACH BRACKET. CRACKED. AFT ENTRY (L2) DOOR LOWER DOOR LINER ATTACHMENT PANEL BRACKET IS CRACKED. REMOVED AND REPLACED AFT ENTRY (L2) DOOR LOWER DOOR LINER ATTACHMENT PANEL BRACKET USI
- [SDR SWAA2026071320213](https://openairdocs.org/sdr/SWAA2026071320213), Jul 10, 2026: BATTERY PACK. FAILED. FLIGHT DECK, BATTERY PACKS M1668 & M1675 EACH FAILED RESPECTIVE CAPACITY TESTS. R & R BATTERY PACKS M1668 & M1675 IAW AMM 33-51-06.
- [SDR SWAA2026071320978](https://openairdocs.org/sdr/SWAA2026071320978), Jul 10, 2026: BATTERY PACK. NO TEST. FLIGHT DECK, BATTERY PACKS M1668 & M1675 EACH FAILED RESPECTIVE CAPACITY TESTS. R & R BATTERY PACKS M1668 & M1675 IAW AMM 33-51-06.
- [SDR SWAA2026071019308](https://openairdocs.org/sdr/SWAA2026071019308), Jul 7, 2026: SIGN. BROKEN. CENTER CABIN CEILING OVER WING EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED IAW AMM 33-51-01-960-802-NG.
- [SDR SWAA2026061807884](https://openairdocs.org/sdr/SWAA2026061807884), May 30, 2026: STRAP. CORRODED. CORROSION ON RETAINER STRAP SEAL, SPOILER 1, LT WING. REPLACED RETAINER STRAP SEAL SPOILER 1 AT LT WING IAW SRM 51-40-02, DWG 115A3500, SHEET 22, REV A.
- [SDR SWAA2026061707972](https://openairdocs.org/sdr/SWAA2026061707972), May 30, 2026: PLATE. CRACKED. CRACKED OTBD TRAILING EDGE CORRUGATED PLATE ON ORSS 314, RT WING. REPLACED CORRUGATED PLATE LOCATED OTBD TRAILING EDGE ON ORSS 314 AT RT WING. IAW SRM 51-40-02-
- [SDR SWAA2026061707883](https://openairdocs.org/sdr/SWAA2026061707883), May 30, 2026: PLATE. CRACKED. CRACKED CORRUGATED PLATE TRAILING EDGE LOCATED ON IRSS 261 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ON IRSS 261 AT LT WING IAW SRM 51-40-02-0
- [SDR SWAA2026061707881](https://openairdocs.org/sdr/SWAA2026061707881), May 30, 2026: SUPPORT ANGLE. CRACKED. CRACKED OTBD TRAILING EDGE SUPPORT ANGLE ON ORSS 287 AT LT WING. REPLACED OTBD TE SUPPORT ANGLE AT ORSS 287, LT WING IAW SRM 51-40-02-0G-0, DWG 115A3700, SHEET 
- [SDR SWAA2026061707882](https://openairdocs.org/sdr/SWAA2026061707882), May 30, 2026: SUPPORT BRACKET. CRACKED. CRACKED TRAILING EDGE SUPPORT BRACKET LOCATED ON IRSS 268 AT LT WING. REPLACED SUPPORT BRACKET LOCATED TRAILING EDGE IRSS 268 AT LT WING IAW SRM 51-10-02-0G-0, 
- [SDR SWAA2026061707886](https://openairdocs.org/sdr/SWAA2026061707886), May 30, 2026: PLATE. CRACKED. CRACKED INBD TRAILING EDGE CORRUGATED PLATE LOCATED ON IRSS 242 AT LT WING. REPLACED CORRUGATED PLATE LOCATED ON INBD TRAILING EDGE IRSS 242 AT LT WING IAW SRM 
- [SDR SWAA2026061807351](https://openairdocs.org/sdr/SWAA2026061807351), May 28, 2026: FITTING. CRACKED. REMOVE AND REPLACE SLAT 1 LT WING DUE TO SECONDARY FINDING: CRACK ON FITTING SLAT 1. REPLACED LEADING EDGE SLAT 1 IAW AMM 27-81-21-401. TESTED OK .
- [SDR SWAA2026061707339](https://openairdocs.org/sdr/SWAA2026061707339), May 27, 2026: RIB. CRACKED. CRACKED INSPAR RIB LOCATED STAB BS 129.50 AND 18 INCH FROM FRONT SPAR RT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB STA 129.50 AND 18 INCHS OF FR
- [SDR SWAA2026061707340](https://openairdocs.org/sdr/SWAA2026061707340), May 27, 2026: SUPPORT ANGLE. ELONGATED. ELONGATED HOLE ON SUPPORT ANGLE FOR ACCESS PANEL 551FB TRAILING EDGE AT LT WING. REPLACED SUPPORT ANGLE AND RE-INSTALLED BRACKET(2E/A) ACCESS PANEL 551FB TRAILI
- [SDR SWAA2026061707341](https://openairdocs.org/sdr/SWAA2026061707341), May 27, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, ACCESS PANEL 651GB AT RT WING. REPLACED SUPPORT ANGLE, ACCESS PANEL 651GB AT RT WING IAW SRM 51-40-02-0G-0 AND SRM 51-10-02 ITEM 9.
- [SDR SWAA2026061706551](https://openairdocs.org/sdr/SWAA2026061706551), May 26, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLE ACCESS PANEL 661BB AT RT WING. REPAIRED THE ACCESS PANEL 661BB AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026061706765](https://openairdocs.org/sdr/SWAA2026061706765), May 26, 2026: SCUFF PLATE. CRACKED. CRACKED AFT CORNER SCUFF PLATE LOCATED AFT CARGO COMPARTMENT. REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 
- [SDR SWAA2026061706766](https://openairdocs.org/sdr/SWAA2026061706766), May 26, 2026: SCUFF PLATE. CRACKED. CRACKED CENTER SCUFF PLATE LOCATED AFT CARGO COMPARTMENT. REPAIRED CENTER SCUFF PLATE LOCATED AFT CARGO COMPARTMENT IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 597
- [SDR SWAA2026061706552](https://openairdocs.org/sdr/SWAA2026061706552), May 26, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLE ON ACCESS PANEL 661CB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661CB TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026061706548](https://openairdocs.org/sdr/SWAA2026061706548), May 26, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLE ACCESS PANEL 561AB AT LT WING. REPAIRED THE ACCESS PANEL 561AB AT LT WING IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026061706550](https://openairdocs.org/sdr/SWAA2026061706550), May 26, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLE ACCESS PANEL 561BB AT LT WING. REPAIRED THE ACCESS PANEL 561BB AT LT WING IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026061706219](https://openairdocs.org/sdr/SWAA2026061706219), May 24, 2026: SKIN. CRACKED. CRACK AROUND FASTENER LOWER SURFACE LEADING EDGE SLAT NOSE SKIN AT THE ACTUATOR FITTING SLAT 7 AT RT WING. REPLACED SLAT NR 7 DUE TO SEVERAL CRACKS DAMAGE AT LO
- [SDR SWAA2026061706218](https://openairdocs.org/sdr/SWAA2026061706218), May 24, 2026: SKIN. CRACKED. CRACK LOWER SURFACE OF LEADING EDGE SLAT 1 NOSE SKIN AT ACTUATOR LOC. AROUND FASTENER AT LT WING. REPLACED SLAT NR 1 DUE TO WAS FOUND SEVERAL CRACKS DAMAGE. FOR
- [SDR SWAA2025121242831](https://openairdocs.org/sdr/SWAA2025121242831), Dec 5, 2025: TAIL CONE. DELAMINATED. THE FORWARD TAIL CONE FAIRING IS DELAMINATED WITH DAMAGE TO THE FACE SHEETS WITH FIBERS AND HONEYCOMB EXPOSED AND CONTAMINATED WITH HYDRAULIC FLUID. LOCATED BS 
- [SDR SWAA2025121242832](https://openairdocs.org/sdr/SWAA2025121242832), Dec 5, 2025: TAIL CONE. DELAMINATED. THE FORWARD TAIL CONE FAIRING IS DELAMINATED WITH DAMAGE TO THE FACE SHEETS WITH FIBERS AND HONEYCOMB EXPOSED AND CONTAMINATED WITH HYDRAULIC FLUID. BS 1193.5; 
- [SDR SWAA2025121246031](https://openairdocs.org/sdr/SWAA2025121246031), Dec 5, 2025: TAIL CONE. DELAMINATED. THE FORWARD TAIL CONE FAIRING IS DELAMINATED WITH DAMAGE TO THE FACE SHEETS WITH FIBERS AND HONEYCOMB EXPOSED AND CONTAMINATED WITH HYDRAULIC FLUID. LOCATED BS 
- [SDR SWAA2025121246032](https://openairdocs.org/sdr/SWAA2025121246032), Dec 5, 2025: TAIL CONE. DELAMINATED. THE FORWARD TAIL CONE FAIRING IS DELAMINATED WITH DAMAGE TO THE FACE SHEETS WITH FIBERS AND HONEYCOMB EXPOSED AND CONTAMINATED WITH HYDRAULIC FLUID, BS 1193.5; 
- [SDR SWAA2025121242833](https://openairdocs.org/sdr/SWAA2025121242833), Dec 5, 2025: TAIL CONE. DELAMINATED. THE FORWARD TAIL CONE FAIRING IS DELAMINATED, BS 1190 21 INCHES RIGHT OF TOP. CRACK LENGTH: L=2.3' W=2.2'. LOCATED & DRILLED INITIAL TAIL CONE SCREW HOLES WITH 
- [SDR SWAA2025091213803](https://openairdocs.org/sdr/SWAA2025091213803), Sep 11, 2025: LENS. LOOSE. OVERHEAD EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS PER AMM 33-51-01.
- [SDR SWAA2025042125797](https://openairdocs.org/sdr/SWAA2025042125797), Apr 16, 2025: SIGN. DETACHED. MID CABIN OVERHEAD EXIT SIGN FELL OFF. SECURED SIGN AS PER SIP
- [SDR SWAA2025030601774](https://openairdocs.org/sdr/SWAA2025030601774), Mar 4, 2025: SEAL. CRACKED. R/H HORIZONTAL UPPER SLIDER CRACKED<[01] REF ADDED;[02] REMOVED AND REPLACED PER 53-31-31.
- [SDR SWAA2025030601773](https://openairdocs.org/sdr/SWAA2025030601773), Mar 4, 2025: SEAL. CRACKED. L/H HORIZONTAL UPPER SLIDER CRACKED<[01] REF ADDED;[02] REMOVED AND REPLACED PER 53-31-31.
- [SDR SWAA2025012489193](https://openairdocs.org/sdr/SWAA2025012489193), Jan 23, 2025: HANDLE. BROKEN. AFT ENTRY DOOR ASSIST HANDLE BROKEN<[01] ROBBED ASSIST HANDLE FROM FWD LAV AND INSTALLED ON AFT LEFT ENTRY DOOR IAW AMM 52-13-31. FWD LAV ASSIST HANDLE INOP. OK
- [SDR SWAA2025012288475](https://openairdocs.org/sdr/SWAA2025012288475), Jan 22, 2025: HANDLE. BROKEN. AFT ENTRY DOOR ASSIST HANDLE BROKEN<[01] ROBBED ASSIST HANDLE FROM AFT LAV AND INSTALLED ON AFT ENTRY DOOR IAW AMM 52-13-31. AFT LAV ASSIST HANDLE INOP. OK TO C
- [SDR SWAA2024080713755](https://openairdocs.org/sdr/SWAA2024080713755), Jul 18, 2024: SEAT TRACK. CRACKED. CRACK INDICATION ON FLOOR STRUCTURE SEAT TRACK AT BS 727 AND AT LBL 45.5 HOLE POSITION B 2024-405210 CRACK INDICATION ON FLOOR STRUCTURE SEAT TRACK AT BS 727B A
- [SDR SWAA2024080709054](https://openairdocs.org/sdr/SWAA2024080709054), Jul 4, 2024: ACCESS PANEL. CRACKED. CRACK LEADING EDGE RIB ACCESS PANEL 331B LOCATED LE STA198.23 LT HORIZONTAL STAB 2024-405175<[01] REPLACED RIB LOC ON LEADING EDGE STA198.23 ACCESS PANEL 331B H
- [SDR SWAA2024080709053](https://openairdocs.org/sdr/SWAA2024080709053), Jul 4, 2024: RIB. CRACKED. CRACK LEADING EDGE RIB ACCESS PANEL 331B LOCATED LE STA188.94 LT HORIZONTAL STAB 2024-405174<[01] REPLACED NEW RIB 188.94 AND FASTENERS LOCATED ON LEADING EDGE 
- [SDR SWAA2024080821406](https://openairdocs.org/sdr/SWAA2024080821406), Jul 2, 2024: UNKNOWN. UNKNOWN. THICKNESS MEASUREMENT OF GAP BETWEEN INNER CHORD AND WEB S-18A BS 727 RIGHT SIDE IS 0.024 INCH 2024-405139<[01] FAULT RESOLVED ON OTHER FAULT TTG8Q00UBC80;[02] 
- [SDR SWAA2024080821405](https://openairdocs.org/sdr/SWAA2024080821405), Jul 2, 2024: UNKNOWN. UNKNOWN. THICKNESS MEASUREMENT OF GAP BETWEEN INNER CHORD AND WEB S-18A BS 727 LEFT SIDE IS 0.037 INCH 2024-405138<[01] FAULT RESOLVED ON OTHER FAULT TTG8Q00UBC7V;[02] F
- [SDR SWAA2024080707754](https://openairdocs.org/sdr/SWAA2024080707754), Jul 1, 2024: FRAME. CRACKED. CRACK ON FRAME WEB LOCATED BS259.5 BTW STR8L AND STR9L AT PASSENGER CABIN 2024-405134<[01] EQUIPMENT USED P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 08-JAN-25;
- [SDR SWAA2024080719012](https://openairdocs.org/sdr/SWAA2024080719012), Jun 29, 2024: STRINGER. CRACKED. CRACK STRINGER 8 INTERNAL AREA FUEL TANK UPPER POSITION LOC. BTW RIB 19 AND RIB 20 AT LT WING 2024-405124<[01] PERFORMED REPAIR CATEGORY A ON STRINGER 8 INTERNA
- [SDR SWAA2024080706185](https://openairdocs.org/sdr/SWAA2024080706185), Jun 27, 2024: BOLT. WORN. WEAR ON GIRT BAR FITTING BOLT FWD POSITION AT AFT GALLEY AREA (2 EA) 2024-405056<[01] REPLACED GIRT BAR FITTING BOLT FWD POSITION ENTRY DOOR AT AFT GALLEY AREA 
- [SDR SWAA2024080706183](https://openairdocs.org/sdr/SWAA2024080706183), Jun 27, 2024: BOLT. WORN. WEAR ON GIRT BAR FITTING BOLT FWD POSITION AT AFT GALLEY AREA (2 EA) 2024-405217<[01] FAULT WILL RESOLVED ON ANOTHER FAULT DUE TO DUPLICATED DISCREPANCY REPORT.
- [SDR SWAA2024080705917](https://openairdocs.org/sdr/SWAA2024080705917), Jun 26, 2024: STRINGER. CRACKED. CRACK STRINGER 26L LOCATED BS540 AT FWD CARGO COMPARTMENT 2024-405036<[01] TOOL USED ULTRASONIC THICKNESS EQUIPMENT PN:45MG; SN:430063701; DUE DATE:24-JUL-24.;[
- [SDR SWAA2024080705918](https://openairdocs.org/sdr/SWAA2024080705918), Jun 26, 2024: STRINGER. CRACKED. CRACK STRINGER 24L LOCATED BS540 FWD CARGO COMPARTMENT 2024-405037 CRACK STRINGER 24L LOCATED BS540 FWD CARGO COMPARTMENT<[01] STEP 2. ULTRASONIC EQUIPMENT USED
- [SDR SWAA2024080705916](https://openairdocs.org/sdr/SWAA2024080705916), Jun 26, 2024: INTERCOSTAL. CRACKED. CRACK WEB - INTERCOSTAL LOCATED BS500D TO BS520 AND S-28R FWD CARGO COMPARTMENT 2024-405034<[01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142
- [SDR SWAA2024080705915](https://openairdocs.org/sdr/SWAA2024080705915), Jun 26, 2024: INTERCOSTAL. CRACKED. CRACK WEB - INTERCOSTAL LOCATED BS 500D TO BS 520 AND S-28L FWD CARGO COMPARTMENT 2024-405035<[01] REPLACED WEB - INTERCOSTAL LOCATED BS 500D TO BS 520 AND S-28
- [SDR SWAA2024080705556](https://openairdocs.org/sdr/SWAA2024080705556), Jun 25, 2024: FRAME. CRACKED. CRACK FRAME WEB LOCATED STA259.5 AND BETWEEN STR8R TO STR9R AT FWD GALLEY AREA 2024-405014<[01] TOOL USED STEP 5 EDDY CURRENT EQUIPMENT. PN: NORTEC 600D; SN:210
- [SDR SWAA2024080705558](https://openairdocs.org/sdr/SWAA2024080705558), Jun 25, 2024: STRINGER. CRACKED. CRACK STRINGER 7L LOCATED BETWEEN STA303.9 TO STA294.5 AT PASSENGER CABIN 2024-405020<[01] STEP 7 TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 20005340
- [SDR SWAA2024080705555](https://openairdocs.org/sdr/SWAA2024080705555), Jun 25, 2024: SUPPORT. ELONGATED. ELONGATED HOLE SUPPORT ZEE LOCATED BS 887 TO BS 907 AND S-25R AT AFT CARGO COMPARTMENT 2024-405009<[01] REJECTION MISSING FASTENERS SUPPORT ZEE AND RIVET BTW ST

All 301: https://openairdocs.org/aircraft/N482WN/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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