# N469WN: 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: 33859 - Year built: 2004 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 22, 2004 - Certificate issued: July 29, 2004 - Expires: October 31, 2027 - Mode S code: A5BD0B - 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=469WN - Page: https://openairdocs.org/aircraft/N469WN 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/N469WN/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 CEN12IA123](https://openairdocs.org/ntsb/CEN12IA123), Dec 22, 2011: Boeing 737-7H4 (N469WN), Denver, CO, incident, minor damage. Probable cause: The snowplow operator’s incapacitation due to fatigue, which resulted in the snowplow contacting a parked airplane. Contributing to the incident was the company’s lack of a policy regarding employee… ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20111222029509I](https://openairdocs.org/incident/20111222029509I), Dec 22, 2011: Boeing 737-7H4 (N469WN), Denver, CO, Minor damage. On December 22, 2011 at approximately 1435 local time swaa aircraft N469WN was struck by a snow plow while parked at gate C29 at den. Weather conditions were… ## Service difficulty reports (319, 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 SWAA2026072827805](https://openairdocs.org/sdr/SWAA2026072827805), Jul 25, 2026: SIGN. DETACHED. OVERHEAD AISLE EXIT SIGN BROKEN AND HANGING_ REPLACED OVERHEAD EXIT SIGN ASSY. IAW AMM 33-51-01 OPS CHECKS GOOD - [SDR SWAA2026010557389](https://openairdocs.org/sdr/SWAA2026010557389), Dec 31, 2025: BATTERY. INOPERATIVE. FWD MEGAPHONE INOPERATIVE. REMOVED AND REPLACED FWD MEGAPHONE BATTERIES IAW AMM 25-64-00 - [SDR SWAA2025122343445](https://openairdocs.org/sdr/SWAA2025122343445), Dec 6, 2025: ACCESS PANEL. CRACKED. CRACK LEADING EDGE RIB ACCESS PANEL 331B LOCATED LE HSS 105.26, LT HORIZONTAL STAB. REPLACED RIB LEADING EDGE ACCESS PANEL 331B IAW SRM 51-40-02, AND DWG 186A10 - [SDR SWAA2025122343212](https://openairdocs.org/sdr/SWAA2025122343212), Dec 5, 2025: ANGLE. CRACKED. CRACKED ANGLE REAR SPAR AREA AT IRSS 140 UPPER POSITION AT LT WING. REPLACED ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 115A2000, SHEET 21, REV -. - [SDR SWAA2025122352792](https://openairdocs.org/sdr/SWAA2025122352792), Dec 5, 2025: FRAME. WRONG PART. BS 328 FRAME STRAP FROM S20 - 22R, DOES NOT MATCH WITH CONFIGURATION TASK 5311-I-17336-NG, FIGURE 15 2025-740400. REPAIRED THE FRAME IAW EA 25-153-03344-WIP1. - [SDR SWAA2025122348656](https://openairdocs.org/sdr/SWAA2025122348656), Dec 5, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 561BB LT WING T/E. REPAIRED ACCESS PANEL 561BB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-10, REPAIR 10. - [SDR SWAA2025122343214](https://openairdocs.org/sdr/SWAA2025122343214), Dec 5, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE OF ACCESS PANEL 651FB RT WING T/E. REPLACED THE SUPPORT ANGLE LOCATED AT ACCESS PANEL 651FB IAW SRM 51-10-02, ITEM 9, AND DWG 115A2710, S - [SDR SWAA2025122343327](https://openairdocs.org/sdr/SWAA2025122343327), Dec 5, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 561BB TRAILING EDGE ON LT WING. - [SDR SWAA2025122348650](https://openairdocs.org/sdr/SWAA2025122348650), Dec 4, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLE ON ACCESS PANEL 661AB, RT WING T/E. REPAIRED ACCESS PANEL 661AB IAW SRM 51-70-04-2R-10, REPAIR 10. - [SDR SWAA2025122348651](https://openairdocs.org/sdr/SWAA2025122348651), Dec 4, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLE ACCESS PANEL 661BB, RT WING. REPAIRED THE ACCESS PANEL 661BB IAW SRM 51-70-04-2R-10, REPAIR 10. - [SDR SWAA2025122348654](https://openairdocs.org/sdr/SWAA2025122348654), Dec 4, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLE ON ACCESS PANEL 661CB RT WING T/E. REPAIRED THE ACCESS PANEL 661CB IAW SRM 51-70-04-2R-10, REPAIR 10. - [SDR SWAA2025122342975](https://openairdocs.org/sdr/SWAA2025122342975), Dec 4, 2025: ANGLE. CRACKED. CRACK ON ANGLE LOCATED AL LEVEL ORSS 271 DEFLECTION CONTROL RIB AREA AT LT WING. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, AND DWG 115A2930, SHEET 7, REV -. - [SDR SWAA2025122342976](https://openairdocs.org/sdr/SWAA2025122342976), Dec 4, 2025: ANGLE. CRACKED. CRACK ON ANGLE LOCATED AT LEVEL ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING. REPLACED THE ANGLE IAW SRM 51-40-02, AND SRM 51-10-02, ITEM 9. - [SDR SWAA2025122342977](https://openairdocs.org/sdr/SWAA2025122342977), Dec 4, 2025: ANGLE. CRACKED. CRACK ON ANGLE LOCATED AT LEVEL ORSS 272 DEFLECTION CONTROL RIB AREA RT WING T/E. REPLACED THE ANGLE IAW SRM 51-40-02, AND SRM 51-10-02, ITEM 9. - [SDR SWAA2025122342980](https://openairdocs.org/sdr/SWAA2025122342980), Dec 4, 2025: ANGLE. CRACKED. CRACK ON ANGLE LOCATED AT LEVEL ORSS 272 DEFLECTION CONTROL RIB AREA LT WING T/E. REPLACED THE ANGLE IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9. - [SDR SWAA2025122342979](https://openairdocs.org/sdr/SWAA2025122342979), Dec 4, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLE ON ACCESS PANEL 661AB TRAILING EDGE ON RT WING. - [SDR SWAA2025122342981](https://openairdocs.org/sdr/SWAA2025122342981), Dec 4, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLE ACCESS PANEL 661BB ON RT WING. - [SDR SWAA2025122342989](https://openairdocs.org/sdr/SWAA2025122342989), Dec 4, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLE ON ACCESS PANEL 661CB TRAILING EDGE ON RT WING. - [SDR SWAA2025122342970](https://openairdocs.org/sdr/SWAA2025122342970), Dec 4, 2025: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, LOCATED BS 807, RBL 21, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, AND DWG 146A0081, SHEET 25, REV A. - [SDR SWAA2025122342534](https://openairdocs.org/sdr/SWAA2025122342534), Dec 3, 2025: BEAM. CRACKED. CRACK INDICATION ON RADIUS OF FORWARD SERVICE DOOR BEAM NR 4. LENGTH OF CRACK: 0.200 INCH. EO 5241-C-14093 OR 5241-C-14344 WILL BE ADDED TO REPAIR ORDER FOR REP - [SDR SWAA2025122342533](https://openairdocs.org/sdr/SWAA2025122342533), Dec 3, 2025: LIGHT. DETERIORATED. DETERIORATED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10EA). REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10EA) IAW AMM 33-51-15-400-802. - [SDR SWAA2025122348649](https://openairdocs.org/sdr/SWAA2025122348649), Dec 3, 2025: BEAM. CRACKED. CRACK INDICATION ON RADIUS OF FORWARD SERVICE DOOR BEAM NR 4. LENGTH OF CRACK: 0.200 INCH. EO 5241-C-14093 OR 5241-C-14344 WILL BE ADDED TO REPAIR ORDER FOR REP - [SDR SWAA2025122342090](https://openairdocs.org/sdr/SWAA2025122342090), Dec 2, 2025: PRESSURE DECK. CRACKED. CRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB AT LBL 31 BETWEEN BS 663 - 675 IN THE MAIN WHEEL WELL. CRACK LENGTH: 0.186 INCH. REPAIRED HORIZONTAL PRES - [SDR SWAA2025122342072](https://openairdocs.org/sdr/SWAA2025122342072), Dec 2, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BS 695 LBL 24.75 WE 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE LOCATED BS 695 LBL 24.75 WL 208.1 AT PASSENGER CABIN IAW SRM - [SDR SWAA2025122341392](https://openairdocs.org/sdr/SWAA2025122341392), Dec 1, 2025: SCUFF PLATE. CRACKED. CRACKED AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT. REPAIRED AFT CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, AND BAC 5975. - [SDR SWAA2025122341393](https://openairdocs.org/sdr/SWAA2025122341393), Dec 1, 2025: SCUFF PLATE. CRACKED. CRACKED FWD CORNER SCUFF PLATE AT FWD CARGO BAY. REPAIRED FWD CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, AND BAC 5975. - [SDR SWAA2025122348643](https://openairdocs.org/sdr/SWAA2025122348643), Nov 30, 2025: SKIN. CRACKED. CRACKED LOWER SURFACE OF LEADING EDGE SLAT NR 8 NOSE SKIN AT ACTUATOR LOCATION AROUND FASTENER AT RT WING. REPAIRED LOWER SURFACE OF LEADING EDGE SLAT 8 NOSE SK - [SDR SWAA2025122341247](https://openairdocs.org/sdr/SWAA2025122341247), Nov 30, 2025: SKIN. CRACKED. CRACKED LOWER SURFACE OF LEADING EDGE SLAT NR 2 NOSE SKIN AT ACTUATOR LOCATION AROUND FASTENER AT LT WING. REPLACED LEADING EDGE SLAT 2 AND PERFORMED ADJUSTMENT - [SDR SWAA2025122348644](https://openairdocs.org/sdr/SWAA2025122348644), Nov 30, 2025: SKIN. CRACKED. CRACKED LOWER SURFACE OF LEADING EDGE SLAT NR 1 NOSE SKIN AT THE ACTUATOR LOCATION, AROUND FASTENER AT LT WING. REPAIRED LOWER SURFACE OF LEADING EDGE SLAT 1 NO - [SDR SWAA2025122341248](https://openairdocs.org/sdr/SWAA2025122341248), Nov 30, 2025: SKIN. CRACKED. CRACKED LOWER SURFACE OF LEADING EDGE SLAT NR 1 NOSE SKIN AT ACTUATOR LOCATION. AROUND FASTENER AT LT WING. - [SDR SWAA2025122341244](https://openairdocs.org/sdr/SWAA2025122341244), Nov 30, 2025: SKIN. CRACKED. CRACK LOWER SURFACE OF LEADING EDGE SLAT NR 8 NOSE SKIN AT ACTUATOR LOCATION. AROUND FASTENER AT RT WING. - [SDR SWAA2025092316985](https://openairdocs.org/sdr/SWAA2025092316985), Sep 21, 2025: SLIDE. UNSECURE. L2 SLIDE DRAGGING. SECURED LOOSE SLIDE MATERIAL PER AMM 25-66-00. - [SDR SWAA2025081404392](https://openairdocs.org/sdr/SWAA2025081404392), Aug 14, 2025: LAMP. INOPERATIVE. R2 DOOR EMERGENCY LIGHT INOP. RELAMPED R2 DOOR EMERGENCY LIGHT BULB IAW AMM 33-51-04. OPS CHECK GOOD. - [SDR SWAA2025081404032](https://openairdocs.org/sdr/SWAA2025081404032), Aug 13, 2025: SEAT BACK. OUT OF ADJUST. SEAT ROW 12DEF WILL NOT STAY UPRIGHT<[01] TIGHTENED ALL SEATS IN ROW 12 DEF AS PER AMM 25-22-00 - [SDR SWAA2025051268786](https://openairdocs.org/sdr/SWAA2025051268786), May 8, 2025: BATTERY PACK. FAULTED. REF PREVIOUS LOG PAGE LP 2937321 C/B LIGHTING EMERGENCY CHGR RF P18-3 B10 POPPED<[01] FOUND EMERGENCY EXIT LIGHT BATTERY PACK POPPING THE C/B (M1672) REF LP 293 - [SDR SWAA2025051268722](https://openairdocs.org/sdr/SWAA2025051268722), May 8, 2025: CHARGER. TRIPPED. C/B LIGHTING EMERGENCY CHGR RF P18-3 B10 POPPED<[01] R+R?D R/H AFT BATTERY CHARGER (M1672) AND BATTERY PACK IAW AMM 31-51-06. EMERGENCY LIGHTS OPS CHK GOOD ALL - [SDR SWAA2024120473938](https://openairdocs.org/sdr/SWAA2024120473938), Dec 3, 2024: LATCH. LOOSE. FWD MAIN ENTRY DOOR SLIDE LATCH ASSY CAME LOOSE.<[01] RESECURED FWD ENTRY DOOR SLIDE LATCH IAW TASK 725-61-06 AC OK FOR SERVICE - [SDR SWAA2024052186890](https://openairdocs.org/sdr/SWAA2024052186890), May 17, 2024: SLIDE. OUT OF ADJUST. FWD SERVICE DOOR SLIDE HANGS DOWN TO LOW<[01] REMOVED AND REPACKED SLIDE GIRT BAR REF MT725-61-06 - [SDR SWAA2024022956834](https://openairdocs.org/sdr/SWAA2024022956834), Feb 27, 2024: LENS. DETACHED. SEAT 9C EMER LIGHT COVER FELL OFF<[01] OK TO CONTINUE PER MEL 33-15-02. SP1;[02] R&R?D LENS PER AMM 33-51-03 - [SDR SWAA2024013045741](https://openairdocs.org/sdr/SWAA2024013045741), Jan 28, 2024: SLIDE. OUT OF ADJUST. AFT ENTRY DOOR ESCAPE SLIDE SKIRT CONTACTS THRESHOLD; UNABLE TO CLOSE DOOR PROPERLY.<[01] RE-TUCKED AED ESCAPE SLIDE Z-FOLD INTO SLIDE PACK IAW AMM INTRODUCTION - [SDR SWAA2024013042679](https://openairdocs.org/sdr/SWAA2024013042679), Jan 18, 2024: SUPPORT. CRACKED. FWD L/H FAIRING SUPPORT FOR PANEL 192E IS CRACKED<[01] REMOVED AND REPLACED SUPPORT BRACKET P/N 149A7712-41 PER SRM 51-40-02 AND DWG 149A7701;[02] VERIFIED MEAS - [SDR SWAA2024013136869](https://openairdocs.org/sdr/SWAA2024013136869), Jan 1, 2024: SEAL. CRACKED. LT. HORIZONTAL STAB UPPER FORWARD SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED LT HORIZONTAL STAB UPPER FORWARD SLIDE SEAL IAW AMM 53-31-31-000-802 AND AMM 53- - [SDR SWAA2024013135889](https://openairdocs.org/sdr/SWAA2024013135889), Dec 28, 2023: ATTACH FITTING. CRACKED. ACB AFT BULKHEAD ATTACH FITTING CRACKED BS947 LBL10 WL180.<[01] REMOVED AND REPLACED FITTING WITH P/N 149A8113-6 LOT. 1510339-2. LOCATED AT BS947 LBL10 WL180. I - [SDR SWAA2024013035893](https://openairdocs.org/sdr/SWAA2024013035893), Dec 28, 2023: ATTACH ANGLE. CRACKED. ACB WASTE COMPARTMENT BULKHEAD ATTACH ANGLE CRACKED BS867 LBL11 WL167.<[01] REMOVED AND REPLACED SUPPORT BRACKET WITH P/N 149A8109-114 LOT 1540507-1 LOCATED AT - [SDR SWAA2024013035735](https://openairdocs.org/sdr/SWAA2024013035735), Dec 28, 2023: SUPPORT BRACKET. CRACKED. CRACKED PNEUMATIC-DUCT SUPPORT BRACKET AT STA 540+4 LBL 6; WL 163.<[01] REMOVED AND REPLACED PNEUMATIC-DUCT SUPPORT BRACKET P/N 212A1116-1 LOT:1549921-1 IAW SRM - [SDR SWAA2024013035885](https://openairdocs.org/sdr/SWAA2024013035885), Dec 28, 2023: SIDEWALL SUPPORT. CORRODED. CORROSION AT ACB ON FLOOR TO SIDEWALL SUPPORT BS727A - BS767 RBL21 WL156.<[01] REMOVED AND REPLACED NEW FLOOR TO SIDEWALL ON ACB BS727 - BS767 RBL21 WL156. IAW - [SDR SWAA2024013035891](https://openairdocs.org/sdr/SWAA2024013035891), Dec 28, 2023: SIDEWALL SUPPORT. CORRODED. CORROSION AT ACB ON FLOOR TO SIDEWALL SUPPORT BS727 - BS807 LBL21 WL156.<[01] REMOVED AND REPLACED AFT CARGO FLOOR TO SIDEWALL SUPPORT
FROM BS 727 TO BS 847 - [SDR SWAA2024013035887](https://openairdocs.org/sdr/SWAA2024013035887), Dec 28, 2023: SHIELD. CORRODED. CORROSION ON FWD SHIELD AT ACB BS767 - BS787 RBL21 WL157.<[01] REMOVED AND REPLACED ACB FWD. SHIELD. IAW SRM 51-40-02 AND DWG # 146A0081 - [SDR SWAA2024013035892](https://openairdocs.org/sdr/SWAA2024013035892), Dec 28, 2023: WEB. CORRODED. CORROSION ON WEB AT ACB BS787+4 RBL19 WL157.<[01] REMOVED AND REPLACED WEB INTERCOSTAL P/N 146A8123-22 LOT. 1551095-1. LOCATE BS.787 - 794 RBL 19 WL 158 PER SRM - [SDR SWAA2024013035127](https://openairdocs.org/sdr/SWAA2024013035127), Dec 23, 2023: SUPPORT BRACKET. CRACKED. FWD CARGO BAY BS500C; L/H FLOOR TO SIDEWALL SUPPORT BRACKET AFT SIDE; CRACKED. (MARKED)<[01] REMOVED AND REPLACED LH FLOOR TO SIDEWALL SUPPORT BRACKET AFT SIDE All 319: https://openairdocs.org/aircraft/N469WN/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.