# N495WN: 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: 33869 - Year built: 2004 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 22, 2004 - Certificate issued: January 24, 2005 - Expires: June 30, 2029 - Mode S code: A624AC - 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=495WN - Page: https://openairdocs.org/aircraft/N495WN 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/N495WN/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 N495WN. ## 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; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20051125032509I](https://openairdocs.org/incident/20051125032509I), Nov 25, 2005: Boeing 7377H4 (N495WN), Buffalo, NY, Minor damage. (-23) On November 26, 2005 at approximately 2030 hours, while powering up to turn out from the gate area after being pushed back, a southwest airlines B-737,… ## Service difficulty reports (316, newest 50) As reported by operators and repair stations. - [SDR SWAA2026083189724](https://openairdocs.org/sdr/SWAA2026083189724), Aug 28, 2026: EXHAUST DUCT. FIRE. NR 1 ENG. TAIL PIPE FIRE REPORTED BY ANOTHER AIRCRAFT. EXTINGUISHED AFTER ENGINE SHUTDOWN. FLAMES FOUND TO BE CANDLE FIRE PHENOMENA IN THE EXHAUST PLUG. C/W INS - [SDR SWAA2026080328107](https://openairdocs.org/sdr/SWAA2026080328107), Jul 31, 2026: BOLT. LOOSE. FWD ENTRY DOOR ASSIST HANDLE WAS LOOSE. TIGHTENED BOLTS ON FED ASSIST HANDLE IAW AMM 52-11-31-400-802, STEP 3.G. (2). - [SDR SWAA2026080375433](https://openairdocs.org/sdr/SWAA2026080375433), Jul 21, 2026: LIGHT. INOPERATIVE. EMERGENCY LIGHT ON BIN AT ROW 7 - 8 DEF INOPERATIVE. REMOVED & REPLACED EMERGENCY LIGHT ON BIN AT ROW 7 - 8 DEF AND PERFORMED GOOD OPS TEST IAW AMM 33-51-03-960 - [SDR SWAA2026080390865](https://openairdocs.org/sdr/SWAA2026080390865), Jul 21, 2026: LAMP. BURNED OUT. RIGHT OVERWING LOWER EMERGENCY EXIT SIGN HAS BURNED OUT BULBS. R & R RT OVERWING LOWER EMERGENCY SIGN LAMPS IAW AMM 33-51-01-960-801. - [SDR SWAA2026080433329](https://openairdocs.org/sdr/SWAA2026080433329), Jul 20, 2026: STIFFENER. CORRODED. CORROSION FOUND ON LT L/E STIFFNER COMMON TO NR 4 TAI DUCT TAB AT OFSS 308 SS 73. REMOVED LT L/E STIFFNER COMMON TO NR 4 TAI DUCT TAB AT OFSS 308 SS 73 IAW SRM - [SDR SWAA2026080486563](https://openairdocs.org/sdr/SWAA2026080486563), Jul 20, 2026: STIFFENER. CORRODED. CORROSION WAS FOUND ON STIFFNER COMMON TO NR 6 TAI DUCT TAB AT OFSS 421 SS 186 [MARKED] REMOVED AND REPLACED STIFFNER COMMON TO NR 6 TAI DUCT TAB AT OFSS 421 SS - [SDR SWAA2026080371392](https://openairdocs.org/sdr/SWAA2026080371392), Jul 16, 2026: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP, BS 727A, S7L. REMOVED, FABRICATED, AND INSTALLED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, AND DWG 146A1101, SHEET 15, REV -. - [SDR SWAA2026080369769](https://openairdocs.org/sdr/SWAA2026080369769), Jul 16, 2026: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP, BS 727A, S6L. REMOVED, FABRICATED, AND INSTALLED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, AND DWG 146A1101, SHEET 15, REV -. - [SDR SWAA2026080388192](https://openairdocs.org/sdr/SWAA2026080388192), Jul 16, 2026: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP, BS 727B, S7L. REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, AND DWG 146A1102, SHEET 15, REV -. - [SDR SWAA2026080393981](https://openairdocs.org/sdr/SWAA2026080393981), Jul 16, 2026: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP AT BS 727E, S3L. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02, AND DOCUMENT NR 146A1112, DWG 0009, REV-. - [SDR SWAA2026080328655](https://openairdocs.org/sdr/SWAA2026080328655), Jul 16, 2026: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP AT PAX CABIN, BS 727B, S6L. REMOVED, FABRICATED, AND INSTALLED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, AND DWG 146A1102, SHEET 15, REV -. - [SDR SWAA2026080388797](https://openairdocs.org/sdr/SWAA2026080388797), Jul 16, 2026: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP AT BS 727E, S4L. REMOVED, FABRICATED, AND INSTALLED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, AND DWG 146A1112, SHEET 09, REV -. - [SDR SWAA2026080388195](https://openairdocs.org/sdr/SWAA2026080388195), Jul 16, 2026: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP, BS 727E, S5L. REMOVED, FABRICATED, AND INSTALLED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, & DWG 146A1112, SHEET 09, REV -. - [SDR SWAA2026080414529](https://openairdocs.org/sdr/SWAA2026080414529), Jul 14, 2026: STRAP. OUT OF TOLERANCE. E/E COMPARTMENT, BS 328 BETWEEN S20R TO S22R, FRAME STRAP CONFIGURATION DOES NOT MATCH FIG. 15 PER EO 5311-I-17336-NG REF FAULT TTG8Q0157B6V AS PER EA 26-153-01 - [SDR SWAA2026061111332](https://openairdocs.org/sdr/SWAA2026061111332), Jun 11, 2026: TAILPIPE. FIRE. TAILPIPE FIRE REPORTED BY SEVERAL AIRCRAFT IN THE LEFT ENGINE WITH FLAMES VISIBLE, WHEN ENGINE WAS SHUTDOWN FLAMES DISAPPEARED BUT SMOKE STILL VISIBLE REPORTED - [SDR SWAA2026051803655](https://openairdocs.org/sdr/SWAA2026051803655), May 15, 2026: SCREW. LOOSE. CREW REPORT L1 DOOR ESCAPE SLIDE MOUNT SCREW LOOSE. SECURED L1 DOOR ESCAPE SLIDE MOUNT SCREW IAW MT 725-61-06. - [SDR SWAA2026033082539](https://openairdocs.org/sdr/SWAA2026033082539), Mar 24, 2026: BATTERY PACK. FAILED. FWD GALLEY EMERGENCY BATTERY PACK RT M1674 FAILED CAPACITY CHECK. R&R CABIN EMERGENCY BATTERY PACK AT M1674 PER AMM 33-51-06;[02] C/W INSPECTION - [SDR SWAA2026032380559](https://openairdocs.org/sdr/SWAA2026032380559), Mar 17, 2026: COALESCER BAG. ODOR. FLIGHT CREW SMELLED SMOKE IN THE COCKPIT AND FLIGHT ATTENDANTS SMELLED SMOKE IN THE CABIN. PERFORMED CONDITIONAL INSPECTION REMOVED AND REPLACED LEFT AND RIGHT - [SDR SWAA2026032380623](https://openairdocs.org/sdr/SWAA2026032380623), Mar 17, 2026: FILTER. ODOR. FLIGHT CREW SMELLED SMOKE IN THE COCKPIT AND FLIGHT ATTENDANTS SMELLED SMOKE IN THE CABIN. PERFORMED CONDITIONAL INSPECTION REMOVED AND REPLACED LEFT AND RIGHT - [SDR SWAA2026032080287](https://openairdocs.org/sdr/SWAA2026032080287), Mar 16, 2026: COMPUTER. INOPERATIVE. ENGINES WOULD NOT MAKE MAX POWER WITH AUTOTHROTTLE ENGAGE. PERFORMED AUTOTHROTTLE SYSTEM OPERATIONAL TEST IAW AMM 22-31-00. OPS CHECKS GOOD. NO FURTHER FAULTS N - [SDR SWAA2026032081730](https://openairdocs.org/sdr/SWAA2026032081730), Mar 16, 2026: SERVO. INOPERATIVE. ENGINES WOULD NOT MAKE MAX POWER WITH AUTOTHROTTLE ENGAGE. - [SDR SWAA2025030400992](https://openairdocs.org/sdr/SWAA2025030400992), Mar 1, 2025: LAMP. INOPERATIVE. LH MAIN SERVICE DOOR SLIDE EMERGENCY LIGHT INOP<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-04-960-801-NG (LH MAIN SERVICE DOOR SLIDE EMERGENCY LIGHT - LAMP R - [SDR SWAA2024112670914](https://openairdocs.org/sdr/SWAA2024112670914), Nov 22, 2024: LIGHT. LOOSE. SIDE WALL OVERWING EXIT SIGN (FO SIDE) FELL OFF DURING DEPLANING.<[01] REATT. SIDEWALL OVERWING EXIT LIGHT REF. S.I.P. - [SDR SWAA2024093041425](https://openairdocs.org/sdr/SWAA2024093041425), Sep 25, 2024: PLATE. DAMAGED. LH WING UPPER FIXED TRAILING EDGE WIGGLE PANEL COMMON TO 551CT; MOUNT TAB HOLES ELONGATED AND PULLED THRU.<[01] CW NDT INSPECTION OF CUTOUT REF NDT 51-00-00 PRO - [SDR SWAA2024092741368](https://openairdocs.org/sdr/SWAA2024092741368), Sep 25, 2024: STRAP. DAMAGED. FWD SERVICE DOOR SAFETY STRAP DETERIORATED .<[01] OK TO CONTINUE PER MEL 25-10-01. SP1B;[02] R/R WARNING STRAP ASSY PER SIP - [SDR SWAA2024092741369](https://openairdocs.org/sdr/SWAA2024092741369), Sep 25, 2024: STRAP. DETERIORATED. FWD ENTRY DOOR SAFETY STRAP DETERIORATED .<[01] OK TO CONTINUE PER MEL 25-10-01. SP1B;[02] R/R WARNING STRAP ASSY PER SIP - [SDR SWAA2024092338657](https://openairdocs.org/sdr/SWAA2024092338657), Sep 17, 2024: HANDLE. LOOSE. PAX CABIN FWD ENTRY DOOR LINING ASSISTANT HANDLE LOOSE 2024-489434<[01] CORRECTED INSTALLED PAX CABIN FWD ENTRY DOOR LINING ASSISTANT HANDLE IAW B737- 700 AMM 5 - [SDR SWAA2024092338663](https://openairdocs.org/sdr/SWAA2024092338663), Sep 17, 2024: HANDLE. LOOSE. PAX CABIN AFT SERVICE RIGHT DOOR AREA ; FWD CUT OUT ASSISTANT HANDLE LOOSE 2024-489451<[01] PAX CABIN AFT SERVICE RIGHT DOOR AREA FWD CUT OUT ASSISTANT HANDLE T - [SDR SWAA2024091930026](https://openairdocs.org/sdr/SWAA2024091930026), Aug 25, 2024: WINDOW FRAME. CRACKED. CRACK WINDOW 3 FRAME LT SIDE AT COCKPIT 2024-489385<[01] PERFORMED A PERMANET REPAIR ON WINDOW 3 FRAME LT SIDE AT COCKPIT IAW EA- 24-153-02350-WIP1 [TTG8Q00VGP0 - [SDR SWAA2024092025383](https://openairdocs.org/sdr/SWAA2024092025383), Aug 12, 2024: WEB. CRACKED. CRACK ON WEB LOCATED BTW BS 500D TO BS 520 AT LEVEL STR 28R AT FWD CARGO COMPARTMENT 2024-489315<[01] REPLACED WEB AND FASTENERS LOCATED BTW BS 500D TO BS 520 A - [SDR SWAA2024092025381](https://openairdocs.org/sdr/SWAA2024092025381), Aug 12, 2024: ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED AT FACE BS 500D AT LEVEL STR 28L AT FWD CARGO COMPARTMENT 2024-489311<[01] REPLACED ANGLE LOCATED AT FACE BS 500D AT LEVEL STR 28 - [SDR SWAA2024091925379](https://openairdocs.org/sdr/SWAA2024091925379), Aug 12, 2024: STRINGER. CRACKED. CRACK STRINGER 25L LOCATED BS 540 AT FWD CARGO COMPARTMENT 2024-489309<[01] TOOL USED: ULTRASONIC EQUIPMENT P/N 45MG S/N 13066401 DUE DATE: 05-OCT-24.;[02] TOOL - [SDR SWAA2024091925380](https://openairdocs.org/sdr/SWAA2024091925380), Aug 12, 2024: STRINGER. CRACKED. CRACK ON STRINGER 27L LOCATED BS 540 AT FWD CARGO COMPARTMENT 2024-489310<[01] TOOL USED: ULTRASONIC EQUIPMENT P/N 45MG S/N 13066401 DUE DATE: 05-OCT-24.;[02] T - [SDR SWAA2024091925382](https://openairdocs.org/sdr/SWAA2024091925382), Aug 12, 2024: STRINGER. CRACKED. CRACK ON STR 26L LOCATED BS 540 AT FWD CARGO COMPARTMENT 2024-489314<[01] TOOL USED: ULTRASONIC EQUIPMENT P/N 45MG S/N 13066401 DUE DATE: 05-OCT-24.;[02] TOOLS - [SDR SWAA2024092325378](https://openairdocs.org/sdr/SWAA2024092325378), Aug 11, 2024: BALANCE ARM. CORRODED. CUSTOMER REQUESTS CORROSION ON LE OF RUDDER BALANCE ARM AT VERTICAL STABILIZER 2024-489272<[01] REPLACED RUDDER BALANCE ARM WEIGHT IAW BOEING 737 CMM 55-40-09.S - [SDR SWAA2024092324801](https://openairdocs.org/sdr/SWAA2024092324801), Aug 10, 2024: ANGLE. CRACKED. CRACK ANGLE LOCATED BS 867 BETWEEN S-2R TO S-3R AT PASSENGER CABIN 2024-489238<[01] REPLACED ANGLE LOCATED BS 867 BETWEEN S-2R TO S-3R AT PASSENGER CABIN IAW B7 - [SDR SWAA2024092324817](https://openairdocs.org/sdr/SWAA2024092324817), Aug 10, 2024: STRINGER. CRACKED. CRACK TIE CLIP LOCATED BS 277 AND S-10R AT PASSENGER CABIN 2024-489249<[01] REPLACED TIE CLIP LOCATED BS 277 AND S-10R AT PASSENGER CABIN IAW B737-700 SRM 51-40 - [SDR SWAA2024092024810](https://openairdocs.org/sdr/SWAA2024092024810), Aug 10, 2024: ACCESS PANEL. DAMAGED. ELONGATED HOLE ACCESS PANEL 123YBC AT FWD CARGO COMPARTMENT 2024-489246<[01] FABRICATED PANEL 123YBC AT FWD CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 - [SDR SWAA2024092024815](https://openairdocs.org/sdr/SWAA2024092024815), Aug 10, 2024: ACCESS PANEL. ELONGATED. ELONGATED HOLE ACCESS PANEL 123YCC AT FWD CARGO COMPARTMENT 2024-489248<[01] FABRICATED PANEL 123YCC AT FWD CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 - [SDR SWAA2024092024813](https://openairdocs.org/sdr/SWAA2024092024813), Aug 10, 2024: ACCESS PANEL. DAMAGED. ELONGATED HOLE ACCESS PANEL 123YAC AT FWD CARGO COMPARTMENT 2024-489251<[01] FABRICATED PANEL 123YAC AT FWD CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 - [SDR SWAA2024092024811](https://openairdocs.org/sdr/SWAA2024092024811), Aug 10, 2024: LIGHT. DETERIORATED. DETERIORATED PHOTOLUMINESCENT STRIP LT AND RT SIDE AT PASSENGER CABIN 2024-489244<[01] REPLACED PHOTOLUMINESCENT STRIP LT AND RT SIDE AT
PASSENGER CABIN IAW - [SDR SWAA2024092024807](https://openairdocs.org/sdr/SWAA2024092024807), Aug 10, 2024: ANGLE. CRACKED. CRACK ANGLE - CLIP LOCATED STA500C AND STR26L FWD CARGO COMPARTMENT 2024-489239<[01] REPLACED CLIP LOCATED STA500C AND STR26L FWD CARGO COMPARTMENT IAW B737-700 - [SDR SWAA2024092024808](https://openairdocs.org/sdr/SWAA2024092024808), Aug 10, 2024: ANGLE. CRACKED. CRACK ANGLE - CLIP LOCATED STA500C AND STR26R FWD CARGO COMPARTMENT 2024-489240<[01] REPLACED ANGLE - CLIP LOCATED STA500C AND STR26R FWD CARGO COMPARTMENT IAW - [SDR SWAA2024091924821](https://openairdocs.org/sdr/SWAA2024091924821), Aug 10, 2024: WEB. CRACKED. CRACK WEB FRAME BS 259.5 BETWEEN S-8R TO S-9R AT PASSENGER CABIN 2024-489252<[01] ON STEP 5; TOOL USED: EDDY CURRENT INSPECTION; PN: NORTEC 600D; SN: 6000916163 - [SDR SWAA2024091924820](https://openairdocs.org/sdr/SWAA2024091924820), Aug 10, 2024: WEB. CRACKED. CRACK WEB FRAME BS 259.5 BETWEEN S-8L TO S-9L AT PASSENGER CABIN 2024-489254<[01] TOOL USED STEP 5 EDDY CURRENT EQUIPMENT PN: NORTEC 600D SN: 200053402 DUE DATE - [SDR SWAA2024091924812](https://openairdocs.org/sdr/SWAA2024091924812), Aug 10, 2024: STRINGER. CRACKED. CRACK STRINGER 7L LOCATED BS 294.5 AT PASSENGER CABIN 2024-489247<[01] TOOL USED : EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138003; DUE DATE: 11-J - [SDR SWAA2024091924798](https://openairdocs.org/sdr/SWAA2024091924798), Aug 10, 2024: WEB. CRACKED. CRACK WEB LOCATED RIB 5 AND RIB 6 FRONT SPAR AT RT HORIZONTAL STABILIZER 2024-489228<[01] EQUIPMENT USED P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 08-JAN-25;[ - [SDR SWAA2024092024797](https://openairdocs.org/sdr/SWAA2024092024797), Aug 9, 2024: ANGLE. CRACKED. CRACK ON FWD ENTRY DOOR AFT UPPER TARGET ANGLE 2024-489223<[01] REPLACED FWD ENTRY DOOR AFT UPPER TARGET ANGLE IAW B737-700 SRM SRM 51-40-02 AND 51-10-02 ITEM 9 - [SDR SWAA2024092324288](https://openairdocs.org/sdr/SWAA2024092324288), Aug 8, 2024: STRAP. CRACKED. CRACK STRAP LOCATED STA440 AND BETWEEN STR20R TO STR21R FWD CARGO COMPARTMENT 2024-489209<[01] REPLACED STRAP LOCATED STA440 AND BETWEEN STR20R TO STR21R FWD CA - [SDR SWAA2024092024283](https://openairdocs.org/sdr/SWAA2024092024283), Aug 8, 2024: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BETWEEN STA727A TO STA767 AND RBL21 WL156 AFT CARGO COMPARTMENT 2024-489195<[01] REPLACED SUPPORT ZEE AND FASTENERS LOCATED BETWEE All 316: https://openairdocs.org/aircraft/N495WN/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 --- 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.