# N765SW: 2000 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: 29805 - Year built: 2000 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: April 24, 2000 - Certificate issued: April 25, 2000 - Expires: March 31, 2030 - Mode S code: AA55C0 - 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=765SW - Page: https://openairdocs.org/aircraft/N765SW 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/N765SW/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; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB ENG17IA027](https://openairdocs.org/ntsb/ENG17IA027), Jun 3, 2017: Boeing 737 7H4 (N765SW), Washington, DC, incident, minor damage. Probable cause: The failure the control alternator gearshaft, which disconnected the accessory gearbox from the rest of the engine and resulted in an uncommanded in-flight shutdown of the left engine and subsequent… ## FAA accident and incident reports None matched to N765SW. ## Service difficulty reports (303, newest 50) As reported by operators and repair stations. - [SDR SWAA2023082190977](https://openairdocs.org/sdr/SWAA2023082190977), Aug 18, 2023: BATTERY PACK. FAILED. EMERGENCY LIGHT BATTERY PACK AT LOCATION M1674 FAILED CAPACITY TEST<[01] R/R M1674 EMERGENCY BATTER PACK PER AMM 33-51-06;[02] ADD PART REMOVAL TO S/O - [SDR SWAA2023072581652](https://openairdocs.org/sdr/SWAA2023072581652), Jul 22, 2023: PANEL. CRACKED. PANEL 193D CRACKED . CRACK MEASURED 3 IN LENGTH.<[01] REMOVED AND REPLACED FAIRING PANEL 193D PER AMM. 53-51-21. - [SDR SWAA2023070573575](https://openairdocs.org/sdr/SWAA2023070573575), Jun 30, 2023: BULB. INOPERATIVE. L/H AFT LOWER FUSELAGE EMER LIGHT INOP<[01] R&R L/H AFT LOWER FUSELAGE EMER LIGHT BULB PER AMM 33-51-04.OPS CHECK GOOD - [SDR SWAA2022122284454](https://openairdocs.org/sdr/SWAA2022122284454), Dec 22, 2022: LAMP. INOPERATIVE. INOPERTIVE BULLNOSE EMERGENCY LIGHT 18DEF. RELAMPED PER AMM 33-51-03 - [SDR SWAA2022102462884](https://openairdocs.org/sdr/SWAA2022102462884), Oct 21, 2022: FLASHLIGHT. INOPERATIVE. FWD GALLEY FLASHLIGHT INOP / [01] REMOVED AND REPLACED FLUSH LIGHT IAW AMM 25-64-00;[02] REMOVED AND REPLACED FLASH LIGHT IAW AMM 25-64-00;[03] REMOVED AN REPLA - [SDR SWAA2022101258449](https://openairdocs.org/sdr/SWAA2022101258449), Oct 11, 2022: NONE. INOPERATIVE. MULTIPLE EMERGENCY LIGHTS INOP / [01] REMOVED AND REPLACED FWD RH (M1674) BATTERY AND BATTERY CHARGER PACK ASSEMBLY IN REFERENCE TO AMM 33-51-06. OPS CHECK GOOD - [SDR SWAA2022090649818](https://openairdocs.org/sdr/SWAA2022090649818), Sep 3, 2022: NONE. OUT OF POSITION. FWD SERVICE SIDE EMERGENCY EXIT LENSE FELL OFF / [01] OK TO CONT PER MEL 25-10-01 SP1B
AUTH#86171;[02] RE-SECURED FWD SERVICE DOOR EMERGENCY EXIT LENSE PER S - [SDR SWAA2022081843182](https://openairdocs.org/sdr/SWAA2022081843182), Aug 18, 2022: PANEL. DELAMINATED. PANEL 193 B HAS WORN/DELAMINATED AREAS AT FASTENER HOLE LOCATIONS 6; 8; 10; 11; 13; 14; 17; 22; 33; AND 34. PANEL 193 B HAS WORN/DELAMINATED AREAS AT FASTENER H - [SDR SWAA2022080137105](https://openairdocs.org/sdr/SWAA2022080137105), Jul 30, 2022: O-RING. LEAKING. DURING FLIGHT AT 29K FEET WE LOST HYDRAULIC SYS B FLUID WENT TO ZERO AND TOTAL LOSS OF PRESSURE / [01] REF TTG8Q00DVGLL ALT BRAKE SELECTOR VALVE LEAKING. MT 729 - [SDR SWAA2022080136782](https://openairdocs.org/sdr/SWAA2022080136782), Jul 30, 2022: SELECTOR VALVE. LEAKING. DURING FLIGHT AT 29K FEET WE LOST HYDRAULIC SYS B FLUID WENT TO ZERO AND TOTAL LOSS OF PRESSURE / [01] REF TTG8Q00DVGLL ALT BRAKE SELECTOR VALVE LEAKING. MT 729 - [SDR SWAA2022080137104](https://openairdocs.org/sdr/SWAA2022080137104), Jul 30, 2022: SELECTOR VALVE. LEAKING. DURING FLIGHT AT 29K FEET WE LOST HYDRAULIC SYS B FLUID WENT TO ZERO AND TOTAL LOSS OF PRESSURE / [01] REF TTG8Q00DVGLL ALT BRAKE SELECTOR VALVE LEAKING. MT 729 - [SDR SWAA2022070524810](https://openairdocs.org/sdr/SWAA2022070524810), Jul 1, 2022: LIGHT. LOOSE. EXIT LIGHT COVER FELL OFF ON TAKEOFF (MIDDLE OF AIRCRAFT). WILL NOT STAY SECURED. / [01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT IAW MM 33-51-01. OPS A CHECK - [SDR SWAA2022040690679](https://openairdocs.org/sdr/SWAA2022040690679), Apr 2, 2022: LIGHT. FAILED. FWD OVERHEAD EXIT SIGN FELL OFF / [01] SECURED LENS PER SIP/AMM 33-51-01. OK FOR SERVICE - [SDR SWAA2022010457003](https://openairdocs.org/sdr/SWAA2022010457003), Dec 30, 2021: BATTERY PACK. INOPERATIVE. INOP BATTERY EMERGENCY LIGHT AFT GALLEY AREA RH ; 2021-549938 / [01] REPLACED BATTERY PACK ON AFT GALLEY AREA ON RH SIDE P/N OFF: D717-01-100SWA S/N OFF: 19023 - [SDR SWAA2022010452051](https://openairdocs.org/sdr/SWAA2022010452051), Dec 10, 2021: SHOCK MOUNT. BROKEN. BROKEN FWD SERVICE DOOR SLIDE SHOCK MOUNT AT PASSENGER CABIN (1 EA) ; 2021-549919 / [01] REPLACED SLIDE SHOCK MOUNT LOC. FWD SERVICE DOOR AT PASSENGER CABIN (1 - [SDR SWAA2022010451586](https://openairdocs.org/sdr/SWAA2022010451586), Dec 8, 2021: GUSSET. CRACKED. CRACK GUSSET LOCATED BS 500D STR 19R FWD CARGO COMPARTMENT. REPLACED GUSSET LOCATED BS 500D STR 19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. DGW: 143A79 - [SDR SWAA2022010451587](https://openairdocs.org/sdr/SWAA2022010451587), Dec 8, 2021: GUSSET. CRACKED. CRACK GUSSET LOCATED BS 500D STR 19L FWD CARGO COMPARTMENT ; 2021-549916 / [01] REPLACED GUSSET LOCATED BS 500D STR 19L FWD CARGO COMPARTMENT. IAW B737-700 SRM - [SDR SWAA2022010450232](https://openairdocs.org/sdr/SWAA2022010450232), Dec 4, 2021: WEB. CORRODED. CORROSION WEB LOCATED BS196.5 TO BS203.8 AND LBL 9; WL148.5 AT LOWER FUSELAGE ; 2021-549878 / [01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: - [SDR SWAA2022010549814](https://openairdocs.org/sdr/SWAA2022010549814), Dec 3, 2021: NONE. CRACKED. SUPPLEMENTAL INFORMATION: CRACK INSPAR RIB LOC STAB STA 129.50 AT 35 INCH FROM FRONT SPART LT HORIZONTAL STAB (1 E/A) ; 2021-549836 / [01] TOOL USED. EDDY CURRE - [SDR SWAA2022010550229](https://openairdocs.org/sdr/SWAA2022010550229), Dec 3, 2021: ACCESS PANEL. CRACKED. SUPPLEMENTAL INFORMATION: CRACK ACCESS PANEL 651GB CORRUGATED PLATE AT RT WING ; 2021-549847 / [01] REPLACED CORRUGATED PLATE ON ACCESS PANEL 651GB AT RT WING. - [SDR SWAA2022010549976](https://openairdocs.org/sdr/SWAA2022010549976), Dec 3, 2021: STRINGER. CRACKED. SUPPLEMENTAL INFORMATION: CRACK INTERNAL CAVITY STRINGER U-8 UPPER SURFACE BETWEEN RIB 19 TO RIB 20 AT LT WING ; 2021-549843 / [01] TOOL USED: TEMPERATURE CONTR - [SDR SWAA2022010549598](https://openairdocs.org/sdr/SWAA2022010549598), Dec 2, 2021: ACCESS PANEL. CRACKED. SUPPLEMENTAL INFORMATION: CRACK ACCESS PANEL 532NB FUEL TANK FLOAT AT LT WING ; 2021-549811 / [01] FAULT RESOLVED ON OTHER FAULT REPLACED FUEL TANK FLOAT ON ACC - [SDR SWAA2022010549813](https://openairdocs.org/sdr/SWAA2022010549813), Dec 2, 2021: RIB. CRACKED. CRACK DORSAL FIN RIB 8 AT VERTICAL STABILIZER ; 2021-549833 / [01] REPLACED RIB 8 AND FASTENERS LOC. DORSAL FIN AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 - [SDR SWAA2022010449600](https://openairdocs.org/sdr/SWAA2022010449600), Dec 2, 2021: ANGLE. CRACKED. CRACK ANGLE - CLIP LOCATED ON BS 500C AFT FACE AT LEVEL STR 26L AT FWD CARGO COMPARTMENT ; 2021-549817 / [01] REPLACED CLIP AND FASTENERS LOCATED ON BS 500C AFT - [SDR SWAA2022010449601](https://openairdocs.org/sdr/SWAA2022010449601), Dec 2, 2021: NONE. CRACKED. CRACK ANGLE - CLIP LOC ON BS 400 AFT FACE AT LEVEL STR 26L AT FWD CARGO COMPARTMENT ; 2021-549819 / [01] REPLACED CLIP AND FASTENERS LOC ON BS 400 AFT FACE AT L - [SDR SWAA2022010449812](https://openairdocs.org/sdr/SWAA2022010449812), Dec 2, 2021: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 AT LEVEL STR 25R RBL 21 AT AFT CARGO COMPARTMENT ; 2021-549830 / [01] REPLACED SUPPORT ZEE LOCATED BTW BS 727 - [SDR SWAA2022010549416](https://openairdocs.org/sdr/SWAA2022010549416), Dec 1, 2021: NONE. CRACKED. SUPPLEMENTAL INFORMATION: CRACK FLOOR STRUCTURE PLATE LOCATED ON BS 540 BTW BL 0 TO LBL 25 AT PASSENGER CABIN ; 2021-549793 / [01] REPLACED FLOOR STRUCTURE PLAT - [SDR SWAA2022010549415](https://openairdocs.org/sdr/SWAA2022010549415), Dec 1, 2021: PLATE. CRACKED. CRACK FLOOR STRUCTURE PLATE LOCATED ON BS 540 BTW BL 0 TO RBL 25 AT PASSENGER CABIN ; 2021-549792 / [01] REPLACED FLOOR STRUCTURE PLATE LOCATED ON BS 540 BTW BL - [SDR SWAA2022010449414](https://openairdocs.org/sdr/SWAA2022010449414), Dec 1, 2021: STRINGER. CORRODED. CORROSION STRINGER 23L BS 540 AT WL 164 AT FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR STRINGER 23L BETWEEN BS500D TO BS540 AT FWD CARGO COMPARTMENT IAW S - [SDR SWAA2022010449413](https://openairdocs.org/sdr/SWAA2022010449413), Dec 1, 2021: STRINGER. CORRODED. CORROSION STRINGER 26L LOCATED ON BS 540 AT FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR STRINGER 26L BETWEEN BS500D TO BS540 AT FWD CARGO COMPARTMENT IAW - [SDR SWAA2022010549024](https://openairdocs.org/sdr/SWAA2022010549024), Nov 30, 2021: PLATE. BROKEN. BROKEN TRAILING EDGE CORRUGATED PLATE LOCATED WS180.00 INTERNAL AREA OF ACCESS PANEL 651EB AT RT WING ; 2021-549676 / [01] REPLACED CORRUGATED PLATE LOCATED WS1 - [SDR SWAA2022010549025](https://openairdocs.org/sdr/SWAA2022010549025), Nov 30, 2021: PLATE. BROKEN. BROKEN TRAILING EDGE CORRUGATED PLATE LOCATED WS204.25 INTERNAL AREA OF ACCESS PANEL 651EB AT RT WING ; 2021-549674 / [01] REPLACED CORRUGATED PLATE LOCATED WS2 - [SDR SWAA2022010549030](https://openairdocs.org/sdr/SWAA2022010549030), Nov 30, 2021: BRACKET. BROKEN. BROKEN SUPPORT BRACKET LOCATED IRSS140 REAR SPAR UPPER AREA AT LT WING ; 2021-549710 / [01] REPLACED SUPPORT BRACKET LOCATED IRSS140 REAR SPAR UPPER AREA AT LT - [SDR SWAA2022010549032](https://openairdocs.org/sdr/SWAA2022010549032), Nov 30, 2021: ANGLE. BROKEN. BROKEN ANGLE TRAILING EDGE LOCATED ORSS174 REAR SPAR UPPER AREA AT RT WING ; 2021-549722 / [01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS174 REAR SPAR UPPER ARE - [SDR SWAA2022010449027](https://openairdocs.org/sdr/SWAA2022010449027), Nov 30, 2021: STRINGER. CRACKED. CRACKED STRINGER 26R, AT BS 540 IN FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR STRINGER 26R LOCATED BTW BS500D TO BS540 IAW SRM B737-700 53-00-03-2R-1 REP - [SDR SWAA2022010449026](https://openairdocs.org/sdr/SWAA2022010449026), Nov 30, 2021: STRINGER. CRACKED. CORROSION STRINGER 24R LOCATED AT BS 540 AND WL 160 AT FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR STRINGER 24R BETWEEN BS500D TO BS540 AND WL 160 AT FWD - [SDR SWAA2022010449029](https://openairdocs.org/sdr/SWAA2022010449029), Nov 30, 2021: STRINGER. CORRODED. CORROSION STRINGER 25R AT BS 540 AND WL 156 AT FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR LOCATED STRINGER 25R BETWEEN BS500C TO BS540 AT FWD CARGO COMPA - [SDR SWAA2022010449023](https://openairdocs.org/sdr/SWAA2022010449023), Nov 30, 2021: STRINGER. CORRODED. CORROSION STRINGER 22R LOCATED AT BS 540 AND WL 168 AT FWD CARGO COMPARTMENT ; 2021-549688. PERFORMED PERMANENT REPAIR LOCATED STRINGER 22R BETWEEN BS500C TO BS - [SDR SWAA2022010449022](https://openairdocs.org/sdr/SWAA2022010449022), Nov 30, 2021: STRINGER. CORRODED. CORROSION STRINGER 23R LOCATED AT BS 540. WL164 AT FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR STRINGER 23R BETWEEN BS500D TO BS540 WL154 AT FWD CARGO COM - [SDR SWAA2022010548687](https://openairdocs.org/sdr/SWAA2022010548687), Nov 29, 2021: ACCESS PANEL. CRACKED. CRACK ACCESS PANEL 561AB HOLES AT LT WING ; 2021-549546 / [01] TOOL USED: CALIPER P/N: 500-464; S/N: 15331932; DUE DATE: 26-OCT-22; [02] HOT BONDER PN: HCS9200B - [SDR SWAA2022010548688](https://openairdocs.org/sdr/SWAA2022010548688), Nov 29, 2021: ACCESS PANEL. CRACKED. CRACK ACCESS PANEL 561BB HOLES AT LT WING ; 2021-549549 / [01] TOOL USED: CALIPER P/N: 500-464; S/N: 15331932; DUE DATE: 26-OCT-22; [02] HOT BONDER PN: HCS9200B - [SDR SWAA2022010548179](https://openairdocs.org/sdr/SWAA2022010548179), Nov 28, 2021: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED BS695 AND RBL24.75 LOWER POSITION CENTER SECTION ; 2021-549498 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 1 - [SDR SWAA2022010548182](https://openairdocs.org/sdr/SWAA2022010548182), Nov 28, 2021: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED BS695 AND LBL24.75 LOWER POSITION CENTER SECTION ; 2021-549500 / [01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 11203 - [SDR SWAA2022010448177](https://openairdocs.org/sdr/SWAA2022010448177), Nov 28, 2021: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED BS695 AND BL0 LH SIDE CENTER SECTION ; 2021-549495 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DU - [SDR SWAA2022010448181](https://openairdocs.org/sdr/SWAA2022010448181), Nov 28, 2021: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED BS695 AND BL0 RH SIDE CENTER SECTION ; 2021-549493. REPLACED SUPPORT ANGLE LOCATED BS695 AND BL0 RH SIDE CENTER SECTION I.A.W B737-7 - [SDR SWAA2022010448185](https://openairdocs.org/sdr/SWAA2022010448185), Nov 28, 2021: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED BS695 AND RBL24.75 VERTICAL POSITION CENTER SECTION ; 2021-549502. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS695 AND RBL24.75 V - [SDR SWAA2022010448176](https://openairdocs.org/sdr/SWAA2022010448176), Nov 28, 2021: SCUFF PLATE. CRACKED. CRACK ON AFT CORNER SCUFF PLATE LOCATED BS 492 AT FWD CARGO COMPARTMENT ; 2021-549491 / [01] TOOL USED; DIGITAL CALIPER P/N:500-197-30 S/N:A21142022 DUE DATE: 0 - [SDR SWAA2022010448178](https://openairdocs.org/sdr/SWAA2022010448178), Nov 28, 2021: SCUFF PLATE. CRACKED. CRACK ON FWD CORNER SCUFF PLATE LOCATED BS 440 AT FWD CARGO COMPARTMENT ; 2021-549494 / [01] TOOL USED; DIGITAL CALIPER; P/N:500-197-30 S/N:A21142022 DUE DATE:0 - [SDR SWAA2022010448186](https://openairdocs.org/sdr/SWAA2022010448186), Nov 28, 2021: SCUFF PLATE. CRACKED. CRACK ON AFT CORNER SCUFF PLATE LOCATED BS 847 AT AFT CARGO BAY. REPAIRED BY WELDING AFT CORNER SCUFF PLATE LOCATED BS 847 AT AFT CARGO COMPARTMENT I.A.W. BOEIN - [SDR SWAA2021120248183](https://openairdocs.org/sdr/SWAA2021120248183), Nov 28, 2021: SCUFF PLATE. CRACKED. CRACK ON FWD CORNER SCUFF PLATE LOCATED BS 792 AT AFT CARGO BAY. REPAIRED BY WELDING FWD CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1. All 303: https://openairdocs.org/aircraft/N765SW/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.