# N286WN: 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: 32471 - Year built: 2004 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 13, 2004 - Certificate issued: August 16, 2004 - Expires: February 29, 2028 - Mode S code: A2E646 - 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=286WN - Page: https://openairdocs.org/aircraft/N286WN From the FAA registry file of October 22, 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/N286WN/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 N286WN. ## FAA accident and incident reports None matched to N286WN. ## Service difficulty reports (295, 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 SWAA2026092188951](https://openairdocs.org/sdr/SWAA2026092188951), Sep 15, 2026: LIGHT. BROKEN. OVERHEAD EMERGENCY LIGHT ASSEMBLY FOR AISLE BROKEN REPLACED OVERHEAD EMERGENCY LIGHT ASSEMBLY IAW AMM 33-51-01. OPS CHKD GOOD. - [SDR SWAA2026061004193](https://openairdocs.org/sdr/SWAA2026061004193), May 18, 2026: SKIN. CORRODED. CORROSION FOUND ON LOWER FUSELAGE SKIN AT BS 400+6'- 400+15' BTW STR 27L- 26L. IAW EA 26-153-01372; THE REWORK IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION - [SDR SWAA2026061003731](https://openairdocs.org/sdr/SWAA2026061003731), May 17, 2026: SCUFF PLATE. CRACKED. AFT CARGO AFT CORNER SCUFF PLATE CRACKED. REMOVED AND REPLACED CRACKED SCUFF PLATE IAW AMM 53-11-02-020-801 AND AMM 53-11-02-420-801. - [SDR SWAA2026061003734](https://openairdocs.org/sdr/SWAA2026061003734), May 17, 2026: FAIRING. CORRODED. CORROSION FOUND ON LOWER FUSELAGE AT BS 440+14, STRINGER 26L; NEAR LOW RANGE RADIO ALTIMETER ANTENNA AREA. REPLACED (FAIRING ASSY; NUT PLATE ASSEMBLIES; COVER P - [SDR SWAA2026061003735](https://openairdocs.org/sdr/SWAA2026061003735), May 17, 2026: FAIRING. CORRODED. CORROSION FOUND ON LOWER FUSELAGE AT STA 400+7, STRINGER 26L; NEAR LOW RANGE RADIO ALTIMETER ANTENNA AREA. REPLACED THE FAIRING ASSY; NUT PLATE ASSEMBLIES; COVE - [SDR SWAA2026060303736](https://openairdocs.org/sdr/SWAA2026060303736), May 17, 2026: SKIN. CORRODED. CORROSION FOUND ON LOWER FUSELAGE SKIN AT STA 440+6 IN; BETWEEN STRINGERS 26L AND 27L; NEAR LOW RANGE RADIO ALTIMETER ANTENNA AREA (MARKED)<[01] AS PER EA 26-15 - [SDR SWAA2026060303725](https://openairdocs.org/sdr/SWAA2026060303725), May 16, 2026: ATTACH ANGLE. CRACKED. LH 663 VAPOR BARRIER UPPER ATTACH ANGLE CRACKED LBL 11. REMOVED FASTENERS AS REQUIRED COMMON TO REPAIR BSTA. 663 UPPER ATTACH ANGLE LEFT SIDE; VAPOR BARRIER PER - [SDR SWAA2026040786179](https://openairdocs.org/sdr/SWAA2026040786179), Apr 3, 2026: FLOORBOARD. CRACKED. CREW REPORTS FWD CARGO METAL FLOORBOARD CRACKED. OK TO CONTINUE PER MEL 25-16-01 SP1B. R &R FWD CENTER. FLOORBOARD IAW AMM 25-52-10. - [SDR SWAA2026030976578](https://openairdocs.org/sdr/SWAA2026030976578), Mar 4, 2026: SCUFF PLATE. CRACKED. CRACK MEASURING 0.5 IN. ON DENT MEASURING L=0.625; W=0.5; D=0.054, ON THE FWD CARGO SCUFF PLATE. R & R THE SCUFF PLATE IAW AMM 53-11-01, & 53-11-02, - [SDR SWAA2025110330548](https://openairdocs.org/sdr/SWAA2025110330548), Oct 31, 2025: RING. ENGAGED. GIRT BAR FORWARD SERVICE DOOR LOOSE. INSTALLED GIRT BAR STOP RELEASE RING IAW AMM 25-66-01. OPS CHECKED GOOD. - [SDR SWAA2025101523864](https://openairdocs.org/sdr/SWAA2025101523864), Oct 12, 2025: LAMP. INOPERATIVE. LEFT OVERWING EXIT SIGN SIDEWALL LIGHT INOPERATIVE. R & R LEFT OVERWING EXIT SIGN LAMP IAW AMM 33-51-04. OPS CHECKED GOOD. - [SDR SWAA2025042126532](https://openairdocs.org/sdr/SWAA2025042126532), Apr 20, 2025: ELEC CONNECTOR. DIRTY. WITH LAP LEVER TO 25; FLAP INDICATOR SHOWED SPLIT FLAP CONDITION WITH 1 NEEDLE AT 0 AND THE OTHER AT .5. RAN QRH FOR TRAILING EDGE FLAP ASYMMETRY. FLAPS OPERATE - [SDR SWAA2025010382230](https://openairdocs.org/sdr/SWAA2025010382230), Jan 1, 2025: SLIDE. LOOSE. CREW REPORTS ANTS LH ESCAPE SLIDE HARDWARE LOOSE<[01] VERIFIED HARDWARE SECURE PER AMM 25-66-01 - [SDR SWAA2024070908947](https://openairdocs.org/sdr/SWAA2024070908947), Jul 4, 2024: SLIDE. OUT OF ADJUST. CUSTOMER WALK - L2 DOOR SLIDE SKIRT HITS THRESHOLD WHEN CLOSING<[01] READJUSTED THE GIRT Z-FOLD ON L2 DOOR SLIDE REF 'TASK CARD '725-61-06 (REM/INST - SLIDE REM - [SDR SWAA2024070908953](https://openairdocs.org/sdr/SWAA2024070908953), Jul 4, 2024: SLIDE. OUT OF ADJUST. CUSTOMER WALK - R2 DOOR SLIDE SKIRT HITS THRESHOLD WHEN CLOSING<[01] REFER TO TASK CARD '725-61-06 (REM/INST - SLIDE REMOVAL AND INSTALLATION) [TTG8Q00UDCAY]' F - [SDR SWAA2024070908946](https://openairdocs.org/sdr/SWAA2024070908946), Jul 4, 2024: BULB. BURNED OUT. CUSTOMER WALK - SEVERAL BULBS BURNT OUT ON EMER EXIT SIGN ON AFT GALLEY OUTBD SIDE<[01] RELAMPED BULBS ON EMER EXIT SIGN ON AFT GALLEY OUTBD SIDE AS PER B737 AM - [SDR SWAA2024070906475](https://openairdocs.org/sdr/SWAA2024070906475), Jun 27, 2024: FUSE. INOPERATIVE. MULTIPLE PAX EMERGENCY LIGHTS INOP<[01] REPLACED FUSES ON BATTERY PACK M1669 I/A/W B737 AMM 33-51-06-960-804. OPS CHECK PASSED.;[02] VERIFIED STEP 1. - [SDR SWAA2024070903575](https://openairdocs.org/sdr/SWAA2024070903575), Jun 19, 2024: SEAT TRACK. CORRODED. FLIGHT DECK FIRST OFFICER FWD SEAT TRACK I/B HAS CORROSION.<[01] RECEIVED SERVICEABLE TRACK FOR FIRST OFFICER FWD SEAT TRACK I/B. INSTALLATION WILL BE ACCOMPLIS - [SDR SWAA2024070903576](https://openairdocs.org/sdr/SWAA2024070903576), Jun 19, 2024: SEAT TRACK. CORRODED. FLIGHT DECK FIRST OFFICER FWD SEAT TRACK O/B HAS CORROSION.<[01] RECEIVED SERVICEABLE TRACK FOR FIRST OFFICER FWD SEAT TRACK O/B. INSTALLATION WILL BE ACCOMPLIS - [SDR SWAA2024070903577](https://openairdocs.org/sdr/SWAA2024070903577), Jun 19, 2024: SEAT TRACK. CORRODED. FLIGHT DECK CAPTAIN FWD SEAT TRACK I/B HAS CORROSION.<[01] RECEIVED SERVICEABLE TRACK FOR CAPTAIN FWD SEAT TRACK I/B. INSTALLATION WILL BE ACCOMPLISHED ON TASK - [SDR SWAA2024070903574](https://openairdocs.org/sdr/SWAA2024070903574), Jun 19, 2024: SEAT TRACK. CORRODED. FLIGHT DECK CAPTAIN FWD SEAT TRACK O/B HAS CORROSION.<[01] RECEIVED SERVICEABLE TRACK FOR CAPTAIN FWD SEAT TRACK O/B. INSTALLATION WILL BE ACCOMPLISHED ON TASK - [SDR SWAA2024070900662](https://openairdocs.org/sdr/SWAA2024070900662), Jun 12, 2024: WEB. CRACKED. CRACK FOUND AT UNDERLYING STRUCTURE OF EXISTING FLIGHT DECK FLOOR WEB AT STA 260; RBL 4 ADJACENT TO PRODUCTION FASTENER HOLE. CRACK FOUND AT UNDERLYING STRUCTUR - [SDR SWAA2024070999343](https://openairdocs.org/sdr/SWAA2024070999343), Jun 8, 2024: FLOOR PANEL. CRACKED. FLOOR PANEL BREAK ASSEMBLY AT STA 540 FROM BL 0 TO LBL 24.75 FOUND CRACKED.<[01] WORK ACCOMPLISHED ON FAULT #TTG8Q00TSRFU;[02] VERIFIED STEP 1
AUDIT PER MPM - [SDR SWAA2024070998871](https://openairdocs.org/sdr/SWAA2024070998871), Jun 6, 2024: FLOOR PANEL. CRACKED. CABIN FLOOR PANEL BREAK CRACKED AT STA.540 LBL 1.<[01] REMOVED AND REPLACED CABIN FLOOR PANEL BREAK ASSY AT STA.540 LBL 1. AS PER REF B737 SRM 51-40-02-0G-0.;[0 - [SDR SWAA2024070998872](https://openairdocs.org/sdr/SWAA2024070998872), Jun 6, 2024: FLOOR PANEL. CRACKED. CABIN FLOOR PANEL BREAK CRACKED AT STA.540 RBL 1.<[01] REMOVED AND REPLACED CABIN FLOOR PANEL BREAK ASSY AT STA.540 RBL1 AS PER REF B737 SRM 51-40-02-0G-0.;[02] - [SDR SWAA2024070391723](https://openairdocs.org/sdr/SWAA2024070391723), May 30, 2024: RIB. CRACKED. L/H HORIZONTAL STAB RIB #3 CRACKED AT STIFFENER #3 LWR RADIUS. STA. 111.10.<[01] REMOVED CRACK DAMAGE AND ACCOMPLISHED REPAIR AT L/H HORIZ. STAB RIB 3 AT STIFFE - [SDR SWAA2024070391724](https://openairdocs.org/sdr/SWAA2024070391724), May 30, 2024: RIB. CRACKED. L/H HORIZONTAL STAB RIB #3 CRACKED AT STIFFENER #4 LWR RADIUS. STA. 111.10.<[01] REMOVED CRACK DAMAGE AND ACCOMPLISHED REPAIR AT L/H HORIZ; STAB. RIB 3 AT STRIF - [SDR SWAA2024070391725](https://openairdocs.org/sdr/SWAA2024070391725), May 30, 2024: RIB. CRACKED. R/H HORIZONTAL STAB RIB #1 CRACKED AT STIFFENER #3 LWR RADIUS. STA. 92.70.<[01] REMOVED CRACK DAMAGE AND ACCOMPLISHED REPAIR AT R/H STABILIZER RIB #1; STIFFENER - [SDR SWAA2024070991110](https://openairdocs.org/sdr/SWAA2024070991110), May 29, 2024: BRACKET. CORRODED. CORROSION **LEFT W/W LT & RT ENGINES FIRE EXTINGUISHERS BOTTLES' SUPPORT BRACKETS AT AROUND FASTENERS HOLES MKD DOTS<[01] REMOVED AND REPLACED LT & RT FIRE EXTI - [SDR SWAA2024070990661](https://openairdocs.org/sdr/SWAA2024070990661), May 28, 2024: RETAINER. CRACKED. LEFT WING FIXED T/E REAR SPAR DEFLECTION CONTROL RIB PANEL LOWER T/EHORIZONTAL BULB SEAL RETAINER O/B ATTACHED CLIP CRACKED @ FASTENER HEAD MKD DOT<[01] REMOVED - [SDR SWAA2024070990655](https://openairdocs.org/sdr/SWAA2024070990655), May 28, 2024: RETAINER. CRACKED. RIGHT WING FIXED T/E REAR SPAR DEFLECTION CONTROL RIB PANEL LOWER VERTICAL SEAL RETAINER CRACKED @ FASTENER HEAD MKD DOT<[01] REMOVED AND REPLACED SEAL RETAIN A - [SDR SWAA2024070990654](https://openairdocs.org/sdr/SWAA2024070990654), May 28, 2024: VAPOR BARRIER. CRACKED. R/H WHEEL WELL AT VAPOR BARRIOR; VERTICAL SUPPORT STIFFENER CRACKED.<[01] REMOVED AND REPLACED STIFFENER AT R/H WHEEL WELL VAPOR BARRIER RBL 25 REF B737-700 SRM - [SDR SWAA2024070390663](https://openairdocs.org/sdr/SWAA2024070390663), May 28, 2024: SUPPORT ANGLE. CRACKED. R/H WING-TO-BODY ACCESS PANEL 191AR AS SUPPORT ANGLE CRACKED<[01] REMOVED AND REPLACED NEW SUPPORT ANGLE AT R/H WING-TO-BODY ACCESS PANEL 191AR PER REF B 737 SR - [SDR SWAA2024052287861](https://openairdocs.org/sdr/SWAA2024052287861), May 20, 2024: SLIDE. LOOSE. AFT LEFT SERVICE DOOR SLIDE LOOSE<[01] LOOSE SCREWS SECURED; ON SLIDE. REF MM 25-66-01 - [SDR SWAA2024050782776](https://openairdocs.org/sdr/SWAA2024050782776), May 5, 2024: GIRT BAR. DAMAGED. AFT SVC DOOR SLIDE GRIT BAR MISSING STOP-RINGE<[01] 01 - REMOVED AND REPLACED PER [AMM 25-66-01-000-804-NG (ESCAPE SLIDE GIRT BAR INSTALLATION - PERMANENT)] - [SDR SWAA2024042979360](https://openairdocs.org/sdr/SWAA2024042979360), Apr 26, 2024: SLIDER. CRACKED. L/H HORIZONTAL STAB UPPER FORWARD SLIDERL CRACKED<[01] R&R L/H HORIZONTAL STAB UPPER FORWARD SLIDER. IAW AMM 53-31-31 - [SDR SWAA2024040369286](https://openairdocs.org/sdr/SWAA2024040369286), Mar 31, 2024: GIRT BAR. LOOSE. L2 DOOR SLIDE GIRT BAR LOOSE ON ATTACHMENT<[01] RESECURED L2 DOOR SLIDE GIRT BAR REF AMM 25-66-01. NO FURTHER DEFECTS NOTED. - [SDR SWAA2024032567454](https://openairdocs.org/sdr/SWAA2024032567454), Mar 25, 2024: SLIDE. DETACHED. L2 DOOR SLIDE FELL OFF<[01] INSTALLED L2 DOOR SLIDE PER MT 725-61-06. A/C OK FOR SVC - [SDR SWAA2024013046014](https://openairdocs.org/sdr/SWAA2024013046014), Jan 28, 2024: SLIDE. OUT OF ADJUST. FORWARD SERVICE DOOR SLIDE PACK SAGGING<[01] DETERMINED SLIDE IS PROPERLY PACKED WITHOUT REMOVING SLIDE FROM DOOR. PER AMM 25-66-01 - [SDR SWAA2024011842008](https://openairdocs.org/sdr/SWAA2024011842008), Jan 17, 2024: LENS. DETACHED. CEILING EMERGENCY EXIT SIGN LENS DETACHED<[01] RE-ATTACHED EMERGENCY EXIT SIGN LENS COVER PER S.I.P. - [SDR SWAA2023120125523](https://openairdocs.org/sdr/SWAA2023120125523), Nov 28, 2023: PUMP. FAULTY. B ELEC HYDRAULIC PUMP CREATED A FLOOR VIBRATION AT MID CABIN FLOOR ASSOCIATED LOUD NOISE AS WELL. FLIGHT ATTENDANT REPORTED AN ELECTRICAL SMELL AT MID AND AFT C - [SDR SWAA2023090898067](https://openairdocs.org/sdr/SWAA2023090898067), Sep 8, 2023: SEAT. OUT OF ADJUST. PASSENGER CABIN: SEAT 11E RECLINES INTO THE EMERGENCY EXIT LANE.<[01] ADJUSTED HYDRO-LOCK PER AMM 25-22-00;[02] C/W INSPECTION PER AMM 25-22-00. - [SDR SWAA2023071978645](https://openairdocs.org/sdr/SWAA2023071978645), Jul 15, 2023: WIRE. SHORTED. AT CRUISE; HYDRAULIC B SYSTEM PRESSURE INDICATED ZERO AND THEN FLUCTUATED FROM 0 TO 1400. NO LIGHTS ILLUMINATED AND QUANTITY WAS 90%. FLAPS EXTENDED NORMALLY. N - [SDR SWAA2023031014446](https://openairdocs.org/sdr/SWAA2023031014446), Mar 9, 2023: MEGAPHONE. LOOSE. MEGA HONE HANDLE LOOSE WILL NOT TIGHTEN<[01] REPLACED MEGA-PHONE IAW 25-64-00 - [SDR SWAA2023030210409](https://openairdocs.org/sdr/SWAA2023030210409), Feb 27, 2023: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT BATTERY PACK M01675 L/H FWD ENTRY LIGHT IS INOP<[01] REMOVED AND REPLACED LH FWD EMERGENCY LIGHT BATTERY PACK M01675 IAW AMM 33-51-06-960-805.