# N481WN: 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: 29853 - Year built: 2004 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 1, 2004 - Certificate issued: September 28, 2004 - Expires: May 31, 2028 - Mode S code: A5EE51 - 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=481WN - Page: https://openairdocs.org/aircraft/N481WN 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/N481WN/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 DCA15CA050](https://openairdocs.org/ntsb/DCA15CA050), Dec 11, 2014: Boeing 737 7H4 (N481WN), San Jose, CA, no damage. Probable cause: an inadvertent encounter with convective turbulence during descent. ## FAA accident and incident reports None matched to N481WN. ## Service difficulty reports (317, 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 SWAA2026101391729](https://openairdocs.org/sdr/SWAA2026101391729), Oct 9, 2026: SLIDE. DISLODGED. OPS REPORTS FWD SERVICE DOOR SLIDE FELL OUT REINSTALLED FWD SERVICE DOOR SLIDE IAW MT 725-61-06. - [SDR SWAA2026080344267](https://openairdocs.org/sdr/SWAA2026080344267), Aug 2, 2026: SLIDE. LOW PRESSURE. AFT ENTRY SLIDE PRESSURE GAUGE SHOWING LOW. REMOVED AND REPLACED AFT ENTRY DOOR SLIDE PACK IAW AMM 25-66-00 AND MT 725-61-06. - [SDR SWAA2026070115636](https://openairdocs.org/sdr/SWAA2026070115636), Jun 25, 2026: BATTERY PACK. INOPERATIVE. MUTIPLE EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED; INSTALLED SERVICEABLE, AND PERFORMED OPS CHECK OF EMERGENCY LIGHT BATTERY PACKS M1672, M1673, AND M1675 IAW - [SDR SWAA2026070111069](https://openairdocs.org/sdr/SWAA2026070111069), Jun 11, 2026: ATTACH ANGLE. CRACKED. RIGHT VAPOR BARRIER ATTACH ANGLE CRACKED AT BS 663, RBL 25. REMOVED AND REPLACED RH VAPOR BARRIER UPPER ATTACH ANGLE AT BS 663 IAW SRM 51-40-02 AND BOEING DWG 1 - [SDR SWAA2026070117650](https://openairdocs.org/sdr/SWAA2026070117650), Jun 10, 2026: SUPPORT BEAM. DAMAGED. RIGHT WING TRAILING EDGE STRUCTURE; DEFLECTION CONTROL RIB AND SUPPORT BEAM ATTACHMENT. ELONGATED FASTENER HOLES NOTED. REPAIRED RIGHT WING TRAILING EDGE STRUCT - [SDR SWAA2026070111065](https://openairdocs.org/sdr/SWAA2026070111065), Jun 10, 2026: RIB. DAMAGED. RIGHT WING TRAILING EDGE STRUCTURE; DEFLECTION CONTROL RIB AND SUPPORT BEAM ATTACHMENT. ELONGATED FASTENER HOLES NOTED. REPAIRED RIGHT WING TRAILING EDGE STRUCT - [SDR SWAA2026033083879](https://openairdocs.org/sdr/SWAA2026033083879), Mar 27, 2026: LENS. MISSING. EXIT SIGN LENS AT EXIT ROW RIGHT MISSING. INSTALLED A NEW EXIT SIGN LENS IAW AMM 33-51-01. - [SDR SWAA2026020668358](https://openairdocs.org/sdr/SWAA2026020668358), Feb 5, 2026: SLIDE. LOOSE. ESCAPE SLIDE FRONT GALLEY DOOR LOOSE. REPACKED FWD SERVICE DOOR SLIDE IAW MT 725-61-06. - [SDR SWAA2025110330366](https://openairdocs.org/sdr/SWAA2025110330366), Oct 31, 2025: LIGHT. DIM. LEFT EMERGENCY EXIT LIGHT IS DIM ABOVE HATCH. R & R THE OVERWING SIDEWALL LIGHT AND LENS PER AMM 33-51-03. - [SDR SWAA2025110331272](https://openairdocs.org/sdr/SWAA2025110331272), Oct 31, 2025: LIGHT. DIM. LEFT EMERGENCY EXIT LIGHT IS DIM ABOVE HATCH. R & R THE OVERWING SIDEWALL LIGHT AND LENS PER AMM 33-51-03. - [SDR SWAA2025110330365](https://openairdocs.org/sdr/SWAA2025110330365), Oct 31, 2025: LIGHT. INOPERATIVE. RIGHT EMERGENCY EXIT LIGHT IS INOP ABOVE HATCH. R & R THE OVERWING SIDEWALL LIGHT AND LENS IAW AMM 33-51-03. - [SDR SWAA2025110331273](https://openairdocs.org/sdr/SWAA2025110331273), Oct 31, 2025: LIGHT. INOPERATIVE. RIGHT EMERGENCY EXIT LIGHT IS INOP ABOVE HATCH. R & R OVERWING SIDEWALL LIGHT AND LENS IAW AMM 33-51-03. - [SDR SWAA2025102025214](https://openairdocs.org/sdr/SWAA2025102025214), Oct 16, 2025: TRIM MOTOR. INOPERATIVE. ELECTRIC STABILIZER TRIM INOPERATIVE. ] R & R STAB TRIM MOTOR PER AMM 27-41-71 OPS CHECK GOOD. - [SDR SWAA2025030602135](https://openairdocs.org/sdr/SWAA2025030602135), Mar 5, 2025: HANDLE. CRACKED. AFT ENTRY DOOR ASSIST HANDLE IS CRACKED.<[01] R&R AFT ENTRY DOOR ASSIST HANDLE ATTACH FITTING IAW AMM 52-13-31.;[02] INSP IAW AMM 52-13-31 - [SDR SWAA2024080923909](https://openairdocs.org/sdr/SWAA2024080923909), Aug 8, 2024: ELEMENT. ARCED. LEFT SIDE SLIDING WINDOW HEATING ELEMENT ARC-ED. LASTED A FEW SECONDS WITH A STRONG SMELL. TURNED WINDOW HEAT OFF; NO CBS POPPED.<[01] REPLACED LT. NO. 2 OPENAB - [SDR SWAA2024080220366](https://openairdocs.org/sdr/SWAA2024080220366), Jul 31, 2024: SKIRT. OUT OF ADJUST. CUSTOMER WALK ITEMS / R2DOOR SLIDE SKIRT HANGS ON THRESHOLD WHEN DOOR OPERATED<[01] REPOSITION R2 DOOR ESCAPE SLIDE SKIRT AS PER WORK INSTRUCTIONS 725-61-06;[02 - [SDR SWAA2024080220362](https://openairdocs.org/sdr/SWAA2024080220362), Jul 31, 2024: BULB. INOPERATIVE. CUSTOMER WALK ITEMS/ 1 EA BULB BURNED OUT ON EMER EXIT SIGN ABOVE R2 DOOR<[01] RE-LAMPED 1 LAMP ON EMERGENCY EXIT SIGN ABOVE R2 DOOR AS PER AMM REF 33-51-01-960 - [SDR SWAA2024080220363](https://openairdocs.org/sdr/SWAA2024080220363), Jul 31, 2024: SLIDE. OUT OF ADJUST. CUSTOMER WALK ITEMS / L2 DOOR SLIDE SKIRT HANGS ON THRESHOLD WHEN DOOR OPERATED<[01] REPOSITION L2 DOOR ESCAPE SLIDE SKIRT AS PER WORK INSTRUCTIONS 725-61-06;[0 - [SDR SWAA2024080518605](https://openairdocs.org/sdr/SWAA2024080518605), Jul 29, 2024: SKIN. CRACKED. R1 DOOR FWD CUTOUT PANEL CRACKED AT LOWER SECTION<[01] REPAIRED R1 DOOR FWD CUTOUT PANEL AT LOWER SECTION AS PER B737 AMM 25-00-00-300-802.;[02] VERIFIED STEP 1 - [SDR SWAA2024080217837](https://openairdocs.org/sdr/SWAA2024080217837), Jul 27, 2024: LIGHT. INOPERATIVE. L/H AFTER WING EXTERIOR EMERGENCY LIGHT INOPERATIVE.<[01] TROUBLESHOT INOPERATIVE L/H AFT WING EMERGENCY LIGHT (L547) REF B737 FIM 33-50 TASK 801; REMOVED AND R - [SDR SWAA2024080217840](https://openairdocs.org/sdr/SWAA2024080217840), Jul 27, 2024: LIGHT. INOPERATIVE. L2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE.<[01] REPLACED LAMP AT L2 DOOR EXTERIOR EMERGENCY LIGHT (L732) IN REF WITH B737 AMM 33-51-04-960-801.LAMP TEST NORM - [SDR SWAA2024080217116](https://openairdocs.org/sdr/SWAA2024080217116), Jul 26, 2024: SIGN. INOPERATIVE. L1 DOOR LINER EMERGENCY EXIT SIGN INOP<[01] FOUND CONNECTOR D2972 FOR EXIT LIGHT NOT PROPERLY SEATED; RESEAT I/A/W BOEING WDM 33-51-12; PERFORMED OPS CHECK OF E - [SDR SWAA2024080515287](https://openairdocs.org/sdr/SWAA2024080515287), Jul 22, 2024: SCUFF PLATE. CRACKED. **REJECTION** DURING OK TO CLOSE FOUND AFT CARGO SCUFF PLATE AFT CORNER CRACKED MKD (107-001)<[01] RECEIVED AFT CARGO SCUFF PLATE AFT CORNER P;O 2074280 WILL BE - [SDR SWAA2024080514751](https://openairdocs.org/sdr/SWAA2024080514751), Jul 20, 2024: COVER. CRACKED. RIGHT WING O/B AFT FLAP AT #6 CUT OUT EDGE COVER CRACKED<[01] REMOVED AND REPLACED RIGHT WING O/B AFT FLAP AT #6 CUT OUT EDGE COVER B737 SRM-51-40-02-0G-0 DWG#1 - [SDR SWAA2024080511465](https://openairdocs.org/sdr/SWAA2024080511465), Jul 11, 2024: CHANNEL. CORRODED. FOUND CHANNEL TIE WITH PITTING CORROSION AT E&E COMP INTERNAL SIDE STA 351.2+8 BL0<[01] REMOVED; FABRICATED AND INSTALLED NEW CHANNEL TIE AT SKIN BS 351.2+8 BL - [SDR SWAA2024080511464](https://openairdocs.org/sdr/SWAA2024080511464), Jul 11, 2024: SUPPORT. WORN. KEEL BEAM UNDER WING-TO-BODY FAIRING PANEL 192E HAS SUPPORT WITH FRETTING AT STA 600. 8-48<[01] REMOVED AND INSTALLED NEW SUPPORT AT KEEL BEAM UNDER WING-TO-BOD - [SDR SWAA2024080510312](https://openairdocs.org/sdr/SWAA2024080510312), Jun 29, 2024: PANEL. CRACKED. L/W LOWER LEADING-EDGE PANEL#521XB HAS SCREW HOLE CRACKED. 8-46<[01] APPLIED PERMANENT REPAIR ON DAMAGE AREA AS MARKED ON PANEL #521XB AS PER B737 SRM 51-70-04- - [SDR SWAA2024080505912](https://openairdocs.org/sdr/SWAA2024080505912), Jun 26, 2024: CHANNEL. CORRODED. CORROSION SPOT IN E&E AT SKIN BS 351.2+6 BL O. 8-25<[01] REMOVED; FABRICATED AND INSTALLED NEW CHANNEL AT SKIN BS 351.2+6 BL 0 PER REF SRM 51-40-02-0G-0 AND DWG - [SDR SWAA2024080505749](https://openairdocs.org/sdr/SWAA2024080505749), Jun 26, 2024: RIB. CRACKED. LEFT HORIZONTAL STABILIZER L/E PANEL RIB # 2 CRACK.<[01] REMOVED CRACKED RIB #2 AT LEFT HORIZONTAL STABILIZER L/E PER B737-700 SRM 51-40-02-0G-0. LOCATED AND DR - [SDR SWAA2024080505750](https://openairdocs.org/sdr/SWAA2024080505750), Jun 26, 2024: RIB. CRACKED. LEFT HORIZONTAL STABILIZER L/E PANEL RIB # 3 CRACK.<[01] LOCATED AND DRILLED NEW RIB #3 AT LEFT HORIZONTAL STABILIZER L/E PER B737-700 SRM 51-40-05-0G-0 AND DWG - [SDR SWAA2024080506177](https://openairdocs.org/sdr/SWAA2024080506177), Jun 26, 2024: ANGLE. CRACKED. RH HORIZONTAL STAB PANEL 343 BLADE SEAL RETAINER CRACK. RH HORIZONTAL STAB PANEL 343AB BLADE SEAL RETAINER CRACK.<[01] REMOVED AND REPLACED RH HORIZONTAL STAB P - [SDR SWAA2024080505743](https://openairdocs.org/sdr/SWAA2024080505743), Jun 25, 2024: BRACKET. CRACKED. AFT OF AFT CARGO COMPARTMENT BILGE FLOOR SUPPORT BRACKET CRACKED @ AFT END FWD OF WATER TANK STA 947.75 S-26L MKD DOT<[01] INSTALLED BRACKETED AT AFT CARGO COMP - [SDR SWAA2024080505748](https://openairdocs.org/sdr/SWAA2024080505748), Jun 25, 2024: FLOOR PANEL. PEELING. CENTER CABIN FLOOR PANEL 241BF HAS UPPER SURFACE LAYER FIBERS PEELED AND 3EA EXISTING REPAIRS. 124-002<[01] RECEIVED NEW PANEL # 241BF ; INSTALLATION WILL BE AC - [SDR SWAA2024080505746](https://openairdocs.org/sdr/SWAA2024080505746), Jun 25, 2024: GUSSET. CRACKED. FWD CARGO COMPARTMENT GAUSET CRACKED AT S-21R STA 500D MKD DOT<[01] REMOVED GAUSET AT S-21R STA 500D PER SRM 51-40-02-0G-0; LOCATED AND DRILLED NEW PART PER SRM - [SDR SWAA2024080505742](https://openairdocs.org/sdr/SWAA2024080505742), Jun 25, 2024: PLATE. CRACKED. FWD CABIN L-1 DOOR CUTOUT AFT JAMB LOWER INB COVER PLATE APPEARS CRACKED @ LOWER HOLE STA 348.2 MKD DOT<[01] PERFORMED HFEC INSP. ON SUSPECTED CRACK IAW B737 ND - [SDR SWAA2024080205747](https://openairdocs.org/sdr/SWAA2024080205747), Jun 25, 2024: FLOOR PANEL. PEELING. CENTER CABIN FLOOR PANEL 231YF HAS UPPER SURFACE LAYER FIBERS PEELED. 124-001<[01] RECEIVED NEW PANEL # 231YF INSTALLATION WILL BE ACCOMPLISH ON # TTG8Q00TNY32; - [SDR SWAA2024080205552](https://openairdocs.org/sdr/SWAA2024080205552), Jun 25, 2024: SHIELD. CORRODED. CORROSION** FWD CARGO COMPARTMENT FLOOR SUPPORT SHIELD @ S-26R STA 500 TO 500A MKD DOT<[01] REMOVED FWD CARGO COMPARTMENT FLOOR SUPPORT SHIELD AT S-26R FROM STA - [SDR SWAA2024073105745](https://openairdocs.org/sdr/SWAA2024073105745), Jun 25, 2024: GUSSET. CRACKED. FWD CARGO COMPARTMENT GUSSET CRACKED AT S-19R STA 500D MKD DOT<[01] REMOVED GUSSET AT S-19R STA 500D PER SRM 51-40-02-0G-0; LOCATED AND DRILLED NEW PART PER SRM - [SDR SWAA2024073105744](https://openairdocs.org/sdr/SWAA2024073105744), Jun 25, 2024: GASKET. CRACKED. FWD CARGO COMPARTMENT GAUSET CRACKED AT S-19L STA 500D MKD DOT<[01] REMOVED GAUSET AT S-19L STA 500D PER SRM 51-40-02-0G-0; LOCATED AND DRILLED NEW PART PER SRM - [SDR SWAA2024073005544](https://openairdocs.org/sdr/SWAA2024073005544), Jun 25, 2024: DOUBLER. CORRODED. CORROSION ** AFT CARGO COMPARTMENT BILGE SKIN PREVIOUS DOUBLER REPAIR @ S-26R STA 807+5' MKD DOT<[01] ACCOMPLISHED REPAIR PER EA -24-153-01888 AT AFT CARGO COMP - [SDR SWAA2024072911624](https://openairdocs.org/sdr/SWAA2024072911624), Jun 25, 2024: PANEL. CRACKED. RIGHT VERTICAL FIN PANEL#323AR ASSY SUPPORT ANGLE LOWER SURFACE HAS BARE METAL. RIGHT VERTICAL FIN PANEL#323AR ASSY CRACKED AT LOWER CORNER<[01] RECEIVED NEW PA - [SDR SWAA2024080505136](https://openairdocs.org/sdr/SWAA2024080505136), Jun 24, 2024: LINKAGE. CORRODED. CORROSION ** L/H RAM AIR INLET FWD DOOR ACTUATING ROD LOWER LINK MKD DOT<[01] REMOVED AND REPLACED L/H RAM AIR INLET FWD DOOR ACTUATING ROD LOWER LINK AS PER AM - [SDR SWAA2024080505137](https://openairdocs.org/sdr/SWAA2024080505137), Jun 24, 2024: FLOOR SUPPORT. CRACKED. AFT OF FWD CARGO COMPARTMENT INTERCOSTAL SUPPORT CRACKED @ AFT END BETWEEN STA 500D AND 520 S-25R<[01] REMOVED FWD CARGO COMPARTMENT INTERCOSTAL SUPPORT BETWEEN - [SDR SWAA2024080505009](https://openairdocs.org/sdr/SWAA2024080505009), Jun 23, 2024: SCUFF PLATE. CRACKED. AFT CARGO COMPARTMENT AFT SCUFF PLATE CRACKED<[01] REPAIRED PART 'AFT CARGO AFT SCUFF PLATE' RECEIVED AND WILL BE INSTALLED ON CARD: TTG8Q00229WY;[02] VERIFIED - [SDR SWAA2024080507976](https://openairdocs.org/sdr/SWAA2024080507976), Jun 23, 2024: SUPPORT. CRACKED. MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK CRACKED AT LBL 1 STA 540<[01] REVOVED AND REPLACED PANEL BREAK AT MAIN CABIN CENTER SECTION; STA 540; LBL 1 AS PER - [SDR SWAA2024080504869](https://openairdocs.org/sdr/SWAA2024080504869), Jun 23, 2024: SUPPORT. CRACKED. MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK CRACKED AT RBL 1 STA 540<[01] REMOVED AND REPLACED PANEL BREAK AT MAIN CABIN CENTER SECTION; STA 540; RBL 1 AS PER - [SDR SWAA2024080505003](https://openairdocs.org/sdr/SWAA2024080505003), Jun 23, 2024: ANGLE. CRACKED. LOWER FUS CENTER SECTION ATTACHED ANGLE CRACKED @ RAM AIR EXIT EXHAUST DUCT CUTOUT SEAL O/B LOWER CORNER MKD DOT<[01] REMOVED AND INSTALLED ANGLE AT LOWER FUS C - [SDR SWAA2024080504866](https://openairdocs.org/sdr/SWAA2024080504866), Jun 23, 2024: SKIN. DELAMINATED. L/W OUB AFT FLAP INB END LOWER SURFACE DELAMINATION AROUND PREVIOUS REPAIR MKD DOT<[01] REMOVE AND REPLACED L/W OUB AFT FLAP AS PER AMM 27-51-22-000-801 AND 27- - [SDR SWAA2024080505006](https://openairdocs.org/sdr/SWAA2024080505006), Jun 23, 2024: PANEL. ELONGATED. L/W REAR SPAR LOWER FIXED T/E PANEL 551GB INB AFT SUPPORT ROD LOWER ATTACHED FITTING ELONGATED HOLE MKD DOT<[01] REMOVED AND REPLACED L/W REAR LSPAR LOWER FIXED - [SDR SWAA2024080504309](https://openairdocs.org/sdr/SWAA2024080504309), Jun 21, 2024: PANEL. CORRODED. PANEL 192F HAS FLAME SPRAY CORRODED AT ANTENNA MOUNT AREA. 8-22<[01] RECIEVED NEW PANEL. WORK WILL BE ACCOMPLISHED ON TTG8Q00U3UBG;[02] CORRECTION TO STEP 1: