# N205WN: 2005 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: 34010 - Year built: 2005 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 14, 2005 - Certificate issued: March 23, 2005 - Expires: December 31, 2029 - Mode S code: A1A697 - 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=205WN - Page: https://openairdocs.org/aircraft/N205WN 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/N205WN/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 N205WN. ## FAA accident and incident reports None matched to N205WN. ## Service difficulty reports (315, 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 SWAA2026081189738](https://openairdocs.org/sdr/SWAA2026081189738), Aug 7, 2026: BATTERY PACK. NO TEST. FLIGHT DECK POWER SUPPLY, BATTERY PACK M1673 FAILED A CAPACITY TEST. R & R THE BATTERY PACK M1673 IAW AMM 33-51-06. - [SDR SWAA2026081170250](https://openairdocs.org/sdr/SWAA2026081170250), Aug 7, 2026: BATTERY PACK. NO TEST. FLIGHT DECK, POWER SUPPLY, BATTERY PACK M1672 FAILED A CAPACITY TEST. R & R BATTERY PACK M1672 IAW AMM 33-51-06. - [SDR SWAA2026081142051](https://openairdocs.org/sdr/SWAA2026081142051), Aug 7, 2026: SEAT TRACK. WORN. FLIGHT DECK, CAPTAIN`S AFT INBD SEAT TRACK WORN TO BEYOND LIMITS. R & R THE SEAT TRACK IAW AMM 25-11-11. - [SDR SWAA2026073043492](https://openairdocs.org/sdr/SWAA2026073043492), Jul 26, 2026: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS COMMON TO RT OVERWING EXIT INOP REPLACED CHARGER AND BATTERY PACK ASSEMBLY FOR EMERGENCY LIGHTS COMMON TO RT OVERWING EXIT PER AMM 33-51-06. OP - [SDR SWAA2026070718713](https://openairdocs.org/sdr/SWAA2026070718713), Jul 4, 2026: SLIDE. DISLODGED. FWD SERVICE DOOR ESCAPE SLIDE FELL OUT OF ITS COMPARTMENT WHEN DOOR WAS OPENED. REPACKED IAW MT 725-61-06 - [SDR SWAA2026051195707](https://openairdocs.org/sdr/SWAA2026051195707), May 5, 2026: SLIDE. OUT OF ADJUST. R1 DOOR SLIDE FELL OUT OF THE COMPARTMENT. REMOVED SLIDE FROM CASE IAW 25-66-01; FOUND LEFT LADDER TIE AND BONDING JUMPER LOCKING PIN MISSING FROM CASE. REF PRE - [SDR SWAA2026050895708](https://openairdocs.org/sdr/SWAA2026050895708), May 5, 2026: SLIDE. OUT OF ADJUST. R1 DOOR SLIDE FELL OUT OF THE COMPARTMENT. RE-INSTALLED LOCK COVER PIN ON R1 DOOR SLIDE COVER AND PROPERLY REPOSITIONED SLIDE AND COVER; REF AMM 25-66-01. C/W M - [SDR SWAA2025123157028](https://openairdocs.org/sdr/SWAA2025123157028), Dec 30, 2025: FSEU. FAULTY. ENCOUNTERED TRAILING EDGE FLAP ASSYMETRY; RAN QRH FOR T.E. ASSEMETRY; LANDED WITH LEADING EDGE FLAPS AND SLATS; FULL EXTEND. VRG TARGET 167; 174 ON SPEED LANDIN - [SDR SWAA2025111333732](https://openairdocs.org/sdr/SWAA2025111333732), Nov 11, 2025: RIB. CRACKED. LEFT WING DEFLECTION CONTROL TAB, RIB CRACKED APPROX 2 FROM AFT EDGE. COMPLETED STEPS UP TO AND INCLUDING STEP 4.P OF LT WING INBD FIXED TE DEFLECTION CONTROL R - [SDR SWAA2025040720838](https://openairdocs.org/sdr/SWAA2025040720838), Apr 1, 2025: COVER. DETACHED. R/H EMERGENCY EXIT COVER FELL OFF OF WALL<[01] R&R?D RT EMERGENCY EXIT LIGHT ASSY REF AMM 33-51-01; WDM 33-51-13 - [SDR SWAA2025032608867](https://openairdocs.org/sdr/SWAA2025032608867), Mar 24, 2025: HANDLE. LOOSE. AFT AED ASSIST HANDLE LOOSE<[01] TIGHTENED AND SECURED AFT ENTRY DOOR ASSIST HANDLE IAW AMM 52-13-31-400-802. STEP G. (2).;[02] VERIFIED CORRECTIVE ACTION 1 - [SDR SWAA2025032608868](https://openairdocs.org/sdr/SWAA2025032608868), Mar 24, 2025: HANDLE. LOOSE. FSD ASSIST HANDLE LOOSE<[01] TIGHTENED AND SECURED AFT ENTRY DOOR ASSIST HANDLE IAW AMM 52-41-31-400-802. STEP G. (2).;[02] CORRECTION: TIGHTENED AND SECURED FS - [SDR SWAA2025032608437](https://openairdocs.org/sdr/SWAA2025032608437), Mar 23, 2025: ELEC CONNECTOR. DISCONNECTED. EMERGENCY AISLE LIGHT ON STOW BIN 1L IS INOP<[01] FOUND CONNECTOR D11344 DISCONNECTED FROM D11088 ON TOP OF STOW BIN 1L. RECONNECTED CONNECTOR D11344 TO D11088 - [SDR SWAA2025032608381](https://openairdocs.org/sdr/SWAA2025032608381), Mar 22, 2025: DOUBLER. CRACKED. EXTERNAL GROUND POWER RECEPTACLE CUTOUT DOUBLER IS CRACKED AT AFT SIDE<[01] REPAIRED EXTERNAL GROUND POWER RECEPTACLE CUT OUT IAW SRM 53-10-15-2R-4 REPAIR 4.;[0 - [SDR SWAA2025032606182](https://openairdocs.org/sdr/SWAA2025032606182), Mar 17, 2025: LAMP. INOPERATIVE. EMERGENCY ASILE LIGHT AT ROW 9 ABC DOES NOT ILLUMINATE<[01] RELAMPED AND PERFORMED GOOD OPS CHECK OF EMERGENCY AISLE LIGHT AT ROW 9 ABC PER AMM 33-51-03-960-801 - [SDR SWAA2025032606309](https://openairdocs.org/sdr/SWAA2025032606309), Mar 17, 2025: LAMP. INOPERATIVE. R/H SLIDE/OVERWING LIGHT INOP R/H EMERGENCY EXIT SLIDE/OVERWING LIGHT INOP<[01] ALL ACTIONS COMPLETED FOR CC# TTG8Q00ZB2FB;[02] RELAMPED R/H EMERGENCY EXIT SLID - [SDR SWAA2025032601728](https://openairdocs.org/sdr/SWAA2025032601728), Mar 4, 2025: LIGHT. BROKEN. SIDEWALL PANEL 231YHW EMERGENCY EXIT LIGHT ASSEMBLY IS BROKEN<[01] REPLACED SIDEWALL PANEL 231YHW EMERGENCY EXIT LIGHT ASSEMBLY IAW AMM 33-51-01-960-802. STEP 1 - [SDR SWAA2025032601729](https://openairdocs.org/sdr/SWAA2025032601729), Mar 4, 2025: LIGHT. BROKEN. SIDEWALL PANEL 232YHW EMERGENCY EXIT LIGHT ASSEMBLY IS BROKEN<[01] REPLACED SIDEWALL PANEL 232YHW EMERGENCY EXIT LIGHT ASSEMBLY IAW AMM 33-51-01-960-802. STEP 1 - [SDR SWAA2025032600484](https://openairdocs.org/sdr/SWAA2025032600484), Feb 27, 2025: SEAL. CRACKED. PANEL 333AT SLIDE SEAL (SHARK FIN) CRACKED (MARKED).<[01] REMOVED AND REPLACED HORIZ STAB GAP PANEL 333AT SLIDE SEAL IAW SRM 51-40-02-0G-0 STEP 4 AND FIG 8; MM - [SDR SWAA2025032699652](https://openairdocs.org/sdr/SWAA2025032699652), Feb 26, 2025: WEB. CORRODED. CORROSION ON AFT CARGO BAY DOOR SUB THRESHOLD WEB AT MULTIPLE PLACES<[01] REMOVED AND REPLACED AFT CARGO BAY DOOR SUB THRESHOLD WEB I.A.W SRM 51-40-02-0G-0 AND - [SDR SWAA2025032600090](https://openairdocs.org/sdr/SWAA2025032600090), Feb 26, 2025: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL AT FWD CABIN BS295.5 S-16L WL216.<[01] REMOVED AND REPLACED INTERCOSTAL AT FWD CABIN BS295.5 S-16L WL216 I.A.W SRM 51-40-02-0G-0 AND DWG 141 - [SDR SWAA2025032699650](https://openairdocs.org/sdr/SWAA2025032699650), Feb 26, 2025: SIDEWALL SUPPORT. CORRODED. CORROSION ON FLOOR TO SIDEWALL SUPPORT STA 727A; 727C; 727D+10; 727E; 767; RBL 25<[01] REMOVED AND REPLACED AT ACB FLOOR TO SIDEWALL SUPPORT BETWEEN BS.727+4' - - [SDR SWAA2025032699651](https://openairdocs.org/sdr/SWAA2025032699651), Feb 26, 2025: SIDEWALL SUPPORT. CORRODED. CORROSION ON LH FLOOR TO SIDEWALL SUPPORT STA 727C+10; 727D+10; 747+12; 767; 787+10; LBL 25<[01] REMOVED AND REPLACED ACB LH FLOOR TO SIDEWALL SUPPORT FROM STA - [SDR SWAA2025032699648](https://openairdocs.org/sdr/SWAA2025032699648), Feb 25, 2025: STRAP. CRACKED. CRACKED FASTENER HOLE FOUND AT LH BS639 STUB BEAM STRAP; AFT LOWER HOLE; O/B TITANIUM LAYER; PROPAGATING IN THE AFT DIRECTION.<[01] 'REFER TO EA 25-153-00450 WH - [SDR SWAA2025032699647](https://openairdocs.org/sdr/SWAA2025032699647), Feb 25, 2025: STRAP. CRACKED. CRACKED FASTENER HOLE FOUND AT RH BS639 STUB BEAM STRAP; AFT LOWER HOLE; O/B TITANIUM LAYER; PROPAGATING IN THE AFT DIRECTION.<[01] 'REFER TO EA 25-153-00450 WH - [SDR SWAA2025032699202](https://openairdocs.org/sdr/SWAA2025032699202), Feb 25, 2025: SEAT TRACK. CORRODED. CORROSION ON LBL 45 SEAT TRACK WELL AT STA: 480+16; 500A+8; 500B+18; 500C+9; 500D+10; WL 208.5<[01] SEAT TRACK BS 480 - BS520 WILL BE REPLACED BY CUSTOMER CARD - [SDR SWAA2025032607904](https://openairdocs.org/sdr/SWAA2025032607904), Feb 21, 2025: STRAP. CRACKED. CUSTOMER REQUEST: LH AND RH BS 639 STUB BEAM STRAP VALIDATION OF 737-53A1404. OPEN HOLE INSPECTION<[01] 'INSPECTION VALIDATION AND REPLACEMENT OF CRACKED PARTS - [SDR SWAA2025032698415](https://openairdocs.org/sdr/SWAA2025032698415), Feb 21, 2025: SIGN. DAMAGED. AFT ENTRY CEILING EXIT LIGHT HOUSING DAMAGED<[01] REMOVED AND REPLACED A NEW AFT ENTRY PANEL EXIT SIGN LIGHT ASSEMBLY IAW AMM 33-51-01-960-802.
OPS CHECK; OK - [SDR SWAA2025032698115](https://openairdocs.org/sdr/SWAA2025032698115), Feb 20, 2025: SEAL. CRACKED. RT HORIZONAL STAB FWD UPPER SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED RT HORIZONTAL STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-400-802.;[02] VERIFIED CORREC - [SDR SWAA2025032698114](https://openairdocs.org/sdr/SWAA2025032698114), Feb 20, 2025: SEAL. CRACKED. LT HORIZONAL STAB FWD UPPER SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED LT HORIZONTAL STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-400-802.;[02] VERIFIED CORREC - [SDR SWAA2025032697721](https://openairdocs.org/sdr/SWAA2025032697721), Feb 19, 2025: SKIN. CRACKED. CRACK ON RH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 18' FROM FWD EDGE; .35' IN LENGTH (MARKED)<[01] REMOVED THE DAMAGED PART ON RH HORIZONTAL STAB - [SDR SWAA2025032697507](https://openairdocs.org/sdr/SWAA2025032697507), Feb 19, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 242DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR P - [SDR SWAA2025032697502](https://openairdocs.org/sdr/SWAA2025032697502), Feb 19, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 232RF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 232RF FLOOR PANEL HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR - [SDR SWAA2025032697503](https://openairdocs.org/sdr/SWAA2025032697503), Feb 19, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 232SF FLOOR PANEL HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR - [SDR SWAA2025032697504](https://openairdocs.org/sdr/SWAA2025032697504), Feb 19, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 241AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00 - [SDR SWAA2025032697505](https://openairdocs.org/sdr/SWAA2025032697505), Feb 19, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 241DF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00 - [SDR SWAA2025032697506](https://openairdocs.org/sdr/SWAA2025032697506), Feb 19, 2025: FLOOR PANEL. PULLED. FLOOR PANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 242AF FLOOR PANEL HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR - [SDR SWAA2025032697725](https://openairdocs.org/sdr/SWAA2025032697725), Feb 19, 2025: SIDEWALL SUPPORT. CORRODED. FCB - MULTIPLE CORROSION SPOT ON SIDEWALL SUPPORT BS 500A+6; BS 500A+10 BS 500A+14; BS 500C+1.5; BS 500C+7 RBL 23.5 WL 156 (MARKED)<[01] REMOVED AND REPLACED SI - [SDR SWAA2025032697726](https://openairdocs.org/sdr/SWAA2025032697726), Feb 19, 2025: SHIELD. CORRODED. FCB - MULTIPLE CORROSION SPOT ON AFT SHIELD BS 480+18; BS 500+2 BS 500+6; BS 500+10 RBL 24.75 WL 156 (MARKED)<[01] REMOVED AND REPLACED AT FCB AFT SHIELD BETWEE - [SDR SWAA2025032697727](https://openairdocs.org/sdr/SWAA2025032697727), Feb 19, 2025: WEB. CORRODED. FCB - CORROSION ON THRESHOLD WEB BS 480+1 RBL 29 (MARKED)<[01] REMOVED AND REPLACED AT FCB SUB-THRESHOLD WEB BETWEEN BS.440 - BS 492.4 RBL29 WL 156 IAW B-737-70 - [SDR SWAA2025032697720](https://openairdocs.org/sdr/SWAA2025032697720), Feb 19, 2025: SIDEWALL SUPPORT. CORRODED. FCB - MULTIPLE CORROSION SPOT ON SIDEWALL SUPPORT BS 500+6.5; BS 500+14 BS 500A+10; BS 500B+2; BS 500+7 LBL 23.5 WL 156 (MARKED)<[01] REMOVED AND REPLACED SIDEW - [SDR SWAA2025032697070](https://openairdocs.org/sdr/SWAA2025032697070), Feb 17, 2025: SCUFF PLATE. CRACKED. ACB FWD CORNER SCUFF PLATE CRACKED<[01] ALL STEPS COMPLETED;[02] REPAIRED ACB FWD CORNER SCUFF PLATE PER SRM 53-60-12-2R-1. TASK CARD COMPLETED.;[03] VERIFIED C - [SDR SWAA2025032696277](https://openairdocs.org/sdr/SWAA2025032696277), Feb 14, 2025: LAMP. INOPERATIVE. EMERGENCY AREA LIGHT AT SEATROW 13 FED IS INOP.<[01] RELAMPED AND PERFORMED GOOD OPS CHECK OF EMERGENCY AREA LIGHT AT SEATROW 13 FED PER AMM 33-51-03-960-801
OPS CHECK GOOD
I/A/W AMM 33-51-06-960-805;[0 - [SDR SWAA2024092741463](https://openairdocs.org/sdr/SWAA2024092741463), Sep 25, 2024: STRAP. DAMAGED. FWD ENTRY DOOR ACCORDION STRAP STRETCHED<[01] 01 - REMOVED AND REPLACED PER [AMM INTRODUCTION-NG (USE OF STANDARD INDUSTRY PRACTICES - SIP - PERMANENT)] - [SDR SWAA2024080219842](https://openairdocs.org/sdr/SWAA2024080219842), Jul 30, 2024: BATTERY PACK. INOPERATIVE. BOTH L AND R OVER WING GROUND AND 2 LEFT AISLE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT M1670 IAW AMM 33-51-06. OPS CHECK GOOD. - [SDR SWAA2024052086414](https://openairdocs.org/sdr/SWAA2024052086414), May 16, 2024: LIGHT. FAILED. R/H EXTERIOR OVERWING EMERGENCY LIGHT OUT.<[01] R&R R/H EXTERIOR OVERWING EMERGENCY LIGHT; OPS CHECK NORMAL I/A/W AMM 33-51-04. - [SDR SWAA2024050781903](https://openairdocs.org/sdr/SWAA2024050781903), May 3, 2024: ISOLATOR. CRACKED. AFT ENTRY DOOR FWD SLIDE MOUNT UPPER AND LWR ISOLATORS CRACKED<[01] R&R AFT ENTRY DOOR FWD SLIDE MOUNT UPPER AND LWR ISOLATORS IAW SRM 51-40-02. - [SDR SWAA2024041774916](https://openairdocs.org/sdr/SWAA2024041774916), Apr 15, 2024: CIRCUIT BREAKER. TRIPPED. INFO ONLY: FOUND EMERGENCY PANEL LIGHT CB TRIPPED ON PREFLT; CONTACTED MOC DAVE. NO 10 DAYS HISTORY. PERFORMED ONE TIME RESERT OF TRIPPED CB D-8 ON PANEL 16-3. - [SDR SWAA2024010437118](https://openairdocs.org/sdr/SWAA2024010437118), Jan 2, 2024: SLIDE. LOW PRESSURE. FWD DOOR SLIDE PRESSURE BAND NOT IN THE GREEN<[01] REMOVED AND REPLACED L1 DOOR SLIDE IAW MM 25-66-00 AND MT 725-61-06 All 315: https://openairdocs.org/aircraft/N205WN/reports.md ## STCs that may be installed (OpenAirDocs) (37) Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do. ### Approved for the airframe (Boeing 737-7H4) - [STC ST00555AT](https://openairdocs.org/stc/ST00555AT): Installation of Airshow 210 system. AIRCRAFT RECONFIG TECHNOLOGIES, LLC. Lists 737 Series - [STC SA4842SW](https://openairdocs.org/stc/SA4842SW): Modification of air to air heat exchanger (P/N 182820-2 Series 2). Honeywell International Inc. Lists 737 Series - [STC SA270NW](https://openairdocs.org/stc/SA270NW): Installation of modified seat. Aviation Technical Services. Lists 737 Series - [STC ST01162NY](https://openairdocs.org/stc/ST01162NY): Installation of Literature Pockets. Magee Plastics Company. Lists 737 Series - [STC SA2607SO](https://openairdocs.org/stc/SA2607SO): Installation of coffee maker P/N 416-1001-29. B/E Aerospace Inc. Lists 737 Series - [STC SA2608SO](https://openairdocs.org/stc/SA2608SO): Installation of rail assembly, P/N 416-0201-15. B/E Aerospace Inc. Lists 737 Series - [STC SA3058SO](https://openairdocs.org/stc/SA3058SO): Installation of coffee maker 416-0001-23 and rail assembly 416-0201-5. B/E Aerospace Inc. Lists 737 Series - [STC ST01476AT](https://openairdocs.org/stc/ST01476AT): Installation of coffee maker. B/E Aerospace Inc. Lists 737 Series - [STC ST01778AT](https://openairdocs.org/stc/ST01778AT): Installation of espresso maker p/n 3510-0066-01. B/E Aerospace Inc. Lists 737 Series - [STC SA629GL](https://openairdocs.org/stc/SA629GL): Installation of Grimes galley, Model 1545LW unit 2 and unit 4. B/E Aerospace. Lists 737 Series - [STC ST01332AT](https://openairdocs.org/stc/ST01332AT): Installation of Galley Service Carts. Champ International, Inc. Lists 737 Series - [STC ST09870SC](https://openairdocs.org/stc/ST09870SC): Installation of Mechanical Window Shades. Lou Martin & Associates. Lists 737 Series - [STC ST00033AT](https://openairdocs.org/stc/ST00033AT): Installation of a single Mode S system and provisions for a TCAS II system. General Aerospace, Inc. Lists 737 Series - [STC SA4532NM](https://openairdocs.org/stc/SA4532NM): Installation of Coltech, CTD-80 ATSCALL, enabling company calling of selected aircraft via company selected radio. Avtech Corporation. Lists 737 Series - [STC ST4532NM](https://openairdocs.org/stc/ST4532NM): Installation of Coltech CTD-80 ATSCALL, enabling company calling of selected aircraft via company selected radio. Avtech Corporation. Lists 737 Series - [STC ST00774NY](https://openairdocs.org/stc/ST00774NY): Installation of a passenger cabin Liquor/beverage service cart P/N E500170. (757-222) (767-222) (727-222) (737 SERIES 222, 291, 322, 522) (747-100 SERIES 238B). Driessen Aircraft Interior Systems USA, Inc. Lists 737 Series - [STC ST02052AT](https://openairdocs.org/stc/ST02052AT): Installation of a single Collins GNLU910A flight management system, along with global navigation satellite system sensor. General Aerospace, Inc. Lists 737 Series - [STC SA02034AT](https://openairdocs.org/stc/SA02034AT): Manufacture of tray carrier, P/N 2282-506. BFE Services. Lists 737 Series - [STC ST01968AT](https://openairdocs.org/stc/ST01968AT): Manufacture of inserts for galley stowage. JK Aerospace, Inc. Lists 737 Series - [STC SA01916AT](https://openairdocs.org/stc/SA01916AT): Manufacture of Tray Carrier P/N 1839-501. BFE Services. Lists 737 Series - [STC SA2534SO](https://openairdocs.org/stc/SA2534SO): Installation of window shades, acoustic panes and reveals. Magee Plastics Company. Lists 737 Series - [STC ST179CH](https://openairdocs.org/stc/ST179CH): Installation of cargo container curtain. Plastic Composites Corp. Lists 737 Series - [STC SA00056LA](https://openairdocs.org/stc/SA00056LA): Installation of Weber Coffeemaker, P/N 870130-415. Monogram Systems. Lists 737 Series - [STC SA6090NM](https://openairdocs.org/stc/SA6090NM): Installation of emergency vision assurance system (EVAS). VisionSafe Corporation. Lists 737 Series - [STC SA370NW](https://openairdocs.org/stc/SA370NW): Removal of passenger interior, installation of cargo compartment liners and cargo tie down equipment. Western Metal Products. Lists 737 Series - [STC SA2589CE](https://openairdocs.org/stc/SA2589CE): Install Bennetts Seat Converter Stowage Compartment on passenger seat(s). John's Aircraft and Upholstery. Lists 737 Series - [STC SA1029NW](https://openairdocs.org/stc/SA1029NW): Installation of a cargo system. Western Metal Products. Lists 737 Series - [STC SA1258EA](https://openairdocs.org/stc/SA1258EA): Installation of Cosco model78-( ) child restraint system. (172M S/N 17263459 - 17267584). Miller Stuart R. Lists 737 Series - [STC SA1052SO](https://openairdocs.org/stc/SA1052SO): Installation of GE battery P/N43B022RB36 in place of Marathon P/N CA-727-7, CA-727-20, or CA-27-20 batteries or SAFT P/N23180 batteries; or installation of GE battery P/N 43B020RB10 replacing Marathon P/N CA-727-7, CA-727-20 or CA-27-20 or SAFT P/N 23186 or 23180 batteries. General Electric Company. Lists 737 Series - [STC SA1082NW](https://openairdocs.org/stc/SA1082NW) (historical): Installation of auxiliary fuel tanks in the aft cargo compartment. (737 series -2K9A). Rogerson ATS. Lists 737 Series ### Approved for the engine (CFM International CFM56 series) - [STC SE04840NY](https://openairdocs.org/stc/SE04840NY): Installation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engine. Kilroy Aviation LLC. Lists CFM56-7B20 - [STC SE03036CH](https://openairdocs.org/stc/SE03036CH): Application of a deep compressive stress layer using a Low Plasticity Burnishing (LPB) process on CFM56-7 Series Engines Stage 1 High Pressure Compressor (HPC) Blade Dovetails in accordance with Delta Air Lines Inc. Drawing No. 72-0396, Revision B, dated November 3, 2011, or later FAA Approved revision. Delta Air Lines Inc. Lists CFM56-7B20 - [STC SE00032EN](https://openairdocs.org/stc/SE00032EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 Fan/Booster Module. Pratt & Whitney. Lists CFM56-3 - [STC SE00033EN](https://openairdocs.org/stc/SE00033EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 High Pressure Compressor Module. Pratt & Whitney. Lists CFM56-3 - [STC SE00034EN](https://openairdocs.org/stc/SE00034EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 High Pressure Turbine Module. Pratt & Whitney. Lists CFM56-3 - [STC SE00035EN](https://openairdocs.org/stc/SE00035EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 Low Pressure Turbine Module. Pratt & Whitney. Lists CFM56-3 - [STC SE00822CH](https://openairdocs.org/stc/SE00822CH): Install AeroControlex P/N 2604880-001 variable stator feedback control cable and P/N 2604880-002 variable bleed valve feedback control cable on CFM International engines. AeroControlex Group TransDigm Inc. Lists CFM56-2 ## Related - Other Boeing 737-7H4 aircraft: https://openairdocs.org/model/boeing-737-7h4/aircraft.md - The CFM International CFM56 series engine: https://openairdocs.org/engine/cfm-international-cfm56-series.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.