# N207WN: 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: 34012
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 24, 2005
- Certificate issued: April 13, 2005
- Expires: March 31, 2030
- Mode S code: A1AE05
- 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=207WN
- Page: https://openairdocs.org/aircraft/N207WN

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/N207WN/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 LAX07LA064](https://openairdocs.org/ntsb/LAX07LA064), Dec 27, 2006: Boeing 737-7H4 (N207WN), San Diego, CA, minor damage. Probable cause: Failure of the captain of the other taxiing airplane to maintain clearance from an occupied airplane stopped on the ramp.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20061226029532A](https://openairdocs.org/incident/20061226029532A), Dec 26, 2006: Boeing 7377H4 (N207WN), San Diego, CA, Substantial damage. (-23) Pilot of N207WN taxied into N673AA in the alleyway of the southwest ramp at ksan. Regional officer's report: on 12/26/2006, at 1816 hours, harbor police…

## Service difficulty reports (380, 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 SWAA2026091602212](https://openairdocs.org/sdr/SWAA2026091602212), Sep 7, 2026: STIFFENER. CRACKED. CRACKED INTERNAL STRUCTURE STIFFENER LOCATED BTW BS 907 TO BS 927 AND BTW STRG 25R TO STRG 27R FWD POSITION AT AFT CARGO COMPARTMENT. REPLACED THE STIFFENER & F
- [SDR SWAA2026091661779](https://openairdocs.org/sdr/SWAA2026091661779), Sep 7, 2026: STIFFENER. CRACKED. CRACK INTERNAL STRUCTURE STIFFENER LOCATED BTW BS 907 TO BS 927 AND BTW STRG 25R TO STRG 27R AFT POSITION AT AFT CARGO COMPARTMENT 2026-505555 REPLACED STIFFENE
- [SDR SWAA2026091199190](https://openairdocs.org/sdr/SWAA2026091199190), Sep 4, 2026: HANDLE. DETERIORATED. DETERIORATED HANDLE NUT, & YELLOW STRAP ON AFT ENTRY DOOR LINING AT AFT GALLEY AREA. REPLACED HANDLE NUT & YELLOW STRAP ON AFT ENTRY DOOR LINING AT AFT GALLEY A
- [SDR SWAA2026091438273](https://openairdocs.org/sdr/SWAA2026091438273), Aug 27, 2026: BRACKET. CRACKED. CRACK BRACKET TRAILING EDGE LOCATED IRSS 210 APROX AT RT WING. REPLACED BRACKET IAW SRM 51-40-02, SRM 51-10-02, AND DWG 115A2001, SHEET 24, REV A.
- [SDR SWAA2026091654020](https://openairdocs.org/sdr/SWAA2026091654020), Aug 23, 2026: STRAP. CRACKED. CRACK INDICATION FOUND AT BS 616, LBL 45.57 STUB BEAM TRAPS AREA. (FWD FASTENER HOLE). REPLACED STUB BEAM STRAP IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 
- [SDR SWAA2026091671091](https://openairdocs.org/sdr/SWAA2026091671091), Aug 23, 2026: LIGHT. DETERIORATED. DETERIORATED PHOTOLUMINESCENT LIGHT ALONG PASSENGER CABIN. REPLACED THE PHOTOLUMINESCENT LIGHT IAW AMM 33-51-15-400-802.
- [SDR SWAA2026091417259](https://openairdocs.org/sdr/SWAA2026091417259), Aug 23, 2026: WEB. CORRODED. CORROSION ON UPPER MAIN SILL WEB LOCATED BTW BS 440 TO BS 492.4 RBL 68 WL 200 AT FWD CARGO BAY. REPLACED UPPER MAIN SILL WEB AND FASTENERS LOCATED BTW BS 440 TO
- [SDR SWAA2026091480621](https://openairdocs.org/sdr/SWAA2026091480621), Aug 23, 2026: SKIN. DEBONDED. DEBONDED LOWER SKIN ON OTBD AFT FLAP RT WING. REPAIRED OTBD AFT FLAP RT WING IAW SRM 57-53-01-2R-4, REPAIR 4, & SRM 51-70-10-2R-4, REPAIR 4.
- [SDR SWAA2026091420796](https://openairdocs.org/sdr/SWAA2026091420796), Aug 23, 2026: SKIN. DEBONDED. DEBONDED LOWER SKIN ON OTBD AFT FLAP, LT WING. PERFORMED INTERIM REPAIR ON OTBD AFT FLAP AT LT WING IAW SRM 57-53-01-2R-16 REPAIR 16. PERFORMED TAP TEST INSPECT
- [SDR SWAA2026091605216](https://openairdocs.org/sdr/SWAA2026091605216), Aug 22, 2026: ACCESS PANEL. LEAKING. FUEL LEAK ON ACCESS PANEL 632HB AT RT WING. REMOVED AND REINSTALLED ACCESS PANEL 632HB IAW AMM 28-11-11-000-801 AND AMM 28-11-11-400-801.
- [SDR SWAA2026091462607](https://openairdocs.org/sdr/SWAA2026091462607), Aug 22, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, ACCESS PANEL 651FB, RT WING. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, DWG 115A2710, SHEET 5, REV A, & DWG 287A9
- [SDR SWAA2026091463270](https://openairdocs.org/sdr/SWAA2026091463270), Aug 22, 2026: RIB. CRACKED. CRACKED LEADING EDGE RIB ACCESS PANEL 331B LE HSS 114.55 AT LT HORIZONTAL STAB. REPLACED LEADING EDGE RIB & FASTENERS ON ACCESS PANEL 331B LE HSS 114.55 IAW SRM
- [SDR SWAA2026091453396](https://openairdocs.org/sdr/SWAA2026091453396), Aug 22, 2026: ACCESS PANEL. CRACKED. CRACKED BLADE, ACCESS PANEL 333AT AT LT HORIZONTAL STAB. REPLACED BLADE ON ACCESS PANEL 333AT AT LT HORIZONTAL STAB IAW SRM 51-10-02 AND SRM 51-40-02.
- [SDR SWAA2026091439784](https://openairdocs.org/sdr/SWAA2026091439784), Aug 22, 2026: PANEL. DEBONDED. DEBONDED WEDGE PANEL ON RT INBOARD FLAP AT RT WING. PERFORMED INTERIM REPAIR ON WEDGE PANEL ON RT INBD FLAP AT RT WING IAW SRM 57-53-01-2R-18, REPAIR 18. PERFOR
- [SDR SWAA2026091435509](https://openairdocs.org/sdr/SWAA2026091435509), Aug 22, 2026: ANGLE. CRACKED. CRACK ANGLE, ACCESS PANEL 651GB AT RT WING. REPLACED ANGLE LOCATED ON ACCESS PANEL 651GB AT RT WING IAW SRM 51-40-02, & SRM 51-10-02-0G-0. INSPECTION AND REMOVA
- [SDR SWAA2026091430002](https://openairdocs.org/sdr/SWAA2026091430002), Aug 22, 2026: RIB. CRACKED. CRACK LEADING EDGE RIB ACCESS PANEL 331B LE STA 86.66 AT LT HORIZONTAL STAB. REPLACED LEADING EDGE RIB AND FASTENERS ON ACCESS PANEL 331B LE STA 86.66 AT LT HOR
- [SDR SWAA2026091475041](https://openairdocs.org/sdr/SWAA2026091475041), Aug 22, 2026: ACCESS PANEL. DELAMINATED. ACCESS PANEL 192HL - DENTED & DELAMINATED. REPAIRED THE ACCESS PANEL 192HL IAW SRM 51-70-05-2R-2, REPAIR 2.
- [SDR SWAA2026091493968](https://openairdocs.org/sdr/SWAA2026091493968), Aug 22, 2026: ACCESS PANEL. DELAMINATED. ACCESS PANEL 551AT DENTED WITH DELAMINATION. REPAIRED ACCESS PANEL 551AT IAW SRM 51-70-05-2R-2 REPAIR 2.
- [SDR SWAA2026091689932](https://openairdocs.org/sdr/SWAA2026091689932), Aug 21, 2026: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK (TOP SURFACE) LOCATED BS 639 PLUS 23 INCH RBL 45.50 AT PASSENGER CABIN REFER TO FAULT TTG8Q01DUFY3 WHERE 26-153-02366-WIP1 WAS ADDED AS 
- [SDR SWAA2026091672764](https://openairdocs.org/sdr/SWAA2026091672764), Aug 21, 2026: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK (TOP SURFACE) LOCATED BS 639 PLUS 12 INCH RBL 45.50 AT PASSENGER . REPAIRED SEAT TRACK BTW BSTA 639 & BSTA 706 AT RBL 45.50 AT PASSENGER
- [SDR SWAA2026091689594](https://openairdocs.org/sdr/SWAA2026091689594), Aug 21, 2026: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK (TOP AND BOTTOM SURFACE) LOCATED BTW BS 685 TO BS 706 RBL 45.50 AT PASSENGER CABIN.
- [SDR SWAA2026091621561](https://openairdocs.org/sdr/SWAA2026091621561), Aug 21, 2026: SKIN. CORRODED. CORROSION EXTERNAL SKIN WATER SERVICE CUT OUT BTW BS 907 TO BS 927 AND BTW STRG 26R TO STRG 27R AT LOWER FUSELAGE. REPAIRED EXTERNAL SKIN WATER SERVICE CUT OUT 
- [SDR SWAA2026091613651](https://openairdocs.org/sdr/SWAA2026091613651), Aug 21, 2026: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK (TOP SURFACE) LOCATED BTW BS 663 TO BS 685 RBL 45.50 AT PASSENGER CABIN 2026-505409 REFER TO FAULT TTG8Q01DUFY3 WHERE 26-153-02366-WIP1 
- [SDR SWAA2026091478011](https://openairdocs.org/sdr/SWAA2026091478011), Aug 21, 2026: CROSSBEAM. CRACKED. CRACKED BRAKE PANEL, BS 540, BTWN BL 0 - RBL 24.75. REPLACED THE BRAKE PANEL IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, & DWG 143A0060, SHEET 64, REV-.
- [SDR SWAA2026091100263](https://openairdocs.org/sdr/SWAA2026091100263), Aug 21, 2026: ANGLE. CRACKED. CRACK ON ANGLE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN. REPLACED ANGLE AND FASTENERS IAW SRM 51-40-02 AND DWG 273A9110, SHEET 6, REV A.
- [SDR SWAA2026091682161](https://openairdocs.org/sdr/SWAA2026091682161), Aug 20, 2026: SEAT TRACK. CORRODED. CORROSION SEAT TRACK LOC. ON BS 807 PLUS 6 INCHES AND WL 208 ON TOP SURFACE AT LBL 45.5 AT PASSENGER CABIN REPAIRED SEAT TRACK LOC. ON BS 807 PLUS 6 INCHES AND 
- [SDR SWAA2026091433998](https://openairdocs.org/sdr/SWAA2026091433998), Aug 20, 2026: FRAME. CRACKED. CRACKED FRAME, BS 312 BTW STR 5L - 6L. PERFORMED TRIM OUT OF FRAME UPPER ANGLE IAW EA M-22-153-01244, REV B.
- [SDR SWAA2026091411280](https://openairdocs.org/sdr/SWAA2026091411280), Aug 19, 2026: STRAP. CRACKED. CRACK STRAP LOCATED ON ACCESS PANEL 142KW AT AFT CARGO BAY. TOOK MEASURES OF CRACK ON STRAP LOCATED ON ACCESS PANEL 142KW AT AFT CARGO COMPARTMENT DUE TO NO FOU
- [SDR SWAA2026091483813](https://openairdocs.org/sdr/SWAA2026091483813), Aug 19, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLE ON ACCESS PANEL 671CB TRAILING EDGE, RT WING. PERFORMED VISUAL INSPECTION ON REPORTED AREA AND NOT FOUND ELONGATED HOLE ONLY FOUND BURN PAINT ARO
- [SDR SWAA2026091465029](https://openairdocs.org/sdr/SWAA2026091465029), Aug 19, 2026: ACCESS PANEL. ELONGATED. ELONGATED HOLE ACCESS PANEL 561BB ON LT WING. REPAIRED THE ACCESS PANEL 561BB IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026091482156](https://openairdocs.org/sdr/SWAA2026091482156), Aug 19, 2026: ACCESS PANEL. ELONGATED. ELONGATED HOLE ACCESS PANEL 561CB AT LT WING. REPAIRED ACCESS PANEL 561CB IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026091139224](https://openairdocs.org/sdr/SWAA2026091139224), Aug 19, 2026: SKIN. CRACKED. CRACK EXTERNAL GROUND ELECTRICAL POWER CUTOUT LOWER AREA AT LOWER FUSELAGE. REPAIRED EXTERNAL GROUND ELECTRICAL POWER DOOR CUTOUT LOWER AREA AT LOWER FUSELAGE I
- [SDR SWAA2026091100219](https://openairdocs.org/sdr/SWAA2026091100219), Aug 18, 2026: SCUFF PLATE. CRACKED. CRACK ON AFT CORNER SCUFF PLATE IN THE AFT CARGO BAY. REPAIRED THE AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, PARAGRAPH 4. B, STEPS (2 TO 7) FIGURE
- [SDR SWAA2026072831243](https://openairdocs.org/sdr/SWAA2026072831243), Jul 25, 2026: SCREW. MISSING. FWD GALLEY SERVICE DOOR SLIDE IS GETTING CAUGHT ON FLOOR METAL COVER PLATE. INSTALLED MISSING SCREW ON FLOOR METAL COVER PLATE BY FWD GALLEY SERVICE DOOR SLIDE 
- [SDR SWAA2026072034663](https://openairdocs.org/sdr/SWAA2026072034663), Jul 14, 2026: LENS. MISSING. FORWARD OVERWING EXIT SIGN IS MISSING. REPLACED LENS COVER PER SIP.
- [SDR SWAA2026051197064](https://openairdocs.org/sdr/SWAA2026051197064), May 8, 2026: BOLT. LOOSE. SEAT 15D WILL NOT LOCK IN UPRIGHT POSITION<[01] OK TO CONTINUE PER MEL 25-6-01 SP 1B. FOUND LOOSE & STRIPPED BOLT REPLACED BOLT PER CMM 25-21-42
- [SDR SWAA2025112639129](https://openairdocs.org/sdr/SWAA2025112639129), Nov 23, 2025: LIGHT. DETACHED. FORWARD GALLEY EMERGENCY EXIT LIGHT COVER FELL OFF. R & R FWD GALLEY EMERGENCY LIGHT ASSY IAW AMM 33-51-01-960-802-NG, OPS CHECKED NORMAL.
- [SDR SWAA2025110530947](https://openairdocs.org/sdr/SWAA2025110530947), Nov 2, 2025: SIGN. INOPERATIVE. AFT SERVICE DOOR, BOTH RT AND LT OVER WING EMERGENCY EXIT SIGNS LIGHTS MISSING BULBS. REPLACED THE BULBS IN THE SIGNS AND PERFORMED GOOD TEST IAW AMM 33-51-01-9
- [SDR SWAA2025092518029](https://openairdocs.org/sdr/SWAA2025092518029), Sep 25, 2025: GIRT BAR. UNPACKED. L2 DOOR ESCAPE SLIDE GIRT REQUIRES REPACK. REPACKED L2 DOOR ESCAPE SLIDE GIRT IAW AMM 25-66-01-000-804-NG.
- [SDR SWAA2025092518027](https://openairdocs.org/sdr/SWAA2025092518027), Sep 25, 2025: GIRT BAR. UNPACKED. R2 DOOR ESCAPE SLIDE GIRT REQUIRES REPACK. REPACKED R2 DOOR ESCAPE SLIDE GIRT IAW AMM 25-66-01-000-804-NG.
- [SDR SWAA2025081199344](https://openairdocs.org/sdr/SWAA2025081199344), Aug 7, 2025: LENS. DETACHED. CREW REPORTS F.O. SIDE OVERWING EXIT LIGHT LENS COVER DEATTACHED. SECURED WITH TAPE. OK TO CONT. PER EA# MT M-21-133-00720.
- [SDR SWAA2025052774702](https://openairdocs.org/sdr/SWAA2025052774702), May 24, 2025: LAMP. INOPERATIVE. RH EMERGENCY EXIT DOOR LIGHT INOP. RELAMPED RH EXIT DOOR LAMP REF AMM 33-51-01.OPS CHECKED GOOD.
- [SDR SWAA2025050565193](https://openairdocs.org/sdr/SWAA2025050565193), Apr 29, 2025: SEAL. CRACKED. L/H STABILIZER-TO-BODY UPPER FRONT SPAR SLIDING SEAL CRACKED<[01] REMOVED AND REPLACED L/H STABILIZER-TO-BODY UPPER FRONT SPAR SLIDING SEAL IN ACCORDANCE WITH A
- [SDR SWAA2024111156197](https://openairdocs.org/sdr/SWAA2024111156197), Nov 3, 2024: LIGHT. MISSING. MAIN CABIN EPL STRIPS MISSING AT ROWS 10ABC AND 18DEF.<[01] INSTALLED MAIN CABIN EPL STRIPS AT ROWS 10ABC AND 18DEF AS PER B737 AMM 33-51-15-400-802;[02] VERIFI
- [SDR SWAA2024111156196](https://openairdocs.org/sdr/SWAA2024111156196), Nov 3, 2024: HANDLE. MISSING. L-1 DOOR AFT ASSISTED HANDLE AND SAFETY STRAP MISSING.<[01] INSTALLED L1 DOOR AFT ASSISTED HANDLE AND SAFETY STRAP AS PER B737 AMM 25-21-25-420-801;[02] VERIFIE
- [SDR SWAA2024111155286](https://openairdocs.org/sdr/SWAA2024111155286), Oct 31, 2024: BATTERY PACK. INOPERATIVE. INTERIOR/EXTERIOR EMERGENCY EXIT LIGHTS INOP<[01] PERFORMED TROUBLESHOOTING AS PER BOEING 737 WDM 33-51-13; FOUND M1670 EMERGENCY EXIT LIGHT BATTERY PACK DEFECT
- [SDR SWAA2024110854620](https://openairdocs.org/sdr/SWAA2024110854620), Oct 30, 2024: SIGN. BROKEN. L-1 DOOR EXIT SIGN INDICATOR BROKEN.<[01] ITEM ENTER IN ERROR;[02] ITEM ENTERED ON ERROR WILL BE ACCOMPLISHED TTG8Q004Z0B5;[03] VERIFIED STEPS 1 AND 2
- [SDR SWAA2024110848216](https://openairdocs.org/sdr/SWAA2024110848216), Oct 13, 2024: SEAT TRACK. CRACKED. F/O I/B FORWARD SEAT TRACK HAS CRACK FWD END<[01] RECEIVED NEW SEAT TRACK P/N 1A226-0204ATSMRO P.O. 2074280 PER B737-700 AMM 25-11-01-200-802. FOR SEAT TRACK IN
- [SDR SWAA2024111145898](https://openairdocs.org/sdr/SWAA2024111145898), Oct 7, 2024: SCUFF PLATE. CRACKED. AFT CARGO COMPARTMENT DOOR CUTOUT LOWER SILL FWD SCUFF PLATE CRACKED MKD DOT<[01] RECIEVED AFT CARGO COMPARTMENT DOOR CUTOUT LOWER SILL FWD SCUFF PLATE REF INST
- [SDR SWAA2024111146262](https://openairdocs.org/sdr/SWAA2024111146262), Oct 7, 2024: SUPPORT. CORRODED. CORROSION, RIGHT MAIN W/W CUTOUT AFT ALL BLADE SEAL SUPPORTS TOP SURFACE. REMOVED CORROSION AT RIGHT MAIN W/W CUTOUT AFT SEAL TOP SURFACE AS PER B-737 SRM 51-10

All 380: https://openairdocs.org/aircraft/N207WN/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

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