# N215WN: 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: 32487
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 2, 2005
- Certificate issued: June 20, 2005
- Expires: August 31, 2027
- Mode S code: A1CE16
- 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=215WN
- Page: https://openairdocs.org/aircraft/N215WN

From the FAA registry file of October 24, 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/N215WN/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 N215WN.

## FAA accident and incident reports

None matched to N215WN.

## Service difficulty reports (291, 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 SWAA2026080446798](https://openairdocs.org/sdr/SWAA2026080446798), Jul 31, 2026: STARTER. FAILED. DURING PUSH BACK NR 2 ENG FAILED TO START. NO ROTATION. REMOVED AND REPLACED NR 2 ENGINE STARTER IAW AMM 80-11-01 OPS AND LEAK CHECKED GOOD.
- [SDR SWAA2026021269236](https://openairdocs.org/sdr/SWAA2026021269236), Feb 10, 2026: ISOLATOR. CRACKED. PASSENGER CABIN FORWARD GALLEY SERVICE DOOR FORWARD UPPER SLIDE ISOLATOR CRACKED. R & R UPPER SLIDE ISOLATOR IAW SRM 51-40-02.
- [SDR SWAA2025122254056](https://openairdocs.org/sdr/SWAA2025122254056), Dec 19, 2025: SLIDE. LOW PRESSURE. AFT SERVICE DOOR SLIDE LOW PRESSURE<[01] R&R AFT SERVICE ESCAPE SLIDE PER AMM 25-66-01; MT 725-61-06 REM/INSTL
- [SDR SWAA2025100620121](https://openairdocs.org/sdr/SWAA2025100620121), Oct 1, 2025: LENS. DAMAGED. AFT LAVATORY EMERGENCY EXIT SIGN HAS DAMAGED LENS. REMOVED AND REPLACED DAMAGED LENS FROM AFT LAV EMERGENCY EXIT SIGN AND PERFORMED GOOD INSTALLATION TEST IAW A
- [SDR SWAA2025090309867](https://openairdocs.org/sdr/SWAA2025090309867), Aug 30, 2025: HANDLE. LOOSE. ASSIST HANDLE ON FWD ENTRY DOOR LOOSE RE-SECURED FWD ENTRY DOOR ASSIST HANDLE PER AMM 52-11-31. RESECURED ASSIST HANDLE PER AMM 52-11-31.<BR><BR>3194309
- [SDR SWAA2025072894222](https://openairdocs.org/sdr/SWAA2025072894222), Jul 22, 2025: FAIRING. DAMAGED. STRUT FAIRING ON NR 2 ENGINE AT 3 O`CLOCK POSITION HAS ELONGATED HOLE. PARTIALLY INSTALLED STRUT FAIRING PANEL IAW AMM 73-21-06, FINISHED INSTALLING REMAINING 2
- [SDR SWAA2025062584647](https://openairdocs.org/sdr/SWAA2025062584647), Jun 23, 2025: GIRT BAR. OUT OF POSITION. FWD SERVICE DOOR GIRT BAR TO SLIDE IS OUT OF POSITION<[01] RESET GIRT BAR AS NEEDED PER SIP
- [SDR SWAA2025060377055](https://openairdocs.org/sdr/SWAA2025060377055), Jun 1, 2025: HOLDER. BROKEN. FWD GALLEY EMERGENCY FLASHLIGHT HOLDER BROKEN <[01]. REPLACED BROKEN FLASHLIGHT HOLDER PER SRM 51-40-01 AND AMM 25-64-00.
- [SDR SWAA2025022498262](https://openairdocs.org/sdr/SWAA2025022498262), Feb 23, 2025: LAMP. INOPERATIVE. RH EMERGENCY EXIT WINDOW EXIT LIGHT BULB OUT <[01]. CORRECTLY INSTALLED RH EMERGENCY WINDOW EXIT LIGHT LAMP PER AMM 33-25-00-960-804;[02] VERIFIED CORRECTIVE AC
- [SDR SWAA2025022498258](https://openairdocs.org/sdr/SWAA2025022498258), Feb 23, 2025: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT INSIDE CABIN ROW 12 ABC; 9 ABC ARE INOP <[01]. DURING TROUBLESHOOTING; DETERMINED THAT THIS DEFECT AND DEFECT TTG8Q00YW88E ARE BOTH CONTROLLED B
- [SDR SWAA2025022499085](https://openairdocs.org/sdr/SWAA2025022499085), Feb 23, 2025: CHARGER. INOPERATIVE. EMERGENCY LIGHT INSIDE CABIN ROW 12 ABC; 9 ABC ARE INOP <[01]. DURING TROUBLESHOOTING; DETERMINED THAT THIS DEFECT AND DEFECT TTG8Q00YW88E ARE BOTH CONTROLLED B
- [SDR SWAA2025022498257](https://openairdocs.org/sdr/SWAA2025022498257), Feb 23, 2025: BATTERY PACK. INOPERATIVE. AFT OF WING EMERGENCY SLIDE LIGHT BOTH LH AND RH SIDE ARE OUT <[01]. DURING TROUBLESHOOTING; DETERMINED THAT THIS DEFECT AND DEFECT TTG8Q00YW88S ARE BOTH CONTRO
- [SDR SWAA2025022499086](https://openairdocs.org/sdr/SWAA2025022499086), Feb 23, 2025: CHARGER. INOPERATIVE. AFT OF WING EMERGENCY SLIDE LIGHT BOTH LH AND RH SIDE ARE OUT <[01]. DURING TROUBLESHOOTING; DETERMINED THAT THIS DEFECT AND DEFECT TTG8Q00YW88S ARE BOTH CONTRO
- [SDR SWAA2025022498256](https://openairdocs.org/sdr/SWAA2025022498256), Feb 22, 2025: LIGHT. DISCONNECTED. EMERGENCY EXIT LIGHT INOP AFT OF FED <[01]. CHECKED FOR GROUND AND POWER AT L731 (FORWARD ESCAPE SLIDE LIGHT); FOUND NEITHER GROUND OR VOLTAGE AY L731 LIGHT SOC
- [SDR SWAA2025022497379](https://openairdocs.org/sdr/SWAA2025022497379), Feb 19, 2025: LIGHT. BURNED OUT. EMERGENCY EXIT LIGHT SIDEWALL SIGN AT L/H OVERWING EXIT HAS BURNED OUT BULBS <[01]. RELAMPED EMERGENCY EXIT LIGHT AT L/H SIDEWALL OVERWING EXIT AND PERFORMED A 
- [SDR SWAA2025022496769](https://openairdocs.org/sdr/SWAA2025022496769), Feb 16, 2025: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS FWD RIGHT OVERDOOR EXIT INOP L1067 <[01]. PER TROUBLESHOOTING PERFORMED GOOD CONTINUITY CHECK FROM CONNECTOR D10750 TO CONNECTOR D2968 IAW WDM 
- [SDR SWAA2025022494152](https://openairdocs.org/sdr/SWAA2025022494152), Feb 8, 2025: LENS. DAMAGED. AFT LAVE 'B' EMERGENCY EXIT LIGHT LENS DAMAGED<[01] REMOVED AND REPLACED AFT LAVE 'B' EMERGENCY EXIT LIGHT LENS PER AMM 33-51-01-960-801;[02] VERIFIED COMPLETIO
- [SDR SWAA2025022493806](https://openairdocs.org/sdr/SWAA2025022493806), Feb 7, 2025: WIRE. BROKEN. G-1 GALLEY MOUNTED EMERGENCY EXIT LIGHT WIRE BROKEN AT CONNECTOR<[01] DISCONNECTABLE SPLICE AT EMERGENCY EXIT LIGHT-FWD-FLOOR PROXIMITY G-1 GALLEY WAS REPLACED 
- [SDR SWAA2025022489513](https://openairdocs.org/sdr/SWAA2025022489513), Jan 25, 2025: BAFFLE. CRACKED. FWD CARGO BAY L/H BAFFLE CRACKED BS440 TO BS460 LBL22 WL156<[01] CORRECTION: FORWARD CARGO BAY L/H BAFFLE CRACKED BS440 TO BS460 LBL22 WL156 [TTG8Q00YBXHD].;[02
- [SDR SWAA2025022588983](https://openairdocs.org/sdr/SWAA2025022588983), Jan 24, 2025: VAPOR BARRIER. CRACKED. STIFFENER CRACKED COMMON TO VAPOR BARRIER BS663 LBL26 WL151 <[01]. REMOVED AND REPLACED NEW STIFFENER COMMON TO VAPOR BARRIER BS663 LBL26 WL151 IAW SRM 51-40-02
- [SDR SWAA2025022488980](https://openairdocs.org/sdr/SWAA2025022488980), Jan 23, 2025: BAFFLE. CRACKED. FORWARD CARGO BAY BAFFLE IS CRACKED BS460 TO BS480 LBL25 WL156<[01] REMOVED DAMAGED BAFFLE AND INSTALLED NEW BAFFLE AS PER SRM 51-40-02-0G-0 AND DRAWING 143A750
- [SDR SWAA2025022588169](https://openairdocs.org/sdr/SWAA2025022588169), Jan 22, 2025: SEAT TRACK. CORRODED. CORROSION ON LBL 45 SEAT TRACK WELL AT STA 500A+8; WL 208.1. <[01] DISCREPANCY RECORD ON CCN TTG8Q00Y9RNQ REQUIRED REMOVED AND REPLACED THEREFORE CARD TO BE CLO
- [SDR SWAA2025022588170](https://openairdocs.org/sdr/SWAA2025022588170), Jan 22, 2025: SEAT TRACK. CORRODED. CORROSION ON LBL 24 SEAT TRACK WELL AT STA 500B+18; WL 208.1. <[01] DISCREPANCY RECORD ON CCN TTG8Q00Y9RP3 REQUIRED REMOVED AND REPLACED THEREFORE CARD TO BE CL
- [SDR SWAA2025022488151](https://openairdocs.org/sdr/SWAA2025022488151), Jan 22, 2025: STRAP. CORRODED. CORROSION ON AFT CARGO BAY FLOOR T STRAP BS 727D+5 RBL 9 TO RBL 18 WL 156<[01] CORRECTION TO DISCREPANCY; SHOULD READ; CORROSION ON AFT CARGO BAY FLOOR T STRAP 
- [SDR SWAA2025022488150](https://openairdocs.org/sdr/SWAA2025022488150), Jan 22, 2025: STRAP. CORRODED. CORROSION ON AFT CARGO BAY FLOOR T STRAP BS 767+5 RBL 12 - TO RBL 19 WL 156<[01] EVALUATED CORROSION FOUND TO BE OUT OF LIMITS; RECEIVED NEW STRAP AND PAINTED W
- [SDR SWAA2025022488537](https://openairdocs.org/sdr/SWAA2025022488537), Jan 22, 2025: ATTACH ANGLE. CORRODED. CORROSION AFT CARGO BAY ATTACH ANGLE UNDER SHIELD HAS MULTIPLE AREAS UNDER NUT PLATES BS767 TO BS787 RBL21 WL156<[01] CORROSION ON AFT CARGO BAY ATTACH ANGLE UN
- [SDR SWAA2025022488538](https://openairdocs.org/sdr/SWAA2025022488538), Jan 22, 2025: SHIELD. CORRODED. CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] CORROSION ON AFT CARGO BAY FWD SHIELD; FOUND 
- [SDR SWAA2025022488148](https://openairdocs.org/sdr/SWAA2025022488148), Jan 21, 2025: SUPPORT PLATE. CORRODED. CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156<[01] CORROSION ON AFT CARGO BAY L/
- [SDR SWAA2025022488149](https://openairdocs.org/sdr/SWAA2025022488149), Jan 21, 2025: SUPPORT. CORRODED. CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] DAMAGED ON R/H FLOOR TO S
- [SDR SWAA2025022487908](https://openairdocs.org/sdr/SWAA2025022487908), Jan 21, 2025: THRESHOLD. CRACKED. AFT CARGO BAY AFT CORNER THRESHOLD IS CRACKED <[01]. REPAIRED AFT CARGO BAY AFT CORNER THRESHOLD PER SRM 53-60-15-2R-1.
- [SDR SWAA2025022487909](https://openairdocs.org/sdr/SWAA2025022487909), Jan 21, 2025: THRESHOLD. CRACKED. AFT CARGO BAY FORWARD CORNER THRESHOLD IS CRACKED <[01]. REPAIRED AFT CARGO BAY FORWARD CORNER THRESHOLD PER SRM 53-60-15-2R-1.
- [SDR SWAA2025022487794](https://openairdocs.org/sdr/SWAA2025022487794), Jan 20, 2025: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 242NF DELAMINATED. (CUSTOMER REQUEST)<[01] PASSENGER CABIN FLOOR PANEL 242NF WITH UPPER SKIN DELAMINATIONS WAS REPLACED WITH A SERVI
- [SDR SWAA2025022487795](https://openairdocs.org/sdr/SWAA2025022487795), Jan 20, 2025: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 242MF DELAMINATED. (CUSTOMER REQUEST)<[01] PASSENGER CABIN FLOOR PANEL 242MF WITH UPPER SKIN DELAMINATION WAS REPLACED WITH A SERVIC
- [SDR SWAA2025022487797](https://openairdocs.org/sdr/SWAA2025022487797), Jan 20, 2025: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 241SF DELAMINATED. (CUSTOMER REQUEST)<[01] PASSENGER CABIN FLOOR PANEL 241SF WITH UPPER SKIN DELAMINATION WAS REPLACED WITH A SERVIC
- [SDR SWAA2025022487796](https://openairdocs.org/sdr/SWAA2025022487796), Jan 20, 2025: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 241RF DELAMINATED. (CUSTOMER REQUEST)<[01] PASSENGER CABIN FLOOR PANEL 241RF; WITH DELAMINATION; WAS REPLACED WITH A NEWLY FABRICATE
- [SDR SWAA2025022487793](https://openairdocs.org/sdr/SWAA2025022487793), Jan 20, 2025: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 241TF DELAMINATED. (CUSTOMER REQUEST)<[01] PASSENGER CABIN FLOOR PANEL 241TF WITH UPPER SKIN DELAMINATION WAS REPLACED WITH A SERVIC
- [SDR SWAA2025022487628](https://openairdocs.org/sdr/SWAA2025022487628), Jan 20, 2025: FLOOR PANEL. DELAMINATED. MAIN CABIN; FLOOR PANEL 241AAF TOP LAYER FIBER GLASS EXPOSED.<[01] 241AAF; WITH UPPER SURFACE DAMAGE; WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER [SRM 
- [SDR SWAA2025022586847](https://openairdocs.org/sdr/SWAA2025022586847), Jan 17, 2025: FORMER. CRACKED. WING TO BODY FAIRING FORMER IS CRACKED BS 500D BETWEEN STRINGER 19 AND 20 L/H <[01]. REMOVED DAMAGED FAIRING FORMER AND INSTALLED NEW FAIRING FORMER BS 500D BET
- [SDR SWAA2025022487207](https://openairdocs.org/sdr/SWAA2025022487207), Jan 17, 2025: STIFFENER. CRACKED. STIFFENER CRACKED AT BS 250 LBL 4 WL 208 <[01]. REMOVE AND REPLACED STIFFENER AT BS 250 LBL 4 WL 208 I.A.W SRM 51-10-02-0G-0; SRM 51-40-02-0G-0 AND BOEING DWG 1
- [SDR SWAA2025022586760](https://openairdocs.org/sdr/SWAA2025022586760), Jan 16, 2025: PANEL. CRACKED. CRACKED PANEL BREAK BS 540 BL 0 - RBL 25 WL 207 (MARKED) <[01]. REPLACED CRACKED PANEL BREAK WITH NEW AT BS 540 BL 0 - RBL 25 WL 207. REMOVED PART AND FOUND NO 
- [SDR SWAA2025022487904](https://openairdocs.org/sdr/SWAA2025022487904), Jan 16, 2025: FLOOR PANEL. DELAMINATED. PANEL 241BF HAS BUBBLES; DENTS AND FRAYED ON TOP PLY FIBERGLASS (MARKED)<[01] PANEL 241BF WITH BUBBLES (DELAMINATION); DENTS AND FIBERGLASS STRAND FRAYING ON TO
- [SDR SWAA2025022586303](https://openairdocs.org/sdr/SWAA2025022586303), Jan 15, 2025: VAPOR BARRIER. CRACKED. L/H B.S. 663 VAPOR BARRIER IS CRACKED AT MID SPAN <[01]. L/H B.S. 663 VAPOR BARRIER DAMAGE AT MID SPAN HAS BEEN REPAIRED PER [SRM 51-70-04-2R-10-A00755 (REPAIR 
- [SDR SWAA2025022486038](https://openairdocs.org/sdr/SWAA2025022486038), Jan 15, 2025: DOOR. CORRODED. LAV SERVICE DOOR IS CORRODED AT BONDING JUMPER ATTACH POINT <[01]. EVALUATED CORROSION ON LAV SERVICE DOOR; FOUND 0.040 REMOVED FROM ORIGINAL .100 IN A 1'X1' AR
- [SDR SWAA2025022586024](https://openairdocs.org/sdr/SWAA2025022586024), Jan 14, 2025: SKIN. CRACKED. RH WING #5 SLAT FOUND CRACK AT LEADING EDGE NOSE SKIN LOWER SURFACE FASTENER; MARKED <[01]. REPAIRED RH WING #5 SLAT AT LEADING EDGE NOSE SKIN LOWER SURFACE IAW
- [SDR SWAA2025022586029](https://openairdocs.org/sdr/SWAA2025022586029), Jan 14, 2025: SLAT. CRACKED. LH WING #2 SLAT FOUND CRACK AT LEADING EDGE NOSE SKIN LOWER SURFACE FASTENER; MARKED <[01]. REPAIRED LH WING #2 SLAT AT LEADING EDGE NOSE SKIN LOWER SURFACE IAW
- [SDR SWAA2025022586030](https://openairdocs.org/sdr/SWAA2025022586030), Jan 14, 2025: SLAT. CRACKED. LH WING #4 SLAT FOUND CRACK AT LEADING EDGE NOSE SKIN LOWER SURFACE FASTENER; MARKED <[01]. REPAIRED LH WING #4 SLAT AT LEADING EDGE NOSE SKIN LOWER SURFACE IAW
- [SDR SWAA2024110455247](https://openairdocs.org/sdr/SWAA2024110455247), Oct 30, 2024: ACM. SEIZED. ON CLIMB OUT F/A NOTICED SMOKE SMELL. NO SMOKE VISIBLE+ SMELL CLEARED AFTER A MINUTE. RAN PACKS FUL COLD BUT DUCT TEMP NEVER WENT BELOW 80 DEGREES. AFTER LANDIN
- [SDR SWAA2024091135478](https://openairdocs.org/sdr/SWAA2024091135478), Sep 8, 2024: CHARGER. INOPERATIVE. 3 INTERIOR AND 1 EXTERIOR EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED CHARGER ASSEMBLY AND BATTERY PACK FWD OF LH EMERGENCY EXIT DOOR IAW AMM 33-51-06. OPS 
- [SDR SWAA2023110316359](https://openairdocs.org/sdr/SWAA2023110316359), Oct 31, 2023: SEAL. CRACKED. -LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED.<[01] REMOVED AND REPLACED LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM 53-31-31
- [SDR SWAA2023072882803](https://openairdocs.org/sdr/SWAA2023072882803), Jul 27, 2023: PANEL. OUT OF ADJUST. RH WING INBOARD FIXED TRAILING EDGE UPPER PANEL IS OUT OF ADJUSTMENT.<[01] ADJUSTED PANEL REF AMM 57-50-01.;[02] REMOVED INSPECTION REQUIREMENTS. ADJUSTED PANEL

All 291: https://openairdocs.org/aircraft/N215WN/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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