# N225WN: 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: 34333
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 7, 2005
- Certificate issued: January 5, 2006
- Expires: June 30, 2029
- Mode S code: A1F595
- 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=225WN
- Page: https://openairdocs.org/aircraft/N225WN

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/N225WN/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 DCA24FA300](https://openairdocs.org/ntsb/DCA24FA300), Sep 12, 2024: Boeing 737-7H4 (N225WN), Nashville, TN, incident, no damage, investigation ongoing

## FAA accident and incident reports

None matched to N225WN.

## Service difficulty reports (289, 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 SWAA2026072069448](https://openairdocs.org/sdr/SWAA2026072069448), Jul 17, 2026: PROBE. FAULTED. NR 1 ENGINE HIGH EGT ON T/O CLIMB. PERFORMED EA M-21-177-01860 UP TO STEP 19 FOUND CJ10 HARNESS FAULTY. R & R CJ10 HARNESS IAW AMM 73-21-06. STILL REQUIRES STEP
- [SDR SWAA20260720694UI](https://openairdocs.org/sdr/SWAA20260720694UI), Jul 17, 2026: WIRE HARNESS. FAULTY. ON CLIMBOUT APPROX 5,000FT NUMBER ONE ENGINE EGT WENT INTO REDLINE & COMPLETED APPROPRIATE QRC AND QRH CHECKLIST AND DIVERTED TO LAX. LANDED NORMALLY WITHOUT IS
- [SDR SWAA2026062915293](https://openairdocs.org/sdr/SWAA2026062915293), Jun 24, 2026: ANGLE. CRACKED. AFT FIXED T/E L ANGLE THAT ATTACHES TO THE FLAP PROGRAMING BEAM IS CRACKED. REMOVED AND REPLACED 1 EACH AFT FIXED T/E L ANGLE THAT ATTACHES TO THE FLAP PROGRAMM
- [SDR SWAA2026062915291](https://openairdocs.org/sdr/SWAA2026062915291), Jun 24, 2026: FITTING. CRACKED. AFT UPPER FIXED T/E SEAL RETAINER IS CRACKED JUST INBD OF FLAP PROGRAMING BEAM. REMOVED AND REPLACED SEAL RETAINER FITTING IAW SRM 51-40-02.;[02] C/W INSPECTION
- [SDR SWAA2026062515277](https://openairdocs.org/sdr/SWAA2026062515277), Jun 24, 2026: LIGHT. DAMAGED. PASSENGER CABIN SEAT ROW 27ABC AND 27DEF PHOTOLUMINESCENT STRIPS HAS MOISTURE UNDER LENS. REMOVED AND REPLACED IAW AMM 33-51-15-400-802.
- [SDR SWAA2026062515294](https://openairdocs.org/sdr/SWAA2026062515294), Jun 24, 2026: BATTERY PACK. FAILED. FOUR EMERGENCY LIGHT BATTERY PACK FAILED THE CAPACITY TEST FWD AND AFT ENTRY DOORS AND SERVICE DOORS. REMOVED AND REPLACED BATTERY PACKS FWD LT AND RT BATTERY P
- [SDR SWAA2026050494549](https://openairdocs.org/sdr/SWAA2026050494549), Apr 30, 2026: GUARD. MISSING. AFT F/A PANEL EMERGENCY LIGHT SWITCH GUARD MISSING. R & R SWITCH PANEL ASSY REF SWPM 20-71-03 OPS CHECK NORMAL IAW AMM 33-51-00.
- [SDR SWAA2025092215252](https://openairdocs.org/sdr/SWAA2025092215252), Sep 16, 2025: SIGN. DETACHED. OVERHEAD EXIT SIGN MID CABIN FALLING OFF CEILING. RESECURED OVERHEAD EXIT SIGN MID CABIN AS REQUIRED PER M/M 33-51-01. OPS NORMAL.
- [SDR SWAA2025071683989](https://openairdocs.org/sdr/SWAA2025071683989), Jun 20, 2025: RIB. CRACKED. CRACK ACCESS PANEL 341B LEADING EDGE RIB LOCATED LE STA 105.26 RT HORIZONTAL STAB. REPLACED RIB LOCATED LEADING EDGE LE STA 105.26 ON RT HORIZONTAL STAB IAW B73
- [SDR SWAA2025071683206](https://openairdocs.org/sdr/SWAA2025071683206), Jun 19, 2025: LENS. BROKEN. BROKEN EMERGENCY EXIT LENS LAVATORY A AT FWD GALLEY AREA (1 EA). REPLACED EMERGENCY EXIT LENS LAVATORY A AT FWD GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-01-960
- [SDR SWAA2025071683209](https://openairdocs.org/sdr/SWAA2025071683209), Jun 19, 2025: LENS. BROKEN. BROKEN EMERGENCY EXIT LENS LAVATORY B AT AFT GALLEY AREA (1 EA). REPLACED EMERGENCY EXIT LENS LAVATORY B AT AFT GALLEY AREA (1 EA) IAW AMM 33-51-01-960-801 PROC
- [SDR SWAA2025071683208](https://openairdocs.org/sdr/SWAA2025071683208), Jun 19, 2025: LENS. BROKEN. BROKEN EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA). REPLACED EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA IAW AMM 33-51-01-960-802 STEP 3.C. ITEM 
- [SDR SWAA2025071683212](https://openairdocs.org/sdr/SWAA2025071683212), Jun 19, 2025: HOUSING. BROKEN. BROKEN HOUSING ASSY EMERGENCY LIGHT OVERHEAD STOWAGE BIN 3 LH SIDE AT PASSENGER CABIN. REPLACED HOUSING ASSY EMERGENCY LIGHT OVERHEAD STOWAGE BIN 3 LH SIDE AT P
- [SDR SWAA2025071682978](https://openairdocs.org/sdr/SWAA2025071682978), Jun 18, 2025: STRINGER. CRACKED. CRACK STRINGER 25L LOCATED BS540 FWD CARGO COMPARTMENT. REPAIRED STRINGER 25L LOCATED BS540 FWD CARGO COMPARTMENT IAW SRM 53-00-03-2R-1 REPAIR 1.
- [SDR SWAA2025071682801](https://openairdocs.org/sdr/SWAA2025071682801), Jun 17, 2025: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED BS 259.5 AND S-8L PASSENGER CABIN. REPLACED SUPPORT ANGLE LOCATED BS 259.5 AND S-8L PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0;S
- [SDR SWAA2025071682182](https://openairdocs.org/sdr/SWAA2025071682182), Jun 15, 2025: SUPPORT BRACKET. CORRODED. CORROSION SUPPORT BRACKET LOCATED BS986.5 TO BS1006 AND WL156 AT AFT CARGO COMPARTMEN. REPLACED SUPPORT BRACKET (DRAIN MAST SUPPORT) LOCATED BS 986.5 TO BS 1006
- [SDR SWAA2025071682180](https://openairdocs.org/sdr/SWAA2025071682180), Jun 15, 2025: PANEL. CORRODED. CORROSION O/B FIXED LEADING EDGE FUEL QUANTITY INDICATOR HOUSING AT RT WING . REPAIRED FUEL SYSTEM PANEL LEADING EDGE BTW SS150.81 & SS163.95 RT WING IAW EA# 25
- [SDR SWAA2025071682181](https://openairdocs.org/sdr/SWAA2025071682181), Jun 15, 2025: STRINGER. CORRODED. CORROSION ON STRINGER 25L LOCATED BS947.5 TO BS967 AND WL156 AT AFT CARGO COMPARTMENT. SRM SUPPLEMENT WAS NOT CONSULTED FOR REPAIR INSTRUCTIONS STEP 15 ITEM 2;[
- [SDR SWAA2025071681666](https://openairdocs.org/sdr/SWAA2025071681666), Jun 14, 2025: SUPPORT. CORRODED. CORROSION ON SUPPORT STRUCTURE LOCATED BS947.5 AT LEVEL STR25L TO STR25R AT AFT CARGO COMPARTMENT. REPLACED SUPPORT STRUCTURE LOCATED BS947.5 AT LEVEL STR25L TO
- [SDR SWAA2025071681667](https://openairdocs.org/sdr/SWAA2025071681667), Jun 14, 2025: STUB FRAME. CRACKED. CRACK ON STUB FRAME LOCATED BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA. REPLACED STUB FRAME LOCATED BS 294.5 AT LEVEL STR 14R TO 17R AT FWD GALLEY AREA IAW B7
- [SDR SWAA2025071681670](https://openairdocs.org/sdr/SWAA2025071681670), Jun 14, 2025: SUPPORT BRACKET. CRACKED. CRACK ON SUPPORT BRACKET BULKHEAD AREA LOCATED BS727 AT LEVEL BL 0 AT AFT CARGO COMPARTMENT. REPLACED SUPPORT BRACKET BULKHEAD AREA LOCATED BS727 AT LEVEL BL 0 
- [SDR SWAA2025071681668](https://openairdocs.org/sdr/SWAA2025071681668), Jun 14, 2025: INTERCOSTAL. CRACKED. CRACK ON INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA. REPAIRED INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16
- [SDR SWAA2025071681662](https://openairdocs.org/sdr/SWAA2025071681662), Jun 14, 2025: STUB FRAME. CRACKED. CRACK INDICATION ON STUB FRAME LOCATED BTW BS 294.5 TO BS 296 AND S-8R TO S-9R AT FWD GALLEY DOOR AREA(1EA). CRACK LENGTH APPROX 0.312 INCH AT PASSENGER CABIN. 
- [SDR SWAA2025071681867](https://openairdocs.org/sdr/SWAA2025071681867), Jun 14, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BS 695 AND BL0 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE LOCATED BS 695 AND BL0 AT PASSENGER CABIN AND FASTENERS IAW B737-700 SR
- [SDR SWAA2025071681669](https://openairdocs.org/sdr/SWAA2025071681669), Jun 14, 2025: SUPPORT WEB. CRACKED. CRACK ON SUPPORT WEB CEILING AREA LOCATED BS847 TO BS867 AT LEVEL LBL24 AT AFT CARGO COMPARTMENT. REPLACED SUPPORT WEB CEILING AREA AND FASTENER LOCATED BS847 T
- [SDR SWAA2025071681665](https://openairdocs.org/sdr/SWAA2025071681665), Jun 14, 2025: INTERCOSTAL. CORRODED. CORROSION WEB - INTERCOSTAL LOCATED BS767 TO BS787 AND STR25R AT AFT CARGO COMPARTMENT. REPLACED WEB - INTERCOSTAL LOCATED BS767 TO BS787 AND STR25R AT AFT CARG
- [SDR SWAA2025071681663](https://openairdocs.org/sdr/SWAA2025071681663), Jun 14, 2025: SUPPORT ANGLE. CRACKED. CRACK ON CARGO LINER SUPPORT ANGLE CEILING AREA LOCATED BS727C AT LEVEL LBL 45 AT AFT CARGO COMPARTMENT. REPAIRED CARGO LINER SUPPORT ANGLE CEILING AREA LOCATED
- [SDR SWAA2025071681458](https://openairdocs.org/sdr/SWAA2025071681458), Jun 13, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED FRONT SPAR BOOST PUMP IFSS 116 TO IFSS 126 AT RT WING. REPLACED SUPPORT ANGLE LOCATED FRONT SPAR BOOST PUMP IFSS 116 TO IFSS 126 
- [SDR SWAA2025071681659](https://openairdocs.org/sdr/SWAA2025071681659), Jun 13, 2025: FRAME. CRACKED. CRACK ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA. REPAIRED FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA IAW B737-700 EA M-2
- [SDR SWAA2025071681660](https://openairdocs.org/sdr/SWAA2025071681660), Jun 13, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BS 294.5 BTW STR 13L TO STR 14L AT FWD GALLEY AREA. REPLACED SUPPORT ANGLE LOCATED BS 294.5 BTW STR 13L TO STR 14L AT FWD GALLEY 
- [SDR SWAA2025071681460](https://openairdocs.org/sdr/SWAA2025071681460), Jun 13, 2025: ACCESS PANEL. CRACKED. CRACK BLADE ACCESS PANEL 343AB AT RT HORIZONTAL STAB. REPLACED ON BLADE ACCESS PANEL 343AB AT RT HORIZONTAL STAB IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9.
- [SDR SWAA2025071680989](https://openairdocs.org/sdr/SWAA2025071680989), Jun 12, 2025: SUPPORT ANGLE. CORRODED. CORROSION ANGLE - SUPPORT LOCATED BS 500D AND BTW STR26R TO STR26L WL 156 FWD CARGO COMPARTMENT. EVALUATED ANGLE - SUPPORT LOCATED BS 500D AND BTW STR26R TO STR
- [SDR SWAA2025071680987](https://openairdocs.org/sdr/SWAA2025071680987), Jun 12, 2025: FRAME. CRACKED. CRACK WEB FRAME LOCATED BS 259.5 BETWEEN S-8R TO S-9R AT PASSENGER CABIN. REPAIRED WEB FRAME LOCATED BS 259.5 BTW WL240 AND WL280 AND BTW RBL20 TO RBL50 AT PASS
- [SDR SWAA2025071681294](https://openairdocs.org/sdr/SWAA2025071681294), Jun 12, 2025: WEB. CORRODED. CORROSION UPPER SILL WEB LOCATED BTW BS440 TO BS494 AT LEVEL STR18R WL196 AT FWD CARGO COMPARTMENT. REPLACED UPPER SILL WEB LOCATED BTW BS440 TO BS494 AT LEVEL 
- [SDR SWAA2025071681292](https://openairdocs.org/sdr/SWAA2025071681292), Jun 12, 2025: SUPPORT ANGLE. CRACKED. CRACK ANGLE - SUPPORT LOCATED BS440 AND STR26L FWD CARGO COMPARTMENT. REPLACED ANGLE - SUPPORT LOCATED BS440 AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 5
- [SDR SWAA2025071680993](https://openairdocs.org/sdr/SWAA2025071680993), Jun 12, 2025: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR STRUCTURE SUPPORT ZEE LOCATED BTW BS500 TO BS500B AT LEVEL S-26L WL156 AT FWD CARGO COMPARTMENT. REMOVED DAMAGE AND EVALUATED REWORK AREAS ON
- [SDR SWAA2025071680062](https://openairdocs.org/sdr/SWAA2025071680062), Jun 10, 2025: LIGHT. BROKEN. BROKEN FLOOR PROXIMITY LIGHTING PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10 EA). REPLACED FLOOR PROXIMITY LIGHTING PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (
- [SDR SWAA2025071680234](https://openairdocs.org/sdr/SWAA2025071680234), Jun 10, 2025: SUPPORT ANGLE. CRACKED. CRACK ANGLE - SUPPORT LOCATED BS 500B FWD SIDE AND S-26L FWD CARGO COMPARTMENT 2025-371389<[01] REMPLACED ANGLE - SUPPORT LOCATED AND FASTENERS LOCATED BS 500B 
- [SDR SWAA2025071680231](https://openairdocs.org/sdr/SWAA2025071680231), Jun 10, 2025: GUSSET. CRACKED. CRACK GUSSET LOCATED BS 500D AND S-21L FWD CARGO COMPARTMENT. REPLACED GUSSET LOCATED BS 500D AND S-21L FWD CARGO COMPARTMEN IAW B737-700 SRM 51-10-02 ITEM 9 AN
- [SDR SWAA2025071680232](https://openairdocs.org/sdr/SWAA2025071680232), Jun 10, 2025: GUSSET. CRACKED. CRACK GUSSET LOCATED BS500D AND S-19L FWD CARGO COMPARTMENT. REPLACED GUSSET LOCATED BS500D AND S-19L FWD CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 AND
- [SDR SWAA2025071680463](https://openairdocs.org/sdr/SWAA2025071680463), Jun 10, 2025: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED BS 695 AND RBL 24.75 PASSENGER CABIN. REPLACED SUPPORT ANGLE LOCATED BS 695 AND RBL 24.75 PASSENGER CABIN IAW B737-700 51-10-02 ITEM
- [SDR SWAA2025071680461](https://openairdocs.org/sdr/SWAA2025071680461), Jun 10, 2025: STIFFENER. CRACKED. CRACK STIFFENER ASSY FLOOR STRUCTURE LOCATED BS540 AND BTW BL0 TO LBL 24.75 PASSENGER CABIN. REPLACED STIFFENER ASSY FLOOR STRUCTURE LOCATED BS540 AND BTW BL0 T
- [SDR SWAA2025071680464](https://openairdocs.org/sdr/SWAA2025071680464), Jun 10, 2025: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED BS 695 AND BL 0 PASSENGER CABIN. REPLACED SUPPORT ANGLE LOCATED BS 695 AND BL 0 PASSENGER CABIN IAW SRM 51-10-02 ITEM 9 AND DWG 273A
- [SDR SWAA2025071680462](https://openairdocs.org/sdr/SWAA2025071680462), Jun 10, 2025: STIFFENER. CRACKED. CRACK STIFFENER ASSY FLOOR STRUCTURE LOCATED BS540 AND BTW BL 0 TO RBL24.75 PASSENGER CABIN. REPLACED STIFFENER ASSY FLOOR STRUCTURE LOCATED BS540 AND BTW BL 0 
- [SDR SWAA2025071680063](https://openairdocs.org/sdr/SWAA2025071680063), Jun 10, 2025: SKIN. DELAMINATED. DELAMINATED TRAILING EDGE SPOILER 7 AT RT WING. REPAIRED TRAILING EDGE SPOILER 7 AT RT WING IAW B737-700 SRM 51-70-10-2R-4 REPAIR 4.
- [SDR SWAA2025071680061](https://openairdocs.org/sdr/SWAA2025071680061), Jun 9, 2025: BATTERY PACK. INOPERATIVE. INOP BATTERY PACK EMERGENCY EXIT DOOR LT SIDE PASSENGER CABIN (1EA). REPLACED BATTERY PACK EMERGENCY EXIT DOOR LT SIDE PASSENGER CABIN IAW B737-700 AMM 33-51-06
- [SDR SWAA2025071680060](https://openairdocs.org/sdr/SWAA2025071680060), Jun 9, 2025: BATTERY PACK. INOPERATIVE. INOP BATTERY PACK EMERGENCY EXIT DOOR RT SIDE PASSENGER CABIN (1EA). REPLACED BATTERY PACK EMERGENCY EXIT DOOR RT SIDE PASSENGER CABIN IAW AMM 33-51-06-960-805.
- [SDR SWAA2025071679675](https://openairdocs.org/sdr/SWAA2025071679675), Jun 8, 2025: HINGE. CORRODED. CORROSION HINGE WASTE SERVICE DOOR 145AL AT LOWER FUSELAGE 1 EA, REPLACED HINGE WASTE SERVICE DOOR 145AL AT LOWER FUSELAGE (1 EA) IAW SRM 51-10-02-0G-0 ITEM 9; 
- [SDR SWAA2025052273303](https://openairdocs.org/sdr/SWAA2025052273303), May 21, 2025: LIGHT. INOPERATIVE. RT EMERGENCY EXIT DOOR PASSENGER LIGHT INOP. <[01] RELAMPED PER AMM 33-51-01; [02] C/W INSP. RELAMPED PER AMM 33-51-01.
- [SDR SWAA2025021997331](https://openairdocs.org/sdr/SWAA2025021997331), Feb 18, 2025: HANDLE. BROKEN. DOOR HANDLE AFT ENTRY DOOR BROKE OFF<[01] R&R'D AFT ENTRY DOOR HANDLE PER 52-41-31;[02] R&R'D AFT ENTRY DOOR ASSIST HANDLE PER 52-13-31

All 289: https://openairdocs.org/aircraft/N225WN/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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