# N232WN: 2006 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: 32500
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 2, 2006
- Certificate issued: April 7, 2006
- Expires: March 31, 2030
- Mode S code: A211EF
- 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=232WN
- Page: https://openairdocs.org/aircraft/N232WN

From the FAA registry file of October 21, 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/N232WN/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; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA15CA176](https://openairdocs.org/ntsb/DCA15CA176), Aug 23, 2015: Boeing 737 7H4 (N232WN), Oakland, CA, no damage. Probable cause: inadvertent jet blast, resulting in debris striking ground operations personnel.

## FAA accident and incident reports

None matched to N232WN.

## Service difficulty reports (294, newest 50)

As reported by operators and repair stations.

- [SDR SWAA2026072757416](https://openairdocs.org/sdr/SWAA2026072757416), Jul 22, 2026: LIGHT. INOPERATIVE. EMERGENCY LIGHT AT SEAT 17ABC INOPERATIVE. REMOVED AND REPLACED EMERGENCY AREA LIGHT AT SEAT 17ABC IAW AMM 33-51-03-960-801 OPS CHECK GOOD.
- [SDR SWAA2026062213874](https://openairdocs.org/sdr/SWAA2026062213874), Jun 18, 2026: GIRT BAR. OUT OF ADJUST. AFTER ENTRY GIRT BAR DOES NOT SEAT FIRMLY IN CLIPS. INSPECTED AND CLEANED AFT ENTRY GIRT BAR. OPS CHKD GOOD IAW SIP.
- [SDR SWAA2026061510946](https://openairdocs.org/sdr/SWAA2026061510946), Jun 10, 2026: SLIDE. OUT OF POSITION. R2 DOOR ESCAPE SLIDE PROTRUDING FROM SLIDE BOX. TUCKED SLIDE FLAP INTO SLIDE COMPARTMENT IAW SIP
- [SDR SWAA2026050494367](https://openairdocs.org/sdr/SWAA2026050494367), May 1, 2026: BRACKET. LOOSE. FWD SERVICE SLIDE CONTAINER AFT BRACKET IS LOOSE THAT HOLDS GIRT BAR FWD SERVICE DOOR SLIDE CONTAINER AFT BRACKET IS LOOSE THAT HOLDS GIRT BAR. R&R FASTENERS ON
- [SDR SWAA2026021169009](https://openairdocs.org/sdr/SWAA2026021169009), Feb 9, 2026: LIGHT. INOPERATIVE. RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. R & R RT OVERWING EMERGENCY EXIT LIGHT BULB AND LENS IAW AMM 33-51-04. OPS CHECKED GOOD.
- [SDR SWAA2025081292284](https://openairdocs.org/sdr/SWAA2025081292284), Jul 17, 2025: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP AT PAX CABIN BS 727B, S7L. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1102 REV -.
- [SDR SWAA2025081292089](https://openairdocs.org/sdr/SWAA2025081292089), Jul 16, 2025: STRAP. CORRODED. CORROSION ON STRAP AT MID CABIN BS 703, LBL 68, WL 203. REFER TO FAULT TTG8Q013SLHA. EA 25-153-01977.
- [SDR SWAA2025081292091](https://openairdocs.org/sdr/SWAA2025081292091), Jul 16, 2025: STRAP. CORRODED. CORROSION ON STRAP AT MID CABIN, BS 709, LBL 63, WL 203. REFER TO FAULT TTG8Q013SLHA WHERE EA 25-153-01977 WAS ADDED AS A SUBTASK.
- [SDR SWAA2025081292092](https://openairdocs.org/sdr/SWAA2025081292092), Jul 16, 2025: STRAP. CORRODED. CORROSION ON STRAP AT MID CABIN, BS 713, LBL 64 - LBL 67, WL 203. REFER TO FAULT TTG8Q013SLHA WHERE EA 25-153-01977 WAS ADDED AS A SUBTASK.
- [SDR SWAA2025081292085](https://openairdocs.org/sdr/SWAA2025081292085), Jul 16, 2025: FLOORBEAM. CRACKED. CRACKED PANEL BREAK AT PASSENGER CABIN BS 540, LBL 26, WL 208. REPLACED PANEL BREAK IAW SRM 51-40-02, AND BOEING DWG 143A0060 REV:-;[02] VERIFIED ACTION 1.<BR>J
- [SDR SWAA2025081292086](https://openairdocs.org/sdr/SWAA2025081292086), Jul 16, 2025: FLOORBEAM. CRACKED. CRACKED PANEL BREAK AT PASSENGER CABIN BS 540, LBL 1, WL 208. REPLACED PANEL BREAK PASSENGER CABIN BS540 LBL1 IAW SRM 51-40-02 AND DWG 143A0060 REV-.
- [SDR SWAA2025081292088](https://openairdocs.org/sdr/SWAA2025081292088), Jul 16, 2025: STRAP. CORRODED. CORROSION ON STRAP AT MID CABIN BS692 LBL68 WL203. REMOVED CORROSION ON STRAP BS 692, LBL 68, WL 203 AND ACCOMPLISHED REWORK OF STRAP IAW EA 25-153-01977.
- [SDR SWAA2025081292087](https://openairdocs.org/sdr/SWAA2025081292087), Jul 16, 2025: STRAP. CORRODED. CORROSION ON STRAP AT MID CABIN BS718 RBL62 WL203. CORROSION ON STRAP AT MID CABIN BS718 RBL62 WL203 REPAIRED PER EA 25-153-01971-WIP1.
- [SDR SWAA2025081291672](https://openairdocs.org/sdr/SWAA2025081291672), Jul 15, 2025: SUPPORT. CORRODED. CORROSION ON AFT BULKHEAD SUPPORT BS 947; RBL 20; WL 160. REMOVED AND REPLACED AFT BULKHEAD SUPPORT STA 947. STR 25L-STR 25R IAW SRM 51-40-02; DWG 149A8117 REV:
- [SDR SWAA2025081291365](https://openairdocs.org/sdr/SWAA2025081291365), Jul 14, 2025: SIDEWALL SUPPORT. CORRODED. CORROSION ON AFT CARGO COMPARTMENT R/H FLOOR TO SIDEWALL SUPPORT BS 867+10, 867+15-16, RBL 22, WL 158. REMOVED AND REPLACED ON AFT CARGO COMPARTMENT R/H FLOOR S
- [SDR SWAA2025081291379](https://openairdocs.org/sdr/SWAA2025081291379), Jul 14, 2025: SHIELD. CORRODED. CORROSION ON AFT CARGO COMPARTMENT AFT SHIELD BS 847-867, RBL 22, WL 157. NO ALLOWABLE DAMAGE GIVEN FOR THIS PART IN SRM 53-00-53-1A-2. REPAIRED BY REPLACEMENT 
- [SDR SWAA2025081291349](https://openairdocs.org/sdr/SWAA2025081291349), Jul 14, 2025: SHIELD. CORRODED. CORROSION ON FWD CARGO COMPARTMENT SHIELD BS 500+6, 500+10, RBL 22, WL 156. CORROSION FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2. REPAIR B
- [SDR SWAA2025081291350](https://openairdocs.org/sdr/SWAA2025081291350), Jul 14, 2025: SIDEWALL SUPPORT. CORRODED. CORROSION ON FWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT BS 400-500D, LBL 22, WL 157. SUPPORT HAS MISSING FASTENER AND IS NOT DRILLED AT BS 396, LBL 22, WL 
- [SDR SWAA2025081291351](https://openairdocs.org/sdr/SWAA2025081291351), Jul 14, 2025: SIDEWALL SUPPORT. CORRODED. CORROSION ON FWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT BS 500A-500D; RBL 22; WL 157. REMOVED AND REPLACED SIDEWALL SUPPORT IAW SRM 51-4-02 AND DWG 143A750
- [SDR SWAA2025081291373](https://openairdocs.org/sdr/SWAA2025081291373), Jul 14, 2025: SHIELD. CORRODED. CORROSION ON AFT CARGO COMPARTMENT FWD SHIELD BS 767-787, RBL 22, WL 156-157. INSTALLED NEW SHIELD IAW SRM 51-40-02, 51-40-05, AND DWG 146A8127 REV -.
- [SDR SWAA2025081291375](https://openairdocs.org/sdr/SWAA2025081291375), Jul 14, 2025: SIDEWALL SUPPORT. CORRODED. CORROSION ON AFT CARGO COMPARTMENT L/H FLOOR TO SIDEWALL SUPPORT BS 727+4 - 787+1-10, LBL 22, WL 156. REMOVED AND REPLACED AFT CARGO COMPARTMENT LT FLOOR TO SID
- [SDR SWAA2025081291376](https://openairdocs.org/sdr/SWAA2025081291376), Jul 14, 2025: SIDEWALL SUPPORT. CORRODED. CORROSION ON AFT CARGO COMPARTMENT R/H FLOOR TO SIDEWALL SUPPORT STA 727+4-767 RBL 22; WL 156. REMOVED OLD AND INSTALLED NEW AFT CARGO COMPARTMENT R/H FLOOR TO 
- [SDR SWAA2025081291377](https://openairdocs.org/sdr/SWAA2025081291377), Jul 14, 2025: SIDEWALL SUPPORT. CORRODED. CORROSION ON AFT CARGO COMPARTMENT R/H FLOOR TO SIDEWALL SUPPORT STA 887+4-887+12; 907+2; RBL 22; WL 159. REMOVED AND REPLACED ON AFT CARGO COMPARTMENT R/H FLOO
- [SDR SWAA2025081291378](https://openairdocs.org/sdr/SWAA2025081291378), Jul 14, 2025: STRAP. CORRODED. CORROSION ON AFT CARGO COMPARTMENT FLOOR TIEDOWN STRAP STA 887; BETWEEN FLOOR PANELS 140CF-140DF. REMOVED AND REPLACED SPLICE / TEE ASSY IAW SRM 51-40-05 AND DW
- [SDR SWAA2025081291371](https://openairdocs.org/sdr/SWAA2025081291371), Jul 14, 2025: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK LBL 45 AT STA 616+18 APPROX.; BS 663; BS 663+12 APPROX.; STA 685+12 APPROX. AND AT STA 727A+10 APPROX. WAS FOUND CORRODED ON CROWN. REMOVE
- [SDR SWAA2025081291364](https://openairdocs.org/sdr/SWAA2025081291364), Jul 14, 2025: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK LBL 45 AT STA 540 AND STA 727+12 APPROX. WAS FOUND MECHANICAL DAMAGE ON CROWN. AND AT STA 559+10 APPROX. WAS FOUND CORROSION ON WELL. SEAT
- [SDR SWAA2025081203486](https://openairdocs.org/sdr/SWAA2025081203486), Jul 11, 2025: STRINGER. CRACKED. CRACKED STRINGER AT AREA AFT OF FCB BS535 S-23L WL164. REMOVED DAMAGED STRINGER S-23L BS 540 - BS500D+10; FABRICATED AND INSTALLED NEW STRINGER AND SPLICE AT ST
- [SDR SWAA2025081290412](https://openairdocs.org/sdr/SWAA2025081290412), Jul 11, 2025: STRINGER. CRACKED. CRACKED STRINGER AT AREA AFT OF FCB BS 535, S-23L, WL164. REMOVED DAMAGED STRINGER S-23L BS 540 - BS500D+10; FABRICATED AND INSTALLED NEW STRINGER AND SPLICE AT
- [SDR SWAA2025081290413](https://openairdocs.org/sdr/SWAA2025081290413), Jul 11, 2025: STRINGER. CRACKED. CRACKED STRINGER AT AREA AFT OF FCB BS535 S-26L WL153. REMOVED DAMAGED STRINGER S-26L BS 540 - BS500D+10; FABRICATED AND INSTALLED NEW STRINGER AND SPLICE AT ST
- [SDR SWAA2025081203487](https://openairdocs.org/sdr/SWAA2025081203487), Jul 11, 2025: STRINGER SPLICE. CRACKED. CRACKED STRINGER AT AREA AFT OF FCB BS535 S-26L WL153. REMOVED DAMAGED STRINGER S-26L BS 540 - BS500D+10; FABRICATED AND INSTALLED NEW STRINGER AND SPLICE AT ST
- [SDR SWAA2025081290534](https://openairdocs.org/sdr/SWAA2025081290534), Jul 11, 2025: PLATE. CRACKED. RIGHT WING T/E WIGGLE PLATE AT ORSS 261 IS CRACKED.
- [SDR SWAA2025081290178](https://openairdocs.org/sdr/SWAA2025081290178), Jul 10, 2025: SCUFF PLATE. CRACKED. FWD CARGO COMPARTMENT FWD CORNER SCUFF PLATE IS CRACKED. REPAIRED FWD CARGO COMPARTMENT FWD CORNER SCUFF PLATE PER SRM 53-30-15-2R-1, SOPM 20-43-03, SOPM 20-41-
- [SDR SWAA2025081289830](https://openairdocs.org/sdr/SWAA2025081289830), Jul 10, 2025: STUB FRAME. CRACKED. CRACK FOUND ON STUB FRAME BS 294.5 +8.5'; ABOVE SEAL DEPRESSOR, BETWEEN S8R AND S9R; LENGTH 1.4'. REMOVED OLD FWD SERVICE DOOR STUB FRAME BS 294 +8.5' IAW SRM 5
- [SDR SWAA2025081489485](https://openairdocs.org/sdr/SWAA2025081489485), Jul 9, 2025: ASSIST HANDLE. BROKEN. AFT SERVICE DOOR SURROUND ASSIST HANDLE IS BROKEN.
- [SDR SWAA2025081289822](https://openairdocs.org/sdr/SWAA2025081289822), Jul 9, 2025: RIB. CRACKED. L/H HORIZONTAL STAB REMOVABLE L/E; 3RD RIB FROM I/B END IS CRACKED. REMOVED AND REPLACED 3RD RIB FROM I/B END OF L/H HORIZONTAL STAB. L/E IAW SRM 51-40-02-0G-0 
- [SDR SWAA2025081289823](https://openairdocs.org/sdr/SWAA2025081289823), Jul 9, 2025: RIB. CRACKED. L/H HORIZONTAL STAB REMOVABLE L/E; 4TH RIB FROM I/B END IS CRACKED. REMOVED AND REPLACED 4TH RIB FROM I/B END OF L/H HORIZONTAL STAB. L/E IAW SRM 51-40-02-0G-0 
- [SDR SWAA2025081289824](https://openairdocs.org/sdr/SWAA2025081289824), Jul 9, 2025: RIB. CRACKED. L/H HORIZONTAL STAB REMOVABLE L/E; 5TH RIB FROM I/B END IS CRACKED. REMOVED AND REPLACED 5TH RIB FROM I/B END OF L/H HORIZONTAL STAB. L/E IAW SRM 51-40-02-0G-0 
- [SDR SWAA2025081289062](https://openairdocs.org/sdr/SWAA2025081289062), Jul 8, 2025: RIB. CRACKED. RIGHT HORIZONTAL STAB RIB 5 STIFFENER HAS CRACK ON LOWER RADIUS. REPAIRED RT HORIZONTAL STAB RIB 5, STAB STA 129.5 IAW SRM 51-40-2-0G-0 AND SRM 55-10-09-2R-4 RE
- [SDR SWAA2025081289464](https://openairdocs.org/sdr/SWAA2025081289464), Jul 8, 2025: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 232SF HAS AREAS OF DELAMINATION ON UPPER SKIN. FABRICATED NEW FLOOR PANEL 232SF IAW SRM 53-00-50-2R-0 AND DWG 144A5810 SHEET 159.
- [SDR SWAA2025081289466](https://openairdocs.org/sdr/SWAA2025081289466), Jul 8, 2025: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 241AF HAS AREAS OF DELAMINATION ON UPPER SKIN. FLOOR PANEL 241AF WITH AREAS OF UPPER SURFACE DELAMINATION WAS REPLACED BY FABRICATIN
- [SDR SWAA2025081289467](https://openairdocs.org/sdr/SWAA2025081289467), Jul 8, 2025: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 241BF HAS AREAS OF DELAMINATION ON UPPER SKIN. FLOOR PANEL 241BF WITH AREAS OF UPPER SURFACE DELAMINATION WAS REPLACED BY FABRICATIN
- [SDR SWAA2025081289468](https://openairdocs.org/sdr/SWAA2025081289468), Jul 8, 2025: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 242AF HAS AREAS OF DELAMINATION ON UPPER SKIN. FABRICATION OF NEW 242AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-
- [SDR SWAA2025081289469](https://openairdocs.org/sdr/SWAA2025081289469), Jul 8, 2025: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 242BF HAS AREAS OF DELAMINATION ON UPPER SKIN. FABRICATED NEW FLOOR PANEL 242BF IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0122.
- [SDR SWAA2025081289470](https://openairdocs.org/sdr/SWAA2025081289470), Jul 8, 2025: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 241EF HAS AREAS OF DELAMINATION ON UPPER SKIN. FLOOR PANEL 241EF WITH AREAS OF DELAMINATION ON UPPER SKIN WAS REPLACED BY FABRICATIN
- [SDR SWAA2025081289471](https://openairdocs.org/sdr/SWAA2025081289471), Jul 8, 2025: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 241FF HAS AREAS OF DELAMINATION ON UPPER SKIN. FLOOR PANEL 241FF WITH AREAS OF UPPER SKIN DELAMINATION WAS REPLACED BY FABRICATING A
- [SDR SWAA2025081289472](https://openairdocs.org/sdr/SWAA2025081289472), Jul 8, 2025: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 242CF HAS AREAS OF DELAMINATION ON UPPER SKIN. FLOOR PANEL 242CF WITH AREAS OF UPPER SURFACE DELAMINATION WAS REPLACED BY FABRICATIN
- [SDR SWAA2025081189462](https://openairdocs.org/sdr/SWAA2025081189462), Jul 8, 2025: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 231XF HAS AREAS OF DELAMINATION ON UPPER SKIN. FABRICATED NEW FLOOR PANEL 231XF IAW SRM 53-00-50-2R-0 AND BOEING DRAWING 144A5810 SH
- [SDR SWAA2025081189463](https://openairdocs.org/sdr/SWAA2025081189463), Jul 8, 2025: FLOOR PANEL. DELAMINATED. PASSENGER CABIN FLOOR PANEL 231YF HAS AREAS OF DELAMINATION ON UPPER SKIN. FABRICATED NEW FLOOR PANEL 231YF IAW SRM 53-00-50-2R-0 AND BOEING DRAWING 144A5810 SH
- [SDR SWAA2025081289061](https://openairdocs.org/sdr/SWAA2025081289061), Jul 7, 2025: SKIN. PULLED. L/H ENGINE INLET COWL BARREL SKIN HAS A PULLED THROUGH FASTENER AT 10:00 O'CLOCK POSITION.NR 1 ENGINE INLET COWL WAS REMOVED AND REPLACED ON CARD 7111-E-17062-N
- [SDR SWAA2025050667558](https://openairdocs.org/sdr/SWAA2025050667558), May 4, 2025: LENS. DISPLACED. RAMP REPORTS. EMERGENCY LIGHT LENSE DISPLACED AIRCRAFT LEFT AFT<[01] SECURED EMERGENCY LIGHT LENSE REF SIP

All 294: https://openairdocs.org/aircraft/N232WN/reports.md

## Related

- Other Boeing 737-7H4 aircraft: https://openairdocs.org/model/boeing-737-7h4/aircraft.md
- STCs for the Boeing 737-7H4: https://openairdocs.org/model/boeing-737-7h4/stcs.md
- The CFM International CFM56 series engine: https://openairdocs.org/engine/cfm-international-cfm56-series.md

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