# N925WN: 2008 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 CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 36630
- Year built: 2008
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 30, 2008
- Certificate issued: April 9, 2025
- Expires: April 30, 2032
- Mode S code: ACD2BE
- 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: 32.6590° N, 96.8396° W: Placed by OpenAirDocs at the center of ZIP code 75232, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=925WN
- Page: https://openairdocs.org/aircraft/N925WN

From the FAA registry file of October 22, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every CFM International CFM56-7B24 model are included.

## ADs that may apply (OpenAirDocs): 19 in force

### Matched by airframe (Boeing 737-7H4)

None in force.

### Matched by engine (CFM International CFM56-7B24 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 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 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 2010-01-05](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 2009-11-02](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 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 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 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 2001-02-12](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 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

### 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 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

## Information bulletins (advisory) (1 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-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 N925WN.

## FAA accident and incident reports (1)

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

- [Incident 20091129052042I](https://openairdocs.org/incident/20091129052042I), Nov 29, 2009: Boeing 737-7H4 (N925WN), Salt Lake City, UT, Minor damage. On 11/29/09, at approximately 07:09 MST, a fedx DC-10 taxiing north on h clipped the right winglet of a swaa B-737. The top half of the winglet was severed off…

## Service difficulty reports (252, 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 SWAA2026061508637](https://openairdocs.org/sdr/SWAA2026061508637), Jun 2, 2026: FUSE. INOPERATIVE. EMERGENCY LIGHTS AT RT OVERWING EXIT HATCH INOPERATIVE. REMOVED AND REPLACED THE FUSE AND PERFROMED GOOD OPS TEST IAW AMM 33-51-06-960-804.
- [SDR SWAA2026061508638](https://openairdocs.org/sdr/SWAA2026061508638), Jun 2, 2026: FUSE. INOPERATIVE. EMERGENCY LIGHTS AT LT OVERWING HATCH INOPERATIVE. REPLACED FUSE, AND PERFORMED GOOD OPS TEST IAW AMM 33-51-06-960-804.
- [SDR SWAA2026061507012](https://openairdocs.org/sdr/SWAA2026061507012), May 27, 2026: FAN COWL. CRACKED. NUMBER 2 ENGINE O/B FAN COWL IS CRACKED AT FWD LOWER CORNER 3 INCHES FROM LEADING EDGE. REMOVED AND REPLACED PER AMM 71-11-02.
- [SDR SWAA2026061506484](https://openairdocs.org/sdr/SWAA2026061506484), May 26, 2026: SCUFF PLATE. OUT OF POSITION. FWD SERVICE DOOR SCUFF PLATE AFT VERTICAL HOLES DON'T LINE UP TO AIRCRAFT. LOCATED AND DRILLED FSD REPLACEMENT SCUFF PLATE IAW SRM 51-40-05-0G-0; INSTALLATION W
- [SDR SWAA2026061504197](https://openairdocs.org/sdr/SWAA2026061504197), May 18, 2026: ATTACH ANGLE. CRACKED. RIGHT BS 663, A CRACK FOUND ON VAPOR BARRIER UPPER ATTACH ANGLE AT RBL 25, WL 167.68. REMOVED DAMAGE AND REPAIRED IAW SRM 57-10-10-2R-5.
- [SDR SWAA2026061504198](https://openairdocs.org/sdr/SWAA2026061504198), May 18, 2026: ATTACH ANGLE. CRACKED. LEFT BS 663, CRACK FOUND ON VAPOR BARRIER UPPER ATTACH ANGLE AT LBL 25, WL 167.68. REMOVED DAMAGE AND REPAIRED IAW SRM 57-10-10-2R-5.
- [SDR SWAA2026061503106](https://openairdocs.org/sdr/SWAA2026061503106), May 14, 2026: FAIRING. CRACKED. NR 1 ENGINE AFT FAIRING AFT END IS CRACKED. REMOVED; AND REPLACED NR 1 ENGINE AFT FAIRING AFT END TRAILING EDGE ASSY IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; D
- [SDR SWAA2026061598287](https://openairdocs.org/sdr/SWAA2026061598287), May 13, 2026: SEAT TRACK. CORRODED. CORROSION ON PAX CABIN SEAT TRACK LBL 25 WL 208 STA 500A+10 WELL; STA 500D+10 TOP; STA 500D+10 WELL. REMOVED AND REPLACED SEAT TRACK AT 480-520 LBL25 IAW SRM 51
- [SDR SWAA2026061598289](https://openairdocs.org/sdr/SWAA2026061598289), May 13, 2026: RIB. CRACKED. CRACKED RIB RT INSPAR HORIZ STAB STA 120.30 COMMON TO UPPER RETURN FLANGE AND FWD SPAR. REPAIRED PER EA 26-155-01306. THIS IS A CATEGORY A REPAIR IAW SRM 51-00-
- [SDR SWAA2026061597632](https://openairdocs.org/sdr/SWAA2026061597632), May 12, 2026: RIB. CRACKED. RT HORZ STAB L/E 341B 4TH RIB FROM I/B CRACKED AT LE STA 105.26. CRACKED RIB FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN SRM. .REMOVED AND REPLACED 
- [SDR SWAA2026061597865](https://openairdocs.org/sdr/SWAA2026061597865), May 12, 2026: SKIN. CRACKED. CRACK ON RT LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90. CRACKED WAS FOUND TO BE OUT OF LIMITS; REMOVED DAMAGE AND REPAIRED AS PER SRM 55-10-01-2R-11 R
- [SDR SWAA2026061597617](https://openairdocs.org/sdr/SWAA2026061597617), May 11, 2026: BAFFLE. CRACKED. BAFFLE ANGLES CRACKED BS 500C AND BS 400 AFT SIDE OF FRAMES, LBL 25, WL 155. REMOVED AND REPLACED BAFFLE ANGLES IAW SRM 51-40-02-0G-0, AND DWG 143A7505, REV B.
- [SDR SWAA2026061597628](https://openairdocs.org/sdr/SWAA2026061597628), May 11, 2026: BAFFLE. CRACKED. BAFFLE ANGLE CRACKED BS 500C FWD SIDE OF FRAME, LBL 25, WL 155. REMOVED AND REPLACED BAFFLE ANGLE IAW SRM 51-40-02-0G-0; AND DWG 143A7505, REV B.
- [SDR SWAA2026061597457](https://openairdocs.org/sdr/SWAA2026061597457), May 11, 2026: STRAP. CORRODED. CORROSION ON STRAP AT BS 1019-1032 LBL 3 WL 208. REMOVED AND REPLACED STRAP IAW SRM 51-40-02-0G-0 AND DWG 147A5600, SHEET 32, REV B.
- [SDR SWAA2026061597458](https://openairdocs.org/sdr/SWAA2026061597458), May 11, 2026: STRAP. CORRODED. CORROSION ON STRAP AT BS 1025 RBL 3 WL 208. REMOVED AND REPLACED STRAP IAW SRM 51-40-02-0G-0 AND DWG 147A5730, SHEET 23, REV C.
- [SDR SWAA2026061597462](https://openairdocs.org/sdr/SWAA2026061597462), May 11, 2026: FLOOR SUPPORT. CRACKED. CRACKED FLOOR SUPPORT AT BS 344 - 360, LBL 11, WL 208. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 141A5400, SHEET 46, REV A.
- [SDR SWAA2026061597464](https://openairdocs.org/sdr/SWAA2026061597464), May 11, 2026: FLOOR SUPPORT. CRACKED. CRACKED FLOOR SUPPORT, BS 380 - 400, LBL 16, WL 208. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 143A5400, SHEET 109, REV A.
- [SDR SWAA2026061597465](https://openairdocs.org/sdr/SWAA2026061597465), May 11, 2026: FLOOR SUPPORT. CRACKED. CRACKED FLOOR SUPPORT, BS 380-400, RBL 40, WL 208. EMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 143A5400, SHEET 109, REV A.
- [SDR SWAA2026061597616](https://openairdocs.org/sdr/SWAA2026061597616), May 11, 2026: STRINGER CLIP. CRACKED. BS 727B, STRINGER CLIP 5R UPPER CORNER CRACKED. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1106 REV-.
- [SDR SWAA2026061597623](https://openairdocs.org/sdr/SWAA2026061597623), May 11, 2026: STRINGER CLIP. CRACKED. BS 727E, STRINGER CLIP 5R UPPER CORNER CRACKED. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1112 REV-.
- [SDR SWAA2026061597624](https://openairdocs.org/sdr/SWAA2026061597624), May 11, 2026: STRINGER CLIP. CRACKED. BS 727B STRINGER CLIP 6R UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1106 REV-.
- [SDR SWAA2026061597625](https://openairdocs.org/sdr/SWAA2026061597625), May 11, 2026: STRINGER CLIP. CRACKED. BS 727B, STRINGER CLIP 7L UPPER CORNER CRACKED. HFEC INSPECTED STRINGER CLIP IAW NDTM PART 6; 51-00-00 PROCEDURE 23 AND FOUND NO CRACKS PRESENT. REMOVED AND REP
- [SDR SWAA2026061597613](https://openairdocs.org/sdr/SWAA2026061597613), May 11, 2026: STRINGER CLIP. CRACKED. BS 685, STRINGER CLIP 2L UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 144A1106 REV A.
- [SDR SWAA2026061597615](https://openairdocs.org/sdr/SWAA2026061597615), May 11, 2026: STRINGER CLIP. CRACKED. BS 727A, STRINGER CLIP 7L UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1101 REV-.
- [SDR SWAA2026061597621](https://openairdocs.org/sdr/SWAA2026061597621), May 11, 2026: STRINGER CLIP. CRACKED. BS 727A, STRINGER CLIP 5L UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1101 REV-.
- [SDR SWAA2026061597622](https://openairdocs.org/sdr/SWAA2026061597622), May 11, 2026: STRINGER CLIP. CRACKED. BS 727A STRINGER CLIP 5R UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1101; REV-.
- [SDR SWAA2026061597461](https://openairdocs.org/sdr/SWAA2026061597461), May 11, 2026: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL AT BS 344-360 BL 0 WL 208<[01] OK TO INSTALL GIVEN FOR STEP 2 ITEM 2;[02] REMOVED AND REPLACED NEW INTERCOSTAL BS344-BS360 BL 0 WL208 I.A.W 
- [SDR SWAA2026061597463](https://openairdocs.org/sdr/SWAA2026061597463), May 11, 2026: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL AT BS 312-328 RBL 31 WL 208<[01] REMOVED AND REPLACED INTERCOSTAL AT BS 312-328 RBL 31 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 141A5400 SHEET 3
- [SDR SWAA2026061597460](https://openairdocs.org/sdr/SWAA2026061597460), May 11, 2026: TEE FITTING. CORRODED. CORROSION AT BS 986, RBL 43, WL 208. TASK CARD C/W. REMOVED AND REPLACED PREVIOUS REPAIR TEE FITTING SECTION, RBL14 - RBL50, WL 208 IAW SRM 51-40-02-0G-0 AS SHO
- [SDR SWAA2026061597618](https://openairdocs.org/sdr/SWAA2026061597618), May 11, 2026: STRINGER CLIP. CRACKED. STA 727E STR CLIP 7L UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1112; REV-
- [SDR SWAA2026061597626](https://openairdocs.org/sdr/SWAA2026061597626), May 11, 2026: STRINGER CLIP. NO DISCREPANCY. STA 727B STR CLIP 8L UPPER CORNER CRACKED. HFEC INSPECTED STRINGER CLIP AT 727B; S-8L IAW 737 NDTM PART 6; 51-00-00 PROCEDURE 23 AND FOUND NO CRACKS PRESENT.
- [SDR SWAA2026061597627](https://openairdocs.org/sdr/SWAA2026061597627), May 11, 2026: STRINGER CLIP. NO DISCREPANCY. STA 767 STR CLIP 10L UPPER CORNER CRACKED. HFEC INSPECTED STRINGER CLIP AT 767; S-10L IAW 737 NDTM PART 6; 51-00-00 PROCEDURE 23 AND FOUND NO CRACKS PRESENT.
- [SDR SWAA2026061597629](https://openairdocs.org/sdr/SWAA2026061597629), May 11, 2026: STRINGER CLIP. CRACKED. STA 727E STR CLIP 6L UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1112; REV- DATED:09/20/01;[02] VERIFIED ACTION 1
- [SDR SWAA2026061597630](https://openairdocs.org/sdr/SWAA2026061597630), May 11, 2026: FRAME. CRACKED. CRACKED FRAME AT BS 312 LBL 45 WL 284 BETWEEN STR 6L AND STR 5L. COMPLETED PER EA M-22-153-01244 (737-NG - SWA - BS 312 FRAME UPPER CHORD CRACK DAMAGE AT LBL 33
- [SDR SWAA2026061597459](https://openairdocs.org/sdr/SWAA2026061597459), May 11, 2026: FLOOR PANEL. CORRODED. CORROSION AT BS 986 RBL 36 WL 208. PREVIOUS REPAIR AND NO LIMITS ALLOWED PART TO BE REMOVED AND REPLACED ON CCN TTG8Q01C4FD9.
- [SDR SWAA2026061597471](https://openairdocs.org/sdr/SWAA2026061597471), May 11, 2026: SEAT TRACK. CORRODED. CORROSION ON PAX CABIN SEAT TRACK RBL 45 WL 208 STA 480+7 WELL; STA 480+7 TOP; STA 500+6 TOP; STA 500A TOP. SEAT TRACK WILL BE REPLACED ON TASK CARD TTG8Q01C4H2
- [SDR SWAA2026061597474](https://openairdocs.org/sdr/SWAA2026061597474), May 11, 2026: SEAT TRACK. CORRODED. CORROSION ON PAX CABIN SEAT TRACK RBL 25 WL 208 STA 480+7 WELL; STA 500+6 TOP; STA 500A+17 TOP; STA 500A+18 WELL. SEAT TRACK WILL BE REPLACED ON TASK CARD TTG8Q
- [SDR SWAA2026061597477](https://openairdocs.org/sdr/SWAA2026061597477), May 11, 2026: SEAT TRACK. CORRODED. CORROSION ON PAX CABIN SEAT TRACK LBL 25 WL 208 STA 500A+10 WELL; STA 500D+10 TOP; STA 500D+10 WELL. UPON FURTHER INVESTIGATION FOUND DAMAGE TO BE AT A PREVIOUS
- [SDR SWAA2026061597470](https://openairdocs.org/sdr/SWAA2026061597470), May 11, 2026: SEAT TRACK. CORRODED. CORROSION ON PAX CABIN SEAT TRACK LBL 45 WL 208 STA 480+17 TOP; STA 500+8 WELL; STA 500A+15 WELL; STA 500B+18 WELL; STA 500B+17 TOP. SEAT TRACK WILL BE REPLACED
- [SDR SWAA2026061597319](https://openairdocs.org/sdr/SWAA2026061597319), May 10, 2026: STRINGER CLIP. CRACKED. BS 727C STRINGER CLIP 6L UPPER SURFACE CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1103; REV- .
- [SDR SWAA2026061597320](https://openairdocs.org/sdr/SWAA2026061597320), May 10, 2026: STRINGER CLIP. CRACKED. BS 727C STRINGER CLIP 7L UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1103; REV-.
- [SDR SWAA2026061597321](https://openairdocs.org/sdr/SWAA2026061597321), May 10, 2026: STRINGER CLIP. CRACKED. BS 727C STRINGER CLIP 5R CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1103; REV- .
- [SDR SWAA2026061597322](https://openairdocs.org/sdr/SWAA2026061597322), May 10, 2026: STRINGER CLIP. CRACKED. BS 727C STRINGER CLIP 6R UPPER SURFACE CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1103; REV-.
- [SDR SWAA2026061597318](https://openairdocs.org/sdr/SWAA2026061597318), May 10, 2026: STRINGER CLIP. CRACKED. STA 727C STR CLIP 5L UPPER CORNER CRACKED. MARKED.<[01] REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1103; REV- DATED:09/15/01;[02] VERI
- [SDR SWAA2026061597014](https://openairdocs.org/sdr/SWAA2026061597014), May 9, 2026: FLOOR PANEL. DAMAGED. AFT FLOOR PANEL 242WF HAS MISSING PLIES ON LOWER SURFACE. DUE TO THE EXTENT OF DAMAGE, REPLACED THE AFT FLOOR PANEL 242WF IAW SRM 51-10-02-0G-0, PARA 9, AND AIP
- [SDR SWAA2026061597013](https://openairdocs.org/sdr/SWAA2026061597013), May 9, 2026: FLOOR PANEL. DELAMINATED. AFT FLOOR PANEL 241AEF UPPER SURFACE DELAMINATED. AFT FLOOR PANEL 241AEF WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026061596718](https://openairdocs.org/sdr/SWAA2026061596718), May 8, 2026: STUB FRAME. CRACKED. CRACK NOTED ON R1 DOOR CUT OUT STUB FRAME, 0.1 INCH ABOVE SEAL DEPRESSOR, 0.4 INCH FROM FWD EDGE, L: 2.3 INCH. REMOVED DAMAGE FSD STUB FRAME. LOCATED, DRILLED, 
- [SDR SWAA2026061596492](https://openairdocs.org/sdr/SWAA2026061596492), May 8, 2026: RIB. CRACKED. RT HORZ STAB L/E 341B 3RD RIB FROM I/B CRACKED AT LE STA 95.9. CRACKED RIB FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. REMOVED AND REPLACED
- [SDR SWAA2026061596495](https://openairdocs.org/sdr/SWAA2026061596495), May 8, 2026: STIFFENER. CRACKED. RIGHT HORIZONTAL STAB RIB 4 STIFFENER NR 3 IS CRACKED. REPAIRED LOWER SIDE OF STIFFENER #3 AT RIB NR 4 RT HORIZONTAL STABILIZER IAW SRM 55-10-09-2R-5.
- [SDR SWAA2026061596494](https://openairdocs.org/sdr/SWAA2026061596494), May 8, 2026: RUB STRIP. CRACKED. NR 3 AFT FLAP FAIRING 542BB O/B RUB STRIP CRACKED. REMOVED AND INSTALLED NEW OTB RUB STRIP ON NR 3 AFT FLAP FAIRING 542BB IAW AMM 20-50-11-910-801 .

All 252: https://openairdocs.org/aircraft/N925WN/reports.md

## STCs that may be installed (OpenAirDocs) (32)

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 CFM56-7B24 series)

- [STC SE04840NY](https://openairdocs.org/stc/SE04840NY): Installation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engine. Kilroy Aviation LLC
- [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

## Related

- Other Boeing 737-7H4 aircraft: https://openairdocs.org/model/boeing-737-7h4/aircraft.md
- The CFM International CFM56-7B24 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md

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