# N295WN: 2007 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: 32541
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 27, 2007
- Certificate issued: November 19, 2007
- Expires: November 30, 2028
- Mode S code: A30A0E
- 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=295WN
- Page: https://openairdocs.org/aircraft/N295WN

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 CFM56-7B24 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 N295WN.

## FAA accident and incident reports

None matched to N295WN.

## 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 SWAA2026072005218](https://openairdocs.org/sdr/SWAA2026072005218), Jul 15, 2026: SEAT BACK. OUT OF ADJUST. EXIT ROW SEAT 14B RECLINES REMOVED SEAT RECLINE FEATURE AT 14B IAW CMM 25-21-42 IAW CMM 25-21-42. 02.
- [SDR SWAA2026071694829](https://openairdocs.org/sdr/SWAA2026071694829), Jul 12, 2026: HOLDER. FAULTED. GIRT BAR STUCK. REMOVED GIRT BAR FROM SLIDE BOX GIRT BAR HOLDER IAW AMM 25-66-01.
- [SDR SWAA2026032582825](https://openairdocs.org/sdr/SWAA2026032582825), Mar 24, 2026: BALLAST. OVERTEMP. PLASTIC BURNING SMELL IN AFT GALLEY. PERFORMED CONDITIONAL INSPECTION 05-51-56. FOUND AFT ENTRY LIGHT BALLAST OVERHEATED. REMOVED AND REPLACED BALLAST AND LAMPS
- [SDR SWAA2026032583093](https://openairdocs.org/sdr/SWAA2026032583093), Mar 24, 2026: BALLAST. OVERTEMP. PLASTIC BURNING ODOR IN AFT GALLEY. PERFORMED CONDITIONAL INSPECTION 05-51-56. FOUND AFT ENTRY LIGHT BALLAST OVERHEATED. REMOVED AND REPLACED BALLAST AND LAMPS 
- [SDR SWAA2025120140670](https://openairdocs.org/sdr/SWAA2025120140670), Nov 28, 2025: PRESSURE SWITCH. FAULTED. APU LOW OIL PRESSURE LIGHT ILLUMINATED IN CRUISE, RESULTING IN SINGLE ELECTRICAL SOURCE. OVERWEIGHT LANDING PERFORMED IAW AOM 12-1-7. SMLDW EXCEEDED BY 10.3. SE
- [SDR SWAA2025102226015](https://openairdocs.org/sdr/SWAA2025102226015), Oct 19, 2025: HANDLE. LOOSE. FO SIDE OVER WING EMERGENCY EXIT DOOR HANDLE LOOSE. REINSTALLED STRAP COVER ON FO SIDE EMERGENCY EXIT DOOR IAW AMM 52-22-00.
- [SDR SWAA2025063076680](https://openairdocs.org/sdr/SWAA2025063076680), May 30, 2025: SKIN. CORRODED. AAI: AFT CARGO COMPARTMENT; INTERNAL SKIN SURFACE HAS CORROSION BWT STA 747 & STA 767; STR 27L & STR 27R. PERFORMED PERMANENT REPAIR ON AFT CARGO COMPARTMENT IN
- [SDR SWAA2025063076455](https://openairdocs.org/sdr/SWAA2025063076455), May 30, 2025: FLOOR SUPPORT. CRACKED. AAI: MAIN CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75. REPLACED FLOOR STRUCTURE SUPPORT LOCATED PASSENGER CABIN FLOOR STRUCTURE STA54
- [SDR SWAA2025063076575](https://openairdocs.org/sdr/SWAA2025063076575), May 30, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLE ACCESS PANEL 661BB TRAILING EDGE AT RT WING 2025-335666<[01] TOOL USED CALIPER P/N 500-197-30 S/N B20189334 DUE DATE 26 JAN 26;[02] TOOL USED ON 
- [SDR SWAA2025063075332](https://openairdocs.org/sdr/SWAA2025063075332), May 27, 2025: SKIN PANEL. CRACKED. CRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16.0 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LE
- [SDR SWAA2025063075152](https://openairdocs.org/sdr/SWAA2025063075152), May 25, 2025: FLOOR SUPPORT. CRACKED. CRACK INTERCOSTAL LOCATED ON FLOOR STRUCTURE BTW BS 312 TO BS 328 AND RBL 29 FWD GALLEY AREA. REPLACED INTERCOSTAL LOCATED ON FLOOR STRUCTURE BTW BS 312 TO BS 3
- [SDR SWAA2025063074471](https://openairdocs.org/sdr/SWAA2025063074471), May 23, 2025: PLATE. CRACKED. CRACK OUTBOARD TRAILING EDGE CORRUGATED PLATE LOCATED AT ORSS 297 AT LT WING 2025-335620<[01] REPLACED CORRUGATED PLATE LOCATED AT ORSS 297 AT LT WING IAW B737-
- [SDR SWAA2025063076453](https://openairdocs.org/sdr/SWAA2025063076453), May 23, 2025: SUPPORT BRACKET. CRACKED. CRACK OUTBOARD FAN COWL HOLD OPEN ROD SUPPORT BRACKET AFT POSITION ON ENGINE 1. REPLACED SUPPORT BRACKET LOC. FAN COWL HOLD OPEN ROD AFT POSITION ON ENGINE 1 IA
- [SDR SWAA2025062774462](https://openairdocs.org/sdr/SWAA2025062774462), May 23, 2025: ACCESS PANEL. CRACKED. CRACK AROUND HOLES OF ACCESS PANEL 661BB TRAILING EDGE AT RT WING 2025-335601<
- [SDR SWAA2025063074220](https://openairdocs.org/sdr/SWAA2025063074220), May 22, 2025: SHIELD. CRACKED. CRACK SHIELD WEB LOCATED BETWEEN STA492.4 TO STA500A AND RBL21 AT FWD CARGO COMPARTMENT 2025-335533 <[01]. REPLACED SHIELD WEB LOCATED BETWEEN STA492.4 TO STA50
- [SDR SWAA2025063074218](https://openairdocs.org/sdr/SWAA2025063074218), May 22, 2025: WEB. CORRODED. CORROSION WEB DOOR CUT OUT LOCATED STA827 AND RBL64 WL200 AT AFT CARGO COMPARTMENT 2025-335528 <[01]. REPLACED WEB DOOR CUT OUT LOCATED STA 767 AND 847 RBL 64 W
- [SDR SWAA2025063074223](https://openairdocs.org/sdr/SWAA2025063074223), May 22, 2025: FAIRING. CRACKED. CRACK ON INTERNAL SKIN OF ACCESS PANEL 644BB FLAP SUPPORT FAIRING 8 AT RT WING 2025-335582<[01] REPAIRED ACCESS PANEL 644BB FLAP SUPPORT FAIRING 8 AT RT WING IA
- [SDR SWAA2025063073730](https://openairdocs.org/sdr/SWAA2025063073730), May 21, 2025: ANGLE. CRACKED. CRACK REAR SPAR ANGLE LOCATED ON IRSS 148 AT MAIN LANDING GEAR AREA AT LT WING 2025-335508 <[01]. REPLACED REAR SPAR ANGLE LOCATED ON IRSS 148 AT MAIN LANDING G
- [SDR SWAA2025063073486](https://openairdocs.org/sdr/SWAA2025063073486), May 21, 2025: TRACK. CRACKED. CRACK TRACK RBBL 13.84 LOCATED STA747 AFT CARGO COMPARTMENT 2025-335494 <[01] TOOL USED ON STEP 4: EDDY CURRENT EQUIPMENT P/N:NORTEC 600D; S/N:210135503; DUE DA
- [SDR SWAA2025063073488](https://openairdocs.org/sdr/SWAA2025063073488), May 21, 2025: ANGLE. CRACKED. CRACK ANGLE LOCATED BETWEEN STA907 TO STA927 AND STR25R TO STR27R AFT POSITION AT AFT CARGO COMPARTMENT. REPLACED ANGLE LOCATED BETWEEN STA 907 TO STA 927 AND S
- [SDR SWAA2025063073484](https://openairdocs.org/sdr/SWAA2025063073484), May 21, 2025: TIE CLIP. CRACKED. CRACK TIE CLIP LOCATED BS 277 AND S-10R PASSENGER CABIN 2025-335493<[01] REPLACED TIE CLIP LOCATED BS 277 AND S-10R PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G
- [SDR SWAA2025063073489](https://openairdocs.org/sdr/SWAA2025063073489), May 21, 2025: ANGLE. CRACKED. CRACK ANGLE LOCATED BETWEEN STA907 TO STA927 AND STR25R TO STR27R FWD POSITION AT AFT CARGO COMPARTMENT. REPLACED ANGLE LOCATED BETWEEN STA 907 TO STA 927 AND S
- [SDR SWAA2025063073727](https://openairdocs.org/sdr/SWAA2025063073727), May 21, 2025: RAIL. CORRODED. CORROSION ON RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS449 AT RT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS 449 AT 
- [SDR SWAA2025063073729](https://openairdocs.org/sdr/SWAA2025063073729), May 21, 2025: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED BS 867 BETWEEN S-2R TO S-3R PASSENGER CABIN. REPLACED SUPPORT ANGLE LOCATED BS 867 BETWEEN S-2R TO S-3R PASSENGER CABIN IAW B737-700
- [SDR SWAA2025063073487](https://openairdocs.org/sdr/SWAA2025063073487), May 21, 2025: ACCESS PANEL. CRACKED. CRACK SEAL - PLATE ACCESS PANEL 343AB AT RT HORIZONTAL STAB. REPLACED SEAL - PLATE ACCESS PANEL 343AB AT RT HORIZONTAL STAB IAW B737-700 SRM 51-40-02-0G-0 AND S
- [SDR SWAA2025063073239](https://openairdocs.org/sdr/SWAA2025063073239), May 20, 2025: INTERCOSTAL. CRACKED. CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS344 TO BS 360 LBL 12 FWD GALLEY AND LAV 2025-335415 <[01]. REPLACED NEW WEB INTERCOSTAL LOC. ON FLOOR STRUCTUR
- [SDR SWAA2025063072652](https://openairdocs.org/sdr/SWAA2025063072652), May 19, 2025: FLOORBEAM. CRACKED. CRACK FLOOR BEAM LOCATED BS 328 AND RBL 24 FWD GALLEY AND LAV 2025-335317 <[01]. STEP 21 TOOL USED: EDDY CURRENT FLAW DETECTOR. P/N: NORTEC 600D; S/N:190023010;
- [SDR SWAA2025063072654](https://openairdocs.org/sdr/SWAA2025063072654), May 19, 2025: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE ORSS 271 AT LT WING. REPLACED ANGLE TRAILING EDGE ORSS 271 AT LT WING IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 115A6200 SHEE
- [SDR SWAA2025063072653](https://openairdocs.org/sdr/SWAA2025063072653), May 19, 2025: SUPPORT BEAM. CRACKED. CRACK DEFLECTION CONTROL RIB SUPPORT BEAM ORSS 281 TRAILING EDGE AT LT WING. PERFORMED PERMANENT REPAIR LOC. ON DEFLECTION CONTROL RIB SUPPORT BEAM ORSS 281 TRA
- [SDR SWAA2025063072913](https://openairdocs.org/sdr/SWAA2025063072913), May 19, 2025: STUB FRAME. CRACKED. CRACK INDICATION ON STUB FRAME LOCATED BETWEEN BS 294.5 TO BS 296.5 BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 1.430 IN. APROX.AT PASSENGER CABIN. RE
- [SDR SWAA2025063072202](https://openairdocs.org/sdr/SWAA2025063072202), May 18, 2025: NUT. DETERIORATED. DETERIORATED NUT ASSIST HANDLE AFT SERVICE INTERIOR STRUCTURE FWD OF DOOR OPENING (2EA) 2025-335269 <[01]. REPLACED NUT ASSIST HANDLE AFT SERVICE INTERIOR STRUC
- [SDR SWAA2025063072201](https://openairdocs.org/sdr/SWAA2025063072201), May 18, 2025: NUT. DETERIORATED. DETERIORATED NUT ASSIST HANDLE AFT ENTRY INTERIOR STRUCTURE FWD OF DOOR OPENING (2EA). REPLACED NUT ASSIST HANDLE AFT ENTRY INTERIOR STRUCTURE FWD OF DOOR OPENI
- [SDR SWAA2025063072204](https://openairdocs.org/sdr/SWAA2025063072204), May 18, 2025: NUT. DETERIORATED. DETERIORATED NUT ASSIST HANDLE FWD ENTRY INTERIOR STRUCTURE AFT OF DOOR OPENING (2EA). REPLACED NUT ASSIST HANDLE FWD ENTRY INTERIOR STRUCTURE AFT OF DOOR OPENI
- [SDR SWAA2025063072205](https://openairdocs.org/sdr/SWAA2025063072205), May 18, 2025: NUT. DETERIORATED. DETERIORATED NUT FWD ENTRY DOOR LINER LOWER ASSIST HANDLE (2EA) . REPLACED NUT FWD ENTRY DOOR LINER LOWER ASSIST HANDLE (2EA) IAW B737-700 AMM-52-11-31-400-802 
- [SDR SWAA2025063072501](https://openairdocs.org/sdr/SWAA2025063072501), May 18, 2025: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE ON WING TO BODY FAIRING STRUCTURE BS 500D AT LEVEL STRINGER 19R LOWER FUSELAGE. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED ON WING TO BODY
- [SDR SWAA2025063072391](https://openairdocs.org/sdr/SWAA2025063072391), May 18, 2025: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE ON INBOARD AUXILIARY TRACK SLAT 8 AT RT WING. REPLACED SUPPORT ANGLE ON INBOARD AUXILIARY TRACK SLAT 8 AT RT WING IAW SRM 51-40-02-0G AND SR
- [SDR SWAA2025063072392](https://openairdocs.org/sdr/SWAA2025063072392), May 18, 2025: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE ON INBOARD AUXILIARY TRACK SLAT 1 AT LT WING. REPLACED SUPPORT ANGLE ON INBOARD AUXILIARY TRACK SLAT 1 AT LT WING IAW SRM 51-40-02-0G AND SR
- [SDR SWAA2025063072396](https://openairdocs.org/sdr/SWAA2025063072396), May 18, 2025: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE ON INBOARD AUXILIARY TRACK SLAT 2 AT LT WING. REPLACED SUPPORT ANGLE ON INBOARD AUXILIARY TRACK SLAT 2 AT LT WING IAW B737-700 SRM 51-40-02-
- [SDR SWAA2025063072500](https://openairdocs.org/sdr/SWAA2025063072500), May 18, 2025: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE ON WING TO BODY FAIRING STRUCTURE BS 500D AT LEVEL STRINGER 19L LOWER FUSELAGE. REPLACED NEW ANGLE ON WING TO BODY FAIRING STRUCTURE BS 500D
- [SDR SWAA2025063072192](https://openairdocs.org/sdr/SWAA2025063072192), May 17, 2025: PANEL. CORRODED. RUST ON LOWER STUD BULKHEAD PANEL 121LW AT FWD CARGO COMPARTMENT (6E/A) 2025-335249 <[01]. REPLACED LOWER STUD BULKHEAD PANEL 121LW AT FWD CARGO COMPARTMENT (6E
- [SDR SWAA2025063071696](https://openairdocs.org/sdr/SWAA2025063071696), May 16, 2025: SKIN. CORRODED. CUSTOMER REQUEST EVIDENCE OF CORROSION ON EXTERNAL SKIN VACUUM WASTE VENT CUTOUT LOCATED BTW S-21L TO S-22L STA 907 PLUS 10 INCH 2025-335136 <[01]. ON STEP 4; U
- [SDR SWAA2025051970234](https://openairdocs.org/sdr/SWAA2025051970234), May 13, 2025: BATTERY PACK. FAILED. L/H AFT EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2025051970232](https://openairdocs.org/sdr/SWAA2025051970232), May 13, 2025: BATTERY PACK. FAILED. EMERGENCY LIGHTING BATTERY PACK AT THE L/H OVERWING EXIT FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2025051970230](https://openairdocs.org/sdr/SWAA2025051970230), May 13, 2025: BATTERY PACK. FAILED. L/H FWD EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2025011686597](https://openairdocs.org/sdr/SWAA2025011686597), Jan 16, 2025: LIGHT. INOPERATIVE. L2 DOOR EMERGENCY LIGHT INOP.<[01] R & R L2 DOOR EMERGENCY LIGHT REF AMM 33-51-04. OPS CHK GOOD.
- [SDR SWAA2025011385227](https://openairdocs.org/sdr/SWAA2025011385227), Jan 12, 2025: GUARD. INOPERATIVE. GUARD ON EMERGENCY LIGHT SWITCH INOP<[01] REMOVED AND REPLACED GUARD IN REF TO SIP
- [SDR SWAA2024120974575](https://openairdocs.org/sdr/SWAA2024120974575), Dec 5, 2024: ENGINE. SMOKE. EXCESSIVE SMOKE FROM #1 ENGINE TAILPIPE WITH PUDDLING ON GROUND AT REAR OF ENGINE SMOKE ACCOMPANIED BY FLAMES. OIL QUANTITY AT SHUTDOWN 52%. BP AERO JONATHAN NI
- [SDR SWAA2024120674339](https://openairdocs.org/sdr/SWAA2024120674339), Dec 5, 2024: TAILPIPE. LEAKING. EXCESSIVE SMOKE FROM #1 ENGINE TAIL PIPE REPORTED BY RAMP WITH OIL PUDDLING ON GROUND AT REAR OF ENGINE.<[01] C/W ENGINE VENTS & DRAINS INSPECTION IAW AMM 71-71
- [SDR SWAA2024083031078](https://openairdocs.org/sdr/SWAA2024083031078), Aug 27, 2024: FLASHLIGHT. INOPERATIVE. 1 FWD CABIN EMERGENCY FLASHLIGHT INOP.<
- [SDR SWAA2024080823926](https://openairdocs.org/sdr/SWAA2024080823926), Aug 7, 2024: SEAT BACK. OUT OF ADJUST. SEATS 11DEF WILL NOT STAY UPRIGHT WHILE OCCUPIED<[01] 11F SEAT RECLINE ACTUATOR NOT LOCKED OUT FOR EMERGENCY EXIT; LOCKED RECLINE ACTUATOR TO UP POSITION AND TI

All 291: https://openairdocs.org/aircraft/N295WN/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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