# N265WN: 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: 32522
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 2, 2007
- Certificate issued: March 12, 2007
- Expires: December 31, 2029
- Mode S code: A29391
- 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=265WN
- Page: https://openairdocs.org/aircraft/N265WN

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 N265WN.

## FAA accident and incident reports

None matched to N265WN.

## Service difficulty reports (258, 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 SWAA2026081717035](https://openairdocs.org/sdr/SWAA2026081717035), Aug 12, 2026: NUT PLATE. CRACKED. AFT ENTRY DOOR FWD LOWER NUT PLATE CRACKED ON SLIDE ISOLATOR BRACKET. R & R AFT ENTRY DOOR FWD LOWER ISOLATOR IAW SRM 51-40-02.
- [SDR SWAA2026081787218](https://openairdocs.org/sdr/SWAA2026081787218), Aug 12, 2026: RIB. CRACKED. LEFT AFT TRAILING EDGE FLAP DEFLECTION RIB, UPPER ATTACH ANGLE CRACKED. NR 8 SPOILER ACTUATOR SHUTTERING & NR 6 SPOILER ACTUATOR BYPASSING. WORKING SRM 57-51-02
- [SDR SWAA2026081705976](https://openairdocs.org/sdr/SWAA2026081705976), Aug 12, 2026: LENS. CONTAMINATED. PASSENGER CABIN SEAT ROW 1DEF PHOTOLUMINESCENT STRIP HAS MOISTURE UNDER LENS. R & R CABIN PHOTOLUMINESCENT STRIP IAW AMM 33-51-15.
- [SDR SWAA2026051297824](https://openairdocs.org/sdr/SWAA2026051297824), May 11, 2026: WINDOW. FAILED. L1 WINDSHIELD SHATTERED IN FLIGHT FOLLOWED QRH NO PRESSURIZATION ISSUES LANDED HEAVY WEIGHT. REMOVED AND REPLACED L1 WINDOW IAW AMM 56-11-11. OPS CHECK GOOD. CO
- [SDR SWAA2025121551847](https://openairdocs.org/sdr/SWAA2025121551847), Dec 12, 2025: STOP PIN. BROKEN. FWD SERVICE DOOR ESCAPE SLIDE GIRT BAR BROKEN; PLASTIC STOP RING BROKE OFF. INSTALLED NEW STOP PINS PER AMM 25-66-01
- [SDR SWAA2025090811271](https://openairdocs.org/sdr/SWAA2025090811271), Sep 4, 2025: PLATE. BULGED. DOUBLER FOR LAV SERVICE PAN ASSY HAS BULGING AROUND LOWER ROW OF FASTNERS DUE TO CORROSION FROM BS 847 - 867 JUST ABOVE S25L. THERE IS ALSO HEAVY INTERGRANULAR 
- [SDR SWAA2025052875179](https://openairdocs.org/sdr/SWAA2025052875179), May 26, 2025: LAMP. INOPERATIVE. L2 OUTSIDE EMERGENCY LIGHT INOP<[01] RELAMPED PER AMM 33-51-04 OPS CHECK GOOD
- [SDR SWAA2025030601742](https://openairdocs.org/sdr/SWAA2025030601742), Mar 4, 2025: SEAT BACK. OUT OF ADJUST. PASSENGER SEAT 11D RECLINES INTO AN EXIT ROW<[01] LOCKED OUT RECLINE HYDROLOK PER CMM 25-22-46.;[02] INSPECTED PER CMM 25-22-46
- [SDR SWAA2025030601756](https://openairdocs.org/sdr/SWAA2025030601756), Mar 4, 2025: MOUNT. CRACKED. AFT ENTRY DOOR FWD SLIDE MOUNT; UPPER ISOLATOR CRACKED<[01] R&R AFT ENTRY DOOR FWD SLIDE MOUNT; UPPER ISOLATOR IAW SRM 51-40-02.;[02] INSPECTED PER [SRM 51-40-0
- [SDR SWAA2024101645691](https://openairdocs.org/sdr/SWAA2024101645691), Oct 6, 2024: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS COMMON TO BATTERY PACK M1670 INOP<[01] REPLACED POWER SUPPLY - BATTERY PACK M1670 PER AMM 33-51-06-960-805. GOOD TEST.;[02] CERTIFIED CARD
- [SDR SWAA2024101644577](https://openairdocs.org/sdr/SWAA2024101644577), Oct 3, 2024: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS COMMON TO BATTERY PACK M1674 INOP<[01] REPLACED BATTERY PACK M1674 AND PERFORMED A GOOD FUNCTIONAL TEST PER AMM 33-51-06-960-805 & WDM 33-
- [SDR SWAA2024101644578](https://openairdocs.org/sdr/SWAA2024101644578), Oct 3, 2024: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS COMMON TO BATTERY PACK M1668 INOP<[01] REPLACED BATTERY PACK M1668 PER AMM 33-51-06-960-805 & WDM 33-51-13<BR><BR>ASILE LIGHTS ON ROW 9-12
- [SDR SWAA2024101637510](https://openairdocs.org/sdr/SWAA2024101637510), Sep 13, 2024: SKIN. CORRODED. WI-FI ANTENNA SKIN DOUBLER HAS SEVERAL CORROSION SPOTS (FASTENERS AND SKIN) BS 727B+12 TO BS 747+6; STR 3L TO STR 3R CROWN AREA.<[01] 'REPAIRED PER EA 24-153-02
- [SDR SWAA2024101637509](https://openairdocs.org/sdr/SWAA2024101637509), Sep 13, 2024: PLATE. CORRODED. PLATE UNDER PSC ANTENNA HAS CORROSION AT BS 727E+15; LBL5 AND WL 306<[01] 'REFER TO FAULT TTG8Q00VV56H.';[02] VERIFIED ITEM 1
- [SDR SWAA2024101636998](https://openairdocs.org/sdr/SWAA2024101636998), Sep 12, 2024: FRAME. CRACKED. CRACKED FRAME BS 312 COMMON TO STR 6L LBL 33 WL 282.<[01] REPAIRED FRAME BS 312 COMMON TO STR 6L; LBL33; WL 282 PER EA M-22-153-01244 CUSTOMER SYSTEM ID: TTG8Q0
- [SDR SWAA2024101636533](https://openairdocs.org/sdr/SWAA2024101636533), Sep 11, 2024: SIDEWALL SUPPORT. CORRODED. CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156<[01] REMOVED AND REPLACE FLOOR TO 
- [SDR SWAA2024101636547](https://openairdocs.org/sdr/SWAA2024101636547), Sep 11, 2024: SPLICE STRAP. CORRODED. CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS767+6 RBL11.5 WL156<[01] CORROSION ON STRAP WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS AR
- [SDR SWAA2024101636548](https://openairdocs.org/sdr/SWAA2024101636548), Sep 11, 2024: SUPPORT PLATE. CORRODED. CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] EVALUATION AND REMOVED DA
- [SDR SWAA2024101635622](https://openairdocs.org/sdr/SWAA2024101635622), Sep 9, 2024: ATTACH ANGLE. CRACKED. CRACKED ATTACH ANGLE AT FWD WET AREA BS294 RBL53 WL208. MARKED<[01] CRACKED ATTACH ANGLE WILL BE REPLACED ON TTG8Q00VPT1S.;[02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2024101635292](https://openairdocs.org/sdr/SWAA2024101635292), Sep 8, 2024: WEB. CORRODED. WHILE WORKING R/H OVERWING EXIT DUE TO CORROSION EVAL; REMOVED SEALANT AROUND CORRODED AREAS; AND NOTICED A DRILLED START AT BS 616+20; WL221; RBL70.<[01] COMPL
- [SDR SWAA2024101634889](https://openairdocs.org/sdr/SWAA2024101634889), Sep 6, 2024: GIRT BAR. CORRODED. CORROSION ON FWD ENTRY DOOR FWD GIRT BAR FITTING BS 312 LBL 50 WL 208.<[01] REMOVED & REPLACED FWD ENTRY DOOR FWD GIRT BAR FITTING BS 312 LBL 50 WL 208 IAW SRM 
- [SDR SWAA2024101634890](https://openairdocs.org/sdr/SWAA2024101634890), Sep 6, 2024: ANGLE. CRACKED. CRACKED ANGLE BS 294 O/B OF MOPSILL RBL 53 WL 208.<[01] REMOVE AND REPLACED NEW REPAIR ANGLE BS 294 O/B OF MOPSILL RBL 53 WL 208 IAW SRM 53-10-15-2R-7 AND SRM 5
- [SDR SWAA2024101634881](https://openairdocs.org/sdr/SWAA2024101634881), Sep 6, 2024: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL BS 294-297 RBL 1 WL 208.<[01] UPDATED STEP 1.;[02] UPDATED STEP 3.;[03] UPDATED STEP 3.;[04] REMOVED & REPLACED INTERCOSTAL BS 294-297 RBL 1
- [SDR SWAA2024101634882](https://openairdocs.org/sdr/SWAA2024101634882), Sep 6, 2024: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL BS 312-328 LBL 45 WL 208.<[01] REMOVED AND REPLACED INTERCOSTAL BS312-BS328 LBL45 WL208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A5400 REV 
- [SDR SWAA2024101634883](https://openairdocs.org/sdr/SWAA2024101634883), Sep 6, 2024: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL BS 328-344 LBL 45 WL 208. EDIT: INTERCOSTAL IS AT BS 312-328 LBL 45 WL 208<[01] REMOVED AND REPLACED INTERCOSTAL AT BS 312-328 LBL 45 WL 208
- [SDR SWAA2024101634884](https://openairdocs.org/sdr/SWAA2024101634884), Sep 6, 2024: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL BS 344-360 RBL 11 WL 208.<[01] REMOVED AND REPLACED INTERCOSTAL AT BS 344-360 RBL 11 WL 208 IAW SRM 51-40-02-0G-0 REF DWG 141A5400 NO REV; D
- [SDR SWAA2024101634885](https://openairdocs.org/sdr/SWAA2024101634885), Sep 6, 2024: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL BS 344-360 LBL 12 WL 208.<[01] UPDATED STEP 3.;[02] REMOVED CRACKED INTERCOSTAL BS 344-360 LBL 12 WL 208 IAW SRM 51-40-02-0G-0 AND REPLACED 
- [SDR SWAA2024101634707](https://openairdocs.org/sdr/SWAA2024101634707), Sep 5, 2024: STUB FRAME. CRACKED. CRACK FOUND ON FSD STUB FRAME AT BS291.5 + 8; 0.8' ABOVE SEAL DEPRESSOR 1.2' IN LENGTH (MARKED)<[01] REMOVED FSD STUB FRAME IAW SRM 51-40-02-0G-0 AND INSTALLED 
- [SDR SWAA2024101634710](https://openairdocs.org/sdr/SWAA2024101634710), Sep 5, 2024: SHEAR WEB. CORRODED. CORROSION ON AFT L/H SHEAR WEB BS 1016 LBL 11-LBL 22 WL 208.<[01] UPDATED STEP 1;[02] REMOVED AND REPLACED AFT L/H SHEAR WEB AT BS 1016-1026 LBL 0 - LBL 38 WL 2
- [SDR SWAA2024101634711](https://openairdocs.org/sdr/SWAA2024101634711), Sep 5, 2024: STRAP. CORRODED. CORROSION ON REINFORCEMENT STRAP BS 1016-1029 LBL 2 WL 208.<[01] REMOVED AND REPLACED REINFORCEMENT STRAP AT BS 1016-1029 LBL 2 WL 208 IAW SRM 51-40-02-0G-0 AND
- [SDR SWAA2024101634716](https://openairdocs.org/sdr/SWAA2024101634716), Sep 5, 2024: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL BS 927-947 LBL 3 WL 208. CRACKED ATTACH UPPER ANGEL ON INTERCOSTAL AT BS 927-947 LBL 3 WL 208.<[01] REMOVED AND REPLACED CRACKED INTERCOSTAL
- [SDR SWAA2024101634309](https://openairdocs.org/sdr/SWAA2024101634309), Sep 5, 2024: DOOR. CORRODED. LAV SERVICE DOOR INNER SURFACE HAS CORROSION ON AFT EDGE<[01] REMOVED AND REPLACED DAMAGED LAV SERVICE PANEL PER AMM 52-49-07-000-801; 52-49-07-400-801; AMM 20-
- [SDR SWAA2024101634713](https://openairdocs.org/sdr/SWAA2024101634713), Sep 5, 2024: FLOORBEAM. CORRODED. CORROSION ON FLOOR BEAM BS 986 RBL 45 WL 208.<[01] CORROSION ON FLOOR BEAM BS 986 RBL 45 WL 208 FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AND REPAIRED IAW SRM 
- [SDR SWAA2024101634712](https://openairdocs.org/sdr/SWAA2024101634712), Sep 5, 2024: REINFORCEMENT. CORRODED. CORROSION ON REINFORCEMENT STRAP BS 1016-1026 RBL 3 WL 208.<[01] REMOVED AND REPLACED REINFORCEMENT STRAP BS 1016-1026 RBL 3 WL 208 IAW SRM 51-40-02-0G-0 AND DW
- [SDR SWAA2024101534497](https://openairdocs.org/sdr/SWAA2024101534497), Sep 5, 2024: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 241ABF O/B EDGE IS DELAMINATED (AS MARKED)<[01] FLOOR PANEL 241ABF O/B EDGE DAMAGE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-10-A00948 (REPAIR 10
- [SDR SWAA2024101633487](https://openairdocs.org/sdr/SWAA2024101633487), Sep 3, 2024: WEB. CORRODED. CORROSION ON R/H OVERWING EXIT CUT-OUT SILL AT STA 616+8; 616+9M 616+14; 616+15; 616+20; WL 221; RBL 70.<[01] COMPLETED STEPS 2 AND 3;[02] REMOVED CORROSION FRO
- [SDR SWAA2024101633603](https://openairdocs.org/sdr/SWAA2024101633603), Sep 3, 2024: BULKHEAD. CRACKED. CRACKED LOWER R/H COMPOSITE BULKHEAD AT BS663 RBL36 WL163.<[01] CRACKED LOWER R/H BULKHEAD BS663 WAS REPAIRED IAW SRM 51-70-04-2R-10;[02] VERIFIED CORRECTIVE AC
- [SDR SWAA2024101633481](https://openairdocs.org/sdr/SWAA2024101633481), Sep 3, 2024: VAPOR BARRIER. DEBONDED. STA 663 VAPOR BARRIER PREVIOUS REPAIR IS DISBONDED AT WL 160; LBL 40.<[01] VAPOR BARRIER PREVIOUS REPAIR REMOVED & REPAIRED IAW SRM 51-70-04-2R-10;[02] VERIFIED
- [SDR SWAA2024101633473](https://openairdocs.org/sdr/SWAA2024101633473), Sep 2, 2024: ATTACH ANGLE. CRACKED. (RIGHT WING) UPPER WING PANEL SUPPORT U CHANEL AT 9-INCH O/B OF FUSELAGE; ATTACH ANGLE CRACKED AT REAR SPAR ATTACH POINT<[01] REMOVED AND REPLACED ANGLE P/N 115
- [SDR SWAA2024101632859](https://openairdocs.org/sdr/SWAA2024101632859), Aug 31, 2024: ATTACH ANGLE. CRACKED. LT WING T/E DEFLECTION CONTROL RIB I/B ATTACHED ANGLE CRACK<[01] VERIFIED;[02] VERIFIED;[03] REMOVED AND REPLACED LEFT WING T/E DEFLECTION CONTROL RIB I/B ATTAC
- [SDR SWAA2024042678968](https://openairdocs.org/sdr/SWAA2024042678968), Apr 25, 2024: THRESHOLD. CRACKED. FUSELAGE FORWARD CARGO CENTER THRESHOLD IS CRACKED AT AFT DOOR STOP.<[01] R/R FWD CARGO DOOR CENTER THRESHOLD PER AMM 53-11-02
- [SDR SWAA2024042578970](https://openairdocs.org/sdr/SWAA2024042578970), Apr 25, 2024: BATTERY PACK. NO TEST. EMX LIGHT BATT PACK M01672 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX LIGHT BATT PACK M01672 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTER
- [SDR SWAA2023021603460](https://openairdocs.org/sdr/SWAA2023021603460), Feb 16, 2023: BATTERY PACK. FAILED. AFT CABIN LH SIDE EMERGENCY BATTERY FAILED CAPACITY TEST.<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACK M1673 IAW AMM 33-51-06.
- [SDR SWAA2023021603454](https://openairdocs.org/sdr/SWAA2023021603454), Feb 16, 2023: BATTERY PACK. FAILED. MID CABIN RH SIDE EMERGENCY BATTERY FAILED CAPACITY TEST.<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACK M1669 IAW AMM 33-51-06.
- [SDR SWAA2023021603461](https://openairdocs.org/sdr/SWAA2023021603461), Feb 16, 2023: PANEL. CRACKED. AFT SERVICE R2 DOOR LOWER PANEL 844DZ AFT BRACKET CRACKED<[01] REMOVED AND REPLACED AFT SERVICE DOOR LOWER PANEL 844DZ PAN REF AMM 52-41-31.
- [SDR SWAA2022101056386](https://openairdocs.org/sdr/SWAA2022101056386), Oct 5, 2022: NONE. INOPERATIVE. INOP BATTERY PACK LOCATED LT SIDE AT FWD GALLEY AREA 2022-467055 / [01] REPLACED BATTERY PACK P/N AD-B717-01-100SWA S/N 41847 OFF; P/N AD-B717-01-100SWA S/N BN 
- [SDR SWAA2022101046562](https://openairdocs.org/sdr/SWAA2022101046562), Sep 22, 2022: ANGLE. BROKEN. BROKEN BODY FAIRING SUPPORT ANGLE LOCATED AT BS 500D LT SIDE AT LOWER FUSELAGE 2022-467011 / [01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED AT BS 500D LT SID
- [SDR SWAA2022101046563](https://openairdocs.org/sdr/SWAA2022101046563), Sep 22, 2022: STUD. BROKEN. BROKEN STUD RECEPTACLE ON BRACKET AE0502A E5-2 2022-467012 / [01] REPLACED STUD RECEPTACLE LOCATED ON BRACKET AE0502A E5-2 I.A.W B737-700 SRM 51-40-02-0G-0.;[02
- [SDR SWAA2022101016065](https://openairdocs.org/sdr/SWAA2022101016065), Sep 22, 2022: SUPPORT ANGLE. BROKEN. BROKEN BODY FAIRING SUPPORT ANGLE LOCATED AT BS 500D LT SIDE AT LOWER FUSELAGE 2022-467011 /
- [SDR SWAA2022100646564](https://openairdocs.org/sdr/SWAA2022100646564), Sep 22, 2022: STRAP. CRACKED. CRACK STRAP AT FLOOR AREA BS 500 BTW STR 25R TO STR 25L AT FWD CARGO COMPARTMENT 2022-467013 / [01] REPLACED STRAP AT FLOOR AREA BS 500 BTW STR 25R TO STR 25L A

All 258: https://openairdocs.org/aircraft/N265WN/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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