# N260WN: 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 CFM56-7B24 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: 32518
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 19, 2006
- Certificate issued: January 8, 2007
- Expires: June 30, 2029
- Mode S code: A280FE
- 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=260WN
- Page: https://openairdocs.org/aircraft/N260WN

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 N260WN.

## FAA accident and incident reports

None matched to N260WN.

## Service difficulty reports (261, 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 SWAA2026081181799](https://openairdocs.org/sdr/SWAA2026081181799), Aug 10, 2026: MEC. LEAKING. LOSS OF SYSTEM B HYD SYS. R & R NR 2 ENG EDP IAW AMM 29-11-11, LEAK CHECKED GOOD, OPS CHECKED GOOD.
- [SDR SWAA2026081330201](https://openairdocs.org/sdr/SWAA2026081330201), Aug 9, 2026: LAMP. INOPERATIVE. AFT SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. RELAMPED PER AMM 33-51-04. OPS CHECK GOOD
- [SDR SWAA2026080510395](https://openairdocs.org/sdr/SWAA2026080510395), Aug 1, 2026: FIRE WARNING. NO TEST. NR 2 ENGINE OVERHEAT AND FIRE LIGHTS FAILED TO LIGHT DURING TEST IN NORMAL POSITION. LIGHTS UP WITH SELECTOR IN A & B POSITIONS. NR 2 ENGINE OVERHEAT LIGHT ON I
- [SDR SWAA2026072094632](https://openairdocs.org/sdr/SWAA2026072094632), Jul 14, 2026: LAMP. INOPERATIVE. EMERGENCY EXIT LIGHT BEHIND L1 DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT LAMP BEHIND L1 DOOR IAW AMM 33-51-04. OPS CHKD GOOD.
- [SDR SWAA2026062913646](https://openairdocs.org/sdr/SWAA2026062913646), Jun 18, 2026: FAIRING. CUT. TWO ELONGATED HOLES ON AFT STRAKE FAIRING AT WINGLET SCIMITAR LT. REPAIRED AFT STRAKE FAIRING AT WINGLET SCIMITAR LT IAW SRM 51-70-04-2R-9 REPAIR 9.
- [SDR SWAA2026062509303](https://openairdocs.org/sdr/SWAA2026062509303), Jun 5, 2026: WEB. DAMAGED. ELONGATED HOLE ON WEB LOCATED BTW BS 500 TO BS 500A AT LEVEL STRG 26L ON FWD CARGO COMPARTMENT. REPLACED WEB LOCATED BTW BS 500 TO BS 500A AT LEVEL STRG 26L ON 
- [SDR SWAA2026062908234](https://openairdocs.org/sdr/SWAA2026062908234), Jun 1, 2026: RIB. CRACKED. CRACK LEADING EDGE RIB LOC LE STA 95.96 AT LT HORIZONTAL STAB. REPLACED RIB AND FASTENERS LOC LE STA 95.96 AT LT HORIZONTAL STAB IAW SRM 51-40-02-0G-0, AND DWG 
- [SDR SWAA2026062907712](https://openairdocs.org/sdr/SWAA2026062907712), May 29, 2026: STRINGER. CRACKED. CRACKED STRINGER 23R, BS 540 IN THE FWD CARGO BAY. PERFORMED PERMANENT REPAIR ON STRINGER 23R LOCATED BS 500D TO BS 540 IAW SRM 53-00-03?2R-1, REPAIR 1.
- [SDR SWAA2026062907594](https://openairdocs.org/sdr/SWAA2026062907594), May 29, 2026: ACCESS PANEL. CRACKED. CRACKED BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB. REPLACED BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02.
- [SDR SWAA2026062907716](https://openairdocs.org/sdr/SWAA2026062907716), May 29, 2026: RIB. CRACKED. CRACK ON INSPAR RIB LOWER CHORD LOCATED ON STAB STA 120.30 AND 36 INCHES FROM FRONT SPAR AT RT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR LOCATED ON INSPAR RIB
- [SDR SWAA2026062507595](https://openairdocs.org/sdr/SWAA2026062507595), May 29, 2026: SUPPORT. CORRODED. CORROSION ON SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 RBL 22 WL 156.1 AT AFT CARGO BAY. REPLACED SUPPORT ZEE LOCATED WL156 BTW BS727 TO BS767 AND RBL22 WL 156.1
- [SDR SWAA2026062507597](https://openairdocs.org/sdr/SWAA2026062507597), May 29, 2026: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BTW BS 727E TO BS 787 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT. PERFORMED REPAIR LOC BTW BS727E MORE 10 INCH TO BS847 AND (CLIP) S
- [SDR SWAA2026062507596](https://openairdocs.org/sdr/SWAA2026062507596), May 29, 2026: CARGO TRACK. CRACKED. CRACK ON CARGO TRACK LOCATED BS 767 LBL 17.24 WL 156.1 AT AFT CARGO BAY. PERFORMED PERMANENT REPAIR LOCATED BETWEEN BS 747 MORE 5 INCH TO BS 767 MORE 15 INCH LB
- [SDR SWAA2026062507714](https://openairdocs.org/sdr/SWAA2026062507714), May 29, 2026: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED AFT FACE BS 500D, STR 28L AT FWD CARGO BAY. REPLACED SUPPORT ANGLE LOCATED AFT FACE BS 500D AT LEVEL STR 28L AT FWD CARGO COMPART
- [SDR SWAA2026062907209](https://openairdocs.org/sdr/SWAA2026062907209), May 28, 2026: SUPPORT BRACKET. CRACKED. CRACKED SUPPORT BRACKET, BS 540 AIR CONDITIONING BAY LT SIDE. INSPECTED AND REPLACED SUPPORT BRACKET ON PNEUMATIC DUCT BS 540 AND LBL 6 AT AIR CONDITIONING BAY 
- [SDR SWAA2026062907206](https://openairdocs.org/sdr/SWAA2026062907206), May 27, 2026: ACCESS PANEL. DELAMINATED. DELAMINATED ELEVATOR ACCESS PANEL 334GT ON LT ELEVATOR. REPAIRED ACCESS PANEL 334GT ON LT ELEVATOR IAW SRM 55-20-01-2R-4 REPAIR 4 AND SRM 51-70-04-2R-10, REPAIR
- [SDR SWAA2026062906689](https://openairdocs.org/sdr/SWAA2026062906689), May 26, 2026: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BTW BS 480 - 500D, STR 26L, WL 157 IN THE FWD CARGO BAY. PERFORMED PERMANENT REPAIR ON SUPPORT ZEE LOCATED BTW BS 480 - 500D, STR 
- [SDR SWAA2026062906534](https://openairdocs.org/sdr/SWAA2026062906534), May 26, 2026: FRAME. CRACKED. CRACK INDICATION ON FRAME WEB SURFACE AROUND FASTENER LOCATED AT BS 328 BETWEEN S-20R TO S-21R IN AVIONIC BAY. REPAIRED WITH THE REPLACEMENT OF FRAME AND STRAP 
- [SDR SWAA2026062906694](https://openairdocs.org/sdr/SWAA2026062906694), May 26, 2026: ACCESS PANEL. DELAMINATED. DELAMINATED ACCESS PANEL 194CL BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCES PANEL 194CL BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-04-2R-2, REPAIR 2.
- [SDR SWAA2026062506533](https://openairdocs.org/sdr/SWAA2026062506533), May 26, 2026: TIE CLIP. CRACKED. CRACK TIE CLIP LOCATED STA 500D AND STR 26L AT FWD CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED BS 500D AND STR 26L AT FWD CARGO COMPARTMENT IAW SRM 51-40-02 AN
- [SDR SWAA2026062506688](https://openairdocs.org/sdr/SWAA2026062506688), May 26, 2026: WEB. ELONGATED. ELONGATED HOLES ON SHIELD WEB BTW STA 492.4 TO STA 500A STR 26R AT FWD CARGO COMPARTMENT. REPLACED SHIELD WEB BTW STA 492.4 TO STA 500A STR 26R AT FWD CARGO COM
- [SDR SWAA2026062506692](https://openairdocs.org/sdr/SWAA2026062506692), May 26, 2026: INTERCOSTAL. CRACKED. CRACK ON INTERCOSTAL LOCATED BTW BS 685 - 706, STR 14L. REPLACED INTERCOSTAL LOCATED BTW BS 685 TO BS 706 AT LEVEL STR 14L AT PASSENGER CABIN IAW SRM 51-40-02 A
- [SDR SWAA2026062506693](https://openairdocs.org/sdr/SWAA2026062506693), May 26, 2026: STIFFENER. CRACKED. CRACKED ON STIFFENER LOCATED FWD FACE BULKHEAD BS 540 LBL 24.75 AT FWD CARGO BAY. REPLACED STIFFENER LOCATED AT FWD FACE BULKHEAD BS 540 LBL 24.75 AT FWD CARGO 
- [SDR SWAA2026062906304](https://openairdocs.org/sdr/SWAA2026062906304), May 25, 2026: RIB. CRACKED. CRACKED INSPAR RIB, STAB STA 120.30 AND 28 INCHES FROM FRONT SPAR, RT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR LOCATED ON INSPAR RIB 120.30 AT 28 INCHES FROM
- [SDR SWAA2026062506302](https://openairdocs.org/sdr/SWAA2026062506302), May 25, 2026: SUPPORT ANGLE. CRACKED. CRACK ON CARGO LINER SUPPORT ANGLE LOCATED BS 867 RBL 54 AT AFT CARGO COMPARTMENT. REPLACED ANGLE LINER SUPPORT LOCATED BTW BS847 TO BS 887+13? RBL 54 AT AFT CA
- [SDR SWAA2026062506303](https://openairdocs.org/sdr/SWAA2026062506303), May 25, 2026: SUPPORT ANGLE. CRACKED. CRACK ON CARGO LINER SUPPORT ANGLE LOCATED BS 727B LBL 52 AT AFT CARGO COMPARTMENT. PERFORMED REPAIR ON CARGO LINER SUPPORT ANGLE LOCATED BS 727B LBL 52 AT AFT 
- [SDR SWAA2026062506305](https://openairdocs.org/sdr/SWAA2026062506305), May 25, 2026: SUPPORT ANGLE. ELONGATED. ELONGATED HOLE ON CARGO LINER SUPPORT ANGLE LOCATED BS 947.5 RBL 41 AT AFT CARGO BAY. REPLACED ANGLE LINER SUPPORT AND FASTENERS LOCATED BTW BS887+13 TO 947.5 R
- [SDR SWAA2026062905869](https://openairdocs.org/sdr/SWAA2026062905869), May 23, 2026: ANGLE. CRACKED. CRACKED GUSSET ANGLE LOCATED BS 500D AT LEVEL STR 19R AT FWD CARGO BAY. REPLACED GUSSET ANGLE AND FASTENERS LOCATED BS 500D AT STR 19R AT FWD CARGO BAY IAW SRM 
- [SDR SWAA2026062905870](https://openairdocs.org/sdr/SWAA2026062905870), May 23, 2026: ANGLE. CRACKED. CRACK GUSSET ANGLE LOCATED BS 500D AT LEVEL STR 21L AT FWD CARGO BAY. REPLACED GUSSET ANGLE AND FASTENERS LOCATED BS 500D AT LEVEL STR 21L AT FWD CARGO COMPARTM
- [SDR SWAA2026062906012](https://openairdocs.org/sdr/SWAA2026062906012), May 23, 2026: STRINGER. CRACKED. CRACKED STRINGER 15L BTW BS 294.5 - BS 303.9 IN FWD GALLEY AREA. PERFORMED PERMANENT REPAIR LOCATED ON STR 15L BETWEEN BS 277 MORE 10 INCHES TO BS 294.5 AT FWD 
- [SDR SWAA2026062906011](https://openairdocs.org/sdr/SWAA2026062906011), May 23, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE LOCATED BS 294.5 AT LEVEL STR 13L AT FWD GALLEY AREA. REPLACED THE SUPPORT ANGLE AND FASTENERS LOCATED BS 294.5 AT LEVEL STR 13L AT FWD GA
- [SDR SWAA2026062505863](https://openairdocs.org/sdr/SWAA2026062505863), May 23, 2026: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED FWD FACE BS 695 BL 0 WL 208.1 REPLACED SUPPORT ANGLE AND FASTENERS LOCATED FWD FACE BS 695 BL 0 WL 208.1 RT SIDE AT PASSENGER CAB
- [SDR SWAA2026062505868](https://openairdocs.org/sdr/SWAA2026062505868), May 23, 2026: ANGLE. CRACKED. CRACK ON ANGLE LOCATED FWD FACE BS 500C AT LEVEL STR 26L AT FWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS LOCATED FWD FACE BS 500C AT LEVEL STR 26L IAW SRM 51
- [SDR SWAA2026062506013](https://openairdocs.org/sdr/SWAA2026062506013), May 23, 2026: TIE CLIP. CRACKED. CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA. REPLACED TIE CLIP AND FASTENERS, BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW SRM 51-10-
- [SDR SWAA2026062505865](https://openairdocs.org/sdr/SWAA2026062505865), May 23, 2026: GUSSET. CRACKED. CRACKED GUSSET ANGLE LOCATED BS 500D AT LEVEL STR 19L AT FWD CARGO BAY. REPLACED GUSSET ANGLE AND FASTENERS LOCATED BS 500D STR 19L AT FWD CARGO BAY IAW SRM 51-
- [SDR SWAA2026062505441](https://openairdocs.org/sdr/SWAA2026062505441), May 21, 2026: HANDLE. DETERIORATED. DETERIORATED WASHER ASSISST HANDLE FWD ENTRY DOOR LINING. REPLACED WASHER ASSIST HANDLE FWD ENTRY DOOR LINING IAW AMM 52-11-31-400-802 STEP 3.G. ITEM (2)(B).
- [SDR SWAA2026062505438](https://openairdocs.org/sdr/SWAA2026062505438), May 21, 2026: STUB FRAME. CRACKED. CRACK INDICATION ON STUB FRAME LOCATED BETWEEN BS 294.5 TO BS 296.5 AND BETWEEN S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 0.250 IN. APPROX.AT PASSENGER 
- [SDR SWAA2026062505064](https://openairdocs.org/sdr/SWAA2026062505064), May 20, 2026: CROSSBEAM. CRACKED. CRACKED BRAKE PANEL LOCATED BS 540 BTW BL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN. REPLACED BRAKE PANEL LOCATED BS 540 BTW BL 0 TO LBL 24.75 WL 208.1 AT PASS
- [SDR SWAA2026062505068](https://openairdocs.org/sdr/SWAA2026062505068), May 20, 2026: PRESSURE DECK. CRACKED. CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB LBL 31 STA 663 AT PASSENGER CABIN. PERFORMED REPAIR ON HORIZONTAL PRESSURE DECK WEB LBL 31 STA 663 AT PASSENGER
- [SDR SWAA2026050595334](https://openairdocs.org/sdr/SWAA2026050595334), May 4, 2026: ENGINE. FIRE. WHILE TAXING FOR T/O ACFT BEHIND STATED FLAMES COMING OUT OF THE NR 2 ENGINE. ALL ENGINE PARAMETERS NORMAL. CFR FIRE, RESCUE DID NOT OBSERVE ANY FLAMES OR SMOKE
- [SDR SWAA2025100319466](https://openairdocs.org/sdr/SWAA2025100319466), Sep 30, 2025: LAMP. INOPERATIVE. ENTRY DOOR L-1 EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP PER M/M 33-51-04.
- [SDR SWAA2025100319477](https://openairdocs.org/sdr/SWAA2025100319477), Sep 30, 2025: BATTERY PACK. FAILED. LEFT FWD EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2025100319478](https://openairdocs.org/sdr/SWAA2025100319478), Sep 30, 2025: BATTERY PACK. FAILED. L/H AFT EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2025100319479](https://openairdocs.org/sdr/SWAA2025100319479), Sep 30, 2025: BATTERY PACK. FAILED. R/H AFT EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2025021094064](https://openairdocs.org/sdr/SWAA2025021094064), Feb 6, 2025: ENGINE. BIRD INGESTION. INGESTED BIRD ON #1 ENGINE ON FINAL APPROACH . IMEDIATELY SMELLED IN CABIN AND COCKPIT. FELT A VIBRATION ON LEFT SIDE BUT ALL ENGINE PARAMETERS NORMAL. REDUCED 
- [SDR SWAA2024121978818](https://openairdocs.org/sdr/SWAA2024121978818), Dec 18, 2024: FLOOR SUPPORT. CRACKED. FWD CARGO COMPARTMENT AC DISTRIBUTION BAY CABIN FLOOR SUPPORT CRACKED AT FWD AND AFT INBD FASTENERS LOCATED R/H OF BASELINE 0 STATION 540<[01] R&R FWD CARGO COM
- [SDR SWAA2024101648042](https://openairdocs.org/sdr/SWAA2024101648042), Oct 12, 2024: SLIDE. DISLODGED. SLIDE POPPED OUT OF PLACE R1 DOOR<[01] REINSTALLED SLIDE AT R1 DOOR PER MT 725-61-06
- [SDR SWAA2024081927629](https://openairdocs.org/sdr/SWAA2024081927629), Aug 18, 2024: TRANSMITTER. INOPERATIVE. DURING CONFIGURATION FOR LDG FLAPS INDICATE 25* WITH 30* SELECTED. RAN QRH AND LANDED; AFTER LANDING FLAPS INDICATED 30*<[01] R&R L/H T/E FLAP POSITION TRANSMIT
- [SDR SWAA2024070105294](https://openairdocs.org/sdr/SWAA2024070105294), Jun 24, 2024: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS ASSOCIATED WITH M1672; M1673; AND M1674 ARE INOP. EMERGENCY EXIT LIGHTS ASSOCIATED WITH M1672 M1673 AND M1674 ARE INOP.<[01] REMOVED; REPL
- [SDR SWAA2024070291788](https://openairdocs.org/sdr/SWAA2024070291788), May 30, 2024: DOOR FRAME. CRACKED. FRAME CRACKED ON FED CUTOUT AT BS 312 LBL 53 WL 216 ; BELOW S-5L.<[01] UPON INVESTIGATION FOUND FRAME CRACKED ON FED CUTOUT AT BS 312 LBL 53 WL 283 ; BELOW S-5L

All 261: https://openairdocs.org/aircraft/N260WN/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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