# N261WN: 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: 32517
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 13, 2006
- Certificate issued: January 31, 2007
- Expires: June 30, 2029
- Mode S code: A284B5
- 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=261WN
- Page: https://openairdocs.org/aircraft/N261WN

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 (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB WPR12LA053](https://openairdocs.org/ntsb/WPR12LA053), Dec 2, 2011: Boeing 737-7H4 (N261WN), Oakland, CA, no damage. Probable cause: The flight crew’s flight into known severe turbulence associated with mountain wave activity.

## 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.

- [Accident 20111201030229A](https://openairdocs.org/incident/20111201030229A), Dec 1, 2011: Boeing 737-7H4 (N261WN), Mammoth Lakes, CA, No damage. This is a FAA final report and is now considered closed. NTSB report will remain open until 12/1/2012 iaw NTSB policy of one year from date of occurrence. On…

## Service difficulty reports (241, 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 SWAA2026061511326](https://openairdocs.org/sdr/SWAA2026061511326), Jun 10, 2026: FIRE LOOP. FAULTED. NR 2 ENG FIRE LOOP A GIVES FAULT LIGHT. OK TO CONTINUE PER MEL 26-2-01. REMOVED AND REPLACED THE NR 2 ENG FIRE LOOP A UPPER. IAW AMM 26-11-01. OPS CHECKED OK.
- [SDR SWAA2026041488197](https://openairdocs.org/sdr/SWAA2026041488197), Apr 11, 2026: FLOOR PANEL. CRACKED. AFT CARGO BIN FLOOR CRACKED. PANEL 140CF 15. OK TO CONTINUE IAW MEL 25-16-01 SP1B AUTH 314501. R & R AFT FLOOR PANEL 140CF IAW AMM25-52-10.
- [SDR SWAA2026010658063](https://openairdocs.org/sdr/SWAA2026010658063), Jan 4, 2026: LOCK. LOOSE. SEAT 11D OVER RECLINES INTO EXIT ROW. SECURED RECLINE LOCK IAW CMM 25-21-42. NO FURTHER DEFECTS NOTED FOR SEAT 11D.
- [SDR SWAA2025102025128](https://openairdocs.org/sdr/SWAA2025102025128), Oct 17, 2025: BATTERY PACK. NO TEST. L/H AFT EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06
- [SDR SWAA2025091514592](https://openairdocs.org/sdr/SWAA2025091514592), Sep 14, 2025: SLIDE. OUT OF LIMITS. R2 SLIDE OUT OF LIMITS. REMOVED AND REPLACED THE R2 SLIDE IAW AMM 25-60 6-01.
- [SDR SWAA2025063086339](https://openairdocs.org/sdr/SWAA2025063086339), Jun 27, 2025: SHIMMY DAMPENER. VIBRATION. AT ROTATION AIRCRAFT YAWED TO THE LEFT WITH A VIBRATION FELT; AFTER ABEING AIRBORNE NO FLIGHT CONTROL DISCREPANCIES NOTICED; NO ABNORMAL ENGINE PERAMETERS NOTED
- [SDR SWAA2025042940304](https://openairdocs.org/sdr/SWAA2025042940304), Apr 25, 2025: GLOWSTRIP. DAMAGED. FO SIDE 1ST ROW PHOTOLUMINESCENT STRIP DAMAGED<[01] OK TO CONTINUE PER MEL 33-19-01 SP1<BR>AUTH# 248928;[02] REMOVED AND REPLACED FO SIDE 1ST ROW PHOTOLUMINESCE
- [SDR SWAA2025030502296](https://openairdocs.org/sdr/SWAA2025030502296), Mar 5, 2025: ELEC CONNECTOR. FAILED. LEADING EDGE FLAPS + SLATS AND TRAILING EDGE FLAPS DID NOT EXTEND WHEN FLAPS LEVER PLACED TO FIVE. FLAP ASYMMETRY INDICATED WHEN ALT FLAP SWITCHED DOWN. LEADING
- [SDR SWAA2025030502292](https://openairdocs.org/sdr/SWAA2025030502292), Mar 5, 2025: TRANSMITTER. FAILED. LEADING EDGE FLAPS + SLATS AND TRAILING EDGE FLAPS DID NOT EXTEND WHEN FLAPS LEVER PLACED TO FIVE. FLAP ASYMMETRY INDICATED WHEN ALT FLAP SWITCHED DOWN. LEADING
- [SDR SWAA2024110656273](https://openairdocs.org/sdr/SWAA2024110656273), Nov 3, 2024: LIGHT. INOPERATIVE. FLOOR LIGHTING STRIP SEGMENT INOP. FRONT; FO SIDE ROW 1.<[01] R&R FLOOR LIGHTING STRIP AT ROW 1; FO?S SIDE PER AMM 25-27-31.
- [SDR SWAA2024070910031](https://openairdocs.org/sdr/SWAA2024070910031), Jul 6, 2024: BATTERY. FAULTED. POPPED OUT C/B LIGHTING EMER CHGR WHEN TURN THE EMER EXIT LIGHT SWITCH TO OFF POSITION<[01] REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY M1673 IAW B737-7
- [SDR SWAA2024070809527](https://openairdocs.org/sdr/SWAA2024070809527), Jul 6, 2024: SLIDE. OUT OF POSITION. PAX CABIN AFT LEFT ENTRY DOOR SLIDE LOWER COVER IS CHAFFING AGAINST WITH SCUFF PLATE WHEN TO CLOSE THE DOOR 2024-361966<[01] PERFORMED REPOSITION OF SLIDE IN TH
- [SDR SWAA2024070806972](https://openairdocs.org/sdr/SWAA2024070806972), Jun 28, 2024: SCUFF PLATE. CRACKED. CRACK ON SERVICE DOOR SCUFF PLATE CENTER SIDE AT FWD GALLEY AREA 2024-361946<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:A23217720;DUE DATE:14-FEB-25.;[02
- [SDR SWAA2024070999413](https://openairdocs.org/sdr/SWAA2024070999413), Jun 7, 2024: SUPPORT BRACKET. CRACKED. CRACK BODY STATION 540 SUPPORT BRACKET LOCATED AT LT SIDE AT KEEL BEAM 2024-361808<[01] REPLACED BODY STATION 540 SUPPORT BRACKET LOCATED AT LT SIDE AT KEEL BEA
- [SDR SWAA2024070999412](https://openairdocs.org/sdr/SWAA2024070999412), Jun 7, 2024: SUPPORT BRACKET. CRACKED. CRACK SLAT 1 AUXILIARY TRACK ON SUPPORT BRACKET LOCATED LEADING EDGE AREA INTERNAL CAVITY AT LT WING 2024-361803<[01] REPLACED SUPPORT BRACKET LOCATED SLAT 1 AU
- [SDR SWAA2024070899084](https://openairdocs.org/sdr/SWAA2024070899084), Jun 7, 2024: FITTING. DETERIORATED. DETERIORATED HARDWARE GIRT BAR FITTING ON FWD SERVICE AND ENTRY DOOR AT FWD GALLEY AREA 2024-361788<[01] REPLACED HARDWARE GIRT BAR FITTING ON FWD SERVICE AND E
- [SDR SWAA2024070899086](https://openairdocs.org/sdr/SWAA2024070899086), Jun 7, 2024: FITTING. DETERIORATED. DETERIORATED HARDWARE GRIT BAR FITTING ON AFT SERVICE AND ENTRY DOOR AT AFT GALLEY AREA 2024-361792<[01] REPLACED HARDWARE GRIT BAR FITTING ON AFT SERVICE AND E
- [SDR SWAA2024070999077](https://openairdocs.org/sdr/SWAA2024070999077), Jun 6, 2024: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BTW BS727 TO BS787 WL156 LBL21 AT AFT CARGO COMPARTMENT 2024-361772<[01] TOOL USED ON STEP 3 UT EQUIPMENT P/N: 45MG; S/N: 13006410
- [SDR SWAA2024070999076](https://openairdocs.org/sdr/SWAA2024070999076), Jun 6, 2024: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BTW BS727 TO BS767 WL156 AND RBL21 AT AFT CARGO COMPARTMENT 2024-361770<[01] TOOL USED ON STEP 3 UT EQUIPMENT P/N: 45MG; S/N: 1300
- [SDR SWAA2024070999074](https://openairdocs.org/sdr/SWAA2024070999074), Jun 6, 2024: CARGO TRACK. CRACKED. CRACK TRACK RBBL 13.84 AT LEVEL OF BS 767 AFT CARGO COMPARTMENT 2024-361768<[01] TOOL USED ON STEP 4 AND 5: EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X1693
- [SDR SWAA2024070999075](https://openairdocs.org/sdr/SWAA2024070999075), Jun 6, 2024: CARGO TRACK. CRACKED. CRACK TRACK RBBL 13.84 AT LEVEL OF BS 727E AFT CARGO COMPARTMENT 2024-361771<[01] FAULT WAS RESOLVED ON ANOTHER FAULT DUE TO REPAIR WAS PERFORMED FROM BS 727D P
- [SDR SWAA2024070999072](https://openairdocs.org/sdr/SWAA2024070999072), Jun 6, 2024: ACCESS PANEL. CRACKED. CRACK BLADE ACCESS PANEL 343AB AT RT HORIZONTAL STAB 2024-361769<[01] REPLACED BLADE ASSY LOC. ACCESS PANEL 343AB AT RT HORIZONTAL STAB I.A.W. B737-700 SRM 51-4
- [SDR SWAA2024070998561](https://openairdocs.org/sdr/SWAA2024070998561), Jun 5, 2024: SUPPORT. CRACKED. CRACK BILGE AREA SUPPORT ZEE LOCATED BETWEEN STA 500B TO STA 500C RH SIDE AT FWD CARGO COMPARTMENT 2024-361692<[01] REPLACED SUPPORT ZEE LOCATED BETWEEN STA 500
- [SDR SWAA2024070998756](https://openairdocs.org/sdr/SWAA2024070998756), Jun 5, 2024: FITTING. DETERIORATED. DETERIORATED GIRT BAR FITTING SLEEVE ON ACCESS FLOOR PANEL 242UF (2EA) AND 241ABF (2EA) AT AFT GALLEY AREA (4EA) 2024-361723<[01] REPLACED GIRT BAR FITTING SLEE
- [SDR SWAA2024070998415](https://openairdocs.org/sdr/SWAA2024070998415), Jun 5, 2024: STIFFENER. CRACKED. CRACK ON STIFFENER LOCATED BS 540 BTW BL 0 TO LBL 24.75 AT PASSENGER CABIN 2024-361678<[01] REPLACED STIFFENER AND FASTENERS LOCATED ON BS 540 BETWEEN BL 0 TO L
- [SDR SWAA2024070898757](https://openairdocs.org/sdr/SWAA2024070898757), Jun 5, 2024: SCUFF PLATE. CRACKED. CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT 2024-361725<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:B20189516;DUE DATE:17-JAN-25.;[02] TOOL USED
- [SDR SWAA2024070898560](https://openairdocs.org/sdr/SWAA2024070898560), Jun 5, 2024: INTERCOSTAL. CRACKED. CRACK ENTRY DOOR CUT OUT WEB INTERCOSTAL AT S-16L AND BETWEEN STA294.5 TO STA 303.9 AT FWD GALLEY AREA 2024-361693<[01] REPLACED INTERCOSTAL AND FASTENERS LOCAT
- [SDR SWAA2024070810380](https://openairdocs.org/sdr/SWAA2024070810380), Jun 5, 2024: INTERCOSTAL. CRACKED. CRACK ENTRY DOOR CUT OUT WEB INTERCOSTAL AT S-16L AND BETWEEN STA294.5 TO STA 303.9 AT FWD GALLEY AREA 2024-361693<[01] REPLACED INTERCOSTAL AND FASTENERS LOCAT
- [SDR SWAA2024070898565](https://openairdocs.org/sdr/SWAA2024070898565), Jun 5, 2024: SUPPORT ANGLE. CRACKED. CRACK ENTRY DOOR CUT OUT SUPPORT ANGLE LOCATED AT FWD FACE THE STA294.5 AND S-13L AT FWD GALLEY AREA 2024-361700<[01] REPLACED SUPPORT ANGLE LOCATED ENTRY DOOR 
- [SDR SWAA2024070898563](https://openairdocs.org/sdr/SWAA2024070898563), Jun 5, 2024: TIE CLIP. CRACKED. CRACK FWD SERVICE DOOR CUT OUT TIE-CLIP AT S-10R AND STA 277 AT PASSENGER CABIN 2024-361697<[01] REPLACED TIE-CLIP AND FASTENERS AT FWD SERVICE DOOR CUT OUT S-1
- [SDR SWAA2024070810381](https://openairdocs.org/sdr/SWAA2024070810381), Jun 5, 2024: TIE CLIP. CRACKED. CRACK FWD SERVICE DOOR CUT OUT TIE-CLIP AT S-10R AND STA 277 AT PASSENGER CABIN 2024-361697<[01] REPLACED TIE-CLIP AND FASTENERS AT FWD SERVICE DOOR CUT OUT S-1
- [SDR SWAA2024070898411](https://openairdocs.org/sdr/SWAA2024070898411), Jun 4, 2024: STRUCTURE. CRACKED. CRACK INNER CHORD AT STA 312 AND AT LEVEL S-17L AT FWD GALLEY AREA 2024-361648<[01] REPLACED INNER CHORD; BS 270 TO BS 360 AND LBL 55 AT FWD GALLEY AREA I.A.W B
- [SDR SWAA2024070998038](https://openairdocs.org/sdr/SWAA2024070998038), Jun 3, 2024: FLOORBEAM. CRACKED. CRACK FLOOR BEAM LOCATED STA 328 RBL 20 AT FWD GALLEY AREA 2024-361601<[01] TOOL USED EDDY CURRENT HIGH FREQUENCY INSPECTION P/N: NORTEC600D; S/N: 60009161631; 
- [SDR SWAA2024070998041](https://openairdocs.org/sdr/SWAA2024070998041), Jun 3, 2024: FLOOR SUPPORT. CRACKED. CRACK WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 312 TO BS 328 AND LBL 45 FWD GALLEY AND LAV 2024-361600<[01] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED F
- [SDR SWAA2024070998043](https://openairdocs.org/sdr/SWAA2024070998043), Jun 3, 2024: FLOORBEAM. CORRODED. CORROSION FLOOR BEAM LOCATED STA 986.5 LBL 43 WL 208.1 AT AFT GALLEY AREA 2024-361607<[01] TOOL USED: ULTRASONIC EQUIPMENT P/N: 45MG; S/N: 130063701; DUE DATE: 
- [SDR SWAA2024070898045](https://openairdocs.org/sdr/SWAA2024070898045), Jun 3, 2024: FLOORBEAM. CORRODED. CORROSION FLOOR BEAM LOCATED STA 986.5 RBL 43 WL 208.1 AT AFT GALLEY AREA 2024-361606<[01] TOOL USED: ULTRASONIC EQUIPMENT P/N: 45MG; S/N: 130063701; DUE DATE: 
- [SDR SWAA2024070898042](https://openairdocs.org/sdr/SWAA2024070898042), Jun 3, 2024: FLOOR SUPPORT. CRACKED. CRACK WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 328 TO BS 344 AND LBL 45 FWD GALLEY AND LAV 2024-361603<[01] REPLACED WEB - INTERCOSTAL LOCATED FLOOR STRUCTU
- [SDR SWAA2024070898044](https://openairdocs.org/sdr/SWAA2024070898044), Jun 3, 2024: INTERCOSTAL. CRACKED. CRACK WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AND LAV 2024-361597<[01] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED F
- [SDR SWAA2024070810383](https://openairdocs.org/sdr/SWAA2024070810383), Jun 3, 2024: WEB. CRACKED. CRACK WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AND LAV 2024-361597<[01] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED F
- [SDR SWAA2024070997363](https://openairdocs.org/sdr/SWAA2024070997363), Jun 2, 2024: VAPOR BARRIER. CRACKED. (CUSTOMER REQUEST) CRACK ON VAPOR BARRIER LOCATED ON BS 663 LH SIDE AT WING CENTER SECTION. 2024- 361522<[01] CALIPER P/N: 8647A42; S/N: B22058354; DUE DATE: 07
- [SDR SWAA2024070997678](https://openairdocs.org/sdr/SWAA2024070997678), Jun 2, 2024: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET TRAILING EDGE ORSS 271 RT WING 2024-361560<[01] REPLACED SUPPORT BRACKET TRAILING EDGE ORSS 271 RT WING IAW B737-700 SRM 51-10-02 ITEM 9.<
- [SDR SWAA2024070997671](https://openairdocs.org/sdr/SWAA2024070997671), Jun 2, 2024: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE ORSS 271 LT WING 2024-361555<[01] REPLACED ANGLE LOCATED ON TRAILING EDGE ORSS 271 LT WING I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 A
- [SDR SWAA2024070906492](https://openairdocs.org/sdr/SWAA2024070906492), Jun 2, 2024: SUPPORT BEAM. WORN. WEAR ON DEFLECTION CONTROL RIB SUPPORTS BEAM O/B TRAILING EDGE AT LT WING 2024-361557. POWER PACK P/N: PE1068; S/N: PE0318-95852; DUE DATE: 16-SEP-25. REPAIRED 
- [SDR SWAA2024070897673](https://openairdocs.org/sdr/SWAA2024070897673), Jun 2, 2024: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED BS693 RBL25 AND WL202 AT PASSENGER CABIN 2024-361562<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; D
- [SDR SWAA2024070810382](https://openairdocs.org/sdr/SWAA2024070810382), Jun 2, 2024: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED BS693 RBL25 AND WL202 AT PASSENGER CABIN 2024-361562<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; D
- [SDR SWAA2024070997361](https://openairdocs.org/sdr/SWAA2024070997361), Jun 1, 2024: ACCESS PANEL. DELAMINATED. DELAMINATED ACCESS PANEL 193AL BODY FAIRING AT LOWER FUSELAGE 2024-361518<[01] TOOL USED CALIPER PN: 500-197-30; SN: B20189521; DUE DATE: 26/JAN/25.;[02] TOOL U
- [SDR SWAA2024070897048](https://openairdocs.org/sdr/SWAA2024070897048), Jun 1, 2024: HANDLE. DETERIORATED. DETERIORATED PLASTIC NUT OF ASSIST HANDLES AT FWD ENTRY DOOR (4 EA) 2024-361511<[01] REPLACED PLASTIC NUT OF ASSIST HANDLES AT FWD ENTRY DOOR I.A.W B737-700 AMM
- [SDR SWAA2024042578730](https://openairdocs.org/sdr/SWAA2024042578730), Apr 23, 2024: HOLDER. LOOSE. R2 GIRT BAR DOES NOT STAY SECURE WHEN DOOR IS OPENED<[01] INCREASE CLIP PRESSURE PER SIP
- [SDR SWAA2024041172760](https://openairdocs.org/sdr/SWAA2024041172760), Apr 10, 2024: GIRT BAR. DAMAGED. FWD ENTRY DOOR ESCAPE SLIDE GIRT BAR SKIRT FLAP RUBBER DISBONDED. R&R FWD ENTRY DOOR ESCAPE SLIDE IAW MT 725-61-06. INSPECTION C/W R&R FWD ENTRY DOOR ESCAPE SLI
- [SDR SWAA2024041172752](https://openairdocs.org/sdr/SWAA2024041172752), Apr 10, 2024: ISOLATOR. CRACKED. AFT SERVICE DOOR EMERGENCY SLIDE AFT LOWER ISOLATOR CRACKED. R & R AFT SERVICE DOOR EMERGENCY SLIDE AFT LOWER ISOLATOR IAW SRM 51-40-02.

All 241: https://openairdocs.org/aircraft/N261WN/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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