# N267WN: 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: 32525
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 25, 2007
- Certificate issued: March 30, 2007
- Expires: December 31, 2029
- Mode S code: A29AFF
- 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=267WN
- Page: https://openairdocs.org/aircraft/N267WN

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 N267WN.

## FAA accident and incident reports (1)

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

- [Incident 20090309004249I](https://openairdocs.org/incident/20090309004249I), Mar 9, 2009: Boeing 7377H4 (N267WN), Albany, NY, Minor damage. (-23) On 03/09/2009, at approximately 12:25, ground operations crew prepared the aircraft for push-back from the gate to the de-icing pad "a". Once the dual…

## Service difficulty reports (303, 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 SWAA2026070718223](https://openairdocs.org/sdr/SWAA2026070718223), Jul 3, 2026: BATTERY PACK. NO TEST. 20 ABC EMERGENCY BATTERY PACK AT1670 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026070718218](https://openairdocs.org/sdr/SWAA2026070718218), Jul 3, 2026: BATTERY PACK. NO TEST. RT EMERGENCY EXIT EMERGENCY BATTERY. PACK AT 1669 FAILED CAPACITY CHECK. R&R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06
- [SDR SWAA2026021169123](https://openairdocs.org/sdr/SWAA2026021169123), Feb 9, 2026: LIGHT. INOPERATIVE. FIRST OFFICER`S SIDE EMERGENCY WINDOW LIGHT INOPERATIVE. R & R THE EMERGENCY WINDOW LIGHT . OPS CHECKED GOOD IAW AMM 33-21-00.
- [SDR SWAA2025102025675](https://openairdocs.org/sdr/SWAA2025102025675), Oct 18, 2025: SEAL. MISSING. CAPTAIN L2 WOULD NOT SEAL. AIRPLANE WOULD NOT PRESSURIZE;CABIN CLIMBING AT CLIMB RATE.ON LANDING SMOOTH TOUCHDOWN WITH NO SIDE LOADING ON AIRPLANE.NOSE WHEEL TO
- [SDR SWAA2025013191498](https://openairdocs.org/sdr/SWAA2025013191498), Jan 31, 2025: DOOR. CRACKED. L/H MAIN LANDING GEAR CENTER STRUT DOOR IS CRACKED ON LOWER FWD POCKET .<[01] REMOVED LG L/H CTR & INNER DOOR ASSEMBLY. I.A.W. AMM 32-13-11 OK TO CONTINUE SERVI
- [SDR SWAA2024092038677](https://openairdocs.org/sdr/SWAA2024092038677), Sep 18, 2024: BULB. BURNED OUT. EMERGENCY EXIT SIGN ABOVE FWD ENTRY DOOR HAS BURNED OUT BULBS<[01] RELAMPED AND PERFORMED GOOD OPERATIONAL TEST OF EMERGENCY EXIT SIGN ABOVE FWD ENTRY DOOR IAW 
- [SDR SWAA2024092039086](https://openairdocs.org/sdr/SWAA2024092039086), Sep 18, 2024: BULB. INOPERATIVE. LH ASD EMERGENCY EXIT LIGHT INOP<[01] REPLACED LH SLIDE EMERGENCY LIGHT BULB AND PERFORMED GOOD OPERATIONAL TEST PER AMM 33-51-04-960-801.;[02] VERIFIED CORRECT
- [SDR SWAA2024092038676](https://openairdocs.org/sdr/SWAA2024092038676), Sep 17, 2024: WIRE. DISCONNECTED. G-1 GALLEY EMERGENCY LIGHT IS NOT CONNECTED.<[01] DISPLACED G-1 GALLEY FWD SIDE WALL; CONNECTED EMERGENCY LIGHT AND INSTALLED FWD GALLEY SIDE WALL IAW AMM 25-21
- [SDR SWAA2024092038546](https://openairdocs.org/sdr/SWAA2024092038546), Sep 14, 2024: BATTERY PACK. FAILED. BATTERIES PACKS M1675 AND M1673 FAIL TEST<[01] REPLACED EMERGENCY BATTERIES PACKS M1673 AND M1675 PER AMM 33-51-06-960-805; STEP 4.A THRU 4.E(1-5);[02] VERIFIED
- [SDR SWAA2024091933592](https://openairdocs.org/sdr/SWAA2024091933592), Sep 3, 2024: STIFFENER. CRACKED. DURING NDI HFEC INSPECTION; FOUND LEFT HORIZONTAL STAB RIB 3 STIFFENER 4 IS CRACKED; L:0.5' MARKED<[01] REPAIRED LEFT HORIZONTAL STAB RIB 3 STIFFENER 4 IAW SRM 
- [SDR SWAA2024091930070](https://openairdocs.org/sdr/SWAA2024091930070), Aug 25, 2024: STUB FRAME. CRACKED. DURING HFEC OPEN HOLES INSPECTION; CRACK NOTED AT HOLE COMMON TO VERTICAL FLANGE OF MOPSILL AND STUB FRAME AT BS294.5; RBL 54; WL208.5<[01] VERIFIED STEPS 1;2 C
- [SDR SWAA2024092027725](https://openairdocs.org/sdr/SWAA2024092027725), Aug 19, 2024: WEB. CRACKED. L/H WEB AT BS 993.50 CRACKED/DAMAGED COMMON TO LAV 'B' O/B MOUNT<[01] REMOVED; REPLACED; AND INSTALLED A NEW L/H WEB AT BS 993.50; LBL33.80; WL208 IAW SRM 51-40
- [SDR SWAA2024092325858](https://openairdocs.org/sdr/SWAA2024092325858), Aug 14, 2024: SEAL. CRACKED. RT HORIZ STAB F/S UPPER SLIDE SEAL CRACKED.<[01] RECEIVED NEW RT SLIDE SEAL AND REMOVED AND REPLACED SLIDE SEAL ATTACHMENT FITTING ON NEW PART IAW SRM 51-40-02-
- [SDR SWAA2024092325856](https://openairdocs.org/sdr/SWAA2024092325856), Aug 14, 2024: SPAR WEB. CORRODED. CORROSION ON LH WING REAR SPAR WEB AT UPPER END OF CUTOUT FOR #1 FUEL TANK AFT BOOST PUMP<[01] VERIFIED APPLICABILITY OF SRM 57-20-10-1A-3 PER STC ST00830SE;[02
- [SDR SWAA2024092325857](https://openairdocs.org/sdr/SWAA2024092325857), Aug 14, 2024: SEAL. CRACKED. LT HORIZ STAB F/S UPPER SLIDE SEAL CRACKED.<[01] RECEIVED NEW LT SLIDE SEAL AND REMOVED AND RE-INSTALLED EXISTING SLIDE SEAL ATTACHMENT FITTING ON NEW PART IAW 
- [SDR SWAA2024092025854](https://openairdocs.org/sdr/SWAA2024092025854), Aug 13, 2024: SHIELD. CORRODED. CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] REMOVED DAMAGED ACB SHIELD FWD OF ACD BS 767-
- [SDR SWAA2024091925849](https://openairdocs.org/sdr/SWAA2024091925849), Aug 13, 2024: PLATE. 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 DAMAGED L/H FLOOR TO 
- [SDR SWAA2024091925850](https://openairdocs.org/sdr/SWAA2024091925850), Aug 13, 2024: SUPPORT. 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] REMOVED DAMAGED R/H FLOOR
- [SDR SWAA2024092025439](https://openairdocs.org/sdr/SWAA2024092025439), Aug 12, 2024: THRESHOLD. CRACKED. AFT CARGO BAY AFT CORNER THRESHOLD IS CRACKED<[01] REPAIRED AFT CARGO BAY AFT CORNER THRESHOLD PER SRM 53-60-15-2R-1;[02] VERIFIED STEPS 5;6 COMPLETE; ALL STEPS
- [SDR SWAA2024092324295](https://openairdocs.org/sdr/SWAA2024092324295), Aug 8, 2024: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL BS 344-360 BL 0 WL 208.<[01] REMOVED AND REPLACED INTERCOSTAL BS 344-360 BL 0 WL 208 IAW SRM 51-40-02-0G-0 AND BOEING DOCUMENT NUMBER 141A54
- [SDR SWAA2024092324299](https://openairdocs.org/sdr/SWAA2024092324299), Aug 8, 2024: FRAME. CRACKED. CRACKED FRAME BS 312 COMMON TO STRINGER 6L.<[01] ACCOMPLISHED REPAIR OF FRAME AT STA 312; STR 7L PER EA M-22-153-01244; DOCUMENTED ON TASK ID TTG8Q00V943A;[02] 
- [SDR SWAA2024092324296](https://openairdocs.org/sdr/SWAA2024092324296), Aug 8, 2024: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL BS 312-328 LBL 46 WL 208.<[01] ALL STEPS COMPLETED REMOVED INTERCOSTAL BS 312-328 LBL 46 WL 208 PER SRM 51-40-02 COMPLETED MEASURMENT TABLE 
- [SDR SWAA2024092324308](https://openairdocs.org/sdr/SWAA2024092324308), Aug 8, 2024: SKIN. DEBONDED. RH #8 FLIGHT SPOILER UPPER SURFACE HAS DISBOND 2.9' FROM O/B EDGE AND 8.3' FROM T/E.<[01] REMOVED AND REPLACED RH #8 FLIGHT SPOILER IAW AMM 27-61-11-400-801;[02
- [SDR SWAA2024092024058](https://openairdocs.org/sdr/SWAA2024092024058), Aug 8, 2024: STUB FRAME. CRACKED. CRACK ON FSD STUB FRAME. LOCATED AT BS 291.5 + 10; .7' ABOVE SEAL DEPRESSOR; .4' IN LENGTH (MARKED) CORRECTION TO FAULT NAME: CRACK FOUND ON FSD STUB FRAME<[01]
- [SDR SWAA2024092024300](https://openairdocs.org/sdr/SWAA2024092024300), Aug 8, 2024: SUPPORT ANGLE. CRACKED. CRACKED SCUFF PLATE SUPPORT ANGLE FWD LOWER CORNER OF FWD ENTRY DOOR CUTOUT BS 309 WL 217.<[01] REMOVED AND REINSTALLED SCUFFPLATE SUPPORT ANGLE FWD LOWER CORNE
- [SDR SWAA2024092024303](https://openairdocs.org/sdr/SWAA2024092024303), Aug 8, 2024: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL BS 277-294 RBL 1 WL 208.<[01] REMOVED CRACKED INTERCOSTAL @ BS 277-294 RBL 1 WL 208 PER SRM 51-40-02 AND LOCATED AND DRILLED NEW INTERCOSTAL
- [SDR SWAA2024092024304](https://openairdocs.org/sdr/SWAA2024092024304), Aug 8, 2024: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL BS 328-344 LBL 46 WL 208.<[01] REMOVED CRACKED INTERCOSTAL AT BS 328 TO 344 LBL 46 WL 208 IAW SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW INTE
- [SDR SWAA2024092024305](https://openairdocs.org/sdr/SWAA2024092024305), Aug 8, 2024: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL BS 380-400 LBL 14 WL 208.<[01] ALL STEPS COMPLETED REMOVED CRACKED INTERCOSTAL BS 380-400 LBL 14 WL 208 PER SRM 51-40-02 COMPLETED MEASUREME
- [SDR SWAA2024092024297](https://openairdocs.org/sdr/SWAA2024092024297), Aug 8, 2024: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL BS 380-400 LBL 1 WL 208.<[01] REMOVED CRACKED INTERCOSTAL BS 380-400 LBL 1 WL 208 PER SRM 51-40-02 AND LOCATED AND DRILLED NEW INTERCOSTAL T
- [SDR SWAA2024092024307](https://openairdocs.org/sdr/SWAA2024092024307), Aug 8, 2024: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL BS 380-400 RBL 39 WL 208.<[01] ALL STEPS COMPLETED REMOVED INTERCOSTAL BS 380-400 RBL 39 WL 208 PER SRM 51-40-02 COMPLETED MEASUREMENT TABLE
- [SDR SWAA2024091924301](https://openairdocs.org/sdr/SWAA2024091924301), Aug 8, 2024: ANGLE. CRACKED. CRACKED ANGLE BS 294.5 FWD SIDE OF FRAME RBL 54 WL 208.<[01] STUB FRAME OF THE FORWARD GALLEY DOOR SURROUND STRUCTURE AT STA 296.4 REPAIR IS ACCOMPLISHED ON CUS
- [SDR SWAA2024091924306](https://openairdocs.org/sdr/SWAA2024091924306), Aug 8, 2024: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL BS 380-400 RBL 8 WL 208.<[01] ALL STEPS COMPLETED REMOVE INTERCOSTAL BS 380-400 RBL 8 WL 208 PER SRM 51-40-02 COMPLETED MEASUREMENT TABLE. L
- [SDR SWAA2024091923881](https://openairdocs.org/sdr/SWAA2024091923881), Aug 8, 2024: STIFFENER. CRACKED. LEFT HORIZONTAL STAB RIB 3 STIFFENERS 2 & 3 ARE CRACKED IN THE LOWER RADIUS.<[01] REPAIRED LEFT HORIZONTAL STAB RIB 3 STIFFENERS 2 & 3 IAW SRM 55-10-09-2R-4.;[0
- [SDR SWAA2024091924049](https://openairdocs.org/sdr/SWAA2024091924049), Aug 8, 2024: SKIN. CRACKED. CRACK ON RH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 18' FROM FWD EDGE; .3' IN LENGTH (MARKED CORRECTION TO FAULT NAME. 26.5' FROM FWD EDGE<[01] RE
- [SDR SWAA2024091924052](https://openairdocs.org/sdr/SWAA2024091924052), Aug 8, 2024: SKIN. CRACKED. CRACK ON LH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 18' FROM FWD EDGE; .65' IN LENGTH (MARKED)<[01] REPAIR AS PER SRM 55-10-01-2R-11.;[02] VERIFIE
- [SDR SWAA2024091923837](https://openairdocs.org/sdr/SWAA2024091923837), Aug 7, 2024: BEARING. OUT OF LIMITS. DURING ACCOMPLISHMENT OF CUSTOMER CARD 5510-I-16685-NG (INSP-STABILIZERS-HORIZONTAL STABILIZER SPHERICAL BEARING) FOUND DIMENSION H TO BE .0825 AND OUT OF LIMIT
- [SDR SWAA2024091923855](https://openairdocs.org/sdr/SWAA2024091923855), Aug 7, 2024: SUPPORT. CRACKED. UPPER BULB SEAL RETAINER SUPPORT IS CRACKED AT LOWER FASTENER HOLE AT RIGHT WING FIXED TE PANEL JUST AFT OF THE PYLON. MARKED<[01] REMOVED AND REPLACED UPPER BU
- [SDR SWAA2024091923365](https://openairdocs.org/sdr/SWAA2024091923365), Aug 6, 2024: VAPOR BARRIER. CRACKED. R/H BS 663 VAPOR BARRIER IS CRACKED AT MID SPAN<[01] 04 - REPAIRED PER [SRM 51-70-04-2R-10-A00755 (REPAIR 10 - REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH IN S
- [SDR SWAA2024091923366](https://openairdocs.org/sdr/SWAA2024091923366), Aug 6, 2024: VAPOR BARRIER. CRACKED. L/H BS 663 VAPOR BARRIER IS CRACKED AT MID SPAN<[01] 04 - REPAIRED PER [SRM 51-70-04-2R-10-A00755 (REPAIR 10 - REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH IN S
- [SDR SWAA2024092322980](https://openairdocs.org/sdr/SWAA2024092322980), Aug 5, 2024: SUPPORT. CRACKED. LH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL TRANSVERSE SUPPORT O/B RIVET HAS CRACK.<[01] REMOVED AND REPLACED LT WING DEFLECTION CONTROL RIB FIXED UPP
- [SDR SWAA2024092322984](https://openairdocs.org/sdr/SWAA2024092322984), Aug 5, 2024: SUPPORT FITTING. CRACKED. LH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL MID SUPPORT BEAM ORRS 261+8 AFT END HAS CRACK.<[01] REMOVED AND REPLACED LT WING DEFLECTION CONTROL RIB FI
- [SDR SWAA2024092322981](https://openairdocs.org/sdr/SWAA2024092322981), Aug 5, 2024: BEAM. CRACKED. RH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL MID SUPPORT BEAM ORRS 261+8 AFT END HAS CRACK<[01] REMOVED AND REPLACED RH WING TE: DEFLECTION CONTROL RIB
- [SDR SWAA2024092322986](https://openairdocs.org/sdr/SWAA2024092322986), Aug 5, 2024: BRACKET. CRACKED. RH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL TRANSVERSE SUPPORT O/B BRACKET FWD FACE HAS CRACK.<[01] REMOVED AND REPLACED RH WING TE: DEFLECTION CONTRO
- [SDR SWAA2023092501958](https://openairdocs.org/sdr/SWAA2023092501958), Sep 19, 2023: ESCAPE ROPE. OUT OF POSITION. RIGHT OVERWING EXIT ESCAPE ROPE IS NOT STOWED PROPERLY.<[01] RESECURED RIGHT OVERWING EXIT ESCAPE ROPE PER SIP
- [SDR SWAA2023091801555](https://openairdocs.org/sdr/SWAA2023091801555), Sep 16, 2023: LIGHT. INOPERATIVE. AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] RELAMPED PER AMM 33-51-04 OPS CHK GOOD
- [SDR SWAA2023091398812](https://openairdocs.org/sdr/SWAA2023091398812), Sep 11, 2023: LIGHT. INOPERATIVE. EXTERIOR EMERGENCY LIGHT AFT OF THE REAR ENTRY DOOR INOP<[01] INSTALLED NEW LAMP FOR EXTERIOR EMERGENCY LIGHT AFT OF REAR ENTRY DOOR IAW AMM 33-51-04
- [SDR SWAA2023022105186](https://openairdocs.org/sdr/SWAA2023022105186), Feb 20, 2023: HANDLE. BROKEN. FORWARD ENTRY DOOR ASSIST HANDLE BROKEN. FWD LAV ASSIST HANDLE MISSING.<[01] SWAPPED FWD ENTRY HANDLE WITH FWD LAV IAW AMM 52-11-31. INSTALLED FWD LAV ASSIST HA
- [SDR SWAA2023012594013](https://openairdocs.org/sdr/SWAA2023012594013), Jan 22, 2023: LENS. MISSING. EMERGENCY EXIT SIGN AT RIGHT OVER WING EXIT DOOR MISSING LENS. INSTALLED NEW LENS AS PER M/M SIP.
- [SDR SWAA2022121481219](https://openairdocs.org/sdr/SWAA2022121481219), Dec 13, 2022: BULB. INOPERATIVE. FORWARD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT AFT BULB IS INOP<[01] REPLACED INOP LAMP IN FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT AND PERFORMED GOOD TES
- [SDR SWAA2022121478970](https://openairdocs.org/sdr/SWAA2022121478970), Dec 6, 2022: WINDOW FRAME. CRACKED. CAPTAIN'S #3 WINDOW FRAME HAS A CRACK EMINATING FROM THE LWR FASTENER HOLE ON THE FWD VERTICAL FASTENER ROW.<[01] REQUEST NDI VERIFICATION OF CRACK;[27] REPAIRE

All 303: https://openairdocs.org/aircraft/N267WN/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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