# N268WN: 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: 32524
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 5, 2007
- Certificate issued: April 9, 2007
- Expires: March 31, 2030
- Mode S code: A29EB6
- 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=268WN
- Page: https://openairdocs.org/aircraft/N268WN

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 N268WN.

## FAA accident and incident reports

None matched to N268WN.

## Service difficulty reports (262, 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 SWAA2026092274966](https://openairdocs.org/sdr/SWAA2026092274966), Sep 18, 2026: COVER. MISSING. AISLE OVERHEAD EXIT SIGN MISSING FORWARD FACING COVER. REPLACED AISLE FRONT FACING OVERHEAD EXIT SIGN COVER REF AMM 33-51-01-960-802. OPS CHECKS NORMAL.
- [SDR SWAA2026090870845](https://openairdocs.org/sdr/SWAA2026090870845), Sep 3, 2026: COVER. MISSING. EMERGENCY LIGHT ROW 14 & 15 A,B & C, COVER MISSING. INSTALLED MISSING COVER IAW AMM 33-51-03.
- [SDR SWAA2026081423387](https://openairdocs.org/sdr/SWAA2026081423387), Aug 10, 2026: LENS. DETACHED. EMERGENCY EXIT SIGN OVERHEAD IN CABIN FELL DOWN REINSTALLED LENS COVER REF AMM 33-51-00.
- [SDR SWAA2026080575007](https://openairdocs.org/sdr/SWAA2026080575007), Aug 1, 2026: FLOOR PANEL. CRACKED. FWD CARGO FLOOR PANEL CRACKED (6 , 5.5 2 SPOT) BS 500. PERFORMED A PATCH REPAIR IAW AMM 25-52-01. NO OTHER LINER AND PANEL DAMAGE NOTED.
- [SDR SWAA2026060208207](https://openairdocs.org/sdr/SWAA2026060208207), May 31, 2026: FLOOR PANEL. SPLIT. RAMP REPORTS AFT CARGO PIT FIBERGLASS FLOOR SPLIT. SPLIT IS IN FIBERGLASS FLOOR FROM STATION 751-768. OK TO CONT PER MEL 25-16-01. REMOVED AND REPLACED AFT CARG
- [SDR SWAA2026022372823](https://openairdocs.org/sdr/SWAA2026022372823), Feb 21, 2026: COVER. LOOSE. EMERGENCY EXIT LIGHT COVER ON F/O SIDE OVERWING EXIT FELL OFF DURING FLIGHT. SECURED EMERGENCY EXIT LIGHT COVER IAW AMM 33-51-01.
- [SDR SWAA2025082909134](https://openairdocs.org/sdr/SWAA2025082909134), Aug 28, 2025: LIGHT. LOOSE. RH PHOTO LUMINESCENT STRIP LOOSE AT FWD GALLEY MAT. SECURED RT PHOTOLUMINESCENT STRIP AT FWD GALLEY BALL MAT IN REF TO AMM 33-51-15.
- [SDR SWAA2025080697913](https://openairdocs.org/sdr/SWAA2025080697913), Aug 3, 2025: BATTERY PACK. INOPERATIVE. FOUND FRONT LEFT EMERGENCY LIGHTS OUT. R & R FWD LT BATTERY PACK PER AMM 33-51-06 OPS GOOD.
- [SDR SWAA2025070186477](https://openairdocs.org/sdr/SWAA2025070186477), Jun 28, 2025: FAIRING. DAMAGED. STRUT 4 FAIRING HAS AN ENLARGED MOUNT HOLE ON TOP AFT SIDE<[01] C/W 25-172-01732
- [SDR SWAA2024103054003](https://openairdocs.org/sdr/SWAA2024103054003), Oct 27, 2024: CONNECTOR. DAMAGED. INOP EMERGENCY EXIT LIGHT ON CEILING PANEL AT FWD GALLEY AREA 2024-593383<[01] CONNECTED CORRECTLY ELECTRICAL CONNECTOR D3160 OF THE EMERGENCY LIGHT ON CEILING 
- [SDR SWAA2024103045313](https://openairdocs.org/sdr/SWAA2024103045313), Oct 5, 2024: WEB. CRACKED. CRACK ON LOWER SILL WEB LOCATED BS 294.5 AT LEVEL STR 17R FWD GALLEY AREA 2024-593316<[01] REPLACED LOWER SILL WEB (1EA) LOCATED BTW BS 291.5 TO BS 332.1 AT LEV
- [SDR SWAA2024103042819](https://openairdocs.org/sdr/SWAA2024103042819), Sep 28, 2024: SUPPORT ANGLE. CRACKED. CRACK BODY FAIRING SUPPORT T ANGLE LOCATED BS500D; BETWEEN STRINGER 18R AND STRINGER 19R AT LOWER FUSELAGE 2024-593247<[01] REPLACED SUPPORT T ANGLE LOCATED AT 
- [SDR SWAA2024103042817](https://openairdocs.org/sdr/SWAA2024103042817), Sep 27, 2024: SUPPORT BRACKET. CRACKED. CRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO 3R AT PASSENGER CABIN 2024-593237<[01] REPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO 3R AT PASSENG
- [SDR SWAA2024103041983](https://openairdocs.org/sdr/SWAA2024103041983), Sep 26, 2024: LENS. BROKEN. BROKEN LENS EMERGENCY EXIT ON LAVATORY A AT FWD GALLEY AREA 2024-593195<[01] REPLACED LENS EMERGENCY EXIT ON LAVATORY A AT FWD GALLEY AREA IAW B737-700 AMM 33-5
- [SDR SWAA2024103041726](https://openairdocs.org/sdr/SWAA2024103041726), Sep 25, 2024: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE LOCATED ORSS 269 AT LT WING 2024-593185<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 269 AT LT WING IAW B737-700 SRM 51-10-02 PARAGR
- [SDR SWAA2024103041725](https://openairdocs.org/sdr/SWAA2024103041725), Sep 25, 2024: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE LOCATED ORSS 269 AT RT WING 2024-593183<[01] REPLACED ANGLE AND FASTENERS TRAILING EDGE LOCATED ORSS 269 AT RT WING IAW B737-700 SRM 5
- [SDR SWAA2024103041527](https://openairdocs.org/sdr/SWAA2024103041527), Sep 25, 2024: SKIN. CRACKED. CRACK INDICATION FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.90 RIB AND 8 INCH. FROM REAR SPAR. INBOARD SIDE OF RIB. CRACK LENGT
- [SDR SWAA2024103041229](https://openairdocs.org/sdr/SWAA2024103041229), Sep 24, 2024: WEB. CRACKED. CRACK ON WEB LOCATED BTW BS 277 TO BS 294.5 RBL 1 AT FWD GALLEY AREA 2024-593135<[01] REPLACED WEB LOCATED BTW BS 277 TO BS 294.5 RBL 1 AT FWD GALLEY AREA IAW B
- [SDR SWAA2024103041519](https://openairdocs.org/sdr/SWAA2024103041519), Sep 24, 2024: ANGLE. CRACKED. CRACK ANGLE AFT POSITION LOCATED BTW STA 907 TO STA 927 AND BTW STR 25R TO STR 27R AT AFT CARGO COMPARTMENT 2024-593151<[01] REPLACED ANGLE LOCATED AFT POSITION
- [SDR SWAA2024103041230](https://openairdocs.org/sdr/SWAA2024103041230), Sep 24, 2024: WEB. CRACKED. CRACK ON WEB LOCATED BTW BS 328 TO BS 344 LBL 46.5 AT FWD GALLEY AREA 2024-593132<[01] REPLACED WEB LOCATED BTW BS 328 TO BS 344 LBL 46.5 AT FWD GALLEY AREA IAW
- [SDR SWAA2024103041226](https://openairdocs.org/sdr/SWAA2024103041226), Sep 24, 2024: PLATE. CORRODED. CORROSION ON PLATE LOCATED BS 1006 PLUS 23 INCHES RBL 3 WL 208.1 AT AFT GALLEY AREA 2024-593121<[01] TOOL USED CALIPER P/N: 500-752-20; S/N:B12037208; DUE DATE:
- [SDR SWAA2024103041512](https://openairdocs.org/sdr/SWAA2024103041512), Sep 24, 2024: FITTING. CORRODED. CORROSION INNER CHORD LOCATED BTW BS 303.9 TO BS 328 LBL 54 WL 208.1 AT FWD GALLEY AREA 2024-593138<[01] TOOL USED ULTRASONIC EQUIPMENT PN: 45MG SN 130061901; D
- [SDR SWAA2024103041520](https://openairdocs.org/sdr/SWAA2024103041520), Sep 24, 2024: FRAME. CRACKED. CRACK ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA 2024-593152<[01] TRIM OUT BS 312 FRAME UPPER CHORD AT LBL 33 BETWEEN S-5L AND S-6L IAW EA#
- [SDR SWAA2024103041522](https://openairdocs.org/sdr/SWAA2024103041522), Sep 24, 2024: ANGLE. CRACKED. CRACK ON ANGLE LOCATED FWD FACE BS 294.5 AT LEVEL STR 13L AT FWD GALLEY 2024-593153<[01] REPLACED ANGLE LOCATED ON FWD FACE BS 294.5 AT LEVEL STR 13L AT FWD GAL
- [SDR SWAA2024103041513](https://openairdocs.org/sdr/SWAA2024103041513), Sep 24, 2024: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13 AT PASSENGER CABIN 2024-593140<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400
- [SDR SWAA2024103041515](https://openairdocs.org/sdr/SWAA2024103041515), Sep 24, 2024: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 10 AT PASSENGER CABIN 2024-593142<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400
- [SDR SWAA2024103041516](https://openairdocs.org/sdr/SWAA2024103041516), Sep 24, 2024: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 41 AT PASSENGER CABIN 2024-593144<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400
- [SDR SWAA2024103041517](https://openairdocs.org/sdr/SWAA2024103041517), Sep 24, 2024: PLATE. CORRODED. CORROSION ON PLATE LOCATED BS 312 LBL 54 WL 208.1 AT FWD GALLEY AREA 2024-593146<[01] REPLACED PLATE LOCATED BS312 LBL54 WL 208.1 AT FWD GALLEY AREA IAW B737-70
- [SDR SWAA2024103041526](https://openairdocs.org/sdr/SWAA2024103041526), Sep 24, 2024: SKIN. CRACKED. CRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.90 RIB AND 8 INCH. FROM REAR SPAR. INBOARD SIDE OF RIB. CRACK LENGT
- [SDR SWAA2024103041514](https://openairdocs.org/sdr/SWAA2024103041514), Sep 24, 2024: SUPPORT. CRACKED. CRACK SUPPORT ZEE LOCATED BTW STA 727D TO STA 727E AT LEVEL STR 25R AT AFT CARGO COMPARTMENT 2024-593141<[01] REPLACED SUPPORT ZEE SECTION;AND FASTENERS LOCATED
- [SDR SWAA2024103041511](https://openairdocs.org/sdr/SWAA2024103041511), Sep 24, 2024: STUB FRAME. CRACKED. CRACK ON STUB FRAME LOCATED 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2024-593136<[01] STEPS 6 AND 7 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 210
- [SDR SWAA2024103041521](https://openairdocs.org/sdr/SWAA2024103041521), Sep 24, 2024: STRINGER. CRACKED. CRACK ON STRINGER 16L LOCATED BTW BS 294.5 TO BS 303.9 AT FWD GALLEY AREA 2024-593150<[01] ON STEP 3; TOOL USED ULTRASONIC EQUIPMENT P/N: 45MG; S/N: 130064101; 
- [SDR SWAA2024103040716](https://openairdocs.org/sdr/SWAA2024103040716), Sep 23, 2024: WEB. CRACKED. CRACK SUPPORT WEB LOCATED BTW STA 847 TO STR 867 AT LEVEL LBL 24.82 CEILING AREA AT AFT CARGO COMPARTMENT 2024-593041<[01] REPLACED SUPPORT WEB AND FASTENERS LO
- [SDR SWAA2024103040953](https://openairdocs.org/sdr/SWAA2024103040953), Sep 23, 2024: CONNECTOR. BROKEN. BROKEN CONNECTOR OF THE OVERWING SCAPE LOCATED BTW STA 747 TO STA 767 AND BTW STR 21L TO STR 22L AT AFT CARGO COMPARTMENT 2024-593054<[01] REPLACED CONNECTOR OF
- [SDR SWAA2024103040962](https://openairdocs.org/sdr/SWAA2024103040962), Sep 23, 2024: WEB. CRACKED. CRACK ON INTERCOSTAL WEB LOCATED BTW BS 344 TO BS 360 BL 0 AT FWD GALLEY AREA 2024-593092<[01] REPLACED WEB LOCATED BTW BS 344 TO BS 360 BL 0 AT FWD GALLEY AREA
- [SDR SWAA2024103040721](https://openairdocs.org/sdr/SWAA2024103040721), Sep 23, 2024: ANGLE. CRACKED. CRACK ANGLE LOCATED STA 927 AT LEVEL STR 18R AT AFT CARGO COMPARTMENT 2024-593042<[01] REPAIRED ANGLE LOCATED BTW STA 900 TO STA 927 AT LEVEL STR 18R AT AFT CAR
- [SDR SWAA2024103040954](https://openairdocs.org/sdr/SWAA2024103040954), Sep 23, 2024: FLOORBEAM. CORRODED. CORROSION LOCATED ON FLOOR BEAM 986.5 RBL 42 WL 208.1 AT AFT GALLEY AREA 2024-593056<[01] PERFORMED PERMANENT REPAIR CAT A LOCATED ON FLOOR BEAM 986.5; LBL13 TO
- [SDR SWAA2024103040955](https://openairdocs.org/sdr/SWAA2024103040955), Sep 23, 2024: FLOORBEAM. CORRODED. CORROSION LOCATED ON FLOOR BEAM 986.5 LBL 42 WL 208.1 AT AFT GALLEY AREA 2024_593057<[01] ET TOOL USED PN: MIZ-21C; SN:769680; DUE DATE: 28-AUG-25;[02] TOOL USE
- [SDR SWAA2024103040189](https://openairdocs.org/sdr/SWAA2024103040189), Sep 22, 2024: SCUFF PLATE. CRACKED. CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2024-592934<[01] TOOL USED DIGITAL CALIPER P/N:500-196-30;S/N:B23272676;DUE DATE:17-MAR-25.;[02] TOOL USED
- [SDR SWAA2024103040179](https://openairdocs.org/sdr/SWAA2024103040179), Sep 21, 2024: STRIP. CRACKED. CRACK STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH SIDE CENTER SECTION (8 EA) 2024-592911<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH
- [SDR SWAA2024103040180](https://openairdocs.org/sdr/SWAA2024103040180), Sep 21, 2024: LIGHT. CRACKED. CRACK STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RH SIDE CENTER SECTION (8 EA) 2024-592912<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RH
- [SDR SWAA2024103040169](https://openairdocs.org/sdr/SWAA2024103040169), Sep 21, 2024: PANEL. DEBONDED. CUSTOMER REQUEST - DEBONDED IB MAIN FLAP TRAILING EDGE WEDGE PANEL AT RH WING LOWER SURFACE 2024-592880<[01] TOOL USED CALIPER PN: 500-196-30; SN: A193117217; D
- [SDR SWAA2024103039504](https://openairdocs.org/sdr/SWAA2024103039504), Sep 19, 2024: SKIN. CRACKED. CRACK SLAT 2 LOWER SKIN AROUND THE FASTENER THAT ATTACH THE ACTUATOR FITTING AT SLAT STATION 322.71 AT LT WING 2024-592769<[01] TOOL USED ON STEP 3: EDDY CURREN
- [SDR SWAA2024103039505](https://openairdocs.org/sdr/SWAA2024103039505), Sep 19, 2024: VAPOR BARRIER. CRACKED. CUSTOMER REQUEST CRACK VAPOR BARRIER LH SIDE BS663 AT MAIN WHEEL WELL COMPARTMENTS 2024-592759<[01] TOOL USED CALIPER P/N: 500-197-30; S/N: B20189443; DUE DATE:
- [SDR SWAA2024103039503](https://openairdocs.org/sdr/SWAA2024103039503), Sep 19, 2024: VAPOR BARRIER. CRACKED. CUSTOMER REQUEST CRACK VAPOR BARRIER RH SIDE BS663 AT MAIN WHEEL WELL COMPARTMENT 2024-592758<[01] TOOL USED CALIPER P/N: 500-197-30; S/N: A18229508; DUE DATE: 
- [SDR SWAA2024060397128](https://openairdocs.org/sdr/SWAA2024060397128), May 31, 2024: TIRE. BLOWN. #2 MLG TIRE BLEW ON TAXI IN<[01] REMOVED AND REPLACED #1 AND #2 MAIN TIRE AND WHEEL ASSY?S PER AMM 34-45-11
- [SDR SWAA2024060397804](https://openairdocs.org/sdr/SWAA2024060397804), May 31, 2024: TIRE. BLOWN. #2 MLG TIRE BLEW ON TAXI IN<[01] REMOVED AND REPLACED #1 AND #2 MAIN TIRE AND WHEEL ASSY?S PER AMM 34-45-11
- [SDR SWAA2024020247465](https://openairdocs.org/sdr/SWAA2024020247465), Feb 1, 2024: WIRE. BROKEN. LOWER LEFT EMERGENCY LIGHT ON FWD LAV INOP<[01] FOUND BROKEN WIRE ON FOR EMERGENCY LIGHT ASSY. REPAIRED WIRE IAW SWPM 20-30-12. OPS CHECK GOOD AT THIS TIME.
- [SDR SWAA2024013046004](https://openairdocs.org/sdr/SWAA2024013046004), Jan 28, 2024: COVER. DETACHED. OVER WING EXIT SIGN COVER KNOCKED OFF FWD SIDE<[01] RESECURED EMERGENCY EXIT SIGN COVER AS REQUIRED PER SIP
- [SDR SWAA2023110919384](https://openairdocs.org/sdr/SWAA2023110919384), Nov 8, 2023: BATTERY PACK. FAILED. EMX BATT PACK M01670 FAILS CAPACITANCE CHECK / [01] REMOVED AND REPLACED EMX BATT PACK M01670 PER AMM 33-51-06

All 262: https://openairdocs.org/aircraft/N268WN/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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