# N292WN: 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: 32538
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 14, 2007
- Certificate issued: October 3, 2007
- Expires: August 31, 2028
- Mode S code: A2FEE9
- 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=292WN
- Page: https://openairdocs.org/aircraft/N292WN

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 N292WN.

## FAA accident and incident reports

None matched to N292WN.

## Service difficulty reports (299, 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 SWAA2026102200930](https://openairdocs.org/sdr/SWAA2026102200930), Oct 18, 2026: FLASHLIGHT. INOPERATIVE. CABIN EMERGENCY FLASHLIGHT WILL NOT TEST/INOP. R&R AFTER F/A FLASHLIGHT INBOARD SIDE PER AMM 25-64-00. TYPO CORRECTION R&R AFT F/A FLASHLIGHT INBOARD SIDE PER A
- [SDR SWAA2026101995103](https://openairdocs.org/sdr/SWAA2026101995103), Oct 15, 2026: LENS. DETACHED. EMERGENCY LIGHT LENS ON FO SIDE FELL OFF. REMOVED AND REPLACED THE EMERGENCY EXIT LENS IAW AMM 33-51-01. OPS CHKD GOOD.
- [SDR SWAA2026061511712](https://openairdocs.org/sdr/SWAA2026061511712), Jun 12, 2026: LAMP. INOPERATIVE. AFT GALLEY OVERHEAD EMERG EXIT SIGN F/O SIDE 4 LOWER LIGHTS INOPERATIVE. RELAMPED IAW AMM 33-51-01 OPS CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR SWAA2025110731905](https://openairdocs.org/sdr/SWAA2025110731905), Nov 4, 2025: NUT. LOOSE. SEATS @ ROW 12 FO SIDE WILL NOT STAY UPRIGHT. TIGHTENED JAM NUTS ON HYDROLOCKS PER CMM 25-21-42
- [SDR SWAA2025110531188](https://openairdocs.org/sdr/SWAA2025110531188), Nov 2, 2025: SIGN. DETACHED. OVERWING EMER EXIT SIGN DETATCHED. RESECURED LENS PER S.I.P
- [SDR SWAA2025071583646](https://openairdocs.org/sdr/SWAA2025071583646), Jun 19, 2025: FLOOR SUPPORT. CRACKED. AAI REPORT MAIN CABIN - FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540 BTW BL 0 TO RBL 24.75 . REPLACED FLOOR STRUCTURE SUPPORT LOCATED AT 540 BETWEEN BLO TO RBL 
- [SDR SWAA2025071583647](https://openairdocs.org/sdr/SWAA2025071583647), Jun 19, 2025: FLOORBEAM. CRACKED. AAI REPORT MAIN CABIN - FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540 BTW BL 0 TO LBL 24.75. REPLACED FLOOR STRUCTURE SUPPORT LOCATED AT 540 BETWEEN BLO TO LBL 2
- [SDR SWAA2025071583643](https://openairdocs.org/sdr/SWAA2025071583643), Jun 19, 2025: GROMMET. MISSING. AAI REPORT MAIN CABIN - FLOOR BEAM WEB HOLES FLIGHT CONTROL CABLES MLGEA AND EA PASS THROUGH PROTECTOR GROMMETS ARE MISSING STA 312 AT REPLACED INTERCOSTAL AREA
- [SDR SWAA2025071582057](https://openairdocs.org/sdr/SWAA2025071582057), Jun 15, 2025: ANGLE. ELONGATED. ELONGATED HOLE ANGLE - CLIP BS 500A AFT FACE BTW S-25L AND S-26L FWD CARGO COMPARTMENT. REPLACED ANGLE - CLIP BS 500A AFT FACE BTW S-25L AND S-26L FWD CARGO COM
- [SDR SWAA2025071581631](https://openairdocs.org/sdr/SWAA2025071581631), Jun 13, 2025: SUPPORT. CORRODED. CORROSION SUPPORT ZEE BTW BS727 AND BS 727E PLUS 10 INCHES;LBL 21 AND WL 156.4 AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE AND FASTENERS LOC. BS727 TO BS847 LBL
- [SDR SWAA2025071581457](https://openairdocs.org/sdr/SWAA2025071581457), Jun 13, 2025: TIE CLIP. CORRODED. CORROSION TIE CLIP AT LEVEL BS 727D AND STRINGER 26R AFT CARGO COMPARTMENT. REPLACED TIE CLIP AND FASTENERS AT LEVEL BS 727D AND STRINGER 26R AFT CARGO COMPARTM
- [SDR SWAA2025071581634](https://openairdocs.org/sdr/SWAA2025071581634), Jun 13, 2025: TIE CLIP. CORRODED. CORROSION TIE CLIP FRAME ON BS 747 STRINGER 26R AT AFT CARGO COMPARTMENT REPLACED TIE CLIP FRAME AND FASTENERS ON BS 747 STRINGER 26R AT AFT CARGO COMPARTMENT I
- [SDR SWAA2025071581633](https://openairdocs.org/sdr/SWAA2025071581633), Jun 13, 2025: SUPPORT. CORRODED. CORROSION SUPPORT ZEE BTW BS 727E PLUS 10 INCHES TO BS 807; LBL21 AND WL156.4 AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE BTW BS 727E PLUS 10 INCHES TO BS 847; 
- [SDR SWAA2025071580985](https://openairdocs.org/sdr/SWAA2025071580985), Jun 12, 2025: BRACKET. CRACKED. CRACK BRACKET AT LEVEL BS 400 AND STR 26L AT FWD CARGO COMPARTMEN. REPLACED BRACKET AND FASTENERS LOCATED LEVEL BS 400 AND STR 26L AT FWD CARGO COMPARTMENT IAW 
- [SDR SWAA2025071581284](https://openairdocs.org/sdr/SWAA2025071581284), Jun 12, 2025: INTERCOSTAL. CRACKED. CRACK INTERCOSTAL - WEB LOCATED BTW STA 294.5 TO STA 303.9 STR 16L PASSENGER CABIN. REPAIRED INTERCOSTAL BETWEEN BSTA 294.5 & BSTA 303.9 AND AT S-16L FWD ENTRY 
- [SDR SWAA2025071580978](https://openairdocs.org/sdr/SWAA2025071580978), Jun 12, 2025: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BETWEEN BS500A TO BS500D STR26R WL152.7 AT FWD CARGO COMPARTMENT. REPLACED SUPPORT ZEE AND FASTENERS LOCATED BETWEEN BS500A TO BS5
- [SDR SWAA2025071580981](https://openairdocs.org/sdr/SWAA2025071580981), Jun 12, 2025: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BETWEEN BS400 TO BS480 STR26L WL152.7 AT FWD CARGO COMPARTMENT. REPLACED SUPPORT ZEE LOCATED BETWEEN BS400 TO BS500D STR26L WL152.
- [SDR SWAA2025071581269](https://openairdocs.org/sdr/SWAA2025071581269), Jun 12, 2025: INTERCOSTAL. CORRODED. CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS493 TO BS 500A STR26R WL152.7 FWD CARGO COMPARTMENT. REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BETWEEN BS49
- [SDR SWAA2025071581277](https://openairdocs.org/sdr/SWAA2025071581277), Jun 12, 2025: SUPPORT ANGLE. CRACKED. CRACK ANGLE - SUPPORT LOCATED BETWEEN BS918 AND STR25R TO STR27R AFT CARGO COMPARTMENT. REPLACED ANGLE - SUPPORT (STIFFENER) LOCATED BETWEEN BS918 AND STR25R TO
- [SDR SWAA2025071581278](https://openairdocs.org/sdr/SWAA2025071581278), Jun 12, 2025: SUPPORT. CORRODED. CORROSION SUPPORT ZEE BTW BS 727 TO BS 767 AT LEVEL OF STR 25R; RBL21 AND WL156.4 AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 AT LE
- [SDR SWAA2025071581279](https://openairdocs.org/sdr/SWAA2025071581279), Jun 12, 2025: SUPPORT ANGLE. CRACKED. CRACK ANGLE - SUPPORT LOCATED BETWEEN BS914 AND STR25R TO STR27R AFT CARGO COMPARTMENT. REPLACED ANGLE - SUPPORT(STIFFENER ) AND FASTENERS LOCATED BETWEEN BS914
- [SDR SWAA2025071580980](https://openairdocs.org/sdr/SWAA2025071580980), Jun 12, 2025: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BETWEEN BS480 TO BS500D STR26L WL152.7 AT FWD CARGO COMPARTMENT. REPLACED SUPPORT ZEE LOCATED BETWEEN BS400 TO BS500D STR26L WL152
- [SDR SWAA2025071581283](https://openairdocs.org/sdr/SWAA2025071581283), Jun 12, 2025: SHIELD. CORRODED. CORROSION SHIELD FLOOR STRUCTURE BTW BS 767 TO BS 794.5 ;WL 156.4 RBL 21 AT AFT CARGO COMPARTMENT. REPLACED SHIELD FLOOR STRUCTURE LOCATED BTW BSTA 767 TO BSTA 
- [SDR SWAA2025071581272](https://openairdocs.org/sdr/SWAA2025071581272), Jun 12, 2025: TIE CLIP. CRACKED. CRACK TIE CLIP LOCATED STA 277 AND STR 10R PASSENGER CABIN. REPLACED TIE CLIP AND FASTENERS ON STA277 AND STR10R IAW SRM 51-40-02 AND DRAWING 141A1110 SHEET 17 
- [SDR SWAA2025071580982](https://openairdocs.org/sdr/SWAA2025071580982), Jun 12, 2025: RIB. CRACKED. CRACK ON LEADING EDGE RIB ACCESS PANEL 341B LOCATED LE STA 95.96 AT RT HORIZONTAL STABILIZER. REPLACED RIB AND FASTENERS LOCATED LEADING EDGE ACCESS PANEL 341B 
- [SDR SWAA2025071580586](https://openairdocs.org/sdr/SWAA2025071580586), Jun 11, 2025: WEB. CRACKED. CRACK WEB LOCATED BTW BS 277 TO BS 294.5 BL0 AT FWD GALLEY AREA. REPLACED WEB LOCATED BETWEEN BS 277 TO BS 294.5 BL0 AT FWD GALLEY AREA IAW BOEING 737-700 SRM 5
- [SDR SWAA2025071580589](https://openairdocs.org/sdr/SWAA2025071580589), Jun 11, 2025: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE AT LEVEL ORSS 270 APPROX RT WING. REPLACED ANGLE AND FASTENERS TRAILING EDGE AT LEVEL ORSS 270 APPROX RT WING IAW SRM 51-40-02 AND DRA
- [SDR SWAA2025071580590](https://openairdocs.org/sdr/SWAA2025071580590), Jun 11, 2025: PLATE. CRACKED. CRACK SUPPORT CORRUGATED PLATE TRAILING EDGE BTW ORSS297 AND ORSS 290 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE BTW ORSS297 AND ORSS 290 AT RT WING IA
- [SDR SWAA2025071580588](https://openairdocs.org/sdr/SWAA2025071580588), Jun 11, 2025: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE AT LEVEL ORSS 297 AT LT WING 2025-366177 <[01]. REPLACED CORRUGATED PLATE TRAILING EDGE AT LEVEL ORSS 297 AT LT WING IAW B7
- [SDR SWAA2025071580438](https://openairdocs.org/sdr/SWAA2025071580438), Jun 10, 2025: NUT PLATE. CRACKED. CRACK RAIL NUTPLATE LEADING EDGE INTERNAL CAVITY FRONT SPAR LOCATED BETWEEN OFSS 565 TO OFSS 580 AT LT WING. REPLACED RAIL NUTPLATE LEADING EDGE INTERNAL CAVITY
- [SDR SWAA2025071180437](https://openairdocs.org/sdr/SWAA2025071180437), Jun 10, 2025: SPAR. CRACKED. CRACK ANGLE REAR SPAR LOCATED ON IRSS 139 AT LT WING. REPLACED ANGLE REAR SPAR LOCATED ON IRSS 139 AT LT WING IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 1
- [SDR SWAA2025071180436](https://openairdocs.org/sdr/SWAA2025071180436), Jun 10, 2025: SPAR. CRACKED. CRACK REAR SPAR ANGLE LOCATED ON IRSS 139 AT RT WING. REPLACED REAR SPAR ANGLE LOCATED ON IRSS 139 AT RT WING IAW B737-700 SRM 51-10-02-0G ITEM 9; SRM 51-40-02-
- [SDR SWAA2025071579848](https://openairdocs.org/sdr/SWAA2025071579848), Jun 9, 2025: ACCESS PANEL. CRACKED. CRACK BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB. REPLACED BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB IAW SRM 51-10-02-0G-0 PARAGRAPH 9 AND SRM 51-40-02
- [SDR SWAA2025071579386](https://openairdocs.org/sdr/SWAA2025071579386), Jun 8, 2025: STUB FRAME. CRACKED. CRACK INDICATIONS(2EA) ON STUB FRAME LOCATED BETWEEN BS 294.5 TO BS 296.5 BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTHS 0.437 IN. AND 0.625 IN. APROX.A
- [SDR SWAA2025071579393](https://openairdocs.org/sdr/SWAA2025071579393), Jun 8, 2025: GUSSET. CRACKED. CRACK GUSSET LOCATED STA 500D AND STR 21L FWD CARGO COMPARTMENT. REPLACED GUSSET AND FASTENER LOCATED STA 500D AND STRINGER 21L FWD CARGO COMPARTMENT IAW BOEING
- [SDR SWAA2025071579389](https://openairdocs.org/sdr/SWAA2025071579389), Jun 8, 2025: GUSSET. CRACKED. CRACK GUSSET LOCATED STA 500D AND STR 19L FWD CARGO COMPARTMENT. REPLACED GUSSET AND FASTENER LOCATED STA 500D AND STRINGER 19L FWD CARGO COMPARTMENT IAW BOEING
- [SDR SWAA2025071579390](https://openairdocs.org/sdr/SWAA2025071579390), Jun 8, 2025: GUSSET. CRACKED. CRACK GUSSET LOCATED STA 500D AND STR 19R FWD CARGO COMPARTMENT. REPLACED GUSSET AND FASTENERS LOCATED STA 500D AND STR 19R FWD CARGO COMPARTMENT IAW B737-700 S
- [SDR SWAA2025071579387](https://openairdocs.org/sdr/SWAA2025071579387), Jun 8, 2025: SUPPORT ANGLE. CRACKED. CRACK INBOARD SUPPORT ANGLE OF OUTBOARD AUXILIARY TRACK SLAT 8 AT RT WING. REPLACED SUPPORT BRACKET AND FASTENERS LOCATED ON OUTBOARD AUXILIARY TRACK SLAT 8 AT 
- [SDR SWAA2025071579663](https://openairdocs.org/sdr/SWAA2025071579663), Jun 8, 2025: WEB. CRACKED. CRACK WEB BTW STA 847 TO STA 867 AND BTW AT LEVEL LBL 24.75 AT AFT CARGO COMPARTMENT. REPLACED WEB LOCATED BTW BS 847 TO BS 867 AT LEVEL LBL 24.75 AT AFT CARGO 
- [SDR SWAA2025071579392](https://openairdocs.org/sdr/SWAA2025071579392), Jun 8, 2025: ANGLE. CRACKED. CRACK INBOARD SUPPORT ANGLE OF INBOARD AUXILIARY TRACK SLAT 7 AT RT WING. REPLACED SUPPORT BRACKET AND FASTENERS LOCATED ON INBOARD AUXILIARY TRACK SLAT 7 AT RT
- [SDR SWAA2025071579394](https://openairdocs.org/sdr/SWAA2025071579394), Jun 8, 2025: SUPPORT ANGLE. CRACKED. CRACK INBOARD SUPPORT ANGLE OF INBOARD AUXILIARY TRACK SLAT 1 AT LT WING. REPLACED INBOARD SUPPORT ANGLE OF INBOARD AUXILIARY TRACK SLAT 1 AT LT WING IAW SRM 51
- [SDR SWAA2025071579382](https://openairdocs.org/sdr/SWAA2025071579382), Jun 7, 2025: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET BODY STATION 540 ON PNEUMATIC DUCT LBL 6 AT AIR CONDITIONING BAY. REPLACED SUPPORT BRACKET BODY STATION 540 ON PNEUMATIC DUCT LBL 6 AT AIR
- [SDR SWAA2025071579383](https://openairdocs.org/sdr/SWAA2025071579383), Jun 7, 2025: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE ON BODY FAIRING STRUCTURE BS 500D LEVEL STRINGER 19L AT LOWER FUSELAGE. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED AT WING TO BODY FAIRING
- [SDR SWAA2025071579385](https://openairdocs.org/sdr/SWAA2025071579385), Jun 7, 2025: PANEL. ELONGATED. ELONGATED HOLES ON ACCESS PANEL 561AB AT LT WING 2025-366021<[01]. TOOL USED CALIPER PN: 500-197-30; SN: B20189334; DUE DATE: 26/JAN/26.; [02] TOOL USED HOT BON
- [SDR SWAA2025071578894](https://openairdocs.org/sdr/SWAA2025071578894), Jun 6, 2025: HANDLE. DETERIORATED. DETERIORATED ASSIST HANDLE NUT ON FWD ENTRY DOORWAY LINING AT FWD GALLEY AREA (2EA). REPLACED ASSIST HANDLE NUT ON FWD ENTRY DOORWAY LINING AT FWD GALLEY AREA I
- [SDR SWAA2025071578893](https://openairdocs.org/sdr/SWAA2025071578893), Jun 6, 2025: HANDLE. DETERIORATED. DETERIORATED ASSIST HANDLE NUT ON FORWARD ENTRY DOOR LINING AT FORWARD GALLEY AREA (4EA). REPLACED ASSIST HANDLE NUT ON FORWARD ENTRY DOOR LINING AT FORWARD GAL
- [SDR SWAA2025071578890](https://openairdocs.org/sdr/SWAA2025071578890), Jun 6, 2025: HANDLE. DETERIORATED. DETERIORATED ASSIST HANDLE NUT ON AFT ENTRY DOORWAY LINING AT AFT GALLEY AREA (2EA). REPLACED ASSIST HANDLE NUT ON AFT ENTRY DOORWAY LINING AT AFT GALLEY AREA (
- [SDR SWAA2025071578889](https://openairdocs.org/sdr/SWAA2025071578889), Jun 6, 2025: HANDLE. DETERIORATED. DETERIORATED ASSIST HANDLE NUT ON AFT ENTRY DOOR LINING AT AFT GALLEY AREA (2EA) 2025-365933<[01] REPLACED ASSIST HANDLE NUT ON AFT ENTRY DOOR LINING AT AFT GAL
- [SDR SWAA2025071578891](https://openairdocs.org/sdr/SWAA2025071578891), Jun 6, 2025: HANDLE. DETERIORATED. DETERIORATED ASSIST HANDLE NUT ON AFT SERVICE DOORWAY LINING AT AFT GALLEY AREA (2EA). REPLACED ASSIST HANDLE NUT ON AFT SERVICE DOORWAY LINING AT AFT GALLEY AR
- [SDR SWAA2025071578888](https://openairdocs.org/sdr/SWAA2025071578888), Jun 6, 2025: HANDLE. DETERIORATED. DETERIORATED ASSIST HANDLE NUT ON AFT SERVICE DOOR LINING AT AFT GALLEY AREA (2EA). REPLACED ASSIST HANDLE NUT ON AFT SERVICE DOOR LINING AT AFT GALLEY AREA (2E

All 299: https://openairdocs.org/aircraft/N292WN/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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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
