# N282WN: 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: 32534
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 14, 2007
- Certificate issued: August 13, 2007
- Expires: February 29, 2028
- Mode S code: A2D76A
- 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=282WN
- Page: https://openairdocs.org/aircraft/N282WN

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

None matched to N282WN.

## 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 20110524008449I](https://openairdocs.org/incident/20110524008449I), May 24, 2011: Boeing 737-7H4 (N282WN), Denver, CO, No damage. At cruise flight level 400- #1 engine vibration felt, loss of oil pressure. A slight odor was observed and the #1 engine was shut down.

## Service difficulty reports (297, 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 SWAA2025092316551](https://openairdocs.org/sdr/SWAA2025092316551), Sep 20, 2025: PRESSURE DECK. CRACKED. FLIGHT DECK AFT FLOOR WEB DENT WITH CRACKS AT STATION 255 AND LBL 3. REMOVED AND REPLACED WEB SECTION PER SRM 51-40-02 AND IAW EA M-21-153-00734 WHICH HAD BEEN 
- [SDR SWAA2025062785439](https://openairdocs.org/sdr/SWAA2025062785439), Jun 25, 2025: LAMP. INOPERATIVE. L/H OVER WING EMERGENCY EXIT SIGN AREA LIGHTS INOP<[01] REVAMPED L/H OVER WING EMERGENCY EXIT SIGN AREA LIGHTS & OPS CHECK GOOD REF AMM 33-51-01.
- [SDR SWAA2025051671198](https://openairdocs.org/sdr/SWAA2025051671198), May 14, 2025: GIRT BAR. OUT OF ADJUST. INSTALL CORRECTLY GIRT BAR ESCAPE SLIDE FLOOR BRACKET SERVICE DOOR AT FWD GALLEY AREA 2025-242657<[01] INSTALL CORRECTLY GIRT BAR ESCAPE SLIDE FLOOR BRACKET SER
- [SDR SWAA2025051956321](https://openairdocs.org/sdr/SWAA2025051956321), Apr 18, 2025: WEB. CRACKED. CRACK INDICATION IN HOLE ON LOWER SILL LOCATED BS 294.5 PLUS 1 INCH AT LEVEL STR 17R AT FWD GALLEY AREA. CRACK DIRECTION IS: 6 0 CLOCK VIEW LOOKING FWD. 2025-24
- [SDR SWAA2025051956307](https://openairdocs.org/sdr/SWAA2025051956307), Apr 13, 2025: ANGLE. CRACKED. CRACK ON INNER CHORD LOCATE BS 294.5 RBL 53 WL 208.1 AT FWD GALLEY AREA. REPLACED INNER CHORD LOC. BTW BS 259.50 TO BS 360 RBL 53 WL 208.1 AT FWD GALLEY AREA IA
- [SDR SWAA2025051956303](https://openairdocs.org/sdr/SWAA2025051956303), Apr 12, 2025: PLATE. CRACKED. CRACK ON CORRUGATED PLATE LOCATED AT LEVEL ORSS 465 TRAILING EDGE AT LT WING 2025-242575<[01] REPLACED CORRUGATED PLATE LOCATED AT LEVEL ORSS 465 TRAILING EDGE 
- [SDR SWAA2025051956298](https://openairdocs.org/sdr/SWAA2025051956298), Apr 12, 2025: PLATE. CRACKED. CRACK ON CORRUGATED PLATE LOCATED AT LEVEL IRSS 218 TRAILING EDGE AT LT WING 2025-242568<[01] REPLACED CORRUGATED PLATE LOCATED AT LEVEL IRSS 218 TRAILING EDGE 
- [SDR SWAA2025051956305](https://openairdocs.org/sdr/SWAA2025051956305), Apr 12, 2025: PLATE. CRACKED. CRACK ON CORRUGATED PLATE LOCATED AT LEVEL ORSS 297 TRAILING EDGE AT LT WING 2025-242574<[01] REPLACED CORRUGATED PLATE LOCATED AT LEVEL ORSS 297 TRAILING EDGE 
- [SDR SWAA2025051923757](https://openairdocs.org/sdr/SWAA2025051923757), Apr 11, 2025: ANGLE. CRACKED. CRACK ANGLE LOCATED TRAILING EDGE ON IRSS 140 RIGHT WING 2025-242538<[01] REPLACED ANGLE (CLIP) LOCATED TRAILING EDGE ON IRSS 140 RIGHT WING IAW B737-700 SRM 51
- [SDR SWAA2025051956289](https://openairdocs.org/sdr/SWAA2025051956289), Apr 11, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED ON TRAILING EDGE ORSS 271 RT WING 2025-242547<[01] REMOVED AND PERFORMED GVI; NO FOUND ADDITIONAL DAMAGES AND INSTALLED NEW SUPPO
- [SDR SWAA2025051923880](https://openairdocs.org/sdr/SWAA2025051923880), Apr 11, 2025: SUPPORT BRACKET. CRACKED. CRACK ON SUPPORT BRACKET LOC. ON TRAILING EDGE ORSS 271 RT WING. 2025-242544<[01] REPLACED SUPPORT BRACKET LOC. ON TRAILING EDGE ORSS 271 RT WING IAW-B737-700-S
- [SDR SWAA2025051956291](https://openairdocs.org/sdr/SWAA2025051956291), Apr 11, 2025: ANGLE. CRACKED. CRACK ON ANGLE LOCATED ON TRAILING ORSS 281 RT WING 2025-242548<[01] REPLACED ANGLE (CLIP) LOCATED ON TRAILING ORSS 281 RT WING IAW B737-700 SRM 51-10-02-0G-0 I
- [SDR SWAA2025051956297](https://openairdocs.org/sdr/SWAA2025051956297), Apr 11, 2025: ANGLE. CRACKED. CRACK ACCESS PANEL 551FB ON ANGLE AT LT WING 2025-242556<[01] REPLACED ANGLE ON ACCESS PANEL 551FB AT LT WING IAW B737-700 SRM 51-40-02-0G 51-10-02-0G-0 STEP 9 
- [SDR SWAA2025051956277](https://openairdocs.org/sdr/SWAA2025051956277), Apr 10, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED AT LEVEL ORSS 261 DEFLECTION CONTROL RIB AREA TRAILING EDGE AT LT WING 2025-242530<[01] REMOVED AND PERFORMED GVI; NO FOUND ADDIT
- [SDR SWAA2025051956272](https://openairdocs.org/sdr/SWAA2025051956272), Apr 9, 2025: ACCESS PANEL. CRACKED. CRACK ACCCESS PANEL 834DZ ENTRY DOOR AFT BRACKET AT AFT GALLEY AREA. REPLACED ACCCESS PANEL 834DZ ENTRY DOOR AFT BRACKET AT AFT GALLEY AREA;IAW B737-700 SRM 51-
- [SDR SWAA2025051956250](https://openairdocs.org/sdr/SWAA2025051956250), Apr 8, 2025: LENS. BROKEN. BROKEN LIGHT EXIT LENS ON SIDEWALL PANEL 232YJW AT PASSENGER CABIN 2025-242400<[01] REPLACED LIGHT EXIT LENS ON SIDEWALL PANEL 232YJW AT PASSENGER CABIN IAW B73
- [SDR SWAA2025051956252](https://openairdocs.org/sdr/SWAA2025051956252), Apr 8, 2025: ACCESS PANEL. CRACKED. CRACK ACCESS PANEL 333AT PLATE AT LT HORIZONTAL STABILIZER 2025-242408<[01] REPLACED ACCESS PANEL 333AT PLATE AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40
- [SDR SWAA2025051922884](https://openairdocs.org/sdr/SWAA2025051922884), Apr 8, 2025: RIB. CRACKED. CRACK ACCESS PANEL 331B LEADING EDGE RIB LOCATED LE STA 105.26 AT LT HORIZONTAL STABILIZER 2025-242429<[01] REPLACED RIB LOC. ON LEADING EDGE STA 105.26 AT LT H
- [SDR SWAA2025051956227](https://openairdocs.org/sdr/SWAA2025051956227), Apr 7, 2025: FLOORBEAM. CORRODED. CORROSION ON FLOOR BEAM LOCATED BS 986.5 RBL 43 WL 208.1 AT AFT GALLEY AREA 2025-242324<[01] STEP 8 TOOL USED: EDDY CURRENT FLAW DETECTOR. P/N: NORTEC 600D; S/N
- [SDR SWAA2025051956234](https://openairdocs.org/sdr/SWAA2025051956234), Apr 7, 2025: ACCESS PANEL. CRACKED. CRACK AROUND HOLES ACCESS PANEL 561BB TRAILING EDGE AT LT WING 2025-242338<[01] TOOL USED: SCALE PN: CR5200 SN: 8343110809 DUE DATE: 06-MAR-26.;[02] TOOL USED: 
- [SDR SWAA2025051956242](https://openairdocs.org/sdr/SWAA2025051956242), Apr 7, 2025: FLOOR SUPPORT. CRACKED. CRACK ON WEB - INTERCOSTAL LOCATED BTW BS927 TO BS947.5 AND RBL21 AFT CARGO COMPARTMENT 2025-242368<[01] REPLACED WEB - INTERCOSTAL LOCATED BTW BS927 TO BS947.5
- [SDR SWAA2025051956243](https://openairdocs.org/sdr/SWAA2025051956243), Apr 7, 2025: KEELBEAM. CRACKED. CRACK INTERNAL STRUCTURE KEEL BEAM LOCATED BTW BS727 TO BS727A AND STR27L AT AFT CARGO COMPARTMENT 2025-242372<[01] ON STEPS 4 AND 5; TOOL USED P/N: NORTEC 500D
- [SDR SWAA2025051956206](https://openairdocs.org/sdr/SWAA2025051956206), Apr 6, 2025: FLOORBEAM. CRACKED. CRACK ON FLOOR BEAM LOCATED BS 294.5 RBL 56 WL 208.1 AT FWD GALLEY AREA 2025-242295<[01] TOOL USED P/N: NORTEC 500D; S/N: N500X11290U021704; CAL DUE: 14-APR-25.
- [SDR SWAA2025051956204](https://openairdocs.org/sdr/SWAA2025051956204), Apr 6, 2025: FLOORBEAM. CRACKED. CRACK ON ANGLE LOCATED BS 540 AND RBL 6 AT CENTER WING BOX 2025-242293<[01] REPLACED ANGLE LOCATED BS 540 AND RBL 6 AT CENTER WING BOX IAW-B737-700-SRM-51-40-02
- [SDR SWAA2025051956208](https://openairdocs.org/sdr/SWAA2025051956208), Apr 6, 2025: INTERCOSTAL. CRACKED. CRACK ON INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 15L AT FWD GALLEY AREA 2025-242297<[01] REPLACED INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9
- [SDR SWAA2025051956201](https://openairdocs.org/sdr/SWAA2025051956201), Apr 6, 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 1.812 IN. AND 0.437 IN. APROX.A
- [SDR SWAA2025051956205](https://openairdocs.org/sdr/SWAA2025051956205), Apr 6, 2025: STUB FRAME. CRACKED. CRACK ON STUB FRAME LOCATED BS 294.5 AT LEVEL STR 17R WL 208.1 AT FWD GALLEY AREA PERFORMED REPAIR ON STUB FRAME LOC. BS 294.5 AT LEVEL STR 17R WL 208.1 AT FWD 
- [SDR SWAA2025051956207](https://openairdocs.org/sdr/SWAA2025051956207), Apr 6, 2025: INTERCOSTAL. CRACKED. CRACK ON INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA 2025-242296<[01] REPLACED INTERCOSTAL LOC. BTW BS 294.5 TO BS 303.9 AT
- [SDR SWAA2025051956202](https://openairdocs.org/sdr/SWAA2025051956202), Apr 6, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 10 WL 208.1 AT PASSENGER CABIN 2025-242298<[01] REPLACED NEW SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 
- [SDR SWAA2025051956203](https://openairdocs.org/sdr/SWAA2025051956203), Apr 6, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 41 WL 208.1 AT PASSENGER CABIN 2025-242299<[01] REPLACED SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 
- [SDR SWAA2025051956159](https://openairdocs.org/sdr/SWAA2025051956159), Apr 5, 2025: ANGLE. CRACKED. CRACK ANGLE LOCATED BS 500D BODY FAIRING BETWEEN S-18L TO S-20L AT LOWER FUSELAGE 2025-242251<[01] REPLACED NEW ANGLE LOCATED BS 500D BODY FAIRING BETWEEN S-18L
- [SDR SWAA2025051956156](https://openairdocs.org/sdr/SWAA2025051956156), Apr 5, 2025: SCUFF PLATE. CRACKED. CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT. REPAIRED THE AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 
- [SDR SWAA2025051956183](https://openairdocs.org/sdr/SWAA2025051956183), Apr 5, 2025: PRESSURE DECK. CRACKED. CRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB AT LBL 31 BETWEEN STA 663 TO STA 675 AT MAIN WHEEL WELL COMPARTMENT. CRACK LENGTH: 0.250 IN. APPROX. PERF
- [SDR SWAA2025051956151](https://openairdocs.org/sdr/SWAA2025051956151), Apr 4, 2025: VAPOR BARRIER. CRACKED. CRACK VAPOR BARRIER WEB LOCATED BS 663.75 RBL 25 AT MAIN WHELL WELL 2025-242190<[01] TOOL USED: CALIPER P/N: 500-197-30; S/N: A21147758; DUE DATE: 05 JAN 25.;[0
- [SDR SWAA2025052220787](https://openairdocs.org/sdr/SWAA2025052220787), Apr 2, 2025: VAPOR BARRIER. CRACKED. CRACK VAPOR BARRIER WEB LOCATED BS 663.75 RBL 25 AT MAIN WHELL WELL COMPARTMENT 2025-242107.
- [SDR SWAA2025051921217](https://openairdocs.org/sdr/SWAA2025051921217), Apr 2, 2025: ACCESS DOOR. CRACKED. CRACK ON ACCESS DOOR 732 ON LT MAIN LANDING GEAR 2025-242142<[01] ON STEP 6. TOOL USED: ET INSTRUMENT. P/N: NORTEC 600D. S/N: 210138503. DUE DATE: 05-AUG-25.;[0
- [SDR SWAA2025032609517](https://openairdocs.org/sdr/SWAA2025032609517), Mar 26, 2025: HANDLE. BROKEN. CREW REPORTS FWD MEGAPHONE HANDLE IS BROKEN.<[01] REMOVED AND REPLACED FWD MEGAPHONE PER AMM 25-64-00.
- [SDR SWAA2025022699969](https://openairdocs.org/sdr/SWAA2025022699969), Feb 26, 2025: MOTOR. INOPERATIVE. ELECTRIC STAB TRIM INOP MANUAL TRIM NORMAL<[01]. REMOVED AND REPLACED STABILIZER TRIM MOTOR PER AMM 27-41-71. OPS CHECK GOOD.
- [SDR SWAA2025021094168](https://openairdocs.org/sdr/SWAA2025021094168), Feb 8, 2025: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS FWD SECTION DOES NOT ILLUMINATE.<[01] REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY BATTERY PACK IAW AMM 33-51-06. OP-CHECK GOOD.
- [SDR SWAA2025021094169](https://openairdocs.org/sdr/SWAA2025021094169), Feb 8, 2025: PANEL. DELAMINATED. LEADING EDGE; EDGE EROSION AND DELAMINATION TO WING TO BODY FAIRING PANEL 192BR EDGE EROSION AND DELAMINATION TO WING TO BODY FAIRING PANEL 192BR LEADING EDGE<[
- [SDR SWAA2024102551403](https://openairdocs.org/sdr/SWAA2024102551403), Oct 21, 2024: THRESHOLD. CRACKED. AFT CARGO REAR THRESHOLD CAP CRACKED<[01] UPDATED STEP 1;[02] REPLACED AFT CARGO REAR THRESHOLD CORNER CAP. DRILLED FASTENER HOLES IAW SRM 51-40-05
- [SDR SWAA2024072415237](https://openairdocs.org/sdr/SWAA2024072415237), Jul 22, 2024: BATTERY PACK. INOPERATIVE. MULTIPLE EMERGENCY LIGHTS INOP ON LH AFT SIDE.<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1673 PER AMM 33-51-06; OPS CHECK GOOD AT THIS TIME.
- [SDR SWAA2024031563936](https://openairdocs.org/sdr/SWAA2024031563936), Mar 15, 2024: VAPOR BARRIER. CRACKED. RH WHEEL WELL FWD BULKHEAD VAPOR BARRIER PANEL HAS 2 CRACKS. ONE APPROXIMATELY 2 THE OTHER 4<[01] REPAIRED PER M-21-157-00675-REPREF.
- [SDR SWAA2024030860727](https://openairdocs.org/sdr/SWAA2024030860727), Mar 8, 2024: BULB. INOPERATIVE. EMERGENCY LIGHT AFT OF THE AFT ENTRY DOOR DOES NOT ILLUMINATE<[01] REMOVED AND REPLACED EMEGENCY LIGHT BULB ON LH EXTERIOR AFT OF L2 DOOR IN REFERENCE WITH AMM 
- [SDR SWAA2024021552518](https://openairdocs.org/sdr/SWAA2024021552518), Feb 15, 2024: LAMP. INOPERATIVE. AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP.<[01] RELAMPED EXIT LIGHT PER AMM 33-51-04.
- [SDR SWAA2024010437683](https://openairdocs.org/sdr/SWAA2024010437683), Jan 3, 2024: UNKNOWN. UNKNOWN. #1 FUEL TANK SHOWS APROX 2000 LBS LOWER FUEL QTY THAN #2 TANK IN CRUISE PERFORMED AMM 28-11-00 NO LEAKS NOTED. PERFORMED AMM 28 28-41-00 NO FAULTS AND QTY INDIC
- [SDR SWAA2023120728915](https://openairdocs.org/sdr/SWAA2023120728915), Dec 7, 2023: IDG. SHEARED. IN CRUISE #1 DRIVE LIGHT; #1 SOURCE LIGHT; & #1 GEN OFF BUS LIGHT ILLUMINATED; FOLLOWED PROCEDURE IN QRH. DISCONNECTED #1 DRIVE. DIVERTED TO MCI. PERFORMED NORM
- [SDR SWAA2023071277411](https://openairdocs.org/sdr/SWAA2023071277411), Jul 12, 2023: LENS. OUT OF ADJUST. 1ABC OVERHEAD BIN EMERGENCY LIGHT LENS IS PUSHED INTO BULLNOSE AND LOOSE.<[01] REPOSITION EMERGENCY LIGHT LENS COVER <BR>REF AMM 33-51-03;[02] C/W
- [SDR SWAA2023062170112](https://openairdocs.org/sdr/SWAA2023062170112), Jun 21, 2023: PIN. OUT OF POSITION. LANDING GEAR LEVER WOULD NOT RAISE TO UP POSITION AFTER TAKEOFF. RAN QRH CHECKLIST. TAKEOFF WARNING HORN CONTINUED TO SOUND AFTER FLAPS UP. TAKEOFF WARNING CUTO
- [SDR SWAA2023050124475](https://openairdocs.org/sdr/SWAA2023050124475), Apr 6, 2023: BRACKET. ELONGATED. ELONGATED HOLES ON NEW BRACKET LOCATED ON WING TO BODY FAIRING AT LOWER FUSELAGE RH 2023-212859<[01] PERFORMED OVERSIZE HOLE ON BRACKET LOC WING TO BODY FAIRING

All 297: https://openairdocs.org/aircraft/N282WN/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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