# N914WN: 2008 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: 36622
- Year built: 2008
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 7, 2008
- Certificate issued: April 17, 2008
- Expires: March 31, 2030
- Mode S code: ACA788
- 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=914WN
- Page: https://openairdocs.org/aircraft/N914WN

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 N914WN.

## FAA accident and incident reports

None matched to N914WN.

## Service difficulty reports (256, 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 SWAA2026101256846](https://openairdocs.org/sdr/SWAA2026101256846), Oct 8, 2026: COVER. LOOSE. ESCAPE SLIDE PACK COVER LOOSE AFT ENTRY DOOR. REMOVED ADJUSTED & REINSTALLED AFT ENTRY ESCAPE SLIDE IAW AMM 25-66-01.
- [SDR SWAA2026061010645](https://openairdocs.org/sdr/SWAA2026061010645), Jun 10, 2026: BATTERY PACK. NO TEST. AFT LEFT EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK IAW MM 33-51-06.
- [SDR SWAA2026061010644](https://openairdocs.org/sdr/SWAA2026061010644), Jun 10, 2026: BATTERY PACK. NO TEST. AFT RT EMERGENCY LIGHTING BATTERY PACK FAILED A CAPACITY CHECK. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK IAW MM 33-51-06.
- [SDR SWAA2025120943260](https://openairdocs.org/sdr/SWAA2025120943260), Dec 5, 2025: HANDLE. LOOSE. PAX CABIN AFT LEFT DOOR LINING ASSISTANT HANDLE LOOSE. PAX CABIN AFT LEFT DOOR LINING ASSISTANT HANDLE IAW AMM-52-13-31-400-802 STEP 3.G.(2).
- [SDR SWAA2025121039101](https://openairdocs.org/sdr/SWAA2025121039101), Nov 23, 2025: ACCESS PANEL. CRACKED. CRACKED ACCESS PANEL 344GB AT RT HORIZONTAL STABILIZER. REPAIRED ACCESS PANEL 344GB AT RT HORIZONTAL STABILIZER IAW SRM 55-20-01-2R-4, REPAIR 4.
- [SDR SWAA2025121039100](https://openairdocs.org/sdr/SWAA2025121039100), Nov 23, 2025: ACCESS PANEL. CRACKED. CRACKED ACCESS PANEL 334GB AT LT HORIZONTAL STABILIZER. REPAIRED ACCESS PANEL 334GB AT LT HORIZONTAL STABILIZER IAW SRM 55-20-01-2R-4, REPAIR 4.
- [SDR SWAA2025120939102](https://openairdocs.org/sdr/SWAA2025120939102), Nov 23, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLE ON ACCESS PANEL 334GB AT LT HORIZONTAL STABILIZER. REPAIRED ACCESS PANEL 334GB AT LT HORIZONTAL STABILIZER IAW SRM 51-70-04-2R-9, REPAIR 9.
- [SDR SWAA2025121035632](https://openairdocs.org/sdr/SWAA2025121035632), Nov 15, 2025: STIFFENER. CRACKED. CRACK ON STIFFENER LOCATED ON STAB STA 129.50 AT FRONT SPAR RT HORIZONTAL STABILIZER. REPLACED STIFFENER ON STAB STA 129.50 AT FRONT SPAR RT HORIZONTAL STABILIZ
- [SDR SWAA2025121034210](https://openairdocs.org/sdr/SWAA2025121034210), Nov 11, 2025: FILLER. MISMANUFACTURED. RIGHT WING OTBD FIXED L/E REPAIR, BTW SS 61.75 & SS 67.53, REPAIR FILLER DOES NOT HAVE THE REQUIRED SIZE IAW EA 1-757-16674. FILLER HAS BEEN ADJUSTED ON RT WING
- [SDR SWAA2025121033790](https://openairdocs.org/sdr/SWAA2025121033790), Nov 11, 2025: WEB. CRACKED. CRACKED NR 2 VAPOR BARRIER WEB, BS 663.75, RBL 25 MAIN WHEEL WELL. REPAIRED THE VAPOR BARRIER WEB IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2025121034214](https://openairdocs.org/sdr/SWAA2025121034214), Nov 11, 2025: FLOORBEAM. CRACKED. MAIN CABIN FLOORBEAM CRACKED, BS 540, BL 0 - LBL 24.75. REPLACED THE FLOORBEAM IAW SRM 51-40-02-0G-0, AND DWG 143A0060, SHEET 46, REV -. .
- [SDR SWAA2025120434212](https://openairdocs.org/sdr/SWAA2025120434212), Nov 11, 2025: FLOORBEAM. CRACKED. MAIN CABIN FLOORBEAM HAS CRACK AT BS 540; BL 0 TO RBL 24.75. REPLACED THE FLOORBEAM IAW SRM 51-40-02-0G-0, DWG 143A5240, SHEET 13, REV -, AND DWG 143A0060, SHEE
- [SDR SWAA2025121033223](https://openairdocs.org/sdr/SWAA2025121033223), Nov 9, 2025: BRACKET. CRACKED. CRACK ACCESS PANEL 651FB TRAILING EDGE BRACKET RT WING. REPLACED BRACKET ON ACCESS PANEL 651FB TRAILING EDGE BRACKET RT WING IAW SRM 51-40-02 AND SRM 51-10-02. 
- [SDR SWAA2025121033220](https://openairdocs.org/sdr/SWAA2025121033220), Nov 9, 2025: BRACKET. CRACKED. CRACK ACCESS PANEL 551FB TRAILING EDGE BRACKET LT WING. REPLACED BRACKET ON ACCESS PANEL 551FB TRAILING EDGE LT WING IAW SRM 51-40-02, SRM 51-20-01, AND DWG 115
- [SDR SWAA2025121033221](https://openairdocs.org/sdr/SWAA2025121033221), Nov 9, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLE ACCESS PANEL 651FB TRAILING EDGE LOCATED ON STIFFENER RT WING. REPLACED BEAM ON ACCESS PANEL 651FB TRAILING EDGE LOCATED ON STIFFENER RT WING IAW
- [SDR SWAA2025121033222](https://openairdocs.org/sdr/SWAA2025121033222), Nov 9, 2025: SUPPORT ANGLE. CRACKED. CRACK ACCESS PANEL 551GB TRAILING EDGE SUPPORT ANGLE LT WING. REPLACED SUPPORT ANGLE ON ACCESS PANEL 551GB TRAILING EDGE IAW SRM 51-40-02; SRM 51-10-02, AND DWG
- [SDR SWAA2025121033217](https://openairdocs.org/sdr/SWAA2025121033217), Nov 8, 2025: PLATE. CRACKED. CRACKED CORRUGATED PLATE LOCATED TRAILING EDGE IRSS 216 AT LT WING. MEASUREMENT OF CRACK: L 0.800 INCHES. REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE IRSS 2
- [SDR SWAA2025121033218](https://openairdocs.org/sdr/SWAA2025121033218), Nov 8, 2025: PLATE. CRACKED. CRACK CORRUGATED PLATE ON TRAILING EDGE IRSS 216 AT RT WING. REPLACED CORRUGATED PLATE ON TRAILING EDGE IRSS 216, RT WING IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G
- [SDR SWAA2025121033219](https://openairdocs.org/sdr/SWAA2025121033219), Nov 8, 2025: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET LOCATED TRAILING EDGE IRSS139 RT WING. MEASURE OF CRACK SUPPORT BRACKET IS L:1.664 INCHES, AND NOT FOUND ALLOWABLE DAMAGE, SRM 57-51-02-1A
- [SDR SWAA2025121033037](https://openairdocs.org/sdr/SWAA2025121033037), Nov 7, 2025: ANGLE. CRACKED. CRACKED BILGE ANGLE, BS 867, S26L IN THE AFT CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02-0G-0, 51-10-02-0G-0, STEP 9, AND DWG 149A8102, SHEET 17, REV -. MEAS
- [SDR SWAA2025121033041](https://openairdocs.org/sdr/SWAA2025121033041), Nov 7, 2025: PLATE. CORRODED. CORRODED BILGE PLATE BTW BS 787 - 796, S25R, WL 156. REPLACED THE BILGE PLATE IAW SRM 51-40-02, AND DWG 146A0081, SHEET 37, REV-.
- [SDR SWAA2025120933039](https://openairdocs.org/sdr/SWAA2025120933039), Nov 7, 2025: CARGO TRACK. CRACKED. CRACK TRACK RBL 13.80 ON BS 767 IN THE AFT CARGO COMPARTMENT. PERFORMED REPAIR ON TRACK, RBL 13.80 ON BS 767 AT AFT CARGO COMPARTMENT IAW SRM 53-00-53-2R-3, REP
- [SDR SWAA2025120933040](https://openairdocs.org/sdr/SWAA2025120933040), Nov 7, 2025: CARGO TRACK. CRACKED. CRACK TRACK RBL 13.80 ON BS 727C IN THE AFT CARGO COMPARTMENT. PERFORMED REPAIR ON TRACK LOC. RBL 13.80 ON BS 727C AT AFT CARGO COMPARTMENT IAW SRM 53-00-53-2R-
- [SDR SWAA2025121032243](https://openairdocs.org/sdr/SWAA2025121032243), Nov 5, 2025: SUPPORT. CORRODED. CORRODED LOWER SILL, BTW BS 440 - 492.4, RBL 22, WL 156 IN FWD CARGO BAY. (8 EA). REPLACED THE LOWER SILL IAW SRM 51-40-02, AND DWG 143A8330, SHEET 42, REV A.
- [SDR SWAA2025121046461](https://openairdocs.org/sdr/SWAA2025121046461), Nov 5, 2025: WEB. CORRODED. CORROSION SHIELD WEB LOCATED BTW BS 492.4 - 500A, S26R, WL 156 IN FWD CARGO COMPARTMENT. REPLACED SHIELD WEB AND FASTENERS IAW SRM 51-40-02, AND DWG 143A0080, S
- [SDR SWAA2025121032242](https://openairdocs.org/sdr/SWAA2025121032242), Nov 5, 2025: WEB. CORRODED. CORROSION SHIELD WEB LOCATED BTW BS 492.4 - 500A, S26R, WL 156 IN FWD CARGO COMPARTMENT. REPLACED THE SHIELD WEB AND FASTENERS BS 492.4 - 500A, S26R, WL 156 IAW
- [SDR SWAA2025120432245](https://openairdocs.org/sdr/SWAA2025120432245), Nov 5, 2025: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE ON AUXILIARY TRACK SLAT 8 INBOARD POSITION AT RT WING. REPLACED SUPPORT ANGLE ON AUXILIARY TRACK SLAT 8 INBD POSITION AT RT WING IAW CMM-57-
- [SDR SWAA2025121031762](https://openairdocs.org/sdr/SWAA2025121031762), Nov 4, 2025: ACCESS PANEL. DELAMINATED. DELAMINATED ACCESS PANEL 542EB AT LT WING. REPLACED BY A NEW ACCESS PANEL 542EB IAW AMM 27-51-18-400-802, STEP 5.G(5).
- [SDR SWAA2025121046456](https://openairdocs.org/sdr/SWAA2025121046456), Nov 4, 2025: ACCESS PANEL. DELAMINATED. DELAMINATED ACCESS PANEL 542EB AT LT WING. REPLACED DELAMINATED ACCESS PANEL 542EB DUE TO WAS FOUND OUT OF LIMIT IAW AMM 27-51-18-400-802 STEP 5.G5.
- [SDR SWAA2025121030900](https://openairdocs.org/sdr/SWAA2025121030900), Nov 2, 2025: SCUFF PLATE. CRACKED. CRACKED FWD SCUFF PLATE IN THE FWD CARGO BAY CUTOUT. REPAIRED FWD SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, AND BAC 5975.
- [SDR SWAA2025121031135](https://openairdocs.org/sdr/SWAA2025121031135), Nov 2, 2025: STIFFENER. CRACKED. FWD CARGO BAY BULKHEAD VERTICAL STIFFENER CRACKED, BS 540, LBL 24.97. REPLACED VERTICAL STIFFENER IAW SRM 51-40-02-0G-0, SRM 51-10-02-G-0, ITEM 9, AND DWG 11A20
- [SDR SWAA2025121031136](https://openairdocs.org/sdr/SWAA2025121031136), Nov 2, 2025: STIFFENER. CRACKED. FWD CARGO BAY BULKHEAD VERTICAL STIFFENER CRACKED BS 540, LBL 0.22. REPLACED THE VERTICAL STIFFENER IAW SRM 51-40-02-0G-0, SRM 51-10-02-G-0, ITEM 9, AND DWG 11A
- [SDR SWAA2025121031139](https://openairdocs.org/sdr/SWAA2025121031139), Nov 2, 2025: GUSSET. CRACKED. CRACKED GUSSET, BS 500D, S19R IN THE FWD CARGO BAY. REPLACED THE GUSSET IAW SRM 51-40-02-0G-0, AND DWG 143A7902, SHEET 209, REV-.
- [SDR SWAA2025121031140](https://openairdocs.org/sdr/SWAA2025121031140), Nov 2, 2025: GUSSET. CRACKED. CRACKED GUSSET, BS 500D, S19L IN FWD CARGO BAY. INSTALLED GUSSET IAW SRM 51-40-02-0G-0, AND DWG 143A7902, SHEET 209, REV-.
- [SDR SWAA2025121031134](https://openairdocs.org/sdr/SWAA2025121031134), Nov 2, 2025: PLATE. CRACKED. CRACKED SEAL PLATE, ACCESS PANEL 333AB AT THE LT HORIZONTAL STAB. REPLACED THE SEAL ON ACCESS PANEL 333AB AT LT HORIZONTAL STAB IAW SRM 51-40-02-0G-0, AND SRM 5
- [SDR SWAA2025120931138](https://openairdocs.org/sdr/SWAA2025120931138), Nov 2, 2025: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET LOCATED BS 540 AT LEVEL RBL 6 AT AIR CONDITIONING. REPLACED SUPPORT SUPPORT BRACKET LOCATED BS 540 AT LEVEL RBL 6 AT AIR CONDITIONING BAY 
- [SDR SWAA2025120931023](https://openairdocs.org/sdr/SWAA2025120931023), Nov 2, 2025: RIB. CRACKED. CRACK ON INSPAR RIB LOCATED STAB STA 129.50 AND 28 INCHES OF FROM SPAR AT RT HORIZONTAL STABILIZER. STEP 5 ANND STEP 6. EDDY CURRENT EQUIPMENT USED P/N: NORTEC 
- [SDR SWAA2025121030757](https://openairdocs.org/sdr/SWAA2025121030757), Nov 1, 2025: PRESSURE DECK. CRACKED. CRACK INDICATION ON THE HORIZONTAL PRESSURE DECK WEB, LBL 31, BS 663 IN MAIN WHEEL WELL. CRACK LENGTH: 0.312 IN. PERFORMED REPAIR ON HORIZONTAL PRESSURE DECK WE
- [SDR SWAA2025121030762](https://openairdocs.org/sdr/SWAA2025121030762), Nov 1, 2025: SKIN. CORRODED. CORROSION ON INTERNAL SKIN TOILET SERVICE DOOR 145AL, LOWER FUSELAGE. PERFORMED REPAIR ON TOILET SERVICE DOOR 145AL AT LOWER FUSELAGE IAW SRM 52-40-01-2R-8, REP
- [SDR SWAA2025121030756](https://openairdocs.org/sdr/SWAA2025121030756), Nov 1, 2025: STUB FRAME. CRACKED. CRACK INDICATION ON STUB FRAME, BETWEEN BS 294.5 - 296.5, S8R - 9R AT THE FWD GALLEY DOOR AREA. CRACK LENGTH: 1.187 IN. REPLACED THE STUB FRAME IAW SRM 51-40-02
- [SDR SWAA2025121030758](https://openairdocs.org/sdr/SWAA2025121030758), Nov 1, 2025: ACCESS PANEL. CRACKED. CRACKED ACCESS PANEL 193AR AT FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL 193AR IAW SRM 51-70-05-2R-2, REPAIR 2.
- [SDR SWAA2025121050826](https://openairdocs.org/sdr/SWAA2025121050826), Nov 1, 2025: ACCESS PANEL. CRACKED. CRACKED ACCESS PANEL 193AL, BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL 193AL BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-05-2R-2, REPAIR 2
- [SDR SWAA2025120430899](https://openairdocs.org/sdr/SWAA2025120430899), Nov 1, 2025: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 695, RBL 24.75, WL208.1 IN PASSENGER CABIN. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DWG 111A6000, SHEET 304
- [SDR SWAA2025120930608](https://openairdocs.org/sdr/SWAA2025120930608), Oct 31, 2025: LIGHT. BROKEN. BROKEN PHOTOLUMINESCENT STRIPS RT AT PASSENGER CABIN ( 6 EA). REPLACED PHOTOLUMINESCENT STRIP IAW AMM-33-51-15-400-802.
- [SDR SWAA2025120930609](https://openairdocs.org/sdr/SWAA2025120930609), Oct 31, 2025: LIGHT. CRACKED. CRACKED PHOTOLUMINESCENT STRIPS LT IN PASSENGER CABIN (5 EA). REPLACED PHOTOLUMINESCENT STRIP AT LT PASSENGER CABIN (5 EA) IAW AMM-33-51-15-400-802
- [SDR SWAA2025121030190](https://openairdocs.org/sdr/SWAA2025121030190), Oct 30, 2025: VAPOR BARRIER. CRACKED. CRACK VAPOR BARRIER WEB, BS 663.75, BTW RBL 25 - 35. REPAIRED THE VAPOR BARRIER WEB IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2025072895488](https://openairdocs.org/sdr/SWAA2025072895488), Jul 25, 2025: PCU. FAULTY. DURING CLIMB OUT AT 14000 AND AGAIN AT 16000 FT THE RUDDER KICKED LEFT WITHOUT PILOT INPUT. OCCURRED AGAIN AT FL370 APPROX 30 MINUTES LATER. AUTOPILOT DID NOT D
- [SDR SWAA2025071691134](https://openairdocs.org/sdr/SWAA2025071691134), Jul 13, 2025: LENS. DAMAGED. OVERHEAD EMERGENCY EXIT SIGN DAMAGED BY PASSENGER. FOUND FWD LENS OF CENTER AISLE OVERHEAD EXIT SIGN BY EMERGENCY EXIT ROW CAME LOOSE. RESECURED LENS TO HOUSING
- [SDR SWAA2025060276130](https://openairdocs.org/sdr/SWAA2025060276130), May 29, 2025: LAMP. INOPERATIVE. R/H OVER WING EMERGENCY LIGHT INOP. <[01] R/R R/H OVERWING EMERGENCY EXIT LAMP PER AMM 33-51-04. OPS CHECK GOOD.
- [SDR SWAA2025050565143](https://openairdocs.org/sdr/SWAA2025050565143), Apr 29, 2025: LIGHT. BROKEN. FOUND AFT R2 DOOR LOWER EMERGENCY EXIT LIGHT ASSY BROKEN.<[01] REMOVED + REPLACED R2 DOOR LOWER EMERGENCY EXIT LIGHT ASSY IAW AMM 33-51-01; OPS CHECK GOOD.;[02]

All 256: https://openairdocs.org/aircraft/N914WN/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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