# N929WN: 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 CFM56-7B24/3 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-3-series) (registry code 13074)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 36631
- Year built: 2008
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 1, 2008
- Certificate issued: August 26, 2008
- Expires: February 29, 2028
- Mode S code: ACE19A
- 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=929WN
- Page: https://openairdocs.org/aircraft/N929WN

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 CFM56-7B24/3 model are included.

## ADs that may apply (OpenAirDocs): 10 in force

### Matched by airframe (Boeing 737-7H4)

None in force.

### Matched by engine (CFM International CFM56-7B24/3 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 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 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

### 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 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

## 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 N929WN.

## FAA accident and incident reports

None matched to N929WN.

## Service difficulty reports (267, 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 SWAA2026081780267](https://openairdocs.org/sdr/SWAA2026081780267), Aug 13, 2026: EXTINGUISHER. LOW PRESSURE. LEFT ENGINE FIRE BOTTLE IN WHEEL WELL READS 450 PSI. R & R ENGINE FIRE EXTINGUISHING BOTTLE NR 1 IAW AMM 26-21-01. OPS CHKD GOOD.
- [SDR SWAA2026070115977](https://openairdocs.org/sdr/SWAA2026070115977), Jun 26, 2026: FUSE. INOPERATIVE. EMERGENCY EXIT SIGN MOUNTED ON FDR ACCESS DOOR IS INOPERATIVE. REMOVED AND REPLACED FUSE ON (M1672) AND PERFORMED A GOOD TEST EMERGENCY EXIT SIGN MOUNTED ON FDR
- [SDR SWAA2026070107929](https://openairdocs.org/sdr/SWAA2026070107929), May 30, 2026: BATTERY. INOPERATIVE. RIGHT OVER WING EMERGENCY EXIT LIGHT (EXTERNAL) INOPERATIVE. REPLACED M1669 EMERGENCY BATTERY IAW AMM 33-51-06-960-805. RELAMPED RIGHT OVERWING EMERGENCY EXIT S
- [SDR SWAA2026063007668](https://openairdocs.org/sdr/SWAA2026063007668), May 29, 2026: WINDOW FRAME. CRACKED. F/O'S NR 1 WINDOW FRAME POST OTBD UPPER CORNER IS CRACKED. F/O'S NR 1 WINDOW FRAME REPAIRED IAW EA 26-153-01462.
- [SDR SWAA2026063007029](https://openairdocs.org/sdr/SWAA2026063007029), May 27, 2026: STRAP. CRACKED. CRACK NOTED IN ONE FASTENER HOLE DURING OHEC INSPECTION (TTG8Q01BLWC6; STEP 22) OF RT STUB BEAM STRAP, BS 639, RBL 45, LOWER AFT HOLE, EXTENDING IN AFT DIRECTIO
- [SDR SWAA2026063006488](https://openairdocs.org/sdr/SWAA2026063006488), May 26, 2026: FRAME. CRACKED. BS 312 FRAME CRACKED WL 283 LBL 35 ABOVE FWD ENTRY UPPER SILL WEB. ACCOMPLISHED REPAIR OF FRAME AT BS 312, WL 283, LBL 35, BTW S5L AND S6L IAW EA M-22-153-01244
- [SDR SWAA2026070105686](https://openairdocs.org/sdr/SWAA2026070105686), May 22, 2026: WINDOW FRAME. CRACKED. CAPTAINS #1 WINDOW FRAME HAS CRACK IN LOWER INBOARD CORNER<[01] ACCOMPLISHED HFEC SURFACE SCAN OF SUSPECTED CRACKED LOCATION IAW 737 NDTM PART 6 CHAPTER 51-00-0
- [SDR SWAA2026063005364](https://openairdocs.org/sdr/SWAA2026063005364), May 21, 2026: RIB. CRACKED. RIGHT HORIZONTAL STAB REMOVABLE LEADING-EDGE 2ND FROM INBD RIB CRACKED. REMOVED, LOCATED, AND DRILLED. REPLACED NEW RT HORIZONTAL STAB REMOVABLE LEADING-EDGE 2N
- [SDR SWAA2026063004615](https://openairdocs.org/sdr/SWAA2026063004615), May 20, 2026: CARTRIDGE. CRACKED. CRACKED FOUND ON RT OTBD AFT FLAP CARTRIDGE. RECEIVED A NEW AFT FLAP. NO FURTHER ACTION REQUIRED ON THIS FAULT.
- [SDR SWAA2026063004616](https://openairdocs.org/sdr/SWAA2026063004616), May 20, 2026: RIB. CRACKED. CRACK FOUND ON RT OTBD AFT FLAP CLOSURE RIB. PROCURED NEW LT OTBD AFT FLAP. REMOVAL AND INSTALLATION TO BE ACCOMPLISHED ON FAULT TTG8Q01C9QA5. IAW AMM 27-51-22-
- [SDR SWAA2026063004981](https://openairdocs.org/sdr/SWAA2026063004981), May 20, 2026: SKIN. CRACKED. CRACK NOTED ON RT HORIZONTAL STABILIZER LOWER SKIN, BS 193.90; APPROX 3.6' FWD OF PREVIOUS REPAIR; L: 0.25'. REPAIRED PER EA 26-155-01375 WITH REPETITIVE INSPEC
- [SDR SWAA2026063004259](https://openairdocs.org/sdr/SWAA2026063004259), May 18, 2026: SEAT TRACK. CORRODED. CORROSION IN WELL ON PASSENGER CABIN SEAT TRACKS AT BS 480+15- BS 500+8, BS 500A+6 - BS 500A+18, BS 500D+8 - BS 500D+19. ON CROWN BS 500A+18 AT LBL 25 WL 208. S
- [SDR SWAA2026063004261](https://openairdocs.org/sdr/SWAA2026063004261), May 18, 2026: SEAT TRACK. CORRODED. CORROSION ON PASSENGER CABIN SEAT TRACKS IN WELL AT BS 480+14 - BS 480+19, BS 500A+4 - BS 500A+16, BS 500D+9 - BS 500D+13. ON CROWN BS 480+8 - BS 480+13, LBL 45
- [SDR SWAA2026063003768](https://openairdocs.org/sdr/SWAA2026063003768), May 17, 2026: INTERCOSTAL. CORRODED. CORRODED FLOOR SUPPORT AT BS 294 - 312, LBL 11, WL 208. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G-0, DWG 141A5600, SHEET 1, REV N, AND DWG 141A56
- [SDR SWAA2026063003561](https://openairdocs.org/sdr/SWAA2026063003561), May 16, 2026: STRAP. CORRODED. CORROSION ON STRAP AT BS 1022-1029, RBL 3, WL 208. REMOVED AND REPLACED STRAP IAW SRM 51-40-02-0G-0 AND DWG 147A5730, SHEET 23, REV C.
- [SDR SWAA2026063003562](https://openairdocs.org/sdr/SWAA2026063003562), May 16, 2026: WEB. CORRODED. CORROSION ON WEB AT BS 1018 LBL 1 WL 208. NO ALLOWABLE ENTRIES FOUND THEREFORE SHEAR WEB DAMAGE TO BE REMOVE IAW SRM 51-10-02-0G-0 AND SENT TO ENGINEERING FOR F
- [SDR SWAA2026063003555](https://openairdocs.org/sdr/SWAA2026063003555), May 16, 2026: STRAP. CORRODED. CORRODED ON STRAP AT BS 1016-1029, LBL 3, WL 208. REMOVED AND REPLACED STRAP AT BS 1016-1029, LBL 3, WL 208 IAW SRM 51-40-02-0G-0, AND DWG 147A5600, SHEET 32, R
- [SDR SWAA2026063003565](https://openairdocs.org/sdr/SWAA2026063003565), May 16, 2026: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL AT BS 380-400, RBL 40, WL 208. REMOVED AND REPLACED INTERCOSTAL FROM BS 380-400 RBL 40 WL 208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 143A540
- [SDR SWAA2026063003566](https://openairdocs.org/sdr/SWAA2026063003566), May 16, 2026: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL AT BS 380-400, LBL 13, WL 208. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02-0G-0, AND DWG 143A5400, REV A.
- [SDR SWAA2026063003558](https://openairdocs.org/sdr/SWAA2026063003558), May 16, 2026: CREASE BEAM. CORRODED. CORROSION ON CREASE BEAM WEB AT BS 727A+16 LBL 69 WL 208. REMOVED AND TREATED CORROSION OF CREASE BEAM WEB AT BS 727A+16 LBL 69 WL 208 PER SRM 51-10-02-0G-0 AND
- [SDR SWAA2026063003556](https://openairdocs.org/sdr/SWAA2026063003556), May 16, 2026: FLOOR SUPPORT. CRACKED. CRACKED FLOOR SUPPORT AT BS 270 - 277, LBL 1, WL 208. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0, & DWG 141A5210, SHEET 19, REV -.
- [SDR SWAA2026063003563](https://openairdocs.org/sdr/SWAA2026063003563), May 16, 2026: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL AT BS 312 - 328, RBL 31, WL 208. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G-0, AND DWG 141A5400, REV-.
- [SDR SWAA2026063003567](https://openairdocs.org/sdr/SWAA2026063003567), May 16, 2026: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL AT BS 312 - 328, LBL 45, WL 208. REMOVED AND REPLACED THE INTERCOSTAL AT BS 312-328 LBL 45 WL 208 IAW SRM 51-40-02, & DWG 141A5400, REV-.
- [SDR SWAA2026062903560](https://openairdocs.org/sdr/SWAA2026062903560), May 16, 2026: STRAP. CORRODED. CORROSION ON STRAP AT BS 1026-1028, RBL 17, WL 208. REMOVED AND REPLACED STRAP AT BS 1026-1028, RBL 17, WL 208 IAW SRM 51-40-02-0G-0, AND DWG 147A5730, SHEET 23
- [SDR SWAA2026063003549](https://openairdocs.org/sdr/SWAA2026063003549), May 15, 2026: FLOOR PANEL. PULLED. AFT FLOOR PANEL 242TF UPPER SURFACE HAS PULLED STRANDS<[01] 242TF AFT FLOOR PANEL FOUND UPPER AND LOWER SURFACE DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.;
- [SDR SWAA2026062903537](https://openairdocs.org/sdr/SWAA2026062903537), May 15, 2026: FLOOR PANEL. PULLED. AFT FLOOR PANEL 241YF UPPER SURFACE HAS PULLED STRANDS. REPAIRED PER SRM 53-00-50-2R-1-A00939.
- [SDR SWAA2026062903543](https://openairdocs.org/sdr/SWAA2026062903543), May 15, 2026: FLOOR PANEL. PULLED. AFT FLOOR PANEL 242UF UPPER SURFACE HAS PULLED STRANDS. 242UF AFT FLOOR PANEL FOUND UPPER AND LOWER SURFACE DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026062903535](https://openairdocs.org/sdr/SWAA2026062903535), May 15, 2026: FLOOR PANEL. PULLED. AFT FLOOR PANEL 241AAF UPPER SURFACE HAS PULLED STRANDS. FABRICATION OF NEW 241AAF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026062903540](https://openairdocs.org/sdr/SWAA2026062903540), May 15, 2026: FLOOR PANEL. PULLED. AFT FLOOR PANEL 241ABF UPPER SURFACE HAS PULLED STRANDS. AFT FLOOR PANEL 241ABF UPPER SURFACE WITH PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.
- [SDR SWAA2026062903536](https://openairdocs.org/sdr/SWAA2026062903536), May 15, 2026: FLOOR PANEL. PULLED. AFT FLOOR PANEL 241XF UPPER SURFACE HAS PULLED STRANDS. AFT FLOOR PANEL 241XF UPPER SURFACE WITH PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.
- [SDR SWAA2026062903547](https://openairdocs.org/sdr/SWAA2026062903547), May 15, 2026: FLOOR PANEL. PULLED. FWD FLOOR PANEL 222BF UPPER SURFACE HAS PULLED STRANDS. FWD FLOOR PANEL 222BF UPPER SURFACE WITH PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.
- [SDR SWAA2026062903548](https://openairdocs.org/sdr/SWAA2026062903548), May 15, 2026: FLOOR PANEL. PULLED. FWD FLOOR PANEL 222DF UPPER SURFACE HAS PULLED STRANDS. PULLED STRANDS ON UPPER SURFACE OF FWD FLOOR PANEL 222DF WERE REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026062903407](https://openairdocs.org/sdr/SWAA2026062903407), May 15, 2026: STUB FRAME. CRACKED. CRACK ON FSD STUB FRAME .6' ABOVE SEAL DEPRESSOR AT BS291.5 + 9, REMOVED DAMAGE FSD STUB FRAME, LOCATED, DRILLED, AND INSTALLED NEW FSD STUB FRAME AT BS 291+9 I
- [SDR SWAA2026063001515](https://openairdocs.org/sdr/SWAA2026063001515), May 14, 2026: FORMER. CRACKED. WING TO BODY FAIRING FORMER IS CRACKED BS 500D BETWEEN STRINGER 19 AND 20 RT. REMOVED DAMAGED FAIRING FORMER AND INSTALLED NEW WING TO BODY FAIRING FORMER AT BS
- [SDR SWAA2026062903174](https://openairdocs.org/sdr/SWAA2026062903174), May 14, 2026: SPLICE STRAP. CORRODED. CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE, BS 767+6, RBL 11.5, WL 156. CORROSION ON STRAP WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS 
- [SDR SWAA2026062998078](https://openairdocs.org/sdr/SWAA2026062998078), May 13, 2026: SKIN. DEBONDED. PANEL 192AL OUTER SKIN IS DISBONDED. REPAIRED OUTER SKIN DISBOND IAW SRM 51-70-05-2R-2-A00733. (REPAIR 2 - REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH (12.70 M
- [SDR SWAA2026062901514](https://openairdocs.org/sdr/SWAA2026062901514), May 13, 2026: PRESSURE DECK. CRACKED. CRACK FOUND ON HORIZONTAL PRESSURE DECK RBL 39, BS 663+2, L: 0.300. REPAIRED HORIZONTAL PRESSURE DECK AT BS 663 - BS 675; RBL 39 - RBL 62 IAW SRM 53-40-51-2R-2,
- [SDR SWAA2026062998042](https://openairdocs.org/sdr/SWAA2026062998042), May 12, 2026: SCUFF PLATE. CRACKED. FWD SERVICE DOOR SCUFF PLATE CRACKED AT AFT EDGE. ACCOMPLISHED REPAIR OF CRACKED FSD SCUFF PLATE PER SRM 53-10-15-2R-2. SCUFF PLATE WILL BE INSTALLED BY TASK TT
- [SDR SWAA2026040785240](https://openairdocs.org/sdr/SWAA2026040785240), Apr 1, 2026: BRACKET. CRACKED. AFT SERVICE DOOR LINER LOWER ATTACH PLATE FWD BRACKET CRACKED. R & R AFT SERVICE DOOR LINER LOWER PAN IAW AMM 52-41-31.
- [SDR SWAA2026040185248](https://openairdocs.org/sdr/SWAA2026040185248), Apr 1, 2026: LAMP. INOPERATIVE. FLIGHT DECK EMERGENCY LIGHTS, R1 DOOR SLIDE LIGHT INOPERATIVE. REPLACED THE LAMPS IN THE EMERGENCY LIGHTS R1 DOOR SLIDE LIGHT IAW AMM 33-51-04.
- [SDR SWAA2025122655593](https://openairdocs.org/sdr/SWAA2025122655593), Dec 24, 2025: SEAT BACK. NO DISCREPANCY. SEAT 11D SEAT RECLINES INTO EXIT ROW. OPS CHECKED SEAT 11D, FOUND SMALL FORWARD MOVEMENT BUT NO RECLINE MOVEMENT IAW SOPM.
- [SDR SWAA2025112037052](https://openairdocs.org/sdr/SWAA2025112037052), Nov 20, 2025: BATTERY PACK. NO TEST. PASSENGER CABIN EMERGENCY LIGHTS BATTERY PACKS M1675, M1674, M1673, & M1672 FAILED CAPACITY TEST. R & R THE EMERGENCY LIGHTS BATTERY PACKS IAW AMM 33 51-06.
- [SDR SWAA2025112037147](https://openairdocs.org/sdr/SWAA2025112037147), Nov 20, 2025: BATTERY PACK. NO TEST. PASSENGER CABIN; EMERGENCY LIGHTS BATTERY PACKS M1675, M1674, M1673, & M1672 FAILED CAPACITY TEST. R & R EMERGENCY LIGHTS BATTERY PACKS IAW AMM 33 51-06.
- [SDR SWAA2025112037148](https://openairdocs.org/sdr/SWAA2025112037148), Nov 20, 2025: BATTERY PACK. NO TEST. PASSENGER CABIN EMERGENCY LIGHTS BATTERY PACKS M1675, M1674, M1673, & M1672 FAILED CAPACITY TEST. R & R EMERGENCY LIGHTS BATTERY PACKS IAW AMM 33 51-06.
- [SDR SWAA2025112037149](https://openairdocs.org/sdr/SWAA2025112037149), Nov 20, 2025: BATTERY PACK. NO TEST. PASSENGER CABIN EMERGENCY LIGHTS BATTERY PACKS M1675, M1674, M1673, & M1672 FAILED CAPACITY TEST. R & R EMERGENCY LIGHTS BATTERY PACKS IAW AMM 33 51-06.
- [SDR SWAA2025072894905](https://openairdocs.org/sdr/SWAA2025072894905), Jul 24, 2025: DOUBLER. CORRODED. EVIDENCE OF CORROSION FOUND ON RF CONNECTOR DOUBLER UNDER WIFI RADOME AROUND CONNECTOR D9303 HOLE.<[01] COMPLIED WITH EA 25-153-02026 REF TTG8Q014719L
- [SDR SWAA2025072894906](https://openairdocs.org/sdr/SWAA2025072894906), Jul 24, 2025: DOUBLER. CORRODED. EVIDENCE OF CORROSION FOUND ON RF CONNECTOR DOUBLER BELOW WIFI RADOME AT CONNECTION D9302<[01] COMPLIED WITH EA 25-153-02026 REF TTG8Q014719L
- [SDR SWAA2025072193099](https://openairdocs.org/sdr/SWAA2025072193099), Jul 19, 2025: SIGN. BROKEN. OVERWING EXIT OVERHEAD EMERGENCY LT HOUSING BROKEN. R+R EMERGENCY EXIT SIGN PER AMM 33-51-01.
- [SDR SWAA2025032406381](https://openairdocs.org/sdr/SWAA2025032406381), Mar 18, 2025: HANDLE. LOOSE. AFT SERVICE DOOR ASSIST HANDLE LOOSE <[01]. SECURED ASSIST DOOR HANDLE REF B737 AMM 52-41-31.
- [SDR SWAA2024112671408](https://openairdocs.org/sdr/SWAA2024112671408), Nov 24, 2024: COVER. MISSING. MID-CABIN OVERHEAD AFT EXIT SALIDA SIGN COVER IS MISSING.<[01] FOUND AND RE-INSTALLED OVERHEAD EMERGENCY EXIT SIGN COVER. REF. AMM 33-51-01.

All 267: https://openairdocs.org/aircraft/N929WN/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 CFM56-7B24/3 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 CFM56-7B24/3 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-3-series.md

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