# N241WN: 2006 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: 32504
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 20, 2006
- Certificate issued: July 31, 2006
- Expires: October 31, 2027
- Mode S code: A235B7
- 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=241WN
- Page: https://openairdocs.org/aircraft/N241WN

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 N241WN.

## FAA accident and incident reports

None matched to N241WN.

## Service difficulty reports (293, 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 SWAA2026092111237](https://openairdocs.org/sdr/SWAA2026092111237), Sep 15, 2026: SCREW. MISSING. TRAY TABLE AT 14C BROKEN. REPLACED TRAY TABLE SCREW IAW SIP
- [SDR SWAA2026081364358](https://openairdocs.org/sdr/SWAA2026081364358), Aug 9, 2026: WARNING MESSAGE. FALSE ACTIVATION. NR 2 ENG OVERHEAT IND WITH NO FUEL APPLIED. INSPECTED NR 2 ENG INLET AND EXHAUST AREA NO DEFECTS NOTED. PERFORMED NORMAL ENG START PER AMM 71-00-00. NO DEFECTS 
- [SDR SWAA2026011561698](https://openairdocs.org/sdr/SWAA2026011561698), Jan 12, 2026: LENS. LOOSE. FWD GALLEY OVERHEAD LIGHT ANNUNCIATOR LENS LOOSE INDICATOR LIGHTS WORKS NORMAL AT THIS TIME. OK TO CONTINUE IAW MEL 25-10-01, SP-1B, 301789. LENS COVER SECURED 
- [SDR SWAA2026010954929](https://openairdocs.org/sdr/SWAA2026010954929), Dec 23, 2025: WEB. CRACKED. CRACK WEB LOCATED BTW BS 400 TO 420 AND AT LEVEL STRINGER 26L, FWD CARGO COMPARTMENT. REPLACED WEB AND FASTENERS LOCATED BTW BS 400 - 420, STRINGER 26L FWD CARG
- [SDR SWAA2026011248340](https://openairdocs.org/sdr/SWAA2026011248340), Dec 8, 2025: WEB. CORRODED. CORRODED WEB, BS 1016, RBL 32, REPLACED THE WEB AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, PARAGRAPH 9, AND DWG 148A0922, SHEET 20, REV -.
- [SDR SWAA2026010948341](https://openairdocs.org/sdr/SWAA2026010948341), Dec 8, 2025: WEB. CORRODED. CORROSION ON WEB, ON BS 1016, LBL 26, AFT GALLEY. REPLACED WEB AND FASTENERS, BS 1016, LBL 2 IAW SRM 51-40-02, 51-10-02, & DWG 148A0922, SHEET 20, REV -.
- [SDR SWAA2026010844137](https://openairdocs.org/sdr/SWAA2026010844137), Dec 8, 2025: WEB. CORRODED. CORROSION ON WEB BS 1016, RBL 32 IN AFT GALLEY AREA.
- [SDR SWAA2026010844138](https://openairdocs.org/sdr/SWAA2026010844138), Dec 8, 2025: WEB. CORRODED. CORROSION ON WEB, BS 1016, LBL 26 IN AFT GALLEY.
- [SDR SWAA2026011243640](https://openairdocs.org/sdr/SWAA2026011243640), Dec 7, 2025: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 663.5, LBL 41, REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02, DWG 111A1322, SHEET 5, REV-, AND 
- [SDR SWAA2026011243639](https://openairdocs.org/sdr/SWAA2026011243639), Dec 7, 2025: ACCESS PANEL. CRACKED. CRACKED LEADING EDGE RIB ACCESS PANEL 331B LOCATED LE STA 114.55 AT LT HORIZONTAL STAB. REPLACED LEADING EDGE RIB ACCESS PANEL 331B LOCATED LE STA 114.55 AT LT 
- [SDR SWAA2026011243314](https://openairdocs.org/sdr/SWAA2026011243314), Dec 6, 2025: SCUFF PLATE. CRACKED. CRACK CENTER SCUFF PLATE AT FWD SERVICE DOOR. REPAIRED THE CENTER SCUFF PLATE IAW SRM 53-10-15-2R-2, REPAIR 2. AND BAC 5975.
- [SDR SWAA2026011243548](https://openairdocs.org/sdr/SWAA2026011243548), Dec 6, 2025: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 294.5, S13L. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-10-02, STEP 9, AND DRAWING 141A1311, SHEET 1, REV C.
- [SDR SWAA2026011243547](https://openairdocs.org/sdr/SWAA2026011243547), Dec 6, 2025: STRINGER. CRACKED. CRACKED STRINGER U-8 INTERNAL AREA FUEL TANK UPPER POSITION LOC BTW RIB 19 AND RIB 20 AT RT WING. ACCOMPLISHED EA 25-157-03409-WIP1.
- [SDR SWAA2026011243308](https://openairdocs.org/sdr/SWAA2026011243308), Dec 5, 2025: PLATE. CORRODED. CORRODED BILGE AREA SHIELD PLATE BTW BS 767 & 787, RBL 13, WL 156. REPLACED THE SHIELD PLATEPARTMENT IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, AND DWG 1
- [SDR SWAA2026010943304](https://openairdocs.org/sdr/SWAA2026010943304), Dec 5, 2025: PLATE. CORRODED. CORROSION BILGE AREA SHIELD PLATE BTW BS 847 - 867, S25R, WL 156, IN THE AFT CARGO BAY. REPLACED THE SHIELD PLATE IAW SRM 51-40-02, & DWG 146A0081, SHEET 31, RE
- [SDR SWAA2026011242700](https://openairdocs.org/sdr/SWAA2026011242700), Dec 4, 2025: STRINGER. CRACKED. CRACKED STRINGER 25L, BS 540. PERFORMED A PERMANENT REPAIR ON STRINGER 25L, BTWN BS 500D & 540 IAW SRM 53-00-03-2R-1, REPAIR 1.
- [SDR SWAA2026011242702](https://openairdocs.org/sdr/SWAA2026011242702), Dec 4, 2025: STRINGER. CRACKED. CRACKED STRINGER 26L, BS 540. PERFORMED A PERMANENT REPAIR ON STRINGER 26L BTWN BS 500D & 540 IAW SRM 53-00-03-2R-1, REPAIR 1.
- [SDR SWAA2026011242703](https://openairdocs.org/sdr/SWAA2026011242703), Dec 4, 2025: STRINGER. CRACKED. CRACKED STRINGER 25R, BS 540. PERFORMED PERMANENT REPAIR ON STRINGER 25R BTW BS 500C - 540 IAW SRM 53-00-03-2R-1, REPAIR 1.
- [SDR SWAA2026011242705](https://openairdocs.org/sdr/SWAA2026011242705), Dec 4, 2025: SUPPORT BRACKET. CRACKED. CRACKED SUPPORT BRACKET, BS 867 BTW S2 & 3R. REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02, AND DWG 146A7901, SHEET 66, REV A.
- [SDR SWAA2026011242946](https://openairdocs.org/sdr/SWAA2026011242946), Dec 4, 2025: BRACKET. CORRODED. CORROSION GROUND PLATE LOCATED BTW HINGE 7A TO HINGE 8 AT VERTICAL STABILIZER. REPLACED BRACKET PLATE LOCATED BTW HINGE 7A TO HINGE 8 AT VERTICAL STAB IAW SRM 5
- [SDR SWAA2026010942699](https://openairdocs.org/sdr/SWAA2026010942699), Dec 4, 2025: INTERCOSTAL. CRACKED. CRACK WEB - INTERCOSTAL LOCATED BS 500D - 520, S28R, FWD CARGO BAY. REPLACED INTERCOSTAL IAW SRM-51-10-02, ITEM 9, & DWG 143A7902, SHEET 126, REV A.
- [SDR SWAA2026010942701](https://openairdocs.org/sdr/SWAA2026010942701), Dec 4, 2025: INTERCOSTAL. CRACKED. CRACK WEB - INTERCOSTAL LOCATED BS 500D TO BS 520 AND S-28L FWD CARGO BAY. REPLACED WEB - INTERCOSTAL BS 500D - 520, S28L IAW SRM 51-10-02, ITEM 9, SRM 51-40-02
- [SDR SWAA2026011242281](https://openairdocs.org/sdr/SWAA2026011242281), Dec 3, 2025: RETAINER. MISSING. MISSING RETAINER AT UPPER SILL DOOR CUT OUT IN THE FWD CARGO BAY. INSTALLED THE RETAINER IAW SOPM 20-50-12.
- [SDR SWAA2026010941830](https://openairdocs.org/sdr/SWAA2026010941830), Dec 2, 2025: ANGLE. CRACKED. CRACK ANGLE AT BS 400, S26L IN THE FWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 2, REV B.
- [SDR SWAA2026011241671](https://openairdocs.org/sdr/SWAA2026011241671), Dec 1, 2025: SKIN PANEL. CRACKED. CRACK INDICATION FOUND ON LT HORIZONTAL STAB LOWER SKIN PANEL. HSS 193.9, AND 16 INCHES FROM FRONT SPAR. INBD SIDE OF RIB. CRACK LENGTH = 0.950 INCH. PERFORMED 
- [SDR SWAA2026011241661](https://openairdocs.org/sdr/SWAA2026011241661), Dec 1, 2025: FLOORBEAM. CRACKED. CRACKED FLOORBEAM, BS 540, BETWEEN BL 0 TO LBL 24.75. REPLACED THE FLOORBEAM IAW SRM 51-10-02, PARAGRAPH 9, AND DRAWING 143A0060, SHEET 46, REV -.
- [SDR SWAA2026011241662](https://openairdocs.org/sdr/SWAA2026011241662), Dec 1, 2025: FLOORBEAM. CRACKED. CRACKED FLOORBEAM, BS 540, BL 0 TO RBL 24.75. REPLACED FLOORBEAM IAW SRM 51-10-02, PARAGRAPH 9, AND DRAWING 143A0060, SHEET 46, REV -.
- [SDR SWAA2026011241668](https://openairdocs.org/sdr/SWAA2026011241668), Dec 1, 2025: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 695, RBL 24.75. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, AND DWG 111A6000, SHEET, 246, REV-.
- [SDR SWAA2026011241663](https://openairdocs.org/sdr/SWAA2026011241663), Dec 1, 2025: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 695, BL 0. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, AND DWG 271A9110, SHEET 6, REV A.
- [SDR SWAA2026010941384](https://openairdocs.org/sdr/SWAA2026010941384), Dec 1, 2025: STUB FRAME. CRACKED. CRACK INDICATION ON STUB FRAME LOCATED BETWEEN BS 294.5 TO BS 296.5, BTW S8 - 9R AT FWD GALLEY DOOR AREA. REPLACED THE STUB FRAME BETWEEN BS 294.5 - 296.5, BTW 
- [SDR SWAA2026010941667](https://openairdocs.org/sdr/SWAA2026010941667), Dec 1, 2025: GUSSET. CRACKED. CRACKED GUSSET, BS 500D, S19R IN THE FWD CARGO BAY. REPLACED GUSSET BS 500D S19R IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02, AND DWG 143A7902, SHEET 174, REV -
- [SDR SWAA2026010940918](https://openairdocs.org/sdr/SWAA2026010940918), Nov 30, 2025: LIGHT. DETERIORATED. DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING ON ALONG PASSENGER CABIN. REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN IAW AMM 3
- [SDR SWAA2026010948328](https://openairdocs.org/sdr/SWAA2026010948328), Nov 30, 2025: PRESSURE DECK. CRACKED. CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB, LBL 30, BS 663. PERFORMED PERMANENT REPAIR ON PRESSURE DECK WEB, BS 663.75 - 675, LBL 25 - 60 IN THE MAIN WHEE
- [SDR SWAA2026010740916](https://openairdocs.org/sdr/SWAA2026010740916), Nov 30, 2025: PRESSURE DECK. CRACKED. CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB LBL 30 STA 663 AT PASSENGER CABIN. CRACK LENGTH 0.200 INCH.
- [SDR SWAA2026010940625](https://openairdocs.org/sdr/SWAA2026010940625), Nov 29, 2025: SCUFF PLATE. CRACKED. CRACK CENTER SCUFF PLATE AT FWD CARGO BAY. REPAIRED CENTER SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1.
- [SDR SWAA2026010940624](https://openairdocs.org/sdr/SWAA2026010940624), Nov 29, 2025: SCUFF PLATE. CRACKED. CRACKED CENTER SCUFF PLATE IN THE AFT CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1.
- [SDR SWAA2026010940622](https://openairdocs.org/sdr/SWAA2026010940622), Nov 28, 2025: SCUFF PLATE. CRACKED. CRACKED SCUFF PLATE ON FWD CORNER OF AFT CARGO DOOR CUTOUT. REPAIRED SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1.
- [SDR SWAA2025050565629](https://openairdocs.org/sdr/SWAA2025050565629), Apr 30, 2025: FLOOR PANEL. CORRODED. CORROSION FOUND ON AFT LAV THRESHOLD COMPISITE FLOOR.<[01] C/W EA 25-124-01104;[02] CORRECTED FOR C/W EA 25-125-01104
- [SDR SWAA2025032608826](https://openairdocs.org/sdr/SWAA2025032608826), Mar 24, 2025: SIGN. MISSING. EMERGENCY EXIT SIGN MID CABIN IS MISSING<[01] FOUND AND RE-INSTALLED MID CABIN OVERHEAD EMERGENCY EXIT DIRECTIONAL SIGN COVERS AS NEEDED REF AMM 33-51-03
- [SDR SWAA2025021997634](https://openairdocs.org/sdr/SWAA2025021997634), Feb 19, 2025: SIGN. DETACHED. AFT GALLEY (RT SIDE) EXIT SIGN FELL OFF<[01] REMOVED AND REPLACED AFT RH SERVICE DOOR EXIT SIGN LIGHT ASSY IAW AMM 33-51-01.
- [SDR SWAA2024100844998](https://openairdocs.org/sdr/SWAA2024100844998), Oct 4, 2024: HOOK AND LOOP. DETACHED. AFT SERVICE DOOR SLIDE (R2) HOOK AND LOOP STRIPS ON THE GIRT ARE NOT ATTACHED TO HOOK AND LOOP STRIPS ON THE BACKING PAN SHELF<[01] RESECURED AFT SERVICE DOOR (
- [SDR SWAA2024100845000](https://openairdocs.org/sdr/SWAA2024100845000), Oct 4, 2024: HOOK AND LOOP. DETACHED. FWD ENTRY DOOR SLIDE (L1) HOOK AND LOOP STRIPS ON THE GIRT ARE NOT ATTACHED TO HOOK AND LOOP STRIPS ON THE BACKING PAN SHELF<[01] RESECURED FWD ENTRY DOOR SLIDE
- [SDR SWAA2024100845001](https://openairdocs.org/sdr/SWAA2024100845001), Oct 4, 2024: HOOK AND LOOP. DETACHED. AFT ENTRY DOOR SLIDE (L2) HOOK AND LOOP STRIPS ON THE GIRT ARE NOT ATTACHED TO HOOK AND LOOP STRIPS ON THE BACKING PAN SHELF<[01] RESECURED AFT ENTRY DOOR (L2) 
- [SDR SWAA2024072214201](https://openairdocs.org/sdr/SWAA2024072214201), Jul 19, 2024: BATTERY PACK. FAILED. EMERGENCY LIGHT BATTERY PACK AT LOCATION M1672 (AFT RIGHT) FAILED CAPACITY TEST<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT LOCATION M1672; OPS CH
- [SDR SWAA2024072214208](https://openairdocs.org/sdr/SWAA2024072214208), Jul 19, 2024: SLIDER. CRACKED. RIGHT HORIZONTAL STABILIZER UPPER AFT SLIDER CRACKED.<[01] R&R RIGHT HORIZONTAL STABILIZER UPPER AFT SLIDER. IAW SRM 51-40-02
- [SDR SWAA2024061299697](https://openairdocs.org/sdr/SWAA2024061299697), Jun 8, 2024: SEAT. OUT OF ADJUST. EXIT ROW SEAT 11B RECLINES AND SEAT 23F DOES NOT RECLINE. ADJUSTED 11B RECLINE PER SIP AND PERFORMED OPERATIONAL TEST OF 23F PER SIP. NO DEFECTS NOTED.
- [SDR SWAA2024042577954](https://openairdocs.org/sdr/SWAA2024042577954), Apr 22, 2024: COVER. MISSING. CREW REPORTS OVERWING EMERGENCY EXIT FLOOR SIGN COVER MISSING. INSTALLED OVERWING EMERGENCY EXIT FLOOR EXIT SIGN COVER PER AMM 33-51-01.
- [SDR SWAA2024022355266](https://openairdocs.org/sdr/SWAA2024022355266), Feb 23, 2024: TRAY. BROKEN. TRAY TABLE ROW 11ABC BROKEN<[01] SECURED TRAY TABLE ARM PER CMM 25-23-46
- [SDR SWAA2024011633608](https://openairdocs.org/sdr/SWAA2024011633608), Dec 19, 2023: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STAR 17R AT FWD GALLEY AREA 2023-756880<[01] REPLACED SUPPORT ANGLE LOCATED BTW BS 291.5 TO BS 
- [SDR SWAA2024011633609](https://openairdocs.org/sdr/SWAA2024011633609), Dec 19, 2023: TIE CLIP. CRACKED. CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA 2023-756881<[01] REPLACED TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B

All 293: https://openairdocs.org/aircraft/N241WN/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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