# N910WN: 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: 36618 - Year built: 2008 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 7, 2010 - Certificate issued: February 29, 2008 - Expires: October 31, 2029 - Mode S code: AC98AC - 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=910WN - Page: https://openairdocs.org/aircraft/N910WN From the FAA registry file of October 21, 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 N910WN. ## FAA accident and incident reports None matched to N910WN. ## Service difficulty reports (241, newest 50) As reported by operators and repair stations. - [SDR SWAA2026090142485](https://openairdocs.org/sdr/SWAA2026090142485), Aug 28, 2026: SEAT BACK. OUT OF ADJUST. PASSENGER SEAT AT 14F IS RECLINING INTO EMERGENCY EXIT. REPOSITIONED HYDROLOC STOP REF CMM 25-21-42 - [SDR SWAA2026071670216](https://openairdocs.org/sdr/SWAA2026071670216), Jul 12, 2026: GIRT BAR. STUCK. FWD SERVICE DOOR GIRT BAR RETAINER OUT OF PLACE AND STUCK. SECURED GIRT BAR RELEASE STOP ASSEMBLY ON FWD SERVICE DOOR PER AMM 25-66-01. OPS CK NML. - [SDR SWAA2026021168977](https://openairdocs.org/sdr/SWAA2026021168977), Feb 8, 2026: POTABLE WATER. ODOR. F/A STATED A FOUL WATER ODOR FROM AFT GALLEY COFFEE POT. RAMP DRAINED AND REFILLED WATER TANK IAW SIP. - [SDR SWAA2025112034436](https://openairdocs.org/sdr/SWAA2025112034436), Nov 12, 2025: ACCESS PANEL. CRACKED. CRACK ON ACCESS PANEL 344GB AT RT HORIZONTAL STABILIZER. REPLACED ACCESS PANEL 344GB IAW B737-700 AMM 27-31-00-200-801 STEP 7.D(6). - [SDR SWAA2025112031612](https://openairdocs.org/sdr/SWAA2025112031612), Nov 4, 2025: STRINGER. CORRODED. CORROSION ON STRINGER 28R BTW BS 360 - 380 ON BILGE AREA AT AFT ELECTRONIC COMPARTMENT DOOR. REPAIRED STRINGER 28R BTW BS 360 TO 380 ON BILGE AREA AT AFT ELECTR - [SDR SWAA2025111929796](https://openairdocs.org/sdr/SWAA2025111929796), Oct 29, 2025: SCUFF PLATE. CRACKED. CRACK ON SCUFF PLATE FWD SERVICE DOOR. REPAIRED THE CENTER SCUFF PLATE FWD SERVICE DOOR IAW SRM 53-10-15-2R-2 REPAIR 2. PARAGRAPH 4. B; FIGURE 203. REFER TO BAC - [SDR SWAA2025112027617](https://openairdocs.org/sdr/SWAA2025112027617), Oct 24, 2025: VAPOR BARRIER. CRACKED. CRACK (6) ON VAPOR BARRIER WEB LOCATED AT BS 663.75 AND BTW RBL 25 TO RBL 35 MAIN WHEEL WELL COMPARTMENT. REPAIRED VAPOR BARRIER WEB LOCATED AT BS 663.75 AND BT - [SDR SWAA2025112027611](https://openairdocs.org/sdr/SWAA2025112027611), Oct 23, 2025: TEE ANGLE. CRACKED. CRACK ON TEE ANGLE LOCATED ON BS 663.75 RBL 25 MAIN WHEEL WELL COMPARTMENT. REPAIRED THE TEE ANGLE LOCATED ON BS 663.75, RBL 25 MAIN WHEEL WELL COMPARTMENT IAW - [SDR SWAA2025112027149](https://openairdocs.org/sdr/SWAA2025112027149), Oct 23, 2025: VAPOR BARRIER. CRACKED. CRACK (3) ON VAPOR BARRIER WEB LOCATED AT BS 663.75 AND BTW RBL 25 TO RBL 35 MAIN WHEEL WELL COMPARTMENT. REPAIRED VAPOR BARRIER WEB LOCATED AT BS 663.75 AND BT - [SDR SWAA2025112027147](https://openairdocs.org/sdr/SWAA2025112027147), Oct 23, 2025: VAPOR BARRIER. CRACKED. CRACK (4) ON VAPOR BARRIER WEB LOCATED AT BS 663.75 AND BTW RBL 25 TO RBL 35 MAIN WHEEL WELL COMPARTMENT. REPAIRED VAPOR BARRIER WEB LOCATED AT BS 663.75 AND BT - [SDR SWAA2025112027148](https://openairdocs.org/sdr/SWAA2025112027148), Oct 23, 2025: VAPOR BARRIER. CRACKED. CRACK (5) ON VAPOR BARRIER WEB LOCATED AT BS 663.75 AND BTW RBL 25 TO RBL 35 MAIN WHEEL WELL COMPARTMENT. REPAIRED VAPOR BARRIER WEB LOCATED AT BS 663.75 AND BT - [SDR SWAA2025111927146](https://openairdocs.org/sdr/SWAA2025111927146), Oct 23, 2025: VAPOR BARRIER. CRACKED. TWO CRACK ON VAPOR BARRIER WEB LOCATED AT BS 663.75 AND BTW RBL 25 TO RBL 35 MAIN WHEEL WELL COMPARTMENT REPAIRED VAPOR BARRIER WEB LOCATED AT BS 663.75 AND BTW - [SDR SWAA2025112026659](https://openairdocs.org/sdr/SWAA2025112026659), Oct 22, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 561CB AT LT WING. REPAIRED ACCESS PANEL 561CB AT LT WING IAW SRM 51-70-04-2R-10 REPAIR 10. - [SDR SWAA2025112026657](https://openairdocs.org/sdr/SWAA2025112026657), Oct 22, 2025: ACCESS PANEL. ELONGATED. ELONGATE HOLES ON ACCESS PANEL 561AB LT WING. REPAIRED ACCESS PANEL 561AB LT WING IAW SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] TASK CO - [SDR SWAA2025112026658](https://openairdocs.org/sdr/SWAA2025112026658), Oct 22, 2025: ACCESS PANEL. ELONGATED. ELONGATE HOLES ON ACCESS PANEL 561BB AT LT WING. REPAIRED ACCESS PANEL 561BB AT LT WING IAW SRM 51-70-04-2R-10 REPAIR 10. MAJOR REPAIR. - [SDR SWAA2025112026654](https://openairdocs.org/sdr/SWAA2025112026654), Oct 22, 2025: ACCESS PANEL. ELONGATED. ELONGATE HOLES ON ACCESS PANEL 561AB LT WING. FAULT RESOLVED ON OTHER FAULT; SEE TTG8Q015VWDA. - [SDR SWAA2025111927142](https://openairdocs.org/sdr/SWAA2025111927142), Oct 22, 2025: LENS. BROKEN. BROKEN LENS EMERGENCY EXIT LIGHT (WITH ARROW) AT EMERGENCY EXIT HATCH RH SIDE PASSENGER CABIN (1EA) 2025-636395<[01] REPLACED LENS EMERGENCY EXIT LIGHT (WITH AR - [SDR SWAA2025111926652](https://openairdocs.org/sdr/SWAA2025111926652), Oct 21, 2025: BATTERY PACK. INOPERATIVE. INOPERATIVE BATTERY PACK EMERGENCY EXIT DOOR LT AND RT SIDE PASSENGER CABIN. REPLACED BATTERY PACK EMERGENCY EXIT DOOR LT AND RT SIDE PASSENGER CABIN (2EA) IAW - [SDR SWAA2025112025725](https://openairdocs.org/sdr/SWAA2025112025725), Oct 19, 2025: PLATE. CRACKED. CRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE IRSS216 AT RT WING. REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE IRSS216 AT RT WING. IAW B737-700 SRM 51-10-0 - [SDR SWAA2025112025727](https://openairdocs.org/sdr/SWAA2025112025727), Oct 19, 2025: PLATE. CRACKED. CRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE IRSS216 AT LT WING. REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE IRSS216 AT LT WING IAW SRM 51-40-02 SRM 51-1 - [SDR SWAA2025112025843](https://openairdocs.org/sdr/SWAA2025112025843), Oct 19, 2025: ANGLE. CRACKED. CRACKED ANGLE, BS 420, RBL 24 IN THE FWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02-OG-0, SRM 51-10-02-0G-0, ITEM 9, AND DWG 143A7505, SHEET 8 - [SDR SWAA2025112025842](https://openairdocs.org/sdr/SWAA2025112025842), Oct 19, 2025: ANGLE. CRACKED. CRACK ANGLE, LOCATED BS 440, LBL 24 AT FWD CARGO COMPARTMENT. REPLACED THE ANGLE AND FASTENERS LOCATED BS 440 LBL 24 AT FWD CARGO BAY IAW SRM 51-40-02-0G-0, SRM - [SDR SWAA2025111925841](https://openairdocs.org/sdr/SWAA2025111925841), Oct 19, 2025: WEB. CORRODED. CRACK WEB - INTERCOSTAL LOCATED BTW BS 460 - 480, LBL 24 IN THE FWD CARGO BAY. REPLACED WEB - INTERCOSTAL IAW SRM 51-40-02-0G, DWG 143A7510, SHEET 3, REV B, AND - [SDR SWAA2025111925840](https://openairdocs.org/sdr/SWAA2025111925840), Oct 19, 2025: WEB. CORRODED. CORROSION WEB SHIELD LOCATED BTW BS 492 - 500A, RBL 24, WL156 IN THE FWD CARGO BAY. REPLACED WEB SHIELD AND FASTENERS IAW SRM 51-40-02-0G-0, 51-10-02, ITEM 9, D - [SDR SWAA2025111925844](https://openairdocs.org/sdr/SWAA2025111925844), Oct 19, 2025: WEB. CORRODED. CORROSION WEB SHIELD LOCATED BTW BS420 - 440, RBL 24 AND WL 156 IN THE FWD CARGO BAY. REPLACED WEB SHIELD AND FASTENERS LOCATED IAW SRM 51-40-02-0G-0, 51-10-02, - [SDR SWAA2025111925847](https://openairdocs.org/sdr/SWAA2025111925847), Oct 19, 2025: GLOWSTRIP. DETERIORATED. DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA). REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) - [SDR SWAA2025111925722](https://openairdocs.org/sdr/SWAA2025111925722), Oct 19, 2025: NUT PLATE. CORRODED. CORROSION ON RAIL NUT PLATES LOCATED INTERNAL CAVITY LEADING EDGE OFSS706 AT LT WING. REPLACED RAIL ON NUT PLATES (GANG CHANNEL) LOCATED INTERNAL CAVITY LEADING - [SDR SWAA2025112025574](https://openairdocs.org/sdr/SWAA2025112025574), Oct 18, 2025: SUPPORT BRACKET. CRACKED. CRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN. REPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN - [SDR SWAA2025112025586](https://openairdocs.org/sdr/SWAA2025112025586), Oct 18, 2025: RIB. CRACKED. CRACK INSPAR RIB 120.30 LOCATED 19 INCHES FROM FRONT SPAR LT HORIZONTAL STAB. REPAIRED INSPAR RIB 120.30 LOCATED 19 INCHES FROM FRONT SPAR LT HORIZONTAL STAB IA - [SDR SWAA2025112025580](https://openairdocs.org/sdr/SWAA2025112025580), Oct 18, 2025: RIB. CRACKED. CRACKED INSPAR RIB 120.30 LOCATED 36 INCHES FROM FRONT SPAR LT HORIZONTAL STAB. REPAIRED INSPAR RIB 120.30 LOCATED 36 INCHES FROM FRONT SPAR LT HORIZONTAL STAB - [SDR SWAA2025111925577](https://openairdocs.org/sdr/SWAA2025111925577), Oct 18, 2025: WEB. CORRODED. CORROSION WEB SHIELD LOCATED BTW BS 847 - 867, RBL 22, WL 156. REPLACED WEB SHIELD IAW SRM 51-10-02-0G-0, ITEM 9, DWG 146A0081, SHEET 37, REV-. - [SDR SWAA2025111925572](https://openairdocs.org/sdr/SWAA2025111925572), Oct 18, 2025: NUT PLATE. CRACKED. CRACK ON RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS569 AT RT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS569 AT RT WI - [SDR SWAA2025111925358](https://openairdocs.org/sdr/SWAA2025111925358), Oct 17, 2025: SUPPORT ANGLE. CORRODED. CORRODED SUPPORT ANGLE BETWEEN BS 767 - 787, RBL 22, WL 156, AFT CARGO BAY. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-10-02-0G-0, ITEM 9, DWG 146A8123 - [SDR SWAA2025111925359](https://openairdocs.org/sdr/SWAA2025111925359), Oct 17, 2025: WEB. CORRODED. CORROSION WEB SHIELD LOCATED BTW BS 787 - 794, RBL 22, WL 156. REPLACED NEW WEB SHIELD AND FASTENERS IAW SRM 51-40-02-0G-0, & DWG 146A0081, SHEET 37, REV -. - [SDR SWAA2025111925356](https://openairdocs.org/sdr/SWAA2025111925356), Oct 17, 2025: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BTW BS 727A TO BS 767 RBL22 AND WL156 AT AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE LOCATED BTW BS727 TO BS767 RBL22 AND WL156 AT - [SDR SWAA2025111925352](https://openairdocs.org/sdr/SWAA2025111925352), Oct 17, 2025: ANGLE. CRACKED. CRACK ANGLE ON ACCESS PANEL 551FB TRAILING EDGE AT LT WING. MEASUREMENT OF CRACK IS L: 0.300 INCHES. REPLACED THE ANGLE ON ACCESS PANEL 551FB TRAILING EDGE AT L - [SDR SWAA2025111925353](https://openairdocs.org/sdr/SWAA2025111925353), Oct 17, 2025: ANGLE. CRACKED. CRACK ANGLE ON ACCESS PANEL 651GB TRAILING EDGE AT RT WING. MEASUREMENT OF CRACK IS L:0.300 INCHES. REPLACED ANGLE ON ACCESS PANEL 651GB TRAILING EDGE AT RT WIN - [SDR SWAA2025111925354](https://openairdocs.org/sdr/SWAA2025111925354), Oct 17, 2025: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET ON ACCESS PANEL 651FB AT RT WING. MEASUREMENT OF CRACK IS L: 0.500 INCHES. REPLACED SUPPORT BRACKET ON ACCESS PANEL 651FB AT RT WING IAW S - [SDR SWAA2025111825355](https://openairdocs.org/sdr/SWAA2025111825355), Oct 17, 2025: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BTW BS 727A - 847, LBL 22, WL 156 AFT CARGO. REPAIRED SUPPORT ZEE IAW SRM 53-00-53-2R-6, REPAIR 6, & INSTALLED THE SUPPORT ZEE AND - [SDR SWAA2025111825357](https://openairdocs.org/sdr/SWAA2025111825357), Oct 17, 2025: INTERCOSTAL. CORRODED. CORROSION WEB - INTERCOSTAL LOCATED BTW BS747 TO BS767 RBL22 AND WL156 AT AFT CARGO COMPARTMENT 2025-636043 <[01]. REPLACED WEB - INTERCOSTAL LOCATED BTW BS747 - [SDR SWAA2025111924965](https://openairdocs.org/sdr/SWAA2025111924965), Oct 16, 2025: ANGLE. CRACKED. CRACKED SLAT 1 INBD AUXILIARY TRACK OTBD ANGLE AT LT WING. REPLACED SLAT 1 INBD AUXILIARY TRACK OTBD ANGLE IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, AND - [SDR SWAA2025111924966](https://openairdocs.org/sdr/SWAA2025111924966), Oct 16, 2025: ANGLE. CRACKED. CRACK SLAT 6 INBD AUXILIARY TRACK INBD ANGLE AT RT WING. REPLACED ANGLE LOCATED ON SLAT 6 INBD AUXILIARY TRACK INBD SIDE AT RT WING IAW SRM 51-10-02-0G-0, ITEM - [SDR SWAA2025111924786](https://openairdocs.org/sdr/SWAA2025111924786), Oct 16, 2025: SCUFF PLATE. CRACKED. CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT. REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 53-60-15-2R-1 REPAIR 1, PARA - [SDR SWAA2025111924967](https://openairdocs.org/sdr/SWAA2025111924967), Oct 16, 2025: SLAT TRACK. CRACKED. CRACK SLAT 3 INBD AUXILIARY TRACK I/B ANGLE AT LT WING. REPLACED SLAT 3 INBD AUXILIARY TRACK INBD ANGLE AT LT WING IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0 - [SDR SWAA2025111925076](https://openairdocs.org/sdr/SWAA2025111925076), Oct 16, 2025: TIE CLIP. CRACKED. CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA. REPLACED TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA. IAW SRM 51-10-02-0G- - [SDR SWAA2025111925080](https://openairdocs.org/sdr/SWAA2025111925080), Oct 16, 2025: STUB FRAME. CRACKED. CRACK ON STUB FRAME LOCATED BTW BS 294.5 TO BS 296.5 BTW STR 8R TO STR 9R AT FWD GALLEY AREA. REPLACED STUB FRAME LOCATED BTW BS 294.5 TO BS 296.5 BTW STR 8R TO - [SDR SWAA2025111931677](https://openairdocs.org/sdr/SWAA2025111931677), Oct 15, 2025: SUPPORT BRACKET. CORRODED. CORROSION REAR SPAR FUEL BOOST PUMP UPPER BONDING JUMPER SUPPORT BRACKET AT LT WING. R & R THE UPPER BONDING JUMPER AND UPPER BONDING CLIP OF THE AFT FUEL BOOST - [SDR SWAA2025111924775](https://openairdocs.org/sdr/SWAA2025111924775), Oct 15, 2025: ACCESS PANEL. CRACKED. CRACK ACCESS PANEL 561AB TRAILING EDGE AROUND HOLES LT WING. REPAIRED ACCESS PANEL 561AB TRAILING EDGE LT WING IAW SRM 51-70-04-2R-10 REPAIR 10. - [SDR SWAA2025111924776](https://openairdocs.org/sdr/SWAA2025111924776), Oct 15, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 661BB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661BB TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10. - [SDR SWAA2025111924777](https://openairdocs.org/sdr/SWAA2025111924777), Oct 15, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 661CB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661CB TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10. All 241: https://openairdocs.org/aircraft/N910WN/reports.md ## Related - Other Boeing 737-7H4 aircraft: https://openairdocs.org/model/boeing-737-7h4/aircraft.md - STCs for the Boeing 737-7H4: https://openairdocs.org/model/boeing-737-7h4/stcs.md - The CFM International CFM56-7B24 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.