# N262WN: 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: 32519 - Year built: 2006 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 20, 2006 - Certificate issued: January 31, 2007 - Expires: June 30, 2029 - Mode S code: A2886C - 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=262WN - Page: https://openairdocs.org/aircraft/N262WN 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 N262WN. ## FAA accident and incident reports None matched to N262WN. ## Service difficulty reports (272, newest 50) As reported by operators and repair stations. - [SDR SWAA2026061612672](https://openairdocs.org/sdr/SWAA2026061612672), Jun 16, 2026: BATTERY PACK. NO TEST. THE AFT LT EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. REMOVED AND REPLACED THE BATTERY PACK IAW MM 33-51-06. - [SDR SWAA2026030274904](https://openairdocs.org/sdr/SWAA2026030274904), Feb 27, 2026: COVER. DAMAGED. AFT L2 ENTRY DOOR SLIDE COVER TRIM MISSING AT AFT END. REPLACED AFT L2 ENTRY DOOR SLIDE COVER TRIM, AFT END IAW AMM 25-66-00. - [SDR SWAA2025110330559](https://openairdocs.org/sdr/SWAA2025110330559), Oct 31, 2025: FAN. ODOR. ODOR IN CABIN WITH CONDITIONED AIR HOOKED UP. TROUBLESHOT AND FOUND RECIRC FAN INOPERATIVE. OK TO CONTINUE PER MEL MEL 21-31-02. REMOVED & REPLACED THE RECIRC F - [SDR SWAA2025100320417](https://openairdocs.org/sdr/SWAA2025100320417), Oct 2, 2025: BATTERY PACK. FAILED. AFT R/H EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK.. REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06. - [SDR SWAA2025082105520](https://openairdocs.org/sdr/SWAA2025082105520), Aug 18, 2025: VAPOR BARRIER. CRACKED. FOUND EIGHT CRACKS ON AFT SIDE OF VAPOR BARRIER IN WHEEL WELL FORWARD SIDE, RBL 32 TO RBL 37, WL 154. SEE TTG8Q014MD18 FOR WORK PERFORMED. - [SDR SWAA2025082105521](https://openairdocs.org/sdr/SWAA2025082105521), Aug 18, 2025: VAPOR BARRIER. CRACKED. FOUND THREE CRACKS ON AFT SIDE OF VAPOR BARRIER. RBL 45 TO RBL 48, WL 157. SEE TTG8Q014MD0A FOR WORK PERFORMED. - [SDR SWAA2025072393265](https://openairdocs.org/sdr/SWAA2025072393265), Jul 20, 2025: SIGN. DETACHED. RIGHT SIDE OVER WING EMERGENCY EXIT SIGN HAS COME OFF. RESECURED RT OVER WING EMERGENCY EXIT SIGN PER AMM 33-51-01. - [SDR SWAA2025010883944](https://openairdocs.org/sdr/SWAA2025010883944), Jan 8, 2025: BATTERY PACK. NO TEST. PASSENGER CABIN; BATTERY PACK M1675 FAILED CAPACITY TEST.<[01] R&R BATTERY PACK M1675 IAW AMM 33-51-06. - [SDR SWAA2024111960642](https://openairdocs.org/sdr/SWAA2024111960642), Nov 16, 2024: APU. SHUTDOWN. APU AUTO SHUTDOWN IN CRUISE AND WOULD NOT COME BACK ONLINE 11/12-SMOKE COMING FROM TAILPIPE-REPLACED OIL COOLER 11/8-SERVICED APU GEARBOX OPS CHECKED OK 11/2-RE - [SDR SWAA2024110656041](https://openairdocs.org/sdr/SWAA2024110656041), Nov 2, 2024: APU. SMOKE. APU BLOWING BLACK SMOKE OUT OF EXHAUST<[01] WORKING MEL 49-1-01 SP #1 FROM THIS L/P 2803726. PERFORMED FIM 49-55 TASK 801. OPS CK GOOD. NO SMOKE NOTICED FROM AP - [SDR SWAA2024082627810](https://openairdocs.org/sdr/SWAA2024082627810), Aug 19, 2024: SLIDE. OUT OF POSITION. CUSTOMER REQUEST PAX CABIN AFT LEFT AND RIGHT DOORS SLIDES RUBBING AGAINST TO SCUFF PLATE STRUCTURE TO CLOSE POSITION 2024-421164<[01] CORRECTED INSTALLED PAX C - [SDR SWAA2024082622737](https://openairdocs.org/sdr/SWAA2024082622737), Aug 5, 2024: GATE. CRACKED. CRACK LOWER ENDGATE FWD SERVICE DOOR AT FWD GALLEY AREA 2024-421134<[01] REPLACED LOWER ENDGATE FWD SERVICE DOOR AT FWD GALLEY AREA IAW B737-700 AMM 52-41-61-40 - [SDR SWAA2024082615393](https://openairdocs.org/sdr/SWAA2024082615393), Jul 22, 2024: STRINGER. CRACKED. CRACK STRINGER U8 INTERNAL AREA FUEL TANK UPPER POSITION LOCATED BTW RIB 19 AND RIB 20 AT RT WING 2024-421114<[01] REPAIRED STRINGER U8 INTERNAL AREA FUEL TANK - [SDR SWAA2024082616255](https://openairdocs.org/sdr/SWAA2024082616255), Jul 15, 2024: BALANCE WEIGHT. OUT OF BALANCE. DURING WEIGHT AND BALANCE OF ELEVATOR LT P/N: 183A0103-21 FOUND BALANCE WEIGHTS P/N: 183A0210-15 (1EA) ON BAY 4; P/N: 183A0210-14 (1EA) ON BAY 3; P/N: 183A0210- - [SDR SWAA2024082612915](https://openairdocs.org/sdr/SWAA2024082612915), Jul 15, 2024: WEB. DAMAGED. ELONGATED HOLE LOCATED ON WEB LOWER AREA VAPOR BARRIER R/H SIDE RBL 6.15 AND RBL 31.83 2024-421088<[01] REPLACED WEB LOCATED LOWER AREA VAPOR BARRIER R/H SIDE R - [SDR SWAA2024082612914](https://openairdocs.org/sdr/SWAA2024082612914), Jul 15, 2024: BRACKET. CRACKED. CRACK BRACKET LOCATED ON VAPOR BARRIER R/H SIDE RBL 45 AND RBL 54.21 2024-421087<[01] REPLACED BRACKET LOCATED ON VAPOR BARRIER R/H SIDE RBL 45 AND RBL 54.21 IA - [SDR SWAA2024082612117](https://openairdocs.org/sdr/SWAA2024082612117), Jul 13, 2024: ANGLE. DAMAGED. ELONGATE HOLE ON Z ANGLE (2 EA) LOC. ON LH FWD ENTRY DOOR AT LEVEL LBL 53 PASSENGER CABIN 2024-421055<[01] REPLACED ON Z ANGLE (2 EA) LOC. ON LH FWD ENTRY DOOR - [SDR SWAA2024082612113](https://openairdocs.org/sdr/SWAA2024082612113), Jul 13, 2024: STUB FRAME. CRACKED. CRACK ON STUB FRAME LOCATED ON BS 294.5 LOCATED BTW STR S-8R TO S- 9R AT PASSENGER CABIN 2024-421058<[01] REPLACED STUB FRAME LOCATED ON BS 294.5 BETWEEN STR-7R - [SDR SWAA2024082612116](https://openairdocs.org/sdr/SWAA2024082612116), Jul 13, 2024: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE ORSS 272 AT RT WING 2024-421061<[01] REPLACED ANGLE TRAILING EDGE ORSS 272 AT RT WING
IAW B737-700 SRM 51-10-02 ITEM 9 AND B737-70 - [SDR SWAA2024082612119](https://openairdocs.org/sdr/SWAA2024082612119), Jul 13, 2024: SUPPORT. CORRODED. CORROSION AILERON FEEL AND CENTERING UNIT REACTION SUPPORT AT MAIN WHEEL WELL COMPARTMENT 2024-421064<[01] REPLACED AILERON FEEL AND CENTERING UNIT REACTION SUP - [SDR SWAA2024082611845](https://openairdocs.org/sdr/SWAA2024082611845), Jul 12, 2024: LENS. BROKEN. BROKEN EMERGENCY LIGHT LENS GALLEY 4 AT AFT GALLEY AREA (1EA) 2024-421050<[01] REPLACED EMERGENCY LIGHT LENS GALLEY 4 AT AFT GALLEY AREA IAW B737-700 AMM 33-51- - [SDR SWAA2024082612112](https://openairdocs.org/sdr/SWAA2024082612112), Jul 12, 2024: BRACKET. CRACKED. CRACK BRACKET LOCATED BS540 PLUS 8INCH AND RBL10 AT AIR CONDITIONING BAY 2024-421054<[01] REPLACED BRACKET LOCATED BS540 PLUS 8INCH AND RBL10 AT AIR CONDITIONIN - [SDR SWAA2024082611503](https://openairdocs.org/sdr/SWAA2024082611503), Jul 11, 2024: ANGLE. CRACKED. CRACK ANGLE ON ACCESS PANEL 651FB TRAILING EDGE AT RT WING 2024-421002<[01] REPLACED ANGLE ON ACCESS PANEL 651FB TRAILING EDGE AT RT WING IAW B737-700 SRM 51-10 - [SDR SWAA2024082610796](https://openairdocs.org/sdr/SWAA2024082610796), Jul 9, 2024: SHIELD. CORRODED. CORROSION ON SHIELD WEB LOCATED BTW BS 480 TO BS 500 AT LEVEL STR 26R WL 156.1 AT FWD CARGO COMPARTMENT 2024-420944<[01] REPLACED SHIELD WEB LOCATED BTW BS 480 - [SDR SWAA2024082610959](https://openairdocs.org/sdr/SWAA2024082610959), Jul 9, 2024: LENS. BROKEN. BROKEN LENS ASSY EMERGENCY LIGHT IN LAVATORY B AT AFT GALLEY AREA 2024-420973<[01] REPLACED LENS ASSY EMERGENCY LIGHT IN LAVATORY B AT AFT GALLEY AREA IAW B737- - [SDR SWAA2024082610957](https://openairdocs.org/sdr/SWAA2024082610957), Jul 9, 2024: STRINGER. CORRODED. CORROSION ON STRINGER 23L LOCATED BS 540 WL 155 FWD CARGO COMPARTMENT 2024-420954<[01] ON STEP 9; EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; DUE - [SDR SWAA2024082610793](https://openairdocs.org/sdr/SWAA2024082610793), Jul 9, 2024: ANGLE. CRACKED. CRACK GUSSET ANGLE LOATED BS 500D AT LEVEL STR 19L AT FWD CARGO COMPARTMENT 2024-420924<[01] REPLACED GUSSET ANGLE AND FASTENERS LOC. BS 500D AT LEVEL STR 19L A - [SDR SWAA2024082610789](https://openairdocs.org/sdr/SWAA2024082610789), Jul 9, 2024: ANGLE. CRACKED. CRACK GUSSET ANGLE LOCATED BS 500D AT LEVEL STR 19R AT FWD CARGO COMPARTMENT 2024-420931<[01] REPLACED GUSSET ANGLE AND FASTENERS LOC. BS 500D AT LEVEL STR 19R - [SDR SWAA2024082610955](https://openairdocs.org/sdr/SWAA2024082610955), Jul 9, 2024: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED FWD FACE BS 500C AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2024-420951<[01] REPLACED SUPPORT ANGLE LOCATED FWD FACE BS 500C AT LE - [SDR SWAA2024082610958](https://openairdocs.org/sdr/SWAA2024082610958), Jul 9, 2024: SUPPORT BRACKET. CRACKED. CRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2024-420955<[01] REPLACED SUPPORT BRACKET AND FASTENERS LOCATED BS 867 BTW STR 2 - [SDR SWAA2024082610551](https://openairdocs.org/sdr/SWAA2024082610551), Jul 8, 2024: STRAP. CORRODED. CORROSION STRAP LOCATED BTW BS 767 TO BS 787 AND BTW RBL13.84 TO LBL 17.24 WL 156.1 AT AFT CARGO COMPARTMENT 2024-420866<[01] REPLACED STRAP LOCATED BTW BS 767 - [SDR SWAA2024082610347](https://openairdocs.org/sdr/SWAA2024082610347), Jul 8, 2024: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BTW BS 907 TO BS 927 AND BTW STR 25R TO STR 26R AFT POSITION AT AFT CARGO COMPARTMENT 2024-40848<[01] REPLACED SUPPORT ANGLE AND - [SDR SWAA2024082610356](https://openairdocs.org/sdr/SWAA2024082610356), Jul 8, 2024: SUPPORT BRACKET. CRACKED. CRACK ON SPPORT BRACKET LOCATED PARTITION BS 727 BTW RBL 3 TO LBL 3 AT AFT CARGO COMPARTMENT 2024-420863<[01] REPLACED SUPPORT BRACKET LOCATED PARTITION BS 727 - [SDR SWAA2024082610555](https://openairdocs.org/sdr/SWAA2024082610555), Jul 8, 2024: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BS 727 PLUS 4 INCHES BTW STR 25R TO STR 25L AT AFT CARGO COMPARTMENT 2024-420885<[01] REPLACED SUPPORT ANGLE LOCATED BS 727 PLUS - [SDR SWAA2024082610556](https://openairdocs.org/sdr/SWAA2024082610556), Jul 8, 2024: SUPPORT ANGLE. CRACKED. CRACK INTERNAL STRUCTURE SUPPORT ANGLE LOCATED CEILING AREA BTW BS 847 TO BS 867 AT RBL 46 AT AFT CARGO COMPARTMENT 2024-420888<[01] REPLACED SUPPORT ANGLE LOCA - [SDR SWAA2024082610354](https://openairdocs.org/sdr/SWAA2024082610354), Jul 8, 2024: CARGO TRACK. CRACKED. CRACK ON TRACK LBL 17.24 LOCATED BS 767 AT AFT CARGO COMPARTMENT 2024-420861<[01] TOOL USED STEP 4 AND 5 EDDY CURRENT EQUIPMENT PN: NORTEC 600D SN: 220272712 DU - [SDR SWAA2024082610350](https://openairdocs.org/sdr/SWAA2024082610350), Jul 8, 2024: CARGO TRACK. CRACKED. CRACK ON TRACK RBL 13.84 LOCATED BS 767 AT AFT CARGO COMPARTMENT 2024-420850<[01] REFER TO FAULT TTG8Q00UEXZZ WHERE EA 24-153-02050 WAS ADDED AS A SUBTASK.;[02] - [SDR SWAA2024082610348](https://openairdocs.org/sdr/SWAA2024082610348), Jul 8, 2024: CARGO TRACK. CRACKED. CRACK ON TRACK RBL 13.84 LOCATED BS 747 AT AFT CARGO COMPARTMENT 2024-420852<[01] 'REFER TO FAULT TTG8Q00UEXZZ WHERE EA 24-153-02050 WAS ADDED AS A SUBTASK.';[0 - [SDR SWAA2024082610351](https://openairdocs.org/sdr/SWAA2024082610351), Jul 8, 2024: CARGO TRACK. CRACKED. CRACK ON TRACK RBL 13.84 LOCATED BS 727C AT AFT CARGO COMPARTMENT 2024-420855<[01] EQUIPMENT USED P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 08-JAN-25;[02] ON - [SDR SWAA2024082610349](https://openairdocs.org/sdr/SWAA2024082610349), Jul 8, 2024: CARGO TRACK. CRACKED. CRACK ON TRACK RBL 13.84 LOCATED BS 727E AT AFT CARGO COMPARTMENT 2024-420853<[01] REFER TO FAULT TTG8Q00UEXZZ WHERE EA 24-153-02050 WAS ADDED AS A SUBTASK.;[02 - [SDR SWAA2024082610346](https://openairdocs.org/sdr/SWAA2024082610346), Jul 8, 2024: FITTING. CRACKED. CRACK ON FITTING LOCATED BS 947.5 AT LEVEL STR 25L AT AFT CARGO COMPARTMENT 2024-20847<[01] REPLACED FITTING AND FASTENERS LOCATED BS 947.5 AT LEVEL STR 25L AT - [SDR SWAA2024082610227](https://openairdocs.org/sdr/SWAA2024082610227), Jul 7, 2024: STUB FRAME. CRACKED. CRACK ON STUB FRAME LOCATED BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2024-420826<[01] TOOL USED ON STEP 5 AND 6: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/ - [SDR SWAA2024082610109](https://openairdocs.org/sdr/SWAA2024082610109), Jul 7, 2024: TIE CLIP. CRACKED. CRACK ON TIE CLIP LOCATED 277 AT LEVEL STR 10R AT FWD GALLEY AREA 2024-420817<[01] REPLACED TIE CLIP LOC. BS277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B737-700 - [SDR SWAA2024082610108](https://openairdocs.org/sdr/SWAA2024082610108), Jul 7, 2024: INTERCOSTAL. CRACKED. CRACK ON INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA 2024-420815<[01] REPLACED INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 - [SDR SWAA2024082610106](https://openairdocs.org/sdr/SWAA2024082610106), Jul 7, 2024: FRAME. CRACKED. CRACK ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA 2024-420816<[01] REPAIRED FRAME LOCATED STA 312 BTW STR5L TO STR6L FWD GALLEY AREA IAW EA - [SDR SWAA2024082609962](https://openairdocs.org/sdr/SWAA2024082609962), Jul 6, 2024: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED FLOOR STRUCTURE BTW BS 380 TO BS 400 BL 0 WL 208.1 AT PASSENGER CABIN 2024-420799<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCAT - [SDR SWAA2024082609964](https://openairdocs.org/sdr/SWAA2024082609964), Jul 6, 2024: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED FLOOR STRUCTURE BTW BS 380 TO BS 400 LBL 13 WL 208.1 AT PASSENGER CABIN 2024-420801<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOC - [SDR SWAA2024082609963](https://openairdocs.org/sdr/SWAA2024082609963), Jul 6, 2024: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED FLOOR STRUCTURE BTW BS 380 TO BS 400 RBL 10 WL 208.1 AT PASSENGER CABIN 2024-420802<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOC - [SDR SWAA2024082609805](https://openairdocs.org/sdr/SWAA2024082609805), Jul 6, 2024: BEAR STRAP. CRACKED. CRACK INDICATION ON BEAR STRAP FORWARD GALLEY DOOR BS 290-296 BETWEEN S-8R AND S-9R AT PASSENGER CABIN (1E/A). CRACK LENGTH APPROX. 0.125 INCH 2024-420774<[01] - [SDR SWAA2024082609807](https://openairdocs.org/sdr/SWAA2024082609807), Jul 6, 2024: FLOORBEAM. CORRODED. CORROSION ON FLOOR BEAM LOCATED BS 986.5 LBL 43 WL 208.1 AT AFT GALLEY AREA 2024-420778<[01] FLOR BEAM UPPER SURFACE LOCATED BS 986.5 LBL43 AFT GALEY AREA MUST All 272: https://openairdocs.org/aircraft/N262WN/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.