# N269WN: 2007 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: 32526 - Year built: 2007 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 7, 2007 - Certificate issued: April 12, 2007 - Expires: March 31, 2030 - Mode S code: A2A26D - 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=269WN - Page: https://openairdocs.org/aircraft/N269WN 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 N269WN. ## FAA accident and incident reports None matched to N269WN. ## 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 SWAA2026092132599](https://openairdocs.org/sdr/SWAA2026092132599), Sep 15, 2026: BATTERY PACK. NO TEST. RIGHT FWD EMERGENCY LIGHT SYS BATTERY PACK FAILED A CAPACITY CHECK. REMOVED AND REPLACED THE BATTERY PACK IAW MM 33-51-06. - [SDR SWAA2026052606114](https://openairdocs.org/sdr/SWAA2026052606114), May 23, 2026: BATTERY. INOPERATIVE. FLIGHT ATTENDANT MEGAPHONE INOPERATIVE. REPLACED MEGAPHONE BATTERIES IAW AMM 25-64-00. - [SDR SWAA2026011961493](https://openairdocs.org/sdr/SWAA2026011961493), Jan 15, 2026: BATTERY PACK. NO TEST. BATTERY AT M1669 FAILED TIME CHECK. R & R THE BATTERY PACK AT M166 IAW AMM 33-51-06. - [SDR SWAA2026011961484](https://openairdocs.org/sdr/SWAA2026011961484), Jan 15, 2026: PANEL. PULLED. FOUR FASTENERS PULLED THROUGH LOWER WING PANEL OTBD OF NR 3 FLAP TRACK FAIRING ON LT WING. REMOVED AND REPLACED FASTENERS ON LOWER WING PANEL O/B #3 FLAP TRACK - [SDR SWAA2025041423542](https://openairdocs.org/sdr/SWAA2025041423542), Apr 11, 2025: ISOLATOR. CRACKED. FWD GALLEY DOOR AFT UPPER SLIDE MOUNT ISOLATOR CRACKED<[01] R&R FWD GALLEY DOOR AFT UPPER SLIDE MOUNT ISOLATOR IAW SRM 51-40-02.;[02] C/W - [SDR SWAA2025041423562](https://openairdocs.org/sdr/SWAA2025041423562), Apr 11, 2025: ISOLATOR. CRACKED. AFT ENTRY DOOR AFT UPPER SLIDE MOUNT ISOLATOR CRACKED<[01] R&R AFT ENTRY DOOR AFT UPPER SLIDE MOUNT ISOLATOR IAW SRM 51-40-02.;[02] C/W - [SDR SWAA2025041423561](https://openairdocs.org/sdr/SWAA2025041423561), Apr 11, 2025: SCREW. WORN. FWD SER DOOR HAS SEVERAL WORN SCREWS AND WORN SLIDE ATTACH HARDWARE BOLTS<[01] REPLACED WORN SCREWS AND HARDWARE BOLTS IAW AMM 52-41-00.;[02] C/W - [SDR SWAA2024120657274](https://openairdocs.org/sdr/SWAA2024120657274), Nov 6, 2024: ANGLE. CRACKED. CRACK ON ANGLE LOCATED AT LEVEL STR 8L AND BS 312 AT FWD GALLEY AREA 2024-633958<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DAT - [SDR SWAA2024120655811](https://openairdocs.org/sdr/SWAA2024120655811), Nov 2, 2024: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE ORSS 273 DEFLECTION CONTROL RIB AREA LT WING 2024-633747<[01] REPLACED ANGLE LOCATED ON TRAILING EDGE ORSS 273 DEFLECTION CONTROL RIB - [SDR SWAA2024120551490](https://openairdocs.org/sdr/SWAA2024120551490), Oct 22, 2024: RIB. CRACKED. CRACK INSPAR RIB 120.30 LOCATED 27 INCHES FROM EDGE REAR SPAR AT RT HORIZONTAL STABILIZER 2024-633926<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 60 - [SDR SWAA2024120551162](https://openairdocs.org/sdr/SWAA2024120551162), Oct 20, 2024: WEB. CRACKED. CRACK INDICATION (1E/A) FOUND ON HORIZONTAL WEB ON BS 294.5 AT LEVEL STR 17 R FWD GALLEY AREA 2024-633925<[01] REPLACED HORIZONTAL WEB LOC. BS 294.5 TO BS 332.1 - [SDR SWAA2024120671992](https://openairdocs.org/sdr/SWAA2024120671992), Oct 17, 2024: ANGLE. CRACKED. CRACK ON ANGLE OUTBOARD THRUST REVERSER LOCATED AFT UPPER POSITION ON ENGINE 1 2024-633879<[01] REPLACED ANGLE OUTBOARD THRUST REVERSER LOCATED AFT UPPER POSITI - [SDR SWAA2024120648420](https://openairdocs.org/sdr/SWAA2024120648420), Oct 14, 2024: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE IRSS 217 RT WING 2024-633807<[01] REPLACED CORRUGATED PLATE TRAILING EDGE IRSS 217 RT WING IAW B737-700 SRM 51-10-02 ITEM 9 - [SDR SWAA2024120648421](https://openairdocs.org/sdr/SWAA2024120648421), Oct 14, 2024: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE ACCESS PANEL 651FB RT WING 2024-633808<[01] REPLACED ANGLE TRAILING EDGE ACCESS PANEL 651FB RT WING IAW B737-700 SRM 51-40-02; SRM 51- - [SDR SWAA2024120648419](https://openairdocs.org/sdr/SWAA2024120648419), Oct 14, 2024: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE ACCESS PANEL 551FB LT WING 2024-633809<[01] REPLACED ANGLE TRAILING EDGE ACCESS PANEL 551FB LT WING IAW B737-700 SRM 51-10-02 ITEM 9 A - [SDR SWAA2024120548422](https://openairdocs.org/sdr/SWAA2024120548422), Oct 14, 2024: PANEL. CORRODED. CORROSION BULKHEAD PANEL 121HW AT FWD CARGO COMPARTMENT 2024-633814<[01] REPLACED LOWER STRUCTURAL SECTION AND FASTENERS IAW B737-700 SRM 51-40-02 AND DRAWING 1 - [SDR SWAA2024120548423](https://openairdocs.org/sdr/SWAA2024120548423), Oct 14, 2024: BEAR STRAP. CRACKED. CRACK ON BEAR STRAP LOCATED BTW BS 303.9 TO BS 312 AND BTW STR 7L TO STR 8L AT FWD GALLEY AREA 2024-633815SEE INDIVIDUAL SIGN OFFS BELOW; - [SDR SWAA2024120548073](https://openairdocs.org/sdr/SWAA2024120548073), Oct 13, 2024: TRACK. CRACKED. CRACK TRACK RBBL 13.84 LOCATED BS 767 AFT CARGO COMPARTMENT 2024-633778<[01] TOOL USED: ET EQUIPMENT; P/N: NORTEC600D; S/N: 200048001; CAL DUE DATE: 28-MAY-25;[ - [SDR SWAA2024120548072](https://openairdocs.org/sdr/SWAA2024120548072), Oct 13, 2024: TRACK. CRACKED. CRACK TRACK RBBL 13.84 LOCATED BS 747 AFT CARGO COMPARTMENT 2024-633780<[01] FAULT RESOLVED ON OTHER FAULT; SEE TTG8Q00WDYKT
SEE INDIVIDUAL SIGN OFFS BELOW.; - [SDR SWAA2024120647719](https://openairdocs.org/sdr/SWAA2024120647719), Oct 12, 2024: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE DODY FAIRING BS 500D AT LEVEL STRINGER 19L LOWER FUSELAGE 2024-633745<[01] REPLACED SUPPORT ANGLE LOCATED BODY FAIRING BS 500D AT LEVEL STRI - [SDR SWAA2024120647624](https://openairdocs.org/sdr/SWAA2024120647624), Oct 12, 2024: SKIN PANEL. CRACKED. CRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.90 RIB AND 8 INCH. FROM REAR SPAR. INBOARD SIDE OF RIB. CRACK LENGT - [SDR SWAA2024120647625](https://openairdocs.org/sdr/SWAA2024120647625), Oct 12, 2024: SKIN PANEL. CRACKED. CRACK INDICATION FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENG - [SDR SWAA2024120547909](https://openairdocs.org/sdr/SWAA2024120547909), Oct 12, 2024: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE BS 695 AND BL0 RT SIDE AT CENTER SECTION 2024-633756<[01] REJECTION ELONGATED HOLE BRACKET BS 695 AND BL0 RT SIDE AT CENTER SECTION PAX CABI - [SDR SWAA2024120547718](https://openairdocs.org/sdr/SWAA2024120547718), Oct 12, 2024: SUPPORT BRACKET. CRACKED. CRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2024-633743<[01] REPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT - [SDR SWAA2024120647622](https://openairdocs.org/sdr/SWAA2024120647622), Oct 11, 2024: RIB. CRACKED. CRACK INSPAR RIB 120.30 LOCATED 10 INCHES FROM EDGE REAR SPAR AT RT HORIZONTAL STABILIZER 2024-633675<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 60 - [SDR SWAA2024120647620](https://openairdocs.org/sdr/SWAA2024120647620), Oct 11, 2024: RIB. CRACKED. CRACK INSPAR RIB 120.30 LOCATED 18 INCHES FROM EDGE REAR SPAR AT RT HORIZONTAL STABILIZER 2024-633677<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 60 - [SDR SWAA2024120547510](https://openairdocs.org/sdr/SWAA2024120547510), Oct 11, 2024: WEB. CORRODED. CORROSION WEB FLOOR STRUCTURE LOCATED BS1016 AND LBL1 WL208.1 AT AFT GALLEY AREA CORROSION WEB FLOOR STRUCTURE LOCATED BS1016 AND LBL1 WL208.1 AT AFT GALLEY ARE - [SDR SWAA2024120547508](https://openairdocs.org/sdr/SWAA2024120547508), Oct 11, 2024: FLOORBEAM. CRACKED. CRACK FLOOR BEAM LOCATED BS328 AND RLB24 AT FWD GALLEY AREA 2024-633648<[01] ON STEP 6: TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X11290U021704; - [SDR SWAA2024120547511](https://openairdocs.org/sdr/SWAA2024120547511), Oct 11, 2024: STRAP. CORRODED. CORROSION STRAP FLOOR STRUCTURE LOCATED BS1016 AND RBL3 AT AFT GALLEY AREA 2024-633655<[01] REPLACED STRAP FLOOR STRUCTURE LOCATED BS1006 TO BS1028 AND RBL3 WL2 - [SDR SWAA2024120547512](https://openairdocs.org/sdr/SWAA2024120547512), Oct 11, 2024: FLOORBEAM. CORRODED. CORROSION FLOOR BEAM LOCATED STA986.5 AND RBL42 WL208.1 AT AFT GALLEY AREA 2024-633658<[01] ON STEP 7: TOOL USED EDDY CURRENT EQUIPMENT PN NORTEC 500D; SN: N500 - [SDR SWAA2024120547513](https://openairdocs.org/sdr/SWAA2024120547513), Oct 11, 2024: STRAP. CORRODED. CORROSION STRAP FLOOR STRUCTURE LOCATED STA1016 TO STA1040 AND LBL3 WL208.1 AT AFT GALLEY AREA 2024-633657<[01] REPLACED STRAP AND FASTENERS FLOOR STRUCTURE LOC - [SDR SWAA2024120647162](https://openairdocs.org/sdr/SWAA2024120647162), Oct 10, 2024: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE LOCATED ORSS 270 DEFLECTION CONTROL RIB AREA AT RT WING 2024-633618<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 270 DEFLECTION CONT - [SDR SWAA2024120547164](https://openairdocs.org/sdr/SWAA2024120547164), Oct 10, 2024: ANGLE. CRACKED. CRACK ANGLE LOCATED BETWEEN BS727C TO BS727D AND LBL52 CEILING AREA AFT CARGO COMPARTMENT 2024-633632<[01] TOOL USED ET EQUIPMENT: P/N: NORTEC 600D; S/N: 600071 - [SDR SWAA2024120547165](https://openairdocs.org/sdr/SWAA2024120547165), Oct 10, 2024: WEB. CRACKED. CRACK WEB LOCATED BETWEEN STA847 TO STA867 AND LBL20 CEILING AREA AT AFT CARGO COMPARTMENT 2024-633631<[01] REPLACED WEB AND FASTENERS LOCATED BETWEEN STA847 TO - [SDR SWAA2024120547151](https://openairdocs.org/sdr/SWAA2024120547151), Oct 10, 2024: FITTING. DETERIORATED. DETERIORATED GIRT BAR FITTING HARDWARE LT AT AFT GALLEY AREA 2024-633594<[01] REPLACED GIRT BAR FITTING HARDWARE LT AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02 - [SDR SWAA2024120547146](https://openairdocs.org/sdr/SWAA2024120547146), Oct 10, 2024: FITTING. DETERIORATED. DETERIORATED GIRT BAR FITTING HARDWARE RT AT AFT GALLEY AREA 2024-633595<[01] REPLACED GIRT BAR FITTING HARDWARE RT AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02 - [SDR SWAA2024120546902](https://openairdocs.org/sdr/SWAA2024120546902), Oct 10, 2024: PRESSURE DECK. CRACKED. CRACK INDICATION FOUND ON HORIZONTAL PRESSURE WEB UPPER SURFACE BTW STA 663 TO STA 675; AT LEVEL LBL 30. CRACK LENGTH = 0.250 INCHES APPROX. 2024-633590<[01] TO - [SDR SWAA2024120547324](https://openairdocs.org/sdr/SWAA2024120547324), Oct 10, 2024: STUB FRAME. CRACKED. CRACK STUB FRAME ON BS 294.5 AT LEVEL STR17R AT FWD GALLEY AREA 2024-633637<[01] STEP 4. EDDY CURRENT EQUIPMENT USED P/N: NORTE 600D; S/N: 210138003 AND DUE DAT - [SDR SWAA2024120547328](https://openairdocs.org/sdr/SWAA2024120547328), Oct 10, 2024: INTERCOSTAL. CORRODED. CORROSION WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA294.5 TO STA312 AND LBL12 WL208.1 AT FWD GALLEY AREA 2024-633641<[01] REPLACED WEB INTERCOSTAL LOCA - [SDR SWAA2024120546906](https://openairdocs.org/sdr/SWAA2024120546906), Oct 10, 2024: VAPOR BARRIER. CRACKED. CRACK INDICATION FOUND ON VAPOR BARRIER LOCATED BS 663 AND BTW. RBL 40 TO RBL 43 CRACK LENGTH IS 6 INCH 2024-633591<[01] TOOL USED: SCALE P/N CR5200 S/N 8343110 - [SDR SWAA2024120547327](https://openairdocs.org/sdr/SWAA2024120547327), Oct 10, 2024: INTERCOSTAL. CRACKED. CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA312 TO STA328 AND RBL30 FWD GALLEY AND LAV 2024-633640<[01] REPLACED INTERCOSTAL WEB LOCATED BETWEEN - [SDR SWAA2024120547323](https://openairdocs.org/sdr/SWAA2024120547323), Oct 10, 2024: TIE CLIP. CRACKED. CRACK TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN 2024-633633<[01] REPLACED TIE CLIP AND FASTENERS LOC. BS277 AND STR10R AT PASSENGER CABIN IAW B737-70 - [SDR SWAA2024120547325](https://openairdocs.org/sdr/SWAA2024120547325), Oct 10, 2024: FRAME. CRACKED. CRACK FRAME LOCATED STA312 AND BETWEEN STR5L TO STR6L AT PASSENGER CABIN 2024-633636<[01] REPAIRED FRAME LOCATED STA 312 BTW STR5L TO STR6L FWD GALLEY AREA IAW - [SDR SWAA2024120547326](https://openairdocs.org/sdr/SWAA2024120547326), Oct 10, 2024: STRINGER. CRACKED. CRACK STRINGER 16L LOCATED STA294.5 AT PASSENGER CABIN 2024-633634<[01] ON STEP 6; TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 190023010; DUE DATE: - [SDR SWAA2024120546898](https://openairdocs.org/sdr/SWAA2024120546898), Oct 9, 2024: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED STA695 AND BL0 CENTER SECTION 2024-633566<[01] REPLACED SUPPORT ANGLE LOCATED STA695 BL0 CENTER SECTION IAW B737-700 SRM 51-10-02 IT All 267: https://openairdocs.org/aircraft/N269WN/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 --- 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.