# N7741C: 2007 Boeing 737-7BD - Status: Valid registration - Airframe: [Boeing 737-7BD](https://openairdocs.org/model/boeing-737-7bd) (registry code 1384511, 149 seats) - Engine: [CFM International CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044) - Serial number: 35788 - Year built: 2007 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 11, 2013 - Certificate issued: August 12, 2013 - Expires: August 31, 2029 - Mode S code: AA7A61 - 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=7741C - Page: https://openairdocs.org/aircraft/N7741C 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 737-7BD) 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 N7741C. ## FAA accident and incident reports None matched to N7741C. ## Service difficulty reports (233, 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 SWAA2026022473255](https://openairdocs.org/sdr/SWAA2026022473255), Feb 22, 2026: GIRT BAR. UNSECURE. RAMP REPORTS L2 SLIDE GIRT BAR NOT STOWED. STOWED L2 DOOR SLIDE GIRT BAR IAW AMM25-66-01. - [SDR SWAA2025122955405](https://openairdocs.org/sdr/SWAA2025122955405), Dec 23, 2025: SENSE LINE. BROKEN. AT 30000 CABIN ALT WARNING HORN CAME ON. THE CABIN ALT REACHED 10;000 FEET. STARTED QRH PROCEDURES AND DESCENDED TO 10;000. NO PAX MASKS DROPPED. FOUND SENSE LI - [SDR SWAA2025032408178](https://openairdocs.org/sdr/SWAA2025032408178), Mar 21, 2025: SLIDE. DETACHED. FWD ENTRY DOORESCAPE SLIDE DETACHED FROM DOOR AFTER OPENING<[01] R/R FWD ENTRY DOOR SLIDE PER MT 725-61-06-FE - [SDR SWAA2025031003497](https://openairdocs.org/sdr/SWAA2025031003497), Mar 9, 2025: SLIDE. DISLODGED. FWD ENTRY DOOR SLIDE FELL OUT OF BOX<[01] REPACKED SLIDE INTO BOX PER 25-66-00. NO DEFECTS NOTED - [SDR SWAA2025011384827](https://openairdocs.org/sdr/SWAA2025011384827), Jan 10, 2025: LAMP. INOPERATIVE. ONE EMERGENCY LIGHT INOP BELOW AFT ENTRY DOOR<[01] RELAMPED ONE EMERGENCY LIGHT BELOW AFT ENTRY DOOR REF AMM 33-51-04. OPS CHECK GOOD. - [SDR SWAA2024121776126](https://openairdocs.org/sdr/SWAA2024121776126), Dec 10, 2024: CABIN AIR SYS. ODOR. SHORTLY BEFORE DESCENT CABIN CREW REPORTED A BURN POPCORN SMELL MID CABIN. SMELL DISSIPATED AND DID NOT RETURN<[01] PERFORMED FIM 21-00 TASK 806 AND SMOKE OR FU - [SDR SWAA2024112561272](https://openairdocs.org/sdr/SWAA2024112561272), Nov 19, 2024: LIGHT. INOPERATIVE. FWD SERVICE DOOR SLIDE LIGHT INOP<[01] RELAMPED AND PERFORMED GOOD INSTALLATION TEST OF FWD SERVICE DOOR SLIDE LIGHT IAW AMM 33-51-04-960-801.;[02] VERIFIED ACT - [SDR SWAA2024112560649](https://openairdocs.org/sdr/SWAA2024112560649), Nov 16, 2024: BATTERY PACK. FAILED. EMERGENCY BATERY PACK M1668 FAIL TEST<[01] REMOVED AND REPLACED EMERGENCY BATERY PACK M1668 AND TESTED GOOD PER AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE A - [SDR SWAA2024112553044](https://openairdocs.org/sdr/SWAA2024112553044), Oct 24, 2024: SUPPORT. CRACKED. MAIN CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75.<[01] REMOVED AND REPLACED MAIN CABIN FLOOR STRUCTURE WITH NEW SUPPORT AT STA 540; B - [SDR SWAA2024112151884](https://openairdocs.org/sdr/SWAA2024112151884), Oct 23, 2024: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 221BF TOP SURFACE IS DELAMINATED.<[01] 221BF UPPER SURFACE DAMAGE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-1-A00939 (REPAIR 1 - REPAIR OF DAMAGE - [SDR SWAA2024112551348](https://openairdocs.org/sdr/SWAA2024112551348), Oct 21, 2024: FRAME. CRACKED. FWD SERVICE DOOR FRAME BS 294 CRACKED AT LOWER END RBL 56 WL 208.<[01] REFER TO FAULT TTG8Q00WJ92N FOR REPAIR RESOLUTION;[02] VERIFIED CORRECTIVE ACTION 1 - [SDR SWAA2024112551351](https://openairdocs.org/sdr/SWAA2024112551351), Oct 21, 2024: FRAME. CRACKED. CRACK ON BS 312 FRAME COMMON TO STR 5L LBL 33 WL 282.<[01] REMOVED CRACK ON BS 312 FRAME COMMON TO STR 5L LBL 33 WL 282 PER M-22-153-01244 ON FAULT# TTG8Q00WKNT - [SDR SWAA2024112150854](https://openairdocs.org/sdr/SWAA2024112150854), Oct 19, 2024: STUB FRAME. CRACKED. CRACK ON R1 DOORWAY FWD STUB FRAME IB SURFACE; BS 295 STR 17R<[01] NDT HFEC INSPECTED SURFACE PER 737 NDTM PART 6; 51-00-00; PROC 23; VERIFIED 1 INCH LONG CRACK - [SDR SWAA2024112150857](https://openairdocs.org/sdr/SWAA2024112150857), Oct 19, 2024: SKIN. CORRODED. L/W FRONT SPAR - PITTING CORROSION ON UPPER ROLLER SURFACE AT INB MAIN SLAT TRACK #3 SLAT (MARKED)<[01] FAULT WILL BE RESOLVED ON CUSTOMER CARD:TTG8Q00WJA0T;[02 - [SDR SWAA2024112550123](https://openairdocs.org/sdr/SWAA2024112550123), Oct 18, 2024: THRESHOLD. CRACKED. AFT CARGO BAY AFT CORNER THRESHOLD IS CRACKED<[01] REPAIRED AFT CARGO BAY AFT CORNER THRESHOLD PER SRM 53-60-15-2R-1;[02] VERIFIED COMPLETION CORRECTIVE ACTION - [SDR SWAA2024112550607](https://openairdocs.org/sdr/SWAA2024112550607), Oct 18, 2024: SUPPORT ANGLE. CRACKED. RIGHT WING UPPER T/E PANEL BULB SEAL SUPPORT ANGLE IS CRACKED AT RSS 274<[01] REMOVED; REPLACED; AND INSTALLED A NEW BULB SEAL SUPPORT ANGLE AT R/W UPPER T/E PA - [SDR SWAA2024112550614](https://openairdocs.org/sdr/SWAA2024112550614), Oct 18, 2024: SUPPORT. CRACKED. BULB SEAL RETAINER SUPPORT IS CRACKED AT LEFT WING FIXED T/E PANEL JUST AFT OF THE PYLON ORSS 269. MARKED<[01] REMOVED AND REPLACED BULB SEAL RETAINER SUPPORT F - [SDR SWAA2024112150125](https://openairdocs.org/sdr/SWAA2024112150125), Oct 18, 2024: TRACK. CRACKED. AFT CARGO BAY CARGO TRACK IS CRACKED AT BS767 AND BS747 RBL13 WL156<[01] REMOVED AND REPLACED AFT CARGO BAY CARGO TRACK FROM BS727+4 - BS887 RBL13 WL156 IAW SRM - [SDR SWAA2024112150124](https://openairdocs.org/sdr/SWAA2024112150124), Oct 18, 2024: SHIELD. CORRODED. CORROSION FWD CARGO BAY AFT SHIELD BS500+1 TO BS500+19 RBL22 WL156 HAS MULTIPLE AREAS AROUND NUT PLATE HOLES<[01] REMOVED AND REMPLACED SHIELD BS500A? TO BS500+ - [SDR SWAA2024112150126](https://openairdocs.org/sdr/SWAA2024112150126), Oct 18, 2024: PLATE. CORRODED. CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156<[01] LINE ITEM 2 ON PART REQUIREME - [SDR SWAA2024112150127](https://openairdocs.org/sdr/SWAA2024112150127), Oct 18, 2024: SHIELD. CORRODED. CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] REMOVED AND REPLACED FWD SHIELD BETWEEN BS767 - [SDR SWAA2024112150128](https://openairdocs.org/sdr/SWAA2024112150128), Oct 18, 2024: SUPPORT. CORRODED. CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] CORROSION ON SUPPORT WAS - [SDR SWAA2024112550083](https://openairdocs.org/sdr/SWAA2024112550083), Oct 17, 2024: ATTACH ANGLE. CRACKED. ATTACH ANGLE CRACKED BS 294 FWD SIDE OF STUB FRAME RBL 54 WL 208.<[01] REMOVED DAMAGE CLIP I.A.W SRM 51-10-02-0G-0 AND SRM 51-40-02-0G-0; FABRICATION AND INSTAL - [SDR SWAA2024112550108](https://openairdocs.org/sdr/SWAA2024112550108), Oct 17, 2024: STRAP. CORRODED. CORROSION ON L/H REINFORCEMENT STRAP BS 1017-1020 LBL 27 WL 208.<[01] REMOVED LH REINFORCEMENT STRAP AND INSTALLED NEW LH REINFORCEMENT STRAP BS1006-1020 LBL27 - [SDR SWAA2024112550109](https://openairdocs.org/sdr/SWAA2024112550109), Oct 17, 2024: STRAP. CORRODED. CORROSION ON L/H REINFORCEMENT STRAP BS 1017 LBL 19 WL 208.<[01] REMOVED LH REINFORCEMENT STRAP AND REPLACED WITH NEW LH REINFORCEMENT STRAP BS1006-1025 LBL19 W - [SDR SWAA2024112549565](https://openairdocs.org/sdr/SWAA2024112549565), Oct 17, 2024: FORMER. CRACKED. R/H FAIRING FORMER BS 500D BETWEEN STRINGER 18 R/H AND 19 R/H IS CRACKED<[01] EVALUATED CRACK ON FAIRING FORMER AT BS 500D BETWEEN STRINGER 18R/H AND 19R/H FOUN - [SDR SWAA2024112550098](https://openairdocs.org/sdr/SWAA2024112550098), Oct 17, 2024: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS685 S-3L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 685 S-3L PER SRM 51-40-02-0G-0 AND BOEING DWG 144A1106 REV. A.;[0 - [SDR SWAA2024112550099](https://openairdocs.org/sdr/SWAA2024112550099), Oct 17, 2024: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS706 S-2L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 706 S-2L PER SRM 51-40-02-0G-0 AND BOEING DWG 144A1107 REV. -.;[0 - [SDR SWAA2024112550093](https://openairdocs.org/sdr/SWAA2024112550093), Oct 17, 2024: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727E S-5R. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727E S-5R PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1112 REV. -.; - [SDR SWAA2024112550094](https://openairdocs.org/sdr/SWAA2024112550094), Oct 17, 2024: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727A S-3R. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727A S-3R PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1101 REV. -.; - [SDR SWAA2024112550095](https://openairdocs.org/sdr/SWAA2024112550095), Oct 17, 2024: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727B S-6L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727B S-6L PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1102 REV. -.; - [SDR SWAA2024112550100](https://openairdocs.org/sdr/SWAA2024112550100), Oct 17, 2024: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727C S-6L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727C S-6L PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1103 REV. -.; - [SDR SWAA2024112550096](https://openairdocs.org/sdr/SWAA2024112550096), Oct 17, 2024: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727E S-4L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727E S-4L PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1112 REV. -.; - [SDR SWAA2024112550097](https://openairdocs.org/sdr/SWAA2024112550097), Oct 17, 2024: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727E S-5L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727E S-5L PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1112 REV. -.; - [SDR SWAA2024112550101](https://openairdocs.org/sdr/SWAA2024112550101), Oct 17, 2024: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727E S-6L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727C S-6L PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1112 REV. -.; - [SDR SWAA2024112550102](https://openairdocs.org/sdr/SWAA2024112550102), Oct 17, 2024: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727E S-7L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727E S-7L PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1112 REV. -.; - [SDR SWAA2024112550103](https://openairdocs.org/sdr/SWAA2024112550103), Oct 17, 2024: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS767 S-6L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 767 S-6L PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1132 REV. -.;[0 - [SDR SWAA2024112550104](https://openairdocs.org/sdr/SWAA2024112550104), Oct 17, 2024: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS767 S-5L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP FROM BS 767 S-5L PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1132 REV. -.; - [SDR SWAA2024112549904](https://openairdocs.org/sdr/SWAA2024112549904), Oct 17, 2024: SEAT TRACK. CORRODED. CORROSION ON PAX CABIN SEAT TRACK LBL25 BS500B+12 WL208. MARKED<[01] REMOVED CORROSION ON SEAT TRACK LBL25 BS500B+12 AND APPLIED CHEMICAL CONVERSION AND PRIMER - [SDR SWAA2024112150107](https://openairdocs.org/sdr/SWAA2024112150107), Oct 17, 2024: FLOORBEAM. CORRODED. CORROSION AROUND FASTENER HOLE BS 986 FLOOR BEAM RBL 45 WL 208. CORROSION AROUND FASTENER HOLE PREVIOUS REPAIR BS 986 FLOOR BEAM RBL 45 WL 208<[01] REMOVED AND - [SDR SWAA2024112150092](https://openairdocs.org/sdr/SWAA2024112150092), Oct 17, 2024: FLOORBEAM. CRACKED. BS 294 FLOOR BEAM IS CRACKED ON UPPER FLANGE RBL 52 WL 208.<[01] REMOVED DAMAGE PART OF THE FLOOR BEAM BS294 RBL24-RBL60 WL208 AND REPAIRED I.A.W SRM 53-10-51-2 - [SDR SWAA2024112149568](https://openairdocs.org/sdr/SWAA2024112149568), Oct 17, 2024: FLOOR PANEL. CRACKED. CABIN FLOOR PANEL 221GF FWD O/B CORNER TANG IS CRACKED.<[01] CABIN FLOOR PANEL 221GF FWD O/B CORNER TANG WITH CRACK WAS REPLACED WITH A SERVICEABLE FLOOR PANEL - [SDR SWAA2024112150081](https://openairdocs.org/sdr/SWAA2024112150081), Oct 17, 2024: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 232AF TOP SURFACE DELAMINATED.<[01] CABIN FLOOR PANEL 232AF WITH TOP SURFACE DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM - [SDR SWAA2024112549551](https://openairdocs.org/sdr/SWAA2024112549551), Oct 16, 2024: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 242VF CORRODED INSERTS AND TOP SURFACE DELAMINATION.<[01] CABIN FLOOR PANEL 242VF WITH TOP SURFACE DELAMINATION WAS REPAIRED AND CORRODED INSE - [SDR SWAA2024112549553](https://openairdocs.org/sdr/SWAA2024112549553), Oct 16, 2024: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 241ACF HAS CORRODED INSERTS AND TOP SURFACE DELAMINATION.<[01] TOP SURFACE DAMAGE WAS REPAIRED AND DAMAGED INSERTS WERE REMOVED AND REPLACED I - [SDR SWAA2024112549378](https://openairdocs.org/sdr/SWAA2024112549378), Oct 16, 2024: RIB. CRACKED. FOUND CRACK ON R/H HORIZONTAL STAB LEADING EDGE RIB AT L/E STA 95.96<[01] REMOVED AND REPLACED R/H HORIZONTAL STAB LEADING EDGE RIB AT L/E STA 95.96
I.A.W SR - [SDR SWAA2024112149549](https://openairdocs.org/sdr/SWAA2024112149549), Oct 16, 2024: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 241ZF HAS TOP SURFACE DELAMINATION.<[01] TOP SURFACE DELAMINATION ON CABIN FLOOR PANEL 241ZF WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED - [SDR SWAA2024112149548](https://openairdocs.org/sdr/SWAA2024112149548), Oct 16, 2024: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 241XF HAS TOP SURFACE DELAMINATION.<[01] 241XF FLOOR PANEL UPPER SURFACE DAMAGE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-1-A00939 (REPAIR 1 - RE - [SDR SWAA2024112149367](https://openairdocs.org/sdr/SWAA2024112149367), Oct 16, 2024: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 222CF HAS TOP SURFACE DELAMINATION.<[01] CABIN FLOOR PANEL 222CF WITH TOP SURFACE DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFI - [SDR SWAA2024112149362](https://openairdocs.org/sdr/SWAA2024112149362), Oct 16, 2024: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL 221BF CORRODED INSERTS; BROKEN TAB AND TOP SURFACE DELAMINATION.<[01] 221BF FLOOR PANEL DAMAGED AREAS HAVE BEEN REPAIRED PER [SRM 53-00-50-2R- All 233: https://openairdocs.org/aircraft/N7741C/reports.md ## STCs that may be installed (OpenAirDocs) (2) 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 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 ## Earlier aircraft with N7741C The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7741C before. - [Cancelled 1976-01-28](https://openairdocs.org/deregistered/N7741C-1976-01-28): Piper PA-28-235, S/N 28-7610063. Exported to Australia. Owner: [Globe Aero Ltd Inc](https://openairdocs.org/faa-owner/GLOBE%20AERO%20LTD%20INC), [Lock Haven, PA](https://openairdocs.org/faa-place/PA/Lock%20Haven) ## Related - Other Boeing 737-7BD aircraft: https://openairdocs.org/model/boeing-737-7bd/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.