# N7713A: 2005 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 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Serial number: 33919 - Year built: 2005 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 15, 2005 - Certificate issued: December 11, 2013 - Expires: December 31, 2029 - Mode S code: AA6F80 - 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=7713A - Page: https://openairdocs.org/aircraft/N7713A 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 model are included. ## ADs that may apply (OpenAirDocs): 55 in force ### Matched by airframe (Boeing 737-7BD) None in force. ### Matched by engine (CFM International CFM56 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 2017-14-08](https://openairdocs.org/ad/2017-14-08): Turbine Engine Compressor Section · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Aug 18, 2017 - [AD 2017-05-09](https://openairdocs.org/ad/2017-05-09): Accessory Gearboxes · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 33 more. Effective Apr 13, 2017 - [AD 2016-14-10](https://openairdocs.org/ad/2016-14-10): High-pressure turbine (HPT) disks · CFM International CFM56-3, CFM56-3B and CFM56-3C with STC SE00034EN. Effective Aug 9, 2016 - [AD 2016-02-04](https://openairdocs.org/ad/2016-02-04): Turbine rear frames (TRFs) · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 33 more. Effective Mar 1, 2016 - [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 2013-14-06](https://openairdocs.org/ad/2013-14-06): Hydro-mechanical unit (HMU) fuel control · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 34 more. Effective Sep 3, 2013 - [AD 2012-02-03](https://openairdocs.org/ad/2012-02-03): Engine · CFM International CFM56-5B1/3, CFM56-5B2/3, CFM56-5B3/3 and 8 more. Effective Mar 15, 2012 - [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 2010-12-03](https://openairdocs.org/ad/2010-12-03): Fan blades · CFM International CFM56-3 and CFM56-3B. Effective Jul 13, 2010 - [AD 2010-09-14](https://openairdocs.org/ad/2010-09-14): Exhaust gas temperature (EGT) · CFM International CFM56-5B1/2P, CFM56-5B1/P, CFM56-5B2/2P and 16 more. Effective Jun 8, 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 2009-18-01](https://openairdocs.org/ad/2009-18-01): LP turbine rear frames · CFM International CFM56-5B1/3, CFM56-5B1/P, CFM56-5B2/3 and 19 more. Effective Oct 1, 2009 - [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 2007-24-04](https://openairdocs.org/ad/2007-24-04): Low pressure turbine (LPT) · CFM International CFM56-5C4/1. Effective Dec 6, 2007 - [AD 2007-03-15](https://openairdocs.org/ad/2007-03-15): Exhaust gas temperature (EGT) harness · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 34 more. Effective Mar 19, 2007 - [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 2005-10-05](https://openairdocs.org/ad/2005-10-05): Air turbine starters · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 50 more. Effective Jun 14, 2005 - [AD 97-09-02 R3](https://openairdocs.org/ad/97-09-02-R3): High pressure turbine rotor (HPTR) front shafts · CFM International CFM56-5C2, CFM56-5C3/G and CFM56-5C4. Effective Oct 14, 2004 - [AD 2004-10-13](https://openairdocs.org/ad/2004-10-13): Service main fuel pumps · CFM International CFM56-3, CFM56-5, CFM56-5-A1/F and 4 more. Effective Jun 24, 2004 - [AD 2002-22-12](https://openairdocs.org/ad/2002-22-12): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more. Effective Dec 13, 2002 - [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 2002-02-13](https://openairdocs.org/ad/2002-02-13): Magnetic Drain Plug · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 33 more. Effective Mar 21, 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 2001-09-17](https://openairdocs.org/ad/2001-09-17): Fuel Manifold and CJ9L Harness · CFM International CFM56-5C2, CFM56-5C2/4, CFM56-5C2/F and 13 more. Effective May 14, 2001 - [AD 2001-04-06](https://openairdocs.org/ad/2001-04-06): Fan Disk · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Apr 4, 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 2000-15-01](https://openairdocs.org/ad/2000-15-01): Fuel Leakage · CFM International CFM56-2, CFM56-2A, CFM56-2B and 39 more. Effective Oct 2, 2000 - [AD 2000-05-22](https://openairdocs.org/ad/2000-05-22): CFM International CFM56-2, CFM56-2A, CFM56-2B and 3 more. Effective May 2, 2000 - [AD 99-06-16](https://openairdocs.org/ad/99-06-16): High Pressure Turbine Rotor (HPTR) Front Air Seal · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 3 more. Effective Apr 21, 1999 - [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 - [AD 98-19-10](https://openairdocs.org/ad/98-19-10): Accessory Gearbox · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Sep 28, 1998 - [AD 98-12-32](https://openairdocs.org/ad/98-12-32): High Pressure Turbine Rotor Disks · CFM International CFM56-2, CFM56-2A, CFM56-2B and 3 more. Effective Jul 20, 1998 - [AD 98-10-11](https://openairdocs.org/ad/98-10-11): Accessory Gearbox · CFM International CFM56-3, CFM56-3B, CFM56-3C and 31 more. Effective Jun 3, 1998 - [AD 98-07-02](https://openairdocs.org/ad/98-07-02): Air/oil Seal · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Mar 30, 1998 - [AD 98-02-04](https://openairdocs.org/ad/98-02-04): Low Pressure Turbine Case · CFM International CFM56-5B1/2P, CFM56-5B2/2P, CFM56-5B3/2P and 1 more. Effective Mar 23, 1998 - [AD 89-23-06 R1](https://openairdocs.org/ad/89-23-06-R1): Magnetic Chip Detector · CFM International CFM56-2, CFM56-2A, CFM56-3 and 8 more. Effective Jan 28, 1998 - [AD 97-08-01](https://openairdocs.org/ad/97-08-01): Fan Disks · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Jun 23, 1997 - [AD 97-06-01](https://openairdocs.org/ad/97-06-01): High Pressure Compressor Rotor (HPCR) Stage 1-2 Spool · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 28 more. Effective Jun 3, 1997 - [AD 97-05-13](https://openairdocs.org/ad/97-05-13): Air Turbine Engine Starter · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 3 more. Effective Jun 3, 1997 - [AD 96-25-11](https://openairdocs.org/ad/96-25-11): Redesigned Fan Blades · CFM International CFM56-3B and CFM56-3C. Effective Jan 29, 1997 ### 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 2013-02-02](https://openairdocs.org/ad/2013-02-02) (historical): High-pressure turbine (HPT) disks · CFM International CFM56-3, CFM56-3B and CFM56-3C with STC SE00034EN. Effective Jan 28, 2013 - [AD 2009-01-01](https://openairdocs.org/ad/2009-01-01) (historical): Exhaust gas temperature (EGT) · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 22 more. Effective Dec 31, 2008 - [AD 97-09-02 R2](https://openairdocs.org/ad/97-09-02-R2) (historical): Low pressure turbine rotor (LPTR) · CFM International CFM56-5C2, CFM56-5C2/4, CFM56-5C2/F and 9 more. Effective Apr 29, 2003 - [AD 2003-02-04](https://openairdocs.org/ad/2003-02-04) (historical): Exhaust gas temperature (EGT) · CFM International CFM56-5 Series (all). Effective Feb 27, 2003 - [AD 97-09-02 R1](https://openairdocs.org/ad/97-09-02-R1) (historical): High Pressure Turbine rotor (HPTR) front shaft · CFM International CFM56-5C2/G, CFM56-5C2/G4, CFM56-5C3/G and 3 more. Effective Sep 24, 2002 - [AD 2001-17-14](https://openairdocs.org/ad/2001-17-14) (historical): LPT Conical Supports · CFM International CFM56-5C4/1. Effective Sep 7, 2001 - [AD 2001-08-51](https://openairdocs.org/ad/2001-08-51) (historical): Fuel leakage · CFM International CFM56-5 Series (all) - [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 - [AD 99-08-16](https://openairdocs.org/ad/99-08-16) (historical): CFM International CFM56-2, CFM56-2A, CFM56-2B and 3 more. Effective May 13, 1999 - [AD 97-09-02](https://openairdocs.org/ad/97-09-02) (historical): High/Low Pressure Turbine Rotor · CFM International CFM56-5C2/G, CFM56-5C2/G4, CFM56-5C3/G and 3 more. Effective Jun 30, 1997 All 71: https://openairdocs.org/aircraft/N7713A/ads.md ## Information bulletins (advisory) (4 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-13-33R2](https://openairdocs.org/saib/NE-13-33R2): Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes. Issued Jan 28, 2014 - [SAIB NE-12-29](https://openairdocs.org/saib/NE-12-29): Engine Fuel Distribution CFM56-5B LPTACC Fuel Manifold. Issued Apr 27, 2012 - [SAIB NE-06-02](https://openairdocs.org/saib/NE-06-02): . Issued Oct 18, 2005 - [SAIB NE-13-33R1](https://openairdocs.org/saib/NE-13-33R1) (historical): Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes. Issued Jun 24, 2013 - [SAIB NE-13-33](https://openairdocs.org/saib/NE-13-33) (historical): Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes. Issued May 13, 2013 - [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 N7713A. ## FAA accident and incident reports None matched to N7713A. ## Service difficulty reports (229, 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 SWAA2026091601309](https://openairdocs.org/sdr/SWAA2026091601309), Sep 15, 2026: VALVE. LEAKING. SUSPECTED FUEL LEAK ON NUMBER 1 ENGINE PERFORMED ENGINE VENTS AND DRAINS INSPECTION PER AMM 71-71-00. FOUND FUEL TO BE LEAKING OUT OF BSV & LPTACC DRAIN HOLE AT - [SDR SWAA2026050594423](https://openairdocs.org/sdr/SWAA2026050594423), May 1, 2026: BATTERY PACK. NO TEST. FWD LEFT ENTRY EMERGENCY BATTERY PACK M1675 FAILED A CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06. - [SDR SWAA2025093018940](https://openairdocs.org/sdr/SWAA2025093018940), Sep 28, 2025: FAN. ODOR. FA SMELLED SOMETHING IN THE CABIN, OK TO CONTINUE PER MEL 21-31-02 SP 1 AND 2. AFTER INSPECTION OF CABIN ROWS 7-9 ABC AND DEF AREA AND PSU. FOUND RECIRCULATING - [SDR SWAA2025082206571](https://openairdocs.org/sdr/SWAA2025082206571), Aug 21, 2025: HANDLE. MISSING. AFT CARGO DOOR HANDLE STUD CAP IS MISSING.<[01] REPLACED AFT CARGO DOOR HANDLE STUD PER AMM 52-31-14;[02] INSP AFT CARGO DOOR HANDLE STUD PER AMM 52-31-14 - [SDR SWAA2025081905397](https://openairdocs.org/sdr/SWAA2025081905397), Aug 17, 2025: BRACKET. LOOSE. AFT ENTRY SLIDE BRACKET LOOSE. SECURED SLIDE PACK AND COVER HARDWARE IAW AMM 25-66-01. - [SDR SWAA2025011786751](https://openairdocs.org/sdr/SWAA2025011786751), Jan 16, 2025: BATTERY PACK. INOPERATIVE. L-1 DOOR FORWARD LOWER EMERGENCY EXIT LIGHT INOP 2024-759682<[01] PERFORMED FUSE REPLACE AT M1674 EMERGENCY EXIT BATTERY PACK TEST OK IAW B737-700 AMM 33-51-06- - [SDR SWAA2025011786748](https://openairdocs.org/sdr/SWAA2025011786748), Jan 16, 2025: BATTERY PACK. INOPERATIVE. EMERGENCY ESCAPE LIGHTS INOP ON OVERHEAD BIN BULLNOSE ROWS 4ABC; 9ABC; 11BC AND 8DEF 2024-759683<[01] PERFORMED FUSE REPLACE AT M2335 EMERGENCY EXIT BATTERY PAC - [SDR SWAA2025011786750](https://openairdocs.org/sdr/SWAA2025011786750), Jan 16, 2025: BULB. BURNED OUT. EMERGENCY EXIT LIGHT R-2 DOOR HAS BULB BURNED OUT 2024-759689<[01] REPLACED EXIT LIGHT R-2 DOOR LAMP TEST IS OK IAW B737-700 AMM 33-51-01-960-801;[02] CORRECTED - [SDR SWAA2025011585530](https://openairdocs.org/sdr/SWAA2025011585530), Jan 13, 2025: SKIN. CRACKED. CRACK ON LOWER SURFACE OF SLAT 7 AT RIGHT WING. REPAIRED L/E SLAT FLEX SKIN ON LOWER SURFACE OF SLAT 7 AT RIGHT WING. IAW SRM 57-42-01-2R-13 REPAIR 13. - [SDR SWAA2025011578976](https://openairdocs.org/sdr/SWAA2025011578976), Dec 18, 2024: FLOOR PANEL. CRACKED. CRACK FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT 2024-759629<[01] FABRICATED FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DW - [SDR SWAA2025011582818](https://openairdocs.org/sdr/SWAA2025011582818), Dec 18, 2024: ANGLE. CRACKED. CRACK ANGLE LOCATED WEATHER RADAR SUPPORT BETWEEN STA188 TO STA203.8 AT LOWER NOSE COMPARTMENT 2024-759635<[01] REPLACED ANGLE LOCATED WEATHER RADAR SUPPORT BET - [SDR SWAA2025011578741](https://openairdocs.org/sdr/SWAA2025011578741), Dec 17, 2024: FLOOR PANEL. DAMAGED. ELONGATED HOLES ON FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT 2024-759626<[01] FABRICATED FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-2 - [SDR SWAA2025011577946](https://openairdocs.org/sdr/SWAA2025011577946), Dec 16, 2024: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET BODY STATION 540 AND RBL6 KEEL BEAM 2024-759614<[01] REPLACED SUPPORT BRACKET BODY STATION 540 AND RBL6 KEEL BEAM IAW B737-700 SRM51-10-02 - [SDR SWAA2025011577947](https://openairdocs.org/sdr/SWAA2025011577947), Dec 16, 2024: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET BODY STATION 540 AND LBL6 KEEL BEAM. REPLACED SUPPORT BRACKET BODY STATION 540 AND LBL6 KEEL BEAM IAW B737-700 SRM 51-10-02 ITEM 9 ;B737-7 - [SDR SWAA2025011577516](https://openairdocs.org/sdr/SWAA2025011577516), Dec 15, 2024: FITTING. WORN. WEAR HARDWARE GIRT BAR FITTING SERVICE DOOR AT FWD GALLEY AREA 2024-759600<[01] REPLACED HARDWARE GIRT BAR FITTING SERVICE DOOR AT FWD GALLEY AREA IAW AMM 25-66 - [SDR SWAA2025011577517](https://openairdocs.org/sdr/SWAA2025011577517), Dec 15, 2024: FITTING. WORN. WEAR HARDWARE GIRT BAR FITTING ENTRY DOOR AT FWD GALLEY AREA (1EA) 2024-759601<[01] REPLACED HARDWARE GIRT BAR FITTING ENTRY DOOR AT FWD GALLEY AREA IAW B737-70 - [SDR SWAA2025011577753](https://openairdocs.org/sdr/SWAA2025011577753), Dec 15, 2024: WEB. CRACKED. (CUSTOMER REQUEST)CRACK ON WEB LOCATED BETWEEN BS 294.5 TO BS 303.9 AT LEVEL STR16L AT PASSENGER CABIN. REPAIRED AREA ON WEB BETWEEN BS 294.5 TO BS 303.9 AT LEV - [SDR SWAA2025011577170](https://openairdocs.org/sdr/SWAA2025011577170), Dec 13, 2024: LIGHT. BROKEN. BROKEN PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) 2024-759569<[01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CAB - [SDR SWAA2025011577168](https://openairdocs.org/sdr/SWAA2025011577168), Dec 13, 2024: ANGLE. CRACKED. CRACK ANGLE LOCATED BS663 AND RBL42 AT CENTER WING BOX 2024-759565<[01] REPLACED ANGLE LOCATED BS663 BTW RBL5 AND RBL63 IS DOCUMENTED FAULT TTG8Q00CLVQD; SEE IN - [SDR SWAA2025011577167](https://openairdocs.org/sdr/SWAA2025011577167), Dec 13, 2024: ANGLE. CRACKED. CRACK ANGLE LOCATED BS663 AND LBL42 AT CENTER WING BOX 2024-759564<[01] REPLACED ANGLE LOCATED BS663 AND LBL5 TO LBL65 AT WING CENTER SECTION IAW B737 700 SRM 5 - [SDR SWAA2025011577169](https://openairdocs.org/sdr/SWAA2025011577169), Dec 13, 2024: ANGLE. CRACKED. CRACK ANGLE LOCATED BS663 AND RBL9 AT CENTER WING BOX 2024-759566<[01] REPLACED ANGLE AND FASTENERS LOCATED BS663 BTW RBL5 AND RBL63 AT CENTER WING BOX IAW B737 - [SDR SWAA2025011576780](https://openairdocs.org/sdr/SWAA2025011576780), Dec 13, 2024: ANGLE. CRACKED. CRACK ANGLE LOCATED STA294.5 AND STR13L AT PASSENGER CABIN 2024-759559<[01] REPLACED ANGLE AND FASTENERS LOCATED STA294.5 AND STR13L AT PASSENGER CABIN IAW B737 - [SDR SWAA2025011576778](https://openairdocs.org/sdr/SWAA2025011576778), Dec 13, 2024: TIE CLIP. CRACKED. CRACK TIE CLIP LOCATED BS360 AND STR8R PASSENGER CABIN 2024-759560<[01] REPLACED TIE CLIP LOCATED BS360 AND STR8R PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM - [SDR SWAA2025011576779](https://openairdocs.org/sdr/SWAA2025011576779), Dec 13, 2024: TIE CLIP. CRACKED. CRACK TIE CLIP LOCATED STA277 AND STR10R PASSENGER CABIN 2024-759558<[01] REPLACED TIE CLIP LOCATED STA277 AND STR10R PASSENGER CABIN IAW B737-700 SRM 51-10-02 - [SDR SWAA2025011576584](https://openairdocs.org/sdr/SWAA2025011576584), Dec 12, 2024: STRINGER. CRACKED. CRACK STRINGER 24R LOCATED BS540 AT FWD CARGO COMPARTMENT 2024-759518<[01] TOOL USED ON STEP 2: ULTRASONIC EQUIPMENT P/N 45MG; S/N;232019809; DUE DATE 08-OCT-25 - [SDR SWAA2025011576774](https://openairdocs.org/sdr/SWAA2025011576774), Dec 12, 2024: STRINGER. CRACKED. CRACK STRINGER 9 INTERNAL AREA FUEL TANK LOC. BTW RIB 21 AND RIB 22 UPPER SKIN LOWER SURFACE AFT AREA AT RT WING 2024-759516<[01] REPAIRED STRINGER 9 INTERNAL A - [SDR SWAA2025011576585](https://openairdocs.org/sdr/SWAA2025011576585), Dec 12, 2024: STRINGER. CRACKED. CRACK STRINGER 23R LOCATED BS540 AT FWD CARGO COMPARTMENT 2024-759517<[01] TOOL USED ON STEP 2:ULTRASONIC EQUIPMENT P/N 45MG; S/N;232019809; DUE DATE 08-OCT-25; - [SDR SWAA2025011576586](https://openairdocs.org/sdr/SWAA2025011576586), Dec 12, 2024: STRINGER. CRACKED. CRACK STRINGER 26R LOCATED BS540 AT FWD CARGO COMPARTMENT 2024-759519<[01] TOOL USED ON STEP 2: ULTRASONIC EQUIPMENT P/N 45MG; S/N;232019809; DUE DATE 08-OCT-25 - [SDR SWAA2025011576587](https://openairdocs.org/sdr/SWAA2025011576587), Dec 12, 2024: STRINGER. CRACKED. CRACK STRINGER 26L LOCATED BS540 AT FWD CARGO COMPARTMENT 2024-759520<[01] TOOL USED ON STEP 2: ULTRASONIC EQUIPMENT P/N 45MG; S/N;232019809; DUE DATE 08-OCT-25 - [SDR SWAA2025011576322](https://openairdocs.org/sdr/SWAA2025011576322), Dec 11, 2024: FRAME. CRACKED. CRACK FRAME LOCATED STA 440 AND BETWEEN STR 8R TO STR 9R AT PASSENGER CABIN 2024-759490<[01] REPAIRED FRAME LOCATED STA 440 AND BETWEEN STR 8R TO STR 9R AT PASS - [SDR SWAA2025011576323](https://openairdocs.org/sdr/SWAA2025011576323), Dec 11, 2024: FRAME. CRACKED. CRACK FRAME LOCATED STA 440 AND BETWEEN STR 8L TO STR 9L AT PASSENGER CABIN 2024-759491<[01] REPAIRED FRAME LOCATED STA 440 AND BETWEEN STR 8L TO STR 9L AT PASS - [SDR SWAA2025011576319](https://openairdocs.org/sdr/SWAA2025011576319), Dec 11, 2024: SUPPORT. CRACKED. CRACK SUPPORT ZEE LOCATED BETWEEN STA 747 TO STA 767 AND LBL 21 AFT CARGO COMPARTMENT 2024-759484<[01] REPAIRED SUPPORT ZEE AND FASTENERS SECTION LOCATED BETWEE - [SDR SWAA2025011576327](https://openairdocs.org/sdr/SWAA2025011576327), Dec 11, 2024: FRAME. CRACKED. CRACK FRAME LOCATED STA867 AND BETWEEN STR8R TO STR9R AT PASSENGER CABIN 2024-759492<[01] REPAIRED FRAME LOCATED STA867 AND BETWEEN STR8R TO STR9R AT PASSENGER - [SDR SWAA2025011576320](https://openairdocs.org/sdr/SWAA2025011576320), Dec 11, 2024: FRAME. CRACKED. CRACK FRAME LOCATED STA907 AND BETWEEN STR8R TO STR9R AT PASSENGER CABIN. REPAIRED FRAME LOCATED ON STA907 AND BETWEEN STR 7R TO STR 9R AT PASSENGER CABIN IAW E - [SDR SWAA2025011576321](https://openairdocs.org/sdr/SWAA2025011576321), Dec 11, 2024: FRAME. CRACKED. CRACK FRAME LOCATED STA 360 AND BETWEEN STR 8R TO STR 9R AT PASSENGER CABIN. REPAIRED FRAME LOCATED STA 360 AND BETWEEN STR 6R TO STR 9R AT PASSENGER CABIN IAW - [SDR SWAA2025011576333](https://openairdocs.org/sdr/SWAA2025011576333), Dec 11, 2024: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED STA867 AND BETWEEN STR2R TO STR3R AT PASSENGER CABIN 2024-759507<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 14281 - [SDR SWAA2025011575915](https://openairdocs.org/sdr/SWAA2025011575915), Dec 11, 2024: SKIN. CRACKED. CRACK ON LOWER SURFACE OF SLAT 7 AT RIGHT WING. PERFORMED REPAIR ON LOWER SURFACE OF SLAT 7 AT RIGHT WING SEE INDIVIDUAL SIGN OFF BELOW. APPLICABILITY EVALUATIO - [SDR SWAA2025011575914](https://openairdocs.org/sdr/SWAA2025011575914), Dec 10, 2024: HANDLE. DETERIORATED. DETERIORATE ASSIST HANDLE ASSY AFT SERVICE DOORWAY AT AFT GALLEY AREA 2024-759442<[01] REPLACED ASSIST HANDLE ASSY AFT SERVICE DOORWAY AT AFT GALLEY AREA IAW B7 - [SDR SWAA2025011575695](https://openairdocs.org/sdr/SWAA2025011575695), Dec 10, 2024: FLOORBEAM. CRACKED. CRACK ANGLE FLOOR STRUCTURE LOCATED STA540 AND RBL1 PASSENGER CABIN 2024-759431<[01] REPLACED ANGLE FLOOR STRUCTURE LOCATED STA540 AND RBL1 PASSENGER CABIN IAW - [SDR SWAA2025011575703](https://openairdocs.org/sdr/SWAA2025011575703), Dec 10, 2024: FLOORBEAM. CRACKED. CRACK ANGLE FLOOR STRUCTURE LOCATED STA540 AND LBL1 PASSENGER CABIN 2024-759432<[01] REPLACED ANGLE FLOOR STRUCTURE LOCATED STA540 AND LBL1 PASSENGER CABIN IAW - [SDR SWAA2025011575911](https://openairdocs.org/sdr/SWAA2025011575911), Dec 10, 2024: FILLER. CORRODED. CORROSION ON TAPERED FILLER LOCATED ON BS344 LOWER SURFACE OF STR26R AT E/E COMPARTMENT 2024-759461<[01] REPLACED TAPERED FILLER AND FASTENERS LOCATED ON BS344 - [SDR SWAA2025011575899](https://openairdocs.org/sdr/SWAA2025011575899), Dec 10, 2024: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET KRUEGER FLAP INTERNAL AREA LOCATED IFSS152 AT LT WING 2024-759460<[01] REPLACED SUPPORT BRACKET KRUEGER FLAP INTERNAL AREA LOCATED IFSS152 - [SDR SWAA2025011575290](https://openairdocs.org/sdr/SWAA2025011575290), Dec 9, 2024: SKIN. DEBONDED. CUSTOMER REQUEST - DEBONDED IB MAIN FLAP WEDGE PANEL LOWER SURFACE AT LT WING 2024-759336<[01] TOOL USED CALIPER PN: 500-196-30; SN: A23325649; DUE DATE: 31/DEC - [SDR SWAA2025011575114](https://openairdocs.org/sdr/SWAA2025011575114), Dec 9, 2024: FITTING. CRACKED. CRACK INDICATION FOUND IN UPPER BOLT HOLE LOCATED ON BS 727 FRAME INNER CHORD AREA AT S-18 A RH SIDE; CRACK DIRECTION: 3 OCLOCK. 2024-759236<[01] TOOL USED ON S - [SDR SWAA2025011575292](https://openairdocs.org/sdr/SWAA2025011575292), Dec 9, 2024: SKIN. DEBONDED. CUSTOMER REQUEST - DEBONDED IB MAIN FLAP WEDGE PANEL LOWER SURFACE AT RT WING. TOOL USED: POSITECTOR PN: NS2; SN: 110098; DUE DATE: 05/SEP/25.
TOOL USED: HOT - [SDR SWAA2025011575047](https://openairdocs.org/sdr/SWAA2025011575047), Dec 8, 2024: GUSSET. CRACKED. CRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2024-759209<[01] REPLACED GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 5 - [SDR SWAA2025011575046](https://openairdocs.org/sdr/SWAA2025011575046), Dec 8, 2024: GUSSET. CRACKED. CRACK GUSSET LOCATED STA500D AND STR19R FWD CARGO COMPARTMENT 2024-759210<[01] REPLACED GUSSET LOCATED STA500D AND STR19R FWD CARGO COMPARTMENT IAW B737-700 SRM - [SDR SWAA2024111861144](https://openairdocs.org/sdr/SWAA2024111861144), Nov 17, 2024: MODULE. FAULTY. ANTI SKID INOP LIGHT ILLUMINATED INFLIGHT. 32-44-21-000-801. OK TO CONTINUE PER MEL 32-2-01 SP1+SP2. PERFORMED AACU BITE CHECK PER FIM 32-42 TASK 801. FAULT BOX - [SDR SWAA2024111868440](https://openairdocs.org/sdr/SWAA2024111868440), Nov 17, 2024: CONTROL UNIT. FAULTY. ANTI SKID INOP LIGHT ILLUMINATED INFLIGHT. 32-44-21-000-801<[01] OK TO CONTINUE PER MEL 32-2-01 SP1+SP2;[02] PERFORMED AACU BITE CHECK PER FIM 32-42 TASK 801. F - [SDR SWAA2024111868441](https://openairdocs.org/sdr/SWAA2024111868441), Nov 17, 2024: ANTI-SKID VALVE. FAULTY. ANTI SKID INOP LIGHT ILLUMINATED INFLIGHT. 32-44-21-000-801<[01] OK TO CONTINUE PER MEL 32-2-01 SP1+SP2;[02] PERFORMED AACU BITE CHECK PER FIM 32-42 TASK 801. F All 229: https://openairdocs.org/aircraft/N7713A/reports.md ## STCs that may be installed (OpenAirDocs) (7) 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 series) - [STC SE04840NY](https://openairdocs.org/stc/SE04840NY): Installation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engine. Kilroy Aviation LLC. Lists CFM56-7B20 - [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. Lists CFM56-7B20 - [STC SE00032EN](https://openairdocs.org/stc/SE00032EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 Fan/Booster Module. Pratt & Whitney. Lists CFM56-3 - [STC SE00033EN](https://openairdocs.org/stc/SE00033EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 High Pressure Compressor Module. Pratt & Whitney. Lists CFM56-3 - [STC SE00034EN](https://openairdocs.org/stc/SE00034EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 High Pressure Turbine Module. Pratt & Whitney. Lists CFM56-3 - [STC SE00035EN](https://openairdocs.org/stc/SE00035EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 Low Pressure Turbine Module. Pratt & Whitney. Lists CFM56-3 - [STC SE00822CH](https://openairdocs.org/stc/SE00822CH): Install AeroControlex P/N 2604880-001 variable stator feedback control cable and P/N 2604880-002 variable bleed valve feedback control cable on CFM International engines. AeroControlex Group TransDigm Inc. Lists CFM56-2 ## Earlier aircraft with N7713A The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N7713A before. - [Cancelled 1974-11-08](https://openairdocs.org/deregistered/N7713A-1974-11-08): Cessna 180, S/N 32610. Owner: [Merillat James N](https://openairdocs.org/faa-owner/MERILLAT%20JAMES%20N), [Tecumseh, MI](https://openairdocs.org/faa-place/MI/Tecumseh) ## Related - Other Boeing 737-7BD aircraft: https://openairdocs.org/model/boeing-737-7bd/aircraft.md - The CFM International CFM56 series engine: https://openairdocs.org/engine/cfm-international-cfm56-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.