# N757LV: 1999 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 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (The Boeing Company) (OpenAirDocs) - Serial number: 29850 - Year built: 1999 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 29, 1999 - Certificate issued: December 1, 1999 - Expires: March 31, 2029 - Mode S code: AA3518 - 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=757LV - Page: https://openairdocs.org/aircraft/N757LV 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 737-7H4) 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/N757LV/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 (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB CHI04LA148](https://openairdocs.org/ntsb/CHI04LA148), Jun 4, 2004: Boeing 737-7H4 (N757LV), Liberal, KS, no damage. Probable cause: The adverse weather encountered during cruise flight by the flight crew and the flight attendant not being restrained. A contributing factor was the convective activity. ## NTSB investigations on N757LV not matched to an aircraft (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB FTW85FA159](https://openairdocs.org/ntsb/FTW85FA159), Mar 23, 1985: Cessna 152 (N757LV), Bixby, OK, destroyed, 1 fatal ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Accident 20040604029639A](https://openairdocs.org/incident/20040604029639A), Jun 4, 2004: Boeing 7377H4 (N757LV), Liberal, KS. (-23) On June 4, 2004, at 1817 central daylight time, a Boeing 737-7H4, N757LV, operated by southwest airlines co., as flight 2297, encountered turbulence… ## Reports on N757LV not matched to an aircraft (1) They name N757LV, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Accident 19850322020589A](https://openairdocs.org/incident/19850322020589A), Mar 22, 1985: Cessna 152 (N757LV), Bixby, OK, Destroyed. Made downwind simulated approach to a field. Nose pitched up and aircraft rolled and impacted the ground. ## Service difficulty reports (283, 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 SWAA2023071177258](https://openairdocs.org/sdr/SWAA2023071177258), Jul 11, 2023: LIGHT. INOPERATIVE. RH AFT EMERGENCY EXIT LIGHT INOP<[01] RELAMPED AFT RH EMERGENCY EXIT PER AMM 33-51-03. - [SDR SWAA2023052552088](https://openairdocs.org/sdr/SWAA2023052552088), May 25, 2023: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT BATTERY PACK AT LOCATION M1673 (AFT LEFT SIDE)<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT LOCATION M1673 OPS CHECK GOOD PER AMM 3 - [SDR SWAA2023020900860](https://openairdocs.org/sdr/SWAA2023020900860), Feb 9, 2023: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT BEHIND THE AFT SERVICE DOOR IS INOP.<[01] REMOVED AND REPLACED AFT EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06 - [SDR SWAA2022102764130](https://openairdocs.org/sdr/SWAA2022102764130), Oct 25, 2022: NONE. NONE. FUEL QTY DROPPED 1100 LBS IN LEFT WING IN 20 MINUTES; WITH IMBALANCE OF 1100LBS. SHUT ENGINE DOWN PER QRH. AFTER BURNING FUEL FROM ENG 2; BALANCE WAS ACHIEVED / - [SDR SWAA2022102161711](https://openairdocs.org/sdr/SWAA2022102161711), Oct 20, 2022: PANEL. DELAMINATED. LEFT WING PANEL 521 YB OUTBOARD EDGE DELAMINATED. 2INCHES FROM LEADING EDGE. 1.5 INCH WIDE BY 3 INCH LONG / [01] ACCOMPLISHED TEMP REPAIR PER EA-GENERAL CLEANED - [SDR SWAA2022082344459](https://openairdocs.org/sdr/SWAA2022082344459), Aug 21, 2022: LIGHT. OUT OF POSITION. FA REPORTS AFT EXIT SIGN FELL OFF / [01] R/R'D AFT SIGN ASSY. PER MM 33-51-01. - [SDR SWAA2022080839146](https://openairdocs.org/sdr/SWAA2022080839146), Aug 5, 2022: TAB. LOOSE. FA ADVISES THAT THE FWD SERVICE DOOR SLIDE MANUEL INFLATION PULL TAB HANGS OUT WHEN THE GIRT BAR IS ARMED / [01] RESECURED VELCRO NEAR GIRT BAR ON FWD SERVICE D - [SDR SWAA2022072833419](https://openairdocs.org/sdr/SWAA2022072833419), Jul 25, 2022: FLAP. DELAMINATED. FLAP WAS FOUND WITH DELAMINATION / [01] FLAP REMOVED AND REPLACED. OPS AND ADJUSTMENT CHECKS GOOD IAW AMM 27-51-12;[02] C/W OPS AND ADJUSTMENT CHECK - [SDR SWAA2022012463246](https://openairdocs.org/sdr/SWAA2022012463246), Jan 22, 2022: ENGINE. FAILED. AT 38000 FT THE R/H #2 ENG OIL/QAUATIY SHOWS 20 % ENG INSTRURMENTS FLASHED WHITE BOX AND OTHER ENGINE INSTRUMENTS ARE NORMAL. DECENT #2 QUAITY SLOWY WENT DOWN T - [SDR SWAA2021111532131](https://openairdocs.org/sdr/SWAA2021111532131), Oct 21, 2021: RIB. CRACKED. CRACK LEADING EDGE RIB STA 86.66 AT RT HORIZONTAL STABILIZER ; 2021-462044 / [01] REPLACED LEADING EDGE RIB STA 86.66 AT RT HORIZONTAL STABILIZER IAW B737-700 S - [SDR SWAA2021111531785](https://openairdocs.org/sdr/SWAA2021111531785), Oct 19, 2021: NONE. CRACKED. CRACK ANGLE FLOOR STRUCTURE BETWEEN BS 685 TO BS 706 AT LEVEL RBBL 0.07 CENTER SECTION ; 2021-462040 / [01] REPLACED ANGLE FLOOR STRUCTURE BETWEEN BS 685 TO BS - [SDR SWAA2021111531786](https://openairdocs.org/sdr/SWAA2021111531786), Oct 19, 2021: STRUCTURE. CRACKED. CRACK ANGLE FLOOR STRUCTURE BETWEEN BS 685 TO BS 706 AT LEVEL RBBL 24.5 CENTER SECTION ; 2021-462041 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES000 - [SDR SWAA2021111530902](https://openairdocs.org/sdr/SWAA2021111530902), Oct 16, 2021: NONE. CORRODED. CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS 767 TO BS 794.3 STR 25R WL 156 RBL2184 AT AFT CARGO COMPARTMENT ; 2021-461994 / [01] REPLACED WEB - INTERCOSTAL L - [SDR SWAA2021111530901](https://openairdocs.org/sdr/SWAA2021111530901), Oct 16, 2021: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 767 STR 25R WL156 RBL21.84 AT AFT CARGO COMPARTMENT ; 2021-461993 / [01] REPLACED SUPPORT ZEE LOCATED BETWEEN - [SDR SWAA2021111530903](https://openairdocs.org/sdr/SWAA2021111530903), Oct 16, 2021: NONE. CORRODED. CORROSION SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 847 STR 25L WL156 LBL21.84 AT AFT CARGO COMPARTMENT ; 2021-461995 / [01] REPLACED SUPPORT ZEE LOCATED BETWEEN - [SDR SWAA2021111530898](https://openairdocs.org/sdr/SWAA2021111530898), Oct 15, 2021: TIE CLIP. CRACKED. CRACK BILGE AREA TIE CLIP LOCATED STA 500D AND STR 26L AT FWD CARGO COMPARTMENT ; 2021-461992 / [01] REPLACED TIE CLIP AND FASTENER LOCATED STA 500D AND STR 26L - [SDR SWAA2021111530899](https://openairdocs.org/sdr/SWAA2021111530899), Oct 15, 2021: TIE CLIP. CRACKED. CRACK BILGE AREA TIE CLIP LOCATED STA 500D AND STR 26R AT FWD CARGO COMPARTMENT ; 2021-461991 / [01] REPLACED TIE CLIP AND FASTENER LOCATED STA 500D AND STR 26R - [SDR SWAA2021111530900](https://openairdocs.org/sdr/SWAA2021111530900), Oct 15, 2021: ANGLE. CRACKED. CRACK ANGLE - CLIP LOCATED BS 400 AND STRINGER 26L AT FWD CARGO COMPARTMENT ; 2021-461990 / [01] TOOL USED DIGITAL CALIPER
P/N: 500-172-30 S/N: 15237811 DUE - [SDR SWAA2021111529726](https://openairdocs.org/sdr/SWAA2021111529726), Oct 13, 2021: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE BETWEEN WS 236 TO WS 285 ON REAR SPAR AT RT WING ; 2021-461956 / [01] REPLACED ANGLE LOCATED TRAILING EDGE BETWEEN WS 236 TO WS 285 ON - [SDR SWAA2021111529730](https://openairdocs.org/sdr/SWAA2021111529730), Oct 13, 2021: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE AREA OF ACCESS PANEL 651GB AT RT WING ; 2021-461958 / [01] REPLACED ANGLE TRAILING EDGE AREA OF ACCESS PANEL 651GB AT RT WING IAW SRM - [SDR SWAA2021111529703](https://openairdocs.org/sdr/SWAA2021111529703), Oct 12, 2021: SKIN. CRACKED. CRACK ON INTERNAL SKIN CUT OUT LOWER POSITION GROUND SERVICE DOOR 114AR ; 2021-461865 / [01] TOOL USED EDDY CURRENT EQUIPMENT P/N NORTEC 500D; S/N :00X12101V022 - [SDR SWAA2021111529181](https://openairdocs.org/sdr/SWAA2021111529181), Oct 12, 2021: BATTERY PACK. INOPERATIVE. INOP UPPER BATTERY PACK ON FWD AREA GALLEY (2EA) ; 2021-461844 / [01] REPLACED POWER SUPPLY-BATTERY PACK M1674; M1675 ON FWD PAX CABIN; LIGHTS TEST ARE OK. IAW - [SDR SWAA2021111129710](https://openairdocs.org/sdr/SWAA2021111129710), Oct 12, 2021: STRINGER. CRACKED. CRACK STRINGER 25R AT BS 540 FWD CARGO COMPARTMENT ; 2021-461921 / [01] TOOL USED: ULTRASONIC EQUIPMENT: P/N: 45 MG; S/N: 130064101 DUE DATE: 11-MAR-22; [02] TO - [SDR SWAA2021111129709](https://openairdocs.org/sdr/SWAA2021111129709), Oct 12, 2021: STRINGER. CRACKED. CRACK STRINGER 26R AT BS 540 FWD CARGO COMPARTMENT ; 2021-461920 / [01] TOOL USED: P/N: NORTEC 600D; S/N: 210138003; DUE DATE: 05-MAR-22; [02] TOOL USED PRECISI - [SDR SWAA2021111129713](https://openairdocs.org/sdr/SWAA2021111129713), Oct 12, 2021: STRINGER. CRACKED. CRACK STRINGER 26L AT BS 540 FWD CARGO COMPARTMENT ; 2021-461919 / [01] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N 45MG; S/N: 130061901; DUE DATE: 11 MAY 22.; [0 - [SDR SWAA2021111129712](https://openairdocs.org/sdr/SWAA2021111129712), Oct 12, 2021: STRINGER. CRACKED. CRACK STRINGER 25L AT BS 540 FWD CARGO COMPARTMENT ; 2021-461918 / [01] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N 45MG; S/N: 130061901; DUE DATE: 11 MAY 22.; [0 - [SDR SWAA2021111129711](https://openairdocs.org/sdr/SWAA2021111129711), Oct 12, 2021: STRINGER. CRACKED. CRACK STRINGER 21L AT BS 540 FWD CARGO COMPARTMENT ; 2021-461917 / [01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N: 35DL S/N: 091419910 DUE DATE: 30-NOV-21.; [02] - [SDR SWAA2021111128672](https://openairdocs.org/sdr/SWAA2021111128672), Oct 10, 2021: LIGHT. BROKEN. BROKEN GALLEY 1 EMERGENCY EXIT LIGHT ASSY AT FWD GALLEY AREA ; 2021-461580 / [01] REPLACED GALLEY 1 EMERGENCY EXIT LIGHT ASSY AT FWD GALLEY AREA IAW B737-700 AM - [SDR SWAA2021111528655](https://openairdocs.org/sdr/SWAA2021111528655), Oct 9, 2021: NONE. CRACKED. CRACK EXTERNAL SKIN LOCATED SLAT 6 AT LEVEL SLAT STATION 202.45 AT RT WING ; 2021-461484 / [01] REMOVED ACCESS PANEL 623DB AND FLEX SKIN LOC SLAT 6 AT LEVEL SLA - [SDR SWAA2021111528656](https://openairdocs.org/sdr/SWAA2021111528656), Oct 9, 2021: NONE. CRACKED. CRACK EXTERNAL SKIN LOCATED SLAT 4 AT LEVEL SLAT STATION 85.19 AT LT WING ; 2021-461488 / [01] REMOVED ACCESS PANEL 522DB AND FLEX SKIN LOC SLAT 4 AT LEVEL SLAT - [SDR SWAA2021072997629](https://openairdocs.org/sdr/SWAA2021072997629), Jul 26, 2021: LINE. BROKEN. HAD A LOSS OF HYDRAULIC QTY. IN FLIGHT; COMPLIED WITH QRH FOR LOSS OF HYD A; NORMAL LANDING SPEED; TOUCH DOWN WAS NORMAL. ; / [01] FOUND NOSE LANDING GEAR TRANS - [SDR SWAA2020122838588](https://openairdocs.org/sdr/SWAA2020122838588), Dec 23, 2020: LENS. DETACHED. L1 DOOR LOWER EMERGENCY EXIT SIGN LENS FELL OFF. DMA # 0414460 R & R EXIT 1 BL ASSEMBLY ON L1 ENTRANCE, REF AMM 35-51-01 CL NR 64016. - [SDR SWAA2020111630483](https://openairdocs.org/sdr/SWAA2020111630483), Nov 12, 2020: SLIDE. LOOSE. L2 AFT EMERGENCY SLIDE IS LOOSE. INSPECTED L2 SLIDE, IAW AMM 25-66-01 NO DEFECTS FOUND R1 SLIDE SLIGHTLY LOOSE. REMOVED RESECURED, IAW MT 725-61-06, AIRCRAFT OK - [SDR SWAA2020082010007](https://openairdocs.org/sdr/SWAA2020082010007), Jun 18, 2020: HMU. SLOW. WAIVE DESCENDING FOR TURBULENCE 400-380 NO PROBLEMS NOTED AFTER DESCENT AND LEVELING @ 380 ENGINE WAS SLOW TO POWER UP (AUTO THROTTLES ON) DESCENDED TO 360 AND - [SDR SWAA2020061291274](https://openairdocs.org/sdr/SWAA2020061291274), Jun 10, 2020: LIGHT. LOOSE. EMERGENCY EXIT LIGHTING FLOOR STRIP AT ROW 8 LOOSE. SECURED FLOOR PROXIMITY LIGHT STRIP PER AMM 33-51-15. - [SDR SWAA2020022841918](https://openairdocs.org/sdr/SWAA2020022841918), Feb 26, 2020: LIGHT. BROKEN. CENTER AISLE EMERGENCY LIGHT BROKEN. / R&R LIGHT ASSEMBLY PER MM. - [SDR SWAA2020012840829](https://openairdocs.org/sdr/SWAA2020012840829), Jan 26, 2020: LIGHT. INOPERATIVE. L1 DOOR EMERGENCY LIGHT INOP. R&R LIGHT ASSEMBLY IAW AMM. - [SDR SWAA2020011640495](https://openairdocs.org/sdr/SWAA2020011640495), Jan 14, 2020: LIGHT. INOPERATIVE. LT OVERWING EXIT DOOR SIDEWALL LIGHT INOP. R&R LIGHT ASSEMBLY PER MM. - [SDR SWAA2019120339300](https://openairdocs.org/sdr/SWAA2019120339300), Dec 2, 2019: SLIDE. LOOSE. L1 DOOR SLIDE NEEDED REPACKED. / STOWED SLIDE PER MT. - [SDR SWAA2019110638648](https://openairdocs.org/sdr/SWAA2019110638648), Nov 5, 2019: LIGHT. INOPERATIVE. R/H EMERGENCY EXIT DOOR, LOWER AFT LIGHT IS INOP. / RELAMPED R/H EMERGENCY EXIT DOOR, LOWER AFT LIGHT. - [SDR SWAA2022032385028](https://openairdocs.org/sdr/SWAA2022032385028), Oct 25, 2019: DOUBLER. DEBONDED. FAIRING PANEL #192F DME ANTENNA NUTPLATE DOUBLER COMMON TO FAIRING IS DISBONDED / INSTALLED FAIRING PANEL 192F DME ANTENNA NUTPLATE IAW AMM 51-31-00-390-801 AND - [SDR SWAA2019102238125](https://openairdocs.org/sdr/SWAA2019102238125), Oct 15, 2019: SUPPORT ANGLE. CORRODED. AFT CARGO BAY BULKHEAD TO FLOOR PANEL LOWER SUPPORT ANGLE CORRODED AT BS. 947, RBL 24. / R&R ANGLE IAW SRM & DWG. - [SDR SWAA2022040685020](https://openairdocs.org/sdr/SWAA2022040685020), Oct 14, 2019: FLOOR SUPPORT. CRACKED. FLOOR SUPPORT CRACKED AT BS 277-294 BL 0 WL 208 / REMOVED CRACK DAMAGED FLOOR SUPPORT AT BS277-294 BL0 WL208 IAW SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW FLOOR - [SDR SWAA2022040485019](https://openairdocs.org/sdr/SWAA2022040485019), Oct 14, 2019: FLOOR PANEL. DELAMINATED. FLOORPANEL 221BF HAS DELAMINATION AND BROKEN INSERTS / REPLACED FLOOR PANEL 221BF DUE TO DELAMINATION AND BROKEN INSERTS. FLOOR PANEL 221BF WILL BE INSTALLED ON - [SDR SWAA2019110638646](https://openairdocs.org/sdr/SWAA2019110638646), Oct 10, 2019: SKIN. DAMAGED. DAMAGED FUSELAGE SKIN BS 1040+6" TO 1040+13" STR 1" ABOVE 23R TO 2" ABOVE 24R REQUIRES SKIN REPAIR (REFERENCE CUSTOMER CARDS T986010,T986011,T986013, T986014, T - [SDR SWAA2022040585008](https://openairdocs.org/sdr/SWAA2022040585008), Oct 8, 2019: ANGLE. CRACKED. FOUND CRACKED SUPPORT ANGLES BEHIND WATER SERVICE PANEL AT ACB BS907+9 RBL12 WL170. MARKED / REMOVED & REPLACED THE SUPPORT ANGLES BEHIND WATER SERVICE PAN A.C. - [SDR SWAA2022040585007](https://openairdocs.org/sdr/SWAA2022040585007), Oct 8, 2019: STRAP. CORRODED. ***CORROSION*** ON TENSION STRAP AT AFT CARGO BAY BS 847 RBL8 WL163. MARKED / AREAS FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 FIG 103.D LOCATED AND DRILLE - [SDR SWAA2019110638644](https://openairdocs.org/sdr/SWAA2019110638644), Oct 8, 2019: FRAME. DENTED. DENT ON THE FRAME AT AFT CARGO BAY BS 727C 3" ABOVE S-22R WL173. / REPAIRED PER: EA 1-753-35959 REV IR AND ATS ER 19-05297 REV IR. - [SDR SWAA2019102338153](https://openairdocs.org/sdr/SWAA2019102338153), Oct 8, 2019: SUPPORT. CORRODED. AFT CARGO BAY FLOOR PANEL SUPPORT SPLICE CORRODED AT BS. 727D+6, BETWEEN LBL 19 TO RBL 19. / R&R SUPPORT SPLICE PER PO. - [SDR SWAA2019102338152](https://openairdocs.org/sdr/SWAA2019102338152), Oct 8, 2019: SPLICE. CORRODED. AFT CARGO BAY FLOOR PANEL SUPPORT SPLICE CORRODED AT BS. 767+6, BETWEEN LBL 19 TO RBL 19. / R&R SPLICE PER WO. All 283: https://openairdocs.org/aircraft/N757LV/reports.md ## STCs that may be installed (OpenAirDocs) (37) 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 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 N757LV The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N757LV before. - [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N757LV-undated): Cessna 152, S/N 15279833. Triennial form not returned ## Related - Other Boeing 737-7H4 aircraft: https://openairdocs.org/model/boeing-737-7h4/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.