# N425LV: 2002 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: 29829 - Year built: 2002 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: April 5, 2002 - Certificate issued: September 18, 2002 - Expires: May 31, 2028 - Mode S code: A50F40 - 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=425LV - Page: https://openairdocs.org/aircraft/N425LV 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/N425LV/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 N425LV. ## FAA accident and incident reports None matched to N425LV. ## Service difficulty reports (272, 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 SWAA2025091915929](https://openairdocs.org/sdr/SWAA2025091915929), Sep 17, 2025: LIGHT. LOOSE. FWD.GALLEY PHOTOILUMINESCENT EMERG. STRIP LOOSE<[01] RE-SECURED LIGHT STRIP PER AMM 33-51-15. - [SDR SWAA2025050565743](https://openairdocs.org/sdr/SWAA2025050565743), Apr 30, 2025: LIGHT. INOPERATIVE. AFT LT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] RESEATED AFT LH SLIDE LIGHT PER AMM 33-51-04.OPS OK - [SDR SWAA2025050164977](https://openairdocs.org/sdr/SWAA2025050164977), Apr 28, 2025: GLOWSTRIP. INOPERATIVE. GLOW IN THE DARK FLOOR STRIPS NOT ILLUMINATING; 1 ROW 1 FO SIDE; 2 AFT CABIN LAV AND AFT BULKHEAD.<[01] REMOVED AND REPLACED PHOTOLUMINESCENT STRIP AT ROW 1DEF - [SDR SWAA2025042826228](https://openairdocs.org/sdr/SWAA2025042826228), Apr 18, 2025: SKIN. DAMAGED. APU DOOR CREASED ANT AFT HINGE AREA.<[01] OK TO INSTALL APU FIRE BLANKET ON SERVICEABLE APU COWL DOOR.;[02] 01 - REMOVED AND REPLACED PER [AMM 52-48-21-401-NG ( - [SDR SWAA2025042825938](https://openairdocs.org/sdr/SWAA2025042825938), Apr 18, 2025: BRACKET. CRACKED. L/H WHEEL WELL STA.663 BULKHEAD; UPPER O/B BRACKET THAT SUPPORTS UPPER WING PANEL CRACKED. REMOVED BRACKET PER SRM 51-40-02. INSTALLED BRACKET IAW SRM 51-40-02. - [SDR SWAA2025042825939](https://openairdocs.org/sdr/SWAA2025042825939), Apr 18, 2025: PANEL. PULLED. PANEL 193D FASTENERS ARE PULLED THROUGH THE PANEL. REMOVED AND REPLACED PANEL 193D FASTENERS AND PANEL. I.A.W. SRM 51-40-02. - [SDR SWAA2025042825925](https://openairdocs.org/sdr/SWAA2025042825925), Apr 18, 2025: RETAINER. CRACKED. RIGHT HORIZONTAL STABILIZER UPPER AFT SLIDER SEAL RETAINER CRACKED. REMOVED AND REPLACED SEAL RETAINER PER SRM 51-40-02. - [SDR SWAA2025042836914](https://openairdocs.org/sdr/SWAA2025042836914), Apr 18, 2025: BRACKET. CRACKED. L/H WHEEL WELL STA.663 BULKHEAD; UPPER O/B BRACKET THAT SUPPORTS UPPER WING PANEL CRACKED. REMOVED BRACKET PER SRM 51-40-02. INSTALLED BRACKET IAW SRM 51-40-02. - [SDR SWAA2025042825937](https://openairdocs.org/sdr/SWAA2025042825937), Apr 18, 2025: RETAINER. CRACKED. L/H HORIZONTAL STABILIZER UPPER AFT SLIDER SEAL RETAINER CRACKED.<[01] R&R?D L/H HORIZONTAL STAB UPPER AFT SLIDER SEAL PER SRM 51-40-02.;[02] INSPECTION C/W - [SDR SWAA2025042225914](https://openairdocs.org/sdr/SWAA2025042225914), Apr 18, 2025: SLIDE. LOOSE. FWD ENTRY DOOR SLIDE HAS A LOOSE ATTACH FASTENER<[01] R&R FWD ENTRY DOOR SLIDE ATTACH FASTENER IAW AMM 52-11-31 AND AMM 20-50-11.;[02] INSP PER AMM 52-11-31 AND - [SDR SWAA2025041423964](https://openairdocs.org/sdr/SWAA2025041423964), Apr 12, 2025: LAMP. INOPERATIVE. EMERGENCY LIGHT BY L2 DOOR IS INOP<[01] RELAMPED EXTERIOR EMERGENCY LIGHT AT L2 IAW AMM 33-51-04 - [SDR SWAA2025030300821](https://openairdocs.org/sdr/SWAA2025030300821), Feb 28, 2025: GIRT BAR. OUT OF ADJUST. LEFT FORWARD ENTRY DOOR GIRT BAR STOW BRACKET BROKEN <[01]. R/R MOUNT RIVITS PER SRM 51-40-02. - [SDR SWAA2025012790005](https://openairdocs.org/sdr/SWAA2025012790005), Jan 26, 2025: BRACKET. OUT OF ADJUST. GIRT BAR RETAINING BRACKET OFF THE CASE FORWARD ENTRY DOOR.<[01] RESECURED L-1 DOOR; FWD ENTRY DOOR SLIDE GIRT BAR RETAINING BRACKET. OPS NORMAL. REF SRM 51-40- - [SDR SWAA2024091838474](https://openairdocs.org/sdr/SWAA2024091838474), Sep 16, 2024: SLIDE. LOOSE. FWD ENTRY DOOR SLIDE CAME LOOSE ON OPENING.<[01] INSTALLED DOOR SLIDE PER M/M 25-66-01 AND COMPLIED
WITH MT 725-61-06 - [SDR SWAA2024050782945](https://openairdocs.org/sdr/SWAA2024050782945), May 6, 2024: SIGN. DETACHED. MID CABIN EMERGENCY EXIT SIGN KNOCKED LOOSE<[01] REMOVED AND REPLACED MID CABIN EMERGENCY EXIT SIGN. OPS OK AT THIS TIME. REF AMM 33-51-01 - [SDR SWAA2024041774589](https://openairdocs.org/sdr/SWAA2024041774589), Apr 14, 2024: SEAT BACK. OUT OF ADJUST. ROW 12 ABC BACK RECLINING MECHANISM INOP.<[01] SEAT REMAIN UPRIGHT WITHOUT PASSENGER AND DOES NOT BLOCK EGRESS. A/C OK TO CONTINUE PER MEL 25-6-01 MDDR#188666 S - [SDR SWAA2024013045409](https://openairdocs.org/sdr/SWAA2024013045409), Jan 27, 2024: SCUFF PLATE. CRACKED. CRACK ON AFT CORNER SCUFF PLATE OF AFT CARGO COMPARTMENT 2024-67376. REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700; - [SDR SWAA2024021243908](https://openairdocs.org/sdr/SWAA2024021243908), Jan 23, 2024: ACCESS PANEL. CRACKED. CRACK ACCESS PANEL 632NB ON FLOAT FUEL TANK AT RT WING 2024-67341<[01] REPLACED FUEL TANK FLOAT AT RT WING ON ACCESS PANEL 632NB IAW B737-700 CMM 28-40-11 SAFRA - [SDR SWAA2024021243909](https://openairdocs.org/sdr/SWAA2024021243909), Jan 23, 2024: ACCESS PANEL. CRACKED. CRACK ACCESS PANEL 632QB ON FLOAT FUEL TANK AT RT WING 2024-67340<[01] REPLACED FUEL TANK FLOAT AT RT WING ON ACCESS PANEL 632QB IAW B737-700 CMM 28-40-11 SAFRA - [SDR SWAA2024021243573](https://openairdocs.org/sdr/SWAA2024021243573), Jan 22, 2024: ACCESS PANEL. DAMAGED. ELONGATED HOLE ACCESS PANEL 661BB TRAILING EDGE AT RT WING 2024-67333<[01] TOOL USED CALIPER PN: 500-197-30; SN: 15120589; DUE DATE: 13/FEB/24.;[02] TOOL USED H - [SDR SWAA2024021243112](https://openairdocs.org/sdr/SWAA2024021243112), Jan 20, 2024: PLATE. CRACKED. CRACK PLATE ASSY TRAILING EDGE LOCATED ORSS284 AT RT WING 2024-67271<[01] REPLACED PLATE ASSY TRAILING EDGE LOCATED BTW ORSS278 TO ORSS321 AT RT WING IAW B737-7 - [SDR SWAA2024021243111](https://openairdocs.org/sdr/SWAA2024021243111), Jan 20, 2024: PLATE. CRACKED. CRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED ON IRSS 217 AT LT WING 2024-67260<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ON IRSS 217 AT LT WING IA - [SDR SWAA2024021243105](https://openairdocs.org/sdr/SWAA2024021243105), Jan 20, 2024: RAIL. CRACKED. CRACK TRAILING EDGE ON RAIL LOCATED ORSS 559 AT RT WING 2024-67270<[01] REPLACED RAIL LOCATED ON TRAILING EDGE ORSS 559 AT RT WING IAW B737-700 SRM 51-40-02 AND - [SDR SWAA2024021248664](https://openairdocs.org/sdr/SWAA2024021248664), Jan 20, 2024: RIB. CRACKED. CRACK ON INBOARD FIXED TRAILING EDGE DEFLECTION CONTROL RIB AT RT WING 2024-67274<[01] TOOL USED: EDDY CURRENT EQUIPMENT. P/N: NORTEC 600D. S/N: 200048001. DUE - [SDR SWAA2024021243106](https://openairdocs.org/sdr/SWAA2024021243106), Jan 20, 2024: PLATE. CRACKED. CRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED IRSS232 AT RT WING 2024-67273<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS232 AT RT WING IAW B737-7 - [SDR SWAA2024013144777](https://openairdocs.org/sdr/SWAA2024013144777), Jan 20, 2024: BRACKET. CRACKED. CRACK BRACKET LOCATED BS 867 BETWEEN S-2R TO S-3R AT PASSENGER CABIN 2024-67266<[01] REPLACED BRACKET LOCATED AT BS 867 BETWEEN S-2R TO S-3R AT PASSENGER CABIN - [SDR SWAA2024021242507](https://openairdocs.org/sdr/SWAA2024021242507), Jan 19, 2024: RIB. CRACKED. CRACK INSPAR RIB LOCATED STAB STA 129.50 AND 28 INCH FROM FRONT SPAR LT HORIZONTAL STAB 2024-67217<[01] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N50 - [SDR SWAA2024020942505](https://openairdocs.org/sdr/SWAA2024020942505), Jan 19, 2024: STRINGER. CRACKED. CRACK STRINGER 26L LOCATED BS540 FWD CARGO COMPARTMENT 2024-67221<[01] TOOL USED: ULTRASONIC THICKNESS GAUGE; PN: 45MG; SN: 130066701 ; DUE DATE: 09-JUN-24;[02] - [SDR SWAA2024020942504](https://openairdocs.org/sdr/SWAA2024020942504), Jan 19, 2024: STRINGER. CRACKED. CRACK STRINGER 24L LOCATED BS540 FWD CARGO COMPARTMENT 2024-67220<[01] TOOL USED: ULTRASONIC THICKNESS GAUGE; PN: 45MG; SN: 130066701 ; DUE DATE: 09-JUN-24;[02] - [SDR SWAA2024020942041](https://openairdocs.org/sdr/SWAA2024020942041), Jan 18, 2024: LENS. BROKEN. BROKEN EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA 2024-67149<[01] REPLACED EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA IAW B737-700 AMM - [SDR SWAA2024021242024](https://openairdocs.org/sdr/SWAA2024021242024), Jan 17, 2024: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED AT LEVEL STA 695 AND LBL 24.82 AT PASSENGER CABIN 2024-67101<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112820025 - [SDR SWAA2024021242025](https://openairdocs.org/sdr/SWAA2024021242025), Jan 17, 2024: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE AT LEVEL STA 695 AND LBL 0.07 AT PASSENGER CABIN 2024-67100<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112820025 DUE DATE - [SDR SWAA2023082392319](https://openairdocs.org/sdr/SWAA2023082392319), Aug 21, 2023: MEGAPHONE. INOPERATIVE. FWD GALLEY MEGAPHONE INOP<[01] REPLACED MEGAPHONE AND BATTERY'S PER AMM 25-64-00. AIRCRAFT OK FOR SERVICE. - [SDR SWAA2023082191216](https://openairdocs.org/sdr/SWAA2023082191216), Aug 17, 2023: LIGHT. OUT OF ADJUST. CABIN AFT GALLEY CEILING CENTER EMERGENCY EXIT LIGHT NOT MOUNTED TO CEILING ON L/H SIDE.<[01] REMOVED AND REPLACED AFT CEILING EMERGENCY EXIT LOCATOR LIGHT PER - [SDR SWAA2023082191222](https://openairdocs.org/sdr/SWAA2023082191222), Aug 17, 2023: GIRT BAR. OUT OF ADJUST. FWD ENTRY DOOR ESCAPE SLIDE GIRT FLAP NOT PROPERLY SECURED.<[01] RE-SECURED FWD ENTRY DOOR ESCAPE SLIDE GIRT FLAP REF AMM SIP. - [SDR SWAA2023072079929](https://openairdocs.org/sdr/SWAA2023072079929), Jul 18, 2023: SIGN. LOOSE. EXIT ROW EMERGENCY EXIT SIGN OF FO SIDE FALLING OFF<[01] RESECURED EMERGENCY EXIT SIGN REF AMM 25-21-20 - [SDR SWAA2023042027249](https://openairdocs.org/sdr/SWAA2023042027249), Apr 14, 2023: BRACKET. CRACKED. AFT GALLEY SERVICE DOOR LOWER GATE PAN CRACKED BOTH FRONT AND BACK<[01] REMOVED AND REPLACED FWD AND AFT BRACKETS ON AFT SERVICE DOOR LOWER GATE PER SRM 51-40-0 - [SDR SWAA2023041927249](https://openairdocs.org/sdr/SWAA2023041927249), Apr 14, 2023: BRACKET. CRACKED. AFT GALLEY SERVICE DOOR LOWER GATE PAN CRACKED BOTH FRONT AND BACK<[01] REMOVED AND REPLACED FWD AND AFT BRACKETS ON AFT SERVICE DOOR LOWER GATE PER SRM 51-40-0 - [SDR SWAA2023041928038](https://openairdocs.org/sdr/SWAA2023041928038), Apr 14, 2023: FAIRING. CRACKED. R/H WING TO BODY WEDGE FAIRING AFT OF MAIN WHEEL WELL CRACKED.<[01] REMOVED BROKEN R/H WING TO BODY WEDGE FAIRING PER SIP;[02] REMOVED AND REPLACED R/H WING TO - [SDR SWAA2022121481159](https://openairdocs.org/sdr/SWAA2022121481159), Dec 13, 2022: INDICATOR. FAULTED. FLAPS FAILED TO RETRACT AFTER TAKEOFF. LEFT FLAP STOPPED AT 2; RIGHT FLAP STOPPED AT 1. PERFORMED FIM 27-51-00-810-836 FOUND FAULT 27-52259 ON FSEU BITE (TE FLA - [SDR SWAA2022121380776](https://openairdocs.org/sdr/SWAA2022121380776), Dec 12, 2022: FLAP SYSTEM. FAULTED. FLAP LOCK OUT ON APPROACH. FLAPS 30 SELECTED, LT FLAP 20 & RT 27. FLT CREW STATED THAT THEY SELECTED FLAPS 15 AFTER LOCKOUT OCCURED. THE FLAPS STAYED AT THEIR L - [SDR SWAA2022100552079](https://openairdocs.org/sdr/SWAA2022100552079), Oct 3, 2022: LIGHT. DETACHED. ESCAPE PATH LIGHTING AT ROW 8 IS COMING UP / [01] RESECURED FLOOR PATH LIGHTING REF MM 25-27-31 - [SDR SWAA2022093049388](https://openairdocs.org/sdr/SWAA2022093049388), Sep 30, 2022: NONE. INOPERATIVE. FWD SERVICE DOOR EXTERIOR EMERGENCY INOP / [01] RELAMPED FWD SERVICE DOOR EXTERIOR EMERGENCY LIGHT
REF AMM 33-51-04. OPS CHECKS GOOD A/C GOOD TO GO. - [SDR SWAA2022081641899](https://openairdocs.org/sdr/SWAA2022081641899), Aug 15, 2022: LIGHT. INOPERATIVE. PASSENGER ROW 14 CBA EMERGENCY EXIT LIGHT INOP / [01] RELAMP PASSENGER ROW 14CBA EMERGENCY EXIT LAMP IAW AMM 33-51-03 OPS CHECK GOOD - [SDR SWAA2022080839599](https://openairdocs.org/sdr/SWAA2022080839599), Aug 8, 2022: FLAP. DETACHED. FWD ENTRY DOOR SLIDE MANUAL DEPLOY FLAP DETACHED / [01] RESECURED MANUAL DEPLOY VELCRO FLAP COVER ON SLIDE AS REQUIRED PER AMM 25-66-01. A/C OK FOR SERVICE. - [SDR SWAA2022040186667](https://openairdocs.org/sdr/SWAA2022040186667), Mar 23, 2022: BATTERY PACK. INOPERATIVE. EMERGENCY BATTERY PACK AT PASSENGER ENTRY CEILING PANEL (M1674) INOP. / [01] REPLACED EMERGENCY BATTERY PACK M1674 AS PER REF B737 AMM 33-51-06-960-805 PERFORME - [SDR SWAA2022040485800](https://openairdocs.org/sdr/SWAA2022040485800), Mar 21, 2022: NONE. CRACKED. PANEL192E ATTACH SUPPORT BRACKET FOUND CRACKED / [01] REMOVED AND REPLACED SUPPORT BRACKET FOR PNEL 192 E IN REF SRM 51-40-02;[02] VERIFIED 1 - [SDR SWAA2022040484555](https://openairdocs.org/sdr/SWAA2022040484555), Mar 16, 2022: PLATE. CORRODED. AFT CARGO DOOR CUTOUT; FWD AND AFT SPLICE PLATES; CORRODED. / [01] RECEIVED NEW FWD AND AFT SPLICE PLATES LOCATED AT AFT CARGO DOOR CUT OUT. P/N 453A2611-1 AND - [SDR SWAA2022040481856](https://openairdocs.org/sdr/SWAA2022040481856), Mar 9, 2022: NONE. CRACKED. FOUND AT R2 DOOR FLOOR STRUCTURE INNER CHORD CRACKED / [01] REMOVED R-2 DOOR INNER CHORD AND REMOVED WEB LOCATED AT RBL 44 BETWEEN STA 986.5 AND STA 1016 FOR AC - [SDR SWAA2022040478389](https://openairdocs.org/sdr/SWAA2022040478389), Feb 27, 2022: RIB. CRACKED. R/H HORIZONTAL STABILIZER L/E FAIRING CRACKED AT RIB # 9 / [01] REMOVED AND REPLACED RIB #9 AT RT. HOR. STAB L/E FAIRING IN REF SRM 51-40-02;[02] VERIFIED STEP All 272: https://openairdocs.org/aircraft/N425LV/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 ## 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.