# N201LV: 2005 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: 29854
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 15, 2005
- Certificate issued: March 3, 2005
- Expires: December 31, 2029
- Mode S code: A196C8
- 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=201LV
- Page: https://openairdocs.org/aircraft/N201LV

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/N201LV/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 N201LV.

## FAA accident and incident reports

None matched to N201LV.

## Service difficulty reports (349, 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 SWAA2026101229421](https://openairdocs.org/sdr/SWAA2026101229421), Sep 22, 2026: ACCESS PANEL. CRACKED. CRACK BRACKET ACCESS PANEL 551FB AT LT WING. REPLACED BRACKET AND FASTENERS LOCATED ON ACCESS PANEL 551FB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9. AND DWG 115A27
- [SDR SWAA2026101299047](https://openairdocs.org/sdr/SWAA2026101299047), Sep 21, 2026: SUPPORT BRACKET. CRACKED. CRACKED LT WING T/E SUPPORT BRACKET, IRSS 199 + 11 INCHES. REPLACED THE SUPPORT BRACKET AND FASTENERS IAW SRM-51-10-02, ITEM (9), & DWG 115A2001, SHEET 24, REV 
- [SDR SWAA2026101270356](https://openairdocs.org/sdr/SWAA2026101270356), Sep 21, 2026: PLATE. CRACKED. CRACKED CORRUGATED PLATE, LT WING TRAILING EDGE AT IRSS 199 + 14 INCHES. REPLACED CORRUGATED PLATE IAW SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG: 115A2781 SHEET:
- [SDR SWAA2026101285909](https://openairdocs.org/sdr/SWAA2026101285909), Sep 21, 2026: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET LOCATED TRAILING EDGE ORSS 288 AT RT WING. REPLACED SUPPORT BRACKET AND FASTENERS LOCATED TRAILING EDGE ORSS 288 AT RT WING IAW SRM 51-40-
- [SDR SWAA2026101223373](https://openairdocs.org/sdr/SWAA2026101223373), Sep 21, 2026: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE AT LEVEL IRSS 199 PLUS 30 INCHES APROX AT LT WING. REPLACED CORRUGATED PLATE LOCATED WING FIXED T/E AT LEVEL IRSS 199 + 30 
- [SDR SWAA2026101229388](https://openairdocs.org/sdr/SWAA2026101229388), Sep 20, 2026: ACCESS PANEL. CRACKED. CRACK BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB. REPLACED BLADE ON ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW SRM-51-40-02-0G-0 AND SRM-51-10-02-0G-0 ITE
- [SDR SWAA2026101279104](https://openairdocs.org/sdr/SWAA2026101279104), Sep 20, 2026: FITTING. DETERIORATED. DETERIORATED PASSENGER SEAT TRACK FITTING AT SEAT ROWS 9 LEFT. REPLACED PASSENGER SEAT TRACK FITTING IAW CMM 25-21-42-3859, REV 07.
- [SDR SWAA2026101254424](https://openairdocs.org/sdr/SWAA2026101254424), Sep 19, 2026: PLATE. DAMAGED. ELONGATED HOLES ON LT WING T/E CORRUGATED PLATE, ORSS 261. REPLACED THE CORRUGATED PLATE IAW SRM 51-10-02, ITEM 9, 51-40-02, DWG 115A2781, SHEET 6, REV -, AND D
- [SDR SWAA2026101254544](https://openairdocs.org/sdr/SWAA2026101254544), Sep 19, 2026: PLATE. DAMAGED. ELONGATED HOLE ON RT WING SUPPORT CORRUGATED PLATE, ORSS 261. REPLACED SUPPORT CORRUGATED PLATE IAW SRM 51-10-02, SRM 51-40-02, & DWG 115A2001, SHEET 29, REV -.
- [SDR SWAA2026101214235](https://openairdocs.org/sdr/SWAA2026101214235), Sep 18, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON RT WING ACCESS PANEL 661BB. REPAIRED ACCESS PANEL 661BB IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026101210727](https://openairdocs.org/sdr/SWAA2026101210727), Sep 18, 2026: ACCESS PANEL. ELONGATED. ELONGATED HOLES ON LT WING ACCESS PANEL 561CB TRAILING EDGE. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026101250031](https://openairdocs.org/sdr/SWAA2026101250031), Sep 18, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLES OF ACCESS PANEL 561AB ON LT WING. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-9 REPAIR 9.
- [SDR SWAA2026101213584](https://openairdocs.org/sdr/SWAA2026101213584), Sep 18, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 661AB AT RT WING. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-9, REPAIR 9.
- [SDR SWAA2026101227866](https://openairdocs.org/sdr/SWAA2026101227866), Sep 18, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON RT WING ACCESS PANEL 661CB. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-9, REPAIR 9.
- [SDR SWAA2026101233454](https://openairdocs.org/sdr/SWAA2026101233454), Sep 18, 2026: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 561BB AT LT WING. REPAIRED ACCESS PANEL 561BB AT LT WING IAW SRM 51-70-04-2R-9, REPAIR 9.
- [SDR SWAA2026101232960](https://openairdocs.org/sdr/SWAA2026101232960), Sep 16, 2026: ACCESS PANEL. CRACKED. CRACK ANGLE OF ACCESS PANEL 333AT ON THE LT HORIZONTAL STAB. REPLACED THE ACCESS PANEL IAW SRM-51-40-02-0G-0, & SRM-51-10-02-0G-0, ITEM 9.
- [SDR SWAA2026101253023](https://openairdocs.org/sdr/SWAA2026101253023), Sep 16, 2026: STRAP. CRACKED. CRACK INDICATION FOUND AT FASTENER HOLE ON STUB BEAM STRAPS, BS 639, RBL 45.57. CRACK DIRECTION 9 OCLOCK LOOKING FWD FROM OTBD L-27. REPLACED THE STRAP AND FAST
- [SDR SWAA2026101282859](https://openairdocs.org/sdr/SWAA2026101282859), Sep 16, 2026: CROSSBEAM. CRACKED. CRACKED CROSSBEAM, BS 540, BL 0 - RBL 24.75, WL 208.1. REPLACED THE CROSSBEAM, BS 540 BTWN BL0 - RBL 24.75 IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G-0, AND DWG143A
- [SDR SWAA2026101249882](https://openairdocs.org/sdr/SWAA2026101249882), Sep 16, 2026: STRAP. CRACKED. CRACK INDICATION FOUND IN OPEN FASTENER HOLE AFT POSITION AT STUB BEAM STRAPS AREA AT BS 639, LBL 45.57. . REPLACED STRAP AND FASTENERS ON STUB BEAM AREA IAW SR
- [SDR SWAA2026101206046](https://openairdocs.org/sdr/SWAA2026101206046), Sep 16, 2026: SKIN. DELAMINATED. DELAMINATED EXTERNAL SKIN ON DOOR LH NOSE LANDING GEAR. REPAIRED EXTERNAL SKIN ON NLG DOOR IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026101278616](https://openairdocs.org/sdr/SWAA2026101278616), Sep 16, 2026: CROSSBEAM. CRACKED. CRACK ON CROSSBEAM, BS 540, BL 0 - LBL 24.75, WL 208.1. REPLACED CROSSBEAM IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, & DWG 143A0060, SHT 36, REV A.
- [SDR SWAA2026101234020](https://openairdocs.org/sdr/SWAA2026101234020), Sep 15, 2026: SCUFF PLATE. CRACKED. CRACKED FWD CORNER SCUFF PLATE AT AFT CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.
- [SDR SWAA2026101287845](https://openairdocs.org/sdr/SWAA2026101287845), Sep 14, 2026: PRESSURE DECK. CRACKED. CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB AT RBL 40 BTW BS 663 - 675. PERFORMED PERMANENT REPAIR ON THE PRESSURE DECK IAW SRM 53-40-51-2R-2, REPAIR 2, FI
- [SDR SWAA2026101278529](https://openairdocs.org/sdr/SWAA2026101278529), Sep 14, 2026: FITTING. DETERIORATED. DETERIORATED PASSENGER SEAT INBD REAR FITTING ROW 25L. REPLACED THE SEAT REAR FITTING IAW CMM 25-21-42-3859, REV 07, DISASSEMBLY STEP 3.Y(5), PAGE 3013, ASSEMBL
- [SDR SWAA2026101257970](https://openairdocs.org/sdr/SWAA2026101257970), Sep 14, 2026: LIGHT. DETERIORATED. DETERIORATED PHOTOLUMINESCENT LIGHTING ALONG PAX CABIN. REPLACED PHOTOLUMINESCENT LIGHTING ALONG PAX CABIN IAW AMM 53-51-15-400-802.
- [SDR SWAA2026083196211](https://openairdocs.org/sdr/SWAA2026083196211), Aug 28, 2026: SENSOR. INDICATION. OTS - TRAILING EDGE FLAP ASYMMETRY, FLAP LESS THAN 1. ON FLAP INDICATOR. FLAP LOCKOUT._ R&R POSITION 8 T/E FLAP SKEW SENSOR IAW AMM 27-59-01. OPS CHECK GOOD.
- [SDR SWAA2026052605806](https://openairdocs.org/sdr/SWAA2026052605806), May 22, 2026: RETAINER. LOOSE. FORWARD SERVICE DOOR GIRT BAR LOOSE. INSPECTED FWD SERVICE DOOR ESCAPE SLIDE GIRT BAR AND BAR RETAINER CLIPS OP CHECK GOOD PER AMM 25-66-01.
- [SDR SWAA2026052606582](https://openairdocs.org/sdr/SWAA2026052606582), May 22, 2026: GIRT BAR. LOOSE. FORWARD SERVICE DOOR GIRT BAR LOOSE. INSPECTED FWD SERVICE DOOR ESCAPE SLIDE GIRT BAR AND BAR RETAINER CLIPS OP CHECK GOOD PER AMM 25-66-01.
- [SDR SWAA2026033084419](https://openairdocs.org/sdr/SWAA2026033084419), Mar 29, 2026: UNKNOWN. ODOR. STRONG FUEL SMELL IN AFT CABIN AND OUTSIDE FUSELAGE AT GATE WITH APU RUNNING<[01] PERFORMED INSPECTION IAW FIM 21-00 TASK 806 NO SMELL NOTED. RAN APU FOR SEVERA
- [SDR SWAA2026022373204](https://openairdocs.org/sdr/SWAA2026022373204), Feb 21, 2026: BATTERY. INOPERATIVE. AFT INBOARD FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT AND BATTERY IAW AMM 25-64-00.
- [SDR SWAA2026010758008](https://openairdocs.org/sdr/SWAA2026010758008), Jan 4, 2026: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK AT ROW 17 ABC AND ROW 11 DEF IAW AMM 33-51-06. OPS CHECKED GOOD.
- [SDR SWAA2025101423897](https://openairdocs.org/sdr/SWAA2025101423897), Oct 12, 2025: SIGN. DETACHED. EMERGENCY EXIT SIGN AT RH OVERWING HATCH FELL OFF. RE INSTALLED SIGN IAW AMM 33-51-04.
- [SDR SWAA2025091614190](https://openairdocs.org/sdr/SWAA2025091614190), Sep 14, 2025: MEGAPHONE. INOPERATIVE. AFT MEGAPHONE AFTER MEGAPHONE WILL NOT TEST. R & R AFT MEGAPHONE IAW AMM 25-64-00.
- [SDR SWAA2025090510566](https://openairdocs.org/sdr/SWAA2025090510566), Sep 2, 2025: SLIDE. LOW PRESSURE. FWD ENTRY EMERGENCY SLIDE AIR BOTTLE IN THE RED. REMOVED AND REPLACED THE FWD ENTRY DOOR SLIDE AS PER MT# 725-SWA-105; 725-61-06.
- [SDR SWAA2025042928067](https://openairdocs.org/sdr/SWAA2025042928067), Apr 25, 2025: HANDLE. LOOSE. FWD ENTRY DOOR UPPER ASSIST HANDLE LOOSE<[01] RE SECURED FWD ENTRY DOOR UPPER ASSIST HANDLE REF AMM 20-50-11.
- [SDR SWAA2025012187047](https://openairdocs.org/sdr/SWAA2025012187047), Jan 17, 2025: FIRE WARNING. FALSE ACTIVATION. ON TAKEOFF AT VR MASTER CAUTION LIGHT ILLUMINATED WITH ANNUNCIATOR LIGHTS FOR FUEL; ELEC; ANTI-ICE; HYD; DOORS; ALONG WITH THE LIGHTS ON THE OVERHEAD PANEL FOR 
- [SDR SWAA2024120272499](https://openairdocs.org/sdr/SWAA2024120272499), Nov 28, 2024: SIGN. BURNED. (CUSTOMER REQUEST) RH OVERWING EMERGENCY EXIT SIGN (SIDEWALL) HAS BURNED OUT BULB 2024-672580<[01] REPLACED LAMP AT RH OVERWING EMERGENCY EXIT SIGN IAW B737-700
- [SDR SWAA2024120272500](https://openairdocs.org/sdr/SWAA2024120272500), Nov 28, 2024: BULB. INOPERATIVE. (CUSTOMER REQUEST) LH ROW 9 AND 11 EMERGENCY EXIT LIGHTS INOP 2024-672582<[01] REPLACED LH ROW 9 AND 11 EMERGENCY EXIT LIGHTS BULBS TEST OK IAW B737-700 AMM 33-
- [SDR SWAA2024112756298](https://openairdocs.org/sdr/SWAA2024112756298), Nov 4, 2024: ANGLE. CORRODED. CORROSION ANGLE INTERNAL STRUCTURE DOOR CUTOUT LOCATED BS 460 FWD SIDE AND S-18R WL 174 AT FWD CARGO COMPARTMENT 2024-672503<[01] REPLACED ANGLE (SHEAR TIE) AND
- [SDR SWAA2024112755393](https://openairdocs.org/sdr/SWAA2024112755393), Nov 1, 2024: SUPPORT BRACKET. CRACKED. CRACK INBOARD TRAILING EDGE SUPPORT BRACKET INTERNAL AREA ACCESS PANEL 651DB AT RT WING 2024-672492<[01] REPLACED SUPPORT BRACKET LOCATED INBOARD TRAILING EDGE 
- [SDR SWAA2024112755392](https://openairdocs.org/sdr/SWAA2024112755392), Oct 31, 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 2024-672487<[01] REPAIRED UPR STRINGER U9 - WST
- [SDR SWAA2024112754594](https://openairdocs.org/sdr/SWAA2024112754594), Oct 29, 2024: GIRT BAR. DETERIORATED. DETERIORATED GIRT BAR FLOOR BRACKETS HARDWARE AND PLATES ON AFT ENTRY DOOR AT AFT GALLEY AREA 2024-672480<[01] REPLACED GIRT BAR FLOOR BRACKETS HARDWARE AND PLA
- [SDR SWAA2024112754595](https://openairdocs.org/sdr/SWAA2024112754595), Oct 29, 2024: GIRT BAR. DETERIORATED. DETERIORATED GIRT BAR FLOOR BRACKETS HARDWARE AND PLATES ON AFT SERVICE DOOR AT AFT GALLEY AREA 2024-672481<[01] REPLACED GIRT BAR FLOOR BRACKETS HARDWARE AND P
- [SDR SWAA2024112754596](https://openairdocs.org/sdr/SWAA2024112754596), Oct 29, 2024: GIRT BAR. DETERIORATED. DETERIORATED GIRT BAR FLOOR BRACKETS HARDWARE AND PLATES ON FWD ENTRY DOOR AT FWD GALLEY AREA 2024-672478<[01] REPLACED GIRT BAR FLOOR BRACKETS HARDWARE AND PLA
- [SDR SWAA2024112754597](https://openairdocs.org/sdr/SWAA2024112754597), Oct 29, 2024: GIRT BAR. DETERIORATED. DETERIORATED GIRT BAR FLOOR BRACKETS HARDWARE AND PLATES ON FWD SERVICE DOOR AT FWD GALLEY AREA 2024-672479<[01] REPLACED GIRT BAR FLOOR BRACKETS HARDWARE AND P
- [SDR SWAA2024112754237](https://openairdocs.org/sdr/SWAA2024112754237), Oct 28, 2024: STRAP. CORRODED. CORROSION ON STRAP LOCATED BS887 WL156 AND LBL3 AT AFT CARGO COMPARTMENT 2024-672446<[01] REPLACED STRAP AND FASTENERS LOCATED BS887 FLOOR STRUCTURE WL156 AT AF
- [SDR SWAA2024112754235](https://openairdocs.org/sdr/SWAA2024112754235), Oct 28, 2024: STUB FRAME. CRACKED. CRACK UPPER STUB FRAME BS 294;5 AND BETWEEN STR 9R TO STR 10R PASS CABIN 2024-672399<[01] REPLACED STUB FRAME AND FASTENERS LOCATED ON BS 294.5 BETWEEN STR-7R T
- [SDR SWAA2024112753932](https://openairdocs.org/sdr/SWAA2024112753932), Oct 27, 2024: RETAINER. MISSING. MISSING RETAINER LOCATED UPPER SILL DOOR CUTOUT AT FWD CARGO COMPARTMENT (1E/A) 2024-672342<[01] INSTALLED RETAINER LOCATED UPPER SILL DOOR CUTOUT AT FWD CARGO 
- [SDR SWAA2024112753516](https://openairdocs.org/sdr/SWAA2024112753516), Oct 26, 2024: SHEAR TIE. CORRODED. CORROSION ANGLE INTERNAL STRUCTURE DOOR CUTOUT LOCATED BS 460 AFT SIDE AND S-18R WL 174 AT FWD CARGO COMPARTMENT 2024-672276<[01] REPLACED ANGLE (SHEAR TIE) INT
- [SDR SWAA2024112753522](https://openairdocs.org/sdr/SWAA2024112753522), Oct 26, 2024: ANGLE. CRACKED. CRACK ANGLE LOCATED BS663 AND RBL55 AT CENTER WING BOX 2024-672307<[01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-

All 349: https://openairdocs.org/aircraft/N201LV/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

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