# N340LV: 1987 Boeing 737-3K2

- Status: Valid registration
- Airframe: [Boeing 737-3K2](https://openairdocs.org/model/boeing-737-3k2) (registry code 13844BA, 149 seats)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Serial number: 23738
- Year built: 1987
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 25, 2000
- Certificate issued: August 7, 2003
- Expires: February 29, 2028
- Mode S code: A3BE5C
- 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=340LV
- Page: https://openairdocs.org/aircraft/N340LV

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 737-3K2)

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/N340LV/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 N340LV.

## FAA accident and incident reports

None matched to N340LV.

## Service difficulty reports (436, 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 SWAA2016101108579](https://openairdocs.org/sdr/SWAA2016101108579), Oct 10, 2016: COVER. MISSING. L1 DOOR EMERGENCY EXIT LIGHT LENS COVER MISSING. INSTALLED COVER IAW MM.
- [SDR SWAA2016070553399](https://openairdocs.org/sdr/SWAA2016070553399), Jun 29, 2016: LENS. LOOSE. CENTER CABIN OVERHEAD EMERGENCY LIGHT LENS ASSEMBLY LOOSE. SECURED LIGHT ASSEMBLY PER SOPM.
- [SDR SWAA2016062753224](https://openairdocs.org/sdr/SWAA2016062753224), Jun 22, 2016: LIGHT. INOPERATIVE. L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT IAW AMM.
- [SDR SWAA2016062353149](https://openairdocs.org/sdr/SWAA2016062353149), Jun 22, 2016: LIGHT. INOPERATIVE. L1 EMERGENCY EXIT SIDEWALL LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.
- [SDR SWAA2016062353148](https://openairdocs.org/sdr/SWAA2016062353148), Jun 22, 2016: LIGHT. INOPERATIVE. L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.
- [SDR SWAA2016062353144](https://openairdocs.org/sdr/SWAA2016062353144), Jun 22, 2016: LIGHT. INOPERATIVE. R1 EMERGENCY EXIT SIDEWALL LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.
- [SDR SWAA2016052652125](https://openairdocs.org/sdr/SWAA2016052652125), May 25, 2016: LIGHT. DAMAGED. L1 DOOR EMER EXIT LIGHT DAMAGED. R & R LIGHT ASSEMBLY IAW MM.
- [SDR SWAA2016052652124](https://openairdocs.org/sdr/SWAA2016052652124), May 25, 2016: BATTERY PACK. DISCHARGED. FORWARD LOWER PROXIMITY EMER EXIT LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM.
- [SDR SWAA2016042051124](https://openairdocs.org/sdr/SWAA2016042051124), Apr 17, 2016: SLIDE. OUT OF POSITION. R1 DOOR ESCAPE SLIDE GIRT BAR FLAP OUT OF POSITION. REPOSITIONED SLIDE IAW MT.
- [SDR SWAA2016030849732](https://openairdocs.org/sdr/SWAA2016030849732), Mar 7, 2016: CHARGER. INOPERATIVE. ENTRY DOOR FLOOR EMER EXIT LIGHTS INOPERATIVE AT M9132. R & R BATTERY CHARGER IAW AMM.
- [SDR SWAA2016020248580](https://openairdocs.org/sdr/SWAA2016020248580), Jan 27, 2016: SKIN. CRACKED. FUSELAGE CROWN SKIN CRACKED AT BS 536, BETWEEN STRINGER 5R - 6R. REPAIRED SKIN IAW EA.
- [SDR SWAA2016012548328](https://openairdocs.org/sdr/SWAA2016012548328), Jan 23, 2016: SIGN. BROKEN. L DOOR EXIT SIGN BROKEN. R & R SIGN IAW AMM.
- [SDR SWAA2016011147845](https://openairdocs.org/sdr/SWAA2016011147845), Jan 8, 2016: LENS. MISSING. ENTRY DOOR EMER EXIT LIGHT LENS MISSING. INSTALLED LENS IAW SIP.
- [SDR SWAA2015102245219](https://openairdocs.org/sdr/SWAA2015102245219), Oct 20, 2015: SIGN. UNSECURE. R2 DOOR EXIT SIGN ADJACENT TO BOTTOM FELL OFF. INSTALLED SIGN IAW AMM.
- [SDR SWAA2015101244820](https://openairdocs.org/sdr/SWAA2015101244820), Oct 6, 2015: SKIN. CRACKED. R1 DOOR LOWER HINGE CUT OUT CRACKED AT BS 291.5. REPAIRED CUT OUT IAW EA.
- [SDR SWAA2015082743246](https://openairdocs.org/sdr/SWAA2015082743246), Aug 26, 2015: LENS. MISSING. LEFT OVERWING EMER EXIT SIGN LENS MISSING. R & R LENS ASSEMBLY IAW MM.
- [SDR SWAA2015072342160](https://openairdocs.org/sdr/SWAA2015072342160), Jul 22, 2015: SLIDE. OUT OF ADJUST. R1 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.
- [SDR SWAA2015071441901](https://openairdocs.org/sdr/SWAA2015071441901), Jul 11, 2015: FLAP. DELAMINATED. RIGHT WING OTBD AFT FLAP INBD CORNER DELAMINATED. R & R AFT FLAP IAW AMM.
- [SDR SWAA2015060240273](https://openairdocs.org/sdr/SWAA2015060240273), May 29, 2015: LENS. LOOSE. EXIT LIGHT LENS LOOSE AT FWD FLIGHT ATTENDANT`S SEAT. R & R LIGHT ASSEMBLY IAW MM.
- [SDR SWAA2015052740066](https://openairdocs.org/sdr/SWAA2015052740066), May 26, 2015: LENS. MISSING. L1 DOOR EXIT LIGHT LENS MISSING. R & R LENS IAW SIP.
- [SDR SWAA2015051839776](https://openairdocs.org/sdr/SWAA2015051839776), May 14, 2015: BATTERY PACK. DISCHARGED. EMERGENCY EXIT LIGHT INOPERATIVE AT BS 338. R & R BATTERY PACK IAW AMM.
- [SDR SWAA2015041638581](https://openairdocs.org/sdr/SWAA2015041638581), Apr 14, 2015: BATTERY PACK. DISCHARGED. R1 EXIT LIGHT INOPERATIVE. R & R BATTERY PACK ASSEMBLY IAW AMM.
- [SDR SWAA2015041638576](https://openairdocs.org/sdr/SWAA2015041638576), Apr 14, 2015: BATTERY PACK. DISCHARGED. L1 EXIT LIGHT INOPERATIVE. R & R BATTERY PACK ASSEMBLY IAW AMM.
- [SDR SWAA2015041538555](https://openairdocs.org/sdr/SWAA2015041538555), Apr 13, 2015: COVER. BROKEN. L1 DOOR EMER SIGN COVER BROKEN. R & R SIGN ASSEMBLY IAW MM.
- [SDR SWAA2015030937198](https://openairdocs.org/sdr/SWAA2015030937198), Mar 6, 2015: BATTERY PACK. DISCHARGED. FORWARD EMER EXT LIGHT INOPERATIVE. R & R BATTERY PACK IAW MM.
- [SDR SWAA2015030937207](https://openairdocs.org/sdr/SWAA2015030937207), Mar 6, 2015: CHARGER. INOPERATIVE. FORWARD EMER EXT LIGHT INOPERATIVE. R & R BATTERY CHARGER ASSEMBLY IAW MM.
- [SDR SWAA2015020936416](https://openairdocs.org/sdr/SWAA2015020936416), Feb 7, 2015: BATTERY. DISCHARGED. L1 DOOR LOWER EMER EXIT LIGHT INOPERATIVE. R & R BATTERY IAW AMM.
- [SDR SWAA2015020936415](https://openairdocs.org/sdr/SWAA2015020936415), Feb 7, 2015: LIGHT. BROKEN. L1 DOOR EMER EXIT SIGN LIGHT ASSEMBLY BROKEN. R & R LIGHT ASSEMBLY IAW WDM.
- [SDR SWAA2015020936411](https://openairdocs.org/sdr/SWAA2015020936411), Feb 7, 2015: BATTERY. DISCHARGED. R1 DOOR LOWER EMER EXIT LIGHT INOPERATIVE. R & R BATTERY IAW AMM.
- [SDR SWAA2015020236282](https://openairdocs.org/sdr/SWAA2015020236282), Jan 31, 2015: ACTUATOR. FAULTY. DECLARED EMER, FLAPS EXTENDED THROUGH 0 TO 5 LE FLAPS TRANSIT LIGHT ILLUMINATED. RECYCLED ILLUMINATED THROUGH FLAPS 15 THROUGH SECURED LIGHT OVERHEAD INDICATOR 
- [SDR SWAA2014120834742](https://openairdocs.org/sdr/SWAA2014120834742), Dec 6, 2014: ANGLE. CRACKED. L1 DOOR FWD FRAME ANGLE CRACKED. R & R ANGLE IAW SRM.
- [SDR SWAA2014120834741](https://openairdocs.org/sdr/SWAA2014120834741), Dec 4, 2014: LIGHT. INOPERATIVE. AFT EMER LIGHT INOPERATIVE. R & R LIGHT IAW AMM.
- [SDR SWAA2014120334608](https://openairdocs.org/sdr/SWAA2014120334608), Nov 28, 2014: ANGLE. CRACKED. VERTICAL STABILIZER ACCESS PANEL 9545 ANGLE BY RIB 12 CRACKED ON ANGLE BY RIB 12. R & R ANGLE IAW SRM & DWG.
- [SDR SWAA2014120334607](https://openairdocs.org/sdr/SWAA2014120334607), Nov 28, 2014: SKIN. DELAMINATED. RIGHT WING INBD FORE FLAP DELAMINATED ON UPPER SURFACE. REPAIRED FORE FLAP IAW SRM.
- [SDR SWAA2014112434400](https://openairdocs.org/sdr/SWAA2014112434400), Nov 23, 2014: GLOWSTRIP. DAMAGED. EEPLS PHOTO LUMINESCENT STRIPS DAMAGED. R & R EEPLS IAW MM.
- [SDR SWAA2014120134518](https://openairdocs.org/sdr/SWAA2014120134518), Nov 19, 2014: STRINGER. CORRODED. STRINGER CORRODED AT BS 827+10 STRINGER 25L. REPAIRED STRINGER IAW SRM.
- [SDR SWAA2014120134517](https://openairdocs.org/sdr/SWAA2014120134517), Nov 19, 2014: STRINGER. CORRODED. STRINGER CORRODED AT BS 807+10, STRINGER 25L. REPAIRED STRINGER IAW SRM.
- [SDR SWAA2014112134382](https://openairdocs.org/sdr/SWAA2014112134382), Nov 14, 2014: BATTERY. DISCHARGED. FORWARD FLASHLIGHT BATTERY INOPERATIVE. R & R BATTERY IAW CMM.
- [SDR SWAA2014120234585](https://openairdocs.org/sdr/SWAA2014120234585), Nov 8, 2014: FAIRING. CRACKED. LEFT WING NR 3 MAIN FLAP TRACK FAIRING CRACKED ON CAP LOCATED UPPER SURFACE. R & R FAIRING IAW SRM & DWG.
- [SDR SWAA2014111434181](https://openairdocs.org/sdr/SWAA2014111434181), Nov 8, 2014: ATTACH FITTING. CORRODED. LEFT WING NR 4 FLAP TRACK FWD ATTACH FITTING CORRODED AROUND HOLE. REPAIRED FITTING IAW CMM.
- [SDR SWAA2014120434659](https://openairdocs.org/sdr/SWAA2014120434659), Nov 6, 2014: STRINGER. CORRODED. STRINGER CHANNEL CORRODED BETWEEN BS 344 TO 360, STRINGER 28R. R & R CHANNEL IAW SRM & DWG.
- [SDR SWAA2014120234584](https://openairdocs.org/sdr/SWAA2014120234584), Nov 6, 2014: LIGHT. INOPERATIVE. LEFT EXTERIOR EMER EXIT LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.
- [SDR SWAA2014120234583](https://openairdocs.org/sdr/SWAA2014120234583), Nov 6, 2014: FLAP. CRACKED. LEFT WING NR 1 LE FLAP CRACKED. R & R NR 1 FLAP IAW AMM.
- [SDR SWAA2014111734195](https://openairdocs.org/sdr/SWAA2014111734195), Nov 6, 2014: TIE CLIP. CRACKED. TIE CLIP CRACKED AT BS 727D, STRINGER 25R. R & R TIE CLIP IAW SRM & DWG.
- [SDR SWAA2014111734194](https://openairdocs.org/sdr/SWAA2014111734194), Nov 6, 2014: TIE CLIP. CRACKED. TIE CLIP CRACKED AT BS 380, STRINGER 26L. R & R TIE CLIP IAW SRM & DWG.
- [SDR SWAA2014111134007](https://openairdocs.org/sdr/SWAA2014111134007), Nov 6, 2014: SUPPORT ANGLE. CRACKED. SUPPORT ANGLE CRACKED AT BS 328 RBL 32. R & R ANGLE IAW SRM & DWG.
- [SDR SWAA2014111134006](https://openairdocs.org/sdr/SWAA2014111134006), Nov 6, 2014: STRAP. CRACKED. STRAP CRACKED AT BS 328 RBL 32. R & R STRAP IAW SRM & DWG.
- [SDR SWAA2014120334606](https://openairdocs.org/sdr/SWAA2014120334606), Nov 5, 2014: ANGLE. CRACKED. RIGHT WING NR 6 FLAP TRACK FAIRING ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.
- [SDR SWAA2014120234582](https://openairdocs.org/sdr/SWAA2014120234582), Nov 5, 2014: STRINGER. CORRODED. RIGHT SIDE TORQUE BOX STRINGER CORRODED BETWEEN BS 1088 TO 1138. R & R STRINGER IAW SRM & DWG.
- [SDR SWAA2014120234581](https://openairdocs.org/sdr/SWAA2014120234581), Nov 5, 2014: FITTING. CRACKED. RIGHT WING NR 6 FLAP TRACK CLIP CRACKED. R & R CLIP IAW SRM & DWG.

All 436: https://openairdocs.org/aircraft/N340LV/reports.md

## STCs that may be installed (OpenAirDocs) (7)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the engine (CFM International CFM56 series)

- [STC SE04840NY](https://openairdocs.org/stc/SE04840NY): Installation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engine. Kilroy Aviation LLC. Lists CFM56-7B20
- [STC SE03036CH](https://openairdocs.org/stc/SE03036CH): Application of a deep compressive stress layer using a Low Plasticity Burnishing (LPB) process on CFM56-7 Series Engines Stage 1 High Pressure Compressor (HPC) Blade Dovetails in accordance with Delta Air Lines Inc. Drawing No. 72-0396, Revision B, dated November 3, 2011, or later FAA Approved revision. Delta Air Lines Inc. Lists CFM56-7B20
- [STC SE00032EN](https://openairdocs.org/stc/SE00032EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 Fan/Booster Module. Pratt & Whitney. Lists CFM56-3
- [STC SE00033EN](https://openairdocs.org/stc/SE00033EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 High Pressure Compressor Module. Pratt & Whitney. Lists CFM56-3
- [STC SE00034EN](https://openairdocs.org/stc/SE00034EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 High Pressure Turbine Module. Pratt & Whitney. Lists CFM56-3
- [STC SE00035EN](https://openairdocs.org/stc/SE00035EN): Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 Low Pressure Turbine Module. Pratt & Whitney. Lists CFM56-3
- [STC SE00822CH](https://openairdocs.org/stc/SE00822CH): Install AeroControlex P/N 2604880-001 variable stator feedback control cable and P/N 2604880-002 variable bleed valve feedback control cable on CFM International engines. AeroControlex Group TransDigm Inc. Lists CFM56-2

## Related

- Other Boeing 737-3K2 aircraft: https://openairdocs.org/model/boeing-737-3k2/aircraft.md
- The CFM International CFM56 series engine: https://openairdocs.org/engine/cfm-international-cfm56-series.md

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