# N626SW: 1996 Boeing 737-3H4

- Status: Valid registration
- Airframe: [Boeing 737-3H4](https://openairdocs.org/model/boeing-737-3h4) (registry code 138447K, 149 seats)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Serial number: 27702
- Year built: 1996
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 1, 1996
- Certificate issued: September 5, 2025
- Expires: September 30, 2032
- Mode S code: A82E2C
- Registered owner: [Tvpx Ars Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20ARS%20INC%20TRUSTEE)
- Location: [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake)
- Owner type: Corporation
- Owner's area on the map: 40.8386° N, 111.9179° W: Placed by OpenAirDocs at the center of ZIP code 84054, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=626SW
- Page: https://openairdocs.org/aircraft/N626SW

From the FAA registry file of October 21, 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 737-3H4)

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/N626SW/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 N626SW.

## FAA accident and incident reports

None matched to N626SW.

## Service difficulty reports (358, newest 50)

As reported by operators and repair stations.

- [SDR I5EA2021090800001](https://openairdocs.org/sdr/I5EA2021090800001), Sep 8, 2021: POWER SUPPLY. NO TEST. EMERGENCY LIGHT IN FWD GALLEY AREA NEAREST TO L1 DOOR INOP. PERFORMED REPLACEMENT BATTERY POWER SUPPLY AND OPERATIONAL CHECK OK IAW AMM 33-51-51
- [SDR I5EA2021022700009](https://openairdocs.org/sdr/I5EA2021022700009), Feb 27, 2021: CHARGER. NO TEST. EMERGENCY BATTERY CHARGER AT M1672 INOP. REMOVED AND REPLACED EMERGENCY BATTERY CHARGER M1672 AT STA.973 WITH SERVICEABLE UNIT IAW B-737-300 AMM 33-51-51. TEST 
- [SDR I5EA2020010901](https://openairdocs.org/sdr/I5EA2020010901), Jan 9, 2020: LIGHT. INOPERATIVE. EMERGENCY LIGHT INOP AT M1695, STA 565, WL 213, RBL 68.
- [SDR SWAA2017051713802](https://openairdocs.org/sdr/SWAA2017051713802), May 14, 2017: TRU. FOD. NR 2 TRANSFORMER BOX CLOGGED UP. R&R NR 2 TRANSFORMER RECTIFIER UNIT PER AMM.
- [SDR SWAA2017051713801](https://openairdocs.org/sdr/SWAA2017051713801), May 14, 2017: TRU. FOD. NR 1 TRANSFORMER BOX CLOGGED UP. R&R NR 1 TRANSFORMER RECTIFIER UNIT PER AMM.
- [SDR SWAA2017051713800](https://openairdocs.org/sdr/SWAA2017051713800), May 14, 2017: TRU. FOD. NR 3 TRANSFORMER BOX CLOGGED UP. R&R NR 3 TRANSFORMER RECTIFIER UNIT PER AMM.
- [SDR SWAA2017051713699](https://openairdocs.org/sdr/SWAA2017051713699), May 12, 2017: FEEDER CABLE. SHORTED. FLIGHT ATTENDANTS REPORTED FUMES IN CABIN. EMERGENCY DECLARED AND DIVERTED. R & R NR 1 ENGINE GENERATOR POWER FEEDER HARNESS IAW MM.
- [SDR SWAA2017051113685](https://openairdocs.org/sdr/SWAA2017051113685), May 9, 2017: LAMP. INOPERATIVE. EMERGENCY LIGHT INOPERATIVE BETWEEN ROWS 20 TO 29. REPLACED THE LAMPS IAW AMM.
- [SDR SWAA2017050913639](https://openairdocs.org/sdr/SWAA2017050913639), Apr 26, 2017: SIGN. DAMAGED. FORWARD LAV CEILING EMERGENCY EXIT SIGN DAMAGED. R&R SIGN IAW AMM.
- [SDR SWAA2017050913638](https://openairdocs.org/sdr/SWAA2017050913638), Apr 25, 2017: DOUBLER. CRACKED. FORWARD ENTRY DOOR LOWER HINGE DOUBLER CRACKED AT CUTOUT. REPAIRED CUTOUT IAW EA.
- [SDR SWAA2017042713409](https://openairdocs.org/sdr/SWAA2017042713409), Apr 24, 2017: LIGHT. INOPERATIVE. RT EMERGENCY LIGHT INOP AT ROW 16. RELAMPED LIGHT PER AMM.
- [SDR SWAA2017041113067](https://openairdocs.org/sdr/SWAA2017041113067), Apr 5, 2017: FLAP. DELAMINATED. LT WING OUTBD AFT FLAP DELAMINATED AT AFT INBD CORNER. REPAIRED FLAP PER EA.
- [SDR SWAA2017032112675](https://openairdocs.org/sdr/SWAA2017032112675), Mar 17, 2017: COVER. LOOSE. L1 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. SECURED A COVER IAW SIP.
- [SDR SWAA2017032112674](https://openairdocs.org/sdr/SWAA2017032112674), Mar 17, 2017: COVER. DETACHED. L1 DOOR EMERGENCY EXIT SIGN COVER FELL. SECURED THE COVER IAW SIP.
- [SDR SWAA2017030912422](https://openairdocs.org/sdr/SWAA2017030912422), Mar 6, 2017: COVER. UNSECURE. L1 DOOR EXIT LIGHT COVER CAME OFF. SECURED COVER IAW SIP.
- [SDR SWAA2017030712371](https://openairdocs.org/sdr/SWAA2017030712371), Mar 3, 2017: LENS. UNSECURE. FORWARD ENTRY LOWER EMERGENCY LIGHT LENS LOOSE. SECURED THE LENS IAW AMM.
- [SDR SWAA2017022312044](https://openairdocs.org/sdr/SWAA2017022312044), Feb 21, 2017: LENS. UNSECURE. L1 DOOR EXIT LIGHT LENS CAME OFF. INSTALLED LENS PER SIP.
- [SDR SWAA2017021611910](https://openairdocs.org/sdr/SWAA2017021611910), Feb 13, 2017: LENS. BROKEN. FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT LENS COVER BROKEN. R&R LIGHT ASSEMBLY PER AMM.
- [SDR SWAA2017021411862](https://openairdocs.org/sdr/SWAA2017021411862), Feb 12, 2017: LENS. UNSECURE. L1 DOOR "EXIT" LIGHT LENS FELL OFF. R&R LENS IAW AMM.
- [SDR SWAA2017021411861](https://openairdocs.org/sdr/SWAA2017021411861), Feb 10, 2017: LIGHT. DAMAGED. L1 DOOR EMERGENCY EXIT LIGHT BASE DAMAGED. R&R BASE ASSEMBLY PER MM.
- [SDR SWAA2017013011536](https://openairdocs.org/sdr/SWAA2017013011536), Jan 27, 2017: LENS. LOOSE. L1 EMERGENCY EXIT LIGHT LENS LOOSE. SECURED THE LENS IAW SIP.
- [SDR SWAA2017012411436](https://openairdocs.org/sdr/SWAA2017012411436), Jan 21, 2017: LENS. LOOSE. FORWARD ENTRY EMERGENCY EXIT LIGHT COVER LENS LOOSE. SECURED LENS PER SIP.
- [SDR SWAA2017011611194](https://openairdocs.org/sdr/SWAA2017011611194), Jan 10, 2017: LENS. UNSECURE. L1 DOOR EMERGENCY EXIT SIGN LENS FELL OFF. SECURED LENS PER AMM.
- [SDR SWAA2017010410961](https://openairdocs.org/sdr/SWAA2017010410961), Jan 2, 2017: HINGE. BROKEN. LT WING INBOARD GROUND SPOILER CENTER OUTBOARD HINGE BROKEN. R&R SPOILER IAW AMM.
- [SDR SWAA2016122710782](https://openairdocs.org/sdr/SWAA2016122710782), Dec 20, 2016: LENS. LOOSE. FWD ENTRY EXIT LIGHT LENS LOOSE. SECURED THE LENS IAW MM.
- [SDR SWAA2016112109883](https://openairdocs.org/sdr/SWAA2016112109883), Nov 18, 2016: LENS. LOOSE. FORWARD ENTRY DOOR EXIT SIGN LENS LOOSE. REPLACED THE LENS IAW MM.
- [SDR SWAA2016110409375](https://openairdocs.org/sdr/SWAA2016110409375), Nov 3, 2016: LENS. UNSECURE. FORWARD EMERGENCY EXIT LIGHT LENS FELL OFF. SECURED LENS PER SIP.
- [SDR SWAA2016101708850](https://openairdocs.org/sdr/SWAA2016101708850), Oct 15, 2016: GIRT BAR. OUT OF ADJUST. R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR OUT OF ADJUST. ADJUSTED THE GIRT BAR IAW SIP.
- [SDR SWAA2016092108015](https://openairdocs.org/sdr/SWAA2016092108015), Sep 19, 2016: WEDGE. DELAMINATED. LEFT WING NR 2 SLAT T/E WEDGE INBD L/E DELAMINATED. R & R NR 2 SLAT IAW AMM.
- [SDR SWAA2016092108014](https://openairdocs.org/sdr/SWAA2016092108014), Sep 19, 2016: SLIDE. OUT OF ADJUST. R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW AMM.
- [SDR SWAA2016091907929](https://openairdocs.org/sdr/SWAA2016091907929), Sep 16, 2016: LIGHT. INOPERATIVE. L1 DOOR EMERGENCY EXIT DOOR LOWER SIGN LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW AMM.
- [SDR SWAA2016090855602](https://openairdocs.org/sdr/SWAA2016090855602), Sep 7, 2016: SLIDE. DETACHED. L1 DOOR EMERGENCY SLIDE FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. R & R THE SLIDE IAW MT.
- [SDR SWAA2016090655479](https://openairdocs.org/sdr/SWAA2016090655479), Sep 3, 2016: SIGN. LOOSE. RIGHT OVERWING EXIT SIGN LOOSE. SECURED THE SIGN IAW AMM.
- [SDR SWAA2016082254933](https://openairdocs.org/sdr/SWAA2016082254933), Aug 21, 2016: LENS. MISSING. L1 DOOR LOWER EXIT SIGN COVER LENS MISSING. REINSTALLED THE LENS IAW SIP.
- [SDR SWAA2016081854912](https://openairdocs.org/sdr/SWAA2016081854912), Aug 15, 2016: LENS. LOOSE. FORWARD ENTRY EMERGENCY EXIT LENS LOOSE. SECURED THE LENS IAW SIP.
- [SDR SWAA2016071353737](https://openairdocs.org/sdr/SWAA2016071353737), Jul 12, 2016: SHUTOFF VALVE. FAILED. ANTI-SKID LIGHT FLICKING WHEN AUTO BRAKE INITIALLY SELECTED. CONTINUE TO FLICKER AFTER AUTO BRAKES SELECTED OFF. DECLARED EMERGENCY. R & R THE PARKING BRAKE SHU
- [SDR SWAA2016061352788](https://openairdocs.org/sdr/SWAA2016061352788), Jun 9, 2016: LENS. MISSING. RT OVERWING DOOR SIDEWALL EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS IAW SIP.
- [SDR SWAA2016041250809](https://openairdocs.org/sdr/SWAA2016041250809), Apr 11, 2016: SIGN. LOOSE. FORWARD ENTRY DOOR EXIT SIGN LOOSE. SECURED SIGN IAW SIP.
- [SDR SWAA2016041150776](https://openairdocs.org/sdr/SWAA2016041150776), Apr 8, 2016: SIGN. LOOSE. L1 DOOR EXIT SIGN LOOSE. SECURED SIGN IAW SIP.
- [SDR SWAA2016033150472](https://openairdocs.org/sdr/SWAA2016033150472), Mar 30, 2016: LENS. UNSECURE. L1 DOOR LOWER EXIT SIGN LENS FELL OFF. R & R LENS IAW MM.
- [SDR SWAA2016032150076](https://openairdocs.org/sdr/SWAA2016032150076), Mar 19, 2016: BATTERY PACK. DISCHARGED. LEFT EMER EXIT LIGHTS DIM. R & R BATTERY PACK IAW MM.
- [SDR SWAA2016032150055](https://openairdocs.org/sdr/SWAA2016032150055), Mar 19, 2016: BATTERY PACK. DISCHARGED. RIGHT EMER EXIT LIGHTS DIM. R & R BATTERY PACK IAW MM.
- [SDR SWAA2016032150078](https://openairdocs.org/sdr/SWAA2016032150078), Mar 17, 2016: SKIN. DAMAGED. FUSELAGE SKIN CREASED AT BS 827, BETWEEN STRINGER 27L - 27R. REPAIRED SKIN IAW SRM.
- [SDR SWAA2016032150077](https://openairdocs.org/sdr/SWAA2016032150077), Mar 17, 2016: SLAT. DELAMINATED. RIGHT WING LE NR 5 SLAT DELAMINATED. R & R NR 5 SLAT IAW AMM.
- [SDR SWAA2016030849763](https://openairdocs.org/sdr/SWAA2016030849763), Mar 6, 2016: LENS. MISSING. L1 DOOR BULKHEAD EMER EXIT SIGN LENS MISSING. INSTALLED LENS IAW EA.
- [SDR SWAA2016022649475](https://openairdocs.org/sdr/SWAA2016022649475), Feb 24, 2016: LENS. OUT OF ADJUST. RIGHT EMER EXIT LIGHT LENS COVER OUT OF ADJUSTMENT. ADJUSTED LENS IAW AMM.
- [SDR SWAA2016022349340](https://openairdocs.org/sdr/SWAA2016022349340), Feb 20, 2016: LENS. MISSING. FORWARD ENTRY EMER EXIT INDICATOR LENS MISSING. INSTALLED LENS IAW MM.
- [SDR SWAA2016022349339](https://openairdocs.org/sdr/SWAA2016022349339), Feb 18, 2016: COVER. LOOSE. FORWARD ENTRY EMER EXIT SIGN COVER LOOSE. SECURED COVER IAW SIP.
- [SDR SWAA2016012248292](https://openairdocs.org/sdr/SWAA2016012248292), Jan 20, 2016: ACTUATOR. FAULTY. CROSS FEED VLV LIGHT ILLUMINATED BRIGHT WITH SELECTOR IN CLOSED POSITION. R & R FUEL SOV CROSS FEED VLV ACTUATOR IAW MM.
- [SDR SWAA2016011548015](https://openairdocs.org/sdr/SWAA2016011548015), Jan 12, 2016: SIGN. UNSECURE. FORWARD DOOR EXIT SIGN FELL OFF. SECURED SIGN IAW AMM.

All 358: https://openairdocs.org/aircraft/N626SW/reports.md

## Related

- Other Boeing 737-3H4 aircraft: https://openairdocs.org/model/boeing-737-3h4/aircraft.md
- STCs for the Boeing 737-3H4: https://openairdocs.org/model/boeing-737-3h4/stcs.md
- The CFM International CFM56 series engine: https://openairdocs.org/engine/cfm-international-cfm56-series.md

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