# N625SW: 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: 27701
- Year built: 1996
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 23, 1996
- Certificate issued: May 1, 2024
- Expires: May 31, 2031
- Mode S code: A82A75
- Registered owner: [Eastern 737 Asset Holdings LLC](https://openairdocs.org/faa-owner/EASTERN%20737%20ASSET%20HOLDINGS%20LLC)
- Location: [Kansas City, MO](https://openairdocs.org/faa-place/MO/Kansas%20City)
- Owner type: LLC
- Owner's area on the map: 39.2746° N, 94.7266° W: Placed by OpenAirDocs at the center of ZIP code 64153, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=625SW
- Page: https://openairdocs.org/aircraft/N625SW

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/N625SW/ads.md

## Information bulletins (advisory) (4 in force)

- [SAIB NE-08-17R3](https://openairdocs.org/saib/NE-08-17R3): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued May 28, 2014
- [SAIB NE-13-33R2](https://openairdocs.org/saib/NE-13-33R2): Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes. Issued Jan 28, 2014
- [SAIB NE-12-29](https://openairdocs.org/saib/NE-12-29): Engine Fuel Distribution  CFM56-5B LPTACC Fuel Manifold. Issued Apr 27, 2012
- [SAIB NE-06-02](https://openairdocs.org/saib/NE-06-02): . Issued Oct 18, 2005
- [SAIB NE-13-33R1](https://openairdocs.org/saib/NE-13-33R1) (historical): Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes. Issued Jun 24, 2013
- [SAIB NE-13-33](https://openairdocs.org/saib/NE-13-33) (historical): Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes. Issued May 13, 2013
- [SAIB NE-08-17R2](https://openairdocs.org/saib/NE-08-17R2) (historical): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued Mar 7, 2011
- [SAIB NE-08-17R1](https://openairdocs.org/saib/NE-08-17R1) (historical): Propulsion Technology LLC Unapproved Repair. Issued May 22, 2008
- [SAIB NE-08-17](https://openairdocs.org/saib/NE-08-17) (historical): Propulsion Technologies International Unapproved Repair. Issued May 14, 2008

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB WPR13CA016](https://openairdocs.org/ntsb/WPR13CA016), Oct 17, 2012: Boeing 737-3H4 (N625SW), Las Vegas, NV, no damage. Probable cause: The flight attendant's encounter with an unseen obstruction in the aisle, which resulted in a fall.

## FAA accident and incident reports

None matched to N625SW.

## Service difficulty reports (353, newest 50)

As reported by operators and repair stations. Reports filed since January 18, 1989, when the mark's previous registration was cancelled.

- [SDR 4TXA202506182502](https://openairdocs.org/sdr/4TXA202506182502), Jun 4, 2025: SKIN. DAMAGED. FUSELAGE SKIN DAMAGE AT FUSELAGE SECTION 41 LEFT UPPER PLATING AROUND FS 306 AND BETWEEN STRINGERS 12L AND 13L. REPAIRED IAW EO B737-53-00-09
- [SDR I5EA2022030800001](https://openairdocs.org/sdr/I5EA2022030800001), Mar 8, 2022: BATTERY PACK. NO TEST. OVERHEAD EMERGENCY LIGHTS AT OVER WING EXIT IS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK M1668 AT STA.603. OPS CHECK GOOD IAW B737 AMM 33-51-51.
- [SDR I5EA2021100600002](https://openairdocs.org/sdr/I5EA2021100600002), Oct 6, 2021: POWER SUPPLY. NO TEST. IN REFERENCE DAILY CHECK FOUND CABIN L/H SIDE EMERGENCY LIGHT INOP. REMOVED AND REPLACED CABIN L/H SIDE EMERGENCY POWER SUPPLY (M1675) PERFORMED OPS CHECK NORMA
- [SDR SWAA2017092816717](https://openairdocs.org/sdr/SWAA2017092816717), Sep 26, 2017: SLIDE. OUT OF POSITION. R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.
- [SDR SWAA2017072515276](https://openairdocs.org/sdr/SWAA2017072515276), Jul 23, 2017: SLIDE. OUT OF POSITION. R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR OUT OF POSITION. REPOSITIONED SLIDE PER MT.
- [SDR SWAA2017060914239](https://openairdocs.org/sdr/SWAA2017060914239), Jun 9, 2017: SLIDE. OUT OF POSITION. R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.
- [SDR SWAA2017051613719](https://openairdocs.org/sdr/SWAA2017051613719), May 10, 2017: SLIDE. OUT OF POSITION. R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.
- [SDR SWAA2017040512962](https://openairdocs.org/sdr/SWAA2017040512962), Apr 3, 2017: SLIDE. OUT OF POSITION. R2 DOOR SLIDE OUT OF POSITION. REPOSITIONED THE SLIDE IAW MT.
- [SDR SWAA2017040512961](https://openairdocs.org/sdr/SWAA2017040512961), Apr 3, 2017: SLIDE. OUT OF POSITION. L2 DOOR SLIDE OUT OF POSITION. REPOSITIONED THE SLIDE IAW MT.
- [SDR SWAA2017040412862](https://openairdocs.org/sdr/SWAA2017040412862), Mar 30, 2017: INDICATOR. OUT OF POSITION. R2 DOOR SLIDE PRESSURE GAUGE OUT OF POSITION. REPOSITIONED THE SLIDE IAW MT.
- [SDR SWAA2017033012856](https://openairdocs.org/sdr/SWAA2017033012856), Mar 28, 2017: SLIDE. LOOSE. L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER.
- [SDR SWAA2016122010698](https://openairdocs.org/sdr/SWAA2016122010698), Dec 17, 2016: HYDRAULIC LINE. LEAKING. DECLARED EMERGENCY, A SYSTEM ENGINE PUMP FAILED, NOW PRESSURE LIGHT ILLUMINATED O QUANTITY. R&R HYDRAULIC FLEX LINE HOSE IAW SWPM.
- [SDR SWAA2016120110117](https://openairdocs.org/sdr/SWAA2016120110117), Nov 29, 2016: SLIDE. OUT OF POSITION. R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.
- [SDR SWAA2016111409624](https://openairdocs.org/sdr/SWAA2016111409624), Nov 11, 2016: SLIDE. OUT OF POSITION. R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER SIP.
- [SDR SWAA2016110209316](https://openairdocs.org/sdr/SWAA2016110209316), Oct 31, 2016: SLIDE. OUT OF POSITION. R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.
- [SDR SWAA2016110209306](https://openairdocs.org/sdr/SWAA2016110209306), Oct 31, 2016: SLIDE. OUT OF POSITION. R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.
- [SDR SWAA2016081154747](https://openairdocs.org/sdr/SWAA2016081154747), Aug 9, 2016: SIGN. LOOSE. L1 DOOR EMERGENCY EXIT SIGN LOOSE. SECURED SIGN IAW SIP.
- [SDR SWAA2016061652949](https://openairdocs.org/sdr/SWAA2016061652949), Jun 14, 2016: LENS. UNSECURE. L1 DOOR EMERGENCY EXIT LIGHT LENS COVER FELL OFF. R & R LENS IAW AMM.
- [SDR SWAA2016041150775](https://openairdocs.org/sdr/SWAA2016041150775), Apr 8, 2016: LIGHT. INOPERATIVE. RIGHT EXTERIOR OVERWING EMER EXIT LIGHT INOPERATIVE. RELAMPED BULBS IAW AMM.
- [SDR SWAA2016041150774](https://openairdocs.org/sdr/SWAA2016041150774), Apr 8, 2016: BATTERY PACK. DISCHARGED. RIGHT EMER LIGHT INOPERATIVE, BETWEEN ROW 20 - 24. R & R BATTERY PACK IAW AMM.
- [SDR SWAA2016022349272](https://openairdocs.org/sdr/SWAA2016022349272), Feb 18, 2016: LENS. OUT OF ADJUST. FORWARD LOWER CEILING AFT EXIT LENS OUT OF ADJUSTMENT. ADJUSTED LENS IAW AMM.
- [SDR SWAA2016022349271](https://openairdocs.org/sdr/SWAA2016022349271), Feb 18, 2016: SLIDE. OUT OF POSITION. L2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.
- [SDR SWAA2016022349270](https://openairdocs.org/sdr/SWAA2016022349270), Feb 18, 2016: SLIDE. OUT OF POSITION. R2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.
- [SDR SWAA2016021148970](https://openairdocs.org/sdr/SWAA2016021148970), Feb 8, 2016: CONNECTOR. MISSING. FORWARD LAVATORY EXIT SIGN WIRE CONNECTOR MISSING. INSTALLED CONNECTOR IAW AMM.
- [SDR SWAA2016022349269](https://openairdocs.org/sdr/SWAA2016022349269), Jan 21, 2016: LINK ASSY. CORRODED. RIGHT MLG BEAM ATTACH LINK ASSEMBLY CORRODED. REPAIRED LINK ASSEMBLY IAW EA.
- [SDR SWAA2016020948779](https://openairdocs.org/sdr/SWAA2016020948779), Jan 21, 2016: LINK ASSY. CORRODED. LEFT MLG BEAM ATTACH LINK ASSEMBLY CORRODED. R & R LINK ASSEMBLY IAW EA & DWG.
- [SDR SWAA2016012648392](https://openairdocs.org/sdr/SWAA2016012648392), Jan 9, 2016: STIFFENER. CRACKED. WATER SERVICE PAN STIFFENER CRACKED AT BS 956, STRINGER 25L. R & R STIFFENER IAW SRM.
- [SDR SWAA2016011948146](https://openairdocs.org/sdr/SWAA2016011948146), Jan 8, 2016: BRACKET. CRACKED. BULKHEAD CLOSE OUT BRACKET CRACKED, AT BS 727, RBL 5. R & R BRACKET IAW SRM.
- [SDR SWAA2016021849174](https://openairdocs.org/sdr/SWAA2016021849174), Jan 7, 2016: SKIN. CRACKED. LEFT UPPER WING SKIN CRACKED, BETWEEN RSS 239 - 269, FROM TE. REPAIRED SKIN IAW EA.
- [SDR SWAA2016021649112](https://openairdocs.org/sdr/SWAA2016021649112), Jan 4, 2016: SKIN. CRACKED. RIGHT WING UPPER SKIN, CRACKED AFT SPAR ROW, BETWEEN RSS 224 - 270. REPAIRED SKIN IAW EA.
- [SDR SWAA2016021649111](https://openairdocs.org/sdr/SWAA2016021649111), Jan 4, 2016: FITTING. CRACKED. LEFT MLG FITTING CRACKED IN NR 5 HOLE. REPAIRED FITTING IAW EA.
- [SDR SWAA2016011948145](https://openairdocs.org/sdr/SWAA2016011948145), Jan 3, 2016: BRACKET. CRACKED. RIGHT WING BRACKET, COMMON TO UPPER SPAR CHORD CRACKED, AT RSS 235. R & R BRACKET IAW DWG & SRM.
- [SDR SWAA2016011948144](https://openairdocs.org/sdr/SWAA2016011948144), Jan 3, 2016: SPAR. CRACKED. LEFT WING BRACKET, COMMON TO UPPER SPAR CHORD CRACKED, AT RSS 235. REPAIRED CHORD IAW DWG & EA.
- [SDR SWAA2016020248598](https://openairdocs.org/sdr/SWAA2016020248598), Dec 30, 2015: CREASE BEAM. CORRODED. FORWARD SERVICE DOOR CREASE BEAM WEB CORRODED AT BS 332, STRINGER 17R. R & R WEB IAW SRM & DWG.
- [SDR SWAA2016021649110](https://openairdocs.org/sdr/SWAA2016021649110), Dec 29, 2015: STRINGER. CORRODED. STRINGER CORRODED, BETWEEN BS 1006 - 1016, STRINGER 26R. R & R STRINGER IAW SRM.
- [SDR SWAA2016021649096](https://openairdocs.org/sdr/SWAA2016021649096), Dec 29, 2015: SUPPORT FITTING. CRACKED. RIGHT WING REAR SPAR, UPPER CHORD MLG SUPPORT FITTING CRACKED, AT RSS 222.5. REPAIRED CHORD ER & EA.
- [SDR SWAA2016021849191](https://openairdocs.org/sdr/SWAA2016021849191), Dec 24, 2015: SPAR. CRACKED. RIGHT WING REAR SPAR, UPPER CHORD FASTENER HOLES CRACKED, BETWEEN RSS 222.5 - 228.5. REPAIRED IAW EA.
- [SDR SWAA2016021849173](https://openairdocs.org/sdr/SWAA2016021849173), Dec 24, 2015: SPAR. CRACKED. RIGHT WING REAR SPAR WEB FASTENER HOLES CRACKED, BETWEEN RSS 219.50 - 222.5. REPAIRED WEB IAW EA.
- [SDR SWAA2016021649109](https://openairdocs.org/sdr/SWAA2016021649109), Dec 24, 2015: SPAR. CRACKED. LEFT WING, REAR SPAR UPPER WEB FASTENER HOLES CRACKED, LOCATED BETWEEN RSS 219 - 222.5. REPAIRED WEB IAW EA.
- [SDR SWAA2016021649108](https://openairdocs.org/sdr/SWAA2016021649108), Dec 24, 2015: SPAR. CRACKED. LEFT WING REAR SPAR UPPER CHORD, ONE EACH FASTENER HOLE CRACKED, LOCATED AT RSS 222.5. REPAIRED CHORD IAW EA.
- [SDR SWAA2016021649095](https://openairdocs.org/sdr/SWAA2016021649095), Dec 23, 2015: SKIN. CORRODED. SKIN CORRODED, BETWEEN BS 987 - 1006, STRINGER 27L. REPAIRED SKIN IAW EA.
- [SDR SWAA2016020948778](https://openairdocs.org/sdr/SWAA2016020948778), Dec 23, 2015: SHEAR TIE. CORRODED. SHEAR TIE CORRODED AT BS 967, STRINGER 27L. R & R SHEAR TIE IAW DWG & SRM.
- [SDR SWAA2016011347978](https://openairdocs.org/sdr/SWAA2016011347978), Dec 23, 2015: SHEAR TIE. CORRODED. SHEAR TIE CORRODED AT BS 1006, BETWEEN STRINGER 27L - 27R. R & R SHEAR TIE IAW SRM & DWG.
- [SDR SWAA2016011347977](https://openairdocs.org/sdr/SWAA2016011347977), Dec 23, 2015: SHEAR TIE. CORRODED. SHEAR TIE CORRODED AT BS 987, BETWEEN STRINGER 27L - 27R. R & R SHEAR TIE IAW SRM & DWG.
- [SDR SWAA2016012248309](https://openairdocs.org/sdr/SWAA2016012248309), Dec 21, 2015: STRINGER. CORRODED. INNER CHANNEL STRINGER CORRODED AT BS 967, STRINGER 25L. R & R STRINGER IAW SRM.
- [SDR SWAA2016011948143](https://openairdocs.org/sdr/SWAA2016011948143), Dec 21, 2015: STRAP. CRACKED. FUSELAGE UPPER BUTT JOINT SPLICE STRAP CRACKED AT BS 360, STRINGER 3R. FASTENER HOLE REMOVED FOR INSPECTION. REPAIR SPLICE STRAP IAW ER & EA.
- [SDR SWAA2016021849190](https://openairdocs.org/sdr/SWAA2016021849190), Dec 20, 2015: BRACKET. CRACKED. R1 DOOR AFT STOP NR 1, T BRACKET CRACKED ON INBD LOWER RADIUS. R & R T BRACKET IAW EA.
- [SDR SWAA2016021849172](https://openairdocs.org/sdr/SWAA2016021849172), Dec 20, 2015: SKIN. CRACKED. FORWARD ENTRY DOOR LOWER AFT CORNER SKIN CRACKED AT BS 346, STRINGER 17L. REPAIRED SKIN IAW ER & EA.
- [SDR SWAA2015123147589](https://openairdocs.org/sdr/SWAA2015123147589), Dec 20, 2015: STRINGER CLIP. CRACKED. STRINGER CLIP CRACKED AT STATION 360, STRINGER 11L. R & R CLIP IAW SRM.
- [SDR SWAA2016020548722](https://openairdocs.org/sdr/SWAA2016020548722), Dec 19, 2015: FLOOR SUPPORT. CRACKED. LONGITUDINAL FLOOR BEAM CRACKED BETWEEN BS 665 TO BS 669, LBL 24.5. REMOVED AND REPLACED BEAM IAW DWG AND SRM.

All 353: https://openairdocs.org/aircraft/N625SW/reports.md

## Earlier aircraft with N625SW

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N625SW before.

- [Cancelled 1989-01-18](https://openairdocs.org/deregistered/N625SW-1989-01-18): Piper PA-18, S/N 187613. Triennial form not returned

## 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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