# N359SW: 1992 Boeing 737-3H4

- Status: Registration pending
- 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: 26596
- Year built: 1992
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 3, 1992
- Mode S code: A407E1
- Location: [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake)
- Owner type: Individual
- 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=359SW
- Page: https://openairdocs.org/aircraft/N359SW

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/N359SW/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 N359SW.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports 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.

- [Incident 19930508012599I](https://openairdocs.org/incident/19930508012599I), May 8, 1993: Boeing 737300 (N359SW), Pahrump, NV. Severe turbulence encounted on descent. Passenger injuried. Seat belt sign on.

## Service difficulty reports (335, newest 50)

As reported by operators and repair stations.

- [SDR SWAA2017050813625](https://openairdocs.org/sdr/SWAA2017050813625), May 4, 2017: SLIDE. OUT OF POSITION. R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.
- [SDR SWAA2017041113069](https://openairdocs.org/sdr/SWAA2017041113069), Apr 6, 2017: SLIDE. OUT OF ADJUST. R2 DOOR EVAC SLIDE OUT OF ADJUST. READJUSTED SLIDE PER MM.
- [SDR SWAA2017022812166](https://openairdocs.org/sdr/SWAA2017022812166), Feb 22, 2017: FRAME. CRACKED. FRAME CRACKED AT BS 500A, STRINGER 8L. REPAIRED THE FRAME IAW EA.
- [SDR SWAA2017022812165](https://openairdocs.org/sdr/SWAA2017022812165), Feb 21, 2017: SKIN. CRACKED. FUSELAGE EXTERNAL SKIN CRACKED AT BS 500A+5, STRINGER 8L. REPAIRED THE SKIN IAW EA.
- [SDR SWAA2017022812164](https://openairdocs.org/sdr/SWAA2017022812164), Feb 20, 2017: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT BS 400+14, STRINGER 2R. REPAIRED THE SKIN IAW EA.
- [SDR SWAA2017011711207](https://openairdocs.org/sdr/SWAA2017011711207), Jan 16, 2017: SLIDE. OUT OF POSITION. R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.
- [SDR SWAA2016090655398](https://openairdocs.org/sdr/SWAA2016090655398), Aug 30, 2016: WEB. CRACKED. LOWER INBOARD FASTENER HOLE CLOSE OUT WEB CRACKED BETWEEN BS 349 - 352, BETWEEN STRINGERS 15 - 17L. R & R THE WEB IAW DWG & SRM.
- [SDR SWAA2016090755554](https://openairdocs.org/sdr/SWAA2016090755554), Aug 28, 2016: BEAR STRAP. CRACKED. L1 DOOR LOWER AFT CORNER BEARSTRAP CRACKED AT BS 345, WL 210. REPAIRED THE BEAR STRAP IAW SRM.
- [SDR SWAA2016090655446](https://openairdocs.org/sdr/SWAA2016090655446), Aug 28, 2016: PAN. CRACKED. LEFT WATER SERVICE DOOR PAN CRACKED AT BS 985, STR 26L. REPAIRED DOUBLER IAW ER AND EA.
- [SDR SWAA2016081054695](https://openairdocs.org/sdr/SWAA2016081054695), Aug 8, 2016: BLOWER. INOPERATIVE. DECLARED EMERGENCY ON FINAL, 20NM TO 30NM, F/A CALLED AND SAID THEY SMELLED FUMES, NO SMOKE, IN AFT GALLEY AREA. THE ODOR SPREAD THRU CABIN TO FLIGHT DECK. THE 
- [SDR SWAA2016032950333](https://openairdocs.org/sdr/SWAA2016032950333), Mar 27, 2016: RETAINING CLIP. LOOSE. L1 DOOR GIRT BAR LOOSE. SECURED CLIPS IAW SIP.
- [SDR SWAA2016022349317](https://openairdocs.org/sdr/SWAA2016022349317), Feb 20, 2016: LIGHT. LOOSE. RIGHT LUMINESCENT FLOOR STRIP LOOSE AT ROW 8. SECURED LIGHT IAW AMM.
- [SDR SWAA2015121146970](https://openairdocs.org/sdr/SWAA2015121146970), Dec 3, 2015: SKIN. CRACKED. SKIN CRACKED AT BS 361.5, STRINGER 4R. REPAIRED SKIN IAW SRM.
- [SDR SWAA2015122347372](https://openairdocs.org/sdr/SWAA2015122347372), Dec 2, 2015: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT BS 360, STRINGER 3 - 4R. REPAIRED SKIN IAW EA.
- [SDR SWAA2015121147020](https://openairdocs.org/sdr/SWAA2015121147020), Nov 25, 2015: STRINGER. CRACKED. STRINGER CRACKED, BETWEEN BS 500 - 500B, STRINGER 8L. REPAIRED STRINGER IAW SRM.
- [SDR SWAA2015121547147](https://openairdocs.org/sdr/SWAA2015121547147), Nov 24, 2015: ATTACH FITTING. CRACKED. INTERCOSTAL ATTACH CLIP CRACKED AT BS 291, STRINGER 8R. R & R CLIP IAW SRM.
- [SDR SWAA2015121447068](https://openairdocs.org/sdr/SWAA2015121447068), Nov 24, 2015: STRINGER CLIP. CRACKED. STRINGER CLIP CRACKED AT BS 277, STRINGER 10R. REPAIRED CLIP IAW ER & EA.
- [SDR SWAA2015121147019](https://openairdocs.org/sdr/SWAA2015121147019), Nov 24, 2015: STRINGER. CRACKED. STRINGER CRACKED AT BS 500B, STRINGER 8R. REPAIRED STRINGER IAW SRM.
- [SDR SWAA2015122347371](https://openairdocs.org/sdr/SWAA2015122347371), Nov 23, 2015: SUPPORT CHANNEL. CORRODED. NUMBER 3 VHF LOWER ANTENNA SUPPORT U-CHANNEL CORRODED AT STATION 727D+7, LBL 2. R & R CHANNEL IAW EA.
- [SDR SWAA2015122247319](https://openairdocs.org/sdr/SWAA2015122247319), Nov 23, 2015: FRAME. CRACKED. FUSELAGE FRAME CRACKED AT STATION 360, STRINGER 20R. REPAIRED FRAME IAW EA.
- [SDR SWAA2015121547146](https://openairdocs.org/sdr/SWAA2015121547146), Nov 23, 2015: STRINGER SPLICE. CRACKED. STRINGER SPLICE CRACKED AT BS 360, STRINGER 5R. R & R SPLICE IAW ER & EA.
- [SDR SWAA2015121447067](https://openairdocs.org/sdr/SWAA2015121447067), Nov 23, 2015: STRINGER SPLICE. CRACKED. STRINGER SPLICE CRACKED AT BS 360+2, STRINGER 4R. R & R SPLICE IAW ER & EA.
- [SDR SWAA2015121146969](https://openairdocs.org/sdr/SWAA2015121146969), Nov 23, 2015: STRINGER CLIP. CRACKED. STRINGER CLIP CRACKED AT BS 907, STRINGER 10R. R & R CLIP IAW SRM.
- [SDR SWAA2015121146968](https://openairdocs.org/sdr/SWAA2015121146968), Nov 21, 2015: LENS. MISSING. RIGHT OVERHEAD BULLNOSE BIN EMER LIGHT LENS MISSING AT ROW 2. INSTALLED LENS IAW AMM.
- [SDR SWAA2015121146967](https://openairdocs.org/sdr/SWAA2015121146967), Nov 21, 2015: LENS. MISSING. AFT CTR EMER EXIT SIGN LENS MISSING. INSTALLED LENS IAW AMM.
- [SDR SWAA2015121146966](https://openairdocs.org/sdr/SWAA2015121146966), Nov 21, 2015: CREASE BEAM. CORRODED. CREASE BEAM WEB CORRODED, BETWEEN BS 727C - 727D, WL 208 LT SIDE. R & R WEB IAW SRM.
- [SDR SWAA2015122347397](https://openairdocs.org/sdr/SWAA2015122347397), Nov 20, 2015: SKIN. CRACKED. LEFT SIDE FUSELAGE SKIN CRACKED AT STATION 289, WL 254. REPAIRED SKIN IAW EA.
- [SDR SWAA2015122347370](https://openairdocs.org/sdr/SWAA2015122347370), Nov 20, 2015: ATTACH ANGLE. CORRODED. ATTACH ANGLE CORRODED AT BS 326.7, STRINGER 28L. R & R ANGLE IAW EA.
- [SDR SWAA2015121647188](https://openairdocs.org/sdr/SWAA2015121647188), Nov 20, 2015: FLOOR SUPPORT. CRACKED. FLOOR TRACK FLOOR SUPPORT ANGLE, CRACKED AT BS 380, STRINGER 27R. R & R FLOOR TRACK IAW SRM.
- [SDR SWAA2015121647187](https://openairdocs.org/sdr/SWAA2015121647187), Nov 20, 2015: SHEAR TIE. CORRODED. SHEAR TIE CORRODED AT BS 360, BETWEEN STRINGER 28L - 28R. REPAIRED SHEAR TIE IAW SRM.
- [SDR SWAA2015121447066](https://openairdocs.org/sdr/SWAA2015121447066), Nov 20, 2015: STRINGER CLIP. CRACKED. STRINGER CLIP CRACKED AT BS 360, STRINGER 8R. R & R CLIP IAW SRM.
- [SDR SWAA2015121146965](https://openairdocs.org/sdr/SWAA2015121146965), Nov 20, 2015: STRINGER CLIP. CRACKED. STRINGER CLIP CRACKED AT BS 500D, STRINGER 8R. R & R CLIP IAW SRM.
- [SDR SWAA2015121146964](https://openairdocs.org/sdr/SWAA2015121146964), Nov 20, 2015: STRINGER CLIP. CRACKED. STRINGER CLIP CRACKED AT BS 500C, STRINGER 8R. R & R CLIP IAW SRM.
- [SDR SWAA2015121146963](https://openairdocs.org/sdr/SWAA2015121146963), Nov 20, 2015: STRINGER CLIP. CRACKED. STRINGER CLIP CRACKED AT BS 500B, STRINGER 8R. R & R CLIP IAW SRM.
- [SDR SWAA2015121146962](https://openairdocs.org/sdr/SWAA2015121146962), Nov 20, 2015: SEAT TRACK. CRACKED. SEAT TRACK WEB UPPER RADIUS CRACKED AT BS 727B+1.5, RBL 45.5. REPAIRED SEAT TRACK IAW SRM.
- [SDR SWAA2015121647186](https://openairdocs.org/sdr/SWAA2015121647186), Nov 19, 2015: INTERCOSTAL. CORRODED. INTERCOSTAL CORRODED, BETWEEN BS 727A - 727B, BETWEEN STRINGER 25L - 26L. R & R INTERCOSTAL IAW SRM & DWG.
- [SDR SWAA2015121647185](https://openairdocs.org/sdr/SWAA2015121647185), Nov 19, 2015: ANGLE. CORRODED. AFT CARGO COMPARTMENT, SIDEWALL SUPPORT AROUND FASTENER HOLES, CORRODED AT BS 727D, BETWEEN STRINGER 25R - 27R. R & R ANGLE IAW SRM & DWG.
- [SDR SWAA2015121547145](https://openairdocs.org/sdr/SWAA2015121547145), Nov 19, 2015: INTERCOSTAL. CORRODED. INTERCOSTAL CORRODED, BETWEEN BS 727A - 727B, BETWEEN STRINGER 27R TO 26R. R & R INTERCOSTAL IAW SRM & DWG.
- [SDR SWAA2015120746754](https://openairdocs.org/sdr/SWAA2015120746754), Nov 19, 2015: SUPPORT. CORRODED. AFT CARGO COMPARTMENT, FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 727D - 727E, BETWEEN STRINGER 26R - 27R. R & R SUPPORT IAW SRM.
- [SDR SWAA2015120746753](https://openairdocs.org/sdr/SWAA2015120746753), Nov 19, 2015: SUPPORT. CORRODED. FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 767 - 787, BETWEEN STRINGER 26L - 27R. R & R SUPPORT IAW SRM.
- [SDR SWAA2015120746752](https://openairdocs.org/sdr/SWAA2015120746752), Nov 19, 2015: INTERCOSTAL. CORRODED. INTERCOSTAL CORRODED, BETWEEN BS 847 - 867, STRINGER 27R. R & R INTERCOSTAL IAW SRM.
- [SDR SWAA2015121146961](https://openairdocs.org/sdr/SWAA2015121146961), Nov 18, 2015: WEB. CORRODED. FORWARD CARGO DOOR THRESHOLD SILL WEB CORRODED. R & R WEB IAW SRM.
- [SDR SWAA2015120746751](https://openairdocs.org/sdr/SWAA2015120746751), Nov 18, 2015: SUPPORT. CORRODED. FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 500C - 500D, BETWEEN STRINGER 26R - 25R. R & R SUPPORT IAW SRM.
- [SDR SWAA2015121647184](https://openairdocs.org/sdr/SWAA2015121647184), Nov 15, 2015: COVER. MISSING. LEFT EMER EXIT AISLE LIGHT COVER MISSING AT ROW 10. INSTALLED COVER IAW AMM.
- [SDR SWAA2015120946895](https://openairdocs.org/sdr/SWAA2015120946895), Nov 15, 2015: LENS. MISSING. LEFT OVERHEAD BIN EMER LIGHT LENS MISSING AT ROW 6. INSTALLED LENS IAW AMM.
- [SDR SWAA2015102145180](https://openairdocs.org/sdr/SWAA2015102145180), Oct 20, 2015: CHARGER. INOPERATIVE. RIGHT OVERWING EMER EXIT SIGN INOPERATIVE. R & R BATTERY CHARGER IAW AMM.
- [SDR SWAA2015042438886](https://openairdocs.org/sdr/SWAA2015042438886), Apr 19, 2015: INDICATOR. MISSING. OVERHEAD EMER LIGHTS INDICATOR LIGHT MISSING. INSTALLED INDICATOR IAW AMM.
- [SDR SWAA2015060340316](https://openairdocs.org/sdr/SWAA2015060340316), Mar 21, 2015: FRAME. CRACKED. FUSELAGE MAIN FRAME CRACKED AT LT STATION 727. REPAIRED FRAME IAW EA.
- [SDR SWAA2015042438908](https://openairdocs.org/sdr/SWAA2015042438908), Mar 21, 2015: FRAME. CRACKED. RIGHT FRAME OTBD CHORD CRACKED AT BS 727. REPAIRED CHORD IAW EA.
- [SDR SWAA2014110333644](https://openairdocs.org/sdr/SWAA2014110333644), Oct 31, 2014: SCUFF PLATE. CRACKED. FORWARD CARGO DOOR FRAME MIDDLE SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.

All 335: https://openairdocs.org/aircraft/N359SW/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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