# N696SW: 1988 Boeing 737-3T5, registration cancelled 2009-06-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 23, 2009 - Status when cancelled: Sale reported - Airframe: [Boeing 737-3T5](https://openairdocs.org/model/boeing-737-3t5) (registry code 1384608) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Serial number: 23064 - Year built: 1988 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 17, 1992 - Last registry action: August 13, 2008 - Mode S code: A942A5 - Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - Owner type: Individual - Owner's area on the map: 25.8050° N, 80.3151° W: Placed by OpenAirDocs at the center of ZIP code 33122, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N696SW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=696SW - Page: https://openairdocs.org/deregistered/N696SW-2009-06-23 From the FAA registry file of October 28, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Boeing 737-3T5: https://openairdocs.org/model/boeing-737-3t5.md ## Service difficulty reports (108, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SWAA080051](https://openairdocs.org/sdr/SWAA080051), Jan 1, 2008: BUSHING. CORRODED. DURING SCHEDULED C2 CHECK, FOUND RT MLG TRUNNION LINK HAT BUSHINGS CORRODED. REMOVED AND REPLACED TRUNNION LINK PER MT. - [SDR SWAA080050](https://openairdocs.org/sdr/SWAA080050), Jan 1, 2008: KEELBEAM. CORRODED. DURING SCHEDULED C2 CHECK, FOUND RT KEEL BEAM CORRODED AT BS 500D TO BS 520. REPAIRED KEEL BEAM PER SRM. - [SDR SWAA080052](https://openairdocs.org/sdr/SWAA080052), Jan 1, 2008: BUSHING. CORRODED. DURING SCHEDULED C2 CHECK, FOUND RT MLG STRUT FWD TRUNNION LINK LUG HAT BUSHINGS CORRODED. REMOVED AND REPLACED MLG OUTER CYLINDER AND COLLAR PER MT. - [SDR SWAA080053](https://openairdocs.org/sdr/SWAA080053), Jan 1, 2008: TRUNNION PIN. CORRODED. DURING SCHEDULED C2 CHECK, FOUND RIGHT MLG BEAM CLEVIS TRUNNION PIN CORRODED. REMOVED AND REPLACED CLEVIS PER MT. - [SDR SWAA076486](https://openairdocs.org/sdr/SWAA076486), Dec 23, 2007: COVER. BROKEN. DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER BROKEN FROM ROW 6 TO ROW 7. REMOVED AND REPLACED EEPLS PER MM. - [SDR SWAA076485](https://openairdocs.org/sdr/SWAA076485), Dec 23, 2007: KEELBEAM. CORRODED. DURING SCHEDULED C2 CHECK, FOUND RT FUSELAGE KEEL BEAM CORRODED FROM BS 500C TO BS 540. REMOVED AND REPLACED KEEL BEAM SECTION PER SRM. - [SDR SWAA076031](https://openairdocs.org/sdr/SWAA076031), Dec 5, 2007: SLIDE. OUT OF ADJUST. DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. - [SDR SWAA074368](https://openairdocs.org/sdr/SWAA074368), Sep 1, 2007: SKIN. CRACKED. DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STR 21L. REPAIRED SKIN PER SWA EA. - [SDR SWAA074332](https://openairdocs.org/sdr/SWAA074332), Sep 1, 2007: LAMP. INOPERATIVE. DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. - [SDR SWAA073458](https://openairdocs.org/sdr/SWAA073458), Jul 14, 2007: SKIN. CRACKED. DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740E, STR 18R. REPAIRED SKIN PER SWA EA. - [SDR SWAA072259](https://openairdocs.org/sdr/SWAA072259), May 4, 2007: SLIDE. OUT OF POSITION. L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED EVAC SLIDE PER MM. - [SDR SWAA071103](https://openairdocs.org/sdr/SWAA071103), Feb 24, 2007: SKIN. CRACKED. DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED BS 516D, STR 12R. REPAIRED SKIN PER SWA EA. - [SDR SWAA071015](https://openairdocs.org/sdr/SWAA071015), Feb 19, 2007: LIGHT. INOPERATIVE. DURING SCHEDULED SPV CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. - [SDR SWAA064891](https://openairdocs.org/sdr/SWAA064891), Dec 12, 2006: SKIN. CRACKED. DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 517, STR 12L. REPAIRED SKIN PER SWA EA. - [SDR SWAA064262](https://openairdocs.org/sdr/SWAA064262), Nov 7, 2006: SLIDE. OUT OF ADJUST. DURING SCHEDULED PAE CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. - [SDR SWAA063922](https://openairdocs.org/sdr/SWAA063922), Oct 11, 2006: CHARGER. INOPERATIVE. DURING SCHEDULED C1 CHECK, FOUND FWD CABIN EMERGENCY BATTERY PACK CHARGER NOT CHARGING. REMOVED AND REPLACED BATTERY CHARGER PER MM. - [SDR SWAA062413](https://openairdocs.org/sdr/SWAA062413), Jul 12, 2006: SKIN. CRACKED. DURING SCHEDULED C4 CHECK, FOUND RT WING NR 6 L/E SLAT SKIN CRACKED AT LOWER T/E. REPAIRED L/E SLAT SKIN PER SWA EA. - [SDR SWAA062412](https://openairdocs.org/sdr/SWAA062412), Jul 12, 2006: SKIN. DELAMINATED. DURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP LOWER INBOARD CORNER DELAMINATED. REMOVED AND REPLACED FLAP PER MM. - [SDR SWAA062061](https://openairdocs.org/sdr/SWAA062061), Jun 14, 2006: SLIDE. LOW PRESSURE. R2 DOOR EMERGENCY EVAC SLIDE INDICATED, LOW PRESSURE. REMOVED AND REPLACED EVAC SLIDE PER MM. - [SDR SWAA061908](https://openairdocs.org/sdr/SWAA061908), Jun 2, 2006: SKIN. DELAMINATED. DURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED LOWER SURFACE. REMOVED AND REPLACED RT WING FLAP PER MM. - [SDR SWAA061907](https://openairdocs.org/sdr/SWAA061907), Jun 2, 2006: SKIN. CRACKED. DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504, STR 16R. REPAIRED SKIN PER SRM. - [SDR SWAA061899](https://openairdocs.org/sdr/SWAA061899), Jun 2, 2006: SLIDE. OUT OF POSITION. L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED EVAC SLIDE PER MM. - [SDR SWAA061124](https://openairdocs.org/sdr/SWAA061124), Apr 2, 2006: SKIN. CRACKED. DURING SCHEDULED C3 CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACKED AT AFT SPAR, STAB STA 125. REPAIRED STAB PER SRM. - [SDR SWAA053982](https://openairdocs.org/sdr/SWAA053982), Dec 14, 2005: SKIN. DELAMINATED. DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM. - [SDR SWAA053875](https://openairdocs.org/sdr/SWAA053875), Dec 5, 2005: SKIN. CRACKED. DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740D, STR 19R. REPAIRED SKIN PER SWA EA AND SRM. - [SDR SWAA053874](https://openairdocs.org/sdr/SWAA053874), Dec 5, 2005: SKIN. CRACKED. DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730E, STR 19R. REPAIRED SKIN PER SWA EA & SRM. - [SDR SWAA052515](https://openairdocs.org/sdr/SWAA052515), Aug 18, 2005: STRINGER. CORRODED. DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 991.5, STR 24R. REPAIRED STRINGER PER SRM. - [SDR SWAA052457](https://openairdocs.org/sdr/SWAA052457), Aug 15, 2005: VERTICAL BEAM. CRACKED. DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE VERTICAL BEAM WEB CRACKED AT BS 183.5, RBL 5.7, WL 185. REPAIRED WEB PER SWA EA & SRM. - [SDR SWAA052456](https://openairdocs.org/sdr/SWAA052456), Aug 15, 2005: FRAME. CRACKED. DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME INNER CHORD CRACKED AT BS 348.2, STR 15L. REMOVED AND REPLACED INNER FRAME CHORD PER SRM. - [SDR SWAA052455](https://openairdocs.org/sdr/SWAA052455), Aug 15, 2005: FRAME. CRACKED. DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, STR 10L. REPAIRED FRAME PER SWA EA. - [SDR SWAA052444](https://openairdocs.org/sdr/SWAA052444), Aug 14, 2005: CLIP. CRACKED. DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 500D, STR 7L. REMOVED AND REPLACED CLIP PER SRM. - [SDR SWAA052443](https://openairdocs.org/sdr/SWAA052443), Aug 14, 2005: CLIP. CRACKED. DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED CLIP PER SRM. - [SDR SWAA052442](https://openairdocs.org/sdr/SWAA052442), Aug 14, 2005: STRINGER SPLICE. CRACKED. DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. - [SDR SWAA052441](https://openairdocs.org/sdr/SWAA052441), Aug 14, 2005: SKIN. CRACKED. DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 10L. REPAIRED SKIN PER SWA EA. - [SDR SWAA052440](https://openairdocs.org/sdr/SWAA052440), Aug 14, 2005: BULKHEAD. CRACKED. DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE VERTICAL BEAM WEB CRACKED AT BS 178 BULKHEAD, BETWEEN LBL 17.1 TO RBL 17.1, BETWEEN WL 212 TO WL 227. REPAIRED WEB P - [SDR SWAA052415](https://openairdocs.org/sdr/SWAA052415), Aug 11, 2005: FITTING. BROKEN. DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT FLOOR FITTING BROKEN. REMOVED AND REPLACED FITTING PER MM. - [SDR SWAA052392](https://openairdocs.org/sdr/SWAA052392), Aug 10, 2005: VERTICAL BEAM. CRACKED. DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 181, RBL 17.1, WL 181. REPAIRED WEB PER SRM. - [SDR SWAA052391](https://openairdocs.org/sdr/SWAA052391), Aug 10, 2005: STRINGER CLIP. CRACKED. DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED CLIP PER SRM. - [SDR SWAA052390](https://openairdocs.org/sdr/SWAA052390), Aug 10, 2005: STRINGER CLIP. CRACKED. DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 360, STR 13L. REMOVED AND REPLACED CLIP PER SRM. - [SDR SWAA052362](https://openairdocs.org/sdr/SWAA052362), Aug 8, 2005: BULKHEAD. CRACKED. DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE WEB CRACKS AT BS 178 BULKHEAD, RBL 5 & LBL 5, WL 200. REPAIRED WEB PER SRM. - [SDR SWAA051466](https://openairdocs.org/sdr/SWAA051466), May 19, 2005: LIGHT. BROKEN. DURING SCHEDULED RON CHECK, FOUND RT OVERWING EMERGENCY WALL LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. - [SDR SWAA051378](https://openairdocs.org/sdr/SWAA051378), May 11, 2005: SKIN. DELAMINATED. DURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. - [SDR SWAA051377](https://openairdocs.org/sdr/SWAA051377), May 10, 2005: SLIDE. OUT OF ADJUST. DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. - [SDR SWAA050313](https://openairdocs.org/sdr/SWAA050313), Feb 3, 2005: SKIN. DELAMINATED. DURING SCHEDULED CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING T/E AFT FLAP PER MM. - [SDR SWAA050312](https://openairdocs.org/sdr/SWAA050312), Feb 3, 2005: SKIN. CRACKED. DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 927 + 6, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. - [SDR SWAA043630](https://openairdocs.org/sdr/SWAA043630), Dec 14, 2004: SKIN. CRACKED. DURING SPV, FOUND FUSELAGE SKIN AT BS 727F + 15 BETWEEN STRINGER 18R AND STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. - [SDR SWAA042210](https://openairdocs.org/sdr/SWAA042210), Aug 3, 2004: SLIDE. OUT OF ADJUST. L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. - [SDR SWAA040600](https://openairdocs.org/sdr/SWAA040600), Feb 25, 2004: SKIN. CRACKED. DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STRINGER 23L. REPAIRED SKIN PER SRM. - [SDR SWAA032679](https://openairdocs.org/sdr/SWAA032679), Dec 8, 2003: BATTERY PACK. INOPERATIVE. MID CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. - [SDR SWAA032677](https://openairdocs.org/sdr/SWAA032677), Dec 7, 2003: POWER SUPPLY. INOPERATIVE. DURING SCHEDULED C3 CHECK, FOUND BULLNOSE EMERGENCY LIGHT INOP AT RT SIDE, SECOND FROM AFT END. REMOVED AND REPLACED POWER SUPPLY ASSY PER MM. All 108: https://openairdocs.org/deregistered/N696SW-2009-06-23/reports.md ## 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, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20020105001449I](https://openairdocs.org/incident/20020105001449I), Jan 5, 2002: Boeing 7373T5 (N696SW), Sacramento, CA, Minor damage. (-23) After landing on roll out the aircraft slid off the end of runway 16L while attempting to turn onto taxiway D-11 at ksmf. After departing the runway the… --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.