# N14341: 1987 Boeing 737-3TO, registration cancelled 2009-03-30 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 30, 2009 - Status when cancelled: Valid registration - Airframe: [Boeing 737-3TO](https://openairdocs.org/model/boeing-737-3to) (registry code 138447G) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Serial number: 23579 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: April 13, 1987 - Certificate issued: March 30, 2009 - Last registry action: March 30, 2009 - Mode S code: A0B0D3 - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N14341 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14341 - Page: https://openairdocs.org/deregistered/N14341-2009-03-30 From the FAA registry file of October 31, 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 737-3TO: https://openairdocs.org/model/boeing-737-3to.md ## Service difficulty reports (45) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0700416](https://openairdocs.org/sdr/CALA0700416), Aug 9, 2007: LANDING GEAR. MALFUNCTIONED. ALL LANDING GEAR EXTENDED ON ITS OWN WITH GEAR HANDLE IN OFF POSITION DURING CLIMBOUT AT 18,000 FEET AND 290 KNOTS. THE GEAR LIGHTS INDICATED THREE GREEN AND TH - [SDR CALA0600373](https://openairdocs.org/sdr/CALA0600373), Sep 28, 2006: FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN AFT CARGO DOOR CUTOUT FORWARD FRAME AT LOWER STOP FITTING, STA 794.3. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND - [SDR CALA0600370](https://openairdocs.org/sdr/CALA0600370), Sep 27, 2006: KEELBEAM. CORRODED. INSPECTION FOUND KEEL BEAM CORRODED AT STA 520-530, S28R. THE CORROSION WAS REMOVED AND THE KEEL BEAM WAS REPAIRED IAW SRM 53-60-12 AND 51-40-02. - [SDR CALA0600364](https://openairdocs.org/sdr/CALA0600364), Sep 24, 2006: HINGE FITTING. CORRODED. INSPECTION FOUND L-1 DOOR HINGE FITTING CORRODED AROUND BOLT HOLE AT STA 303.9. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0600363](https://openairdocs.org/sdr/CALA0600363), Sep 23, 2006: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN NR 6 FIXED L/E SKIN AT WS 255-389. REPAIRED IAW SRM 51-70-17 AND 51-40-02. - [SDR CALA0600362](https://openairdocs.org/sdr/CALA0600362), Sep 23, 2006: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN AFT CARGO DOOR SKIN AT LIGHTENING HOLE IN CENTER OF DOOR. A DOUBLER WAS INSTALLED IAW ECRA 5232-01082. - [SDR CALA0600358](https://openairdocs.org/sdr/CALA0600358), Sep 22, 2006: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 1016, RBL 34 TO LBL 27. THE FLOORBEAM TOP CHORD WAS REMOVED AND REPLACED IAW ECRA 5310-03851, REV C. - [SDR CALA0600347](https://openairdocs.org/sdr/CALA0600347), Sep 17, 2006: SEAT TRACK. CORRODED. INSPECTION FOUND MAIN CABIN SEAT TRACK CORRODED AT STA 328-343, RBL 43. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0600346](https://openairdocs.org/sdr/CALA0600346), Sep 17, 2006: ANGLE. CORRODED. INSPECTION FOUND MAIN CABIN L-1 DOOR Z-ANGLE CORRODED AT STA 306-350, LBL 54. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0600345](https://openairdocs.org/sdr/CALA0600345), Sep 16, 2006: SEAT TRACK. CORRODED. INSPECTION FOUND MAIN CABIN SEAT TRACK CORRODED AT STA 277-291, RBL 42. A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-40-02 AND 51-20-01. - [SDR CALA0600344](https://openairdocs.org/sdr/CALA0600344), Sep 16, 2006: FLOORBEAM. CORRODED. INSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED AT STA 295, RBL 45. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-10-5 - [SDR CALA0600341](https://openairdocs.org/sdr/CALA0600341), Sep 15, 2006: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED ON TOP AND BOTTOM AT STA 986.5, RBL 43. A REPAIR STRAP WAS INSTALLED IAW SRM 53-00-51, FIGURE 201, REPAIR 3. - [SDR CALA0300709](https://openairdocs.org/sdr/CALA0300709), Dec 11, 2003: PRESSURE PANEL. CRACKED. INSPECTION FOUND A 12 INCH CRACK IN RT PRESSURE DECK AT STA 670, RBL 43, WL 200. THE PRESSURE DECK WAS REPAIRED IAW ECRA 5312-01031 AND SRM 53-60-51. - [SDR CALA0200484](https://openairdocs.org/sdr/CALA0200484), Oct 3, 2002: SKIN. CRACKED. INSPECTION FOUND A 0.050" CRACK AT EDGE OF LIGHTENING HOLE IN C-2 DOOR INTERIOR SKIN. SECOND ROW FROM LEADING EDGE CENTER OF DOOR. A DOUBLER REPAIR WAS INSTALLE - [SDR CALA0200483](https://openairdocs.org/sdr/CALA0200483), Oct 3, 2002: SKIN. CRACKED. INSPECTION FOUND A .040" CRACK AT EDGE OF LIGHTENING HOLE IN C-1 DOOR INTERIOR SKIN. SECOND ROW AFT OF LEADING EDGE, CENTER OF DOOR INTERIOR. A DOUBLER REPAIR W - [SDR CALA0200478](https://openairdocs.org/sdr/CALA0200478), Sep 28, 2002: FRAME. CRACKED. INSPECTION FOUND A 1" CRACK IN FRAME AND FRAME WAS BENT IN AFT PIT AT STA 807 BETWEEN STRINGER 23L AND 24L. A FRAME REPAIR WAS INSTALLED IAW SRM 51-70-11. - [SDR CALA0200477](https://openairdocs.org/sdr/CALA0200477), Sep 27, 2002: WEB. CORRODED. INSPECTION FOUND AFT CARGO PIT THRESHOLD WEB CORRODED AT STA 793-847. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0200475](https://openairdocs.org/sdr/CALA0200475), Sep 25, 2002: SUPPORT. CORRODED. INSPECTION FOUND AFT BAGGAGE BIN THRESHOLD FORWARD WEB SUPPORT CORRODED. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0200474](https://openairdocs.org/sdr/CALA0200474), Sep 25, 2002: WEB. CORRODED. INSPECTION FOUND AFT BAG BIN THRESHOLD LOWER SUPPORT WEB CORRODED IN SEVERAL SPOTS AT STA 794-847, S26R. THE SUPPORT WEB WAS REMOVED AND REPLACED IAW SRM 51-10- - [SDR CALA0200473](https://openairdocs.org/sdr/CALA0200473), Sep 25, 2002: INTERCOSTAL. CORRODED. INSPECTION FOUND R/H INTERCOSTAL IN AFT CARGO AREA CORRODED AT STA 747-767, RBL 22. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0200472](https://openairdocs.org/sdr/CALA0200472), Sep 24, 2002: WEB. CORRODED. INSPECTION FOUND FORWARD PIT DOOR CUTOUT AFT JAMB R/H LOWER WEB CORRODED ON UNDERSIDE AT STA 500. A WEB SPLICE REPAIR WAS INSTALLED IAW SRM 51-70-13, FIGURE 1. - [SDR CALA0200471](https://openairdocs.org/sdr/CALA0200471), Sep 24, 2002: SEAT TRACK. CORRODED. INSPECTION FOUND L/H O/B SEAT TRACK CORRODED AT STA 500. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-2. - [SDR CALA0200470](https://openairdocs.org/sdr/CALA0200470), Sep 22, 2002: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 947.5-967, LBL 18. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0200469](https://openairdocs.org/sdr/CALA0200469), Sep 20, 2002: STRINGER. CRACKED. INSPECTION FOUND A 1/2" CRACK IN STRINGER 16R FORWARD OF ICE LIGHT AT BS 500C. THE STRINGER SECTION WAS REPLACED IAW SRM 53-00-03, FIGURE 202. - [SDR CALA0200468](https://openairdocs.org/sdr/CALA0200468), Sep 19, 2002: FRAME. CRACKED. INSPECTION FOUND LEFT AND RIGHT MAIN BS 616 FRAME INNER CHORDS CRACKED BELOW MAIN CABIN FLOOR. THE CRACKS WERE 1 INCH EACH. THE CRACKED AREAS WERE CUT OUT AND F - [SDR CALA0200466](https://openairdocs.org/sdr/CALA0200466), Sep 18, 2002: ANGLE. CRACKED. INSPECTION FOUND A 2" CRACK IN WEB L-ANGLE AT STA 927-947. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-02. - [SDR CALA0200462](https://openairdocs.org/sdr/CALA0200462), Sep 15, 2002: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 52 TO RBL 52. THE UPPER CAP WAS REMOVED AND A NEW "T" CHORD REPAIR WAS INSTALLED IAW ECRA 5310-03851. - [SDR CALA0200457](https://openairdocs.org/sdr/CALA0200457), Sep 10, 2002: FLOOR SUPPORT. CORRODED. INSPECTION FOUND RT DIAGONAL FLOOR SUPPORT CORRODED AT STA 1006-1016. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0200456](https://openairdocs.org/sdr/CALA0200456), Sep 10, 2002: FLOOR SUPPORT. CORRODED. INSPECTION FOUND LT DIAGONAL FLOOR SUPPORT CORRODED AT STA 1006 TO 1016. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0000058](https://openairdocs.org/sdr/CALA0000058), Jan 21, 2000: SKIN. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN FUSELAGE SKIN CUTOUT AT STA 380, AFT END OF EQUIPMENT COOLING EXHAUST. REPAIRED IAW ECRA 5330-02894. - [SDR CALA9800149](https://openairdocs.org/sdr/CALA9800149), Jan 30, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AROUND NUT PLATE HOLES AT STA 500C TO 500D BETWEEN STRINGERS 26L AND 27L. THE CORRODED AREA WAS REMOVED, A REPAIR DOUBLER AN - [SDR CALA9800130](https://openairdocs.org/sdr/CALA9800130), Jan 27, 1998: SOCKET. INOPERATIVE. INSPECTION FOUND, RT FORWARD SERVICE DOOR EXTERIOR EMERGENCY LIGHT INTERMITTENT. THE LIGHT SOCKET WAS REPLACED IAW MM 33-51-00. - [SDR CALA9800097](https://openairdocs.org/sdr/CALA9800097), Jan 22, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 967, LBL 15. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51. - [SDR CALA9800096](https://openairdocs.org/sdr/CALA9800096), Jan 22, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 967, RBL 0 TO RBL 29. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51. - [SDR CALA9800095](https://openairdocs.org/sdr/CALA9800095), Jan 21, 1998: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED FROM STA 947-967, RBL 18. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-2. - [SDR CALA9800094](https://openairdocs.org/sdr/CALA9800094), Jan 20, 1998: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED FROM STA 1006 TO 1016, LBL 6 TO 18. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-2. - [SDR CALA9800086](https://openairdocs.org/sdr/CALA9800086), Jan 18, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AROUND SCREW HOLES AT STA 947, LBL 6. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51. - [SDR CALA9800085](https://openairdocs.org/sdr/CALA9800085), Jan 17, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 328, BBL 0 TO RBL 30. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51. - [SDR CALA9800084](https://openairdocs.org/sdr/CALA9800084), Jan 17, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, LBL 10 TO RBL 30. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51. - [SDR CALA9700494](https://openairdocs.org/sdr/CALA9700494), Apr 6, 1997: FIRE DETECT UNIT. INOPERATIVE. THE APU FIRE BELL SOUNDED WHILE STARTING THE APU ON SHORT FINAL. THE OVERSPEED LIGHT CAME ON AND THE BOTTLE DISCHARGE LIGHT DID NOT ILLUMINATE. THE FIRE LIGHT R - [SDR CALA9601211](https://openairdocs.org/sdr/CALA9601211), Aug 23, 1996: AP ACCY UNIT. INOPERATIVE. UPON SELECTING THE APP MODE AIRCRAFT LOST ALL FLIGHT DIRECTION, NR 1 AIRSPEED BUG, YAW DAMPER, BOOST PUMPS, BUT NO BUSS OFF LIGHT ILLUMINATED. THE AIRCRAFT LAND - [SDR CAL960469](https://openairdocs.org/sdr/CAL960469), Apr 11, 1996: SKIN. PUNCTURED. EWR - INSPECTION FOUND A 2 INCH BY 2 INCH PUNCTURE IN RT FUELAGE SKIN ABOVE WINDOW NR 8 AT STA 480. THE AREA WAS REPAIRED IAW SRM 53-00-01, FIGURE 202. (X) - [SDR CAL960079](https://openairdocs.org/sdr/CAL960079), Jan 21, 1996: BATTERY PACK. DISCHARGED. HOU - THE LEFT AFT EMERGENCY CEILING LIGHT BATTERY PACK FAILED CAPACITY TEST. THE BATTERY PACK WAS REMOVED AND REPLACED. (M) - [SDR CAL950734](https://openairdocs.org/sdr/CAL950734), Aug 20, 1995: UPLOCK ACTUATOR. INOPERATIVE. BUF - FLT 0640 - THE RT MLG GAVE AN UNSAFE GEAR INDICATION WHEN GEAR WAS EXTENDED ON APPROACH TO BUF. 'ABNORMAL' PROCEDURES WERE FOLLOWED AND A TOWER FLY-BY WAS - [SDR CAL950621](https://openairdocs.org/sdr/CAL950621), Jul 27, 1995: COUPLER. RATE GYRO FAILED. FLT 0131-MEX-THE YAW DAMPER WENT FULL SCALE RT WITH RUDDER MOVEMENT TO THE RT AT APPROX 11,000 FT WITH AIRSPEED BETWEEN 180 AND 170. THE YAW DAMPER WAS TURNED O ## 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 19950820030959I](https://openairdocs.org/incident/19950820030959I), Aug 20, 1995: Boeing 7373T0 (N14341), Buffalo, NY. Landing gear problems near buf. Right main stayed up. Lowered gear manually. Pinned gear after landing. --- 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.