# N435CA: 2001 Bombardier CL-600-2B19, registration cancelled 2011-09-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 21, 2011 - Exported to: Bermuda - Status when cancelled: Valid registration - Airframe: [Bombardier CL-600-2B19](https://openairdocs.org/model/bombardier-cl-600-2b19) (registry code 1390008) - Engine: [GE CF34 series](https://openairdocs.org/engine/ge-cf34-series) (registry code 30015) - Data sheets: [TCDS A21EA-1](https://openairdocs.org/tcds/A21EA-1) (OpenAirDocs) - Serial number: 7473 - Year built: 2001 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: April 17, 2001 - Certificate issued: January 8, 2008 - Last registry action: January 8, 2008 - Mode S code: A535E4 - 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/N435CA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=435CA - Page: https://openairdocs.org/deregistered/N435CA-2011-09-21 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 Bombardier CL-600-2B19: https://openairdocs.org/model/bombardier-cl-600-2b19.md ## Service difficulty reports (17) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR COMA0660252](https://openairdocs.org/sdr/COMA0660252), Mar 14, 2006: ELEMENT. FAULTY. FLIGHT 5282 - DURING CLIMBOUT OF CVG RECEIVED AN ANTI-ICE DUCT WARNING MESSAGE, FLIGHT RETURNED TO THE FIELD. REPLACED HEAT SENSING ELEMENT A15WK. - [SDR COMA0660111](https://openairdocs.org/sdr/COMA0660111), Feb 4, 2006: LIGHT. INOPERATIVE. FLIGHT 5362 - DURING INSPECTION FOUND THE 3RD CEILING EMERGENCY LIGHT INOPERATIVE. DEFERRED INOPERATIVE EMERGENCY LIGHT PER MEL 33-51-01-1. - [SDR COMA0560658](https://openairdocs.org/sdr/COMA0560658), Nov 30, 2005: VIBRATOR. UNKNOWN. FLIGHT 5525 - LT ENGINE VIBE CAUTION. FOUND LT ENGINE VIBRATION TO BE WITHIN LIMITS. RETURNED TO SERVICE. - [SDR COMA0560205](https://openairdocs.org/sdr/COMA0560205), Mar 27, 2005: SENSOR. FAULTY. FLIGHT 5184 RECEIVED A RT 14TH STAGE DUCT MESSAGE DURING CLIMB OUT OF CVG. AIRCRAFT RETURNED TO THE FIELD. REPLACED THE 14TH STAGE HEAT SENSING ELEMENT. - [SDR COMA0560201](https://openairdocs.org/sdr/COMA0560201), Mar 23, 2005: SENSOR. MALFUNCTIONED. FLIGHT 5060 RECEIVED A WING OVERHEAT WARNING DURING CRUISE FLIGHT. CREW DECLARED AN EMERGENCY AND RETURNED TO CVG. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED WI - [SDR COMA0560122](https://openairdocs.org/sdr/COMA0560122), Feb 13, 2005: CONTROL UNIT. MALFUNCTIONED. FLIGHT 5823 WING OVERHEAT MESSAGE. REPLACED THE TEMP CONTROL UNIT. - [SDR COMA0460565](https://openairdocs.org/sdr/COMA0460565), Oct 7, 2004: FLOOR SUPPORT. CRACKED. RIGHT HAND FLOOR ANGLE FS 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117. - [SDR COMA0460564](https://openairdocs.org/sdr/COMA0460564), Oct 7, 2004: FLOOR SUPPORT. CRACKED. LEFT HAND FLOOR ANGLE FS 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117. - [SDR COMA0460562](https://openairdocs.org/sdr/COMA0460562), Oct 7, 2004: BEAM. CRACKED. CRACK ON THE ENGINE SUPPORT BEAM RIGHT HAND SIDE. PERFORMED REO 601R-53-61-366. - [SDR COMA0460362](https://openairdocs.org/sdr/COMA0460362), Jun 9, 2004: FRAME. CRACKED. RIGHT HAND FS 718.00 BETWEEN STRINGERS 10-12 CRACKED. REMOVED ACCESS PANEL 423CB FROM RIGHT HAND PYLON. REMOVED HI-LOKS AND RIVETS FROM 718 FRAME IN AREA OF REP - [SDR COMA0460361](https://openairdocs.org/sdr/COMA0460361), Jun 9, 2004: FRAME. CRACKED. RIGHT HAND FS 718.00 BETWEEN STRINGERS 10-12 CRACKED. REMOVED ACCESS PANEL 423CB FROM RIGHT HAND PYLON. REMOVED HI-LOKS AND RIVETS FROM 718 FRAME IN AREA OF REP - [SDR COMA0460355](https://openairdocs.org/sdr/COMA0460355), Jun 9, 2004: SKIN. DENTED. DENT IN FUSELAGE SKIN, JUST AFT OF FS 700 AND ABOVE STRINGER. CUT OUT DAMAGED AREA. FABRICATED DOUBLER (2024T-3. 063), INSTALLED DOUBLER. COMPLETED REPAIR IAW R - [SDR COMA0460354](https://openairdocs.org/sdr/COMA0460354), Jun 9, 2004: SKIN. DAMAGED. AIRCRAFT DAMAGED BELOW APU EXHAUST. AIRCRAFT HAS GASH 5.50 INCHES LONG AT FS 682 AND GOUGED SKIN FROM FS 672.00 TO 700. REMOVED EXISITNG FASTENERS AROUND DAMAGE - [SDR COMA0460108](https://openairdocs.org/sdr/COMA0460108), Feb 2, 2004: SENSOR. MALFUNCTIONED. FLIGHT 5167 WING OVERHEAT WARNING MESSAGE. REPLACED THE RT WING OVERHEAT SENSOR. - [SDR COMA0360039](https://openairdocs.org/sdr/COMA0360039), Jan 20, 2003: FAIRING. FLIGHT 5877 RUMBLING NOISE AND VIBRATION FELT IN AIR FRAME.REPLACED MISSING SEALANT AT WING TO FUSELAGE FAIRING. - [SDR COMA0260530](https://openairdocs.org/sdr/COMA0260530), Sep 15, 2002: LATCH HANDLE. CORRODED. UPON INSPECTION MECHANIC FOUND OUTER HANDLE OF CREW EXCAPE HATCH STUCK IN THE DOWN POSITION. WOULD NOT "POP UP" WHEN OPEN BUTTON WAS DEPRESSED.REMOVED HANDLE AS - [SDR COMA0160251](https://openairdocs.org/sdr/COMA0160251), Feb 15, 2001: WARNING SYSTEM. ACTIVATED. ANTI ICE DUCT WARNING. INSTALLED RUBBER BOOTS ON THERMAL SWITCHES WIRE CONNECTION LT OUTBOARD WING LEADING EDGE. ## Other aircraft with N435CA - [Registered now](https://openairdocs.org/aircraft/N435CA): Textron 172S, S/N 172S12060, built 2017 --- 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.