# N965CA: 1996 Canadair CL-600-2B19, registration cancelled 2014-04-15 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 15, 2014 - Status when cancelled: Valid registration - Airframe: [Canadair CL-600-2B19](https://openairdocs.org/model/canadair-cl-600-2b19) (registry code 1900309) - 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: 7131 - Year built: 1996 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 3, 1996 - Certificate issued: October 26, 2007 - Last registry action: August 16, 2012 - Mode S code: AD6EEC - 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: 40.8659° N, 112.0391° W: Placed by OpenAirDocs at the center of ZIP code 84116, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N965CA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=965CA - Page: https://openairdocs.org/deregistered/N965CA-2014-04-15 From the FAA registry file of November 5, 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 Canadair CL-600-2B19: https://openairdocs.org/model/canadair-cl-600-2b19.md ## Service difficulty reports (119, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR COMA2011080850051](https://openairdocs.org/sdr/COMA2011080850051), Aug 6, 2011: SELECTOR VALVE. FAILED. ON APPROACH INTO DTW RECEIVED GEAR DISAGREE AFTER SELECTING GEAR DOWN, BOTH MLG FAILED TO EXTEND. EMERGENCY DECLARED, QRH FOLLOWED, A/C LANDED SAFELY AT DTW. RE - [SDR COMA2010092850209](https://openairdocs.org/sdr/COMA2010092850209), Sep 27, 2010: VANE. CHAFED. RIGHT I/B FLAP VANE LEADING EDGE FOUND TO HAVE CHAFE DAMAGE. REPLACED THE RIGHT I/B FLAP VANE LEADING EDGE IAW CRJ 200 SRM. - [SDR COMA2010092850208](https://openairdocs.org/sdr/COMA2010092850208), Sep 27, 2010: BULKHEAD. CRACKED. FS 559.0 BULKHEAD WEB FOUND TO BE CRACKED. REPAIRED IAW REO 601R-53-41-260 AND DEVIATION REO 601R-53-41-609. - [SDR COMA2010091650202](https://openairdocs.org/sdr/COMA2010091650202), Sep 15, 2010: CROSSBEAM. CORRODED. FS 280 FLOOR SUPPORT CROSSBEAM AT LBL 9 TO RBL 9 IS CORRODED. REPAIRED CROSSBEAM PER SRM 51-42-06. - [SDR COMA2010091650201](https://openairdocs.org/sdr/COMA2010091650201), Sep 15, 2010: BULKHEAD. CORRODED. FS 280 BULKHEAD WEB AT LBL 11 TO LBL 13 IS CORRODED. REPAIRED BULKHEAD WEB AT FS 280 PER SRM 53-11-19. - [SDR COMA086355](https://openairdocs.org/sdr/COMA086355), Aug 9, 2008: SKIN. DAMAGED. PASSENGER DOOR CUTOUT AIRFRAME SIDE FWD LOWER CORNER EXISTING REPAIR IS DAMAGED. REPAIRED PASSENGER DOOR CUTOUT AIRFRAME SIDE LOWER FWD CORNER PER CRJ REO 601R- - [SDR COMA086354](https://openairdocs.org/sdr/COMA086354), Aug 9, 2008: FLOOR SKIN. CRACKED. PRESSURE FLOOR SKIN AT STA 460 BETWEEN LBL 9 AND RBL 9 IS CRACKED. REPAIRED PRESSURE FLOOR SKIN WEB AT FS 460.00 WITH TEMPORARY REPAIR PER REO 601R-53-41-103 RE - [SDR COMA086353](https://openairdocs.org/sdr/COMA086353), Aug 9, 2008: SUPPORT BEAM. CRACKED. RT UPPER WEB-ENG SUPPORT BEAM ASSEMBLY CRACKED. COMPLIED WITH REPAIR TO UPPER WEB-ENG SUPPORT. BEAM ASSEMBLY BETWEEN BL 27.5 AND 36.2 PER REO601R-53-61-569. (S) - [SDR COMA086352](https://openairdocs.org/sdr/COMA086352), Aug 9, 2008: SUPPORT BEAM. CRACKED. LT UPPER WEB-ENG SUPPORT BEAM ASSEMBLY CRACKED. COMPLIED WITH REPAIR TO UPPER WEB-ENG SUPPORT. BEAM ASSEMBLY BETWEEN BL27.5 AND 36.2 PER REO601R-53-51-569. (S) - [SDR COMA086351](https://openairdocs.org/sdr/COMA086351), Aug 9, 2008: DOUBLER. CRACKED. RT SIDE FUSELAGE FRAME DOUBLER AT FS 640.00 IS CRACKED. COMPLIED WITH MODIFICATION K601R360094 AT FS 640 IAW S/B 601R-53-061. (S) - [SDR COMA086350](https://openairdocs.org/sdr/COMA086350), Aug 9, 2008: FRAME. CRACKED. LT SIDE FUSELAGE FRAME DOUBLER AT FS 640.00 IS CRACKED. COMPLIED WITH MODIFICATION K601R36009-R AT FS 640 IAW S/B 601R-53-061. (S) - [SDR COMA086349](https://openairdocs.org/sdr/COMA086349), Aug 9, 2008: DOUBLER. CRACKED. RT INTERNAL SKIN DOUBLER AT STA 640 IS CRACKED. FABRICATED PARTS AT STA 640 IAW CRJ REO 601R-53-61-506. (S) - [SDR COMA086348](https://openairdocs.org/sdr/COMA086348), Aug 9, 2008: DOUBLER. CRACKED. LT INTERNAL SKIN DOUBLER AT STA 640 IS CRACKED. FABRICATED PARTS AT STA 640 IAW CRJ REO 601R-53-61-506. (S) - [SDR COMA0860321](https://openairdocs.org/sdr/COMA0860321), Jul 13, 2008: LAMP. BURNED OUT. FLIGHT 9422. DURING LINE CHECK FOUND ROW 2-5 EMERGENCY FLOOR LIGHTS INOP. REMOVED AND REPLACED FLOOR EMERGENCY LIGHT STRIP. (A) - [SDR COMA0860234](https://openairdocs.org/sdr/COMA0860234), Apr 30, 2008: INVERTER. INOPERATIVE. FLIGHT 5326 - EMERGENCY LIGHTS NOT WORKING FROM ROW 9 AFT. REPLACED NR 4 INVERTER. NO FURTHER DEFECTS. - [SDR COMA0860213](https://openairdocs.org/sdr/COMA0860213), Apr 6, 2008: LIGHT. NO TEST. FLIGHT 5027 - THE AFT EMERGENCY EXIT FLOOR LIGHTS FAILED TO TEST. DEFERRED PER MEL 33-51-01-6. - [SDR COMA0860185](https://openairdocs.org/sdr/COMA0860185), Mar 20, 2008: RELIEF VALVE. FAULTY. FLIGHT 5103- RECEIVED RIGHT COWL ANTI-ICE MESSAGE WHEN ANTI-ICE SELECTED ON. RETURNED TO JFK, LANDED WITHOUT INCIDENT. REPLACED PRESSURE RELIEF VALVE. NO FURTHE - [SDR COMA0860157](https://openairdocs.org/sdr/COMA0860157), Mar 4, 2008: BATTERY PACK. DISCHARGED. FLIGHT 5479 - FLOOR MOUNTED EMERGENCY STRIP BEHIND ROW 8A IS INOP. REPLACED BATTERY PACK NR 4. NO FURTHER DEFECTS. - [SDR COMA0760489](https://openairdocs.org/sdr/COMA0760489), Jul 16, 2007: BULKHEAD. CRACKED. REAR PRESSURE BULKHEAD CRACKED AROUND LINTEL FITTING. PERFORMED PERMANENT REPAIR TO AFT PRESSURE BULKHEAD IAW REO 601R-53-11-563. - [SDR COMA0760488](https://openairdocs.org/sdr/COMA0760488), Jul 16, 2007: BULKHEAD. CRACKED. FORWARD PRESSURE BULKHEAD CRACKED AT PARKING BRAKE CABLE. REPAIRED IAW REO 601R-53-11-563. - [SDR COMA0670390](https://openairdocs.org/sdr/COMA0670390), May 21, 2007: ENGINE. OVERTEMP. FLIGHT 4988 - DURING TAKEOFF ROLL THE RIGHT ENGINE ITT INDICATED 905C, ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED THE RIGHT ENGINE ASSEMBLY. - [SDR COMA0760386](https://openairdocs.org/sdr/COMA0760386), May 20, 2007: PUMP. MALFUNCTIONED. FLIGHT 5389 - HYD PUMP 1B CIRCUIT BREAKER POPPED WHILE STARTING NR 1 ENGINE. RETURNED TO GATE. RESET BREAKER, PERFORMED OPS CHECK, NO FURTHER DEFECTS. - [SDR COMA0760359](https://openairdocs.org/sdr/COMA0760359), May 3, 2007: BULKHEAD. CRACKED. DURING FS 559 INSPECTION FOUND SEMI-BULKHEAD CRACKED AT RBL 18. STOP DRILLED CRACK AND INSTALLED DOUBLER IAW REO 601R-53-41-353. - [SDR COMA076027](https://openairdocs.org/sdr/COMA076027), Jan 14, 2007: WIRE. FAULTY. FLIGHT 5342 - RECEIVED ANTI-ICE DUCT WARNING MESSAGE IN FLIGHT. FOLLOWED QRH AND DIVERTED TO GSO. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THERMAL SWITCH WIRE A - [SDR COMA0660734](https://openairdocs.org/sdr/COMA0660734), Dec 27, 2006: ACTUATOR. FAILED. FLIGHT 5206 - RECEIVED A FLAP FAIL CAUTION MESSAGE DURING BGR APPROACH AT 30 DEGREE FLAP SETTING. REPLACED THE LEFT OUTBOARD FLAP INBOARD ACTUATOR. - [SDR COMA0660733](https://openairdocs.org/sdr/COMA0660733), Dec 27, 2006: ACTUATOR. FAILED. FLIGHT 5206 - RECEIVED A FLAP FAIL CAUTION MESSAGE DURING BGR APPROACH AT 30 DEGREE FLAP SETTING. REPLACED THE LEFT INBOARD FLAP INBOARD ACTUATOR. - [SDR COMA0660732](https://openairdocs.org/sdr/COMA0660732), Dec 27, 2006: FLAP. MALFUNCTIONED. FLIGHT 5206 - RECEIVED A FLAP FAIL CAUTION MESSAGE DURING BGR APPROACH AT 30 DEGREE FLAP SETTING. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- - [SDR COMA0660720](https://openairdocs.org/sdr/COMA0660720), Dec 21, 2006: WIRE HARNESS. CHAFED. FLIGHT 5323 - DURING CLIMBOUT RECEIVED AN ANTI-ICE DUCT CAUTION MESSAGE, FLIGHT RETURNED TO CVG. REPAIRED CHAFED WIRING ON THE LEFT WING LEADING EDGE AT STA 330 - [SDR COMA0660512](https://openairdocs.org/sdr/COMA0660512), Aug 25, 2006: SUPPORT BEAM. CRACKED. DURING INSPECTION OF THE ENGINE SUPPORT BEAM IAW EO 53-021 (AD 2004-10-03) FOUND CRACK AT LOCATION FS 640, LBL 9.0, WL 119.12 (UPPER BOX BEAM SKIN).PERFORMED RE - [SDR COMA0660383](https://openairdocs.org/sdr/COMA0660383), Jun 8, 2006: PRESSURE VALVE. MALFUNCTIONED. FLIGHT 5063 - DURING CLIMBOUT OF GSO RECEIVED A CABIN DOOR OUTER HANDLE CAUTION MESSAGE, FLIGHT RETURNED TO THE FIELD. RE-RIGGED THE CABIN DOOR PRESSURE VALVE V - [SDR COMA0660381](https://openairdocs.org/sdr/COMA0660381), Jun 6, 2006: WARNING SYSTEM. MALFUNCTIONED. FLIGHT 5063 - AFTER TAKEOFF FROM GSO RECEIVED A CABIN DOOR OUTER HANDLE CAUTION MESSAGE, FLIGHT RETURNED TO THE FIELD. DEFERRED THE CABIN DOOR INDICATION PER ME - [SDR COMA0660351](https://openairdocs.org/sdr/COMA0660351), May 18, 2006: ECU. FAULTY. FLIGHT 5285 - RECEIVED A FLAP FAIL CAUTION MESSAGE AT ZERO DEGREES DURING TAXI AT DCA. REPLACED THE FLAP ELECTRONIC CONTROL UNIT. - [SDR COMA0660348](https://openairdocs.org/sdr/COMA0660348), May 15, 2006: CAUTION MESSAGE. FALSE ACTIVATION. FLIGHT 5719 - FLAP FAIL MESSAGE AT GATE. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). - [SDR COMA0660322](https://openairdocs.org/sdr/COMA0660322), May 1, 2006: FLAP SYSTEM. OUT OF RIG. FLIGHT 5450 - FLAP FAIL CAUTION MESSAGE. FLAPS WILL NOT COME OUT OF ZERO POSITION. FOUND LEFT SIDE FLAP SYSTEM OUT OF RIG. MECHANICALLY AND ELECTRICALLY RIGGED - [SDR COMA0660317](https://openairdocs.org/sdr/COMA0660317), Apr 28, 2006: FLAP SYSTEM. MALFUNCTIONED. FLIGHT 5049 - FLAP FAIL MESSAGE ON GROUND AT 0 DEGREES. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT, MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3, ( - [SDR COMA0660310](https://openairdocs.org/sdr/COMA0660310), Apr 22, 2006: FLAP SYSTEM. MALFUNCTIONED. FLIGHT 5381 - DURING PUSHBACK RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 DEGREES, FLIGHT RETURNED TO THE GATE. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FI - [SDR COMA0660223](https://openairdocs.org/sdr/COMA0660223), Mar 2, 2006: LATCH. DAMAGED. FLIGHT 5701 - EN ROUTE BTV-ATL RECEIVED A CABIN DOOR LATCH CAUTION MESSAGE, FLIGHT DIVERTED TO SYR. ADJUSTED ROD-END OF CABIN DOOR LATCH ROLLER ASSEMBLY. - [SDR COMA0660118](https://openairdocs.org/sdr/COMA0660118), Feb 7, 2006: PRESSURE SWITCH. FAULTY. FLIGHT 5093 - DURING CLIMB-OUT OF EVV RECEIVED A LEFT ENGINE COWL A/ICE CAUTION MESSAGE, FLIGHT RETURNED TO EVV. REPLACED THE LEFT ENGINE COWL ANTI ICE PRESSURE - [SDR COMA0560815](https://openairdocs.org/sdr/COMA0560815), Jan 17, 2006: WINDSHIELD. CRACKED. FLIGHT 5701- PILOT'S WINDSHIELD SHATTERED. REPLACED WINDSHIELD. - [SDR COMA0560652](https://openairdocs.org/sdr/COMA0560652), Nov 27, 2005: FLAP SYSTEM. MALFUNCTIONED. FLIGHT 5850 - RECEIVED A FLAP FAIL CAUTION MESSAGE AFTER LANDING WHEN FLAPS WERE SELECTED TO 20 DEGREES. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST E - [SDR COMA0560490](https://openairdocs.org/sdr/COMA0560490), Sep 6, 2005: LIGHT. INOPERATIVE. FLIGHT 5565 - EMERGENCY FLOOR LIGHTING INOPERATIVE FROM ROWS 2 THROUGH 5. CLEANED CONTACTORS ON EMERGENCY FLOOR TRACK LIGHT STRIP. - [SDR COMA0560484](https://openairdocs.org/sdr/COMA0560484), Sep 2, 2005: LAMP. INOPERATIVE. FLIGHT 5387 - EMERGENCY LIGHTS ROW 1-5 INOPERABLE. RESECURED LIGHT STRIP. - [SDR COMA0560458](https://openairdocs.org/sdr/COMA0560458), Aug 21, 2005: BPSU. OUT OF RIG. FLIGHT 5858 - FLAPS FAIL CAUTION. ADJUSTED THE RIGGING OF THE RT BPSU. - [SDR COMA0560435](https://openairdocs.org/sdr/COMA0560435), Aug 8, 2005: ELEMENT. MALFUNCTIONED. FLIGHT 5105 - LT 14TH STAGE DUCT WARNING. REPLACED THE PYLON DUCT LEAK SENSING ELEMENT. - [SDR COMA0460603](https://openairdocs.org/sdr/COMA0460603), Sep 16, 2004: BULKHEAD. CORRODED. FS 280 HAS CORROSION ON WEB AT CBP WALLS. REPAIRED IAW REO 601R-53-11-584. - [SDR COMA0460519](https://openairdocs.org/sdr/COMA0460519), Sep 16, 2004: SKIN. CORRODED. FS 574 LEFT HAND SIDE HAS TWO CORRODED FASTENERS AT 8 POSITION ABOVE FLOOR. REPAIRED IAW REO 601R-53-61-1135. - [SDR COMA0460522](https://openairdocs.org/sdr/COMA0460522), Sep 16, 2004: FLOORBEAM. CRACKED. CARGO FLOOR CAP CRACKED. IAW SRM 51-42-06, 51-42-13, 51-42-21 AND 51-42-26. - [SDR COMA0460521](https://openairdocs.org/sdr/COMA0460521), Sep 16, 2004: WEB. CRACKED. CARGO CAP WEB AT LIGHTING HOLE IB SIDE CRACKED FROM EXCESSIVE STRESS.IAW SRM 51-42-06, 51-42-13. - [SDR COMA0460520](https://openairdocs.org/sdr/COMA0460520), Sep 16, 2004: SKIN. CRACKED. RT WING PLANK AT VS 148 IS CRACKED. IAW EO 57-020. - [SDR COMA0460518](https://openairdocs.org/sdr/COMA0460518), Sep 16, 2004: BULKHEAD. CORRODED. FS 280 HAS CORROSION ON WEB AT BL AFT SIDE AND CRACKS LOCATED OUTBOARD OF LBL/RBL 9. REPAIRED IAW REO 601R-53-11-136. All 119: https://openairdocs.org/deregistered/N965CA-2014-04-15/reports.md ## Other aircraft with N965CA - [Registered now](https://openairdocs.org/aircraft/N965CA): Costruzioni Aeronautiche Tecna P2012 TRAVELLER, S/N 025/US, built 2020 --- 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.