# N975CA: 1996 Canadair CL-600-2B19, registration cancelled 2008-07-16 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 16, 2008 - 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: 7150 - Year built: 1996 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: January 3, 1997 - Certificate issued: June 11, 2007 - Last registry action: June 11, 2007 - Mode S code: AD966B - 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/N975CA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=975CA - Page: https://openairdocs.org/deregistered/N975CA-2008-07-16 From the FAA registry file of October 29, 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 (57, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR COMA0760107](https://openairdocs.org/sdr/COMA0760107), Jan 31, 2007: FLAP SYSTEM. MALFUNCTIONED. FLIGHT 6056 - FLAPS FAILED AT ZERO DEGREES ON APPROACH, AIRCRAFT LANDED SAFELY. COMPLIED WITH AD 2006-12-21, FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTI - [SDR COMA0760002](https://openairdocs.org/sdr/COMA0760002), Jan 1, 2007: WARNING LIGHT. ILLUMINATED. FLIGHT 5418 - EN ROUTE JAX-LGA RECEIVED A RIGHT THRUST REVERSER UNLOCK MESSAGE, FLIGHT DIVERTED TO CHS. DEFERRED THE RIGHT THRUST REVERSER PER MEL 78-30-01. - [SDR COMA0660621](https://openairdocs.org/sdr/COMA0660621), Nov 8, 2006: PROBE. FAILED. FLIGHT 5339 - DURING CLIMB LEFT ENGINE OIL TEMP WENT TO AMBER RANGE. AIRCRAFT RETURNED TO CVG AND LANDED WITHOUT INCIDENT. FOUND OIL TANK OVER SERVICED AND PROB - [SDR COMA0660598](https://openairdocs.org/sdr/COMA0660598), Nov 2, 2006: SHUTOFF VALVE. FAULTY. FLIGHT 5421- UPON GEAR EXTENSION, INBOARD ANTI-SKID INOP MESSAGE APPEARED. CYCLED GEAR, MESSAGE CLEARED, RE-APPEARED UPON EXTENSION. REPLACED PARKING BRAKE SHUT - [SDR COMA0660582](https://openairdocs.org/sdr/COMA0660582), Oct 22, 2006: CONTROL UNIT. MALFUNCTIONED. FLIGHT 5436 - THRUST TO TAKEOFF POWER, AFTER 5 SECONDS STEERING INOP CAUTION MESSAGE AND CONFIG WARNING SPOILER MESSAGE. ABORTED TAKEOFF AT 50 KTS. THRUST LEVER - [SDR COMA0660446](https://openairdocs.org/sdr/COMA0660446), Jul 22, 2006: SEALANT. DEFECTIVE. ENROUTE, THE MLG INTRANSIT SYMBOLS PULSED APPROXIMATELY 7 TIMES, GEAR LOCKED INTO THE UP POSITION 20 SECONDS LATER. PERFORMED FUNCTIONAL TEST OF LANDING GEAR EX - [SDR COMA0660277](https://openairdocs.org/sdr/COMA0660277), Mar 24, 2006: WARNING MESSAGE. ILLUMINATED. FLIGHT 5676 - DURING TAKEOFF ROLL RECEIVED A LEFT THRUST REVERSER UNLOCK MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GATE. DEFERRED THE LEFT THRUST REVERSER PE - [SDR COMA0660199](https://openairdocs.org/sdr/COMA0660199), Feb 27, 2006: FLAP SYSTEM. MALFUNCTIONED. FLIGHT 5507 - DURING LGA APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE ZERO DEGREES, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. COMPLIED WIT - [SDR COMA0660163](https://openairdocs.org/sdr/COMA0660163), Feb 19, 2006: FLAP. MALFUNCTIONED. FLIGHT 5910 - AFTER LANDING AT MSP AND DURING TAXI TO THE GATE RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 DEGREES. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAG - [SDR COMA0560612](https://openairdocs.org/sdr/COMA0560612), Nov 16, 2005: INDICATOR. READS LOW. FLIGHT 5464 - LEFT ENGINE FUEL FLOW 400 LBS, 1000 LBS NORMAL. OPERATIONAL CHECK OF FUEL FLOW WAS NORMAL. - [SDR COMA0560590](https://openairdocs.org/sdr/COMA0560590), Nov 8, 2005: FLAP SYSTEM. MALFUNCTIONED. FLIGHT 5384 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. - [SDR COMA0560551](https://openairdocs.org/sdr/COMA0560551), Oct 12, 2005: CONTROL UNIT. MALFUNCTIONED. FLIGHT 5033 - FLAPS FAIL CAUTION. REPLACED THE FECU. - [SDR COMA0560406](https://openairdocs.org/sdr/COMA0560406), Jul 24, 2005: FLAP SYSTEM. MALFUNCTIONED. FLIGHT 5497- FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. - [SDR COMA0560241](https://openairdocs.org/sdr/COMA0560241), Apr 3, 2005: PUMP. FAULTY. FLIGHT 5886 DURING CRUISE FLIGHT RECEIVED A LOW HYDRAULIC NR 3 SYSTEM PRESSURE CAUTION, CREW DECLARED AN EMERGENCY AND LANDED AT JFK WITHOUT INCIDENT. REPLACED - [SDR COMA0460695](https://openairdocs.org/sdr/COMA0460695), Dec 17, 2004: ANGLE. CORRODED. FLIGHT DURING HEAVY MAINTENANCE CHECK, (PAX DOOR DETAILED INSPECTION) THE PAX DOOR FORWARD AND AFT BOTTOM CORNERS WERE FOUND TO BE CORRODED. BOTH PARTS WERE REP - [SDR COMA0460629](https://openairdocs.org/sdr/COMA0460629), Nov 17, 2004: WIRE HARNESS. DAMAGED. FLIGHT 5806 RECEIVED AN ANTI-SKID CAUTION MESSAGE DURING TAKEOFF ROLL. ABORTED AND AIRCRAFT RETURNED TO THE GATE. REPLACED THE RIGHT OUTBOARD ANTI-SKID DETECTOR - [SDR COMA0460425](https://openairdocs.org/sdr/COMA0460425), Jul 24, 2004: ECU. MALFUNCTIONED. FLIGHT 5801 NW STEERING INOP MESSAGE. REPLACED THE NWS ECU. - [SDR COMA0460351](https://openairdocs.org/sdr/COMA0460351), Jun 4, 2004: INLET. ERODED. RT HAND ENGINE HEATED IN-LIT LIP ERRODED OUT OF LIMITS. REPAIRED RIGHT HAND ENGINE LIP-SKIN USING SERVICEABLE SKIN, 12.5 SECTION IAW SHORTS CMM 71-61-01. - [SDR COMA0460144](https://openairdocs.org/sdr/COMA0460144), Feb 14, 2004: WARNING LIGHT. ILLUMINATED. FLIGHT 5473 RT THRUST REVERSER UNLOCKED MESSAGE. DEFERRED MAINT. IAW MEL. - [SDR COMA0360507](https://openairdocs.org/sdr/COMA0360507), Nov 18, 2003: ACTUATOR. MALFUNCTIONED. ELEVATOR CONTROLS STIFF. REPLACED THE LEFT ELEVATOR PITCH FEEL ACTUATOR. - [SDR COMA0360048](https://openairdocs.org/sdr/COMA0360048), Jan 23, 2003: LIGHT. FLIGHT 5530 EMERGENCY FLOOR LIGHTS AT WING EXITS ARE INOP.FOUND LIGHTS DISCONNECTED - RECONNECTED WIRING AT EXIT LIGHTS. - [SDR COMA0260361](https://openairdocs.org/sdr/COMA0260361), Jun 8, 2002: HYDRAULIC LINE. LEAKING. FLIGHT 6657 #1 HYDRAULIC SYSTEM INDICATING ZERO PRESSURE AND ZERO QUANTITY.REPLACED THE HYDRAULIC LINES AT THE LT ENGINE TO PYLON INTERFACE. - [SDR COMA0260358](https://openairdocs.org/sdr/COMA0260358), Jun 6, 2002: SELECTOR VALVE. MALFUNCTIONED. FLIGHT 5882 GEAR DISAGREE WARNING, NLG DID NOT EXTEND - USED MANUAL EXTENSION.REPLACED THE NLG SELECTOR VALVE. - [SDR COMA0260291](https://openairdocs.org/sdr/COMA0260291), Apr 29, 2002: SKIN. CRACKED. CRACK FOUND ON RT LOWER WING PLANK AT PANEL 650GB.REPAIRED IAW 601R-57-21-030. - [SDR COMA0260113](https://openairdocs.org/sdr/COMA0260113), Feb 19, 2002: LANDING GEAR. FLIGHT 5032 NLG DID NOT EXTEND, GEAR DISAGREE WARNING. USED MANUAL EXTENSION SYSTEM.COULD NOT DUPLICATE - INSPECTED NLG AND FOUND NO DEFECTS. - [SDR COMA0160972](https://openairdocs.org/sdr/COMA0160972), Dec 17, 2001: PROXIMITY SWITCH. FLIGHT 5970 - CONFIG OK MESSAGE WENT OUT DURING T/O.REMOVED DIRT FROM NLG PROX SWITCHES. - [SDR COMA0160579](https://openairdocs.org/sdr/COMA0160579), Aug 8, 2001: WEB. CRACKED. CRACKS FOUND ON LEFT HAND AND RIGHT HAND LOWER WEBS OF ENGINE SUPPORT BEAM F.S. 625.30.REPAIRED LEFT HAND AND RIGHT HAND LOWER WEBS OF ENGINE SUPPORT BEAM I/A/W - [SDR COMA0160568](https://openairdocs.org/sdr/COMA0160568), Aug 6, 2001: ANGLE. CORRODED. THE FWD J ANGLE AT F.S. 280 BETWEEN LBL9.0 AND RBL9.0 IS CORRODED.REMOVED AND REPLACED THE FWD J ANGLE AT FS 280 BETWEEN LBL9.0 AND RBL9.0 P/N 600-34017-351 I/A - [SDR COMA0160161](https://openairdocs.org/sdr/COMA0160161), Jan 24, 2001: COMPUTER. MALFUNCTIONED. STALL FAIL CAUTION DURING T/O. RESET THE STALL COMPUTER. - [SDR COMA0160158](https://openairdocs.org/sdr/COMA0160158), Jan 23, 2001: COMPUTER. MALFUNCTIONED. STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. - [SDR COMA0160061](https://openairdocs.org/sdr/COMA0160061), Jan 3, 2001: COMPUTER. MALFUNCTIONED. STALL FAIL CAUTION DURING T/O. RESET THE STALL COMPUTER. - [SDR COMA0160035](https://openairdocs.org/sdr/COMA0160035), Dec 30, 2000: COMPUTER. MALFUNCTIONED. STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. - [SDR COMA0061056](https://openairdocs.org/sdr/COMA0061056), Dec 14, 2000: PUMP. FAILED. Left engine low hydraulic pressure message. Replace the left engine hydraulic pump. - [SDR COMA0061016](https://openairdocs.org/sdr/COMA0061016), Dec 6, 2000: ANGLE. CRACKED. FS 621.00 FLOOR ATTACHMENT ANGLE IS CRACKED ON RIGHT HAND SIDE. PERFORMED A MAJOR REPAIR BY REPLACING CRACKED FLOOR SUPPORT ANGLE AT FS 621.0 RIGHT HAND SIDE IA - [SDR COMA0061009](https://openairdocs.org/sdr/COMA0061009), Dec 6, 2000: FLOORBEAM. CRACKED. F.S. 621.00 FLOOR ATTACH ANGLE IS CRACKED RT SIDE. REMOVE AND REPLACED RT SIDE F.S. 621.00 FLOOR ATTACH ANGLE I/A/W CANADAIR S/B 601R-53-018. - [SDR COMA0061010](https://openairdocs.org/sdr/COMA0061010), Dec 2, 2000: ANGLE. CRACKED. PASSENGER DOOR SEAL STRIKER AT F.S. 349.00 CRACKED. FURTHER INVESTIGATION FOUND PREVIOUS REPAIR AND ONLY SEALANT TO BE CRACKED. REMOVED OLD SEALANT AND REAPPLIE - [SDR COMA0060986](https://openairdocs.org/sdr/COMA0060986), Dec 2, 2000: ANGLE. CRACKED. UNDER FLOOR ANGLES ARE CRACKED AT RBL27 AND LBL27 F.S. 484.0 REMOVED CRACKED ANGLES. FABRICATED NEW ANGLES FROM S6144-4 AND INSTALLED NEW ANGLES IAW WVAC EO 601 - [SDR COMA0060984](https://openairdocs.org/sdr/COMA0060984), Dec 2, 2000: ANGLE. CRACKED. PASSENGER DOOR SEAL STRIKER AT F.S. 349.00 CRACKED. REMOVED OLD SEALANT AND REAPPLIED AERODYNAMIC FILLER EC 1751 B/A IAW REO 601R-52-11-008 REV B PART 4. - [SDR COMA0060794](https://openairdocs.org/sdr/COMA0060794), Oct 1, 2000: CONTROLLER. MALFUNCTIONED. CARGO SMOKE WARNING FIRE BOTTLES DISCHARGED. REPLACED FIRE DETECTION CONTROLLER. - [SDR COMA0060387](https://openairdocs.org/sdr/COMA0060387), Apr 27, 2000: WARNING SYSTEM. ACTIVATED. FLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. - [SDR COMA0060298](https://openairdocs.org/sdr/COMA0060298), Mar 30, 2000: SIGN. INOPERATIVE. EXIT SIGN AT CABIN DOOR IS INOPERABLE. REPLACED EXIT SIGN. - [SDR COMA0060007](https://openairdocs.org/sdr/COMA0060007), Dec 27, 1999: WARNING SYSTEM. ILLUMINATED. LEFT WINDOW HEAT CAUTION MESSAGE. COULD NOT DUPLICATE, OPERATIONAL CHECK OF WINDOW HEAT SATISFACTORY. - [SDR COMA9960727](https://openairdocs.org/sdr/COMA9960727), Nov 27, 1999: FRAME. CRACKED. FS 718.00 LEFT HAND AND RIGHT HAND FRAMES AND AFT DOUBLERS WERE CRACKED STR 10-12. REPAIRED LEFT HAND AND RIGHT HAND FRAMES AND AFT DOUBLER IAW CANADAIR REO 601 - [SDR COMA9960495](https://openairdocs.org/sdr/COMA9960495), Sep 8, 1999: BULB. FAILED. EMERGENCY LIGHT ROW 2 IS INOPERABLE. REPLACED LIGHT BULB. - [SDR COMA9960450](https://openairdocs.org/sdr/COMA9960450), Aug 11, 1999: ACTUATOR. MALFUNCTIONED. FLAPS FAILED AT 8 DEGREES. REPLACED THE RIGHT OUTBOARD FLAP ACTUATORS. - [SDR COMA9960439](https://openairdocs.org/sdr/COMA9960439), Aug 10, 1999: PDU. MALFUNCTION. FLAPS FAIL MESSAGE. REPLACED THE PDU. - [SDR COMA9960420](https://openairdocs.org/sdr/COMA9960420), Aug 8, 1999: FAIL MESSAGE. ACTIVATED. FLAPS FAIL MESSAGE. RESET FLAP SYSTEM IAW AD 98 20 01. - [SDR COMA9960417](https://openairdocs.org/sdr/COMA9960417), Aug 3, 1999: BPSU. OUT OF ADJUST. FLAPS FAIL MESSAGE. C/W RIGGING OF LEFT AND RIGHT BPSU. - [SDR COMA9960333](https://openairdocs.org/sdr/COMA9960333), Jun 29, 1999: PSEU. MALFUNCTIONED. GEAR DISAGREE AND PROX SYSTEM FAULT MESSAGE. REPLACED THE PSEU. - [SDR COMA9960276](https://openairdocs.org/sdr/COMA9960276), Jun 15, 1999: VALVE. MALFUNCTIONED. LOUD SQUEAL FROM NOSE AREA WHEN RIGHT BRAKE APPLIED. REMOVED AND REPLACED NR 2 BRAKE CONTROL VALVE. All 57: https://openairdocs.org/deregistered/N975CA-2008-07-16/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 19990118035499I](https://openairdocs.org/incident/19990118035499I), Jan 18, 1999: Cndair CL6002B19 (N975CA), Philipsburg, PA. (-23) Com 877 was level at FL370 and exercised emergency authority to descend to FL360 when an increase in air temperature made it operationally impossible to… ## Other aircraft with N975CA - [Registered now](https://openairdocs.org/aircraft/N975CA): Socata TBM 700, S/N 544, built 2010 --- 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.