# N960CA: 1996 Canadair CL-600-2B19, registration cancelled 2018-02-12

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 12, 2018
- Status when cancelled: Registration expired, pending cancellation
- 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: 7117
- Year built: 1996
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 24, 1996
- Certificate issued: October 17, 2007
- Last registry action: January 30, 2015
- Mode S code: AD5C59
- 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/N960CA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=960CA
- Page: https://openairdocs.org/deregistered/N960CA-2018-02-12

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 (96, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR COMA2010100450214](https://openairdocs.org/sdr/COMA2010100450214), Sep 30, 2010: HYDRAULIC LINE. LEAKING. ON DESCENT INTO DCA RECEIVED HYD 2 LOW PRESS CAUTION MSG, 0 FLUID AND 0 PSI ON EICAS. EMERGENCY DECLARED, A/C DIVERTED TO BWI LANDED SAFELY. REMOVED AND REPLACE
- [SDR COMA2010092050206](https://openairdocs.org/sdr/COMA2010092050206), Sep 17, 2010: ENGINE. OVERTEMP. ON CLIMBOUT FROM BDL TO CVG LEFT ENGINE EXCEEDED ITT LIMITS, REDUCED THRUST TO 85 PERCENT TO MAINTAIN WITH IN LIMITS. EMERGENCY DECLARED, A/C DIVERTED TO ALB LA
- [SDR COMA2010091750204](https://openairdocs.org/sdr/COMA2010091750204), Sep 16, 2010: SENSING ELEMENT. FAILED. EN ROUTE FROM CMH TO MSP RECEIVED LEFT 14TH STAGE DUCT WARNING MSG. EMERGENCY DECLARED, A/C DIVERTED TO DAY LANDED SAFELY. REMOVED AND REPLACED LEFT PYLON 14TH 
- [SDR COMA2009060850152](https://openairdocs.org/sdr/COMA2009060850152), Jun 6, 2009: CONTROL HANDLE. FAILED. ON FINAL RECEIVED FLAPS FAIL CAUTION MSG. EMERGENCY DECLARED, ACFT LANDED SAFELY. REMOVED AND REPLACED FLAP CONTROL HANDLE.
- [SDR COMA2009050750131](https://openairdocs.org/sdr/COMA2009050750131), May 5, 2009: BLEED VALVE. FAILED. EN ROUTE FROM JFK TO CLE LEFT 10TH STAGE BLEED VALVE FAILED TO OPEN. EMERGENCY DECLARED, A/C LANDED SAFELY AT CLE. REMOVED AND REPLACED LEFT 10TH STAGE BLEED VA
- [SDR COMA2008120150020](https://openairdocs.org/sdr/COMA2008120150020), Dec 1, 2008: SKIN PANEL. DAMAGED. COMPLIED WITH MODIFICATION K601R36009-3 ON LT FS 640.00 FRAME AND DOUBLER PER S/B601R-53-061 KIT DRWG K601R36009 REV B, 601R-53-61-506 REV C AND 601R53-61-569. 
- [SDR COMA0860395](https://openairdocs.org/sdr/COMA0860395), Sep 18, 2008: WIRE HARNESS. BROKEN. ON CLIMBOUT FROM CVG RECEIVED PAX DOOR OUTER HANDLE MSG. A/C RETURNED BACK TO CVG AND LANDED SAFELY. R&R PAX DOOR WIRE HARNESS. OPS CHECK GOOD.
- [SDR COMA086345](https://openairdocs.org/sdr/COMA086345), Aug 11, 2008: FLUX DETECTOR. FAILED. EFIS COMP MON MSG, FIRST OFFICER`S HEADING DIFFICULT TO RIGHT. ACFT RETURNED BACK TO CVG, LANDED SAFELY. REMOVED AND REPLACED NR 2 FLUX DETECTOR. (S)
- [SDR COMA0860297](https://openairdocs.org/sdr/COMA0860297), Jun 22, 2008: FLOORBEAM. CRACKED. DURING HMV NR 6 INSPECTION, NDT INSPECTION FOUND A CRACK ON THE FS 559 LBL 18, LOWER CAP ANGLE. CUT OUT DAMAGE SECTION OF CAP ANGLE AND SPLICED IN NEW SECTION W
- [SDR COMA0860293](https://openairdocs.org/sdr/COMA0860293), Jun 17, 2008: BULKHEAD. CRACKED. CRACK ON REAR PRESSURE BULKHEAD AT LBL 36.20 WL 80. REPAIRED REAR PRESSURE BULKHEAD IAW REO 601R-53-61-1285. (S)
- [SDR COMA0860292](https://openairdocs.org/sdr/COMA0860292), Jun 16, 2008: POST. CRACKED. DURING HMV-6, EDDY CURRENT INSPECTION FOUND CRACK ON LOWER POST, FS 409+128, LBL 18, OUTBOARD SIDE. CUT OUT DAMAGE AND INSTALLED A DOUBLER IN ACCORDANCE WITH RE
- [SDR COMA0860291](https://openairdocs.org/sdr/COMA0860291), Jun 16, 2008: STRINGER CLIP. CRACKED. DURING HMV-6, INSPECTION FOUND FRAME 625 TO STRINGER 15L ATTACH CLIP CRACKED. REMOVED AND REPLACED CLIP IN ACCORDANCE WITH SRM 51-42-20. (S)
- [SDR COMA0860288](https://openairdocs.org/sdr/COMA0860288), Jun 15, 2008: BULKHEAD. CRACKED. REAR PRESSURE BULKHEAD CRACKED AT THE TOP OF LINTEL FITTING. REPAIRED REAR PRESSURE BULKHEAD AROUND LINTEL FITTING IAW REO 601R-53-61-1230. (S)
- [SDR COMA0860281](https://openairdocs.org/sdr/COMA0860281), Jun 11, 2008: FRAME. CRACKED. DURING HMV-6, INSPECTION FOUND FLANGE OF FS 640 FRAME CRACKED BETWEEN STRINGERS 13R AND 14R. DAMAGED PORTION OF FLANGE CUT OUT AND REPAIR DOUBLER INSTALLED PER 
- [SDR COMA0860283](https://openairdocs.org/sdr/COMA0860283), Jun 10, 2008: FRAME. CRACKED. LT FUSELAGE FRAME CRACKED AT FS 640 BETWEEN STRINGERS 9 & 10. PERFORMED MODIFICATION K601R36009-3 AS PER PART C OF SB 601R-53-061E. (S)
- [SDR COMA0860282](https://openairdocs.org/sdr/COMA0860282), Jun 10, 2008: STIFFENER. CRACKED. DURING HMV-6, EDDY CURRENT INSPECTION FOUND VERTICAL WEB STIFFENER CRACKED ON FWD SIDE OF FS 280, RBL 12, AT AND ABOVE CABIN FLOOR LINE. REMOVED AND REPLACED DA
- [SDR COMA0860280](https://openairdocs.org/sdr/COMA0860280), Jun 10, 2008: BULKHEAD. CRACKED. CRACK ON REAR PRESSURE BULKHEAD ABOVE CARGO DOOR TRACK. REPAIRED REAR PRESSURE BULKHEAD IAW REO 601R-53-61-1541. (S)
- [SDR COMA0860274](https://openairdocs.org/sdr/COMA0860274), Jun 8, 2008: DOUBLER. CRACKED. RT FS 718.00 FRAME DOUBLER CRACKED ON THE AFT SIDE AT STRINGERS 10 AND 11. REMOVED AND REPLACED FRAME DOUBLER IAW BOMBARDIER REO 601R-53-61-243. (S)
- [SDR COMA0860273](https://openairdocs.org/sdr/COMA0860273), Jun 8, 2008: BULKHEAD. CRACKED. FORWARD PRESSURE BULKHEAD CRACKED AT PARKING BRAKE CABLE AT FS 202.75. REPAIRED FORWARD PRESSURE BULKHEAD AT FS 202.75 IAW CRJ REO 601R-53-11-563. (S)
- [SDR COMA0860272](https://openairdocs.org/sdr/COMA0860272), Jun 8, 2008: PAN. CRACKED. FLOOR BELOW TRUSS CRACKED ON LT SIDE BELOW ACCUMULATOR GAUGE AT FS 193.00. REPAIRED FLOOR IAW REO 601R-53-11-081. (S)
- [SDR COMA0860271](https://openairdocs.org/sdr/COMA0860271), Jun 8, 2008: FLOORBEAM. CRACKED. FS 280 FLOORBEAM (GALLEY SIDE) CRACKED. REPAIRED FS 280 FLOORBEAM IAW REO 601R-53-11-136. (S)
- [SDR COMA0860159](https://openairdocs.org/sdr/COMA0860159), Mar 5, 2008: BRACKET. BENT. FLIGHT 5458 - RECEIVED GEAR DISAGREE MESSAGE AND NOSE DOOR WARNING. NOSE GEAR DID NOT INDICATE UP. COMPLIED WITH QRH. RETURNED TO ATL, LANDED WITHOUT INCIDENT. 
- [SDR COMA0760656](https://openairdocs.org/sdr/COMA0760656), Nov 20, 2007: ANTI-ICE SYSTEM. MALFUNCTIONED. FLIGHT 5181 - DURING TAKEOFF ROLL RECEIVED A WING OVERHEAT WARNING MESSAGE, ABORTED T/O AND RETURNED TO THE GATE. DEFERRED WING ANTI-ICE SYSTEM PER MEL 30-12-03
- [SDR COMA0760434](https://openairdocs.org/sdr/COMA0760434), Jun 13, 2007: NONE. NONE. TEMPORARY REPAIR INCORPORATED FOR LEFT LOWER WING PLANK CRACK AT WS 148.019 IAW REO 601R-57-21-138. COMPLIED WITH PERMANENT REPAIR OF THE LEFT LOWER WING PLANK 
- [SDR COMA0760433](https://openairdocs.org/sdr/COMA0760433), Jun 13, 2007: NONE. NONE. TEMPORARY REPAIR INCORPORATED FOR RIGHT LOWER WING PLANK CRACK AT WS 148.019 IAW REO 601R-57-21-138. COMPLIED WITH PERMANENT REPAIR OF THE RIGHT LOWER WING PLAN
- [SDR COMA0760344](https://openairdocs.org/sdr/COMA0760344), Apr 28, 2007: PRESSURE SWITCH. FAULTY. FLIGHT 5637 - RIGHT ENGINE OIL PRESSURE WARNING DURING CLIMBOUT, AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED RIGHT ENGINE OIL PRESSURE
- [SDR COMA0760061](https://openairdocs.org/sdr/COMA0760061), Jan 25, 2007: TRIM SWITCH. FAULTY. FLIGHT 5078 - DURING CLIMBOUT CAPTAIN SIDE STAB TRIM WOULD NOT MOVE IN THE DOWN POSITION. AIRCRAFT RETURNED BACK TO BOS AND LANDED SAFELY. REMOVED AND REPLACED 
- [SDR COMA0660662](https://openairdocs.org/sdr/COMA0660662), Nov 27, 2006: WARNING SYSTEM. MALFUNCTIONED. FLIGHT 5056 - DURING CLIMBOUT OF BNA RECEIVED A CABIN DOOR OUTER HANDLE MESSAGE, FLIGHT RETURNED TO BNA. PERFORMED AN OPERATIONAL CHECK OF THE CABIN DOOR OUTER 
- [SDR COMA0660534](https://openairdocs.org/sdr/COMA0660534), Sep 8, 2006: WINDOW. CRACKED. FLIGHT 5674 - DURING CRUISE FLIGHT, THE LEFT SIDE COCKPIT WINDOW CRACKED. REPLACED THE LEFT COCKPIT SIDE WINDOW.
- [SDR COMA0660485](https://openairdocs.org/sdr/COMA0660485), Aug 11, 2006: CONTROL HANDLE. FAULTY. FLIGHT 9482 - DURING APPROACH, FLAPS FAILED AT 30 DEGREES. CREW LANDED WITHOUT INCIDENT. REPLACED FLAP CONTROL HANDLE.
- [SDR COMA0660296](https://openairdocs.org/sdr/COMA0660296), Apr 10, 2006: WINDSHIELD. FAILED. FLIGHT 5301 - CAPTAIN'S WINDSHIELD SHATTERED. REMOVED AND REPLACED CAPTAIN'S WINDSHIELD.
- [SDR COMA0560483](https://openairdocs.org/sdr/COMA0560483), Sep 2, 2005: RESERVOIR. MALFUNCTIONED. FLIGHT 5064 - GEAR DISAGREE WARNING. REPLACED THE NR 3 HYDRAULIC RESERVOIR.
- [SDR COMA0560385](https://openairdocs.org/sdr/COMA0560385), Jul 9, 2005: SELECTOR VALVE. MALFUNCTIONED. FLIGHT 5521 - GEAR DISAGREE WARNING. REPLACED THE MLG SELECTOR VALVE.
- [SDR COMA0560023](https://openairdocs.org/sdr/COMA0560023), Jan 2, 2005: WARNING SYSTEM. MALFUNCTIONED. FLIGHT 5164, LEFT AND RIGHT AOA HEAT CAUTION. RESET SYSTEM. COULD NOT DUPLICATE.
- [SDR COMA0460385](https://openairdocs.org/sdr/COMA0460385), Jun 19, 2004: BATTERY. MALFUNCTIONED. FLIGHT 5721 DURING CRUISE FLIGHT APU BATTERY INDICATED 99 AMPS, AIRCRAFT DIVERTED TO CLE. DEFERRED THE APU BATTERY PER MEL 24-32-03.
- [SDR COMA0460341](https://openairdocs.org/sdr/COMA0460341), May 27, 2004: WARNING LIGHT. ILLUMINATED. FLIGHT 5399 LEFT THRUST REVERSER UNLOCKED CAUTION MESSAGE. DEFERRED MAINT ON T/R PER MEL.
- [SDR COMA0460217](https://openairdocs.org/sdr/COMA0460217), Mar 20, 2004: OXYGEN MASK. ACTIVATED. FLIGHT 5118 02 MASK AT ROW 9 DROPPED DURING T/O. RESTOWED 02 MASKS AT ROW 9.
- [SDR COMA0360164](https://openairdocs.org/sdr/COMA0360164), Mar 21, 2003: PROXIMITY SENSOR. OUT OF ADJUST. FLIGHT 9492 AVIONICS DOOR CAUTION MESSAGE AT 8000 FT. ADJUSTED THE AVIONICS DOOR PROXIMITY SENSOR.
- [SDR COMA0360147](https://openairdocs.org/sdr/COMA0360147), Mar 15, 2003: PUMP. MALFUNCTIONED. FLIGHT 5510 GEAR DISAGREE WHEN GEAR SELECTED DOWN.REPLACED THE #3A ACMP
- [SDR COMA0260426](https://openairdocs.org/sdr/COMA0260426), Jul 15, 2002: COWLING. CRACKED. RIGHT ENGINE FIXED CORE COWL IS CRACKED IN AFT CHANNEL APPROX 1/5 INCH. REPAIRED CRACK BY STOP DRILLING AND INSTALLING A DOUBLER IAW SHORTS CMM 71-13-01 REPAIR 
- [SDR COMA0260425](https://openairdocs.org/sdr/COMA0260425), Jul 15, 2002: BUSHING. DAMAGED. THE RIGHT VERTICAL STABILIZER HINGE BUSHING WAS DAMAGED AND REQUIRES REPLACEMENT. REMOVED AND REPLACED BUSHING IAW WVAC EO 601R-55-3359 CRJ AMM 20-26-00-910-803
- [SDR COMA0260414](https://openairdocs.org/sdr/COMA0260414), Jul 5, 2002: FLAP. FLAPS FAILED MESSAGE AFTER LANDING.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
- [SDR COMA0260192](https://openairdocs.org/sdr/COMA0260192), Mar 14, 2002: COMPUTER. MALFUNCTIONED. FLIGHT 5860 MACH TRIM/STAB TRIM CAUTION MESSAGE.REPLACED THE HSTCU.
- [SDR COMA0260063](https://openairdocs.org/sdr/COMA0260063), Jan 24, 2002: SPRING. STUCK. FLIGHT 5602 AVIONICS BAY DOOR WARNING DURING T/O.FOUND AVIONICS DOOR SWITCH JAMMED. REPLACED SWITCH SPRING.
- [SDR COMA0260044](https://openairdocs.org/sdr/COMA0260044), Jan 13, 2002: FLAP. FLIGHT 5553 FLAPS FAILED AT 30 DEGREES DURING APPROACH.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01.
- [SDR COMA0260048](https://openairdocs.org/sdr/COMA0260048), Jan 11, 2002: COMPUTER. FLIGHT 5285 CONFIG AILERONS AND CONFIG TRIM AURAL WARNING DURING T/O.COULD NOT DUPLICATE. TEST OF AILERON TRIM SYSTEM WAS NORMAL.
- [SDR COMA0260003](https://openairdocs.org/sdr/COMA0260003), Dec 24, 2001: PLANK. CRACKED. EDDY CURRENT INDICATES CRACKS.BLENDED OUT DAMAGE AND ROTO-PEENED I/A/W REO 601R-57-21-030.
- [SDR COMA0260005](https://openairdocs.org/sdr/COMA0260005), Dec 22, 2001: BEAM. CRACKED. ENGINE SUPPORT BEAM CRACKED.REPAIRED DAMAGE I/A/W REO601R-53-61-345.
- [SDR COMA0260001](https://openairdocs.org/sdr/COMA0260001), Dec 22, 2001: BEAM. CRACKED. ENGINE SUPPORT BEAM CRACKED.REPAIRED DAMAGE I/A/W REO 601R-53-61-366.
- [SDR COMA0160853](https://openairdocs.org/sdr/COMA0160853), Oct 24, 2001: SWITCH. FAULTY. FLIGHT #5570. DURING TEST OF THE YAW DAMPER SYSTEM THE #2 WOULD NOT ENGAGE.REPLACED THE YAW DAMPER SWITCH.

All 96: https://openairdocs.org/deregistered/N960CA-2018-02-12/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB FTW02IA097](https://openairdocs.org/ntsb/FTW02IA097), Mar 14, 2002: Canadair CL-600-2B19 (N960CA), Tulsa, OK, incident, no damage. Probable cause: The failure of the horizontal stabilizer control system for undetermined reasons.

## 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 20100917046279I](https://openairdocs.org/incident/20100917046279I), Sep 17, 2010: Canadair CL-600-2B19 (N960CA), NY, No damage. On climb out from bradley, CT, itt on #1 engine exceeded limitations. Reduced thrust and diverted to Albany , NY and landed on runway 1. ARFF responded,…

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