# N964CA: 1996 Canadair CL-600-2B19, registration cancelled 2020-12-05

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 5, 2020
- 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: 7129
- Year built: 1996
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 15, 1996
- Certificate issued: August 8, 2014
- Last registry action: December 3, 2018
- Mode S code: AD6B35
- Owner when cancelled: [Golden Mile Aircraft Leasing Inc](https://openairdocs.org/faa-owner/GOLDEN%20MILE%20AIRCRAFT%20LEASING%20INC)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7236° N, 75.5412° W: Placed by OpenAirDocs at the center of ZIP code 19801, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N964CA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=964CA
- Page: https://openairdocs.org/deregistered/N964CA-2020-12-05

From the FAA registry file of November 7, 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 (93, newest 50)

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

- [SDR COMA2012031950015](https://openairdocs.org/sdr/COMA2012031950015), Mar 16, 2012: PUMP. FAILED. ON CLIMBOUT FROM DTW RECEIVED GEAR DISAGREE MSG WHEN GEAR WAS SELECTED UP. EMERGENCY DECLARED, A/C RETURNED TO DTW LANDED SAFELY. REMOVED AND REPLACED ACMP 3B. 
- [SDR COMA2011102850088](https://openairdocs.org/sdr/COMA2011102850088), Oct 27, 2011: WARNING SYSTEM. ACTIVATED. EN ROUTE FROM DTW TO MSN RECEIVED RT THRUST REV UNLOCKED CAUTION MSG, FOLLOWED QRH. EMERGENCY DECLARED, A/C DIVERTED TO LAN LANDED SAFELY. TRANSFERRED TO DEFERR
- [SDR COMA2011102450083](https://openairdocs.org/sdr/COMA2011102450083), Oct 21, 2011: WARNING SYSTEM. ACTIVATED. EN ROUTE FROM DTW TO RIC AT 31000FT RECEIVED RT THRUST REV UNLOCK CAUTION MSG. FOLLOWED QRH PROCEDURES, EMERGENCY DECLARED. A/C DIVERTED TO IAD, LANDED SAFELY. 
- [SDR COMA2010091350195](https://openairdocs.org/sdr/COMA2010091350195), Sep 10, 2010: WIRE HARNESS. FAILED. ON T/O FROM CVG RECEIVED ANTISKID I/B CAUTION MSG. EMERGENCY DECLARED, A/C DIVERTED BACK TO CVG LANDED SAFELY. REMOVED AND REPLACED RIGHT MLG I/B HARNESS SUB AS
- [SDR COMA2010083050186](https://openairdocs.org/sdr/COMA2010083050186), Aug 29, 2010: FLOOR SKIN. CRACKED. PRESSURE FLOOR SKIN IS CRACKED AT FS 461.00 BETWEEN LBL 9 AND RBL 9. CUT OUT DAMAGED AREA AND INSTALLED TEMPORARY REPAIR DOUBLER IAW REO 601R-53-41-103, REV A.
- [SDR COMA2010082650185](https://openairdocs.org/sdr/COMA2010082650185), Aug 26, 2010: POST. CRACKED. FOUND FS 409+128 LOWER BULKHEAD OUTBOARD RBL 18 POST CRACKED AT LOWER RADIUS. REPAIRED FS 409+128 RBL 18 POST ON OUTBOARD LOWER PART OF BULKHEAD IAW BOMBARDIER 
- [SDR COMA2010082650183](https://openairdocs.org/sdr/COMA2010082650183), Aug 26, 2010: ANGLE. CRACKED. FOUND FS 409 INBOARD ANGLE AT LBL 27 CRACKED. REPAIRED IAW REO601R-53-41-056.
- [SDR COMA2010082550184](https://openairdocs.org/sdr/COMA2010082550184), Aug 25, 2010: ANGLE. CRACKED. FOUND CAP ANGLE CRACKED AT FS 559.00, LBL 18.00. COMPLIED WITH REPAIR TO PRESSURE BULKHEAD STRUCTURE FS 559.00 23L-23R IAW REO 601R-53-41-260 AND DEVIATION REO 
- [SDR COMA2010082550182](https://openairdocs.org/sdr/COMA2010082550182), Aug 25, 2010: ANGLE. CRACKED. FOUND CAP ANGLE CRACKED IN RADIUS AT FS 559.00, RBL 18.00. COMPLIED WITH REPAIR TO PRESSURE BULKHEAD STRUCTURE FS 559.00 23L-23R IAW REO 601R-53-41-260 AND DEVI
- [SDR COMA2010082450181](https://openairdocs.org/sdr/COMA2010082450181), Aug 23, 2010: BULKHEAD. CRACKED. BULKHEAD WEB CRACKED ABOVE CARGO DOOR TRACK, AT FS 621, LBL 27.50, WL 130. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1541, REV B.
- [SDR COMA2010082450180](https://openairdocs.org/sdr/COMA2010082450180), Aug 23, 2010: BULKHEAD. CRACKED. BULKHEAD WEB CRACKED AROUND LINTEL ATTACH FITTING AT FS 621, LBL 36.2. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1230 REV D.
- [SDR COMA2009050450126](https://openairdocs.org/sdr/COMA2009050450126), May 4, 2009: WARNING SYSTEM. MALFUNCTIONED. ON CLIMBOUT FROM JFK RECEIVED ANTI-ICE DUCT WARNING MSG. EMERGENCY DECLARED, A/C RETURNED TO JFK LANDED SAFELY. PERFORMED OPS CHECK OF ANTI-ICE SYSTEM, NO DEFEC
- [SDR COMA2009012050064](https://openairdocs.org/sdr/COMA2009012050064), Jan 14, 2009: OIL COOLER. LEAKING. EN ROUTE FROM BHM TO LGA RECEIVED APU OIL PRESSURE MSG. A/C DIVERTED TO TRI, LANDED SAFELY. FOUND APU OIL COOLER LEAKING. R&R APU OIL COOLER.
- [SDR COMA086358](https://openairdocs.org/sdr/COMA086358), Aug 17, 2008: FLOORBEAM. CORRODED. FOUND CORROSION ON UNDER FLOOR FRAME AT FS 280 BETWEEN LBL 9.00 AD RBL 9.00. REMOVED AND REPLACED FLOOR SUPPORT IAW CRJ SRM 51-42-06. (S)
- [SDR COMA0860071](https://openairdocs.org/sdr/COMA0860071), Jan 16, 2008: ENGINE. FAILED. FLIGHT 5341 - EN ROUTE FROM MKE TO CVG SEVERE ENGINE NOISE AND SHUDDER ON LEFT ENGINE. PERFORMED IFSD. EMERGENCY DECLARED AND AIRCRAFT DIVERTED TO ORD AND LANDE
- [SDR COMA0760736](https://openairdocs.org/sdr/COMA0760736), Dec 19, 2007: HYDRAULIC LINE. DEFECTIVE. FLIGHT 5483 - RECEIVED HYD 2 LOW PRESSURE CAUTION MESSAGE, FOLLOWED BY ED2 CAUTION. ALL NR 2 FLUID LOST. LANDED IAD WITHOUT INCIDENT. REPLACED RIGHT ENGINE HYDR
- [SDR COMA0760396](https://openairdocs.org/sdr/COMA0760396), May 24, 2007: STIFFENER. CRACKED. DURING FS 559 INSPECTION FOUND CRACKS AT LOWER END OF VERTICAL BOX STIFFENER, FS 559 RBL 9 INBOARD AND OUTBOARD SIDE. CUT OUT DAMAGE AND INSTALLED DOUBLERS IAW 
- [SDR COMA0760395](https://openairdocs.org/sdr/COMA0760395), May 24, 2007: STIFFENER. CRACKED. DURING FS 559 INSPECTION FOUND CRACKS AT BASE OF VERTICAL BOX STIFFENER, FS 559, LBL 0 INBOARD AND OUTBOARD SIDE. CUT OUT DAMAGE AND INSTALLED DOUBLERS IAW REO 
- [SDR COMA0760008](https://openairdocs.org/sdr/COMA0760008), Jan 5, 2007: DUCT. FAILED. FLIGHT 4935 - AT CRUISE RECEIVED CABIN ALT WARNING MESSAGE. AIRCRAFT DIVERTED TO IND AND LANDED SAFELY. FOUND LEFT PACK ACM COMPRESSOR OUTLET DUCT DISCONNECTED,
- [SDR COMA0660632](https://openairdocs.org/sdr/COMA0660632), Nov 14, 2006: TRANSDUCER. FAULTY. FLIGHT 5576 - DURING CLIMBOUT OF CVG THE LEFT ENGINE OIL PRESSURE FLUCTUATED BETWEEN 64 AND 79 PSI. REPLACED THE OIL PRESSURE TRANSDUCER.
- [SDR COMA0660387](https://openairdocs.org/sdr/COMA0660387), Jun 9, 2006: PRIORITY VALVE. FAULTY. FLIGHT 5141- DURING CVG APPROACH WHEN GEAR WAS SELECTED DOWN, RECEIVED A DISAGREE MESSAGE, NOSE GEAR DID NOT EXTEND. CYCLED LANDING GEAR AND MESSAGE CLEARED. RE
- [SDR COMA0660386](https://openairdocs.org/sdr/COMA0660386), Jun 9, 2006: SELECTOR VALVE. FAULTY. FLIGHT 5141 - DURING CVG APPROACH WHEN GEAR WAS SELECTED DOWN, RECEIVED A DISAGREE MESSAGE, NOSE GEAR DID NOT EXTEND. CYCLED LANDING GEAR AND MESSAGE CLEARED. R
- [SDR COMA0560479](https://openairdocs.org/sdr/COMA0560479), Sep 1, 2005: FLAP SYSTEM. MALFUNCTIONED. FLIGHT 5874 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
- [SDR COMA0460249](https://openairdocs.org/sdr/COMA0460249), Mar 25, 2004: FRAME. CRACKED. RIGHT HAND 718.00 FRAME HAS CRACK IN RADIUS OF ATTACH FLANGE AT TOP OF STRINGER 11R. REPAIRED IN ACCORDANCE WITH REO 601R-53-61.969.
- [SDR COMA0460122](https://openairdocs.org/sdr/COMA0460122), Feb 3, 2004: SELECTOR VALVE. MALFUNCTIONED. FLIGHT 5351 NOSE DOOR OPEN WARNING DURING GEAR RETRACTION. REPLACED THE NLG DOOR SELECTOR VALVE.
- [SDR COMA0460065](https://openairdocs.org/sdr/COMA0460065), Jan 18, 2004: WARNING LIGHT. ILLUMINATED. FLIGHT 5339 LEFT THRUST REVERSER UNLOCK CAUTION DURING T/O. SECURED THRUST REVERSER AND DEFERRED MAINT PER MEL.
- [SDR COMA0360477](https://openairdocs.org/sdr/COMA0360477), Nov 3, 2003: DOUBLER. DENTED. PREVIOUS REPAIR OF FUSELAGE SKIN LHS FS 310.00 BETWEEN STR 16-17 HAS SUSTAINED FURTHER DAMAGE DUE TO CONTACT WITH DOOR PINS. PERFORMED A MAJOR REPAIR BY REMOVIN
- [SDR COMA0360469](https://openairdocs.org/sdr/COMA0360469), Oct 24, 2003: WINDOW. CRACKED. FLIGHT 5441 CO-PILOT SIDE WINDSHIELD SHATTERED. REPLACED SIDE WINDOW.
- [SDR COMA0360212](https://openairdocs.org/sdr/COMA0360212), Apr 22, 2003: STRUT. FLAT. FLIGHT 5758 LANDING GEAR DISAGREE WARNING, NOSE LANDING GEAR DID NOT RETRACT. REPLACED THE NOSE LANDING GEAR STRUT PISTON ASSEMBLY.
- [SDR COMA0360202](https://openairdocs.org/sdr/COMA0360202), Apr 16, 2003: WARNING LIGHT. ILLUMINATED. FLIGHT 5715 RT THRUST REVERSER UNLOCK CAUTION MESSAGE. SECURED T/R AND DEFERRED MAINT PER MEL.
- [SDR COMA0360015](https://openairdocs.org/sdr/COMA0360015), Jan 8, 2003: COALESCER BAG. FLIGHT 5716 TOILET SMOKE WARNING.CLEANED COALESCER SOCKS AND RAN SYSTEM TO CLEAR OIL FUMES FROM PREVIOUS APU FAILURE.
- [SDR COMA0260663](https://openairdocs.org/sdr/COMA0260663), Nov 23, 2002: THROTTLE CONTROL. MALFUNCTIONED. FLIGHT 5273 R/H THRUST REVERSER UNLOCKED MESSAGE.REPLACED THE THROTTLE GEAR BOX.
- [SDR COMA0260610](https://openairdocs.org/sdr/COMA0260610), Oct 25, 2002: APU. SMOKE. FLIGHT 5426 SMOKE TOILET CAUTION MESSAGE.REPLACED THE APU.
- [SDR COMA0260581](https://openairdocs.org/sdr/COMA0260581), Oct 14, 2002: ELEMENT. DEFECTIVE. FLIGHT 5071 - MLG BAY OVERHEAT WARNING.REPLACED OVERHEAT SENSING ELEMENT R/H WHEEL WELL.
- [SDR COMA0260510](https://openairdocs.org/sdr/COMA0260510), Sep 3, 2002: ELEMENT. MALFUNCTIONED. FLIGHT 5983 L/H 14TH STAGE BLEED AIR DUCT WARNING. IFSD.REPLACED THE BLEED AIR LEAK SENSOR ELEMENT IN L/H ENGINE PYLON.
- [SDR COMA0260385](https://openairdocs.org/sdr/COMA0260385), Jun 23, 2002: LANDING GEAR. FLIGHT 5858 GEAR DISAGREE WARNING DURING EXTENSION.COULD NOT DUPLICATE GEAR EXTENSION AND RETRACTION CHECKS WERE NORMAL.
- [SDR COMA0260351](https://openairdocs.org/sdr/COMA0260351), Jun 2, 2002: THERMOCOUPLE. FAULTY. FLIGHT 5640 LT ENG ITT HOT WARNING - ITT FLUCTUATED FROM NORMAL TO OVER 900 DEGREES.REPLACED THE LOW PRESSURE TURBINE ASSY DUE TO DEFECTIVE THERMOCOUPLE ASSY.
- [SDR COMA0260227](https://openairdocs.org/sdr/COMA0260227), Apr 2, 2002: STRAP. CORRODED. TWO FLOOR SUPPORT STRAPS CORRODED TO THE POINT THAT REPLACEMENT IS REQUIRED.REPAIRED I/A/W REO 601R-53-41-080.
- [SDR COMA0260226](https://openairdocs.org/sdr/COMA0260226), Apr 2, 2002: ANGLE. CORRODED. 65 FASTENERS REMOVED FROM LT AND RT FLOOR SUPPORT ANGLES BETWEEN FS 409.0+128 AND FS559.0.REPAIRED I/A/W REO 601R-53-41-081.
- [SDR COMA0260225](https://openairdocs.org/sdr/COMA0260225), Apr 2, 2002: ANGLE. CORRODED. AREAS OF CORROSION NOTED ON LT AND RT FLOOR SUPPORT ANGLES BETWEEN FS 409.0+128 AND FS 559.0. REPAIRED IAW REO 601R-53-41-079.
- [SDR COMA0260224](https://openairdocs.org/sdr/COMA0260224), Apr 2, 2002: PLANK. CRACKED. CRACK FOUND ON RT LOWER WING PLANK AT PANEL 610AB.REPAIRED I/A/W 601R-57-21-030.
- [SDR COMA0260223](https://openairdocs.org/sdr/COMA0260223), Apr 2, 2002: PLANK. CRACKED. CRACK FOUND ON RT LOWER WING PLANK AT PANEL 640DB.REPAIRED I/A/W 601R-57-21-030.
- [SDR COMA0260222](https://openairdocs.org/sdr/COMA0260222), Apr 2, 2002: PLANK. CRACKED. CRACK FOUND ON LT LOWER WING PLANK AT PANEL 550BB.REPAIRED I/A/W 601R-57-21-030.
- [SDR COMA0260221](https://openairdocs.org/sdr/COMA0260221), Apr 2, 2002: PLANK. CRACKED. CRACK FOUND ON LT LOWER WING PLANK AT PANEL 550GB.REPAIRED I/A/W 601R-57-21-030.
- [SDR COMA0260053](https://openairdocs.org/sdr/COMA0260053), Jan 15, 2002: CHARGER. INOPERATIVE. FLIGHT 5492 MAIN BATTERY CHARGER MESSAGE.REPLACED BATTERY CHARGER.
- [SDR COMA0160952](https://openairdocs.org/sdr/COMA0160952), Dec 9, 2001: FITTING. CORRODED. DURING REMOVAL OF THE RIGHT ENGINE ASSEMBLY, DISCOVERED PITTING CORROSION ON THE AFT ENGINE PYLON THRUST FITTING MOUNTING RIB. REPAIRED IAW REO 601R-54-50-040.
- [SDR COMA0160805](https://openairdocs.org/sdr/COMA0160805), Oct 12, 2001: WIRE. FAULTY. FLIGHT 5354, FLOOR PATCH EMERGENCY LIGHTING, ROWS 2 THROUGH 5, ARE INOPERATIVE. REPLACED POWER WIRES FOR INOP SECTION OF LIGHTING.
- [SDR COMA0160620](https://openairdocs.org/sdr/COMA0160620), Aug 18, 2001: WEB. CRACKED. R/H AND L/H SIDES OF THE ENGINE SUPPORT BEAM ASSY ARE CRACKED ON THE LOWER WEB.REPAIRED R/H AND L/H OUTBD LOWER ENGINE SUPPORT BEAM WEB I/A/W CANADAIR REO 601R-
- [SDR COMA0160621](https://openairdocs.org/sdr/COMA0160621), Aug 17, 2001: WEB. CRACKED. UPPER CENTER ENGINE SUPPORT BEAM HAS 1/2 CRACK (CENTER AFT).PERFORMED A TEMPORARY REPAIR I/A/W CANADAIR REO 601R-53-61-345 REV B.
- [SDR COMA0160584](https://openairdocs.org/sdr/COMA0160584), Aug 13, 2001: ANGLE. CORRODED. THE FWD J-ANGLE AT FS280 BETWEEN LBL9.0 AND RBL 9.0 IS CORRODED.REPLACED FWD J-ANGLE AT FS280.0 BETWEEN LBL9.0 AND RBL9.0 I/A/W WVAC EO 601R-53-2641.

All 93: https://openairdocs.org/deregistered/N964CA-2020-12-05/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 20001130043999I](https://openairdocs.org/incident/20001130043999I), Nov 30, 2000: Cndair CL6002B19 (N964CA), Greensboro, NC. (-23) During push back PIC aborted initial start on the #2 engine. Attempted restart of the #2 engine when ground crew noticed excessive smoke from the engine.…

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