# N959CA: 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: 7116
- Year built: 1996
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 24, 1996
- Certificate issued: August 8, 2014
- Last registry action: March 17, 2017
- Mode S code: AD5649
- 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/N959CA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=959CA
- Page: https://openairdocs.org/deregistered/N959CA-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 (118, newest 50)

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

- [SDR COMA2012062750049](https://openairdocs.org/sdr/COMA2012062750049), Jun 21, 2012: SKIN. CRACKED. LEFT AFT NOSE WHEEL WELL CUTOUT CRACKED AT FS 235.00. REPAIRED BY REMOVING DAMAGE AND INSTALLING DOUBLER IAW REO 601R-53-11-010.
- [SDR COMA2012062750048](https://openairdocs.org/sdr/COMA2012062750048), Jun 21, 2012: SKIN. CRACKED. RIGHT AFT NOSE WHEEL WELL CUTOUT CRACKED AT FS 235.00. REPAIRED BY REMOVING DAMAGE AND INSTALLING DOUBLER IAW REO 601R-53-11-010.
- [SDR COMA2010062250132](https://openairdocs.org/sdr/COMA2010062250132), Jun 20, 2010: PIVOT ASSY. MALFUNCTIONED. ON CLIMBOUT FROM CVG RECEIVED PAX DOOR WARNING MSG AND OVERBOARD COOL CAUTION MSG. EMERGENCY DECLARED, A/C RETURNED TO CVG LANDED SAFELY. REMOVED AND REPLACED P
- [SDR COMA2010060850128](https://openairdocs.org/sdr/COMA2010060850128), Jun 7, 2010: BULKHEAD. CRACKED. ON FS 621.00 (REAR PRESSURE BULKHEAD) THERE IS A CRACK AT LBL 27.50, JUST ABOVE AFT CARGO DOOR TRACK. REPAIRED IAW REO 601R-53-61-1541.
- [SDR COMA2010060850127](https://openairdocs.org/sdr/COMA2010060850127), Jun 7, 2010: FLOORBEAM. CORRODED. AT FS 280.00 FLOOR SUPPORT BEAM IS CORRODED THROUGH AT NUT PLATE HOLE. REPAIRED FLOOR SUPPORT BEAM AFT ANGLE AT FS 280.00 LBL 9 - RBL 9 IAW REO 601R-53-11-136.
- [SDR COMA2010060850126](https://openairdocs.org/sdr/COMA2010060850126), Jun 7, 2010: FRAME. CRACKED. FS 280.00 FRAME HAS A CRACK BY THE LOWER RADIUS AT RBL 11. REPAIRED LOWER ANGLE ON FS 280.00 FRAME AT RBL 11, IAW REO 601R-53-11-171 SCHEME B.
- [SDR COMA2010060450125](https://openairdocs.org/sdr/COMA2010060450125), Jun 4, 2010: SILL. CORRODED. CORROSION FOUND ON PAX DOOR LOWER SILL PLATE. REMOVED AND REPLACED PAX DOOR SILL DUE TO EXCESSIVE CORROSION, REF SRM 51-42-06, SRM 51-41-10 AND SRM 51-42-21.
- [SDR COMA2010060250121](https://openairdocs.org/sdr/COMA2010060250121), Jun 2, 2010: FRAME. CRACKED. FOUND CRACK AT RIGHT SIDE FS 640 FRAME AT STRINGER 9 CUT OUT. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH REO 601R-53-61-557 REV A.
- [SDR COMA2009062350158](https://openairdocs.org/sdr/COMA2009062350158), Jun 23, 2009: ANGLE. CRACKED. CARGO FLOOR ANGLE AT REAR BULKHEAD LT SIDE FLOOR LEVEL IS CRACKED. REPAIRED CARGO FLOOR ANGLE IAW REO 601R-53-61-117.
- [SDR COMA0760411](https://openairdocs.org/sdr/COMA0760411), May 28, 2007: VERTICAL BEAM. CRACKED. VERTICAL BEAM LBL 27 FS 409+128 OUTBOARD LOWER SIDE CRACKED. REPAIRED PER REO 601R-53-41-056.
- [SDR COMA0760410](https://openairdocs.org/sdr/COMA0760410), May 28, 2007: STIFFENER. CRACKED. FOUND CRACK ON LOWER INBOARD FLANGE OF VERTICAL STIFFENER AT LBL 18 FS 559.00. REPAIRED PER REO 601R-53-41-067.
- [SDR COMA0760409](https://openairdocs.org/sdr/COMA0760409), May 28, 2007: VERTICAL BEAM. CRACKED. VERTICAL BEAM LBL 27 FS 409+128 INBOARD SIDE CRACKED. REPAIRED PER REO 601R-53-41-056.
- [SDR COMA0760408](https://openairdocs.org/sdr/COMA0760408), May 27, 2007: STIFFENER. CRACKED. CRACK IN LOWER VERTICAL STIFFENER AT FS 409+128 RBL18. REPAIRED BOTTOM VERTICAL BEAM PER REO 601R-53-41-056.
- [SDR COMA0760407](https://openairdocs.org/sdr/COMA0760407), May 27, 2007: STIFFENER. CRACKED. FOUND CRACK ON LOWER INBOARD FLANGE OF VERTICAL STIFFENER AT FS 559 LBL 27. COMPLIED WITH REO 601R-53-41-283.
- [SDR COMA0760406](https://openairdocs.org/sdr/COMA0760406), May 27, 2007: STIFFENER. CRACKED. CRACK IN LOWER OUTBOARD VERTICAL STIFFENER AT LBL 18 FS 409+128. REPAIRED IAW REO 601R-53-41-056.
- [SDR COMA0760405](https://openairdocs.org/sdr/COMA0760405), May 27, 2007: STIFFENER. CRACKED. FOUND CRACK ON LOWER OUTBOARD FLANGE ON SEMI PRESSURE BULKHEAD VERTICAL STIFFENER AT FS 559 RBL 9. REMOVED DAMAGED AREA ON FS 559 RBL 9 VERTICAL STIFFENER AND I
- [SDR COMA0760404](https://openairdocs.org/sdr/COMA0760404), May 27, 2007: STIFFENER. CRACKED. FOUND CRACK ON LOWER INBOARD SIDE FLANGE OF SEMI PRESSURE BULKHEAD VERTICAL STIFFENER AT FS 559, RBL 9. REMOVED DAMAGED AREA ON FS 559 RBL 9 VERTICAL STIFFENER 
- [SDR COMA0760403](https://openairdocs.org/sdr/COMA0760403), May 27, 2007: STIFFENER. CRACKED. FOUND CRACKS ON INBOARD AND OUTBOARD LOWER FLANGES ON LBL 9 VERTICAL AT FS 559. REPAIRED CRACK AT OUTBOARD LOWER FLANGE ON LBL 9 VERTICAL AT FS 559 IAW REO 601R
- [SDR COMA0760060](https://openairdocs.org/sdr/COMA0760060), Jan 25, 2007: ANTI-ICE VALVE. FAULTY. FLIGHT 4963 - EN ROUTE CVG-MDT RECEIVED A LEFT COWL ANTI-ICE CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND DIVERTED TO CMH. FLIGHT LANDED WITHOUT INCIDENT. RE
- [SDR COMA0660685](https://openairdocs.org/sdr/COMA0660685), Dec 4, 2006: WINDOW. FAILED. FLIGHT 5115 - F/O'S SIDE WINDOW CRACKED IN FLIGHT. AIRCRAFT DIVERTED TO ROC AND LANDED SAFELY. REMOVED AND REPLACED F/O'S SIDE WINDOW.
- [SDR COMA0660637](https://openairdocs.org/sdr/COMA0660637), Nov 16, 2006: ECU. MALFUNCTIONED. FLIGHT 5270 - DURING APPROACH TO JFK RECEIVED A STEERING INOPERATIVE CAUTION MESSAGE AFTER SELECTING GEAR DOWN. ABORTED APPROACH THEN LANDED WITHOUT INCIDENT ON
- [SDR COMA0660627](https://openairdocs.org/sdr/COMA0660627), Nov 10, 2006: FAIRING. BROKEN. FLIGHT 5221 - RAMP PERSONNEL REPORTED A PIECE OF DEBRIS WAS FOUND ON RAMP. A/C RETURNED BACK TO TUL AND WAS INSPECTED AND FOUND TO HAVE A DAMAGED RIGHT LOWER ST
- [SDR COMA0660495](https://openairdocs.org/sdr/COMA0660495), Aug 16, 2006: OVERHEAT SENSOR. DIRTY. FLIGHT 5533 - EN ROUTE CVG-CLE RECEIVED A CARGO OVERHEAT CAUTION MESSAGE, FLIGHT RETURNED TO CVG. CLEANED TEMPERATURE SENSORS IN THE CARGO BAY CEILING.
- [SDR COMA0660242](https://openairdocs.org/sdr/COMA0660242), Mar 12, 2006: FCU. FAULTY. FLIGHT 5833 - DURING TAXI-IN RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 DEGREES. REPLACED THE FLAP ELECTRONIC CONTROL UNIT.
- [SDR COMA0660241](https://openairdocs.org/sdr/COMA0660241), Mar 12, 2006: PDU. FAULTY. FLIGHT 5833 - DURING TAXI-IN RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 DEGREES. REPLACED THE POWER DRIVE UNIT.
- [SDR COMA0660172](https://openairdocs.org/sdr/COMA0660172), Feb 18, 2006: PROXIMITY SENSOR. OUT OF ADJUST. FLIGHT 5346 - DURING CLIMBOUT OF BGR RECEIVED A GEAR DISAGREE CAUTION IN THE UP POSITION, FLIGHT RETURNED TO THE FIELD. RIGGED THE PROXIMITY SENSOR PS3GA.
- [SDR COMA0560797](https://openairdocs.org/sdr/COMA0560797), Jan 5, 2006: LATCH. OUT OF ADJUST. FLIGHT 5543 - CABIN DOOR WARNING. ADJUSTED CABIN DOOR LATCH MECHANISM.
- [SDR COMA0560768](https://openairdocs.org/sdr/COMA0560768), Jan 4, 2006: WARNING LIGHT. FALSE ACTIVATION. FLIGHT 5543 - CABIN DOOR WARNING. INSPECTED DOOR AND WARNING SYSTEM, NO DEFECTS FOUND.
- [SDR COMA0560686](https://openairdocs.org/sdr/COMA0560686), Dec 6, 2005: PDU. MALFUNCTIONED. FLIGHT 2750 - FLAPS FAIL CAUTION. REPLACED THE FLAP PDU.
- [SDR COMA0560671](https://openairdocs.org/sdr/COMA0560671), Dec 5, 2005: FLAP SYSTEM. WARNING LIGHT. FLIGHT 5586 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
- [SDR COMA0560415](https://openairdocs.org/sdr/COMA0560415), Jul 28, 2005: SMOKE DETECTOR. UNRELIABLE. SMOKE CARGO WARNING, BOTTLES DISCHARGED. REPLACED SMOKE DETECTORS AND FIRE BOTTLES.
- [SDR COMA0560232](https://openairdocs.org/sdr/COMA0560232), Apr 4, 2005: PROXIMITY SWITCH. OUT OF ADJUST. FLIGHT 5202 RECEIVED A RED NOSE LANDING GEAR DISAGREE CAUTION ON APPROACH INTO CVG, ABORTED 1ST APPROACH THEN LANDED WITHOUT INCIDENT ON 2ND ATTEMPT AFTER FOLLO
- [SDR COMA0560222](https://openairdocs.org/sdr/COMA0560222), Mar 31, 2005: PRIORITY VALVE. FAULTY. FLIGHT 5607 ON APPROACH INTO SAV, RECEIVED A GEAR DISAGREE MASTER WARNING, CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED THE NLG PRIORITY VAL
- [SDR COMA0560221](https://openairdocs.org/sdr/COMA0560221), Mar 31, 2005: PRIORITY VALVE. FAULTY. FLIGHT 5607 ON APPROACH INTO SAV, RECEIVED A GEAR DISAGREE MASTER WARNING, CREW DELCARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED THE MLG PRIORITY VAL
- [SDR COMA0560108](https://openairdocs.org/sdr/COMA0560108), Feb 1, 2005: PRIORITY VALVE. UNRELIABLE. FLIGHT 5035 GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE.
- [SDR COMA0560063](https://openairdocs.org/sdr/COMA0560063), Jan 18, 2005: WIRE HARNESS. FAULTY. FLIGHT 5037 DURING CLIMBOUT OF LGA RECEIVED AN OVERBOARD COOL CAUTION MESSAGE. CREW DECLARED AN EMERGENCY, DIVERTED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED
- [SDR COMA0460664](https://openairdocs.org/sdr/COMA0460664), Dec 6, 2004: PRIORITY VALVE. UNRELIABLE. FLIGHT 5107 - STEERING INOP CAUTION DURING T/O. REPLACED THE NLG PRIORITY VALVE.
- [SDR COMA0460406](https://openairdocs.org/sdr/COMA0460406), Jul 8, 2004: BPSU. MALFUNCTIONED. FLIGHT 5120 FLAPS FAILED DURING APPROACH. REPLACED THE LT BPSU.
- [SDR COMA0460317](https://openairdocs.org/sdr/COMA0460317), May 9, 2004: FLOOR SUPPORT. CRACKED. CARGO BAY FLOOR SUPPORT ANGLE STRUCTURE CRACKED. REPAIRED IAW REO 601R-53-61-004.
- [SDR COMA0460316](https://openairdocs.org/sdr/COMA0460316), May 9, 2004: SKIN. CRACKED. LEFT LOWER WING PLANK CRACKED. REPAIRED IAW REO 601R-57-21-130.
- [SDR COMA0460002](https://openairdocs.org/sdr/COMA0460002), Dec 29, 2003: CONTROL UNIT. FAILED. FLIGHT 5073 FLAPS FAIL MESSAGE. REPLACED THE FECU.
- [SDR COMA0360448](https://openairdocs.org/sdr/COMA0360448), Oct 4, 2003: HYDRAULIC LINE. CUT. FLIGHT 5510 HYDRAULIC SYSTEM NR 2 LOW PRESSURE WARNING. REPLACED LEAKING PRESSURE LINE IN RT PYLON.
- [SDR COMA0360447](https://openairdocs.org/sdr/COMA0360447), Oct 2, 2003: TORQUE LINK. DISCONNECTED. FLIGHT 5319 GEAR DISAGREE WARNING WITH STEERING INOP AND WOW INPUT MESSAGE. FOUND NLG TORQUE LINKS DISCONNECTED. RECONNECTED TORQUE LINKS AND TAXI OPS CHECK, NO
- [SDR COMA0360414](https://openairdocs.org/sdr/COMA0360414), Sep 12, 2003: LIGHT. ODOR. F/A REPORTED BURNING ELECTRICAL ODOR IN LAVATORY. DEFERRED THE LAV LIGHTING SYSTEM PER MEL.
- [SDR COMA0360307](https://openairdocs.org/sdr/COMA0360307), Jun 28, 2003: SELECTOR VALVE. DEFECTIVE. FLIGHT 5803 WHEN LOWERING LANDING GEAR RECEIVED GEAR DISAGREE CAUTION. REPLACED THE NOSE LANDING GEAR SELECTOR VALVE.
- [SDR COMA0360270](https://openairdocs.org/sdr/COMA0360270), Jun 11, 2003: UPLOCK. OUT OF ADJUST. FLIGHT 5301 GEAR DISAGREE WARNING DURING APPROACH. ADJUSTED NOSE LANDING GEAR UPLOCK TO NEW T/R M/M SPECIFICATIONS.
- [SDR COMA0360261](https://openairdocs.org/sdr/COMA0360261), Jun 6, 2003: LANDING GEAR. MALFUNCTIONED. FLIGHT 5738 GEAR DISAGREE WARNING. CLEANED AND LUBED THE NLG. COULD NOT DUPLICATE DISCREPANCY.
- [SDR COMA0360233](https://openairdocs.org/sdr/COMA0360233), May 8, 2003: TORQUE BOX. CRACKED. RIGHT HAND THRUST REVERSER TORQUE BOX WAS FOUND CRACKED AT 6:30 O'CLOCK POSITION. REMOVED AND INSTALLED SERVICEABLE TORQUE BOX.
- [SDR COMA0360192](https://openairdocs.org/sdr/COMA0360192), Apr 15, 2003: PRIORITY VALVE. UNRELIABLE. FLIGHT 5907 LANDING GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE.
- [SDR COMA0360118](https://openairdocs.org/sdr/COMA0360118), Feb 23, 2003: DOOR. FLIGHT 5616 CABIN DOOR WARNING DURING FLIGHT.COULD NOT DUPLICATE. OPERATIONAL CHECK OF DOOR WAS NORMAL.

All 118: https://openairdocs.org/deregistered/N959CA-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 20031002032599I](https://openairdocs.org/incident/20031002032599I), Oct 2, 2003: Cndair CL6002B19 (N959CA), Rochester, NY. (-23) On Thursday October 2, 2003 at 06:15 local time, a Canadair CL-600-2B19 aircraft, bearing registration number N959CA, operating under 14 CFR part 121 as…

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