# N956CA: 1996 Canadair CL-600-2B19, registration cancelled 2018-04-18

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 18, 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: 7105
- Year built: 1996
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard
- Airworthiness date: March 18, 1996
- Certificate issued: August 8, 2014
- Last registry action: August 8, 2014
- Mode S code: AD4B24
- 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/N956CA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=956CA
- Page: https://openairdocs.org/deregistered/N956CA-2018-04-18

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 (100, newest 50)

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

- [SDR COMA2012011750004](https://openairdocs.org/sdr/COMA2012011750004), Jan 13, 2012: BULKHEAD. CRACKED. BIRD STRIKE TO FS 169 BULKHEAD, UPPER RT SIDE, AT AFT EDGE OF RADOME. REMOVED AND REPLACED FS 169 BULKHEAD, IAW SRM 53-11-15.
- [SDR COMA2011012050010](https://openairdocs.org/sdr/COMA2011012050010), Jan 19, 2011: STEERING SYS. MALFUNCTIONED. ON APPROACH INTO ATL RECEIVED STEERING INOP MSG. UNABLE TO RESET. EMERGENCY DECLARED, A/C LANDED SAFELY. PERFORMED SYSTEM RESET FOR THE NOSE WHEEL STEERING SYST
- [SDR COMA2010021650043](https://openairdocs.org/sdr/COMA2010021650043), Feb 15, 2010: POST. CRACKED. FOUND CRACK IN VERTICAL POST AT FS 409+128, RBL 27.00, IN LOWER RADIUS. TRIMMED OUT DAMAGE AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-41-056 REV E.
- [SDR COMA2010021550042](https://openairdocs.org/sdr/COMA2010021550042), Feb 13, 2010: ANGLE. CRACKED. FOUND CRACK IN FRAME CAP ANGLE AT FS 559.00 LBL 18.00 INBOARD SIDE. REPAIRED CAP ANGLE AT FS 559.00 IAW REO 601R-53-41-260.
- [SDR COMA2010021550041](https://openairdocs.org/sdr/COMA2010021550041), Feb 13, 2010: POST. CRACKED. FOUND CRACK IN POST AT FS 409+128 LBL 27.00 LOWER RADIUS. REPAIRED POST AT FS 409+128 IAW REO 601R-53-41-056 REV E.
- [SDR COMA2010021550040](https://openairdocs.org/sdr/COMA2010021550040), Feb 12, 2010: BULKHEAD. CRACKED. DURING EDDY CURRENT FOUND CRACK IN AFT PRESSURE BULKHEAD FS 621.00 ABOVE CARGO DOOR TRACK. REPAIRED AFT PRESSURE BULKHEAD AT FS 621.00 IAW REO 601R-53-61-1541.
- [SDR COMA2010020950034](https://openairdocs.org/sdr/COMA2010020950034), Feb 7, 2010: SUPPORT. CRACKED. FOUND CRACK IN LOWER END OF FS 409+128 LBL 18 VERTICAL SUPPORT. CUT OUT DAMAGE AND INSTALLED REPAIR ANGLES IAW REO 601R-53-41-056 REV E.
- [SDR COMA2010020550033](https://openairdocs.org/sdr/COMA2010020550033), Feb 5, 2010: FLOOR SUPPORT. CRACKED. FOUND CRACK IN FS 280.00 FLOOR SUPPORT IN LOWER RADIUS AT RBL 9.00. REPAIRED FLOOR SUPPORT AT FS 280.00 RBL 9.00 IAW REO 601R-53-11-171.
- [SDR COMA2009093050195](https://openairdocs.org/sdr/COMA2009093050195), Sep 30, 2009: CONTROL HANDLE. FAULTY. ON APPROACH INTO BUF RECEIVED FLAPS FAIL CAUTION MSG WHEN SELECTING FLAPS FROM 20 TO 30 DEG. EMERGENCY DECLARED, A/C LANDED SAFELY. REMOVED AND REPLACED FLAP CO
- [SDR COMA2009032450103](https://openairdocs.org/sdr/COMA2009032450103), Mar 23, 2009: APU. MALFUNCTIONED. DURING TAXI APU MADE A LOUD SQUEAK, A BOOM THEN AUTO SHUTDOWN. SMOKE CAME OUT APU DOOR, NO FLAMES. EMERGENCY DECLARED. DEFERRED APU PER MEL 49-10-01-1.
- [SDR COMA0860064](https://openairdocs.org/sdr/COMA0860064), Jan 13, 2008: OUTFLOW VALVE. OBSTRUCTED. FLIGHT 5228 - ON CLIMBOUT FROM CVG RECEIVED CABIN ALTITUDE WARNING MESSAGE, WITH PACKS ON, CABIN PRESS RISING. AIRCRAFT RETURNED TO CVG AND LANDED SAFELY. UPON 
- [SDR COMA0760674](https://openairdocs.org/sdr/COMA0760674), Nov 29, 2007: CONTROLLER. MALFUNCTIONED. FLIGHT 4953 - A/C WILL NOT PRESSURIZE IN FLIGHT. TRIED BOTH CONTROLLERS AND MANUAL MODE WITH NO AFFECT. A/C RETURNED TO DTW AND LANDED SAFELY. TRANSFERRED TO DE
- [SDR COMA0760673](https://openairdocs.org/sdr/COMA0760673), Nov 27, 2007: CONNECTOR. BROKEN. FLIGHT 5594 - RECEIVED ANTI-SKID OUTBOARD CAUTION MESSAGE ON TAKEOFF ROLL. ABORTED TAKEOFF, RETURNED TO GATE WITHOUT INCIDENT. REPLACED BROKEN CONNECTOR ON WHEE
- [SDR COMA0760640](https://openairdocs.org/sdr/COMA0760640), Nov 13, 2007: CONTROLLER. FAULTY. FLIGHT 5219 - AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF FROM BOS. AIRCRAFT RETURNED TO BOS AND LANDED SAFELY. FOUND CABIN PRESSURE CONTROLLER FAULTY. DEFERRED
- [SDR COMA0760385](https://openairdocs.org/sdr/COMA0760385), May 20, 2007: RESERVOIR. LEAKING. FLIGHT 5661- RECEIVED GEAR DISAGREE MESSAGE. ABORTED APPROACH, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. FOUND NR 3 HYDRAULIC RESERVOIR LEAK DECAY RATE OU
- [SDR COMA0760374](https://openairdocs.org/sdr/COMA0760374), May 16, 2007: STIFFENER. CRACKED. DURING 559 INSPECTION FOUND 2 INCH CRACK ON INBOARD SIDE AND .5 INCH CRACK AT OUTBOARD SIDE OF VERTICAL STIFFENER, RBL 9, FS 559. REMOVED DAMAGE AND INSTALLED D
- [SDR COMA0760373](https://openairdocs.org/sdr/COMA0760373), May 16, 2007: STIFFENER. CRACKED. DURING 559 INSPECTION FOUND .5 INCH CRACK AT BASE OF VERTICAL STIFFENER, FS 559, RBL 18. REMOVED DAMAGE AND INSTALLED DOUBLER PER REO 601R-53-41-067.
- [SDR COMA0760372](https://openairdocs.org/sdr/COMA0760372), May 16, 2007: STIFFENER. CRACKED. DURING 559 INSPECTION FOUND .5 INCH CRACK AT LOWER OUTBOARD SIDE OF LBL VERTICAL STIFFENER. REMOVED DAMAGE AND INSTALLED DOUBLER PER BOMBARDIER REO 601R-53-41-0
- [SDR COMA0760363](https://openairdocs.org/sdr/COMA0760363), May 6, 2007: WARNING SYSTEM. MALFUNCTIONED. FLIGHT 5280 - LEFT T/R UNLOCK MESSAGE DURING POWER-UP. TROUBLESHOT LEFT T/R SYSTEM AND PERFORMED OPS CHECKS, NO DEFECTS NOTED.
- [SDR COMA0660701](https://openairdocs.org/sdr/COMA0660701), Dec 8, 2006: FLAP SYSTEM. MALFUNCTIONED. FLAPS FAILED ON FINAL AT 30 DEGREES. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SY
- [SDR COMA0660486](https://openairdocs.org/sdr/COMA0660486), Aug 12, 2006: SENSOR. FAULTY. FLIGHT 9459 - DURING CVG APPROACH RECEIVED A LANDING GEAR DISAGREE MESSAGE, ABORTED APPROACH, THEN LANDED WITHOUT INCIDENT. REPLACED MLG UPLOCK PROXIMITY SENSOR
- [SDR COMA0660439](https://openairdocs.org/sdr/COMA0660439), Jul 18, 2006: VALVE. FAULTY. FLIGHT 5117- DURING APPROACH RECEIVED A LANDING GEAR DOWN DISAGREE CAUTION, CREW DECLARED AN EMERGENCY, PERFORMED A MANUAL GEAR EXTENSION AND TOWER FLY-BY. FLIG
- [SDR COMA0660292](https://openairdocs.org/sdr/COMA0660292), Apr 6, 2006: LINE. LEAKING. FLIGHT 5662- EN ROUTE MCO-RDU, RECEIVED A NR 1 HYDRAULIC SYSTEM LOW PRESSURE CAUTION, FLIGHT DIVERTED TO SAV. REPLACED LEAKING BRAIDED HYDRAULIC LINE.
- [SDR COMA0560619](https://openairdocs.org/sdr/COMA0560619), Nov 18, 2005: EJECTOR. MALFUNCTIONED. FLIGHT 5440 - RECEIVED A CABIN ALTITUDE MESSAGE DURING CRUISE FLIGHT, DIVERTED TO RDU FOR PRESSURIZATION PROBLEM. REMOVED, INSPECTED AND RE-INSTALLED THE JET PU
- [SDR COMA0560618](https://openairdocs.org/sdr/COMA0560618), Nov 18, 2005: SEAL. DAMAGED. FLIGHT 9452 - DURING CLIMBOUT OF RDU, CABIN WAS SLOW TO PRESSURIZE. FLIGHT RETURNED TO RDU FOR PRESSURIZATION PROBLEM. FERRIED A/C TO CVG FOR REPLACEMENT OF THE
- [SDR COMA0560505](https://openairdocs.org/sdr/COMA0560505), Sep 16, 2005: ACTUATOR. FAULTY. FLIGHT 5786 - DURING CLIMBOUT OF JFK RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 DEGREE FLAP SETTING. REPLACED FLAP ACTUATOR.
- [SDR COMA0560503](https://openairdocs.org/sdr/COMA0560503), Sep 15, 2005: ACTUATOR. UNRELIABLE. FLIGHT 5262 - FLAPS FAIL CAUTION. CND, REPLACED 2 FLAP ACTUATORS AND 1 FLEX DRIVE CABLE. RE-RIGGED SYSTEM.
- [SDR COMA0560501](https://openairdocs.org/sdr/COMA0560501), Sep 14, 2005: BPSU. MALFUNCTIONED. FLIGHT 4960 - FLAPS FAIL CAUTION. REPLACED THE LEFT BPSU.
- [SDR COMA0560488](https://openairdocs.org/sdr/COMA0560488), Sep 5, 2005: CONTROL SYSTEM. FAILED. FLT 5805 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
- [SDR COMA0560437](https://openairdocs.org/sdr/COMA0560437), Aug 11, 2005: WIRE HARNESS. CHAFED. FLIGHT 5164 - EN ROUTE FSD - CVG RECEIVED A NR 2 ENGINE FIRE MESSAGE, SHUTDOWN NR 2 ENGINE. FLIGHT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 ENGINE ASS
- [SDR COMA0560099](https://openairdocs.org/sdr/COMA0560099), Jan 30, 2005: PROXIMITY SENSOR. MALFUNCTIONED. FLIGHT 5443 GEAR DISAGREE WARNING AFTER T/O. REPLACED THE LT NLG DOWNLOCK PROXIMITY SENSOR.
- [SDR COMA0560008](https://openairdocs.org/sdr/COMA0560008), Dec 21, 2004: DOOR. OPEN. FLIGHT 5315, 02 SERVICE DOOR LEFT OPEN. INSPECTED FOR DAMAGE AND SECURED DOOR IN CLOSED POSITION.
- [SDR COMA0460618](https://openairdocs.org/sdr/COMA0460618), Nov 13, 2004: WARNING LIGHT. ACTIVATED. FLIGHT 5316 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. LANDING GEAR EXTENSION AND RETRACTION CHECKS WERE NORMAL AND SATISFACTORY.
- [SDR COMA0460001](https://openairdocs.org/sdr/COMA0460001), Dec 31, 2003: SKIN. CORRODED. THE LEFT AND RIGHT LOWER WING TANK ACCESS PANEL CUTOUTS HAD CORROSION AT PANELS 640AB, 640CB, 640DB, 640FB, 640BB, 540BB, 540FB, 550AB AND 550BB. REMOVED CORROS
- [SDR COMA0360581](https://openairdocs.org/sdr/COMA0360581), Dec 30, 2003: HINGE FITTING. CHAFED. RIGHT ELEVATOR NR 1 HINGE POINT ON THE HORIZONTAL IS CHAFED. REPAIRED BY BLENDING CHAFED AREA SMOOTH, PERFORMED LIQUID PENETRANT INSPECTION, ROTO/FLAP PEEN REWO
- [SDR COMA0360579](https://openairdocs.org/sdr/COMA0360579), Dec 27, 2003: SKIN. DENTED. DENT .018 DEEP IN LEFT FUSELAGE LOWER SKIN AT FS 580.00 + 30 BELOW STR 20 L. RECONTOURED SKIN DAMAGE AREA IAW WVAC EO NR 601R-53-4489.
- [SDR COMA0360577](https://openairdocs.org/sdr/COMA0360577), Dec 27, 2003: SKIN. CRACKED. THE LEFT LOWER WING PLANK FUEL DRAIN FORWARD SCREW HOLE AT WS 85.5 HAD AN INDICATION WHILE PERFORMING EDDY CURRENT INSPECTION (FUEL BOOST PUMP DRAIN VALVE FORWA
- [SDR COMA0360576](https://openairdocs.org/sdr/COMA0360576), Dec 27, 2003: FLOORBEAM. CORRODED. THE FLOORBEAM CAP BETWEEN FS 559+12 TO FS 620, LBL 27 WAS CORRODED. REMOVED THE CORRODED FLOORBEAM CAP AND INSTALLED A NEW BEAM CAP IAW WVAC EO 601R-53-4501.
- [SDR COMA0360468](https://openairdocs.org/sdr/COMA0360468), Oct 23, 2003: ENGINE. FAILED. FLIGHT 5308 LOUD BANG FOLLOWED BY LEFT ENGINE FAILURE. REPLACED LEFT ENGINE.
- [SDR COMA0360240](https://openairdocs.org/sdr/COMA0360240), May 16, 2003: SWITCH. FAILED. FLIGHT 5575 DURING TAKE OFF ROLL RECEIVED A STABILIZER TRIM CAUTION, ABORTED T/O AND RETURNED TO THE GATE. REPLACED THE LEFT AND RIGHT PITCH TRIM DISCONNECT SWI
- [SDR COMA0360144](https://openairdocs.org/sdr/COMA0360144), Mar 11, 2003: FLAP. FLIGHT 5103 FLAPS FAILED AT 20 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
- [SDR COMA0260696](https://openairdocs.org/sdr/COMA0260696), Dec 6, 2002: APU. FLIGHT 5169 FUEL FUMES IN FWD SECTION OF AIRCRAFT AFTER APU START.COULD NOT DUPLICATE, OPERATIONAL CHECK OF APU WAS NORMAL.
- [SDR COMA0260523](https://openairdocs.org/sdr/COMA0260523), Sep 10, 2002: WIRE. FAILED. FLIGHT 5975. AFTER DEPARTING CVT RECEIVED A STEERING IMPERATIVE MESSAGE AFTER GEAR RETRACTION. FLIGHT RETURNED TO THE FIELD.REPLACED THE STEERING WIRING HARNESS
- [SDR COMA0260494](https://openairdocs.org/sdr/COMA0260494), Aug 22, 2002: DOOR LATCH. FLIGHT 5622 CARGO DOOR OPEN CAUTION MESSAGE.FOUND HANDLE UNLATCHED - CLOSED AND LATCHED HANDLE.
- [SDR COMA0260487](https://openairdocs.org/sdr/COMA0260487), Aug 14, 2002: TARGET. LOOSE. FLIGHT 5787 GEAR DISAGREE MESSAGE, R/H MLG DID NOT INDICATE UPLOCK.TIGHTENED LOOSE PROXIMITY SENSOR TARGET ON R/H MLG UPLOCK.
- [SDR COMA0260287](https://openairdocs.org/sdr/COMA0260287), Apr 28, 2002: FCU. MALFUNCTIONED. FLAPS FAIL MESSAGE. REPLACED THE FECU.
- [SDR COMA0260286](https://openairdocs.org/sdr/COMA0260286), Apr 28, 2002: FLAP. FLAPS FAILED AT 20 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
- [SDR COMA0260175](https://openairdocs.org/sdr/COMA0260175), Mar 9, 2002: CABLE. LOOSE. FLIGHT 5010 EMERGENCY FLOOR PATH LIGHTING INOP.SECURED LOOSE WIRE CONNECTION AT ROW 11.
- [SDR COMA0260025](https://openairdocs.org/sdr/COMA0260025), Dec 31, 2001: SWITCH. MALFUNCTIONED. FLIGHT 5527 - AFTER T/O, L/H AC PACK HIGH PRESSURE MESSAGE, FOLLOWED BY BLEED AIR DUCT MESSAGE, FOLLOWED BY L/H JET PIPE OVERHEAT, FOLLWOED BY R/H AC PACK HIGH 
- [SDR COMA0160902](https://openairdocs.org/sdr/COMA0160902), Nov 15, 2001: PLANK. CRACKED. RIGHT LOWER WING CUT OUT AT 640 C B CRACKED.BLENDED OUT DAMAGE AND ROTO-PEENED I/A/W REO 601R-57-21-030.

All 100: https://openairdocs.org/deregistered/N956CA-2018-04-18/reports.md

## Other aircraft with N956CA

- [Registered now](https://openairdocs.org/aircraft/N956CA): Raytheon HAWKER 850XP, S/N 258806

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