# N966CA: 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: 7132
- Year built: 1996
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 30, 1996
- Certificate issued: August 8, 2014
- Last registry action: March 17, 2017
- Mode S code: AD72A3
- 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/N966CA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=966CA
- Page: https://openairdocs.org/deregistered/N966CA-2020-12-05

From the FAA registry file of November 12, 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 (109, newest 50)

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

- [SDR COMA2012073050053](https://openairdocs.org/sdr/COMA2012073050053), Jul 30, 2012: CAMSHAFT. CRACKED. RIGHT RUDDER CENTERING AND FEEL CAM, MOUNT SHAFT CRACKED AT TAPER PIN HOLE. REMOVED AND REPLACED RIGHT RUDDER SYSTEM CENTERING AND FEEL CAM SHAFT IAW AMM 27-21-
- [SDR COMA2011120250096](https://openairdocs.org/sdr/COMA2011120250096), Dec 1, 2011: CONNECTOR. OUT OF POSITION. ON APPROACH INTO DTW RECEIVED NOSE WHEEL STEERING CAUTION MSG WITH LANDING GEAR SELECTED DOWN, WOULD NOT RESET. EMERGENCY DECLARED, A/C LANDED SAFELY. ON INSPEC
- [SDR COMA2010121350259](https://openairdocs.org/sdr/COMA2010121350259), Dec 10, 2010: UNKNOWN. SMOKE. ON CLIMBOUT FROM CLE SMOKE IN COCKPIT AND VERY BACK OF CABIN. EMERGENCY DECLARED, A/C RETURNED TO CLE LANDED SAFELY. SMOKE DISSIPATED BEFORE LANDING. INSPECTED 
- [SDR COMA2010102550229](https://openairdocs.org/sdr/COMA2010102550229), Oct 25, 2010: ANGLE. CRACKED. FS 559.00 RBL 18.00 CRACKED AT CAP ANGLE, IN BEND RADIUS. REPAIRED FS 559 CAP ANGLE AT RBL 18 IAW REO 601R-53-41-260 RT REP AND DEVIATION REO 601R-53-41-609.
- [SDR COMA2010102550228](https://openairdocs.org/sdr/COMA2010102550228), Oct 25, 2010: ANGLE. CRACKED. FS 559.00 LBL 18.00 CRACKED AT CAP ANGLE, IN BEND RADIUS. REPAIRED FS 559 CAP ANGLE AT LBL 18 IAW REO 601R-53-41-260 LT REP.
- [SDR COMA2010101150219](https://openairdocs.org/sdr/COMA2010101150219), Oct 9, 2010: DOUBLER. CRACKED. LEFT SIDE FUSELAGE 640 SKIN DOUBLER FOUND CRACKED. REMOVED DAMAGE FABRICATED PARTS AND INSTALLED PER S/B 601R-53-061 -C , REO 601R-53-61-569, 601R-53-366, REO 6
- [SDR COMA2010101150218](https://openairdocs.org/sdr/COMA2010101150218), Oct 9, 2010: DOUBLER. CRACKED. RIGHT SIDE FUSELAGE 640 SKIN DOUBLER FOUND CRACKED. REMOVED DAMAGE FABRICATED PARTS AND INSTALLED PER S/B 601R-53-061 -C , REO 601R-53-61-569, 601R-53-366, REO 
- [SDR COMA2010101150217](https://openairdocs.org/sdr/COMA2010101150217), Oct 9, 2010: ANGLE. CRACKED. CRACK FOUND ON THE LEFT 640.00 FUSELAGE FRAME REINFORCEMENT ANGLE IN THE RADIUS BETWEEN STR 9 & STR 12. REMOVED DAMAGE FROM LT SIDE OF 640, INSTALLED S/B 601R-5
- [SDR COMA2010100450215](https://openairdocs.org/sdr/COMA2010100450215), Oct 2, 2010: ANGLE. CRACKED. CRACK FOUND ON THE RIGHT 640.00 FUSELAGE FRAME REINFORCEMENT ANGLE IN THE RADIUS BETWEEN STR 9 & STR 12. REMOVED DAMAGE AND INSTALLED S/B601R-53-061, C/W REO 60
- [SDR COMA2010060450123](https://openairdocs.org/sdr/COMA2010060450123), Jun 2, 2010: WARNING SYSTEM. ACTIVATED. ON CLIMBOUT FROM BOS RECEIVED FLAPS FAIL CAUTION MSG AT 18 DEG. EMERGENCY DECLARED, A/C RETURNED TO BOS AND LANDED SAFELY. TRANSFERRED TO DEFERRED LIST PER MEL 
- [SDR COMA2010051750116](https://openairdocs.org/sdr/COMA2010051750116), May 15, 2010: DETECTOR. FAULTY. ON APPROACH INTO DTW FLAPS FAILED AT 22 DEG. EMERGENCY DECLARED, A/C LANDED SAFELY. REMOVED AND REPLACED RIGHT SIDE NR 3 SKEW DETECTOR.
- [SDR COMA2010051050115](https://openairdocs.org/sdr/COMA2010051050115), May 9, 2010: DETECTOR. FAULTY. ON APPROACH INTO ATL RECEIVED FLAPS FAIL CAUTION MSG AT 8 DEG. EMERGENCY DECLARED, FOLLOWED QRH A/C LANDED SAFELY. REMOVED AND REPLACED SKEW DETECTION UNIT.
- [SDR COMA2010041950100](https://openairdocs.org/sdr/COMA2010041950100), Apr 17, 2010: HYDRAULIC LINE. LEAKING. ON APPROACH INTO MCI RECEIVED HYD 2 LOW PRESSURE CAUTION MSG. EMERGENCY DECLARED, A/C LANDED SAFELY. INSPECTED A/C FOUND NR 2 SYSTEM HYD PRESSURE HOSE IN RIGHT 
- [SDR COMA2010040550081](https://openairdocs.org/sdr/COMA2010040550081), Apr 2, 2010: FLAP. FAILED. ON APPROACH INTO IAD FLAPS FAILED AT 3 DEG. EMERGENCY DECLARED, A/C LANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I0002, FLAPS FAIL CAUTION MESSAGE FOLLOW UP MA
- [SDR COMA2010012850025](https://openairdocs.org/sdr/COMA2010012850025), Jan 27, 2010: CARBON SEAL. BLOWN. EN ROUTE FROM LGA TO CHS RECEIVED SMOKE TOILET MSG, F/A CHECKED ALARM AND RESET AND MSG WENT OUT, MSG CAME BACK ON 3 TO 4 MIN LATER THEN WENT OUT AGAIN. F/A REP
- [SDR COMA2009081050178](https://openairdocs.org/sdr/COMA2009081050178), Aug 8, 2009: FLAP. OUT OF RIG. DURING T/O FROM PHL RECEIVED FLAPS FAIL CAUTION MSG AT 17 DEG. EMERGENCY DECLARED, A/C RETURNED TO PHL LANDED SAFELY. RE-RIGGED FLAP SYSTEM, OPS CHECK GOOD.
- [SDR COMA086380](https://openairdocs.org/sdr/COMA086380), Sep 2, 2008: BULKHEAD. CRACKED. CRACK ON AFT PRESSURE BULKHEAD ABOVE CARGO DOOR TRACK AT LBL 27.50. REPAIRED AFT PRESSURE BULKHEAD AT LBL 27.50 IAW REO 601R-53-61-1541.
- [SDR COMA086378](https://openairdocs.org/sdr/COMA086378), Sep 1, 2008: FRAME. CRACKED. DURING HMV6 INSPECTION, FOUND FRAME DOUBLER CRACKED AT FS 718, BETWEEN STRINGERS 10 RT AND 11 RT. CUT OUT DAMAGED SECTION OF FRAME/DOUBLER AND INSTALLED REPAIR 
- [SDR COMA086379](https://openairdocs.org/sdr/COMA086379), Sep 1, 2008: FRAME. CRACKED. DURING HMV6 INSPECTION, FOUND FRAME DOUBLER CRACKED AT FS 718, BETWEEN STRINGERS 10 LT AND 11 LT. CUT OUT DAMAGED SECTION OF FRAME/DOUBLER AND INSTALLED REPAIR 
- [SDR COMA0760667](https://openairdocs.org/sdr/COMA0760667), Nov 23, 2007: DUCT. DISCONNECTED. FLIGHT 5473 - CABIN ALT CAUTION MESSAGE FOLLOWED BY CABIN ALT WARNING MESSAGE AFTER LEVELING OFF AT FS 240. QRH FOLLOWED FOR BOTH MSGS, CONTINUED DESCENT INTO M
- [SDR COMA0760541](https://openairdocs.org/sdr/COMA0760541), Aug 24, 2007: SWITCH. OUT OF POSITION. FLIGHT 4961 - RECEIVED NOSE DOOR WARNING MESSAGE. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. FOUND NOSE DOOR MAINTENANCE SWITCH IN OPEN POSITION. RETURNED 
- [SDR COMA0760353](https://openairdocs.org/sdr/COMA0760353), May 1, 2007: BULKHEAD. CRACKED. DURING FS 559 INSPECTION FOUND CRACK AT SEMI-PRESSURE BULKHEAD, FS 559, RBL 18. STOP DRILLED CRACK AND INSTALLED DOUBLER PER CRJ REO 601R-53-41-353.
- [SDR COMA0760168](https://openairdocs.org/sdr/COMA0760168), Feb 6, 2007: SHAFT. LACK OF LUBE. FLIGHT 5542 - FLAPS FAILED DURING APPROACH. REMOVED, INSPECTED, LUBRICATED AND REINSTALLED ALL FLEX DRIVE SHAFTS.
- [SDR COMA0760139](https://openairdocs.org/sdr/COMA0760139), Feb 5, 2007: FLAP SYSTEM. MALFUNCTIONED. FLIGHT 5464 - DURING JFK APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. COMPLIED WITH AD 2006-12-
- [SDR COMA0660678](https://openairdocs.org/sdr/COMA0660678), Dec 3, 2006: WINDSHIELD. CRACKED. FLIGHT 5330 - LT WINDSHIELD SHATTERED IN FLIGHT. EMERGENCY DECLARED, FLIGHT DIVERTED TO SGF AND LANDED WITHOUT INCIDENT. REPLACED LT WINDSHIELD.
- [SDR COMA0660625](https://openairdocs.org/sdr/COMA0660625), Nov 12, 2006: LAMP. FAILED. FLIGHT 5464 - LAST STRIP OF EMERGENCY LIGHTS ON CABIN FLOOR INOP. REMOVED AND REPLACED LIGHT STRIP.
- [SDR COMA0660575](https://openairdocs.org/sdr/COMA0660575), Oct 8, 2006: STRUT. LOW. FLIGHT 9492 - NOSE DOOR, GEAR DISAGREE AND STEERING INOP MESSAGES ON TAKEOFF. RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. NO EMERGENCY DECLARED. NO PSEU CO
- [SDR COMA0660547](https://openairdocs.org/sdr/COMA0660547), Sep 20, 2006: CONNECTOR. LOOSE. FLIGHT 5330- AFT SECTION OF FLOOR EMERGENCY LIGHTING FAILED TO ILLUMINATE. RESECURED THE ELECTRICAL CONNECTOR FOR AFT FLOOR FLEXIBLE LIGHTING STRIP.
- [SDR COMA0660377](https://openairdocs.org/sdr/COMA0660377), Jun 4, 2006: BPSU. FAULTY. FLIGHT 5674 - FLAP FAIL EN ROUTE JFK-LGA AT 0 DEGREES, CREW DECLARED AN EMERGENCY, RETURNED TO JFK. REPLACED RIGHT BPSU.
- [SDR COMA0660376](https://openairdocs.org/sdr/COMA0660376), Jun 3, 2006: FLAP. MALFUNCTIONED. FLIGHT 5082 - FLAP FAIL MESSAGE CAME ON DURING DESCENT, CREW DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST 
- [SDR COMA0660244](https://openairdocs.org/sdr/COMA0660244), Mar 13, 2006: TILLER. OUT OF ADJUST. FLIGHT 5829 - NWS INOPERABLE MESSAGE. LANDED WITH NWS SELECTED OFF. FOUND LEFT RVDT AND COCKPIT TILLER OUT OF ADJUSTMENT. ADJUSTED IAW CRJ AMM 32-51-20. TAXI CH
- [SDR COMA0560840](https://openairdocs.org/sdr/COMA0560840), Jan 30, 2006: TRANSFORMER. FAILED. FLIGHT 5425 - DURING FLIGHT RECEIVED A STEERING INOPERATIVE MESSAGE, CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. STEERING WAS INTERMITTENT DURING TA
- [SDR COMA0560766](https://openairdocs.org/sdr/COMA0560766), Jan 3, 2006: STEERING SYS. INOPERATIVE. FLIGHT 5468 - STEERING INOP CAUTION. OPERATIONAL CHECK OF NWS WAS SATISFACTORY.
- [SDR COMA0560712](https://openairdocs.org/sdr/COMA0560712), Dec 11, 2005: ECU. MALFUNCTIONED. FLIGHT 9451 - NOSE WHEEL STEERING INOP CAUTION. REPLACED LT AND RT RVDT'S AND THE ECU.
- [SDR COMA0560401](https://openairdocs.org/sdr/COMA0560401), Jul 19, 2005: MODULE. MALFUNCTIONED. FLIGHT 9474- NLG STEERING INOPERATIVE. REPLACED THE ELECTROHYDRAULIC MODULE.
- [SDR COMA0560360](https://openairdocs.org/sdr/COMA0560360), Jun 20, 2005: UPLOCK TARGET. UNRELIABLE. GEAR DISAGREE WARNING. TIGHTENED LOOSE PROX SWITCH TARGET ON RT MLG UPLOCK.
- [SDR COMA0560335](https://openairdocs.org/sdr/COMA0560335), Jun 3, 2005: SELECTOR VALVE. FAULTY. AFTER DEPARTURE, RECEIVED NOSE GEAR DISAGREE WARNING MESSAGE. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD LANDING WITHOUT INCIDENT. REPLACED NLG SELECT
- [SDR COMA0560243](https://openairdocs.org/sdr/COMA0560243), Apr 4, 2005: CABLE. FAILED. FLIGHT 5318 DURING TEST OF LIGHTING SYSTEM THE EMERGENCY LIGHT FROM ROWS 2 THROUGH 5 FAILED TO ILLUMINATE. REPLACED CABLE ASSEMBLY AT ROWS 2 THROUGH 5.
- [SDR COMA0560145](https://openairdocs.org/sdr/COMA0560145), Feb 25, 2005: PDU. FAULTY. FLIGHT 5792 - RECEIVED A FLAP FAIL CAUTION DURING YYZ APPROACH, CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT POWER DRIVE UNIT.
- [SDR COMA0560144](https://openairdocs.org/sdr/COMA0560144), Feb 25, 2005: CONTROL SYSTEM. MALFUNCTIONED. FLIGHT 5792 RECEIVED A FLAP FAIL CAUTION AFTER DEPARTING CVG, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. AIRCRAFT LANDED WITHOUT INCIDENT. COMPLIED W
- [SDR COMA0560143](https://openairdocs.org/sdr/COMA0560143), Feb 25, 2005: BPSU. FAULTY. RECEIVED A FLAP FAIL CAUTION DURING YYZ APPROACH, CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT BRAKE POSITION SENSING UNIT.
- [SDR COMA0560138](https://openairdocs.org/sdr/COMA0560138), Feb 20, 2005: WARNING LIGHT. ILLUMINATED. FLIGHT 5250 FLAPS FAIL CAUTION. COULD NOT DUPLICATE. INSPECTED FLAPS PER AD 98-20-01. NO DEFECTS FOUND.
- [SDR COMA0560135](https://openairdocs.org/sdr/COMA0560135), Feb 18, 2005: DOOR. OUT OF ADJUST. FLIGHT 5825 NOSE DOOR OPEN WARNING AFTER GEAR EXTENSION. ADJUSTED THE LT NLG DOOR.
- [SDR COMA0560116](https://openairdocs.org/sdr/COMA0560116), Feb 10, 2005: COUPLING. WORN. FLIGHT 5738 FLAPS FAIL CAUTION. REPLACED THE RT WING NR 2 FLEX DRIVE SHAFT.
- [SDR COMA0560097](https://openairdocs.org/sdr/COMA0560097), Jan 29, 2005: DOOR. OVERSERVICED. FLIGHT 5165 CABIN DOOR OUTER HANDLE CAUTION. CLEANED EXCESS GREASE FROM DOOR HANDLE, NO DEFECTS FOUND.
- [SDR COMA0560075](https://openairdocs.org/sdr/COMA0560075), Jan 21, 2005: BPSU. UNRELIABLE. FLIGHT 5008 FLAPS FAILED CAUTION. REPLACED THE LEFT BPSU.
- [SDR COMA0560069](https://openairdocs.org/sdr/COMA0560069), Jan 19, 2005: CONTROL UNIT. MALFUNCTIONED. FLIGHT 5330 - FLAPS FAILED AT "O". REPLACED THE FECU.
- [SDR COMA0560056](https://openairdocs.org/sdr/COMA0560056), Jan 18, 2005: WARNING LIGHT. ILLUMINATED. FLIGHT 5786 DURING APPROACH TO HPN RECEIVED A FLAP FAIL MESSAGE, FLAPS REMAINED A ZERO DEGREES WHEN SELECTED TO DEPLOY. CREW DECLARED AN EMERGENCY, ABORTED APPR
- [SDR COMA0560029](https://openairdocs.org/sdr/COMA0560029), Jan 9, 2005: MOTOR. UNRELIABLE. FLIGHT 5803 STAB TRIM CAUTION. REPLACED THE STAB TRIM ACTUATOR.
- [SDR COMA0460700](https://openairdocs.org/sdr/COMA0460700), Dec 20, 2004: ACTUATOR. MALFUNCTIONED. FLIGHT 5316 FLAPS FAILED CAUTION MESSAGE. REPLACED THE LEFT SIDE NR 2 FLAP ACTUATOR.

All 109: https://openairdocs.org/deregistered/N966CA-2020-12-05/reports.md

---
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, except the copies of manufacturers’ service documents, which belong to their rights holders.