# N933CA: 1994 Canadair CL-600-2B19, registration cancelled 2012-08-16 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 16, 2012 - Exported to: Canada - Status when cancelled: Valid registration - 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: 7040 - Year built: 1994 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 29, 1994 - Certificate issued: June 23, 1994 - Last registry action: April 17, 2012 - Mode S code: ACF101 - 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: 40.8659° N, 112.0391° W: Placed by OpenAirDocs at the center of ZIP code 84116, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N933CA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=933CA - Page: https://openairdocs.org/deregistered/N933CA-2012-08-16 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 (97, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR COMA2010082450179](https://openairdocs.org/sdr/COMA2010082450179), Aug 21, 2010: BPSU. FAULTY. ON APPROACH INTO CVG RECEIVED FLAPS FAIL CAUTION MSG. EMERGENCY DECLARED, A/C LANDED SAFELY. REMOVED AND REPLACED LEFT BPSU. - [SDR COMA2010081650174](https://openairdocs.org/sdr/COMA2010081650174), Aug 13, 2010: ANTI-SKID SYS. MALFUNCTIONED. RECEIVED ANTI-SKID I/B CAUTION MSG ON GEAR EXTENSION. EMERGENCY DECLARED, A/C LANDED SAFELY. PERFORMED ANTI-SKID TEST PER AMM, OPS CHECK GOOD. - [SDR COMA2010062550134](https://openairdocs.org/sdr/COMA2010062550134), Jun 25, 2010: SKIN. DENTED. FOUND DENT IN FUSELAGE SKIN AT FS 584.75 STR 21R. REPAIRED FUSELAGE SKIN AT FS 584.75 STR 21R IAW EA 10-5360-02904A. - [SDR COMA2009050450124](https://openairdocs.org/sdr/COMA2009050450124), Apr 29, 2009: HYDRAULIC LINE. LEAKING. EN ROUTE FROM CVG TO CID RECEIVED HYD 1 LOW MSG, 0 QTY AND PSI. EMERGENCY DECLARED, A/C DIVERTED TO MLI LANDED SAFELY. REMOVED AND REPLACED HYDRAULIC SYSTEM 1 R - [SDR COMA2009040750111](https://openairdocs.org/sdr/COMA2009040750111), Apr 6, 2009: ANTI-ICE VALVE. FAILED. EN ROUTE FROM CVG TO EWR RECEIVED LEFT COWL ANTI-ICE CAUTION MSG, WITH COWL ANTI-ICE SWITCHED OFF. EMERGENCY DECLARED, A/C DIVERTED TO PIT LANDED SAFELY. REMOVE - [SDR COMA0860417](https://openairdocs.org/sdr/COMA0860417), Oct 11, 2008: FRAME. CRACKED. DURING 640 FRAME INSPECTION FOUND FRAME CRACKED AT STRINGER 9 RT CUTOUT. REPAIRED 640 FRAME PER REO 601R-53-61-557. - [SDR COMA0860416](https://openairdocs.org/sdr/COMA0860416), Oct 11, 2008: FRAME. CRACKED. DURING 640 FRAME INSPECTION FOUND FRAME CRACKED AT STRINGER 9 LT CUTOUT. REPAIRED 640 FRAME PER REO 601R-53-61-557. - [SDR COMA0860194](https://openairdocs.org/sdr/COMA0860194), Mar 24, 2008: CONTROLLER. MALFUNCTIONED. FLIGHT 5501 - RECEIVED TAT PROBE HEAT, RIGHT AOA HEAT, RIGHT STATIC HEAT AND RIGHT PITOT HEAT CAUTION MESSAGES. RESET NR 2 ADS CONTROLLER. NO FURTHER DEFECTS. - [SDR COMA0860167](https://openairdocs.org/sdr/COMA0860167), Mar 10, 2008: SEALANT. MISSING. FLIGHT 5451 - UPON FLAP SELECTION TO 8 DEGREES A THUMPING WAS FELT. ABORTED APPROACH, DECLARED EMERGENCY, TOWER VERIFIED GEAR DOWN UPON SELECTION. LANDED WITHOU - [SDR COMA0860160](https://openairdocs.org/sdr/COMA0860160), Mar 6, 2008: PRIORITY VALVE. FAULTY. FLIGHT 5236 - RECEIVED GEAR DISAGREE WARNING. RAN QRH, LOWERED GEAR MANUALLY, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED NLG PRIORITY VALVE. NO FURTH - [SDR COMA0860043](https://openairdocs.org/sdr/COMA0860043), Jan 2, 2008: FLAP. MALFUNCTIONED. FLIGHT 5560 - FLAPS FAIL CAUTION MESSAGE DURING APPROACH TO BTV. AIRCRAFT DIVERTED BACK TO JFK AND LANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I001, FLAPS FAI - [SDR COMA0760672](https://openairdocs.org/sdr/COMA0760672), Nov 26, 2007: FLAP. MALFUNCTIONED. FLIGHT 5239 - DURING TAXI OUT FLAPS FAIL CAUTION MESSAGE ILLUMINATED. AIRCRAFT RETURNED BACK TO GATE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EV - [SDR COMA0760612](https://openairdocs.org/sdr/COMA0760612), Oct 25, 2007: LAMP. INOPERATIVE. FLIGHT 4989 - EMERGENCY LIGHT INOP AT PAX DOOR. RELAMPED INOP EMERGENCY LIGHT. NO FURTHER DEFECTS. - [SDR COMA0760567](https://openairdocs.org/sdr/COMA0760567), Sep 11, 2007: FLAP. MALFUNCTIONED. FLIGHT 5459 - FLAP FAIL CAUTION MESSAGE RECEIVED. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- - [SDR COMA0760523](https://openairdocs.org/sdr/COMA0760523), Aug 9, 2007: FLAP. MALFUNCTIONED. FLIGHT 5419 - RECEIVED FLAP FAIL MESSAGE AT GATE. COMPLIED WITH AD 2006-12-21. FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, - [SDR COMA0760226](https://openairdocs.org/sdr/COMA0760226), Mar 5, 2007: FLAP SYSTEM. MALFUNCTIONED. FLIGHT 5559 - FLAPS FAIL AT GATE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYST - [SDR COMA0760180](https://openairdocs.org/sdr/COMA0760180), Feb 12, 2007: SENSOR. FAULTY. FLIGHT 5542 - DISPLAY COOK CAUTION MESSAGE RECEIVED. INSPECTED DUCTING, CLEANED FLOW SENSOR CONNECTOR, REPLACED FLOW SENSOR. NO FURTHER DEFECTS. - [SDR COMA0660700](https://openairdocs.org/sdr/COMA0660700), Dec 8, 2006: STRUT. UNDERSERVICED. AFTER TAKE-OFF AT APPROXIMATELY 145 KTS, GEAR DISAGREE MESSAGE ILLUMINATED, NOSE GEAR HAD RED HASH MARKS AND AFTER 10 SECONDS NOSE GEAR RETRACTED. AIRCRAFT RETU - [SDR COMA0660640](https://openairdocs.org/sdr/COMA0660640), Nov 18, 2006: FLAP SYSTEM. MALFUNCTIONED. FLIGHT 5585 - DURING POWER UP RECEIVED A FLAP FAIL MESSAGE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, - [SDR COMA0660613](https://openairdocs.org/sdr/COMA0660613), Nov 4, 2006: WARNING MESSAGE. ILLUMINATED. FLIGHT 5363- RECEIVED A FLAP FAIL CAUTION MESSAGE WHILE AT THE GATE WITH FLAP SETTING AT 20 DEGREES. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE "FIRST EVE - [SDR COMA0660461](https://openairdocs.org/sdr/COMA0660461), Jul 24, 2006: RESERVOIR. UNKNOWN. FLIGHT 5699 - EN ROUTE CVG-CHA EXPERIENCED HIGH OIL TEMPERATURE, FLIGHT RETURNED TO CVG. DEFERRED THE ENGINE OIL REPLENISHMENT SYSTEM PER MEL 79-12-01. - [SDR COMA0660309](https://openairdocs.org/sdr/COMA0660309), Apr 22, 2006: IDG. FAULTY. FLIGHT 5103 - DURING TAKEOFF ROLL RECEIVED A NR 2 IDG CAUTION MESSAGE, TAKEOFF WAS ABORTED AND FLIGHT RETURNED TO THE GATE. REPLACED THE RIGHT IDG. - [SDR COMA0560276](https://openairdocs.org/sdr/COMA0560276), Apr 26, 2005: SKIN PANEL. CRACKED. DURING COMPLIANCE OF AN H-6 CHECK, ONE CRACK WAS FOUND IN THE PRESSURE FLOOR SKIN NEAR FS 461 BETWEEN BL 0.0 AND RBL 9.0. THE CRACK WAS 1.5 INCHES LONG. THE PRE - [SDR COMA0560228](https://openairdocs.org/sdr/COMA0560228), Apr 3, 2005: WARNING SYSTEM. MALFUNCTIONED. FLIGHT 5175 - DURING TAKEOFF ROLL, RECEIVED A RIGHT WING ANTI ICE CAUTION, ABORTED TAKEOFF AND RETURNED TO THE GATE. C/W RTO INSPECTION AND PERFORMED AN OPERATI - [SDR COMA0560079](https://openairdocs.org/sdr/COMA0560079), Jan 22, 2005: DRAG BRACE. LACK OF LUBE. FLIGHT 5466 GEAR DISAGREE WARNING. NLG DID NOT RETRACT. CLEANED AND LUBED NLG DRAG BRACE. RETRACTION CHECKS WERE SATISFACTORY. - [SDR COMA0460550](https://openairdocs.org/sdr/COMA0460550), Sep 27, 2004: WARNING LIGHT. ILLUMINATED. FLIGHT 5742 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. - [SDR COMA0460433](https://openairdocs.org/sdr/COMA0460433), Jul 30, 2004: CONTROL HANDLE. MALFUNCTIONED. FLIGHT 5768 FLAPS FAIL CAUTION DURING LANDING ROLL. REPLACED THE FLAP SELECTOR LEVER. - [SDR COMA0460343](https://openairdocs.org/sdr/COMA0460343), May 28, 2004: WARNING LIGHT. ILLUMINATED. FLIGHT 5463 FLAPS FAIL CAUTION MESSAGE. RESET FLAPS AND DEFERRED MAINT PER AD 98-20-01. - [SDR COMA0460269](https://openairdocs.org/sdr/COMA0460269), Apr 13, 2004: PSEU. MALFUNCTIONED. FLIGHT 5479 NWS INOP, WOW INPUT CAUTION AND CIRCUIT BREAKER TRIPPED. RESET PSEU AND OPERATIONAL CHECK OF NWS WAS SATISFACTORY. - [SDR COMA0360561](https://openairdocs.org/sdr/COMA0360561), Dec 16, 2003: FLAP. MALFUNCTIONED. FLIGHT 5073 FLAPS DID NOT MOVE WHEN SELECTED TO 20 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. - [SDR COMA0360291](https://openairdocs.org/sdr/COMA0360291), Jun 24, 2003: COMPUTER. MALFUNCTIONED. FLIGHT 5797 SPOILER AND FLIGHT SPOILER CAUTION MESSAGE. REPLACED THE NR 2 SECU. - [SDR COMA0360199](https://openairdocs.org/sdr/COMA0360199), Apr 16, 2003: WARNING SYSTEM. ACTIVATED. FLIGHT 5276 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. - [SDR COMA0260611](https://openairdocs.org/sdr/COMA0260611), Oct 30, 2002: ANTI-ICE SYSTEM. FLIGHT 5883 LEFT WING ANTI-ICE DUCT WARNING MESSAGE.COULD NOT DUPLICATE. INSPECTED ANTI-ICE SYSTEM - NO FAULTS FOUND. - [SDR COMA0260130](https://openairdocs.org/sdr/COMA0260130), Feb 27, 2002: DOOR. FLIGHT 5409 CABIN DOOR OUTER HANDLE CAUTION MESSAGE.LUBRICATED DOOR LOCKING MECH. OPS CHECK SATISFACTORY. - [SDR COMA0260068](https://openairdocs.org/sdr/COMA0260068), Jan 25, 2002: SKIN. DAMAGED. THE LEFT SIDE OF THE FUSELAGE WAS DAMAGED AT STA 379-394 AND STR 23L-24L. REMOVED THE DAMAGED AREA. FABRICATED REPAIR PARTS AND INSTALLED. - [SDR COMA0260030](https://openairdocs.org/sdr/COMA0260030), Jan 5, 2002: DOOR. FLIGHT 5839 CABIN DOOR OUTER HANDLE MESSAGE.COULD NOT DUPLICATE OPERATED DOOR AND PRESSURIZED AIRCRAFT. NO DEFECTS. - [SDR COMA0160826](https://openairdocs.org/sdr/COMA0160826), Oct 20, 2001: BUSHING. WORN. L/H VERTICAL STABILIZER BUSHING P/N 600-21061-7 IS WORN.REMOVED THE WORN BUSHING I/A/W CRJ AMM CH 20-26-00-910-802, FABRICATED NEW BUSHING P/N 601R55-31-033-1 I - [SDR COMA0160822](https://openairdocs.org/sdr/COMA0160822), Oct 17, 2001: DOUBLER. CRACKED. FS 718.00 L/H AND R/H AFT DOUBLERS CRACKED, FRAME SECTIONS L/H UPPER AND R/H UPPER AND LOWER ARE CRACKED.F.S.718.00 L/H AND R/H AFT DOUBLERS REMOVED AND REPLACE - [SDR COMA0160718](https://openairdocs.org/sdr/COMA0160718), Sep 14, 2001: PCU. FAULTY. FLIGHT #5395. DURING TAXI OUT WHILE PERFORMING FLIGHT CONTROL CHECK RECEIVED A FLIGHT SPOILER FAULT STATUS MESSAGE, AIRCRAFT RETURNED TO THE GATE.REPLACED THE L - [SDR COMA0160615](https://openairdocs.org/sdr/COMA0160615), Aug 19, 2001: WIRE. LOOSE. FLIGHT 5931. DURING TAXI OUT OF CVG RECEIVED A PROXIMITY FAULT STATUS MESSAGE ON ELECTRONIC DISPLAY NR 2, AIRCRAFT RETURNED TO THE GATE.REPAIRED WIRING AND SECU - [SDR COMA0160616](https://openairdocs.org/sdr/COMA0160616), Aug 19, 2001: PSEU. FAULTY. FLIGHT #5776. DURING TAXI OUT OF HSV RECEIVED A PROXIMITY SYSTEM FAULT STATUS MESSAGE ON ELECTRONIC DISPLAY #2, AIRCRAFT RETURNED TO THE GATE.REPLACED THE PROXI - [SDR COMA0160543](https://openairdocs.org/sdr/COMA0160543), Jul 25, 2001: WEB. CRACKED. CRACK ON ENGINE SUPPORT BEAM UPPER SKIN.REPAIRED I/A/W REO 601R-53-61-345. - [SDR COMA0160542](https://openairdocs.org/sdr/COMA0160542), Jul 25, 2001: WEB. CRACKED. WHILE PERFORMING REPAIR TO THE ENGINE SUPPORT BEAM PER REO 53-61-345 A CRACK WAS NOTED ON THE UNDER LAYING EXTRUDED ANGLE P/N 601-35006-7 CRACK APPROX 5/16".THE - [SDR COMA0160363](https://openairdocs.org/sdr/COMA0160363), Apr 26, 2001: RIB. CRACKED. THE LT PYLON AT FS 605 IS CRACKED AT THE OUTBOARD LOWER FLANGE. REPAIRED DAMAGED AREA TO THE LT PYLON RIB AT FS 605 AT THE OUTBOARD LOWER FLANGE IAW WVAC EO 601 - [SDR COMA0160362](https://openairdocs.org/sdr/COMA0160362), Apr 24, 2001: ANGLE. CRACKED. THE ANGLES AT BL27 (LT & RT) AND INTERCOSTALS AT BL 36 (LT & RT) AT FS 484 ARE CRACKED. INSTALLED NEW SERVICEABLE LT & RT INBOARD AND OUTBOARD 484 ANGLES IAW WV - [SDR COMA0160057](https://openairdocs.org/sdr/COMA0160057), Jan 3, 2001: NOZZLE. DEPARTED. VIBRATION FELT DURING FLIGHT, VIBRATION STOPPED DURING DECENT. POST FLIGHT INSP FOUND LEFT ENGINE TAILPIPE AND EXHAUST FAIRING HAD DEPARTED ACFT.REPLACED LEFT E - [SDR COMA0060849](https://openairdocs.org/sdr/COMA0060849), Oct 28, 2000: BPSU. MALFUNCTIONED. FLAPS FAILED AT 20 DEGREES. REPLACED THE LEFT HAND BPSU. - [SDR COMA0060833](https://openairdocs.org/sdr/COMA0060833), Oct 14, 2000: CONTROL UNIT. MALFUNCTIONED. FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. - [SDR COMA0060462](https://openairdocs.org/sdr/COMA0060462), May 28, 2000: BULB. FAILED. AFT CEILING EMERGENCY LIGHT IS INOPERABLE. REPLACED LIGHT BULB. - [SDR COMA0060410](https://openairdocs.org/sdr/COMA0060410), May 11, 2000: ACTUATOR. WORN. FOUND LEFT OUTBOARD FLAP, INBOARD ACTUATOR HAD PLAY AT FORWARD BUSHING MOUNT. REMOVED AND REPLACED ACTUATOR WITH A SERVICEABLE ONE. AIRCRAFT RETURNED TO SERVICE All 97: https://openairdocs.org/deregistered/N933CA-2012-08-16/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 NYC01IA072](https://openairdocs.org/ntsb/NYC01IA072), Jan 3, 2001: Bombardier CL-600-2B19 (N933CA), Covington, KY, incident, minor damage. Probable cause: Missing exhaust nozzle bolts for undetermined reasons. A factor was inadequate maintenance inspection of the affected area. ## Other aircraft with N933CA - [Registered now](https://openairdocs.org/aircraft/N933CA): Raytheon B300, S/N FL-372, built 2002 --- 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.