# N949CA: Canadair CL-600-2B19, registration cancelled 2007-10-19

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 19, 2007
- Status when cancelled: Triennial form not returned
- Airframe: [Canadair CL-600-2B19](https://openairdocs.org/model/canadair-cl-600-2b19) (registry code 1900309)
- Data sheets: [TCDS A21EA-1](https://openairdocs.org/tcds/A21EA-1) (OpenAirDocs)
- Serial number: 7080
- Type of aircraft: Fixed wing multi engine
- Certificate issued: September 27, 1995
- Last registry action: November 15, 2005
- Mode S code: AD2ECA
- 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: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N949CA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=949CA
- Page: https://openairdocs.org/deregistered/N949CA-2007-10-19

From the FAA registry file of November 4, 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 (90, newest 50)

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

- [SDR COMA0660588](https://openairdocs.org/sdr/COMA0660588), Oct 27, 2006: ANTI-ICE SYSTEM. WARNING LIGHT. FLIGHT 5644 - ANTI-ICE DUCT MESSAGE AFTER TAKEOFF FROM CVG. AIRCRAFT RETURNED TO CVG AND LANDED WITHOUT INCIDENT. INSPECTED FORWARD FUSELAGE LOOPS AND PERFORMED
- [SDR COMA0660490](https://openairdocs.org/sdr/COMA0660490), Aug 14, 2006: CIRCUIT BREAKER. MALFUNCTIONED. FLIGHT 5470 - DURING FLAP SELECTION FROM 8 DEGREES, RECEIVED 3B HYD PUMP CAUTION MESSAGE. CREW DECLARED AN EMERGENCY, LANDED WITHOUT INCIDENT. FOUND 3B CIRCUIT 
- [SDR COMA0660370](https://openairdocs.org/sdr/COMA0660370), Jun 1, 2006: FLAP. MALFUNCTIONED. FLIGHT 5480 - FLAP FAIL MESSAGE AFTER LANDING IN HSV, FAILED AT 20 DEGREES. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PAR
- [SDR COMA0660357](https://openairdocs.org/sdr/COMA0660357), May 23, 2006: FLAP. MALFUNCTIONED. FLIGHT 4997 - FLAP FAIL CAUTION MESSAGE WHILE IN CRUISE FLIGHT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION PARAGRAPH (B) 1,
- [SDR COMA0660353](https://openairdocs.org/sdr/COMA0660353), May 19, 2006: FLAP. MALFUNCTIONED. FLIGHT 5296 - DURING APPROACH RECEIVED FLAP FAIL MESSAGE AT 20 DEGREES, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. COMPLIED WITH AD 98-20-01
- [SDR COMA0660318](https://openairdocs.org/sdr/COMA0660318), Apr 30, 2006: CAUTION MESSAGE. ILLUMINATED. FLIGHT 5581 - FLAP FAIL CAUTION MESSAGE WHILE SITTING AT GATE. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT, MAINTENANCE ACTION, PARAGRAPH (B) 1, 
- [SDR COMA0660306](https://openairdocs.org/sdr/COMA0660306), Apr 17, 2006: FLAP SYSTEM. MALFUNCTIONED. FLIGHT 5199 - FLAP FAIL CAUTION MESSAGE CAME ON DURING TAXI. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (B) 1, 2
- [SDR COMA0560685](https://openairdocs.org/sdr/COMA0560685), Dec 12, 2005: FLAP SYSTEM. MALFUNCTIONED. FLIGHT 5130- DURING LANDING AT MSG RECEIVED A FLAP FAIL MESSAGE AT 45 DEGREES. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, 
- [SDR COMA0560544](https://openairdocs.org/sdr/COMA0560544), Oct 10, 2005: BATTERY. DISCHARGED. FLIGHT 5903 - EMERGENCY FLOOR LIGHTNING INOPERABLE ROWS 9 TO 13. REPLACED THE EMERGENCY BATTERY.
- [SDR COMA0560515](https://openairdocs.org/sdr/COMA0560515), Sep 21, 2005: BULKHEAD. CRACKED. WHILE PERFORMING TASK CRJ-2-162014, DETAILED INSPECTION OF THE PRESSURE BULKHEAD WEBS AND VERTICAL BEAMS AT FS 559.0, TWO CRACKS WERE DISCOVERED IN THE BULKHEAD
- [SDR COMA0560049](https://openairdocs.org/sdr/COMA0560049), Jan 11, 2005: CONTROLLER. MALFUNCTIONED. FLIGHT 5147 WING OVERHEAT MESSAGE. REPLACED THE CONTROLLER.
- [SDR COMA0560026](https://openairdocs.org/sdr/COMA0560026), Jan 3, 2005: CONNECTOR. DEFECTIVE. FLIGHT 5198, EMERGENCY FLOOR PATH LIGHTING INOP AT ROW 2 THRU 5. REPLACED WIRE CONNECTOR.
- [SDR COMA0460568](https://openairdocs.org/sdr/COMA0460568), Oct 3, 2004: SELECTOR VALVE. UNRELIABLE. FLIGHT 5994 GEAR DISAGREE WARNING. REPLACED THE NLG SELECTOR VALVE.
- [SDR COMA0460528](https://openairdocs.org/sdr/COMA0460528), Sep 11, 2004: RESERVOIR. INOPERATIVE. FLIGHT 5492 GEAR DISAGREE WARNING. REPLACED THE SYSTEM 3 HYDRAULIC RESERVOIR.
- [SDR COMA0460392](https://openairdocs.org/sdr/COMA0460392), Jun 28, 2004: COMPUTER. MALFUNCTIONED. FLIGHT 5546 STAB TRIM AND MACH TRIM CAUTION. RESET HSTCU, COULD NOT DUPLICATE, OPERATIONAL CHECK NORMAL.
- [SDR COMA0460011](https://openairdocs.org/sdr/COMA0460011), Jan 2, 2004: WARNING LIGHT. ILLUMINATED. FLIGHT 5682 RIGHT THRUST REVERSER UNLOCK INFLIGHT. SECURED AND DEFERRED MAINT PER MEL.
- [SDR COMA0360564](https://openairdocs.org/sdr/COMA0360564), Dec 18, 2003: WINDSHIELD. CRACKED. FLIGHT 5815 CO-PILOTS WINDSHIELD CRACKED. REPLACED WINDSHIELD.
- [SDR COMA0360537](https://openairdocs.org/sdr/COMA0360537), Dec 6, 2003: WIRE. LOOSE. THE AFT SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOP. SECURED LOOSE WIRING CONNECTION.
- [SDR COMA0360504](https://openairdocs.org/sdr/COMA0360504), Nov 13, 2003: FRAME. CRACKED. RT 718 FRAME FLANGE CRACKED BELOW STRINGER 10. REPAIRED FRAME IN ACCORDANCE WITH REO 601R-53-61-193.
- [SDR COMA0460314](https://openairdocs.org/sdr/COMA0460314), Nov 6, 2003: SKIN PANEL. CRACKED. PRESSURE FLOOR SKIN HAS CRACK AT FS 461.00. REPAIRED IN ACCORDANCE WITH REO 601R-53-41-102.
- [SDR COMA0360502](https://openairdocs.org/sdr/COMA0360502), Nov 6, 2003: FLOOR PANEL. CRACKED. PRESSURE FLOOR SKIN HAS CRACK AT FS 461.00. REPAIRED IN ACCORDANCE WITH REO 601R-53-41-102.
- [SDR COMA0360289](https://openairdocs.org/sdr/COMA0360289), Jun 24, 2003: IDG. MALFUNCTIONED. FLIGHT 5304 LEFT IDG CAUTION MESSAGE DURING T/O. DEFERRED MAINT PER MEL.
- [SDR COMA0260711](https://openairdocs.org/sdr/COMA0260711), Dec 12, 2002: POWER CABLE. INOPERATIVE. FLIGHT 5893 EMERGENCY FLOOR PATH LIGHTING IS INOP.REPLACED TRACK LIGHTING POWER STRIPS.
- [SDR COMA0260591](https://openairdocs.org/sdr/COMA0260591), Oct 15, 2002: LAMP. FLIGHT 5480 EMERGENCY FLOOR LIGHT AT ROW 3 IS INOP.DEFERRED MAINT PER MEL
- [SDR COMA0260538](https://openairdocs.org/sdr/COMA0260538), Sep 18, 2002: LAMP. FLIGHT 5284 1 SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOP.DEFERRED MAINT PER MEL.
- [SDR COMA0260501](https://openairdocs.org/sdr/COMA0260501), Aug 29, 2002: CART. A/C FUSELAGE STRUCK BY BAGGAGE CART AND SUSTAINED MAJOR DAMAGE BETWEEN F.S. 654 AND 672, AND STRINGERS 21L TO 23L.C/W REPAIR TO SKIN AND STRINGERS I/A/W SRM 53-
- [SDR COMA0260393](https://openairdocs.org/sdr/COMA0260393), Jun 28, 2002: SEAL. LEAKING. FLIGHT 5298 LEFT ENGINE OIL PRESSURE WARNING AFTER T/O, AIRCRAFT RETURNED TO MSP. (IFSD)REPLACED ACCESSORY GEAR BOX OIL SEALS AT AXIS D&F.
- [SDR COMA0260220](https://openairdocs.org/sdr/COMA0260220), Mar 31, 2002: DOOR. FLIGHT 5472 CABIN DOOR WARNING.COULD NOT DUPLICATE OPERATIONAL CHECK OF DOOR NORMAL. NO FAULT CODES IN COMPUTER.
- [SDR COMA0160825](https://openairdocs.org/sdr/COMA0160825), Oct 16, 2001: WINDOW. FRACTURED. FLIGHT 5903. PILOT'S SIDE WINDOW SHATTERED AT 29,000 FT.REPLACED THE PILOT'S SIDE WINDOW.
- [SDR COMA0160729](https://openairdocs.org/sdr/COMA0160729), Sep 14, 2001: ANGLE. CRACKED. LEFT SIDE INBOARD ANGLE AT F.S. 484.0 LBL 9 UNDER FLOOR PANEL 261CLF IS CRACKED.REPAIRED THE ANGLE AT FS 484.0 LBL9 I/A/W WVAC EO 601R-53-2711A.
- [SDR COMA0160728](https://openairdocs.org/sdr/COMA0160728), Sep 14, 2001: ANGLE. CRACKED. LEFT SIDE INBOARD ANGLE AT F.S. 484.0 LBL 27 UNDER FLOOR PANEL 261DLF IS CRACKED.REPAIRED THE ANGLE AT F.S. 484.0 LBL27 I/A/W WVAC EO 601R-53-2711A.
- [SDR COMA0160727](https://openairdocs.org/sdr/COMA0160727), Sep 14, 2001: ANGLE. CRACKED. RIGHT SIDE ELEVATER AND RUDDER PULLEY SUPPORT BRACKET AT F.S. 484.0 UNDER FLOOR PANEL 262DRF IS CRACKED.REPAIRED THE RIGHT SIDE ELEVATER AND RUDDER SUPPORT BRAC
- [SDR COMA0160708](https://openairdocs.org/sdr/COMA0160708), Sep 11, 2001: CAP. CHAFED. THE L/H AND R/H INBOARD FLAP LEADING EDGE INBOARD VANE CAPS ARE CHAFED WHERE THEY CONTACT THE TEFLON BUMPER PADS.REMOVED THE CHAFED INBOARD VANE CAPS. INSTALLED
- [SDR COMA0160707](https://openairdocs.org/sdr/COMA0160707), Sep 11, 2001: CAP. CHAFED. THE R/H INBOARD FLAP LEADING EDGE VANE CAP MIDDLE SKIN IS CHAFED WHERE THE FLAP CONTACTS THE TEFLON BUMPER PAD.REMOVED THE CHAFED MIDDLE VANE CAP. INSTALLED A N
- [SDR COMA0160706](https://openairdocs.org/sdr/COMA0160706), Sep 10, 2001: BUSHING. WORN. HORIZONTAL STABILIZER RHS VERTICLE BUSHING WORN.REMOVED R/H VERTICAL STAB BUSHING P/N 600-21061 INSTALLED NEW BUSHING ALT P/N 600-21061-7/SB I/A/W CRJ MM 20-26-
- [SDR COMA0160552](https://openairdocs.org/sdr/COMA0160552), Aug 5, 2001: WEB. CRACKED. ENGINE SUPPORT BEAM LOWER WEB CRACKED ON LEFT SIDE.PERFORMED A MAJOR REPAIR TO ENGINE SUPPORT BEAM LOWER NIB I/A/W CANADAIR REO 601R-53-61-366 REV C.
- [SDR COMA0160554](https://openairdocs.org/sdr/COMA0160554), Aug 5, 2001: WEB. CRACKED. ENGINE SUPPORT BEAM LOWER WEB CRACKED ON RIGHT SIDE.PERFORMED A MAJOR REPAIR TO ENGINE SUPPORT BEAM LOWER WEB I/A/W CANADAIR REO 601R-53-61-366 REV C.
- [SDR COMA0160553](https://openairdocs.org/sdr/COMA0160553), Aug 5, 2001: WEB. CRACKED. ENGINE SUPPORT BEAM IS CRACKED ON CENTER OF TOP WEB.PERFORMED A TEMPORARY MAJOR REPAIR TO CRACKED ENGINE SUPPORT BEAM I/A/W CANADAIR REO 601R-53-61-315 REV B.
- [SDR COMA0160210](https://openairdocs.org/sdr/COMA0160210), Feb 6, 2001: WARNING LIGHT. ILLUMINATED. FLAP FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE IAW AD 98-20-01.
- [SDR COMA0160128](https://openairdocs.org/sdr/COMA0160128), Jan 17, 2001: CARBON SEAL. LEAKING. LEFT ENGINE OIL PRESSURE FLUCTUATING BETWEEN 30 AND 48 PSI. REPLACED THE ACCESSORY DRIVES CARBON SEALS.
- [SDR COMA0160092](https://openairdocs.org/sdr/COMA0160092), Jan 8, 2001: BULB. BURNED OUT. EMERGENCY LIGHT AT ROW 5 IS INOP. REPLACED LIGHT BULB.
- [SDR COMA0061023](https://openairdocs.org/sdr/COMA0061023), Dec 7, 2000: WARNING SYSTEM. MALFUNCTIONED. STANDBY PITOT HEAT CAUTION MESSAGE. REPLACED THE NR 3 ADSHC.
- [SDR COMA0060897](https://openairdocs.org/sdr/COMA0060897), Nov 8, 2000: SEAL. DAMAGED. LOUD SQUEAL FROM CABIN DOOR AREA. REPAIRED DOOR SEAL NIB DAMAGE I/A/W REO 601R-5211-108.
- [SDR COMA0060868](https://openairdocs.org/sdr/COMA0060868), Nov 1, 2000: FRAME. DAMAGED. FRAME WEB DAMAGED AT FS 654.5 BETWEEN STRINGER 21B AND 22B LEFT HAND. CAUSED BY ELECTRICAL ARCING AT APU GROUND CABLE (N1232) . REMOVED DAMAGED FRAME SECTION AN
- [SDR COMA0060874](https://openairdocs.org/sdr/COMA0060874), Oct 28, 2000: BATTERY. DISCHARGED. APU BATTERY AT ZERO VOLTS, APU BATTERY CHARGER IS INTERMITTENT. APU GROUND CABLE ARCHING AT GROUND STUD N1232, WHICH CAUSED SUBSTANTIAL DAMAGE AT FRAME 654.5. R
- [SDR COMA0060792](https://openairdocs.org/sdr/COMA0060792), Oct 2, 2000: CONNECTOR. LOOSE. SEVERAL EMERGENCY LIGHTS AND SIGNS ARE INOP, FWD CABIN AREA. SECURED LOOSE CONNECTION AT FLOOR TRACK LIGHTING.
- [SDR COMA0060754](https://openairdocs.org/sdr/COMA0060754), Sep 15, 2000: TRANSDUCER. FAILED. STALL FAIL CAUTION MESSAGE DURING TAKEOFF, AIRCRAFT RETURNED TO THE GATE. REPLACED THE NR 1 AOA TRANSDUCER.
- [SDR COMA0060720](https://openairdocs.org/sdr/COMA0060720), Sep 10, 2000: ANGLE. CORRODED. THE FWD J ANGLE AT FS 280 BETWEEN LBL 9.0 AND RBL 9.0 IS CORRODED. PERFORMED A MAJOR REPAIR BY REPLACING CORRODED FWD J ANGLE AT FS 280 BETWEEN LBL 9.0 AND RBL 
- [SDR COMA0060719](https://openairdocs.org/sdr/COMA0060719), Sep 10, 2000: FLOORBEAM. DAMAGED. THE OUTBOARD FLANGE OF THE BEAM AT RBL 9.0 AND FS 409 + 8 WAS PREVIOUSLY REPAIRED. THIS EO PROVIDES FOR MODIFYING THE SPLICE ANGLE TO ACCOMODATE THE REPAIR. PER
- [SDR COMA0060718](https://openairdocs.org/sdr/COMA0060718), Sep 10, 2000: FLOORBEAM. DAMAGED. DURING ACCOMPLISHMENT OF SB 601R-53-037 REV A, THE I/B FLANGE OF THE FLOORBEAM AT RBL 27.0 FS 409 + 8 WAS FOUND TO HAVE A PREVIOUS REPAIR. PERFORMED A MAJOR REP

All 90: https://openairdocs.org/deregistered/N949CA-2007-10-19/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 20020628021019I](https://openairdocs.org/incident/20020628021019I), Jun 28, 2002: Cndair CL6002B19 (N949CA), Minneapolis, MN. (-23) After takeoff from Minneapolis, Minnesota, the crew noticed a flucuation on the left engine oil pressure gauge. The power on the left engine was reduced…

## Other aircraft with N949CA

- [Registered now](https://openairdocs.org/aircraft/N949CA): Costruzioni Aeronautiche Tecna P2012 TRAVELLER, S/N 016/US, built 2020
- [Cancelled 2014-03-26](https://openairdocs.org/deregistered/N949CA-2014-03-26): Boeing 747-428, S/N 25630. First renewal notice. Owner: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)

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