# N785CA: 1999 Bombardier CL-600-2B19, registration cancelled 2012-12-14

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 14, 2012
- Exported to: South Africa
- Status when cancelled: Valid registration
- Airframe: [Bombardier CL-600-2B19](https://openairdocs.org/model/bombardier-cl-600-2b19) (registry code 1390008)
- 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: 7326
- Year built: 1999
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 15, 1999
- Certificate issued: October 31, 2007
- Last registry action: August 9, 2012
- Mode S code: AAA34C
- Owner when cancelled: [Wilmington Trust Company Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20COMPANY%20TRUSTEE)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N785CA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=785CA
- Page: https://openairdocs.org/deregistered/N785CA-2012-12-14

From the FAA registry file of October 31, 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 Bombardier CL-600-2B19: https://openairdocs.org/model/bombardier-cl-600-2b19.md

## Service difficulty reports (63, newest 50)

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

- [SDR COMA2011101050077](https://openairdocs.org/sdr/COMA2011101050077), Oct 9, 2011: CONNECTOR. DEFECTIVE. ON APPROACH INTO CVG RECEIVED LEFT I/B ANTI-SKID CAUTION MSG, FOLLOWED QRH. EMERGENCY DECLARED, A/C LANDED SAFELY IN CVG. REPINNED LEFT I/B ANTI-SKID TRANSDUCER
- [SDR COMA2011041850036](https://openairdocs.org/sdr/COMA2011041850036), Apr 17, 2011: DRAG ANGLE. CRACKED. PAX DOOR AFT DRAG ANGLE IS CRACKED. REMOVED AND REPLACED DAMAGED SECTION OF DRAG ANGLE IAW SRM 51-42-13 AND 51-42-22.
- [SDR COMA2011041550035](https://openairdocs.org/sdr/COMA2011041550035), Apr 15, 2011: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT, FS 280, LBL 9 - RBL 9. REPAIRED FS 280 FLOOR SUPPORT ANGLE BY CUTTING OUT CORRODED SECTION AND SPLICING A REPAIR SECTION IAW REO 601
- [SDR COMA2011041150034](https://openairdocs.org/sdr/COMA2011041150034), Apr 9, 2011: ANGLE. CRACKED. CRACK INDICATION IN RADIUS OF LEFT FS 559 CAP ANGLE AT LBL 9 AND LBL 18. REPAIRED LEFT FS 559 CAP ANGLE AT LBL 9 AND LBL 18 IAW REO 601R-53-41-260 LT REP.
- [SDR COMA2011040850033](https://openairdocs.org/sdr/COMA2011040850033), Apr 8, 2011: ANGLE. CRACKED. FS 559 LOWER CAP ANGLE IS CRACKED AT RBL 9 AND RBL 18. REMOVED AND REPLACED DAMAGED SECTION OF 559 CAP ANGLE IAW REO 601R-53-41-260 RT REP.
- [SDR COMA2011040850032](https://openairdocs.org/sdr/COMA2011040850032), Apr 8, 2011: BULKHEAD. CRACKED. FS 202 BULKHEAD IS CRACKED AT THE PARKING BRAKE CABLE CUTOUT. REPAIRED FS 202 BULKHEAD IAW REO601R53-11-563 REPAIR 2, REV-A, DATED 2011/04/04 AND DEVIATION REO6
- [SDR COMA2011040850031](https://openairdocs.org/sdr/COMA2011040850031), Apr 8, 2011: WEB. CRACKED. FS 559.00 RBL 18, WL 59.10, WEB CRACKED ADJACENT TO DOME NUT. REPAIRED FS 559 WEB AT RBL 18 BY CUTTING OUT DAMAGE AND INSTALLING A DOUBLER IAW REO 601R-53-41-26
- [SDR COMA2009121650229](https://openairdocs.org/sdr/COMA2009121650229), Dec 15, 2009: BULKHEAD. CRACKED. FOUND REAR PRESSURE BULKHEAD CRACKED AROUND LINTEL ATTACHMENT FITTING. REPAIRED CRACK ON REAR PRESSURE BULKHEAD AT LINTEL FITTING IAW REO 601R-53-61-1230 AND RE
- [SDR COMA2009121650228](https://openairdocs.org/sdr/COMA2009121650228), Dec 15, 2009: BULKHEAD. CRACKED. FOUND REAR PRESSURE BULKHEAD CRACKED ABOVE CARGO DOOR TRACK. REPAIRED CRACK ABOVE CARGO DOOR TRACK IAW REO 601R-53-61-1541.
- [SDR COMA2009010750059](https://openairdocs.org/sdr/COMA2009010750059), Jan 6, 2009: FUEL CONTROL. FAILED. ON APPROACH, NR2 ENGINE ROLLED BACK TO SHUTDOWN WHILE BEING VECTORED FOR THE APPROACH. EMERGENCY DECLARED, ACFT LANDED SAFELY. REMOVED AND REPLACED RT ENGINE FU
- [SDR COMA2009010750058](https://openairdocs.org/sdr/COMA2009010750058), Jan 6, 2009: PUMP. FAILED. ON APPROACH, NR 2 ENGINE ROLLED BACK TO SHUTDOWN WHILE BEING VECTORED FOR THE APPROACH. EMERGENCY DECLARED, ACFT LANDED SAFELY. REMOVED AND REPLACED RT ENG FUEL
- [SDR COMA2008121750033](https://openairdocs.org/sdr/COMA2008121750033), Dec 12, 2008: SUPPORT BEAM. CRACKED. ENGINE CENTER SUPPORT BEAM IS CRACKED AT RBL 8.5 AT SENSING LOOP SUPPORT BRACKET. REPAIRED ENGINE SUPPORT BEAM PER CRJ REO 601R-53-61345 REV F.
- [SDR COMA2008121750032](https://openairdocs.org/sdr/COMA2008121750032), Dec 12, 2008: SKIN. DAMAGED. LT WING LOWER DRAIN ATTACHMENT HOLE JUST FWD OF PANEL 540 AB, AT WS 67.75 AFT SCREW HOLE IS DAMAGED. REPAIRED DAMAGE PER EA 10-57-02437.
- [SDR COMA2008121750031](https://openairdocs.org/sdr/COMA2008121750031), Dec 12, 2008: SKIN. DAMAGED. LT WING LOWER DRAIN ATTACHMENT HOLE JUST AFT OF PANEL 510 AB, BETWEEN WS 0.00 AND WS 22.50, AFT SCREW HOLE IS DAMAGED. REPAIRED DAMAGE PER EA 10-57-02437.
- [SDR COMA2008121750030](https://openairdocs.org/sdr/COMA2008121750030), Dec 12, 2008: SKIN. DAMAGED. RT WING LOWER DRAIN ATTACHMENT HOLE JUST FWD OF PANEL 640 DB AT WS 85.50 AFT SCREW HOLE IS DAMAGED. REPAIRED DAMAGE PER EA10-57-02437.
- [SDR COMA2008121750029](https://openairdocs.org/sdr/COMA2008121750029), Dec 12, 2008: SKIN. DAMAGED. LT WING LOWER DRAIN ATTACHMENT HOLES JUST FWD OF PANEL 540AB AT WS.0.00, FWD AND AFT SCREW HOLES ARE DAMAGED. REPAIRED DAMAGE PER EA10-57-02437.
- [SDR COMA0860277](https://openairdocs.org/sdr/COMA0860277), Jun 9, 2008: CHECK VALVE. FAILED. DURING CLIMBOUT FROM CVG RT ENG HIGH OIL TEMP. EMERGENCY DECLARED, ACFT RETURNED BACK TO CVG AND LANDED SAFELY. FOUND RT ENG AGB OVER SERVICED WITH OIL. REMOVED
- [SDR COMA0760694](https://openairdocs.org/sdr/COMA0760694), Dec 5, 2007: SECU. FAULTY. FLIGHT 5151 - ON TAKEOFF ROLL RECEIVED CONFIG SPOILERS MESSAGE WITH FLIGHT SPOILER MESSAGE. ABORTED TAKEOFF AND RETURNED TO GATE SAFELY. REMOVED AND REPLACED NR
- [SDR COMA0760595](https://openairdocs.org/sdr/COMA0760595), Oct 5, 2007: TRANSDUCER. FAULTY. FLIGHT 5350 - RECEIVED STEERING INOP CAUTION. RAN QRH, DIVERTED TO PHL, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. A/C WAS TUGGED FROM RUNWAY. REPLACED RIGHT 
- [SDR COMA0760582](https://openairdocs.org/sdr/COMA0760582), Sep 23, 2007: BPSU. FAULTY. FLIGHT 5699 - RECEIVED FLAP CAUTION MESSAGE. LANDED WITHOUT INCIDENT. REPLACED LEFT BPSU. NO FURTHER DEFECTS.
- [SDR COMA0760272](https://openairdocs.org/sdr/COMA0760272), Mar 20, 2007: SERVO. FAULTY. FLIGHT 5042 - AFTER TAKEOFF ENGAGED AUTO PILOT AT 12000 FT, AT 20000 FT FELT SLIGHT VIBRATION AND YAW MOTION. EICAS SHOWED AILERON FLUTTERING. REPLACED AILERON 
- [SDR COMA0760195](https://openairdocs.org/sdr/COMA0760195), Feb 17, 2007: WINDSHIELD. FAILED. FLIGHT 5284 - F/O WINDSHIELD CRACKED. REMOVED AND REPLACED RIGHT WINDSHIELD.
- [SDR COMA0760073](https://openairdocs.org/sdr/COMA0760073), Jan 26, 2007: PDU. FAULTY. FLIGHT 5206 - RECEIVED FLAP FAIL MESSAGE AT 8 DEGREES. LANDED WITHOUT INCIDENT. REPLACED PDU.
- [SDR COMA0660159](https://openairdocs.org/sdr/COMA0660159), Feb 18, 2006: FLAP. MALFUNCTIONED. FLIGHT 5011 - DURING YUL APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION PARAGRAP
- [SDR COMA0660122](https://openairdocs.org/sdr/COMA0660122), Feb 8, 2006: AMPLIFIER. FAULTY. FLIGHT 9495 - AFTER TAKEOFF AND DURING CLIMBOUT OF CVG ENCOUNTERED SURGING OF LEFT ENGINE N1 AND N2, FLIGHT RETURNED TO CVG. REPLACED THE LEFT SPEED CONTROL AMP
- [SDR COMA0560722](https://openairdocs.org/sdr/COMA0560722), Dec 13, 2005: CONNECTOR. LOOSE. FLIGHT 5852 - RT THRUST REVERSER WARNING. SECURED CANNON PLUGS ON THE STOW, DEPLOY AND PDU SWITCHES. OPERATIONAL CHECKS NORMAL.
- [SDR COMA0550382](https://openairdocs.org/sdr/COMA0550382), Jul 6, 2005: VENT. OBSTRUCTED. FLIGHT 5811- CABIN ALTITUDE CAUTION. F/A REPORTS LOUD SQUEAL FROM CABIN DOOR. FOUND DOOR TRIM OBSTRUCTING THE DOOR VENT VALVE, SECURED TRIM. PRESSURE CHECKS SAT
- [SDR COMA0560346](https://openairdocs.org/sdr/COMA0560346), Jun 11, 2005: GEARBOX. CRACKED. WHEN PERFORMING EO 76-011 AD, THE RIGHT ENGINE THROTTLE GEARBOX HOUSING WAS FOUND CRACKED AT THE ATR ATTACH POINT. REMOVED AND INSTALLED A SERVICABLE GEARBOX.
- [SDR COMA0560224](https://openairdocs.org/sdr/COMA0560224), Apr 3, 2005: VALVE. FAULTY. FLT 5372 RECEIVED A LT ENGINE COWL CAUTION DURING CRUISE FLIGHT (IND-JFK), AIRCRAFT DIVERTED TO CVG. REPLACED THE LT ENGINE ANTI-ICE COWL VALVE.
- [SDR COMA0560125](https://openairdocs.org/sdr/COMA0560125), Feb 11, 2005: CONTROL HANDLE. MALFUNCTIONED. FLIGHT 4961 FLAPS FAIL CAUTION. REPLACED THE FLAP CONTROL HANDLE.
- [SDR COMA0560047](https://openairdocs.org/sdr/COMA0560047), Jan 11, 2005: APU. SMOKE. FLIGHT 5834 APU SMELLED LIKE FUEL, SMOKE COMING FROM INTAKE. COULD NOT DUPLICATE. INSPECTED APU FOR FUEL LEAKS. NO DEFECTS FOUND.
- [SDR COMA0560006](https://openairdocs.org/sdr/COMA0560006), Dec 23, 2004: SKIN. DAMAGED. LOWER NOSE SKIN DAMAGED FORWARD OF FS 280 BETWEEN STRINGERS 25R AND 26R. REPAIRED IAW EA 10-5310-00515.
- [SDR COMA0560005](https://openairdocs.org/sdr/COMA0560005), Dec 23, 2004: SKIN. CRACKED. LOWER LEFT HAND WING PLANK CRACK INBOARD OF WS 149.85. REPAIRED IAW REO 601R-57-21-539.
- [SDR COMA0560004](https://openairdocs.org/sdr/COMA0560004), Dec 22, 2004: FRAME. CRACKED. LEFT HAND FUSELAGE 718 CRACKED BETWEEN STRINGER 10 AND 12. REPAIRED IAW EO 53-027.
- [SDR COMA0560003](https://openairdocs.org/sdr/COMA0560003), Dec 22, 2004: FRAME. CRACKED. RIGHT HAND 718 FRAME CRACKED. REPAIRED IAW EO 53-027.
- [SDR COMA0560002](https://openairdocs.org/sdr/COMA0560002), Dec 22, 2004: ANGLE. CORRODED. FS 280 IS CORRODED ON FORWARD AFT ANGLES AFT OF CREW ENTRY WAY. REPAIRED IAW REO 601R-53-11-584.
- [SDR COMA0560001](https://openairdocs.org/sdr/COMA0560001), Dec 22, 2004: FRAME. CRACKED. LEFT HAND FS FRAME 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117.
- [SDR COMA0460463](https://openairdocs.org/sdr/COMA0460463), Aug 12, 2004: DETECTOR. MALFUNCTIONED. FLIGHT 5731, CARGO SMOKE WARNING. COULD NOT DUPLICATE. FOUND NO DEFECTS, REPLACED DISCHARGED FIRE BOTTLES
- [SDR COMA0460237](https://openairdocs.org/sdr/COMA0460237), Mar 30, 2004: HYDRAULIC LINE. LEAKING. FLIGHT 5291 NR 1 HYDRAULIC SYSTEM LOW PRESSURE WARNING, RESERVOIR INDICATED EMPTY. REPLACED HYDRAULIC SUCTION LINE IN AFT EQUIP BAY.
- [SDR COMA0360456](https://openairdocs.org/sdr/COMA0360456), Oct 14, 2003: ELEMENT. CHAFED. FLIGHT 5808 LEFT 14TH STAGE BLEED LEAK WARNING. REPLACED BLEED LEAK SENSING ELEMENT IN PYLON.
- [SDR COMA0360294](https://openairdocs.org/sdr/COMA0360294), Jun 25, 2003: CONTROLLER. MALFUNCTIONED. FLIGHT 5129 WING OVERHEAT WARNING DURING T/O. REPLACED THE ANTI-ICE CONTROLLER.
- [SDR COMA0360290](https://openairdocs.org/sdr/COMA0360290), Jun 24, 2003: WARNING LIGHT. ILLUMINATED. FLIGHT 5298 WING OVERHEAT MESSAGE DURING T/O. DEFERRED MAINT PER MEL.
- [SDR COMA0360012](https://openairdocs.org/sdr/COMA0360012), Dec 31, 2002: COMPUTER. FLIGHT 5295 NWS CAUTION MESSAGE AFTER T/O.COULD NOT DUPLICATE. SYSTEM TEST NORMAL.
- [SDR COMA0260559](https://openairdocs.org/sdr/COMA0260559), Oct 3, 2002: COMPUTER. MALFUNCTIONED. FLIGHT 5708 WHEN FLIGHT SPOILERS DEPLOYED, AIRCRAFT ROLLED TO LEFT.REPLACED THE #2 SECU.
- [SDR COMA0260012](https://openairdocs.org/sdr/COMA0260012), Dec 29, 2001: CONTROL BOX. MALFUNCTIONED. FLIGHT 5648 L/H PITOT HEAT CAUTION MESSAGE.REPLACED THE #1 ADSHC.
- [SDR COMA0160793](https://openairdocs.org/sdr/COMA0160793), Oct 4, 2001: ACTUATOR. FAILED. FLIGHT 5420. FLAPS FAILED AT 23 DEGREES DURING LANDING APPROACH. POST FLIGHT INSP. FOUND R/H OUTBD FLAP TWISTED.REPLACED THE R/H OUTBD FLAP, BOTH FLAP ACTUATORS
- [SDR COMA0160663](https://openairdocs.org/sdr/COMA0160663), Sep 1, 2001: SENSOR. FAULTY. FLIGHT #5725. DURING CRUISE FLIGHT RECEIVED A FLAP SYSTEM FAIL CAUTION WITH FLAP AT ZERO DEGREE POSITION, CREW DECLARED AN EMERGENCY AND LANDED AT DESTINATION C
- [SDR COMA0160613](https://openairdocs.org/sdr/COMA0160613), Aug 20, 2001: LIGHT. FLIGHT #N/A. EMERGENCY CEILING LIGHT AT ROW 13 IS INOPERATIVE.REPLACED THE EMERGENCY FLOOD LIGHT BULB AT ROW 13.
- [SDR COMA0160534](https://openairdocs.org/sdr/COMA0160534), Jul 27, 2001: LIGHT. INOPERATIVE. LEFT HAND EMERGENCY LIGHT IS INOPERABLE. REPLACED THE LIGHT BULB.
- [SDR COMA0160300](https://openairdocs.org/sdr/COMA0160300), Mar 4, 2001: POWER UNIT. MALFUNCTIONED. FLAPS FAIL CAUTION MESSAGE. REPLACED THE PDU.

All 63: https://openairdocs.org/deregistered/N785CA-2012-12-14/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 CHI01IA073](https://openairdocs.org/ntsb/CHI01IA073), Jan 25, 2001: Canadair CL-600-2B19 (N785CA), Grand Rapids, MI, incident, minor damage. Probable cause: The uncommanded deployment of the right flight spoiler due to the fatigue fracture of the spoiler lug.

## 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 20010125000639I](https://openairdocs.org/incident/20010125000639I), Jan 25, 2001: Cndair CL6002B19 (N785CA), Grand Rapids, MI. (-23) While on approach to the gerald ford international airport, Grand Rapids, MI, conair flight #5689, a Bombardier CL-600-2B19, experienced a rapid roll to…

## Other aircraft with N785CA

- [Registered now](https://openairdocs.org/aircraft/N785CA): Costruzioni Aeronautiche Tecna P2012 TRAVELLER, S/N 021/US, built 2020

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