# N712CA: 1998 Bombardier CL-600-2B19, registration cancelled 2013-07-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 16, 2013
- Status when cancelled: First renewal notice
- 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: 7244
- Year built: 1998
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 26, 1998
- Certificate issued: February 23, 2010
- Last registry action: February 23, 2010
- Mode S code: A983AE
- Owner when cancelled: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%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/N712CA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=712CA
- Page: https://openairdocs.org/deregistered/N712CA-2013-07-16

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 Bombardier CL-600-2B19: https://openairdocs.org/model/bombardier-cl-600-2b19.md

## Service difficulty reports (73, newest 50)

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

- [SDR COMA2010010650009](https://openairdocs.org/sdr/COMA2010010650009), Jan 5, 2010: SKIN. CRACKED. LEFT LOWER WING PLANK DRAIN VALVE ATTACH HOLE SHOWS DEFECT INDICATION AT WS 65.75, STRINGER 15. OVERSIZED SCREW HOLE TO REMOVE DEFECTS AND INSTALLED A FREEZE PL
- [SDR COMA2010010650008](https://openairdocs.org/sdr/COMA2010010650008), Jan 5, 2010: SKIN. GOUGED. LEFT LOWER WING PLANK DRAIN VALVE ATTACH HOLE SHOWS DEFECT INDICATION AT WS 0.0, STRINGER 15. OVERSIZED SCREW HOLE TO REMOVE DEFECTS AND INSTALLED A FREEZE PLUG
- [SDR COMA20100650007](https://openairdocs.org/sdr/COMA20100650007), Jan 5, 2010: SKIN. CRACKED. RIGHT LOWER WING PLANK DRAIN VALVE ATTACH HOLE SHOWS DEFECT INDICATION AT WS 65.75, STRINGER 15. OVERSIZED SCREW HOLE TO REMOVE DEFECTS AND INSTALLED A FREEZE P
- [SDR COMA2010010650006](https://openairdocs.org/sdr/COMA2010010650006), Jan 5, 2010: SKIN. DAMAGED. RIGHT LOWER WING PLANK DRAIN VALVE ATTACH HOLE SHOWS DEFECT INDICATION AT WS 0.0, STRINGER 5. OVERSIZED SCREW HOLE TO REMOVE DEFECTS AND INSTALLED A FREEZE PLUG
- [SDR COMA0860322](https://openairdocs.org/sdr/COMA0860322), Jul 13, 2008: LAMP. BURNED OUT. FLIGHT 5416. GALLEY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMPS. (A)
- [SDR COMA0760741](https://openairdocs.org/sdr/COMA0760741), Dec 21, 2007: BULKHEAD. CRACKED. DURING HMV-5 INSPECTION EDDY CURRENT OF AFT PRESSURE BULKHEAD, FOUND 3 CRACKS AROUND LINTEL ATTACHMENT FITTING. REPAIRED CRACKS TO AFT PRESSURE BULKHEAD AROUND 
- [SDR COMA0760737](https://openairdocs.org/sdr/COMA0760737), Dec 19, 2007: STIFFENER. CRACKED. DURING HMV-5 INSPECTION, FOUND CRACK AT LOWER END OF VERTICAL STIFFENER. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW BOMBARDIER REO 601R-53-41-056. 
- [SDR COMA0760734](https://openairdocs.org/sdr/COMA0760734), Dec 18, 2007: BEAM. CRACKED. CABIN FLOOR LATERAL BEAM CRACKED ON LOWER FLANGE. COMPLIED WITH REO601R-53-11-1308 BY CUTTING OUT DAMAGE AND APPLYING DOUBLER.
- [SDR COMA0760733](https://openairdocs.org/sdr/COMA0760733), Dec 18, 2007: WEB. CRACKED. DURING 559 EDDY CURRENT INSPECTION FOUND A CRACK ON THE 559 WEB. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW SR10-5341-001 REV A SECTION 1 PERMANENT REPAIR.
- [SDR COMA0760730](https://openairdocs.org/sdr/COMA0760730), Dec 17, 2007: STIFFENER. CRACKED. DURING 559 INSPECTION FOUND .6 INCH CRACK ON INBOARD SIDE AND .8 INCH CRACK AT OUTBOARD SIDE OF VERTICAL STIFFENERS. REMOVED DAMAGE AND INSTALLED DOUBLERS PER B
- [SDR COMA0760711](https://openairdocs.org/sdr/COMA0760711), Dec 11, 2007: ATTACH FITTING. CRACKED. LONGITUDINAL FLOORBEAM ATTACH CLIP CRACKED AND HAS LOOSE FASTENERS, INBOARD SIDE OF BEAM FS 280, LBL 9. REMOVED AND REPLACED CLIP IAW CRJ SRM 51-42-21. 
- [SDR COMA0760710](https://openairdocs.org/sdr/COMA0760710), Dec 11, 2007: ATTACH FITTING. CRACKED. LONGITUDINAL FLOORBEAM ATTACH CLIP CRACKED FS 280, LBL 10 OUTBOARD SIDE OF BEAM. REMOVED AND REPLACED CLIP IAW CRJ SRM 51-42-21.
- [SDR COMA0760534](https://openairdocs.org/sdr/COMA0760534), Aug 20, 2007: LIGHT. INOPERATIVE. FLIGHT 5425 - EMERGENCY LIGHT ON CEILING BY LAV INOP. REMOVED AND REPLACED LAMP.
- [SDR COMA0760441](https://openairdocs.org/sdr/COMA0760441), Jun 18, 2007: SEAL. MISSING. FLIGHT 4945 - EN ROUTE CVG-OKC RECEIVED A LEFT ENGINE OIL PRESSURE FLUCTUATION WITH INTERMITTENT OIL PRESSURE WARNING. CREW DECLARED AN EMERGENCY AND FLIGHT RET
- [SDR COMA0760289](https://openairdocs.org/sdr/COMA0760289), Mar 26, 2007: PROXIMITY SENSOR. OUT OF ADJUST. FLIGHT 5598 - RECEIVED GEAR DISAGREE WARNING AFTER TAKEOFF. RETURNED TO SAV AND LANDED WITHOUT INCIDENT. FOUND MLG UPLOCK PROXIMITY SENSOR OUT OF ADJUSTMENT AND
- [SDR COMA0760042](https://openairdocs.org/sdr/COMA0760042), Jan 19, 2007: DRAIN LINE. FAILED. FLIGHT 5385- HYD SYS NR 2 LOW PRESS (SYS QTY SHOWED 5 PERCENT) A/C DIVERTED TO RIC AND LANDED SAFELY. REMOVED AND REPLACED HYD SYS NR 2 CASE DRAIN TUBE ASSY.
- [SDR COMA0660388](https://openairdocs.org/sdr/COMA0660388), Jun 11, 2006: PSEU. MALFUNCTIONED. FLIGHT 5885 - DURING TAKEOFF ROLL RECEIVED A PROXIMITY SYSTEM FAULT MESSAGE, CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. PERFORMED SYSTEM TEST ON PSEU, DISCR
- [SDR COMA0660338](https://openairdocs.org/sdr/COMA0660338), May 10, 2006: CAUTION MESSAGE. FALSE ACTIVATION. FLIGHT 5500 - DURING TAKEOFF ROLL RECEIVED A RIGHT AIR CONDITIONING PACK HIGH PRESSURE CAUTION, ABORTED TAKEOFF AND RETURNED TO THE GATE. PERFORMED AN OPERATION
- [SDR COMA0660263](https://openairdocs.org/sdr/COMA0660263), Mar 18, 2006: STRUT. WORN. FLIGHT 5057 - AFTER TAKEOFF FROM DAY RECEIVED A GEAR DISAGREE/NOSE DOOR OPEN MESSAGE, FLIGHT RETURNED TO THE FIELD. REPLACED THE NLG STRUT LOWER CYLINDER.
- [SDR COMA0560730](https://openairdocs.org/sdr/COMA0560730), Dec 16, 2005: TARGET. BENT. FLIGHT 5463 - NLG WILL NOT RETRACT. NLG CENTERED, PROX SWITCH TARGET BENT. C/W TEMPORARY REPAIR TO PROX SWITCH TARGET.
- [SDR COMA0560436](https://openairdocs.org/sdr/COMA0560436), Aug 9, 2005: PUMP. FAILED. FLIGHT 4998 - NR 2 HYDRAULIC SYSTEM HIGH TEMP AND LOW PRESSURE WARNING. REPLACED THE RT ENGINE HYDRAULIC PUMP.
- [SDR COMA0560371](https://openairdocs.org/sdr/COMA0560371), Jun 30, 2005: STRUT. UNDERSERVICED. GEAR DISAGREE. SERVICED NLG SHOCK STRUT, GEAR SWINGS SATISFACTORY.
- [SDR COMA0460679](https://openairdocs.org/sdr/COMA0460679), Dec 13, 2004: LIGHT. INOPERATIVE. FLIGHT 5309 RT OVERWING EMERGENCY LIGHT IS INOP. REPLACED LIGHT BULB.
- [SDR COMA0460588](https://openairdocs.org/sdr/COMA0460588), Oct 28, 2004: HANDLE. UNSECURE. FLIGHT 5812 CABIN DOOR HANDLE CAUTION MESSAGE. FOUND DOOR HANDLE NOT STOWED. OPERATIONAL CHECK OF DOOR SATISFACTORY. NO DEFECTS FOUND.
- [SDR COMA0460427](https://openairdocs.org/sdr/COMA0460427), Jul 19, 2004: ACM. MALFUNCTIONED. FLIGHT 5888 RT AC PACK HIGH PRESSURE CAUTION. COULD NOT DUPLICATE. AIR CONDITION SYSTEM OPERATES NORMAL.
- [SDR COMA0460408](https://openairdocs.org/sdr/COMA0460408), Jul 11, 2004: SHUTOFF VALVE. MALFUNCTIONED. FLIGHT 5724 PARKING BRAKE SOV CAUTION MESSAGE. REPLACED THE PARKING BRAKE SOV.
- [SDR COMA0460405](https://openairdocs.org/sdr/COMA0460405), Jul 2, 2004: TRANSDUCER. MALFUNCTIONED. FLIGHT 5282 RIGHT ENGINE OIL PRESSURE WARNING DURING T/O. REPLACED THE OIL PRESSURE TRANSDUCER.
- [SDR COMA0460004](https://openairdocs.org/sdr/COMA0460004), Dec 30, 2003: CONTROL UNIT. FAILED. FLIGHT 5073 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU.
- [SDR COMA0360575](https://openairdocs.org/sdr/COMA0360575), Dec 19, 2003: SKIN. CORRODED. FRETTING DAMAGE ON LEFT HAND LOWER WING PLANK FUEL ACCESS HOLE CUTOUT AT 550EB. BLENDED DAMAGE OUT AND ROTO-PEENED AFT OUTBAORD HATCHED AREA IN ACCORDANCE WITH 
- [SDR COMA0360499](https://openairdocs.org/sdr/COMA0360499), Nov 15, 2003: SEAL. LEAKING. FLIGHT 5803 RT ENGINE LOST OIL PRESSURE IFSD. REPLACED THE RT ACCESSORY GEAR BOX OIL SEALS.
- [SDR COMA0360466](https://openairdocs.org/sdr/COMA0360466), Oct 22, 2003: THRUST REVERSER. UNLOCKED. FLIGHT 5141 RIGHT THRUST REVERSER UNLOCKED CAUTION DURING TAKEOFF. SECURED AND DEFERRED MAINTENANCE ON THRUST REVERSER PER MEL.
- [SDR COMA0360373](https://openairdocs.org/sdr/COMA0360373), Aug 17, 2003: RESERVOIR. OVERTEMP. FLIGHT 9457 NR 2 HYDRAULIC SYSTEM HIGH TEMP CAUTION. REPLACED THE NR 2 HYDRAULIC RESERVOIR.
- [SDR COMA0360329](https://openairdocs.org/sdr/COMA0360329), Jul 18, 2003: AILERON. BINDING. FLIGHT 5378 CREW REPORTED "AILERONS BINDING". COULD NOT DUPLICATE - NO AILERON BINDING NOTED - C/W COMAIR EO 27-075 FOR TROUBLESHOOTING.
- [SDR COMA0360265](https://openairdocs.org/sdr/COMA0360265), Jun 10, 2003: PCU. MALFUNCTIONED. FLIGHT 5686 UNCONTROLLED MOMENTARY ROLL DURING CRUISE FLIGHT, FOLLOWED BY SPOILERONS FAULT MESSAGE. REPLACED THE RT INBOARD SPOILERON PCU.
- [SDR COMA0360006](https://openairdocs.org/sdr/COMA0360006), Jan 4, 2003: COUPLING. FLIGHT 5239 LEFT 14TH STAGE BLEED AIR DUCT WARNING.TIGHTENED LOOSE BLEED AIR COUPLING AT THE T/R PDU
- [SDR COMA0360011](https://openairdocs.org/sdr/COMA0360011), Dec 31, 2002: ENGINE. FLIGHT 5848 LEFT ENG FAN VIB WARNING, ITT IN RED. IFSDREPLACED THE LEFT ENGINE.
- [SDR COMA0260463](https://openairdocs.org/sdr/COMA0260463), Jul 30, 2002: DOOR. FLIGHT 5575 CABIN DOOR OUTER HANDLE CAUTION MESSAGE.COULD NOT DUPLCITE. OPERATION OF CABIN DORO NORMAL.
- [SDR COMA0260343](https://openairdocs.org/sdr/COMA0260343), May 30, 2002: APU. FLIGHT 5275 SMOKE IN CABIN AND COCKPIT WHEN BLEEDS SOURCE SELECTED TO APU.PLACED APU ON DEFERRED MAINT LIST PER MEL.
- [SDR COMA0260282](https://openairdocs.org/sdr/COMA0260282), Apr 23, 2002: WIRE. FLIGHT 5966 LEFT ENGINE OIL PRESSURE WARNING.REPAIRED CHAFED WIRE AT OIL PRESSURE SWITCH.
- [SDR COMA0260234](https://openairdocs.org/sdr/COMA0260234), Apr 5, 2002: COMPUTER. MALFUNCTIONED. FLIGHT 5635 UNCOMMANDED RUDDER OSCILLATIONS.REPLACED THE #2 DCU.
- [SDR COMA0160936](https://openairdocs.org/sdr/COMA0160936), Dec 1, 2001: DOUBLER. CRACKED. THE L/H SIDE FRAME AND AFT DOUBLER AT FS718.0 WERE CRACKED BETWEEN STRINGERS 10 AND 12.REMOVED THE CRACKED AFT DOUBLER AND DAMAGED SECTION OF FRAME. INSTALLED N
- [SDR COMA0160935](https://openairdocs.org/sdr/COMA0160935), Nov 30, 2001: BUSHING. FAULTY. VERTICAL STABILIZER, L/II HORIZONTAL ATTACH LUG BUSHING MIGRATED.REPLACED BUSHING P/N #600-21061-7 IAW SERVICE BULLETIN 601R-55-007, REF MAINT LOG PAGE #243117 
- [SDR COMA0160431](https://openairdocs.org/sdr/COMA0160431), Jul 4, 2001: PDU. FROZEN. FLAPS FAILED AT 16 DEGREES.REPLACED THE FLAP PDU.
- [SDR COMA0160438](https://openairdocs.org/sdr/COMA0160438), Jul 3, 2001: BPSU. MALFUNCTIONED. FLAP FAILED AT 17 DEGREES.REPLACED THE LEFT HAND BPSU.
- [SDR COMA0160427](https://openairdocs.org/sdr/COMA0160427), Jun 30, 2001: ACTUATOR. BINDING. FLAPS FAILED AT 13 DEGREES.REPLACED THE R/H #4 FLAP ACTUATOR.
- [SDR COMA0160411](https://openairdocs.org/sdr/COMA0160411), Jun 28, 2001: BPSU. MALFUNCTIONED. FLAPS FAILED AT 13 DEGREES.REPLACED THE LEFT HAND BPSU.
- [SDR COMA0160412](https://openairdocs.org/sdr/COMA0160412), Jun 28, 2001: FLAP. FAILED. FLAPS FAILED AT 17 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
- [SDR COMA0160081](https://openairdocs.org/sdr/COMA0160081), Jan 7, 2001: ACCESS PANEL. CRACKED. LOWER WING ACCESS HOLES CRACKED AT 550BB WS 188.040 550CB WS 209.040 AND 550EB WS 253.022. BLENDED DAMAGE AND ROTO-PEENED IAW REO 601R-57-21-030.
- [SDR COMA0060936](https://openairdocs.org/sdr/COMA0060936), Nov 22, 2000: ENGINE. VIBRATION. LEFT ENGINE N2 VIB WARNING. REPLACED THE LEFT ENGINE.
- [SDR COMA0060836](https://openairdocs.org/sdr/COMA0060836), Oct 17, 2000: FCU. MALFUNCTIONED. FLAPS FAILED AT 8 DEGREES. REPLACED THE FECU.

All 73: https://openairdocs.org/deregistered/N712CA-2013-07-16/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 20070119001779I](https://openairdocs.org/incident/20070119001779I), Jan 19, 2007: Cndair CL6002B19 (N712CA), Richmond, VA. (-23) On 01/19/07 at 1135EST comair flight 5385 diverted and landed on runway 34 after reporting a number 2 hydraulic system failure while enroute from…

## Other aircraft with N712CA

- [Registered now](https://openairdocs.org/aircraft/N712CA): Aerospatiale AS 355F2, S/N 5362, built 1987

---
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.