# N713CA: 1998 Bombardier CL-600-2B19, registration cancelled 2013-08-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 16, 2013
- Exported to: Bermuda
- 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: 7245
- Year built: 1998
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 29, 1998
- Certificate issued: February 19, 2010
- Last registry action: February 19, 2010
- Mode S code: A98765
- Owner when cancelled: [Bank Of Utah Owner Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20OWNER%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/N713CA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=713CA
- Page: https://openairdocs.org/deregistered/N713CA-2013-08-16

From the FAA registry file of November 5, 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 COMA2011092650071](https://openairdocs.org/sdr/COMA2011092650071), Sep 23, 2011: MECHANISM. OUT OF ADJUST. EN ROUTE FROM MSP TO CVG, RECEIVED PAX DOOR LATCH CAUTION MSG. STAYED ON ABOUT 15 MIN UNTIL WE HIT BUMPS AT 6000FT. EMERGENCY DECLARED, A/C DIVERTED TO ORD LAND
- [SDR COMA2011091950070](https://openairdocs.org/sdr/COMA2011091950070), Sep 19, 2011: BULKHEAD. CRACKED. REAR PRESSURE BULKHEAD CRACKED AT TOP OF AFT CARGO TRACK. REMOVED DAMAGED AREA FABRICATED PARTS PER REO 601R-53-61-1541. INSTALLED ALL FABRICATED PARTS PER REO 
- [SDR COMA2011091550069](https://openairdocs.org/sdr/COMA2011091550069), Sep 15, 2011: BULKHEAD. CRACKED. REAR PRESSURE BULKHEAD CRACKED AT LINTEL ATTACHMEMT AREA. REMOVED DAMAGE AREA OF REAR BULKHEAD AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1230 AND REO 601R
- [SDR COMA2011091550068](https://openairdocs.org/sdr/COMA2011091550068), Sep 15, 2011: BULKHEAD. DENTED. REAR PRESSURE BULKHEAD DENTED AND GOUGED JUST INBOARD OF CONNECTOR J257. REMOVED DAMAGE AREA OF REAR BULKHEAD JUST ABOVE LINTEL FITTING AND INSTALLED REPAIR DOU
- [SDR COMA2011091450067](https://openairdocs.org/sdr/COMA2011091450067), Sep 13, 2011: BEAM. CRACKED. CRACK ON BOTTOM OF FS 280 BEAM AT RBL 9. REMOVED DAMAGE FABRICATED REPAIR PARTS AND INSTALLED IAW REO601R-53-11-171 REV D.
- [SDR COMA2011091250066](https://openairdocs.org/sdr/COMA2011091250066), Sep 12, 2011: FLOOR SUPPORT. CORRODED. COCKPIT FLOOR SUPPORT AT FS 280 IS HEAVILY CORRODED (CAMLOCK ANGLE). REPLACED CAMLOCK ANGLE P/N 600-34017-351S IAW SRM 51-42-06 AND 51-42-21.
- [SDR COMA2011091250065](https://openairdocs.org/sdr/COMA2011091250065), Sep 12, 2011: BEAM. CRACKED. CRACK ON TOP ANGLE OF 280 BEAM AT RBL 9. REPAIRED 280 BEAM P/N 600-34017-595 IAW REO 601R-53-11-136 REV A DATED 11/01/07.
- [SDR COMA2011031750027](https://openairdocs.org/sdr/COMA2011031750027), Mar 16, 2011: CONTROL UNIT. FAILED. ON CLIMBOUT FROM BOS TO RDU WITH ANTI-ICE ON RECEIVED WING OVHT WARNING MSG AT ABOUT 3000FT. EMERGENCY DECLARED, FOLLOWED QRH, MSG STAYED ON OVER 40 SEC AND EXT
- [SDR COMA2009092150194](https://openairdocs.org/sdr/COMA2009092150194), Sep 16, 2009: FUEL CONTROL. LEAKING. EN ROUTE FROM JFK TO BNA CREW NOTICED FUMES IN THE COCKPIT. PERFORMED QRH, EMERGENCY DECLARED. A/C DIVERTED TO CRW LANDED SAFELY. INSPECTED A/C FOUND APU FUEL C
- [SDR COMA2009081150181](https://openairdocs.org/sdr/COMA2009081150181), Aug 11, 2009: FRAME. CRACKED. LEFT FRAME CAP ANGLE BEND RADIUS AT FS 559.00 CRACKED AN BL 18.00. REPAIRED CRACK AT FS 559.00 IAW REO 601R-53-41-260.
- [SDR COMA2009062250154](https://openairdocs.org/sdr/COMA2009062250154), Jun 20, 2009: COALESCER BAG. DIRTY. ON T/O F/A AND PASSENGERS REPORTED A BURNING SMELL. EMERGENCY DECLARED, ACFT RETURNED TO DEPARTURE, LANDED SAFELY. REMOVED AND REPLACED COALESCER BAGS. NO FURTH
- [SDR COMA2008122450045](https://openairdocs.org/sdr/COMA2008122450045), Dec 24, 2008: CONTROLLER. FAULTY. DURING CRUISE FLIGHT RECEIVED A LEFT WING ANTI-ICE MESSAGE, FLGIHT DIVERTED TO GSO. REPLACED THE ANTI-ICE CONTROLLER.
- [SDR COMA2008121750036](https://openairdocs.org/sdr/COMA2008121750036), Dec 15, 2008: SHUTOFF VALVE. FAULTY. ON CLIMBOUT FROM CVG RECEIVED WING OVERHEAT WARNING MSG WITH SYSTEM ON, AND IN STANDBY. ACFT RETURNED TO CVG LANDED SAFELY. REMOVED AND REPLACED LEFT ANTI-ICE M
- [SDR COMA0860300](https://openairdocs.org/sdr/COMA0860300), Jun 20, 2008: FIRE BOTTLE. INTERMITTENT. EN ROUTE FROM CLE TO SYR RECEIVED CARGO BOTTLE LOW CAUTION MSG AT 28500, STAYED ON FOR 3 MIN THEN WENT OUT. EMERGENCY DECLARED, ACFT RETURNED BACK TO CLE AND LA
- [SDR COMA0860299](https://openairdocs.org/sdr/COMA0860299), Jun 20, 2008: FIRE BOTTLE. INTERMITTENT. EN ROUTE FROM CLE TO SYR RECEIVED CARGO BOTTLE LOW CAUTION MSG AT 28500. STAYED ON FOR 3 MIN THEN WENT OUT. EMERGENCY DECLARED, ACFT RETURNED BACK TO CLE AND LA
- [SDR COMA0860287](https://openairdocs.org/sdr/COMA0860287), Jun 13, 2008: PRIORITY VALVE. LEAKING. LANDING GEAR WOULD NOT EXTEND. FLUID LEVEL OF HYD SYSTEM 3 WAS 5%. DECLARED EMERGENCY, PERFORMED EMERGENCY EXTENSION, LANDED WITHOUT INCIDENT. REPLACED MLG PRIO
- [SDR COMA0860284](https://openairdocs.org/sdr/COMA0860284), Jun 10, 2008: PRIORITY VALVE. FAULTY. RECEIVED NOSE GEAR DISAGREE MESSAGE ON APPROACH. FOLLOWED QRH, DECLARED EMERGENCY. LANDING GEAR LOWERED ON RECYCLE. LANDED WITHOUT INCIDENT. REPLACED MGL PRIORI
- [SDR COMA0860276](https://openairdocs.org/sdr/COMA0860276), Jun 9, 2008: PRIORITY VALVE. FAULTY. ON APPROACH INTO CVG DURING GEAR DOWN SELECTION RECEIVED GEAR DISAGREE MSG, EXECUTED MISAPPROACH. RAN QRH SECOND GEAR DOWN SELECTION WAS SUCCESSFUL. ACFT LANDED
- [SDR COMA0760728](https://openairdocs.org/sdr/COMA0760728), Dec 14, 2007: TRANSDUCER. FAULTY. FLIGHT 9658 - DURING CRUISE FLIGHT RECEIVED A RIGHT ENGINE OIL PRESSURE WARNING MESSAGE, CREW DECLARED AN EMERGENCY, PERFORMED AN I.F.S.D. AND DIVERTED TO MDT. 
- [SDR COMA0760727](https://openairdocs.org/sdr/COMA0760727), Dec 14, 2007: PUMP. FAULTY. FLIGHT 9658 - DURING CRUISE FLIGHT RECEIVED A RIGHT ENGINE OIL PRESSURE WARNING MESSAGE, CREW DECLARED AN EMERGENCY, PERFORMED AN I.F.S.D. AND DIVERTED TO MDT. 
- [SDR COMA0760440](https://openairdocs.org/sdr/COMA0760440), Jun 17, 2007: GEARBOX. OVERHEATED. FLIGHT 5589 - EN ROUTE CVG-NAS RECEIVED A RIGHT ENGINE OIL HIGH TEMPERATURE INDICATION. FLIGHT RETURNED TO CVG. SERVICED RIGHT ENGINE AGB.
- [SDR COMA0660689](https://openairdocs.org/sdr/COMA0660689), Dec 6, 2006: WARNING MESSAGE. ILLUMINATED. FLIGHT 5099 - NOSE WHEEL STEERING CAUTION MESSAGE DURING TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO GATE. INSPECTED NWS SYSTEM, NO DEFECTS NOTED. PERFORMED O
- [SDR COMA0660195](https://openairdocs.org/sdr/COMA0660195), Feb 26, 2006: WARNING SYSTEM. MALFUNCTIONED. FLIGHT 5843 - DURING TAKEOFF AT ORF RECEIVED A TRIM CONFIGURATION MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GATE. PERFORMED AN OPERATIONAL CHECK OF FLIGHT CO
- [SDR COMA0560701](https://openairdocs.org/sdr/COMA0560701), Dec 9, 2005: ACTUATOR. UNRELIABLE. FLIGHT 5653 - FLAPS FAIL CAUTION. REPLACED THE LT FLAP ACTUATOR.
- [SDR COMA0560678](https://openairdocs.org/sdr/COMA0560678), Dec 7, 2005: WARNING SYSTEM. ACTIVATED. FLIGHT 5457 - DURING DCA APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, FLIGHT LANDED WITHOUT INCIDENT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST EV
- [SDR COMA0560178](https://openairdocs.org/sdr/COMA0560178), Mar 14, 2005: PROXIMITY SWITCH. MALFUNCTIONED. FLIGHT 9452 CABIN DOOR OUTER HANDLE WARNING. REPLACED PROXIMITY SWITCH DI17.
- [SDR COMA0560048](https://openairdocs.org/sdr/COMA0560048), Jan 11, 2005: WIRE. LOOSE. FLIGHT 5509 - 3 EMERGENCY LIGHTS INOP. REPAIRED LOOSE WIRING.
- [SDR COMA0460416](https://openairdocs.org/sdr/COMA0460416), Jul 14, 2004: FRAME. CORRODED. DURING A 72/48 MO INSP, TASK CRJ-2-142005, FOUND FUSELAGE FRAME CORRODED ON TOP EDGE. PERFORMED PERMANENT REPAIR IAW COMAIR EA 10-5310-00389.
- [SDR COMA0460257](https://openairdocs.org/sdr/COMA0460257), Apr 13, 2004: WARNING LIGHT. ILLUMINATED. FLIGHT 5205 FLAP FAIL CAUTION AFTER LANDING. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
- [SDR COMA0460253](https://openairdocs.org/sdr/COMA0460253), Apr 10, 2004: LATCH. OPEN. FLIGHT 5219 CABIN DOOR HANDLE CAUTION MESSAGE. COULD NOT DUPLICATE. FOUND DOOR HANDLE IN OPEN POSITION. OPERATIONAL CHECK OF DOOR LATCH MECH WAS NORMAL.
- [SDR COMA0360572](https://openairdocs.org/sdr/COMA0360572), Dec 19, 2003: BRACKET. CRACKED. THERE WAS A CRACKED INTERCOSTAL SUPPORT BRACKET BEHIND HYDRAULIC SYSTEM NR 1 RETURN FILTER BOWL. REMOVED THE CRACKED BRACKET. FABRICATED AND INSTALLED A NEW BRA
- [SDR COMA0260722](https://openairdocs.org/sdr/COMA0260722), Dec 17, 2002: LANDING GEAR. FLIGHT 5053 GEAR DISAGREE WARNING MESSAGE.COULD NOT DUPLICATE EXTENSION AND RETRACTION CHECKS ALL NORMAL. HYDRAULIC PUMPS AND RESERVOIR REPLACED FOR TROUBLESHOO
- [SDR COMA0260704](https://openairdocs.org/sdr/COMA0260704), Dec 10, 2002: THERMISTER. MALFUNCTIONED. FLIGHT 5859 LT WINDOW HEAT CAUTION MESSAGE. SWAPPED CONTROLLER CONNECTIONS TO THE SPARE THERMISTORS, OPERATIONAL CHECK WAS NORMAL.
- [SDR COMA0260659](https://openairdocs.org/sdr/COMA0260659), Nov 19, 2002: WINDSHIELD WIPER. BROKEN. FLIGHT 5080 COPILOTS WINDSHIELD WIPER CAME APART DURING T/O.REPALCED WIPER BLADE ASSY.
- [SDR COMA0260570](https://openairdocs.org/sdr/COMA0260570), Oct 5, 2002: CONTROL CABLE. LACK OF LUBE. AILERON CONTROLS SEEMED STIFFENER THEN NORMAL. LUBRICATED THE LEFT AND RIGHT AILERON CONTROL ASSEMBLY PER EO 27-069RB.
- [SDR COMA0260450](https://openairdocs.org/sdr/COMA0260450), Jul 24, 2002: SKIN. I/H WING LOWER SKIN FUEL PANEL LANDINGS @ W.S. 106.40, 127.25, 264.00 AND 294.50 HAVE CORROSION FROM 0.010" - 0.012" DEEP.REMOVED CORROSION BY BLENDING. PERFORM
- [SDR COMA0260449](https://openairdocs.org/sdr/COMA0260449), Jul 23, 2002: SKIN. CRACKED. PAX DOOR NIB IS DAMAGED AT F.S. 310.00CUT OUT DAMAGE AND INSTALLED STRAP P/N 601R-52-11-008-1 I/A/W CRJ EO 601R-52-11-008 REV B REPAIR A.
- [SDR COMA0260448](https://openairdocs.org/sdr/COMA0260448), Jul 22, 2002: ANGLE. CRACKED. THE ANGLES AT BL 27 LH AND RH AND INTERCOSTAL AT RBL 36 AT FS 484 WERE FOUND CRACKED.REMVOED DISCREPANT PARTS, FABRICATED AND INSTALLED AND REPLACEMENT PARTS I/
- [SDR COMA0260368](https://openairdocs.org/sdr/COMA0260368), Jun 12, 2002: AILERON. FLIGHT 5759 HEAVIER THAN NORMAL CONTROL FORCE REQUIRED FOR ROLL AND PITCH.INSPECTED FLIGHT CONTROLS AND CABLE TENSIONS. NO DEFECTS FOUND. FORCE CHECKS WITHIN LI
- [SDR COMA0260369](https://openairdocs.org/sdr/COMA0260369), Jun 11, 2002: FLAP. FLIGHT 5285 FLAPS FAILED MESSAGE DURING LANDING.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01
- [SDR COMA0260344](https://openairdocs.org/sdr/COMA0260344), May 30, 2002: ENGINE. FAILED. FLIGHT 5376 R/H ENGINE OIL PRESSURE WARNING - FAILED BY ENGINE FAILURE.REPLACED R/H ENGINE.
- [SDR COMA0260246](https://openairdocs.org/sdr/COMA0260246), Apr 10, 2002: PAINT. FLIGHT 5012 AIRCRAFT ROLLS RIGHT WHEN FLAPS EXTENDED.SANDED ROUGH PAINT ON R/H OUTBD FLAP.
- [SDR COMA0260238](https://openairdocs.org/sdr/COMA0260238), Apr 6, 2002: ACTUATOR. BINDING. FLIGHT 5234 FLAPS FAILED MESSAGE. R/H OUTBD FLAP IS TWISTED.REPLACED R/H OUTBD FLAP ACTUATORS,
- [SDR COMA0260237](https://openairdocs.org/sdr/COMA0260237), Apr 5, 2002: ACTUATOR. MALFUNCTIONED. FLIGHT 5393 FLAPS FAIL MESSAGE. REPLACED THE LT INBOARD FLAP ACTUATORS.
- [SDR COMA0260143](https://openairdocs.org/sdr/COMA0260143), Mar 2, 2002: BPSU. MALFUNCTIONED. FLIGHT 5079 FLAPS FAIL MESSAGE AFTER T/O.REPLACED THE L/H BPSU.
- [SDR COMA0260097](https://openairdocs.org/sdr/COMA0260097), Feb 13, 2002: LANDING GEAR. FLIGHT 5557 GEAR DISAGREE WARNING, NLG DID NOT RETRACT.FOUND NLG FLAT - SERVICED NLG I/A/W M/M INSTRUCTIONS.
- [SDR COMA0260008](https://openairdocs.org/sdr/COMA0260008), Dec 28, 2001: BUSHING. MISLOCATED. THE R/H SIDE VERTICAL STABILIZER HAS A MIGRATING BUSHING AT HORIZONTAL STABILIZER PIVOT POINT.REMOVED THE MIGRATING BUSHING. MACHINED AND CADMIUM PLATED A NEW N
- [SDR COMA0260007](https://openairdocs.org/sdr/COMA0260007), Dec 28, 2001: FRAME. CRACKED. THE RT SIDE FRAME AND AFT DOUBLER AT FS 718.0 BETWEEN STRINGERS 10 AND 12 WAS CRACKED. REMOVED CRACKED SECTION OF FRAME AND AFT DOUBLER AND INSTALLED A NEW SECT
- [SDR COMA0260006](https://openairdocs.org/sdr/COMA0260006), Dec 28, 2001: DOUBLER. CRACKED. THE L/H SIDE AFT DOUBLER AT FS718.0 WAS CRACKED BETWEEN STRINGERS 10 AND 12.REMOVED CRACKED DOUBLER AND INSTALLED A NEW DOUBLER I/A/W REO 601R-53-61-193 REV A A
- [SDR COMA0160206](https://openairdocs.org/sdr/COMA0160206), Feb 5, 2001: SKIN. CRACKED. LT LOWER WING PLANK CRACKED AT ACCESS HOLES, 540 CB WS 76.161, 550 AB WS 163.00 AND 550 FB WS 274.319. BLENDED OUT DAMAGE AND ROTO-PEENED AS REQUIRED IAW REO 60

All 63: https://openairdocs.org/deregistered/N713CA-2013-08-16/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 19991205036399I](https://openairdocs.org/incident/19991205036399I), Dec 5, 1999: Cndair CL6002B19 (N713CA), Grand Rapids, MI. (-23) On December 5, 1999, at 1413Z, a CL6002B19, N713CA, registered to comair airlines, #2 eng. Oil msg warning bell and chimes came on steady, after takeoff.…

## Other aircraft with N713CA

- [Registered now](https://openairdocs.org/aircraft/N713CA): Aerospatiale AS 355F2, S/N 5363

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