# N721CA: 1998 Bombardier CL-600-2B19, registration cancelled 2015-08-26

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 26, 2015
- 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: 7259
- Year built: 1998
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 29, 1998
- Certificate issued: October 26, 2007
- Last registry action: April 14, 2015
- Mode S code: A9A776
- 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/N721CA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=721CA
- Page: https://openairdocs.org/deregistered/N721CA-2015-08-26

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 (67, newest 50)

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

- [SDR COMA2010071950147](https://openairdocs.org/sdr/COMA2010071950147), Jul 15, 2010: HYDRAULIC LINE. CHAFED. EN ROUTE FROM BNA TO MSP RECEIVED HYD NR 1 LOW PSI MSG, PRESSURE AND QTY WENT TO ZERO. EMERGENCY DECLARED, A/C DIVERTED TO STL LANDED SAFELY. FOUND HYD LINE FRO
- [SDR COMA2010032950071](https://openairdocs.org/sdr/COMA2010032950071), Mar 26, 2010: CONTROL HANDLE. FAILED. FLAPS FAILED AT 30 DEG ON APPROACH INTO JFK. EMERGENCY DECLARED, A/C LANDED SAFELY AT JFK. REMOVED AND REPLACED FLAP CONTROL LEVER.
- [SDR COMA2009121450227](https://openairdocs.org/sdr/COMA2009121450227), Dec 12, 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 COMA2009121450226](https://openairdocs.org/sdr/COMA2009121450226), Dec 12, 2009: BULKHEAD. CRACKED. FOUND REAR PRESSURE BULKHEAD CRACKED AROUND LINTEL FITTING. REPAIRED CRACK AT LINTEL FITTING IAW REO 601R-53-61-1230.
- [SDR COMA2009120450221](https://openairdocs.org/sdr/COMA2009120450221), Dec 4, 2009: POST. CRACKED. FOUND POST CRACKED AT FS 409.00+128 RBL 27 I/B LOWER CORNER RADIUS. REPAIRED POST IAW REO 601R-53-41-056.
- [SDR COMA2009120350220](https://openairdocs.org/sdr/COMA2009120350220), Dec 3, 2009: POST. CRACKED. FOUND POST CRACKED AT FS 409.00+128 LBL 27 I/B LOWER CORNER RADIUS. REPAIRED POST IAW REO 601R-53-41-056.
- [SDR COMA2009040150108](https://openairdocs.org/sdr/COMA2009040150108), Mar 29, 2009: ENGINE. VIBRATION. ON CLIMBOUT FROM BOS RECEIVED LEFT ENGINE VIBE MSG ALONG WITH MAX ITT AND OIL PRESSURE OF 20 PSI. PERFORMED IFSD OF LEFT ENGINE. EMERGENCY DECLARED, A/C RETURNE
- [SDR COMA2009022450086](https://openairdocs.org/sdr/COMA2009022450086), Feb 24, 2009: UNKNOWN. SMOKE. EN ROUTE FROM BHM TO LGA, SMOKE IN CABIN WITH APU OFF AND BOTH PACKS RUNNING ON 10TH STAGE BLEED AIR. EMERGENCY DECLARED, A/C RETURNED TO BHM LANDED SAFELY. TRA
- [SDR COMA2009020950078](https://openairdocs.org/sdr/COMA2009020950078), Feb 5, 2009: RVDT. FAILED. RECEIVED NWS INOP MSG AFTER SELECTING LANDING GEAR DOWN. WOULD NOT RESET. EMERGENCY DECLARED, A/C LANDED SAFELY. REMOVED AND REPLACED RT NWS POSITION FEEDBACK R
- [SDR COMA2009010550055](https://openairdocs.org/sdr/COMA2009010550055), Jan 4, 2009: ANGLE. CRACKED. RT FS 559.00 CAP ANGLE CRACKED AT LBL 9.00 AND LBL18.00. REPAIRED IAW REO 601R-53-41-260.
- [SDR COMA2009010550054](https://openairdocs.org/sdr/COMA2009010550054), Jan 2, 2009: ANGLE. CRACKED. LT FS 559.00 CAP ANGLE CRACKED AT LBL 9.00 AND LBL 18.00. REPAIRED CAP ANGLE IAW REO 601R-53-41-260.
- [SDR COMA2008121650025](https://openairdocs.org/sdr/COMA2008121650025), Dec 11, 2008: ALTERNATOR. FAILED. ON CLIMBOUT FROM CVG, NR 2 ENGINE N2 SHOWS 0 RPM. A/C RETURNED TO CVG LANDED SAFELY. REMOVED AND REPLACED NR 2 ENGINE ALTERNATOR STATOR. OPS CHECK GOOD.
- [SDR COMA0860232](https://openairdocs.org/sdr/COMA0860232), Apr 22, 2008: INDICATOR. UNKNOWN. FLIGHT 4972 - ON TAKEOFF ROLL NR 2 ENGINE FUEL FLOW READ OUT WAS 1300 LBS. ABORTED TAKEOFF SAFELY. TRANSFERRED TO DMI LIST PER 73-31-01.
- [SDR COMA0860128](https://openairdocs.org/sdr/COMA0860128), Feb 11, 2008: FLAP. MALFUNCTIONED. FLIGHT 5190 - FLAPS FAIL CAUTION MESSAGE ON APPROACH. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. COMPLIED WITH SI-2-2710001 FLAP CAUTION MESSAGE "FIRST EVENT" 
- [SDR COMA0860125](https://openairdocs.org/sdr/COMA0860125), Feb 11, 2008: ACTUATOR. FAULTY. FLIGHT 5532 - FLAPS FAIL CAUTION MESSAGE AT 0 DEGREES WHEN SELECTING 8 DEGREES. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED RIGHT O/B FLAP 
- [SDR COMA0860124](https://openairdocs.org/sdr/COMA0860124), Feb 11, 2008: ACTUATOR. FAULTY. FLIGHT 5532 - FLAPS FAIL CAUTION MESSAGE AT 0 DEGREES WHEN SELECTING TO 8 DEGREES. EMERGENCY DECLARED, A/C LANDED SAFELY. REMOVED AND REPLACED RIGHT O/B FLAP I/
- [SDR COMA0760497](https://openairdocs.org/sdr/COMA0760497), Jul 23, 2007: FLAP SYSTEM. MALFUNCTIONED. FLIGHT 5120 - FLAPS FAIL AT 30 DEGREES ON APPROACH, AIRCRAFT LANDED SAFELY. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, P
- [SDR COMA0760420](https://openairdocs.org/sdr/COMA0760420), Jun 1, 2007: A/C PACK. UNCONTROLLABLE. FLIGHT 5228 - LEFT A/C PACK UNCONTROLLABLE IN AUTO OR MANUAL. RETURNED TO OMA, LANDED WITHOUT INCIDENT. INSPECTED LEFT PACK AND DUCTS FOR DAMAGE, PERFORMED TEMP
- [SDR COMA0760220](https://openairdocs.org/sdr/COMA0760220), Mar 1, 2007: CONTROL HANDLE. FAULTY. FLIGHT 5686 - FLAP FAIL MESSAGE AFTER LANDING. REPLACED FLAP CONTROL HANDLE AS INDICATED BY FECU INTERROGATION. ALSO PERFORMED EO 27-046AD. NO FURTHER DEFECTS.
- [SDR COMA0760121](https://openairdocs.org/sdr/COMA0760121), Jan 29, 2007: FCU. FAULTY. FLIGHT 5524 - DURING ROC APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE FLAP CONTROL
- [SDR COMA0760084](https://openairdocs.org/sdr/COMA0760084), Jan 28, 2007: FLAP SYSTEM. MALFUNCTIONED. FLIGHT 5529 - DURING CMH APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 8 DEGREE FLAP SETTING, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. 
- [SDR COMA0760050](https://openairdocs.org/sdr/COMA0760050), Jan 23, 2007: ACTUATOR. FAILED. FLIGHT 5156 - FLAPS FAIL MESSAGE APPEARED WHEN FLAPS WERE SELECTED TO 8 DEGREES. LANDED WITHOUT INCIDENT. REPLACED LEFT INBOARD FLAP OUTBOARD ACTUATOR.
- [SDR COMA0760049](https://openairdocs.org/sdr/COMA0760049), Jan 23, 2007: ACTUATOR. FAILED. FLIGHT 5156 - FLAPS FAIL MESSAGE APPEARED WHEN FLAPS WERE SELECTED TO 8 DEGREES. LANDED WITHOUT INCIDENT. REPLACED LEFT INBOARD FLAP INBOARD ACTUATOR.
- [SDR COMA0760048](https://openairdocs.org/sdr/COMA0760048), Jan 23, 2007: FLEX DRIVE. TWISTED. FLIGHT 5156 - FLAPS FAIL MESSAGE APPEARED WHEN FLAPS WERE SELECTED TO 8 DEGREES. LANDED WITHOUT INCIDENT. REPLACED LEFT WING NR 5 FLAP FLEX DRIVE SHAFT.
- [SDR COMA0760047](https://openairdocs.org/sdr/COMA0760047), Jan 23, 2007: FLEX DRIVE. TWISTED. FLIGHT 5156 - FLAPS FAIL MESSAGE APPEARED WHEN FLAPS WERE SELECTED TO 8 DEGREES. LANDED WITHOUT INCIDENT. REPLACED LEFT WING NR 3 FLAP FLEX DRIVE SHAFT.
- [SDR COMA0760046](https://openairdocs.org/sdr/COMA0760046), Jan 23, 2007: FLEX DRIVE. TWISTED. FLIGHT 5156 - FLAPS FAIL MESSAGE APPEARED WHEN FLAPS WERE SELECTED TO 8 DEGREES. LANDED WITHOUT INCIDENT. REPLACED LEFT WING NR 2 FLAP FLEX DRIVE SHAFT.
- [SDR COMA0660238](https://openairdocs.org/sdr/COMA0660238), Mar 10, 2006: ACCELEROMETER. FAULTY. FLIGHT 5199 - EN ROUTE GSO-LGA THE LEFT ENGINE N1 FLUCTUATED FROM 1.8, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. REP
- [SDR COMA0660224](https://openairdocs.org/sdr/COMA0660224), Mar 3, 2006: DRIVE SHAFT. WORN. FLIGHT 5882 - AFTER TAKEOFF FROM JFK RECEIVED A FLAP FAIL CAUTION MESSAGE AT ZERO DEGREES, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED W
- [SDR COMA0660158](https://openairdocs.org/sdr/COMA0660158), Feb 18, 2006: FLAP SYSTEM. MALFUNCTIONED. FLIGHT 5334 - AFTER LANDING AT SDF AND DURING RETRACTION OF THE FLAPS RECEIVED A FLAP CAUTION MESSAGE AT 27 DEGREES. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESS
- [SDR COMA0560716](https://openairdocs.org/sdr/COMA0560716), Dec 13, 2005: BULKHEAD. DAMAGED. HOLE IN AFT PRESSURE BULKHEAD FS 621 AND LBL 45. INSTALLED RIVET IN FS 621 AND LBL 45 AFT PRESSURE BULKHEAD IAW SRM 51-12-00 PG 21, SMALL HOLE REPAIR.
- [SDR COMA0560680](https://openairdocs.org/sdr/COMA0560680), Dec 12, 2005: INTERCOSTAL. CRACKED. INTERCOSTAL CRACKED AT FS 484 BL27.00-36.00 RIGHT SIDE BELOW FLOOR AFT OF EMERGENCY EXIT. REPAIRED CRACK IAW BRAS EO 601R-53-41-059.
- [SDR COMA0560404](https://openairdocs.org/sdr/COMA0560404), Jul 23, 2005: OVERHEAT SENSOR. MALFUNCTIONED. FLIGHT 5580- BRAKE OVERHEAT MESSAGE. INSPECTED BRAKE AND FOUND NO DEFECTS.
- [SDR COMA0560340](https://openairdocs.org/sdr/COMA0560340), Jun 7, 2005: WARNING SYSTEM. ACTIVATED. RT THRUST REVERSER UNLOCK CAUTION. DEFERRED MAINTENANCE ON RIGHT THRUST REVERSER PER MEL.
- [SDR COMA0560314](https://openairdocs.org/sdr/COMA0560314), May 20, 2005: LINE. LEAKING. FLIGHT 5088 HYDRAULIC SYSTEM NR 1 LOW PRESSURE CAUTION, QUANTITY INDICATED 0. REPLACED HIGH PRESSURE LINE IN LEFT HAND ENGINE PYLON.
- [SDR COMA0560245](https://openairdocs.org/sdr/COMA0560245), Apr 7, 2005: CONTROL PANEL. FAILED. FLIGHT 5315 DURING CLIMBOUT OF CVG WITH FLAPS RETRACTED THE STAB AND MACH TRIM MASTER CAUTION MESSAGES ACTIVATED, CREW FOLLOWED QRH PROCEDURES, RE-ENGAGED STAB/
- [SDR COMA0560032](https://openairdocs.org/sdr/COMA0560032), Jan 7, 2005: LAMP. INOPERATIVE. FLIGHT 5681 EMERGENCY FLOOR LIGHTS INOP AT ROW 1 AND 2. REPLACED THE FLEXIBLE LIGHT STRIP.
- [SDR COMA0470032](https://openairdocs.org/sdr/COMA0470032), Apr 19, 2004: ENGINE. OVERHEATED. FLIGHT 5711 DURING TAKEOFF ROLL AT 80 KNOTS NR 2 ENGINE ITT REACHED 906C DEGREES, ABORTED T/O AND RETURNED TO THE GATE. REPLACED THE RIGHT ENGINE.
- [SDR COMA0460240](https://openairdocs.org/sdr/COMA0460240), Apr 4, 2004: WARNING LIGHT. ILLUMINATED. FLIGHT 5390 RIGHT ENGINE ITT OVERTEMP DURING T/O. COULD NOT DUPLICATE. GROUND RUN SATISFACTORY. NO DEFECT FOUND.
- [SDR COMA0460215](https://openairdocs.org/sdr/COMA0460215), Mar 19, 2004: SEAL. LEAKING. FLIGHT 5892 WATER LEAKING FROM CABIN CEILING. RESEALED AROUND ADF ANTENNA.
- [SDR COMA0460157](https://openairdocs.org/sdr/COMA0460157), Feb 21, 2004: PDU. MALFUNCTIONED. FLIGHT 5108 FLAPS FAIL MESSAGE DURING TAXI. REPLACED THE PDU.
- [SDR COMA0360532](https://openairdocs.org/sdr/COMA0360532), Dec 7, 2003: FRAME. CRACKED. CRACK NOTED AT FS 718.00 RT BETWEEN STRINGER 11 - 12. REPAIRED PER SERVICE BULLETIN 601R-53-055 PART B PER EA 10-5320-00242.
- [SDR COMA0360531](https://openairdocs.org/sdr/COMA0360531), Dec 7, 2003: DOUBLER. CRACKED. CRACK NOTED AT FS 718.00 LT AND DOUBLER BETWEEN STRINGER 10 -12. REPAIRED PER EO 53 027 AND SERVICE BULLETIN 601R-53-055 PD.
- [SDR COMA0360530](https://openairdocs.org/sdr/COMA0360530), Dec 7, 2003: DOUBLER. CRACKED. CRACK NOTED AT FS 718.00 RIGHT HAND DOUBLER BETWEEN STRINGER 10 - 12. REPAIRED PER EO 53-027 AND SERVICE BULLETIN 601R-53-055 PE.
- [SDR COMA0360215](https://openairdocs.org/sdr/COMA0360215), Apr 24, 2003: WARNING LIGHT. ILLUMINATED. FLIGHT 5083 ANTI-SKID CAUTION MESSAGE WHEN LANDING GEAR EXTENDED. COULD NOT DUPLICATE, SYSTEM TEST NORMAL.
- [SDR COMA0360200](https://openairdocs.org/sdr/COMA0360200), Apr 16, 2003: GENERATOR. INOPERATIVE. FLIGHT 5261 GENERATOR NR 2 OFF-LINE DURING T/O. DEFERRED MAINT PER MEL.
- [SDR COMA0360142](https://openairdocs.org/sdr/COMA0360142), Mar 9, 2003: PUMP. LEAKING. FOUND SMALL PIN HOLE IN RT ENG FUEL PUMP HOUSING, FOUND DURING A LEAK CHECK FOR A NON RELATED ITEM. REPLACED FUEL PUMP.
- [SDR COMA0260728](https://openairdocs.org/sdr/COMA0260728), Dec 20, 2002: TRANSDUCER. MALFUNCTIONED. LEFT ENGINE OIL PRESSURE INDICATED 157 PSI. REPLACED THE OIL PRESSURE TRANSDUCER.
- [SDR COMA0260417](https://openairdocs.org/sdr/COMA0260417), Jul 7, 2002: PRIORITY VALVE. MALFUNCTIONED. FLIGHT 5222 GEAR DISAGREE WARNING DURING GEAR EXTENSION.REPLACED THE NLG PRIORITY VALVE.
- [SDR COMA0260389](https://openairdocs.org/sdr/COMA0260389), Jun 26, 2002: DOOR. FLIGHT 5726 CABIN DOOR WARNING AFTER T/O.OUTER HANDLE NOT STOWED PROPERLY - INSPECTED AND OPERATED DOOR - FOUND NO DEFECT.
- [SDR COMA0160951](https://openairdocs.org/sdr/COMA0160951), Dec 9, 2001: PIN. FLIGHT #5686 NLG DOES NOT RETRACT WHEN LANDING GEAR SELECTED UP.FOUND NLD DOWN LOCK SAFETY PIN INSTALLED. - REMOVED PIN AND AIRCRAFT RETURNED TO SERVICE.

All 67: https://openairdocs.org/deregistered/N721CA-2015-08-26/reports.md

## FAA accident and incident reports (2)

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 20050723015689I](https://openairdocs.org/incident/20050723015689I), Jul 23, 2005: Cndair CL6002B19 (N721CA), Kansas City, MO. (-23) On July 23, 2005 at 1800 hrs local comair (delta express), pilot advised tower they had no air conditioning and wanted to get airborne quickly. During…
- [Incident 20010203002619I](https://openairdocs.org/incident/20010203002619I), Feb 3, 2001: Cndair CL6002B19 (N721CA), State College, PA. (-23) An APU blew a fuse in flight and poured oil into the bleed-air. This caused smoke in the cabin. A mechanic found the blown fuse, deferred APU, and…

## Other aircraft with N721CA

- [Registered now](https://openairdocs.org/aircraft/N721CA): Cirrus Design SR22T, S/N 2452, built 2021

---
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.