# N797CA: 1999 Bombardier CL-600-2B19, registration cancelled 2022-12-03 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 3, 2022 - Status when cancelled: Registration expired, pending cancellation - 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: 7344 - Year built: 1999 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 17, 1999 - Certificate issued: August 29, 2019 - Last registry action: September 4, 2019 - Mode S code: AAD239 - Owner when cancelled: [Beautech Power Systems LLC](https://openairdocs.org/faa-owner/BEAUTECH%20POWER%20SYSTEMS%20LLC) - Location: [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas) - Owner type: LLC - Owner's area on the map: 32.7883° N, 96.7996° W: Placed by OpenAirDocs at the center of ZIP code 75201, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N797CA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=797CA - Page: https://openairdocs.org/deregistered/N797CA-2022-12-03 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 (46) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR COMA2011032250030](https://openairdocs.org/sdr/COMA2011032250030), Mar 22, 2011: SILL. CORRODED. SERVICE DOOR SILL IS CORRODED. REPLACED DISCREPANT SILL ANGLE (7075-T6 0.063) AND PART NUMBER 601R38338-2 IAW BOMBARDIER SRM 51-42-13, SRM 51-42-21 AND AMM 20-2 - [SDR COMA2011031650026](https://openairdocs.org/sdr/COMA2011031650026), Mar 16, 2011: ANGLE. CRACKED. FS 559.00 RT CAP ANGLE CRACKED AT RBL 18.00. REMOVE AND REPLACED DAMAGED AREA OF WEB AND CAP ANGLE AT FS 559.00 RT SIDE IAW COMAIR TASK CARD REO 601R-53-41-260 - [SDR COMA2011031650025](https://openairdocs.org/sdr/COMA2011031650025), Mar 16, 2011: ANGLE. CRACKED. FS 559 LT CAP ANGLE CRACKED AT RBL 18.00 AND 9.00. REMOVED LT CAP ANGLE AND INSTALLED NEW CAP ANGLE AS PER TASK CARD REO 601R-53-41-260. - [SDR COMA2011031150024](https://openairdocs.org/sdr/COMA2011031150024), Mar 11, 2011: BULKHEAD. CRACKED. BULKHEAD WEB CRACKED AROUND LINTEL ATTACH FITTING, TWO PLACES, AT FS 621, LBL 36.2. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1230, R - [SDR COMA2011031150023](https://openairdocs.org/sdr/COMA2011031150023), Mar 11, 2011: ANGLE. CRACKED. FS 559 CAP ANGLE CRACKED AT LBL 18. CUT OUT DAMAGED AREA AND INSTALLED NEW CAP ANGLE SECTION IAW REO 601R-53-41-260 LT REP. - [SDR COMA2010030450053](https://openairdocs.org/sdr/COMA2010030450053), Mar 4, 2010: BULKHEAD. CRACKED. FORWARD PRESSURE BULKHEAD AT FS 202.75 CRACKED AT CUTOUT FOR PARKING BRAKE CABLE. REPAIRED FWD PRESSURE BULKHEAD AT FS 202.75 IAW REO 601R-53-11-563 AND EA 10-5 - [SDR COMA2009012650069](https://openairdocs.org/sdr/COMA2009012650069), Jan 23, 2009: DOOR. OPEN. AFTER DEPARTURE FROM LGA LOUD NOISE IN FRONT RIGHT SIDE OF A/C. A/C RETURNED TO LGA, LANDED SAFELY. INSPECTED A/C FOUND COMMUNICATION DOOR LEFT OPEN. INSPECTED - [SDR COMA0860209](https://openairdocs.org/sdr/COMA0860209), Apr 4, 2008: SENSOR. MALFUNCTIONED. FLIGHT 5129 - EN ROUTE BUF-CVG RECEIVED A RIGHT WINDSHIELD HEAT CAUTION, FLIGHT RETURNED TO BUF. SWAPPED THE SPARE TEMPERATURE SENSOR ON THE RIGHT WINDSHIELD TO - [SDR COMA0860136](https://openairdocs.org/sdr/COMA0860136), Feb 17, 2008: SELECTOR VALVE. FAILED. FLIGHT 5386 - LANDING GEAR DISAGREE MESSAGE WHEN SELECTING GEAR DOWN. NOSE GEAR DOWN AND LOCKED MAINS REMAINED UP AND LOCKED. FOLLOWED QRH, PERFORMED MANUAL EXT - [SDR COMA0860102](https://openairdocs.org/sdr/COMA0860102), Jan 29, 2008: WINDOW. CRACKED. FLIGHT 5104 - COCKPIT LEFT SIDE WINDOW CRACKED AT CRUISE. RECEIVED WINDOW HEAT CAUTION MESSAGES. DECLARED EMERGENCY, DIVERTED TO ACY, LANDED WITHOUT INCIDENT. R - [SDR COMA0760302](https://openairdocs.org/sdr/COMA0760302), Apr 5, 2007: J-BOX. LOOSE. GEAR DISAGREE ON T/O, A/C RETURNED BACK TO CVG AND LANDED SAFELY. INSPECTED AND FOUND JB11 LOOSE IN IT'S RACK, RESECURED JB11. - [SDR COMA0760260](https://openairdocs.org/sdr/COMA0760260), Mar 15, 2007: CROSSBEAM. CORRODED. FS 280 CROSSBEAM CORRODED. REPAIRED CROSSBEAM IAW REO 601R-53-21-069. - [SDR COMA0760081](https://openairdocs.org/sdr/COMA0760081), Jan 27, 2007: SHAFT. DAMAGED. FLIGHT 5421 - FLAP FAIL MESSAGE AT 8 DEGREES. REPLACED NR 1 FLEX DRIVE, LEFT SIDE. - [SDR COMA0660728](https://openairdocs.org/sdr/COMA0660728), Dec 22, 2006: SENSING ELEMENT. FAULTY. FLIGHT 5007- EN ROUTE CVG-GSO RECEIVED A LEFT 14TH STAGE DUCT MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT RETURNED TO CVG. REPLACED TEMPERATURE SENSING ELEME - [SDR COMA0660675](https://openairdocs.org/sdr/COMA0660675), Dec 2, 2006: BRAKE CABLE. LACK OF LUBE. FLIGHT 5168 - TAKEOFF ABORTED AT 60 KTS FOR TAKEOFF CONFIG WARNING. TAKEOFF CONFIG OK MESSAGE WAS ON UNTIL TAKEOFF THRUST WAS SET. MAX BTMS WAS 6. ABORTED TAKEO - [SDR COMA0660674](https://openairdocs.org/sdr/COMA0660674), Dec 2, 2006: BRAKE CABLE. OUT OF ADJUST. FLIGHT 5348 - CONFIG BRAKE WARNING MESSAGE WITH THRUST PUSHED UP FOR TAKEOFF. TAKEOFF CONFIG OK ADVISORY APPEARS INTERMITTENTLY. ABORTED TAKEOFF WITHOUT INCIDEN - [SDR COMA0660667](https://openairdocs.org/sdr/COMA0660667), Nov 29, 2006: CONTROL UNIT. FAULTY. FLIGHT 5002 - ON APPROACH RECEIVED ANTI-SKID INBD AND OUTBD WARNING MESSAGES. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED ASCU, NO FURTHER DEFECTS. - [SDR COMA0660638](https://openairdocs.org/sdr/COMA0660638), Nov 16, 2006: DCU. FAULTY. FLIGHT 5195 - EN ROUTE JFK-IAD FLIGHT RETURNED TO JFK DUE TO FLAP INDICATION AND TENDENCY TO ROLL RIGHT. REPLACED THE NR 2 DATA CONCENTRATOR UNIT. - [SDR COMA0660532](https://openairdocs.org/sdr/COMA0660532), Sep 7, 2006: BEAM. CRACKED. WHILE PERFORMING EO 57-021 FOUND THE ENGINE BOX BEAM CRACKED ON TIP SKIN. PERFORMED REO 601R-53-61-345/346. - [SDR COMA0660302](https://openairdocs.org/sdr/COMA0660302), Apr 12, 2006: FLAP SYSTEM. MALFUNCTIONED. FLIGHT 5603 - DURING TAXI RECEIVED A FLAP FAIL CAUTION MESSAGE AT 27 DEGREES, AIRCRAFT RETURNED TO THE GATE. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIR - [SDR COMA0660131](https://openairdocs.org/sdr/COMA0660131), Feb 9, 2006: FLAP SYSTEM. MALFUNCTIONED. FLIGHT 5000 - DURING YUL APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT ZERO DEGREES. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE - [SDR COMA0560663](https://openairdocs.org/sdr/COMA0560663), Dec 1, 2005: CHECK VALVE. MALFUNCTIONED. FLIGHT 5153 - RIGHT AC PACK HIGH TEMP AND SMOKE TOILET WARNING WITH VISIBLE SMOKE. REPLACED THE FAN BYPASS CHECK VALVE. - [SDR COMA0560357](https://openairdocs.org/sdr/COMA0560357), Jun 16, 2005: PCU. LEAKING. RECEIVED HYDRAULIC NR 2 LOW PRESSURE CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND DIVERTED TO IAD. ACFT LANDED WITHOUT INCIDENT. REPLACED LEAKING FLIGHT SPOI - [SDR COMA0560356](https://openairdocs.org/sdr/COMA0560356), Jun 16, 2005: PUMP. FAULTY. RECEIVED HYDRAULIC NR 2 LOW PRESSURE CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND DIVERTED TO IAD. ACFT LANDED WITHOUT INCIDENT. REPLACED RT ENGINE HYDRAULIC - [SDR COMA0560355](https://openairdocs.org/sdr/COMA0560355), Jun 16, 2005: LINE. LEAKING. RECEIVED A HYDRAULIC NR 2 LOW PRESSURE CAUTION MESSAGE. CREW DECLARED EMERGENCY AND DIVERTED TO IAD. ACFT LANDED WITHOUT INCIDENT. REPLACED LEAKING NR 2 EDP PRE - [SDR COMA0560294](https://openairdocs.org/sdr/COMA0560294), May 1, 2005: WARNING SYSTEM. ACTIVATED. FLIGHT 5605 FLAPS FAIL CAUTION. RESET FLAPS SYSTEM AND DEFERRED MAINT PER AD 98-20-01. - [SDR COMA0560225](https://openairdocs.org/sdr/COMA0560225), Apr 2, 2005: COMPUTER. FAULTY. FLIGHT DURING TAKEOFF ROLL RECEIVED A STALL FAIL CAUTION MESSAGE, AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED THE STALL PROTECTION COMPUTER. - [SDR COMA0560070](https://openairdocs.org/sdr/COMA0560070), Jan 20, 2005: VALVE. FAULTY. FLIGHT 4983, DURING CLIMB-OUT OF ATL, RECEIVED A LEFT COWL ANTI-ICE CAUTION, FLIGHT DIVERTED BACK TO ATL. REPLACED THE ANTI-ICE VALVE. - [SDR COMA0560065](https://openairdocs.org/sdr/COMA0560065), Jan 20, 2005: WARNING LIGHT. ILLUMINATED. FLIGHT 5790 RECEIVED A FLAP FAIL CAUTION MESSAGE AFTER PUSHBACK FROM ATL GATE. AIRCRAFT RETURNED TO THE GATE. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIR - [SDR COMA0460575](https://openairdocs.org/sdr/COMA0460575), Oct 21, 2004: WARNING LIGHT. ILLUMINATED. FLIGHT 5376 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. - [SDR COMA0460584](https://openairdocs.org/sdr/COMA0460584), Oct 15, 2004: BPSU. FAULTY. FLIGHT 5222 FLAPS FAIL CAUTION MESSAGE. REMOVED AND REPLACED BPSU. - [SDR COMA0460571](https://openairdocs.org/sdr/COMA0460571), Oct 12, 2004: CONTROL UNIT. FAILED. FLIGHT 5370 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. - [SDR COMA0460573](https://openairdocs.org/sdr/COMA0460573), Oct 11, 2004: WARNING LIGHT. FALSE ACTIVATION. FLIGHT 4943 FLAPS FAIL CAUTION MESSAGE. COULD NOT DUPLICATE. INSPECTED FLAP SYSTEM AND FOUND NO DEFECTS. - [SDR COMA0460570](https://openairdocs.org/sdr/COMA0460570), Oct 11, 2004: WARNING SYSTEM. ACTIVATED. FLIGHT 5011 FLAPS FAIL CAUTION MESSAGE. COULD NOT DUPLICATE. INSPECTED FLAP SYSTEM, FOUND NO DEFECTS. - [SDR COMA0460487](https://openairdocs.org/sdr/COMA0460487), Aug 24, 2004: ENGINE. FAILED. FLIGHT 4990 LT ENGINE ROLLBACK TO 50 PERCENT AFTER T/O. REPLACED LEFT ENGINE. - [SDR COMA0360306](https://openairdocs.org/sdr/COMA0360306), Jun 29, 2003: WINDSHIELD. CRACKED. FLIGHT 5620 THE LEFT WINDSHIELD SHATTERED DURING CLIMBOUT OF ATL, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. REPLACED THE LEFT WINDSHIELD. - [SDR COMA0160608](https://openairdocs.org/sdr/COMA0160608), Aug 18, 2001: COMPUTER. FLIGHT #5235. DURING TAXI OUT RECEIVED A STALL FAIL CAUTION MESSAGE, AIRCRAFT RETURNED TO THE GATE.RESET THE STALL PROTECTION COMPUTER. - [SDR COMA0160545](https://openairdocs.org/sdr/COMA0160545), Jul 30, 2001: COMPUTER. MALFUNCTIONED. YAW DAMPNER DROPPED OFF LINE DURING TAXI CHECKS.REPLACED THE #1 FCC-4000. - [SDR COMA0160538](https://openairdocs.org/sdr/COMA0160538), Jul 27, 2001: RUDDER. VERY NOTICEABLE YAWING MOTION INFLIGHT.COULD NOT DUPLICATE. CHEDCKED YAW DAMPNERS AND RUDDER SYSTEM. NO DEFECTS FOUND. - [SDR COMA0160338](https://openairdocs.org/sdr/COMA0160338), Mar 24, 2001: CAP. CHAFED. LEFT INBOARD FLAP HAS CHAFED VANE CAP ON INBOARD END. BLENDED CHAFED AREA IAW CANADAIR REO 601R-57-52-004 AND PAINTED IAW CRJ SRM 51-21-16. - [SDR COMA0160336](https://openairdocs.org/sdr/COMA0160336), Mar 23, 2001: BUSHING. WORN. HORIZONTAL STAB LEFT OUTBOARD PIVOT POINT BUSHING WORN. REMOVED AND REPLACED BUSHING IAW CRJ AMM 20-26-00-910-803. REAMED BUSHING IAW REO 601R-55-11-022 REV A. - [SDR COMA0160335](https://openairdocs.org/sdr/COMA0160335), Mar 23, 2001: BUSHING. WORN. LEFT VERTICAL STAB PIVOT POINT BUSHING WORN. REMOVED AND REPLACED BUSHING IAW CRJ AMM 20-26-00-910-803, REAMED BUSHING IAW CRJ DRAWING 600-21061. MACHINED FLANG - [SDR COMA0160102](https://openairdocs.org/sdr/COMA0160102), Jan 12, 2001: ELEMENT. MALFUNCTIONED. RT 14TH STAGE BLEED AIR LEAK WARNING. REPLACED THE PYLON LEAK SENSE ELEMENT. - [SDR COMA0061035](https://openairdocs.org/sdr/COMA0061035), Dec 12, 2000: WARNING SYSTEM. MALFUNCTIONED. CABIN DOOR HANDLE CAUTION MESSAGE. COULD NOT DUPLICATE. CLEANED WIRING CONNECTION, OPERATIONAL CHECK SATISFACTORY. - [SDR COMA0060124](https://openairdocs.org/sdr/COMA0060124), Jan 29, 2000: FCU. MALFUNCTIONED. RIGHT ENGINE OVER SPEED. REPLACED RIGHT ENGINE FUEL CONTROL. - [SDR COMA0060016](https://openairdocs.org/sdr/COMA0060016), Dec 28, 1999: ACTUATOR. MALFUNCTIONED. FLAPS FAILED AT 37 DEGREES DURING LANDING APPROACH. REPLACED LEFT WING NR 3 FLAP ACTUATOR. ## 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 20080410837819I](https://openairdocs.org/incident/20080410837819I), Apr 10, 2008: Cndair CL6002B19 (N797CA), New York, NY, No damage. (-23) While colgan air was taxiing for takeoff on runway 13 via taxiway bravo, aircraft was stopped inline behind other aircraft on bravo at intersection of… --- 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.