# N812CA: 2000 Bombardier CL-600-2B19, registration cancelled 2019-10-29 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 29, 2019 - 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: 7381 - Year built: 2000 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 20, 2000 - Certificate issued: August 7, 2019 - Last registry action: August 7, 2019 - Mode S code: AB10FD - 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/N812CA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=812CA - Page: https://openairdocs.org/deregistered/N812CA-2019-10-29 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 (54, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR COMA2012030150011](https://openairdocs.org/sdr/COMA2012030150011), Feb 29, 2012: STIFFENER. CRACKED. VERTICAL CHANNEL (STIFFENER) WAS FOUND TO BE CRACKED. REPLACED CHANNEL (STIFFENER) IAW CRJ 200 SRM 51-42-06. - [SDR COMA0212030150010](https://openairdocs.org/sdr/COMA0212030150010), Feb 29, 2012: FRAME. CORRODED. FUSELAGE FRAME FOUND TO BE CORRODED BEYOND LIMITS. REPAIRED FRAME IAW CRJ 200 SRM 53-00-15 AND CRJ 200 MDTM 51-20-08. - [SDR COMA2010030150047](https://openairdocs.org/sdr/COMA2010030150047), Feb 25, 2010: SELECTOR VALVE. FAILED. ON CLIMBOUT FROM DTW DURING GEAR RETRACTION RECEIVED NOSE GEAR DISAGREE AND GEAR DOOR OPEN WARNING MSG. EMERGENCY DECLARED, A/C RETURNED TO DTW LANDED SAFELY. R - [SDR COMA2010012950026](https://openairdocs.org/sdr/COMA2010012950026), Jan 29, 2010: ANGLE. CRACKED. FS 559 CAP ANGLE CRACKED AT RBL 18.00. REPAIRED FS 559 CAP ANGLE AT RBL 18.00 IAW REO 601R-53-41-260 REV D AND DEVIATION 601R-53-41-609 REV B. - [SDR COMA2010012650024](https://openairdocs.org/sdr/COMA2010012650024), Jan 26, 2010: ANGLE. CRACKED. FS 559 LEFT CAP ANGLE CRACKED AT LBL 18.00. REPAIRED CRACK AT LEFT FS 559 IN ACCORDANCE WITH REO 601-53-41-260 REV D DATED 17-SEP-2009. - [SDR COMA2010012550022](https://openairdocs.org/sdr/COMA2010012550022), Jan 22, 2010: BULKHEAD. CRACKED. REAR PRESSURE BULKHEAD AT FS 621.00 LINTEL ATTACHMENT FITTING CRACKED. REPAIRED AFT PRESSURE BULKHEAD WEB FS 621.00 LINTEL INSTALLATION IAW REO 601R-53-61-1230. - [SDR COMA2010012550021](https://openairdocs.org/sdr/COMA2010012550021), Jan 22, 2010: BULKHEAD. CRACKED. AFT PRESSURE BULKHEAD CRACKED AT FS 621.00 LBL 27.50 ABOVE CARGO DOOR TRACK. REPAIRED AFT PRESSURE BULKHEAD FS 621.00 LBL 27.50 IAW REO 601R-53-61-1541. - [SDR COMA2010012550020](https://openairdocs.org/sdr/COMA2010012550020), Jan 22, 2010: POST. CRACKED. FS 409+128 CRACKED ON POST AT LBL 18.00 OUTBOARD RADIUS. REPAIRED LOWER OUTBOARD POST LBL 18.00 AT FS 409+128 IAW REO 601R-53-41-056. - [SDR COMA0760698](https://openairdocs.org/sdr/COMA0760698), Dec 7, 2007: ANTI-ICE VALVE. FAULTY. FLIGHT 5137 - ON CLIMBOUT FROM CVG TO YYZ RECEIVED LEFT COWL ANTI-ICE INOP MESSAGE. CREW DECLARED EMERGENCY AND RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED - [SDR COMA0760697](https://openairdocs.org/sdr/COMA0760697), Dec 7, 2007: RELIEF VALVE. FAULTY. FLIGHT 5137 - ON CLIMBOUT FROM CVG TO YYZ RECEIVED LEFT COWL ANTI-ICE INOP MESSAGE. CREW DECLARED EMERGENCY AND RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED - [SDR COMA0760543](https://openairdocs.org/sdr/COMA0760543), Aug 26, 2007: UNKNOWN. MALFUNCTIONED. FLIGHT 5113 - ON CLIMB, BOX A ON PFD FLASHED 2-3 SECONDS, FOLLOWED BY AUTO-PILOT DISCONNECT. NOTICED STIFFNESS IN CONTROLS WHEN TURNING LEFT. RETURNED TO ATL. L - [SDR COMA0760290](https://openairdocs.org/sdr/COMA0760290), Mar 26, 2007: FLAPPER VALVE. OBSTRUCTED. FLIGHT 5244 - RECEIVED PAX DOOR CAUTION AND CABIN PRESSURE INCREASE ON CLIMBOUT. PERFORMED QRH. RETURNED TO PIT AND LANDED WITHOUT INCIDENT. CLEARED FOD FROM PA - [SDR COMA0760162](https://openairdocs.org/sdr/COMA0760162), Feb 6, 2007: BPSU. FAULTY. FLIGHT 5331 - EN ROUTE BOS-YHZ RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT BRAKE POS - [SDR COMA0760161](https://openairdocs.org/sdr/COMA0760161), Feb 6, 2007: ACTUATOR. FAULTY. FLIGHT 5331 - EN ROUTE BOS-YHZ RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT OUTBOARD - [SDR COMA0760149](https://openairdocs.org/sdr/COMA0760149), Feb 6, 2007: SPOILER SYS. MALFUNCTIONED. FLIGHT 9459 - DURING TAKEOFF ROLL RECEIVED A CONFIG SPOILER MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GATE. PERFORMED SYSTEM RESET WITH NO FURTHER DISCREPANC - [SDR COMA0760145](https://openairdocs.org/sdr/COMA0760145), Feb 5, 2007: FLAP SYSTEM. MALFUNCTIONED. FLIGHT 5567 - DURING BTR APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. COMPLIED WITH AD 2006-12- - [SDR COMA0760091](https://openairdocs.org/sdr/COMA0760091), Jan 29, 2007: SHAFT. DAMAGED. FLIGHT 5170 - FLAP FAIL MESSAGE RECEIVED. ABORTED APPROACH, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOUND WATER IN SYSTEM, REPLACED RIGHT NR 3 FLEX DRIVE S - [SDR COMA0760090](https://openairdocs.org/sdr/COMA0760090), Jan 29, 2007: SHAFT. CORRODED. FLIGHT 5170 - FLAP FAIL MESSAGE RECEIVED. ABORTED APPROACH, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOUND WATER IN SYSTEM, REPLACED LEFT NR 5 FLEX SHAFT. - [SDR COMA0760034](https://openairdocs.org/sdr/COMA0760034), Jan 20, 2007: BPSU. FAULTY. FLIGHT 5168 - FLAPS FAIL MESSAGE WHEN SELECTING 30 DEGREES. FAILED AT 20 DEGREES. REMOVED AND REPLACED RIGHT BPSU. - [SDR COMA0760035](https://openairdocs.org/sdr/COMA0760035), Jan 19, 2007: FLAP. MALFUNCTIONED. FLIGHT 5168 - ON APPROACH FLAPS SELECTED TO 30 BUT REMAINED AT 20 DEGREES. RECEIVED FLAPS FAIL CAUTION MESSAGE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE - [SDR COMA0660646](https://openairdocs.org/sdr/COMA0660646), Nov 20, 2006: WINDSHIELD. CRACKED. FLIGHT 5584 - DURING DESCENT INTO JAX THE CAPTAIN'S WINDSHIELD CRACKED. REPLACED THE CAPAIN'S WINDSHIELD. - [SDR COMA0660299](https://openairdocs.org/sdr/COMA0660299), Apr 10, 2006: ENGINE. FAILED. FLIGHT 9754 - DURING EWR APPROACH AN ABNORMAL NOISE WAS HEARD EMANATING FROM THE RIGHT ENGINE, FOLLOWED BY SLUGGING N1 AND N2 RESPONSE WITH POWER LEVER MOVEMENT - [SDR COMA0560808](https://openairdocs.org/sdr/COMA0560808), Jan 11, 2006: PDU. MALFUNCTIONED. FLIGHT 5354 - FLAPS FAIL CAUTION. REPLACED THE PDU. - [SDR COMA0560583](https://openairdocs.org/sdr/COMA0560583), Nov 2, 2005: ANTI-SKID SYS. WARNING LIGHT. FLIGHT 5904 - PARKING BRAKE SOV AND ANTI/SKID CAUTION. RESET SYSTEM. NO DEFECTS NOTED. - [SDR COMA0560494](https://openairdocs.org/sdr/COMA0560494), Sep 11, 2005: LATCH. MALFUNCTIONED. FLIGHT 5755 - DURING TAKEOFF ROLL RECEIVED A CABIN DOOR HANDLE CAUTION MESSAGE. ABORTED TAKEOFF AND RETURNED TO THE GATE. PERFORMED OPERATIONAL CHECK OF THE CAB - [SDR COMA0560208](https://openairdocs.org/sdr/COMA0560208), Mar 28, 2005: LEAD. FAILED. FLIGHT 5480 RECEIVED A LEFT WINDOW HEAT CAUTION DURING CLIMBOUT OF HSV, AIRCRAFT RETURNED TO THE FIELD. CONNECTED WINDOW ELECTRICAL LEADS TO SPARE TERMINALS. - [SDR COMA0560203](https://openairdocs.org/sdr/COMA0560203), Mar 24, 2005: SENSOR. MALFUNCTIONED. FLIGHT 5443 ABORTED TAKEOFF AT 10 KTS DUE TO LEFT JET OVERHEAT CAUTION, AIRCRAFT RETURNED TO THE GATE. DEFERRED JET OVERHEAT CAUTION PER MEL 16-11-02. - [SDR COMA0560204](https://openairdocs.org/sdr/COMA0560204), Mar 28, 2004: CONTROLLER. FAULTY. FLIGHT 5480 RECEIVED A LEFT WINDOW HEAT CAUTION DURING CLIMBOUT OF GSO, AIRCRAFT RETURNED TO THE FIELD. FERRIED THE AIRCRAFT TO MCO, REPLACED THE WINDOW HEAT CO - [SDR COMA0460175](https://openairdocs.org/sdr/COMA0460175), Feb 29, 2004: TARGET. LOOSE. FLIGHT 5173 GEAR DISAGREE WARNING, LT MLG INDICATES INTRANSIT. TIGHTENED THE PROX SWITCH TARGET ON THE LT MLG UPLOCK. - [SDR COMA0460057](https://openairdocs.org/sdr/COMA0460057), Jan 14, 2004: WINDSHIELD. FAILED. FLIGHT 5219 COPILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD. - [SDR COMA0460119](https://openairdocs.org/sdr/COMA0460119), Jan 3, 2004: STRINGER. DAMAGED. CARGO ENTRY WAY FORWARD FRAME AT FS 574.00 APPROXIMATELY STRINGER 15L HAS DAMAGE. COMPLIED WITH REO 601R-53-61-690 TO FACILITATE CARGO ENTRY WAY FORWARD FRAME F - [SDR COMA0460116](https://openairdocs.org/sdr/COMA0460116), Jan 3, 2004: FLOOR SUPPORT. CRACKED. CARGO FLOOR ANGLE AT FS 621.00 BULKHEAD, LEFT AND RIGH SUPPORT, CRACKED. COMPLIED WTIH BOMBARDIER REO 601R-53-61-004. PAINTED REPAIR IN ACCORDANCE WITH CRJ SRM - [SDR COMA0460115](https://openairdocs.org/sdr/COMA0460115), Jan 3, 2004: PLATE. CRACKED. CARGO FOOR LANDING PLATE AT FS 589 CRACKED FROM RIVET HOLE TO EDGE OF PLATE. COMPLIED WITH BOMBARDIER REO 601R-53-61-433. - [SDR COMA0460114](https://openairdocs.org/sdr/COMA0460114), Jan 3, 2004: PLATE. CRACKED. CARGO FLOOR LANDING PLATE AT FS 589 CRACKED FROM RIVET HOLE TO EDGE OF PLATE. COMPLIED WITH BOMBARDIER REO 601R-53-61-433. - [SDR COMA0260708](https://openairdocs.org/sdr/COMA0260708), Dec 11, 2002: COMPUTER. MALFUNCTIONED. FLIGHT 5263 AIRCRAFT UNABLE TO TRACK GLIDE SLOPE.REPLACED THE #2 VIR-432 - [SDR COMA0260533](https://openairdocs.org/sdr/COMA0260533), Sep 14, 2002: FLAP. FLAPS FAIL CAUTION MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. - [SDR COMA0260228](https://openairdocs.org/sdr/COMA0260228), Apr 1, 2002: DOOR. FLIGHT 6152 LOUD SQUEALING AND VIBRATION FROM R/H SIDE OF COCKPIT.GROUND INTERFONE DOOR FOUND OPEN - SECURED DOOR CLOSED - NO DAMAGE TO AIRCRAFT. - [SDR COMA0160490](https://openairdocs.org/sdr/COMA0160490), Jul 18, 2001: ACTUATOR. BINDING. FLAPS FAILED AT 43 DEGREES.REPLACED THE RIGHT HAND #1 AND #2 FLAP ACTUATORS. - [SDR COMA0160487](https://openairdocs.org/sdr/COMA0160487), Jul 18, 2001: ACTUATOR. BINDING. FLAPS FAILED AT 43 DEGREES.REPLACED THE RIGHT HAND #1 AND #2 FLAP ACTUATORS. - [SDR COMA0160324](https://openairdocs.org/sdr/COMA0160324), Mar 19, 2001: WARNING SYSTEM. FALSE ACTIVATION. EFIS COMP MON CAUTION DURING T/O. REPLACED THE NR 2 AHARS. - [SDR COMA0160299](https://openairdocs.org/sdr/COMA0160299), Mar 5, 2001: COMPUTER. MALFUNCTIONED. STALL FAIL CAUTION MESSAGE DURING T/O. RESET THE STALL COMPUTER. - [SDR COMA0160261](https://openairdocs.org/sdr/COMA0160261), Feb 17, 2001: BPSU. FAILED. FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU. - [SDR COMA0160051](https://openairdocs.org/sdr/COMA0160051), Jan 2, 2001: WARNING SYSTEM. FALSE ACTIVATION. CABIN DOOR OUTER HANDLE CAUTION MESSAGE. COULD NOT DUPLICATE. DOOR LATCH MECHANISM OPERATES NORMALLY. - [SDR COMA0160050](https://openairdocs.org/sdr/COMA0160050), Jan 2, 2001: SMOKE DETECTOR. FALSE INDICATION. SMOKE TOILET CAUTION MESSAGE, F/A REPORTS SMOKE AND ELECTRIC SMELL IN CABIN.COULD NOT DUPLICATE. REPLACED LAV SMOKE DETECTOR. - [SDR COMA0160045](https://openairdocs.org/sdr/COMA0160045), Dec 31, 2000: WARNING SYSTEM. FALSE ACTIVATION. SMOKE TOILET CAUTION MESSAGE. COULD NOT DUPLICATE. INSPECTED TOILET AND FOUND NO DISCREPANCY. - [SDR COMA0160018](https://openairdocs.org/sdr/COMA0160018), Dec 28, 2000: SKIN. DAMAGED. RT SIDE FUSELAGE SKIN WAS DAMAGED BETWEEN F.S. 700.0 AND 718.0 AT STR 18R.REPAIRED FUSELAGE DAMAGE BETWEEN F.S. 700.0 AND 718.0 AT STR 18R IAW WVAC EO 601R-53-2 - [SDR COMA0061033](https://openairdocs.org/sdr/COMA0061033), Dec 12, 2000: HANDLE. BROKEN. LANDING GEAR SELECTOR HANDLE BROKE OFF, WHEN GEAR SELECTED UP. REPLACED THE GEAR SELECTOR ASSY. - [SDR COMA0060961](https://openairdocs.org/sdr/COMA0060961), Nov 23, 2000: AMPLIFIER. MALFUNCTIONED. POWER LEVER SPLIT IN FLIGHT. REPLACED THE N1 CONTROL AMPLIFIER. - [SDR COMA0060920](https://openairdocs.org/sdr/COMA0060920), Nov 13, 2000: WARNING SYSTEM. MALFUNCTIONED. GEAR DISAGREE, PARKING BRAKE SOV, ANTI-SKID MESSAGE AND VIBRATION AFTER GEAR RETRACTION. COULD NOT DUPLICATE. OPERATIONAL TEST OF LANDING GEAR WAS SATISFACTORY. - [SDR COMA0060757](https://openairdocs.org/sdr/COMA0060757), Sep 15, 2000: COMPUTER. FAILED. STALL FAIL CAUTION MESSAGE DURING TAKEOFF ROLL, AIRCRAFT RETURNED TO GATE. RESET THE STALL COMPUTER. All 54: https://openairdocs.org/deregistered/N812CA-2019-10-29/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 20110417006889I](https://openairdocs.org/incident/20110417006889I), Apr 17, 2011: Bombardier Inc CL-600-2B19 (N812CA), Pittsburgh, PA, No damage. On April 17, 2011 at approximately 1627 eastern time, aircraft N812CA, a Bombardier CL-600-2B19, operating under title 14 CFR part 121, operated by comair… --- 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.