# N709CA: 1998 Canadair CL-600-2B19, registration cancelled 2012-04-12

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 12, 2012
- Status when cancelled: Valid registration
- Airframe: [Canadair CL-600-2B19](https://openairdocs.org/model/canadair-cl-600-2b19) (registry code 1900309)
- 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: 7238
- Year built: 1998
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 22, 1998
- Certificate issued: May 14, 2008
- Last registry action: April 11, 2011
- Mode S code: A97630
- Owner when cancelled: [Bombardier Services Corp](https://openairdocs.org/faa-owner/BOMBARDIER%20SERVICES%20CORP)
- Location: [Colchester, VT](https://openairdocs.org/faa-place/VT/Colchester)
- Owner type: Non-citizen corporation
- Owner's area on the map: 44.5541° N, 73.2255° W: Placed by OpenAirDocs at the center of ZIP code 05446, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N709CA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=709CA
- Page: https://openairdocs.org/deregistered/N709CA-2012-04-12

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 Canadair CL-600-2B19: https://openairdocs.org/model/canadair-cl-600-2b19.md

## Service difficulty reports (55, newest 50)

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

- [SDR COMA0860092](https://openairdocs.org/sdr/COMA0860092), Jan 21, 2008: FLAP. MALFUNCTIONED. FLIGHT 5620 - FLAPS FAIL CAUTION MESSAGE, FLAPS FAILED AT 0 DEGREES. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I0001, FLAPS FAI
- [SDR COMA0760509](https://openairdocs.org/sdr/COMA0760509), Aug 1, 2007: OIL SYSTEM. LOW. FLIGHT 5387 - DURING CLIMBOUT RECEIVED LEFT ENGINE LOW OIL PRESS WARNING MESSAGE. AIRCRAFT RETURNED BACK TO CID AND LANDED SAFELY. INSPECTED LEFT ENGINE AND FOU
- [SDR COMA0760417](https://openairdocs.org/sdr/COMA0760417), May 31, 2007: SPRING. OUT OF RIG. FLIGHT 5503 - LEFT AND RIGHT AILERON MORE STIFF THAN NORMAL. -A- ON PFD WITH AUTO-PILOT ON, IN TURNS. HYD PUMP 1A SQUEALING. AILERONS FELT NORMAL WHEN DISCONNEC
- [SDR COMA0760322](https://openairdocs.org/sdr/COMA0760322), Apr 16, 2007: FLAP. MALFUNCTIONED. FLAPS FAIL CAUTION MSG. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESE
- [SDR COMA0660648](https://openairdocs.org/sdr/COMA0660648), Nov 22, 2006: ANTI-ICE VALVE. WARNING MESSAGE. FLIGHT 5380 - EN ROUTE TYS-CHS RECEIVED A LEFT COWL ANTI-ICE CAUTION MESSAGE, FLIGHT RETURNED TO TYS. RESET THE LEFT ENGINE COWL ANTI-ICE VALVE.
- [SDR COMA0660562](https://openairdocs.org/sdr/COMA0660562), Sep 30, 2006: ACTUATOR. FAULTY. FLIGHT 5008 - FLAPS FAIL MESSAGE, FLAPS FAILED AT ZERO DEGREES. REMOVED AND REPLACED LEFT INBOARD FLAP INBOARD ACTUATOR.
- [SDR COMA0660561](https://openairdocs.org/sdr/COMA0660561), Sep 30, 2006: ACTUATOR. FAULTY. FLIGHT 5008 - FLAPS FAIL CAUTION MESSAGE, FLAPS FAILED AT ZERO DEGREES. REMOVED AND REPLACED LEFT INBOARD FLAP OUTBOARD ACTUATOR.
- [SDR COMA0660554](https://openairdocs.org/sdr/COMA0660554), Sep 27, 2006: FLAP SYSTEM. MALFUNCTIONED. FLIGHT 5423 - EN ROUTE CVG-PWM RECEIVED A FLAP FAIL CAUTION AT ZERO DEGREES, CREW DECLARED AN EMERGENCY AND DIVERTED TO BGR. COMPLIED WITH AD 2006-12-21 FLAP CA
- [SDR COMA0660535](https://openairdocs.org/sdr/COMA0660535), Sep 8, 2006: FLAP SYSTEM. MALFUNCTIONED. FLIGHT 5253 - DURING TUL APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT ZERO DEGREES, CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. COMPLIED WITH AD
- [SDR COMA0660367](https://openairdocs.org/sdr/COMA0660367), May 31, 2006: TRANSDUCER. FAULTY. FLIGHT 5262 - EN ROUTE RIC-CVG RECEIVED A RIGHT ENGINE HIGH OIL PRESSURE WARNING, CREW DECLARED AN EMERGENCY, RETURNED TO RIC AND FLIGHT LANDED WITHOUT INCIDENT
- [SDR COMA0660201](https://openairdocs.org/sdr/COMA0660201), Feb 27, 2006: FLAP SYSTEM. MALFUNCTIONED. FLIGHT 5187 - DURING BTV APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 8 DEGREES, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. COMPLIED WIT
- [SDR COMA0560813](https://openairdocs.org/sdr/COMA0560813), Jan 16, 2006: WARNING LIGHT. ILLUMINATED. FLIGHT 5151- GENERATOR NR 2 CAUTION. SERVICED THE IDG OIL SYSTEM.
- [SDR COMA0560698](https://openairdocs.org/sdr/COMA0560698), Dec 8, 2005: COUPLING. DAMAGED. FLIGHT 4989 - FLAPS FAIL CAUTION. REPLACED THE NR 5 FLEX SHAFT.
- [SDR COMA0560687](https://openairdocs.org/sdr/COMA0560687), Dec 6, 2005: BPSU. UNRELIABLE. FLIGHT 5399 - FLAPS FAIL CAUTION. REPLACED THE LT BPSU.
- [SDR COMAO560319](https://openairdocs.org/sdr/COMAO560319), May 24, 2005: PSEU. MALFUNCTIONED. FLT 5183 - DISPLAY COOL CAUTION, CABIN ALTITUDE WARNING AND BURNING ODOR IN COCKPIT. REPLACED THE PSEU.
- [SDR COMA0560316](https://openairdocs.org/sdr/COMA0560316), May 23, 2005: WARNING LIGHT. ILLUMINATED. FLIGHT 9483 GEAR DISAGREE WARNING. FOUND NLG REQUIRED SERVICED. SERVICED NLG IAW MM.
- [SDR COMA0560309](https://openairdocs.org/sdr/COMA0560309), May 14, 2005: SHUTOFF VALVE. MALFUNCTIONED. FLIGHT 4987 - LT AND RT AIR CONDITIONING PACKS FAILED. REPLACED THE LEFT AND RIGHT 10TH STAGE PRSOV.
- [SDR COMA0560223](https://openairdocs.org/sdr/COMA0560223), Apr 3, 2005: BPSU. FAULTY. FLIGHT 5446 RECEIVED A FLAP FAIL CAUTION AFTER LANDING WHEN FLAPS WERE RETRACTED. REPLACED THE LEFT BPSU.
- [SDR COMA0560101](https://openairdocs.org/sdr/COMA0560101), Jan 30, 2005: WINDOW. CRACKED. FLIGHT 5530 PILOTS SIDE WINDOW CRACKED. REPLACED WINDOW.
- [SDR COMA0560020](https://openairdocs.org/sdr/COMA0560020), Jan 1, 2005: WARNING SYSTEM. MALFUNCTIONED. FLIGHT 5316, GEAR DISAGREE WARNING. COULD NOT DUPLICATE. FUNCTIONAL TEST OF LANDING GEAR EXTENSION AND RETRACTION SYSTEM NORMAL, NO DEFECTS FOUND.
- [SDR COMA0460356](https://openairdocs.org/sdr/COMA0460356), Jun 8, 2004: PRIORITY VALVE. UNRELIABLE. FLIGHT 5156 GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE.
- [SDR COMA0460366](https://openairdocs.org/sdr/COMA0460366), Jun 7, 2004: LANDING GEAR. LACK OF LUBE. FLIGHT 5334 GEAR DISAGREE WARNING, WHEN SELECTED DOWN. CLEAN AND LUBED LANDING GEAR.
- [SDR COMA0460231](https://openairdocs.org/sdr/COMA0460231), Mar 29, 2004: SMOKE DETECTOR. FALSE ACTIVATION. FLIGHT 5226 CARGO SMOKE WARNING, DISCHARGED CARGO FIRE BOTTLES. INSPECTED AND FOUND NO EVIDENCE OF OR CONDITION TO CAUSE SMOKE. REPLACED SMOKE DETECTORS.
- [SDR COMA0460071](https://openairdocs.org/sdr/COMA0460071), Jan 19, 2004: CONTROL UNIT. MALFUNCTIONED. FLIGHT 5839 STAB TRIM AND MACH TRIM DISENGAGED DURING FLIGHT. COULD NOT DUPLICATE. NO FAULT CODES IN COMPUTER. OPERATIONAL CHECK NORMAL.
- [SDR COMA0360485](https://openairdocs.org/sdr/COMA0360485), Nov 5, 2003: COMPUTER. FAULTY. FLIGHT 5485 - DURING CLIMBOUT OF MCO RECEIVED A FUEL IMBALANCE CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIELD. REPLACED THE FUEL COMPUTER.
- [SDR COMA0360484](https://openairdocs.org/sdr/COMA0360484), Nov 5, 2003: CONNECTOR. CONTAMINATED. FLIGHT 5484 DURING CLIMBOUT OF MCO RECEIVED A FUEL IMBALANCE CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIELD. CLEANED MOISTURE FROM CONNECTOR J425/P425.
- [SDR COMA0360455](https://openairdocs.org/sdr/COMA0360455), Oct 9, 2003: COMPUTER. MALFUNCTIONED. FLIGHT 5557 LEFT FUEL INDICATION INOP. REPLACED THE FUEL COMPUTER.
- [SDR COMA0360360](https://openairdocs.org/sdr/COMA0360360), Aug 11, 2003: THRUST REVERSER. MALFUNCTIONED. FLIGHT 5229 LT THRUST REVERSER UNLOCKED MESSAGE DURING FLIGHT. DEFERRED MAINT PER MEL.
- [SDR COMA0360113](https://openairdocs.org/sdr/COMA0360113), Feb 22, 2003: CAPACITOR. MALFUNCTIONED. FLIGHT 5022 FUEL QUANTITY INDICATION IS ERRATIC.REPLACED THE #6 FUEL QUANTITY PROBE.
- [SDR COMA0360081](https://openairdocs.org/sdr/COMA0360081), Feb 4, 2003: COMPUTER. MALFUNCTIONED. FLIGHT 5543 LEFT FUEL PUMP CAUTION AND FUEL IMBALANCE CAUTION MESSAGE.REPLACED THE FUEL COMPUTER.
- [SDR COMA0260308](https://openairdocs.org/sdr/COMA0260308), May 8, 2002: BELLCRANK. DIRTY. FLIGHT 5883 A/P TRIM LWD CAUTION MESSAGE. AILERONS VERY STIFF.COULD NOT DUPLICATE PROBLEM ON GROUND - AILERON AFT BELLCRANK ASSY WERE DETERMINED TO BE MOST PROB
- [SDR COMA0260247](https://openairdocs.org/sdr/COMA0260247), Apr 15, 2002: SKIN. DAMAGED. WHILE AIRCRAFT WAS AT HANGAR FOR OVERNIGHT, MAINTENANCE NOTICED EVIDENCE OF A LIGHTNING STRIKE ON RIGHT WING LOWER SKIN TOWARD TIP AT W.S.401.COMPLIED WITH LIGH
- [SDR COMA0260207](https://openairdocs.org/sdr/COMA0260207), Mar 23, 2002: FLAP. FLIGHT 5820 FLAPS FAILED AT 0 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
- [SDR COMA0160841](https://openairdocs.org/sdr/COMA0160841), Oct 23, 2001: WHEEL. CRACKED. DURING N.D.T. INSPECTION OF THE MLG WHEEL INBOARD SUB ASSEMBLY, DISCOVERED A CRACK AT THE SPOKE AREA.WHEEL WAS REMOVED FROM SERVICE AND SCRAPPED.
- [SDR COMA0160831](https://openairdocs.org/sdr/COMA0160831), Oct 21, 2001: CONTROL COLUMN. FLIGHT #5260. WHILE MOVING AILERONS THRU FULL RANGE OF TRAVEL, A SLIGHT BINDING CAN BE FELT AT FULL TRAVEL AND AT NEUTROL.RETROQUED THE NUT HOLDING YOKE TO CONT
- [SDR COMA0160797](https://openairdocs.org/sdr/COMA0160797), Oct 9, 2001: WEB. CRACKED. ENGINE SUPPORT BEAM LOWER WEB CRACKED BETWEEN FS 625.30 AND FS 640.00 AT WL 111.09, BL37 LT AND RT.PERFORMED TEMPORARY REPAIR I/A/W BOMBARDIER REO 601R-53-61-36
- [SDR COMA0160794](https://openairdocs.org/sdr/COMA0160794), Oct 6, 2001: DOUBLER. CRACKED. F.S.718 FRAME DOUBLER CRACKED ON LEFT SIDE OF FUSELAGE.REPAIRED LEFT SIDE DOUBLER I/A/W REO 601R-53-61-193 REV A.
- [SDR COMA0160093](https://openairdocs.org/sdr/COMA0160093), Jan 7, 2001: ENGINE. VIBRATION. RT ENGINE VIB INDICATION AT .7, ENGINE FAILED. REPLACED ENGINE.
- [SDR COMA0060975](https://openairdocs.org/sdr/COMA0060975), Nov 30, 2000: WARNING SYSTEM. ACTIVATED. CABIN DOOR HANDLE CAUTION MESSAGE. COULD NOT DUPLICATE. DOOR AND DOOR WARNING SYSTEM OPERATION SATISFACTORY.
- [SDR COMA0060884](https://openairdocs.org/sdr/COMA0060884), Nov 5, 2000: PANEL. CRACKED. CRACK IN LOWER HORIZONTAL SURFACE OF LT AND RT LOWER WING ACCESS HOLES .540FB WS 136.676, 540DB WS 95.950 AND 640 FB WS 136.676. BLENDED OUT DAMAGE, ROTO PEENED
- [SDR COMA0060436](https://openairdocs.org/sdr/COMA0060436), May 17, 2000: INTERCOSTAL. CRACKED. THE INTERCOSTAL BETWEEN LBL 9 AND LBL 18 AT FS 484.0 HAS A CRACK EXTENDING FROM THE RADIUS AT LBL 18. PERFORMED A MAJOR REPAIR TO CRACKED INTERCOSTAL AT LBL 18 
- [SDR COMA0060435](https://openairdocs.org/sdr/COMA0060435), May 17, 2000: SKIN. DENTED. THE FUSELAGE SKIN IS DENTED AFT OF THE CARGO DOOR AT FS 650 AND STRINGERS 20 - 21 LHS. PERFORMED A MAJOR REPAIR TO FUSELAGE SKIN AT FS 650 STR 20 - 21 LHS IAW W
- [SDR COMA0060425](https://openairdocs.org/sdr/COMA0060425), May 17, 2000: FLOOR SUPPORT. CRACKED. RIGHT FS 621 FLOOR SUPPORT ANGLE IS CRACKED. PERFORMED A MAJOR REPAIR AT FS 621 RIGHT FLOOR SUPPORT ANGLE IAW CANADAIR REO 601R-53-61-117.
- [SDR COMA0060097](https://openairdocs.org/sdr/COMA0060097), Jan 26, 2000: WARNING SYSTEM. ACTIVATED. CABIN DOOR WARNING. ADJUSTED DOOR LATCH MECHANISM.
- [SDR COMA0060096](https://openairdocs.org/sdr/COMA0060096), Jan 26, 2000: WARNING SYSTEM. ACTIVATED. CABIN DOOR WARNING COULD NOT DUPLICATE. OPERATION OF DOOR AND WARNING SYSTEM WAS NORMAL.
- [SDR COMA9960707](https://openairdocs.org/sdr/COMA9960707), Nov 22, 1999: VANE CAP. CHAFED. LEFT HAND AND RIGHT HAND INBOARD CAPS CHAFED LEFT HAND .027 RIGHT HAND .028. REMOVED CHAFED INBOARD FLAP VANE INBOARD CAPS AND INSTALLED NEW CAPS IAW WVAC EO 60
- [SDR COMA9960704](https://openairdocs.org/sdr/COMA9960704), Nov 20, 1999: DOUBLER. CRACKED. AFT DOUBLER (P/N 600-36030-32) AT FS 718 RWS STR 11-12 WAS CRACKED. PERFORMED A MAJOR REPAIR BY REPLACING AFT DOUBLER (P/N 600-36030-32) AT FS 718 RHS STR 11-12
- [SDR COMA9960701](https://openairdocs.org/sdr/COMA9960701), Nov 18, 1999: TE FLAP. FAILED. FLAPS WILL NOT RETRACT, FLAPS STUCK AT 26 DEGREES. RESET FLAP SYSTEM PER AD 98-20-01.
- [SDR COMA9960683](https://openairdocs.org/sdr/COMA9960683), Nov 14, 1999: PANEL. CHAFED. RIGHT HAND OUTBOARD LOWER COVER PANEL ON RIGHT HAND AILERON CHAFED BEYOND LIMITS. FABRICATED NEW PANEL AND INSTALLED AN AILERON IAW WVAC EO 601R-57-0619.
- [SDR COMA9960471](https://openairdocs.org/sdr/COMA9960471), Aug 24, 1999: PACK. MALFUNCTIONED. STRONG SULFURIC SMELL IN AIRCRAFT. DEFERRED LEFT HAND AIR CONDITIONING SYSTEM.

All 55: https://openairdocs.org/deregistered/N709CA-2012-04-12/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB NYC02IA097](https://openairdocs.org/ntsb/NYC02IA097), May 8, 2002: Bombardier CL600-2B19 (N709CA), Covington, KY, incident, no damage. Probable cause: The manufacturer's failure to provide inspection criteria for the BPSU compartment aileron control pulleys, which resulted in eventual pulley corrosion, and subsequent control stiffness when seized…

## Other aircraft with N709CA

- [Registered now](https://openairdocs.org/aircraft/N709CA): New Piper PA-28-181, S/N 2881729, built 2024

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