# N952CA: 1995 Canadair CL-600-2B19, registration cancelled 2008-05-05

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 5, 2008
- Status when cancelled: Sale reported
- 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: 7092
- Year built: 1995
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 11, 1996
- Last registry action: May 9, 2007
- Mode S code: AD3C48
- Location: [Doral, FL](https://openairdocs.org/faa-place/FL/Doral)
- Owner type: Individual
- Owner's area on the map: 25.8050° N, 80.3151° W: Placed by OpenAirDocs at the center of ZIP code 33122, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N952CA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=952CA
- Page: https://openairdocs.org/deregistered/N952CA-2008-05-05

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 (77, newest 50)

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

- [SDR COMA0660313](https://openairdocs.org/sdr/COMA0660313), Apr 25, 2006: PITOT TUBE. CONTAMINATED. FLIGHT 5288 - ON TAKEOFF ROLL OBSERVED NO STANDBY INDICATION. TAKEOFF ABORTED. A/C FERRIED FROM YHZ TO CVG. PURGED WATER FROM STANDBY PITOT SYSTEM.
- [SDR COMA0660232](https://openairdocs.org/sdr/COMA0660232), Mar 6, 2006: REDUCER. FAULTY. FLIGHT 5145 - EN ROUTE CVG-AVP A NUISANCE SQUEALING NOISE EMITTING FROM GALLEY AREA, FLIGHT RETURNED TO THE FIELD. REPLACED THE GALLEY DRAIN REDUCER.
- [SDR COMA0660139](https://openairdocs.org/sdr/COMA0660139), Feb 12, 2006: FLAP SYSTEM. MALFUNCTIONED. FLIGHT 5802 - UPON FLAP RETRACTION DURING PRE-FLIGHT INSPECTION RECEIVED A FLAP FAIL CAUTION MESSAGE. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVEN
- [SDR COMA0560566](https://openairdocs.org/sdr/COMA0560566), Oct 25, 2005: WIRE. BROKEN. FLAPS FAIL CAUTION. REPAIRED BROKEN WIRE AT THE LT BPSU.
- [SDR COMA0460611](https://openairdocs.org/sdr/COMA0460611), Oct 31, 2004: APU. SHUTDOWN. FLIGHT 5028 APU SHUTDOWN. COULD NOT DUPLICATE. APU OPERATIONAL CHECK SATISFACTORY.
- [SDR COMA0460513](https://openairdocs.org/sdr/COMA0460513), Sep 9, 2004: CONNECTOR. LOOSE. 1ST SEGMENT OF EMERGENCY FLOOR PATH LIGHTING IS INOPERATIVE. SECURED LOOSE CONNECTOR. SYSTEM OPERATION NORMAL.
- [SDR COMA0460063](https://openairdocs.org/sdr/COMA0460063), Jan 17, 2004: SKIN. CORRODED. RIGHT SIDE CABIN FLOOR SIL ASSY HAS CORROSION ON TOP SURFACE FROM FS 516 THRU 544. CLEANED CORRODED AREA BY BLENDING OUT CORROSION. CUT OUT AREA THAT WAS OUT OF
- [SDR COMA0460051](https://openairdocs.org/sdr/COMA0460051), Jan 15, 2004: SKIN. CORRODED. WHILE PERFORMING TASK 002-57-900-60/601 FOUND CORROSION ON THE LOWER RT WING PLANK ACCESS HOLE CUTOUT (FOR PANEL 640BB) ON THE FORWAD AND AFT CHAMFERS. REMOVED 
- [SDR COMA0460047](https://openairdocs.org/sdr/COMA0460047), Jan 14, 2004: STIFFENER. CRACKED. VERTICAL BEAM CRACKED AT BL 0 BULKHEAD WEB AT FS 409+128 TOP RIVET LOCATION ON REINFORCING PLATE. PERFORMED A MAJOR REPAIR TO CRACKED VERTICAL BEAM, FS 409+128 
- [SDR COMA0460045](https://openairdocs.org/sdr/COMA0460045), Jan 14, 2004: FLOORBEAM. CORRODED. FLOORBEAM CAP AT FS 559+12 TO 620 AT LBL 27 CORRODED. REMOVED AND REPLACED CAP IAW WVAC EO 601R-53-4581.
- [SDR COMA0460044](https://openairdocs.org/sdr/COMA0460044), Jan 14, 2004: ANGLE. CRACKED. FS 484 RBL 27, OUTBOARD SUPPORT ANGLE/INTERCOSTAL CRACKED. REMOVED ANGLE FABRICATED REPAIR ANGLE FROM 2024-T3.063 (WVAC PO 32572) AND INSTALLED IAW BOMBARDIER R
- [SDR COMA0460043](https://openairdocs.org/sdr/COMA0460043), Jan 14, 2004: ANGLE. CRACKED. FS 484 LBL 27 OUTBOARD SUPPORT ANGLE/INTERCOSTAL CRACKED. REMOVED ANGLE, FABRICATED REPAIR ANGLE FROM 2024-T3.063 (WVAC PO 32572) AND INSTALLED IAW BOMBARDIER, 
- [SDR COMA0460042](https://openairdocs.org/sdr/COMA0460042), Jan 14, 2004: ANGLE. CRACKED. FS 484 RBL 36 INBOARD SUPPORT ANGLE/INTERCOSTAL CRACKED. REMOVED ANGLE, FABRICATED REPAIR ANGLE FROM 2024-T3.063 (WVAC PO 32572) AND INSTALLED IAW BOMBARDIER, I
- [SDR COMA0460041](https://openairdocs.org/sdr/COMA0460041), Jan 14, 2004: ANGLE. CRACKED. FS 484 LBL 36 INBOARD SUPPORT ANGLE/INTERCOSTAL CRACKED. REMOVED ANGLE, FABRICATED REPAIR ANGLE FROM 2024-T3.063 (WVAC PO 32572) AND INSTALLED IAW BOMBARDIER, I
- [SDR COMA0460040](https://openairdocs.org/sdr/COMA0460040), Jan 14, 2004: SKIN. CRACKED. LEFT WING LOWER WING PLANK SKIN AT WS 148.00 IS CRACKED. REMOVED DAMAGE, FABRICATED REPAIR DOUBLERS FROM 2024-T3.125 (WVAC PO 21137) AND FILLER FROM 2024-T3.100
- [SDR COMA0460039](https://openairdocs.org/sdr/COMA0460039), Jan 14, 2004: SKIN. DAMAGED. FS 310 FUSELAGE SKIN PREVIOUS BETYWEEN STRINGERS 16 AND 17 HAS SUSTAINED FURTHER DAMAGE. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER FROM 2024-T3.063 (WVAC PO 325
- [SDR COMA0460038](https://openairdocs.org/sdr/COMA0460038), Jan 14, 2004: SKIN. CRACKED. FS 235 RBL 6 NLG AFT DOOR CUT OUT HAS A .25 INCH CRACK ON FUSELAGE SKIN. REMOVED DAMAGE, FABRICATED REPAIR ANGLE FROM 2024-T42.063 (WVAC PO 169562), FILLER FROM
- [SDR COMA0460012](https://openairdocs.org/sdr/COMA0460012), Jan 2, 2004: ELEMENT. UNRELIABLE. FLIGHT 5874 LEFT 14TH STAGE BLEED LEAK WARNING. REPLACED THE LEFT PYLON BLEED LEAK SENSING ELEMENT.
- [SDR COMA0360382](https://openairdocs.org/sdr/COMA0360382), Aug 21, 2003: START VALVE. MALFUNCTIONED. FLIGHT 5868 RT ENGINE STARTER ENGAGED DURING FLIGHT 3 TIMES. REPLACED THE AIR START VALVE.
- [SDR COMA0360230](https://openairdocs.org/sdr/COMA0360230), May 4, 2003: TARGET. OUT OF ADJUST. LANDING GEAR DISAGREE WARNING; NLG DID NOT RETRACT. ADJUSTED THE NLG CENTERED PROXIMITY SENSOR TARGET.
- [SDR COMA0360108](https://openairdocs.org/sdr/COMA0360108), Feb 18, 2003: SHAFT. BENT. FLIGHT 5751 CABIN DOOR WARNING.COULD NOT DUPLICATE. REPLACED INNER HANDLE ROD END ROLLER.
- [SDR COMA0360072](https://openairdocs.org/sdr/COMA0360072), Feb 3, 2003: TARGET. LOOSE. FLIGHT 5156 GEAR DISAGREE WARNING.TIGHTENED LOOSE TARGET ONTHE L/H MLG UPLOCK.
- [SDR COMA0360055](https://openairdocs.org/sdr/COMA0360055), Jan 26, 2003: DOOR. FLIGHT 5850 DURING T/O A LARGE AMOUNT OF FLUID DRAINED FROM THE LIGHT CONTROL PANEL.RESEALED THE CREW DITCHING HATCH.
- [SDR COMA0260689](https://openairdocs.org/sdr/COMA0260689), Dec 2, 2002: DOOR LATCH. FLIGHT 5103 CABIN DOOR WARNING DURING FLIGHT.ADJUSTED CABIN DOOR LATCH MECHANISM.
- [SDR COMA0260680](https://openairdocs.org/sdr/COMA0260680), Nov 29, 2002: DOOR. FLIGHT 5478 CABIN DOOR WARNING MESSAGE.RIGGED/ADJUSTED THE CABIN DORO LATCHING MECHANISM TO M/M SPECIFICATIONS.
- [SDR COMA0260678](https://openairdocs.org/sdr/COMA0260678), Nov 27, 2002: ROLLER. WORN. FLIGHT 5465 CABIN DOOR LATCH CAUTION MESSAGE.REPLACED THE INNER HANDLE LATCH ROLLER.
- [SDR COMA0260672](https://openairdocs.org/sdr/COMA0260672), Nov 26, 2002: PROXIMITY SWITCH. MALFUNCTIONED. FLIGHT 5863 CABIN DOOR WARNING.REPLACED PROXIMITY SWITCH 546.
- [SDR COMA0260649](https://openairdocs.org/sdr/COMA0260649), Nov 16, 2002: ROD. BROKEN. FLIGHT 5459 CABIN ALTITUDE CAUTION MESSAGE - CABIN WOULD NOT PRESSURIZE.REPLACED BROKEN ROD ON CABIN DOOR VENT VALVE.
- [SDR COMA0260355](https://openairdocs.org/sdr/COMA0260355), Jun 4, 2002: LANDING GEAR. FLIGHT 5494 NOSE GEAR DISAGREE WARNING. NLG UNSAFE INDICATION.INSPECTED NLG AND PERFORMED EXT AND RETRACTION CHECKS. NO FAULTS FOUND.
- [SDR COMA0260245](https://openairdocs.org/sdr/COMA0260245), Apr 10, 2002: IGNITER. INOPERATIVE. FLIGHT 5877 LEFT ENGINE IGNITION STATUS MESSAGE.REPALCED THE ENGINE IGNITERS.
- [SDR COMA0260239](https://openairdocs.org/sdr/COMA0260239), Apr 6, 2002: AILERON. FLIGHT 6066 AILERON CONFIG WARNING DURING T/O.COULD NOT DUPLICATE. INSPECTED AILERON SYSTEM - NO ABNORMALTY FOUND.
- [SDR COMA0260120](https://openairdocs.org/sdr/COMA0260120), Feb 26, 2002: PYLON. CORRODED. DURING REMOVAL OF THE RIGHT ENGINE ASSEMBLY, DISCOVERED FRETTING/PITTING CORROSION ON THE AFT ENGINE PYLON THRUST FITTING MOUNTING VIB.REPAIRED IN ACCORDANCE WI
- [SDR COMA0260083](https://openairdocs.org/sdr/COMA0260083), Feb 1, 2002: BUSHING. SCORED. THE R/H VERTICAL STABILIZER BUSHING WAS SCORED AT HORIZONTAL STABILIZER PIVOT POINT.REMOVED THE SCORED BUSHING. MACHINED FLANGE OF NEW BUSHING P/N 600-21061-7S/
- [SDR COMA0160933](https://openairdocs.org/sdr/COMA0160933), Nov 27, 2001: SWITCH. MALFUNCTIONED. FLIGHT #5843. COPILOTS STABILIZER TRIM IS INTERMITTENT.REPLACED THE COPILOTS TRIM SWITCH.
- [SDR COMA0160709](https://openairdocs.org/sdr/COMA0160709), Sep 10, 2001: RADOME. FLIGHT #5420. DURING TAKE OFF AT CVG AIRCRAFT ENCOUNTERED MULTIPLE BIRD STRIKES ON RADOME, TAKE OFF WAS ABORTED AND RETURNED TO THE GATE.PERFORMED BIRD STRIKE A
- [SDR COMA0160329](https://openairdocs.org/sdr/COMA0160329), Mar 18, 2001: SKIN. CRACKED. RT LOWER WING PLANK CRACKED AT 2 LOCATIONS: 640 DB WS 95.950 AND 640 FB WS 136.676. BLENDED OUT DAMAGED AREAS AND ROTO-PEENED IAW REO 601R-57-21-030.
- [SDR COMA0061074](https://openairdocs.org/sdr/COMA0061074), Dec 26, 2000: HARNESS. FAILED. DURING CLIMB-OUT OF CVG, THE NR 1 AND 3 HYDRAULIC LOW PRESSURE CAUTION MESSAGES ACTIVATED, AIRCRAFT RETURNED TO THE FIELD. REPLACED THE FLAP POSITION HARNESS.
- [SDR COMA0060983](https://openairdocs.org/sdr/COMA0060983), Dec 2, 2000: SEAL. DAMAGED. PAX DOOR LEAKS DURING PRESURIZATION. RECONTOURED ADHESIVE FILLER AT PREVIOUS REPAIR ON PAX DOOR SEAL STRIKER FS 349 IAW REO 601R-52-11-008 REV B.
- [SDR COMA0060873](https://openairdocs.org/sdr/COMA0060873), Oct 31, 2000: COMPUTER. FALSE ACTIVATION. STALL FAIL MESSAGE DURING TAKEOFF. RESET THE STALL COMPUTER.
- [SDR COMA0060834](https://openairdocs.org/sdr/COMA0060834), Oct 14, 2000: CONTROL UNIT. MALFUNCTIONED. CONFIG AILERON WARNING MESSAGE DURING T/O. RESET SECU, COULD NOT DUPLICATE. RESET SECU NR 1 AND 2.
- [SDR COMA0060624](https://openairdocs.org/sdr/COMA0060624), Aug 4, 2000: STRUT. DISCHARGED. GEAR DISAGREE WARNING. WOW CAUTION MESSAGE. FOUND NLG SHOCK STRUT IMPROPERLY SERVICED. SERVICED STRUT IAW M/M.
- [SDR COMA0060565](https://openairdocs.org/sdr/COMA0060565), Jul 12, 2000: ANGLE. CORRODED. THE FORWARD J-ANGLE AT FS 280 BETWEEN LBL 9.0 AND RBL 9.0 IS CORRODED. PERFORMED A MAJOR REPAIR BY REPLACING CORRODED FORWARD J-ANGLE AT FS 280 BETWEEN LBL 9.0 
- [SDR COMA0060566](https://openairdocs.org/sdr/COMA0060566), Jul 11, 2000: DOUBLER. CORRODED. THE DOUBLER (P/N 601R38669-49) FORWARD OF THE SERVICE DOOR IS CORRODED. PERFORMED A MAJOR REPAIR BY REPLACING CORRODED DOUBLER (P/N 601R38669-49) FORWARD OF THE
- [SDR COMA0060554](https://openairdocs.org/sdr/COMA0060554), Jul 8, 2000: BEAM. CORRODED. TRANSVERSE BEAM AT FS 349 CORRODED BETWEEN LBL 9 AND LBL 27. REPAIRED TRANSVERSE BEAM AT FS 349 IAW WVAC EO 601R-53-1491A.
- [SDR COMA0060478](https://openairdocs.org/sdr/COMA0060478), Jun 6, 2000: AILERON. SLUGGISH. A/P TRIM CAUTION MESSAGE. LITTLE TO NO CONTROL OF AILERONS. ELEVATORS ALSO EXTREMELY DIFFICULT TO MOVE. COULD NOT DUPLICATE. INSPECTED ALL FLIGHT CONTROLS AND C
- [SDR COMA0060290](https://openairdocs.org/sdr/COMA0060290), Mar 26, 2000: LEAD. DEFECTIVE. EMERGENCY FLOOR PATH LIGHTING AT ROW 8 IS INOPERABLE. REPLACED POWER LEAD.
- [SDR COMA0060264](https://openairdocs.org/sdr/COMA0060264), Mar 12, 2000: LATCH. OUT OF ADJ. CABIN DOOR LATCH CAUTION MESSAGE. ADJUSTED CABIN DOOR LATCH MECHANISM.
- [SDR COMA0060191](https://openairdocs.org/sdr/COMA0060191), Feb 22, 2000: COMPUTER. COCKPIT. STALL FAIL CAUTION MESSAGE. RESET STALL COMPUTER, SYSTEM TEST NORMAL.
- [SDR COMA9960744](https://openairdocs.org/sdr/COMA9960744), Dec 5, 1999: SKIN. CRACK. LOWER HORIZONTAL SURFACE OF RIGHT LOWER WING ACCESS HOLE AT 640DB CRACKED. BLENDED OUT DAMAGE, ROTO-PEENED, AND ALODINED IAW REO 601R-57-21-030.
- [SDR COMA9960681](https://openairdocs.org/sdr/COMA9960681), Nov 6, 1999: DOUBLER. CRACKED. FS 718 RH5 AFT DOUBLER IS CRACKED BETWEEN STR 11-12. REPLACED CRACKED DOUBLER AT FS 718 RHS BETWEEN STR 11 AND 12 WITH NEW DOUBLERS IAW CRJ REO 601R-53-61-193.

All 77: https://openairdocs.org/deregistered/N952CA-2008-05-05/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 19971209040709I](https://openairdocs.org/incident/19971209040709I), Dec 9, 1997: Cndair CL600* (N952CA), Rochester, NY. Narrative: on Tuesday, December 9, 1997, at 2148 EST, a challenger CL-600, N952CA, flight 3610, operated by comair, inc., during descent phase into Rochester…

## Other aircraft with N952CA

- [Registered now](https://openairdocs.org/aircraft/N952CA): Boeing 747-428, S/N 25238, built 1991
- [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N952CA-undated): Douglas C-47, S/N 4316255. N-number assigned, not yet registered

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