# N918CA: Canadair CL-600-2B19, registration cancelled 2011-03-09

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 9, 2011
- Exported to: Canada
- Status when cancelled: Valid registration
- Airframe: [Canadair CL-600-2B19](https://openairdocs.org/model/canadair-cl-600-2b19) (registry code 1900309)
- Data sheets: [TCDS A21EA-1](https://openairdocs.org/tcds/A21EA-1) (OpenAirDocs)
- Serial number: 7018
- Type of aircraft: Fixed wing multi engine
- Certificate issued: December 1, 2010
- Last registry action: December 1, 2010
- Mode S code: ACB496
- 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/N918CA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=918CA
- Page: https://openairdocs.org/deregistered/N918CA-2011-03-09

From the FAA registry file of November 3, 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 (114, newest 50)

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

- [SDR COMA2009062950166](https://openairdocs.org/sdr/COMA2009062950166), Jun 29, 2009: BULKHEAD. CRACKED. FS 202.75 FWD PRESSURE BULKHEAD CRACKED AT PARKING BRAKE CABLE CUTOUT. REPAIRED PER REO 601R-53-11 AND EA 10-5311-02657.
- [SDR COMA0860327](https://openairdocs.org/sdr/COMA0860327), Jul 20, 2008: STIFFENER. CRACKED. DURING MID CK 8, INSPECTION FOUND .25 INCH CRACK ON INBOARD SIDE LOWER END, OF VERTICAL STIFFENER, AT RBL 18, FS 559. CUT OUT DAMAGE AND INSTALLED DOUBLER PER B
- [SDR COMA0860319](https://openairdocs.org/sdr/COMA0860319), Jul 8, 2008: FRAME. CRACKED. DURING FA 640 FRAME INSPECTION FOUND 640 FRAME CRACKED ON LT SIDE AT STRINGER 9 CUTOUT. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED REPAIR DOUBLER IN ACCORDA
- [SDR COM2008F00002](https://openairdocs.org/sdr/COM2008F00002), Jul 8, 2008: FRAME. CRACKED. DURING FS 640 FRAME INSPECTION FOUND 640 FRAME CRACKED ON LT SIDE AT STRINGER 9 CUTOUT. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED REPAIR DOUBLER IN ACCORDA
- [SDR COMA0860311](https://openairdocs.org/sdr/COMA0860311), Jun 28, 2008: CIRCUIT BREAKER. TRIPPED. RECEIVED A GEAR DISAGREE AND HYDRAULIC PUMP 3B WARNING DURING CLIMBOUT OF JFK, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCID
- [SDR COMA0860116](https://openairdocs.org/sdr/COMA0860116), Feb 9, 2008: CONNECTOR. LOOSE. FLIGHT 5311 - RECEIVED PAX DOOR OUTER HANDLE CAUTION MESSAGE. DIVERTED TO GSP, LANDED WITHOUT INCIDENT. FOUND CARGO DOOR HARNESS CONNECTOR LOOSE. REMOVED, CLEAN
- [SDR COMA0760552](https://openairdocs.org/sdr/COMA0760552), Sep 1, 2007: BATTERY. DISCHARGED. FLIGHT 5348 - FORWARDS EMERGENCY LIGHTS WILL NOT COME ON. REMOVED AND REPLACED NR 1 BATTERY PACK.
- [SDR COMA0760502](https://openairdocs.org/sdr/COMA0760502), Jul 28, 2007: VALVE. MALFUNCTIONED. FLIGHT 5540 - OVERBOARD COOL CAUTION MESSAGE ON IN FLIGHT. AIRCRAFT DID NOT PRESSURIZE NORMALLY. AIRCRAFT RETURNED BACK TO SAV AND LANDED SAFELY. TRANSFERRED TO
- [SDR COMA0760490](https://openairdocs.org/sdr/COMA0760490), Jul 19, 2007: BULKHEAD. DAMAGED. PERMANENT REPAIR REQUIRED ON PREVIOUSLY APPLIED TEMP REPAIR TO FS 621.00 REAR PRESS BULKHEAD FRAME AT WEB BL 0.00 WL 111.09. APPLIED PERMANENT REPAIR ANGLE ON F
- [SDR COMA0760332](https://openairdocs.org/sdr/COMA0760332), Apr 19, 2007: BULKHEAD. CRACKED. DURING FS 559 INSPECTION FOUND 2 EA CRACKS AT SEMI-PRESSURE BULKHEAD, FS 559, RBL 9-18. REMOVED DAMAGE AND INSTALLED DOUBLER PER COMAIR SR10-5341-0001.
- [SDR COMA0760122](https://openairdocs.org/sdr/COMA0760122), Feb 2, 2007: WIRE HARNESS. FAULTY. FLIGHT 5020 - DURING TAXI-OUT TO THE RUNWAY RECEIVED AN ANTI-SKID CAUTION MESSAGE, AIRCRAFT RETURNED TO THE GATE. REPLACED THE RIGHT MLG OUTBOARD TRANSDUCER WIR
- [SDR COMA0660569](https://openairdocs.org/sdr/COMA0660569), Oct 4, 2006: CAUTION MESSAGE. ILLUMINATED. FLIGHT 5217 - AFTER TAKEOFF FROM JFK RECEIVED OVERBOARD COOL CAUTION MESSAGE AT 500 FT. AIRCRAFT WAS NOT PRESSURIZING. RETURNED TO JFK AND LANDED WITHOUT INCIDE
- [SDR COMA0660560](https://openairdocs.org/sdr/COMA0660560), Sep 25, 2006: STATUS MESSAGE. ILLUMINATED. FLIGHT 5001- AFTER TAKEOFF RECEIVED OVBD COOL CAUTION MESSAGE AND INBD COOL FAIL STATUS MESSAGE. RETURNED TO AIRPORT WITHOUT INCIDENT. AFTER LANDING BOTH MESSAG
- [SDR COMA0660414](https://openairdocs.org/sdr/COMA0660414), Jun 30, 2006: SMOKE DETECTOR. MALFUNCTIONED. FLIGHT 5061- EN ROUTE TO BTR OVER TYS RECEIVED CARGO SMOKE WARNING. FOLLOWED QRH PROCEDURE, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED NR 1 SMOKE 
- [SDR COMA0660394](https://openairdocs.org/sdr/COMA0660394), Jun 19, 2006: LEVER. OUT OF POSITION. FLIGHT 5612 - AC ESSENTIAL BUS MESSAGE IN FLIGHT WITH ASSOCIATED MESSAGES. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MANUAL RELEASE LEVER FOUND PU
- [SDR COMA0660325](https://openairdocs.org/sdr/COMA0660325), May 2, 2006: FLAP SYSTEM. FAILED. FLIGHT 5306 - ON APPROACH TO BWI FLAPS FAILED AT 30 DEGREES. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (B) 1, 2
- [SDR COMA0560728](https://openairdocs.org/sdr/COMA0560728), Dec 16, 2005: WARNING LIGHT. FALSE INDICATION. FLIGHT 5001- FOUND CABIN DOOR WARNING. OPERATED CABIN DOOR, NO DEFECTS FOUND.
- [SDR COMA0560656](https://openairdocs.org/sdr/COMA0560656), Nov 30, 2005: SWITCH. OUT OF ADJUST. FLIGHT 5672 - PARKING BRAKE CONFIG WARNING. ADJUSTED THE PARKING BRAKE MICROSWITCH.
- [SDR COMA0560651](https://openairdocs.org/sdr/COMA0560651), Nov 27, 2005: WARNING LIGHT. ILLUMINATED. FLIGHT 5058 - EN ROUTE CMI-CVG, RECEIVED AN ANTI-ICE DUCT WARNING MESSAGE, FLIGHT DIVERTED TO EVV. PERFORMED SYSTEM CHECK OF THE WING ANTI-ICE SYSTEM, CND.
- [SDR COMA0460698](https://openairdocs.org/sdr/COMA0460698), Dec 19, 2004: WINDSHIELD. CRACKED. FLIGHT 5435 CO-PILOTS WINDSHIELD CRACKED. REPLACED WINDSHIELD.
- [SDR COMA0460675](https://openairdocs.org/sdr/COMA0460675), Dec 10, 2004: WARNING SYSTEM. ACTIVATED. FLIGHT 5144 ANTI SKID CAUTION MESSAGE. COULD NOT DUPLICATE. INSPECTED SYSTEM AND OPERATIONAL CHECK, FOUND NO DEFECTS.
- [SDR COMA0460669](https://openairdocs.org/sdr/COMA0460669), Dec 8, 2004: OIL SYSTEM. OVERSERVICED. FLIGHT 5729 HIGH OIL TEMP CAUTION MESSAGE. FOUND ENGINE OIL SYSTEM OVERFILLED. DRAINED SYSTEM AND SERVICED TO PROPER LEVEL.
- [SDR COMA0460656](https://openairdocs.org/sdr/COMA0460656), Dec 1, 2004: CONTROL SYSTEM. MALFUNCTIONED. FLIGHT 5173 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
- [SDR COMA0460505](https://openairdocs.org/sdr/COMA0460505), Sep 5, 2004: TORQUE LINK. DISCONNECTED. FLIGHT 5666 AFTER TAKEOFF RECEIVED A NOSE GEAR UP DISAGREE CAUTION. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. RECONNECTED THE NLG TORQUE LINKS AND R
- [SDR COMA0460060](https://openairdocs.org/sdr/COMA0460060), Jan 15, 2004: INTERPHONE. NOISY. FLIGHT 5718 LOUD TICKING NOISE IN HEADSET DURING T/O. REPLACED THE APU BAY INTERPHONE UNIT.
- [SDR COMA0360565](https://openairdocs.org/sdr/COMA0360565), Dec 18, 2003: DOOR. OPEN. FLIGHT 5400 STALL FAIL WARNING AFTER T/O. LOUD BUZZ FROM NOSE AREA. FOUND 02 SERVICE DOOR OPEN. CLOSED SERVICE DOOR.
- [SDR COMA0360488](https://openairdocs.org/sdr/COMA0360488), Nov 6, 2003: PULLEY. DEFECTIVE. FLIGHT 5369 DURING CRUISE FLIGHT THE AILERON CONTROLS SEEMED TO REQUIRE MORE THAN NORMAL FORCE TO OPERATE. CREW ELECTED TO PERFORM AN EMERGENCY DESCENT TO LOWER
- [SDR COMA0360324](https://openairdocs.org/sdr/COMA0360324), Jul 18, 2003: SKIN PANEL. CRACKED. DURING COMPLIANCE OF TASK NR 002-53-160-610, 2 CRACKS WERE FOUND IN THE PRESSURE FLOOR SKIN NEAR FS 461.0, BETWEEN LBL 9.0 AND RBL 9.0. THE CRACKS RANGE FROM 2.
- [SDR COMA0360149](https://openairdocs.org/sdr/COMA0360149), Mar 13, 2003: FLAP. FLIGHT 5885 FLAPS FAIL CAUTION DURING TAXI.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
- [SDR COMA0360073](https://openairdocs.org/sdr/COMA0360073), Jan 31, 2003: WIRE HARNESS. DEFECTIVE. FLIGHT 5767 INBD ANTI SKID INOP CAUTION MESSAGE.REPLACED ANTI-SKID WIRE HARNESS.
- [SDR COMA0360031](https://openairdocs.org/sdr/COMA0360031), Jan 14, 2003: ACTUATOR. UNRELIABLE. FLIGHT 5575 FLAPS FAIL MESSAGE DURING APPROACH.REPLACED THE L/H #1 FLAP ACTUATOR.
- [SDR COMA0360027](https://openairdocs.org/sdr/COMA0360027), Jan 13, 2003: FLAP. OUT OF RIG. FLIGHT 5133 FLAPS FAIL MESSAGE DURING TAXI. FOUND THE FLAPS TO BE OUT OF RIG 130TH MECHANICALLY AND ELECTRICALLY. RIGGED FLAPS TO M/M SPECIFICATIONS.
- [SDR COMA0360022](https://openairdocs.org/sdr/COMA0360022), Jan 11, 2003: PDU. MALFUNCTIONED. FLIGHT 5621 FLAPS FAILED WHEN SELECTED TO 30 DEGREES.REPLACED THE PDU
- [SDR COMA0260727](https://openairdocs.org/sdr/COMA0260727), Dec 19, 2002: FLAP. FLAPS FAILED DURING TAXI.INSPECTED FLAP SYSTEM IAW AD 98-20-01.
- [SDR COMA0260615](https://openairdocs.org/sdr/COMA0260615), Oct 27, 2002: COALESCER BAG. DIRTY. FLIGHT 5906 BURNING SMELL FILLED COCKPIT.REPLACED THE COALESCER SOCKS ON THE L/H AND R/H ACM WATER SEPERATORS.
- [SDR COMA0260604](https://openairdocs.org/sdr/COMA0260604), Oct 24, 2002: OIL SYSTEM. FLIGHT 5796 APU LOW OIL PRESSURE CAUTION MESSAGE.SERVICED APU OIL - G OPERATONAL CHECKS NORMAL.
- [SDR COMA0260597](https://openairdocs.org/sdr/COMA0260597), Oct 20, 2002: APU. FLIGHT 5502 APU OIL PRESSURE CAUTION MESSAGE.COULD NOT DUPLICATE. OPERATIONAL CHECK OF APU WAS NORMAL.
- [SDR COMA0260542](https://openairdocs.org/sdr/COMA0260542), Sep 25, 2002: LANDING GEAR. FLIGHT 5968 GEAR DISAGREE MESSAGE - NLG DID NOT RETRACT.SERVICED THE NLG SHOCK STRUT WITH OIL AND N2 PER AMM.
- [SDR COMA0260544](https://openairdocs.org/sdr/COMA0260544), Sep 23, 2002: FLAP. FLIGHT 5258 FLAPS FAILED WHEN SELECTED UP AFTER T/O.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01.
- [SDR COMA0260540](https://openairdocs.org/sdr/COMA0260540), Sep 18, 2002: ELEMENT. FALSE ACTIVATION. FLIGHT 5064 R/H ANTI ICE DUCT WARNINGREPLACED FUSELAGE SECTION OF BLEED LEAK SENSING ELEMENT.
- [SDR COMA0260203](https://openairdocs.org/sdr/COMA0260203), Mar 19, 2002: TRIM SWITCH. FLIGHT 5407 T/O CONFIG TRIM WARNING.FOUND AILERON TRIM OUT OF T/O RANGE - OPERATIONAL CHECK OF TRIM SYSTEM WAS NORMAL.
- [SDR COMA0260087](https://openairdocs.org/sdr/COMA0260087), Jan 28, 2002: FUEL TANK. DAMAGED. WHEN L/H BOOST PUMP CANISTER WAS REMOVED FOR REPAIR, FOUND THE WIRING INSULATION PULLED BACK AND WIRE CONDUCTORS EXPOSED.REPLACED CANISTER.
- [SDR COMA0260067](https://openairdocs.org/sdr/COMA0260067), Jan 27, 2002: SKIN. CRACKED. LT FUEL BOOST PUMP ACCESS HOLES ARE CRACKED NR 1 (APPROX.125 INCH LONG BY.020 INCHDEEP), NR 9 (APPROX .200 INCH LONG BY.040 INCH DEEP) AND NR 11 (APPROX .200 IN
- [SDR COMA0260046](https://openairdocs.org/sdr/COMA0260046), Jan 13, 2002: ELEMENT. MALFUNCTIONED. FLIGHT 5991 L/H 14TH STAGE BLEED DUCT WARNING.REPLACED THE L/H PYLON LEAK DETECTOR ELEMENT.
- [SDR COMA0160930](https://openairdocs.org/sdr/COMA0160930), Nov 28, 2001: BEAM. CRACKED. ENGINE SUPPORT BEAM CRACKED.REPAIRED DAMAGE I/A/W REO 601-53-345.
- [SDR COMA0160769](https://openairdocs.org/sdr/COMA0160769), Sep 30, 2001: LIGHT. FLIGHT 5362. DURING INSPECTION FOUND THE FLOOR EMERGENCY EXIT FLOOR LIGHT BY THE CABIN DOOR INOPERATIVE.REPLACED FAULTY LIGHT ASSEMBLY.
- [SDR COMA0160659](https://openairdocs.org/sdr/COMA0160659), Aug 29, 2001: UPLOCK. FAULTY. FLIGHT #5266. SHORTLY AFTER TAKE OFF RECEIVED A NOSE LANDING GEAR DISAGREE LIGHT, AIRCRAFT RETURNED TO THE FIELD.REPLACED THE NOSE LANDING GEAR UPLOCK ASSEMBLY.
- [SDR COMA0160649](https://openairdocs.org/sdr/COMA0160649), Aug 27, 2001: SENSOR. FLIGHT #5572. AFTER TAKE OFF FROM GRB RECEIVED A NOSE LANDING GEAR DISAGREE CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIELD.ADJUSTED THE NOSE LANDING GEAR PS3GA
- [SDR COMA0160479](https://openairdocs.org/sdr/COMA0160479), Jul 15, 2001: BEAM. CRACKED. R/H ENGINE SUPPORT BEAM CRACKED FWD L/H SIDE.R/H ENGINE SUPPORT BEAM REPAIRED I/A/W REO 601R-53-61-366 REV B.
- [SDR COMA0160359](https://openairdocs.org/sdr/COMA0160359), Apr 10, 2001: INTERCOSTAL. CRACKED. FS 484 ANGLES CRACKED T LBL 27 INBOARD AND OUTBOARD. REPAIRED INTERCOSTALS AND ANGLES AT FS 484 IAW WVAC EO 601R-53-2375.

All 114: https://openairdocs.org/deregistered/N918CA-2011-03-09/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 19990908027199I](https://openairdocs.org/incident/19990908027199I), Sep 8, 1999: Cndair CL6002B19 (N918CA), Kansas City, MO. (-23) On September 8, 1999, comair, Canadair CL-600-2B19, N918CA, departed Kansas City International Airport (mci), and returned to mci, because nose gear…
- [Incident 19980731023079I](https://openairdocs.org/incident/19980731023079I), Jul 31, 1998: Cndair CL6002B19 (N918CA), Pittsburgh, PA. Smoke in cabin. Returned. Evacuated on runway. Put out fire in lavatory from careless smoker.

## Other aircraft with N918CA

- [Registered now](https://openairdocs.org/aircraft/N918CA): Beech A200, S/N BC-57, built 1978

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