# N954CA: 1995 Canadair CL-600-2B19, registration cancelled 2014-09-23

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 23, 2014
- Status when cancelled: First renewal notice
- 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: 7100
- Year built: 1995
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 8, 1996
- Certificate issued: August 15, 2007
- Last registry action: February 24, 2012
- Mode S code: AD43B6
- Owner when cancelled: [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC)
- Location: [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta)
- Owner type: Corporation
- Owner's area on the map: 33.6604° N, 84.3865° W: Placed by OpenAirDocs at the center of ZIP code 30354, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N954CA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=954CA
- Page: https://openairdocs.org/deregistered/N954CA-2014-09-23

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

## Service difficulty reports (84, newest 50)

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

- [SDR COMA2011022150019](https://openairdocs.org/sdr/COMA2011022150019), Feb 19, 2011: COMPUTER. FAILED. ON APPROACH INTO RIC WHEN SELECTING FLAPS 45 DEG RECEIVED GS DEPLOY CAUTION MSG, F/C PAGE SHOWED O/B GS DEPLOYED, SPOILERS WERE PHYSICALLY DEPLOYED. EMERGENCY D
- [SDR COMA2010041950099](https://openairdocs.org/sdr/COMA2010041950099), Apr 17, 2010: PROXIMITY SENSOR. FAILED. ON T/O FROM JFK RECEIVED NOSE DOOR OPEN WARNING MSG AND GEAR DISAGREE WARNING MSG. EMERGENCY DECLARED, A/C RETURNED TO JFK LANDED SAFELY. REMOVED AND REPLACED N
- [SDR COMA2010030950056](https://openairdocs.org/sdr/COMA2010030950056), Mar 8, 2010: SENSOR. OUT OF ADJUST. UPON T/O FROM DCA NOSE GEAR WOULD NOT RETRACT. PERFORMED QRH, EMERGENCY DECLARED. A/C DIVERTED TO IAD LANDED SAFELY. INSPECTED A/C FOUND NLG SENSOR PS14GA (NLG 
- [SDR COMA2010012150019](https://openairdocs.org/sdr/COMA2010012150019), Jan 20, 2010: ENGINE. FAILED. ON CLIMBOUT FROM BTV LOSS OF RIGHT ENGINE OIL PRESSURE, PERFORMED IFSD OF RIGHT ENGINE. EMERGENCY DECLARED, A/C RETURNED TO BTV LANDED SAFELY. REMOVED AND REPLA
- [SDR COMA2009111950217](https://openairdocs.org/sdr/COMA2009111950217), Nov 18, 2009: ANGLE. CRACKED. FS 559 CAP ANGLE CRACKED IN RADIUS AT LBL 18. REPAIRED CRACK AT RIGHT FS 559 IAW REO 601R-53-41-260, REV C.
- [SDR COMA2009111950216](https://openairdocs.org/sdr/COMA2009111950216), Nov 18, 2009: ANGLE. CRACKED. FS 559 CAP ANGLE CRACKED IN RADIUS AT RBL 9. REPAIRED CRACK AT RIGHT FS 559 IAW REO 601R-53-41-260, REV C.
- [SDR COMA2009111950215](https://openairdocs.org/sdr/COMA2009111950215), Nov 16, 2009: SKIN. GOUGED. SEVERAL GOUGES WERE FOUND ON THE TOP OF THE FUSELAGE UNDER THE ADF ANTENNA. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND FILLER IN ACCORDANCE WITH REO 
- [SDR COMA2009111050213](https://openairdocs.org/sdr/COMA2009111050213), Nov 9, 2009: BULKHEAD. CRACKED. FOUND A CRACK AT FS 621.00, ON THE AFT PRESSURE BULKHEAD AT THE LINTEL ATTACHMENT FITTING. REPAIRED REAR PRESSURE BULKHEAD IAW REO601R-53-61-1230 REV D, DATED J
- [SDR COMA2009110950212](https://openairdocs.org/sdr/COMA2009110950212), Nov 7, 2009: FLOOR SUPPORT. CRACKED. FOUND FLOOR SUPPORT ANGLE CRACKED AT FS 280.00 RBL 12. REMOVED AND REPLACED FORWARD FLOOR ANGLE IAW SRM 51-42-06.
- [SDR COMA2009110950211](https://openairdocs.org/sdr/COMA2009110950211), Nov 7, 2009: POST. CRACKED. FOUND CRACK ON I/B LOWER POST AT FS 409.00 + 128 RBL 27.00. REPAIRED LOWER POST IAW REO 601R-53-41-056.
- [SDR COMA2009110950210](https://openairdocs.org/sdr/COMA2009110950210), Nov 7, 2009: ANGLE. CRACKED. FOUND ANGLE CRACKED AT FS 280.00 LBL 12. REPAIRED ANGLE IAW REO 601R-53-11-034 REV A.
- [SDR COMA2009110950209](https://openairdocs.org/sdr/COMA2009110950209), Nov 7, 2009: ANGLE. CRACKED. FOUND ANGLE CRACKED AT FS 280.00 RBL 12. REPAIRED ANGLE IAW REO 601R-53-11-034 REV A.
- [SDR COMA2009110950208](https://openairdocs.org/sdr/COMA2009110950208), Nov 7, 2009: FLOORBEAM. CRACKED. FOUND FLOORBEAM CRACKED AT FS 280.00 RBL 12. REPAIRED FLOORBEAM IAW REO 601R-53-11-136.
- [SDR COMA2009110650207](https://openairdocs.org/sdr/COMA2009110650207), Nov 5, 2009: POST. CRACKED. FOUND CRACK ON O/B LOWER POST AT FS 409.00 + 128 LBL 18.00. REPAIRED LOWER POST IAW SRM 601R-53-41-056 AND 601R-53-41-889.
- [SDR COMA0860074](https://openairdocs.org/sdr/COMA0860074), Jan 17, 2008: THROTTLE CABLE. BROKEN. FLIGHT 5175 - LEFT ENGINE WOULD NOT RESPOND WHEN POWER LEVER BROUGHT TO IDLE. ABORTED APPROACH, PERFORMED IFSD, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REP
- [SDR COMA0760565](https://openairdocs.org/sdr/COMA0760565), Sep 10, 2007: INVERTER. FAULTY. FLIGHT 5243 - EMERGENCY LIGHT FLOOR STRIP AND SIDEWALL EMERGENCY EXIT LIGHTS INOP ROWS 9CD THROUGH 6CD. FOUND NR 3 BATTERY PACK INVERTER FAULTY. REPLACED INVERT
- [SDR COMA0760448](https://openairdocs.org/sdr/COMA0760448), Jun 20, 2007: SKIN. CRACKED. LEFT WING PLANK IS CRACKED AT WS 148.019. REPAIRED PER REO 601R-57-21-130.
- [SDR COMA0760447](https://openairdocs.org/sdr/COMA0760447), Jun 20, 2007: SKIN. CRACKED. RIGHT WING PLANK IS CRACKED AT WS 148.019. REPAIRED PER REO 601R-57-21-130.
- [SDR COMA0660677](https://openairdocs.org/sdr/COMA0660677), Dec 3, 2006: CHANNEL. CRACKED. LEFT REAR SPAR CHANNEL IN WHEEL WELL AT WS 58.88 FWD OF COVER PANEL HAS A 1 INCH CRACK IN THE TOP CORNER. APPLIED DOUBLER TO LEFT REAR SPAR CHANNEL PER EA 10-57
- [SDR COMA0660676](https://openairdocs.org/sdr/COMA0660676), Dec 3, 2006: HOUSING. CRACKED. DURING LC2 INSPECTION FOUND AVIONICS DOOR CRACKED AT HANDLE SUPPORT HOUSING. REMOVED AND REPLACED HANDLE SUPPORT HOUSING IAW CRJ SRM 51-40-11.
- [SDR COMA0660291](https://openairdocs.org/sdr/COMA0660291), Apr 6, 2006: LIGHT. INOPERATIVE. FLIGHT 5454 - THE EMERGENCY FLOOR LEVEL LIGHTS FAILED TO ILLUMINATE DURING TEST FROM ROWS 2 THROUGH 5. DEFERRED THE ELECTROLUMINESCENT FLOOR PROXIMITY EMERGENCY
- [SDR COMA0560803](https://openairdocs.org/sdr/COMA0560803), Jan 6, 2006: BPSU. UNRELIABLE. FLIGHT 5206 - FLAPS FAIL CAUTION. REPLACED THE LT BPSU.
- [SDR COMA0560692](https://openairdocs.org/sdr/COMA0560692), Dec 7, 2005: OXYGEN MASKS. DEPLOYED. FLIGHT 5850 - O2 MASK DEPLOYED DURING DEPRESS. REMOVED AND REPLACED O2 GENERATORS THAT DEPLOYED.
- [SDR COMA0560691](https://openairdocs.org/sdr/COMA0560691), Dec 7, 2005: VALVE. OBSTRUCTED. FLIGHT 5850 - RAPID DEPRESSURIZATION. FOUND INSULATION BLANKET SUCKED INTO OUT FLOW VALVE. SECURED INSULATION AND OPERATIONAL CHECK OF PRESS SYSTEM NORMAL.
- [SDR COMA0560443](https://openairdocs.org/sdr/COMA0560443), Aug 12, 2005: WARNING LIGHT. OPEN. FLIGHT 5383 - GROUND POWER SWITCH PANEL OPENED IN FLIGHT. INSPECTED FOR DAMAGE AND CLOSED DOOR.
- [SDR COMA0460615](https://openairdocs.org/sdr/COMA0460615), Nov 12, 2004: FAN BLADE. VIBRATES. FLIGHT 5037 LEFT ENGINE N2 VIBE INDICATION. REPLACED THE LEFT ENGINE FAN BLADES.
- [SDR COMA0460499](https://openairdocs.org/sdr/COMA0460499), Sep 1, 2004: LIGHT. INOPERATIVE. FLIGHT 5378 EMERGENCY FLOOR LIGHTS INOP ROW 9 THRU 12. REPLACED FLOOR LIGHT STRIP ROW 9 THRU 12.
- [SDR COMA0460272](https://openairdocs.org/sdr/COMA0460272), Apr 13, 2004: ECU. MALFUNCTIONED. FLIGHT 5852 FLAPS FAILED CAUTION MESSAGE. REPLACED THE FECU.
- [SDR COMA0460080](https://openairdocs.org/sdr/COMA0460080), Jan 25, 2004: WARNING LIGHT. ILLUMINATED. FLIGHT 5792 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
- [SDR COMA0460311](https://openairdocs.org/sdr/COMA0460311), Dec 1, 2003: FLOOR PANEL. CRACKED. PRESSURE FLOOR SKIN CRACKED IN WING BOX AREA. REPAIRED IAW REO 601R-53-41-102.
- [SDR COMA0360500](https://openairdocs.org/sdr/COMA0360500), Nov 16, 2003: FLAP. MALFUNCTIONED. FLIGHT 5044 FLAPS FAIL WARNING. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
- [SDR COMA0360025](https://openairdocs.org/sdr/COMA0360025), Jan 13, 2003: LAMP. INOPERATIVE. FLIGHT 5214 FLOOR EMERGENCY LIGHTS ARE INOP ROW 8 AFT.REPLACED FLOOR LIGHT STRIP.
- [SDR COMA0360003](https://openairdocs.org/sdr/COMA0360003), Jan 3, 2003: WINDSHIELD. BROKEN. FLIGHT 6029 COPILOTS WINDSHIELD SHATTERED.REPLACED WINDSHIELD
- [SDR COMA0260490](https://openairdocs.org/sdr/COMA0260490), Aug 18, 2002: FLAP. FLIGHT 6008 FLAPS FAILED AT 8 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINTENANE PER AD 98-20-01.
- [SDR COMA0260182](https://openairdocs.org/sdr/COMA0260182), Mar 11, 2002: FLAP. FLIGHT 5447 FLAPS FAILED WHEN SELECTED TO 30 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 9-20-01.
- [SDR COMA0260110](https://openairdocs.org/sdr/COMA0260110), Feb 16, 2002: CONTROL HANDLE. MALFUNCTIONED. FLIGHT 5806 NLG DOORS OPENED IN FLIGHT - GEAR DISAGREE WARNING.REPLACED THE L/G CONTROL - SELECTOR ASSY.
- [SDR COMA0260023](https://openairdocs.org/sdr/COMA0260023), Jan 1, 2002: WINDSHIELD. BROKEN. FLIGHT 5956 COPILOTS WINDSHIELD SHATTERED.REPLACED COPILOTS WINDSHIELD.
- [SDR COMA0260004](https://openairdocs.org/sdr/COMA0260004), Dec 28, 2001: BEAM. CRACKED. ENGINE SUPPORT BEAM CRACK.REPAIRED DAMAGE IN ACCORDANCE WITH CANADAIR REO 601-53-61-345.
- [SDR COMA0160832](https://openairdocs.org/sdr/COMA0160832), Oct 21, 2001: RUDDER. FLIGHT #5775 - CONFIG RUDDER WARNING DURING T/O.C.N.D. NO CONFIG WARNING WITH T/O POWER.
- [SDR COMA0160792](https://openairdocs.org/sdr/COMA0160792), Oct 8, 2001: SKIN. FLIGHT #5572. CREW REPORTED A BIRD STRIKE, LEFT WING TIP.C/W BIRDSTRIKE INSPECTION AND NO DAMAGE WAS FOUND.
- [SDR COMA0160421](https://openairdocs.org/sdr/COMA0160421), Jul 2, 2001: PLANK. CRACKED. L/H LOWER WING PLANK CRACKED AT 540 CB - W.S. 76.161 & 550BB - W.S. 188.040. AND R/H LOWER WING PLANK CRACKED AT 610BB - W.S. 32.263 & 640 CB, W.S. 16.161.BLEND
- [SDR COMA0160098](https://openairdocs.org/sdr/COMA0160098), Jan 13, 2001: SPINNER. VIBRATION. LEFT ENGINE FAN VIB INDICATED 2.7. REPLACED THE AFT FAN SPINNER (OUT OF BALANCE).
- [SDR COMA0061057](https://openairdocs.org/sdr/COMA0061057), Dec 16, 2000: COMPUTER. MALFUNCTIONED. Stall Fail message during T/O. Reset the stall computer
- [SDR COMA0061046](https://openairdocs.org/sdr/COMA0061046), Dec 16, 2000: WARNING SYSTEM. ACTIVATED. CONFIG SPOILERS CAUTION MESSAGE. COULD NOT DUPLICATE. NO FAULT CODES IN SECU. SYSTEM TEST NORMAL.
- [SDR COMA0060978](https://openairdocs.org/sdr/COMA0060978), Nov 29, 2000: WARNING SYSTEM. FALSE ACTIVATION. PITOT BASE HEAT CAUTION MESSAGE. RESET POWER, VERIFIED PITOT BASE HEAT OPERABLE. COULD NOT DUPLICATE.
- [SDR COMA0060877](https://openairdocs.org/sdr/COMA0060877), Nov 3, 2000: LIGHT. MALFUNCTIONED. EMERGENCY FLOOR LIGHTS ROW 8 AND 9 ARE INOPERABLE. COULD NOT DUPLICATE. SYSTEM TEST SATISFACTORY.
- [SDR COMA0060843](https://openairdocs.org/sdr/COMA0060843), Oct 22, 2000: ANGLE. BENT. PASSENGER DOOR SEAL STRIKERS AT FS 310.0 AND FS 349.0 HAVE PREVIOUS REPAIRS DAMAGED. PERFORMED A MAJOR REPAIR TO DAMAGED SEAL STRIKERS AT FS 310 AND FS 349 IAW 
- [SDR COMA0060812](https://openairdocs.org/sdr/COMA0060812), Oct 8, 2000: LAMP. INOPERATIVE. FWD HALF OF EMERGENCY FLOOR LIGHTING IS INOP. REPLACED FLOOR TRACK LIGHT.
- [SDR COMA0060510](https://openairdocs.org/sdr/COMA0060510), Jun 16, 2000: COMPUTER. MALFUNCTIONED. STALL FAIL MESSAGE DURING TAKEOFF. REPLACED THE STALL COMPUTER.
- [SDR COMA0060526](https://openairdocs.org/sdr/COMA0060526), Jun 15, 2000: SENSOR. MALFUNCTIONED. STALL FAIL MESSAGE DURING TAKEOFF. REPLACED THE AOA SENSOR.

All 84: https://openairdocs.org/deregistered/N954CA-2014-09-23/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 20080316013909I](https://openairdocs.org/incident/20080316013909I), Mar 16, 2008: Cndair CL6002B19 (N954CA), Harrisburg, PA, Minor damage. (-23) Comair 5184, CRJ1, returned and landed on runway 31 after reporting a bird ingested into the number 2 engine.

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