# N941CA: 1994 Canadair CL-600-2B19, registration cancelled 2018-04-18

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 18, 2018
- Status when cancelled: Registration expired, pending cancellation
- 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: 7050
- Year built: 1994
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 16, 1994
- Certificate issued: August 8, 2014
- Last registry action: August 8, 2014
- Mode S code: AD1112
- Owner when cancelled: [Golden Mile Aircraft Leasing Inc](https://openairdocs.org/faa-owner/GOLDEN%20MILE%20AIRCRAFT%20LEASING%20INC)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7236° N, 75.5412° W: Placed by OpenAirDocs at the center of ZIP code 19801, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N941CA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=941CA
- Page: https://openairdocs.org/deregistered/N941CA-2018-04-18

From the FAA registry file of November 4, 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 (102, newest 50)

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

- [SDR COMA20111850009](https://openairdocs.org/sdr/COMA20111850009), Jan 17, 2011: SENSING ELEMENT. FAILED. ON CLIMBOUT FROM JAX TO DCA RECEIVED RIGHT ANTI-ICE DUCT WARNING MSG. IN ICING CONDITIONS. EMERGENCY DECLARED, A/C DIVERTED TO GSO LANDED SAFELY. REMOVED AND RE
- [SDR COMA2010060450124](https://openairdocs.org/sdr/COMA2010060450124), Jun 4, 2010: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM RBL 27 FS 618 AROUND NUT PLATE EXCEEDS DAMAGE LIMITATIONS. REMOVED CORROSION AND REPAIRED FLOORBEAM AT FS 618 RBL 27 IAW EA 10-5361-02977
- [SDR COMA2010060150120](https://openairdocs.org/sdr/COMA2010060150120), May 30, 2010: BULKHEAD. CRACKED. BULKHEAD WEB CRACKED AROUND LINTEL ATTACH FITTING AT FS 621, LBL 36.2. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1230 REV D.
- [SDR COMA2010060150200](https://openairdocs.org/sdr/COMA2010060150200), May 30, 2010: BULKHEAD. CRACKED. BULKHEAD WEB CRACKED FS 621.00, LBL 18, JUST ABOVE WL 73.0. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLERS IAW REO 601R-53-61-1285.
- [SDR COMA2009120250222](https://openairdocs.org/sdr/COMA2009120250222), Dec 2, 2009: CONNECTOR. SHORTED. DURING CLIMBOUT FROM CVG RECEIVED AN ANTI-ICE CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. REPLACED SHORTED CONNECTOR (P58WK).
- [SDR COMA2009052750145](https://openairdocs.org/sdr/COMA2009052750145), May 24, 2009: ANGLE. CRACKED. LT 559 CAP ANGLE CRACKED AT FS 559.00, LBL 18.00. PERFORMED PERMANENT REPAIR IAW REO 601R-53-41-260.
- [SDR COMA2009052750144](https://openairdocs.org/sdr/COMA2009052750144), May 24, 2009: ANGLE. CRACKED. RT 559 CAP ANGLE CRACKED AT FS 559.00, RBL 18.00. PERFORMED PERMANENT REPAIR IAW REO 601R-53-41-260.
- [SDR COMA0860257](https://openairdocs.org/sdr/COMA0860257), May 23, 2008: SKIN. DAMAGED. FUSELAGE SKIN HAS DAMAGE FROM DOOR PIN AT FWD LOWER POSITION AT FS 310.00. TRIMMED OUT DAMAGE AND INSTALLED REPAIR PARTS PER REO 601R53-21-180 AND SR 99-5140-00
- [SDR COMA0860252](https://openairdocs.org/sdr/COMA0860252), May 21, 2008: FITTING. CRACKED. WHILE PERFORMING TASK CARD CRJ-2-122006, SPECIAL DETAILED INSP OF THE WINDSHIELD CENTER POST AND BULKHEAD AFT POST AT FS 202.75, FOUND LOWER RT POST FITTING TO 
- [SDR COMA0860251](https://openairdocs.org/sdr/COMA0860251), May 21, 2008: DOOR FRAME. CRACKED. PAX DOOR FRAME FS 338.9 IS CRACKED AT UPPER END. REPAIRED IAW REO 601R-52-11-402.
- [SDR COMA0860250](https://openairdocs.org/sdr/COMA0860250), May 21, 2008: FRAME. CRACKED. CARGO COMPARTMENT UNDERFLOOR FRAME SECTOR AT FS 605 IS CRACKED. REMOVED AND REPLACED WITH SERV FRAME IAW CRJ SRM 51-42-06 AND COMAIR SR99-5140-0001.
- [SDR COMA0860249](https://openairdocs.org/sdr/COMA0860249), May 21, 2008: BULKHEAD. CRACKED. TEMP REPAIR PREVIOUSLY APPLIED TO FS 559.0 BULKHEAD. REMOVED TEMP REPAIR AND PERFORMED PERMANENT REPAIR IAW COMAIR SR10-53-41-0001 REV A SECTION II.
- [SDR COMA0860248](https://openairdocs.org/sdr/COMA0860248), May 21, 2008: PRESSURE PANEL. CRACKED. WHILE PERFORMING TASK CARD CRJ-2-162011, PRESSURE FLOOR SKIN DETAILED INSPECTION FOUND 2 CRACKS IN THE PRESSURE FLOOR SKIN BETWEEN RBL 9 AND LBL 9. CRACKS MEASU
- [SDR COMA0860247](https://openairdocs.org/sdr/COMA0860247), May 21, 2008: FRAME. CORRODED. DURING A 72/48 MO INSPECTION, TASK CRJ-2-142005, FOUND FUSELAGE FRAME CORRODED ON TOP EDGE AND CRACKED ON LOWER EDGE. PERFORMED PERMANENT REPAIR IAW REO 601R-53
- [SDR COMA0860244](https://openairdocs.org/sdr/COMA0860244), May 14, 2008: SILL. CORRODED. SEVERE CORROSION FOUND ON LEFT FLOOR SILL BETWEEN FS 349.00 AND FS 364.00. REMOVED AND SPLICED SECTION OF FLOOR SILL IAW EA 10-5320-02217.
- [SDR COMA0860051](https://openairdocs.org/sdr/COMA0860051), Jan 4, 2008: UNKNOWN. UNKNOWN. FLIGHT 5262 - ON DESCENT INTO JFK RECEIVED PROX SYSTEM CAUTION MESSAGE. EMERGENCY DECLARED, MESSAGE WENT OUT BELOW 200 KTS AND BEFORE GEAR EXTENSION. ALL INDICA
- [SDR COMA0760199](https://openairdocs.org/sdr/COMA0760199), Feb 19, 2007: FLAP. MALFUNCTIONED. FLIGHT 5138 - FLAPS FAIL CAUTION MESSAGE, FLAPS FAILED AT 0 DEGREES. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAP
- [SDR COMA0760010](https://openairdocs.org/sdr/COMA0760010), Jan 6, 2007: WARNING LIGHT. FALSE ACTIVATION. FLIGHT 5662 - DURING CLIMB THRU APPROX FL 180 LEFT REV UNLOCK MESSAGE CAME ON. FOLLOWED QRH AND RETURNED BACK TO PHF AND LANDED SAFELY. INSPECTED LEFT T/R AND S
- [SDR COMA0660584](https://openairdocs.org/sdr/COMA0660584), Oct 20, 2006: PUMP. FAULTY. FLIGHT 5395 - HYD NR 3 LOW PRESSURE CAUTION MESSAGE AT FLIGHT LEVEL 290, QTY ZERO, PRESSURE 1400 PSI. FLIGHT DIVERTED TO CMH AND LANDED WITHOUT INCIDENT. REMOVE
- [SDR COMA0660526](https://openairdocs.org/sdr/COMA0660526), Sep 2, 2006: SWITCH. MALFUNCTIONED. FLIGHT 5542 - RIGHT REV UNLOCK MESSAGE IN FLIGHT FROM MHT TO CVG, FLIGHT DIVERTED TO MDT AND LANDED WITHOUT INCIDENT. FOUND RIGHT THRUST REVERSER STOW SWITCH OU
- [SDR COMA0660521](https://openairdocs.org/sdr/COMA0660521), Sep 1, 2006: WARNING LIGHT. FALSE ACTIVATION. FLIGHT 5664 - RIGHT REV UNLOCK MESSAGE IN FLIGHT FROM CVG TO MSP. FLIGHT DIVERTED TO IND AND LANDED WITHOUT INCIDENT. TRANSFERRED TO DMI LIST PER MEL 78-30-01.
- [SDR COMA0660517](https://openairdocs.org/sdr/COMA0660517), Aug 30, 2006: THRUST REVERSER. MALFUNCTIONED. FLIGHT 9463- EN ROUTE PIT-CVG RECEIVED A RIGHT ENGINE THRUST REVERSER CAUTION, FLIGHT DIVERTED TO CMH. DEFERRED THE RIGHT THRUST REVERSER PER MEL 78-30-01.
- [SDR COMA0660442](https://openairdocs.org/sdr/COMA0660442), Jul 19, 2006: LIGHT. INOPERATIVE. FLIGHT 5233 - FIRST 5 ROWS OF FLOOR TRACK EMERGENCY LIGHTING INOPERATIVE. REPLACED THE FIRST SECTION OF FLOOR TRACK LIGHTING STRIP.
- [SDR COMA0660441](https://openairdocs.org/sdr/COMA0660441), Jul 19, 2006: LIGHT. INOPERATIVE. FLIGHT 5233 - SECTION OF FLOOR TRACK EMERGENCY LIGHTING INOPERATIVE. DEFERRED INOPERATIVE SECTION OF FLOOR TRACK LIGHTING PER MEL 33-51-01.
- [SDR COMA0560506](https://openairdocs.org/sdr/COMA0560506), Sep 17, 2005: ACTUATOR. FAULTY. FLIGHT 5321 - DURING CLIMBOUT OF CVG THE NR 2 HYDRAULIC C/B TRIPPED. REPLACED THE NR 2 HYDRAULIC SOV ACTUATOR.
- [SDR COMA0560491](https://openairdocs.org/sdr/COMA0560491), Sep 7, 2005: WARNING LIGHT. ILLUMINATED. FLIGHT 5089- FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
- [SDR COMA0560414](https://openairdocs.org/sdr/COMA0560414), Jul 27, 2005: OUTFLOW VALVE. MALFUNCTIONED. FLIGHT 5553 - CABIN ALTITUDE CAUTION MESSAGE. REPLACED THE PRIMARY OUTFLOW VALVE.
- [SDR COMA0560318](https://openairdocs.org/sdr/COMA0560318), May 22, 2005: WARNING LIGHT. FALSE ACTIVATION. FLIGHT 5568 CARGO DOOR CAUTION MESSAGE. COULD NOT DUPLICATE. FOUND NO DEFECTS IN CARGO DOOR OR WARNING SYSTEM.
- [SDR COMA0560246](https://openairdocs.org/sdr/COMA0560246), Apr 7, 2005: FCU. FAULTY. FLIGHT 5142 RECEIVED A FLAP FAIL CAUTION WHILE PARKED AT THE GATE. REPLACED THE FLAP ELECTRONIC CONTROL UNIT.
- [SDR COMA0560118](https://openairdocs.org/sdr/COMA0560118), Feb 4, 2005: WARNING LIGHT. ILLUMINATED. FLIGHT 5130 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. C/W EXTENSION AND RETRACTION CHECKS, NO DEFECTS FOUND.
- [SDR COMA0560037](https://openairdocs.org/sdr/COMA0560037), Jan 6, 2005: OVERHEAT LOOP. MALFUNCTIONED. FLIGHT 9487 ANTI ICE DUCT WARNING. REPLACED THE RIGHT WHEEL WELL SENSING LOOP.
- [SDR COMA0560036](https://openairdocs.org/sdr/COMA0560036), Jan 6, 2005: ANTI-ICE SYSTEM. FALSE INDICATION. FLIGHT 4959 ANTI ICE DUCT WARNING. COULD NOT DUPLICATE. INSPECTED AND OPERATIONAL CHECKS WERE NORMAL.
- [SDR COMA0460599](https://openairdocs.org/sdr/COMA0460599), Nov 10, 2004: SKIN. CORRODED. FLIGHT DURING HEAVY MAINTENANCE CHECK (PAX DOOR DETAILED INSPECTION) THE PAX DOOR FORWARD AND AFT BOTTOM CORNERS WERE FOUND TO BE CORRODED. BOTH PARTS WERE REPL
- [SDR COMA0460228](https://openairdocs.org/sdr/COMA0460228), Mar 29, 2004: BULKHEAD. CRACKED. CRACKS IN FORWARD PRESSURE BULKHEAD AT PARKING BRAKE CABLE PASS THROUGH. REPAIRED IN ACCORDANCE WITH REO 601R-53-11-539.
- [SDR COMA0460197](https://openairdocs.org/sdr/COMA0460197), Mar 12, 2004: DUCT. BLOWN. FLIGHT 5200 RIGHT 14TH STAGE DUCT LEAK WARNING. FOUND 14TH STAGE BLEED DUCT BLOWN APART. REPLACED DUCT.
- [SDR COMA0460141](https://openairdocs.org/sdr/COMA0460141), Feb 10, 2004: PCU. BROKEN. FLIGHT 5110 GROUND SPOILER DEPLOY MESSAGE DURING APPROACH. LEFT OUTBOARD SPOILER PCU BROKEN. REPLACED PCU.
- [SDR COMA0460018](https://openairdocs.org/sdr/COMA0460018), Jan 4, 2004: WARNING LIGHT. ILLUMINATED. FLIGHT 5833 ANTI ICE DUCT WARNING MESSAGE. COULD NOT DUPLICATE. SYSTEM OPERATION NORMAL.
- [SDR COMA0360135](https://openairdocs.org/sdr/COMA0360135), Mar 9, 2003: ACM. FLIGHT 5892 AFTER T/O - BURNING ODOR IN COCKPIT AND CABIN.INSPECTED AIRCRAFT, NO DEFECTS NOTED, FLIGHT CHECK SATISFACTORY.
- [SDR COMA0360060](https://openairdocs.org/sdr/COMA0360060), Jan 29, 2003: APU. FLIGHT 5729 APU LOW OIL PRESSURE WARNING.ADDED 2.5 QUARTS OF OIL TO APU.
- [SDR COMA0360029](https://openairdocs.org/sdr/COMA0360029), Jan 14, 2003: APU. UNWANTED. FLIGHT 5807 STRONG FUEL SMELL WHEN APU STARTED.REPLACED APU.
- [SDR COMA0360010](https://openairdocs.org/sdr/COMA0360010), Jan 1, 2003: PRIORITY VALVE. UNRELIABLE. FLIGHT 5495 LANDING GEAR DISAGREE WARNING.REPLACED THE NLG PRIORITY VALVE.
- [SDR COMA0260580](https://openairdocs.org/sdr/COMA0260580), Oct 10, 2002: LAMP. INOPERATIVE. EMERGENCY LIGHTS ROWS 2 THUR 5 ARE INOPERABLE.REPLACED FLEXIBLE LAMP ASSEMBLY.
- [SDR COMA0160843](https://openairdocs.org/sdr/COMA0160843), Oct 22, 2001: WEB. CRACKED. DURING INSPECTION DISCOVERED A CRACK IN THE ENGINE SUPPORT BOX BEAM.PERFORMED TEMPORARY REPAIR TO UPPER AND LOWER WEBS F.S. 630 IN ACCORDANCE WITH CANADAIR REO 
- [SDR COMA0160820](https://openairdocs.org/sdr/COMA0160820), Oct 16, 2001: SKIN. CHAFED. FLIGHT N/A, DURING REPAIR OF ENGINE BOX BEAM DISCOVERED A CHAFED AREA ABOVE THE BOX BEAM AT Z-MEMBER. REPAIRED IN ACCORDANCE WITH REO 601R-53-61-448.
- [SDR COMA0160640](https://openairdocs.org/sdr/COMA0160640), Aug 24, 2001: SWITCH. FAULTY. FLIGHT #5612. DURING CLIMB OUT OF LIT AT 9000 FT. RECEIVED A CABIN DOOR OUTER HANDLE CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIELD.REPLACED D117 PROXIMITY SWI
- [SDR COMA0160455](https://openairdocs.org/sdr/COMA0160455), Jul 10, 2001: FLAP. FAILED. FLAP CAUTION MESSAGE AFTER TAKE-OFF FROM GSP, AIRCRAFT RETURNED TO THE FIELD.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIREST EVENT" MAINTENANCE ACTION, P
- [SDR COMA0160462](https://openairdocs.org/sdr/COMA0160462), Jul 10, 2001: BPSU. WORN. FLAP CAUTION MESSAGE DURING APPROACH INTO CVG, AN EMERGENCY WAS DECLARED, AIRCRAFT LANDED SAFETLY.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "SECOND EVENT" 
- [SDR COMA0160355](https://openairdocs.org/sdr/COMA0160355), Mar 28, 2001: BUSHING. WORN. RIGHT VERT STAB BUSHING AT HORZ STAB PIVOT POINT WORN. REMOVED AND REPLACED BUSHING P/N 601R-55-31-001-5 IAW CRJ AMM 20-26-00-910-803. MACHINED BUSHING IAW WVAC
- [SDR COMA0160322](https://openairdocs.org/sdr/COMA0160322), Mar 15, 2001: WARNING SYSTEM. MALFUNCTIONED. T/O CONFIG MESSAGE DURING T/O. COULD NOT DUPLICATE. OPERATIONAL CHECK OF SYSTEM NORMAL.
- [SDR COMA0061059](https://openairdocs.org/sdr/COMA0061059), Dec 17, 2000: COMPUTER. MALFUNCTIONED. STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER.

All 102: https://openairdocs.org/deregistered/N941CA-2018-04-18/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 20110705018219I](https://openairdocs.org/incident/20110705018219I), Jul 5, 2011: Canadair CL-600-2B19 (N941CA), Romulus, MI, Minor damage. The aircraft was parked on gate C-6 at the detroit metro airport operating on comair flight 6362 as a delta connection. The gate is a non-typical gate, I.e.…
- [Incident 20060902024849I](https://openairdocs.org/incident/20060902024849I), Sep 2, 2006: Cndair CL6002B19 (N941CA), Middletown, PA. (-23) The aircraft landed on runway 13 after reporting a reverse thruster problem. The ARFF responded and the aircraft taxied to the ramp without incident.

## Other aircraft with N941CA

- [Registered now](https://openairdocs.org/aircraft/N941CA): Xag P100 PRO, S/N 821942576FQ2

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