Aircraft record

N912CA1993 Canadair CL-600-2B19

DeregisteredUnclaimedSource: FAA, updated Oct 19, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Mar 9, 2011.

Safety record in brief:No NTSB accidents or incidents since 19825 ADs may apply143 service difficulty reports

Registration: Deregistered
Last based in: Salt Lake City, UT; owner city / state
Engine: CF-34-1A · 9,140 lb thrust; Ge
Owners: 1; since 2010
NTSB events: None; since 1982
ADs may apply: 5; confirm with A&P
Service reports: 143; since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026

Last registered owner: Wells Fargo Bank Northwest NA Trustee
Owner type: Corporation
City, state: Salt Lake City, UT
Certificate issued: Oct 19, 2010
Canceled: Mar 9, 2011
Airworthiness: Standard · Transport
Airworthiness date: May 3, 1993

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer: Canadair
Model: CL-600-2B19
Year: 1993
Serial number: 7011
Aircraft type: Fixed wing multi engine
Category: Land
Certification: Type Certificated
Seats: 55
Engines: 2
Max takeoff weight: 20,000 and over lb
Mode S code: AC9E4C

Engine

Make and model: Ge Cf-34-1a
Type: Turbo-fan
Power: 9,140 lb thrust

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records

2010 – 2011Wells Fargo Bank Northwest NA TrusteeSalt Lake City, UT

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (5)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

AD	Subject	Effective	Applies to
2004-26-02	GE Aircraft Engines (GE) CF34-3A, CF34-3A2, CF34-1A, CF34-3A1, CF34-3B, and CF34-3B1…	Jan 26, 2005	Engine (CF-34-1A)Only with: HPC forward spool P/N 6078T56P03 or 6078T56P04 installed.
2004-07-18	Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) Airplanes	May 11, 2004	Airframe (CL-600-2B19)Certain serial numbers: CL-600-2B19 7375–7632. Only with: Equipped with landing gear control handle assemblies Canadair P/N 601R50967-7 (Vendor P/N 7-45502-1) or Canadair P/N 601R50967-9 (Vendor P/N 7-45502-3).
2000-14-17	Bombardier Model CL-600-2B19 Series Airplanes	Aug 28, 2000	Airframe (CL-600-2B19)Certain serial numbers: CL-600-2B19 7003–7207. Only with: Except airplanes on which Canadair Regional Jet Service Bulletin S.B. 601R-34-094, Revision B, dated November 14, 1997, has been accomplished.
2000-01-12	Bombardier Model CL-600-2B19 (Regional Jet Series 100) Series Airplanes	Feb 17, 2000	Airframe (CL-600-2B19)Certain serial numbers: CL-600-2B19 7003–7185. Only with: Except airplanes on which Canadair Regional Jet Service Bulletin 601R-53-046, Revision B, or 601R-53-047, Revision D, has been accomplished.
95-04-05	Bombardier (Formerly Canadair) Model CL-600-2B19 (Regional Jet Series 100) Series…	Apr 7, 1995	Airframe (CL-600-2B19)Certain serial numbers: CL-600-2B19 7003–on

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (143)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

Fuselage · frame · crackedMay 9, 2009
FS 605.00 FRAME UNDER CARGO DOOR SILL IS CRACKED WHERE IT ATTACHES TO SKIN IN OUTER RADIUS. REMOVED DAMAGE FRAME SECTION AT FS 605.00 JUST BELOW CARGO DOOR SILL AND INSTALLED SERVICEABLE FRAME IAW CRJ SRM 51-42-06 PG 1-20, CRJ SRM 51-42-21 PG 1-21 AND SR 99-5140-0001.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Fuselage · bulkhead · damagedMay 9, 2009
AFT PRESSURE BULKHEAD WEB AT FS 621 LBL 27.5 TOP AREA ABOVE CARGO DOOR TRACK IS CRACKED. REMOVED DAMAGE AND APPLIED A SERVICEABLE PERMANENT REPAIR TO AFT PRESSURE BULKHEAD WEB AT FS 621 LBL 27.5 PER REO 601R-53-61-1541 REV B AND SPOT FACED WEB TO ACCOMMODATE FASTENERS PER EA 10-5361-02606.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Fuselage · floor skin · crackedMay 9, 2009
PRESSURE FLOOR SKIN AT FS 513.00 BETWEEN BL 0 AND RBL 9 IS CRACKED FWD AND AFT OF BEAM. REMOVED DAMAGE AND APPLIED A PERMANENT REPAIR AT FS 513.00 BETWEEN BL 0 AND RBL 9 IAW BOMBARDIER REO 601R-53-41-931.
From FAA Service Difficulty Reports; matched by N-number and serial number.

Show all 10 reports

Fuselage · floor skin · crackedMay 9, 2009
PRESSURE FLOOR SKIN AT FS 513.00 BETWEEN BL 9 AND RBL 18 IS CRACKED FWD AND AFT OF BEAM. REMOVED DAMAGE AND APPLIED A PERMANENT REPAIR AT FS 513.00 BETWEEN BL 9 AND RBL 18 IAW BOMBARDIER REO 601R-53-41-931.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Fuselage · floor skin · crackedMay 9, 2009
PRESSURE FLOOR SKIN AT FS 513.00 BETWEEN LBL 9 AND LBL 18 IS CRACKED. REMOVED DAMAGE AND APPLIED A PERMANENT REPAIR AT FS 513.00 BETWEEN LBL 9 AND LBL 18 IAW BOMBARDIER REO 601R-53-41-931.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Fuselage · rivet · damagedMay 9, 2009
DURING INSPECTION AND REPAIR OF PRESSURE FLOOR SKIN AT FS 513.00 BETWEEN BL 9 AND RBL 18 (REO 601R-53-41-931) FOUND 7 POPPED RIVET HEADS ON PRESSURE FLOOR SKIN JUST I\B AND O\B OF RBL 18. REMOVED DAMAGED FASTENERS AT FS 513.00 I\B AND O\B SIDES OF RBL 18 AND INSTALLED SERVICEABLE HILITE FASTENERS…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Doors · skin · damagedMay 9, 2009
PAX DOOR INNER SKIN HAS DAMAGED FASTENER WHOLE FOR STEPS AT FS 320.10 NEAR DATIM 1 ON FWD UPPER SIDE. INSTALLED A SERVICEABLE REPAIR DOUBLER ON PAX DOOR INNER SKIN PER EA 10-5210-02607.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Fuselage · frame · crackedMar 2, 2009
RIGHT 640.00 FRAME CRACKED BETWEEN STR 9 AND STR 12 ON THE AFT DOUBLER. REPAIRED IAW REO 601R-53-61-506, REO 601R-53-61-569, AND REO 601R-53-61-557.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Landing gear · pseu · faultyMar 17, 2008
FLIGHT 5480 - NOSE LANDING GEAR AND GEAR DOOR INDICATION REMAINED "RED" ON RETRACTION. DECLARED EMERGENCY, LANDED CVG WITHOUT INCIDENT. INSPECTED AND GREASED NLG AND DOORS. ADJUSTED STRUT PROX SENSOR, SWUNG GEAR 15 TIMES INCLUDING PRIORITY TEST. REPLACED PSEU DUE TO NO CODES DISPLAYED FOR EVENT.…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Ice and rain protection · warning system · malfunctionedFeb 5, 2008
FLIGHT 5267 - RECEIVED RT WING ANTI-ICE CAUTION ON TAKEOFF ROLL, WINGS AND COWL "ON". ABORTED TAKEOFF, RETURNED TO GATE WITHOUT INCIDENT. PERFORMED OPERATION CHECK OF WING ANTI-ICE SYSTEM. NO DEFECTS NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 143 reports.

Sources

FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 19, 2026
NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 19, 2026
FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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