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
1997
Serial number
7192
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
A8218B
Engine
Make and model
Ge Cf34 Series
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
2008 – 2009Wells 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 20, 2026 · SDRs · Oct 16, 2026
NTSB events (1)
Incident · minor damage
Jun 28, 2005 · Greensboro, NC
The inadequate assembly of the nose landing gear selector valve by a parts supplier, which resulted in internal seal damage and a hydraulic leak that led to the collapse of the nose landing gear. A factor was the insufficient information provided by the airplane manufacturer in its service bulletin regarding the affected airplanes for inspection of the valves.
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.
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.
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.
UNCOMMANDED LT ROLL WITH AUTOPILOT ENGAGED. INTERROGATED FCC FOR FAULTS, FOUND NO DEFECTS. PERFORMED YAW DAMP COMMAND AND FEEDBACK TEST W/ NO DEFECTS NOTED REF FIM 22-11-00. PERFORMED AILRON/ELV SERVO SPIN UP TEST, FOUND NO DEFECTS AT THIS TIME REF FIM 22-22-00. AC OK FOR SERVICE. FDR WAS…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Hydraulic power · line · leakingSep 10, 2005
HYDRAULIC 3 LOW PRESSURE MESSAGE. REPLACED LINE ON 3A PUMP.
From FAA Service Difficulty Reports; matched by N-number and serial number.
NOSE LANDING GEAR COLLAPSED AT THE GATE UPON SWITCHING TO GROUND POWER. SPANNER END CAP BACKED OUT, VERY HIGH LEAKAGE IN NEUTRAL WITH PRESSURE TO C.2.- DIODE IN NR 2 SOLENOID SHORTED.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Power plant · support beam · crackedFeb 23, 2005
ENGINE SUPPORT BEAM UPPER ANGLE IS CRACKED AT .250 INCH IN LENGTH AT FS 640.00 AND LBL 8.5.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Fuselage · intercostal · crackedFeb 23, 2005
INTERCOSTAL CRACKED AT .250 INCH IN LENGTH ON LT INBOARD SIDE AT FS 484 LEFT BETWEEN BL 27.00 AND 36.00.
From FAA Service Difficulty Reports; matched by N-number and serial number.