|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:No._25_Squadron_RCAF
|
|
gptkbp:aircraft_operated
|
gptkb:Canadair_Tutor_family
fixed-wing aircraft
low-wing monoplane
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:aspect_ratio
|
7.5
|
|
gptkbp:climb_rate
|
15 m/s
|
|
gptkbp:cockpit
|
tandem seating
|
|
gptkbp:controls
|
differential ailerons
|
|
gptkbp:crew
|
2
|
|
gptkbp:decommissioned
|
1990s
|
|
gptkbp:design
|
gptkb:Canadair
Canadair engineers
|
|
gptkbp:engine
|
gptkb:Rolls-Royce_Viper_601
|
|
gptkbp:engine_type
|
twin-engine
|
|
gptkbp:first_flight
|
gptkb:1960
|
|
gptkbp:flaps
|
split flaps
|
|
gptkbp:floors
|
trimmable
|
|
gptkbp:fuel_capacity
|
1,200 liters
|
|
gptkbp:height
|
3.8 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Canadair CL-41 Tutor
|
|
gptkbp:introduced
|
gptkb:1960
|
|
gptkbp:is_used_by
|
gptkb:Royal_Canadian_Air_Force
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
12.5 m
|
|
gptkbp:manufacturer
|
gptkb:Canadair
|
|
gptkbp:max_speed
|
1,000 km/h
|
|
gptkbp:max_takeoff_weight
|
3,600 kg
|
|
gptkbp:nickname
|
Tutor
|
|
gptkbp:notable_ships
|
trimmable
|
|
gptkbp:number_built
|
approximately 200
|
|
gptkbp:operational_history
|
used for training pilots
|
|
gptkbp:primary_user
|
gptkb:Canadian_Forces
|
|
gptkbp:production_years
|
1960-1969
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:retired
|
1990s
|
|
gptkbp:role
|
aerobatic training
jet trainer
|
|
gptkbp:roll_rate
|
60 degrees per second
|
|
gptkbp:service_ceiling
|
12,000 m
|
|
gptkbp:services
|
1960-1990s
|
|
gptkbp:speed
|
110 km/h
|
|
gptkbp:successor
|
gptkb:Canadair_CT-114_Tutor
|
|
gptkbp:surface
|
elevators, ailerons, rudder
|
|
gptkbp:training
|
basic flight training
|
|
gptkbp:used_in
|
air shows
|
|
gptkbp:variant
|
gptkb:CL-41_B
CL-41 A
CL-41 D
|
|
gptkbp:wing_area
|
30 m²
|
|
gptkbp:wingspan
|
10.9 m
|