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gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
7
|
|
gptkbp:bfsParent
|
gptkb:Canadair_CL-41_Tutor
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
fixed-wing aircraft
twin-engine
trainer and light attack
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:aspect_ratio
|
8.5
|
|
gptkbp:climb_rate
|
10 m/s
|
|
gptkbp:cockpit
|
two-seat tandem
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:horse_race
low-wing monoplane
Canadair design team
|
|
gptkbp:elevation
|
10,000 m
|
|
gptkbp:engine
|
gptkb:musical
3,000 lbf
|
|
gptkbp:engine_type
|
gptkb:Rolls-Royce_Viper
gptkb:engine
|
|
gptkbp:first_flight
|
gptkb:1963
|
|
gptkbp:fuel_capacity
|
1,200 L
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CL-41 B
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
11.58 m
|
|
gptkbp:manufacturer
|
gptkb:Canadair
|
|
gptkbp:max_speed
|
500 km/h
|
|
gptkbp:max_takeoff_weight
|
80 km/h
4,500 kg
150 km/h
3,600 kg
|
|
gptkbp:number_built
|
approximately 200
|
|
gptkbp:operational_range
|
1,200 km
|
|
gptkbp:primary_user
|
gptkb:Royal_Canadian_Air_Force
private operators
|
|
gptkbp:production_years
|
1963-1970
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:retirement_year
|
1990s
|
|
gptkbp:role
|
gptkb:aircraft
gptkb:battle
light attack
|
|
gptkbp:seating_capacity
|
1,000 kg
|
|
gptkbp:service_ceiling
|
10,000 m
|
|
gptkbp:services
|
gptkb:1964
|
|
gptkbp:speed
|
110 km/h
|
|
gptkbp:successor
|
gptkb:Canadair_CT-114_Tutor
|
|
gptkbp:variant
|
CL-41 Tutor
|
|
gptkbp:wing_area
|
30 m²
|
|
gptkbp:wingspan
|
12.80 m
|