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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:aircraft_operated
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gptkb:light_aircraft
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:climb_rate
|
5 m/s
|
|
gptkbp:cockpit
|
open cockpit
|
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gptkbp:color_scheme
|
military camouflage
|
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gptkbp:configuration
|
low-wing monoplane
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gptkbp:control_surfaces
|
elevator, ailerons, rudder
|
|
gptkbp:crew
|
1 pilot
|
|
gptkbp:design
|
gptkb:Hawker_de_Havilland
|
|
gptkbp:design_purpose
|
training and aerobatics
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
gptkb:1968
|
|
gptkbp:flaps
|
split flaps
|
|
gptkbp:fuel_capacity
|
200 L
|
|
gptkbp:fuselage_material
|
metal construction
|
|
gptkbp:height
|
2.74 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CT-4 A Airtrainer
|
|
gptkbp:influenced_by
|
gptkb:de_Havilland_Canada_DHC-1_Chipmunk
|
|
gptkbp:introduced
|
gptkb:1970
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.23 m
|
|
gptkbp:manufacturer
|
gptkb:Hawker_de_Havilland
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:max_takeoff_weight
|
1,200 kg
|
|
gptkbp:nickname
|
gptkb:Airtrainer
|
|
gptkbp:notable_features
|
good visibility
|
|
gptkbp:number_built
|
approximately 100
|
|
gptkbp:offers_certificate
|
issued by CASA
|
|
gptkbp:operational_history
|
used for pilot training
|
|
gptkbp:power_output
|
180 hp
|
|
gptkbp:primary_user
|
gptkb:Australian_Defence_Force
|
|
gptkbp:production_years
|
1968-1980
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:related_aircraft
|
gptkb:CT-4_B_Airtrainer
|
|
gptkbp:retired
|
2000s
|
|
gptkbp:role
|
gptkb:trainer_aircraft
basic flight training
|
|
gptkbp:roll_rate
|
4.5°/s
|
|
gptkbp:service_ceiling
|
4,500 m
|
|
gptkbp:stall_speed
|
70 km/h
|
|
gptkbp:successor
|
gptkb:CT-4_B_Airtrainer
|
|
gptkbp:tail_type
|
conventional tail
|
|
gptkbp:used_by
|
gptkb:Royal_Air_Force
|
|
gptkbp:variant
|
gptkb:CT-4_B_Airtrainer
|
|
gptkbp:wing_area
|
15.5 m²
|
|
gptkbp:wingspan
|
10.67 m
|
|
gptkbp:bfsParent
|
gptkb:CT-4_Airtrainer
|
|
gptkbp:bfsLayer
|
7
|