|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_configuration
|
single-engine
|
|
gptkbp:aircraft_operated
|
gptkb:light_aircraft
|
|
gptkbp:aircraft_type
|
fixed-wing aircraft
|
|
gptkbp:avionics
|
basic flight instruments
|
|
gptkbp:climb_rate
|
5 m/s
|
|
gptkbp:cockpit
|
tandem seating
|
|
gptkbp:color_scheme
|
military camouflage
|
|
gptkbp:control_surfaces
|
elevator, ailerons, rudder
|
|
gptkbp:crew
|
1 pilot
|
|
gptkbp:design
|
low-wing monoplane
Hawker de Havilland team
|
|
gptkbp:emergency_services
|
gptkb:parachute
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
gptkb:1970
|
|
gptkbp:flaps
|
split flaps
|
|
gptkbp:fuel_capacity
|
200 L
|
|
gptkbp:height
|
2.74 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CT-4 B Airtrainer
|
|
gptkbp:influences
|
Australian aviation training programs
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:legacy
|
foundation for future trainer designs
|
|
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:notable_features
|
good visibility
|
|
gptkbp:number_built
|
approximately 100
|
|
gptkbp:operational_history
|
used for basic flight training
|
|
gptkbp:operational_use
|
1970s
|
|
gptkbp:power_output
|
180 hp
|
|
gptkbp:primary_function
|
pilot training
|
|
gptkbp:production_years
|
1970-1980s
|
|
gptkbp:propeller
|
constant-speed propeller
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:related_aircraft
|
gptkb:Piper_PA-38_Tomahawk
|
|
gptkbp:retirement
|
2000s
|
|
gptkbp:role
|
gptkb:trainer_aircraft
|
|
gptkbp:roll_rate
|
3.5°/s
|
|
gptkbp:service_ceiling
|
3,000 m
|
|
gptkbp:stall_speed
|
65 km/h
|
|
gptkbp:successor
|
CT-4 C Airtrainer
|
|
gptkbp:tail_type
|
conventional tail
|
|
gptkbp:training
|
aerobatic training
CT-4 B, CT-4 C
|
|
gptkbp:used_by
|
gptkb:Royal_Air_Force
|
|
gptkbp:wing_configuration
|
cantilever wing
|
|
gptkbp:wingspan
|
10.67 m
|
|
gptkbp:bfsParent
|
gptkb:CT-4_Airtrainer
|
|
gptkbp:bfsLayer
|
7
|