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gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:aircraft_configuration
|
low-wing
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|
gptkbp:aircraft_role
|
gptkb:training
reconnaissance
utility
light attack
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|
gptkbp:aircraft_type
|
military trainer
|
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gptkbp:armament
|
gptkb:none
|
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gptkbp:built
|
gptkb:100
|
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gptkbp:ceiling
|
10,000 m
|
|
gptkbp:climb_rate
|
10 m/s
|
|
gptkbp:cockpit
|
tandem seating
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gptkbp:communication_system
|
gptkb:radio_station
|
|
gptkbp:control_surfaces
|
elevators
ailerons
rudder
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
Hawker Siddeley team
|
|
gptkbp:engine_configuration
|
rear-mounted
|
|
gptkbp:engine_type
|
turbofan
|
|
gptkbp:first_flight
|
gptkb:1960
|
|
gptkbp:flaps
|
split flaps
|
|
gptkbp:fuel_capacity
|
1,000 L
|
|
gptkbp:fuselage_material
|
aluminum
|
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gptkbp:height
|
3.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
HS-14
|
|
gptkbp:landing_distance
|
3,000 kg
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:leading_edge_devices
|
slats
|
|
gptkbp:length
|
12.5 m
|
|
gptkbp:manufacturer
|
gptkb:Hawker_Siddeley
|
|
gptkbp:max_speed
|
400 km/h
|
|
gptkbp:max_takeoff_weight
|
3,500 kg
|
|
gptkbp:navigation_system
|
ILS
VOR
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:passenger_capacity
|
2
|
|
gptkbp:primary_user
|
gptkb:Royal_Air_Force
|
|
gptkbp:production_years
|
1960-1965
|
|
gptkbp:propulsion
|
gptkb:jet_engine
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:retirement
|
gptkb:1980s
|
|
gptkbp:role
|
gptkb:trainer_aircraft
|
|
gptkbp:service_entry
|
gptkb:1961
|
|
gptkbp:stall_speed
|
80 km/h
|
|
gptkbp:successor
|
gptkb:HS-15
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:training
|
basic flight training
advanced flight training
|
|
gptkbp:variant
|
HS-14 A
HS-14 B
|
|
gptkbp:wing_area
|
30 m²
|
|
gptkbp:wing_configuration
|
aluminum
|
|
gptkbp:wingspan
|
11.0 m
|
|
gptkbp:bfsParent
|
gptkb:Carrier_Air_Wing_Fifty-One
gptkb:Carrier_Air_Wing_Forty-One
gptkb:Carrier_Air_Wing_Seventeen
gptkb:Carrier_Air_Wing_Thirty-Eight
gptkb:Carrier_Air_Wing_Two
gptkb:Carrier_Air_Wing_5
gptkb:Carrier_Air_Wing_Eleven
|
|
gptkbp:bfsLayer
|
6
|