|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_configuration
|
twin-engine turboprop
|
|
gptkbp:aircraft_type
|
gptkb:transport_aircraft
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:cargo_capacity
|
up to 10,000 kg
|
|
gptkbp:cockpit
|
two-pilot configuration
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Hawker_Siddeley_Aircraft_Limited
high-wing monoplane
|
|
gptkbp:engine_power
|
1,500 hp
|
|
gptkbp:engine_type
|
turboprop
|
|
gptkbp:first_flight
|
gptkb:1963
|
|
gptkbp:fuel_capacity
|
5,000 liters
|
|
gptkbp:height
|
8.1 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Hawker Siddeley Andover
|
|
gptkbp:landing_distance
|
1,000 m
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
24.5 m
|
|
gptkbp:manufacturer
|
gptkb:Hawker_Siddeley
|
|
gptkbp:max_speed
|
400 km/h
|
|
gptkbp:max_takeoff_weight
|
22,680 kg
|
|
gptkbp:notable_features
|
large cargo door
|
|
gptkbp:number_built
|
approximately 50
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:passenger_capacity
|
up to 30
|
|
gptkbp:primary_user
|
gptkb:Royal_Air_Force
|
|
gptkbp:production_years
|
1963-1975
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:related_aircraft
|
gptkb:Hawker_Siddeley_HS.748
|
|
gptkbp:retirement
|
1990s
|
|
gptkbp:role
|
gptkb:transport_aircraft
|
|
gptkbp:roll_rate
|
3.5°/s
|
|
gptkbp:service
|
1965-1990s
|
|
gptkbp:service_ceiling
|
7,600 m
|
|
gptkbp:service_entry
|
gptkb:1965
|
|
gptkbp:stall_speed
|
100 km/h
|
|
gptkbp:successor
|
gptkb:Lockheed_Martin_C-130_Hercules
|
|
gptkbp:takeoff_distance
|
1,200 m
|
|
gptkbp:used_in
|
various military operations
|
|
gptkbp:variant
|
gptkb:Andover_C.1
gptkb:Andover_C.2
gptkb:Andover_CC.1
|
|
gptkbp:wing_area
|
100 m²
|
|
gptkbp:wingspan
|
30.5 m
|
|
gptkbp:bfsParent
|
gptkb:Hawker_Siddeley_Group
|
|
gptkbp:bfsLayer
|
6
|