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gptkbp:instanceOf
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aircraft
|
|
gptkbp:aircraft
|
2.5 m
conventional
fixed-wing aircraft
2.0 m
utility aircraft
high-wing
|
|
gptkbp:cabinType
|
passenger cabin
|
|
gptkbp:capacity
|
12 passengers
|
|
gptkbp:cockpit
|
enclosed
|
|
gptkbp:constructionMaterial
|
metal
|
|
gptkbp:controls
|
elevator
rudder
aileron
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Geoffrey_de_Havilland
1930s
|
|
gptkbp:engine
|
gptkb:Armstrong_Siddeley_Cheetah
2
wing-mounted
|
|
gptkbp:firstFlight
|
1938
1950s
|
|
gptkbp:height
|
4.57 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Armstrong Whitworth A.W.71
|
|
gptkbp:landingGear
|
tailwheel
|
|
gptkbp:length
|
19.81 m
|
|
gptkbp:manufacturer
|
gptkb:Armstrong_Whitworth
|
|
gptkbp:maximumDepth
|
1,500 kg
|
|
gptkbp:maxSpeed
|
300 km/h
|
|
gptkbp:maxTakeoffWeight
|
5,670 kg
|
|
gptkbp:numberBuilt
|
10
|
|
gptkbp:passengerCapacity
|
30 m³
|
|
gptkbp:powerOutput
|
450 hp
|
|
gptkbp:primaryUser
|
gptkb:British_Overseas_Airways_Corporation
|
|
gptkbp:productionCompany
|
1940
|
|
gptkbp:productionStartYear
|
1938
|
|
gptkbp:propulsion
|
variable-pitch
|
|
gptkbp:range
|
1,200 km
|
|
gptkbp:retirementYear
|
1950s
|
|
gptkbp:role
|
military transport
transport aircraft
cargo_aircraft
|
|
gptkbp:services
|
1940
6,000 m
|
|
gptkbp:takeoffDistance
|
500 m
600 m
|
|
gptkbp:usedBy
|
gptkb:Royal_Air_Force
|
|
gptkbp:variant
|
A.W.71A
A.W.71B
|
|
gptkbp:wingArea
|
8.5
|
|
gptkbp:wingspan
|
28.96 m
|