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gptkbp:instanceOf
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aircraft
|
|
gptkbp:aircraft
|
twin-engine
utility aircraft
high-wing
civil aircraft
|
|
gptkbp:cockpit
|
1
|
|
gptkbp:communityService
|
various airlines
|
|
gptkbp:constructionMaterial
|
metal
|
|
gptkbp:crew
|
2
|
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gptkbp:design
|
gptkb:Sir_W._G._Armstrong_Whitworth
1950s
|
|
gptkbp:developer
|
gptkb:Armstrong_Whitworth_A.W.65
|
|
gptkbp:enginePower
|
1,200 hp
|
|
gptkbp:engineType
|
turboprop
|
|
gptkbp:firstFlight
|
1955
1955-07-01
|
|
gptkbp:headlights
|
T-tail
|
|
gptkbp:height
|
8.23 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Armstrong Whitworth A.W.95
|
|
gptkbp:influenced
|
gptkb:Hawker_Siddeley_HS.748
|
|
gptkbp:influencedBy
|
de Havilland Dove
|
|
gptkbp:landingGear
|
tricycle gear
|
|
gptkbp:length
|
22.86 m
|
|
gptkbp:manufacturer
|
gptkb:Armstrong_Whitworth
|
|
gptkbp:maxSpeed
|
400 km/h
|
|
gptkbp:maxTakeoffWeight
|
20,865 kg
|
|
gptkbp:militaryService
|
gptkb:Royal_Air_Force
|
|
gptkbp:notableFeature
|
large cargo door
|
|
gptkbp:numberOfEpisodes
|
2
|
|
gptkbp:operationalRange
|
1,200 km
|
|
gptkbp:passengerCapacity
|
30
3,000 kg
|
|
gptkbp:produces
|
1955-1960
|
|
gptkbp:propulsion
|
variable-pitch
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:retired
|
1970s
|
|
gptkbp:role
|
military transport
transport aircraft
|
|
gptkbp:services
|
6,000 m
|
|
gptkbp:successor
|
gptkb:Hawker_Siddeley_HS.748
|
|
gptkbp:takeoffDistance
|
900 m
1,200 m
|
|
gptkbp:totalGoals
|
50
|
|
gptkbp:usedBy
|
gptkb:Royal_Air_Force
|
|
gptkbp:variant
|
A.W.95A
A.W.95B
|
|
gptkbp:wingArea
|
80 m²
|
|
gptkbp:wingspan
|
28.96 m
|