|
gptkbp:instanceOf
|
aircraft
|
|
gptkbp:armament
|
none
|
|
gptkbp:cockpit
|
pressurized
|
|
gptkbp:controls
|
elevators
ailerons
rudder
|
|
gptkbp:covers
|
slotted flaps
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Sir_W._G._Armstrong_Whitworth
military transport
civil transport
|
|
gptkbp:engineType
|
gptkb:Rolls-Royce_Dart
|
|
gptkbp:financial_aid
|
longitudinal stability
directional stability
lateral stability
|
|
gptkbp:firstFlight
|
1945
|
|
gptkbp:fuelCapacity
|
3,000 liters
|
|
gptkbp:headlights
|
T-tail
|
|
gptkbp:height
|
7.62 m
|
|
gptkbp:historicalSignificance
|
post-war transport aircraft development
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Armstrong Whitworth A.W.82
|
|
gptkbp:influencedBy
|
A.W.41
A.W.52
A.W.55
A.W.60
A.W.61
A.W.62
A.W.63
A.W.64
A.W.65
A.W.66
|
|
gptkbp:landingGear
|
tricycle gear
|
|
gptkbp:length
|
22.86 m
|
|
gptkbp:manufacturer
|
gptkb:Armstrong_Whitworth
|
|
gptkbp:maxSpeed
|
500 km/h
|
|
gptkbp:maxTakeoffWeight
|
15,875 kg
|
|
gptkbp:numberBuilt
|
10
|
|
gptkbp:passengerCapacity
|
30
5,000 kg
|
|
gptkbp:performance
|
good climb rate
good fuel efficiency
good low-speed handling
|
|
gptkbp:productionCompany
|
1945-1946
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:relatedAircraft
|
gptkb:Vickers_Valetta
gptkb:Bristol_Britannia
gptkb:Avro_York
|
|
gptkbp:retirementYear
|
1950s
|
|
gptkbp:role
|
transport aircraft
|
|
gptkbp:services
|
1946
6,000 m
|
|
gptkbp:setting
|
high-wing monoplane
|
|
gptkbp:usedBy
|
gptkb:Royal_Air_Force
|
|
gptkbp:variant
|
A.W.83
|
|
gptkbp:wingArea
|
100 m²
|
|
gptkbp:wingspan
|
30.48 m
|