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gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
fixed-wing aircraft
high-wing
|
|
gptkbp:capacity
|
20 passengers
|
|
gptkbp:cockpit
|
two-pilot cockpit
|
|
gptkbp:communicationEquipment
|
VHF radio
HF radio
|
|
gptkbp:constructionMaterial
|
aluminum
|
|
gptkbp:controls
|
elevators
fly-by-wire
ailerons
rudder
|
|
gptkbp:countryOfOrigin
|
gptkb:United_Kingdom
|
|
gptkbp:covers
|
slotted flaps
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:John_Wright
civil aviation
|
|
gptkbp:emergencyServices
|
first aid kits
fire extinguishers
life vests
|
|
gptkbp:engineType
|
gptkb:Rolls-Royce_Dart
|
|
gptkbp:financial_aid
|
longitudinal stability
directional stability
lateral stability
|
|
gptkbp:firstFlight
|
1946
1946-07-01
|
|
gptkbp:headlights
|
T-tail
|
|
gptkbp:height
|
8.23 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Armstrong Whitworth A.W.61A
|
|
gptkbp:interiorFeatures
|
emergency exits
galley
lavatory
passenger seats
overhead_bins
|
|
gptkbp:landingGear
|
tricycle gear
|
|
gptkbp:length
|
22.86 m
|
|
gptkbp:manufacturer
|
gptkb:Armstrong_Whitworth
|
|
gptkbp:maxSpeed
|
500 km/h
|
|
gptkbp:maxTakeoffWeight
|
10,000 kg
|
|
gptkbp:navigationEquipment
|
VOR
ADF
|
|
gptkbp:notableFeature
|
pressurized cabin
|
|
gptkbp:numberBuilt
|
1
|
|
gptkbp:primaryUser
|
gptkb:British_Overseas_Airways_Corporation
|
|
gptkbp:productionCompany
|
1946-1947
|
|
gptkbp:propulsion
|
turboprop engines
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:relatedAircraft
|
gptkb:Armstrong_Whitworth_A.W.66
|
|
gptkbp:retired
|
1950s
|
|
gptkbp:role
|
transport aircraft
|
|
gptkbp:services
|
7,620 m
|
|
gptkbp:variant
|
A.W.61B
|
|
gptkbp:wingspan
|
30.48 m
|