|
gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
high-wing
civil aircraft
|
|
gptkbp:armament
|
none
|
|
gptkbp:climbRate
|
5 m/s
|
|
gptkbp:cockpit
|
tandem_seating
|
|
gptkbp:constructionMaterial
|
aluminum
|
|
gptkbp:crewCapacity
|
2
|
|
gptkbp:design
|
utility transport
regional transport.
Armstrong_Whitworth_design_team
|
|
gptkbp:engineConfiguration
|
gptkb:Rolls-Royce
|
|
gptkbp:enginePower
|
1,200 hp
|
|
gptkbp:engineType
|
turboprop
|
|
gptkbp:firstFlight
|
1960
1960-07-01
|
|
gptkbp:fuelCapacity
|
1,500 L
|
|
gptkbp:headlights
|
T-tail
|
|
gptkbp:height
|
4.57 m
|
|
gptkbp:helicopterCapacity
|
glass cockpit
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Armstrong Whitworth A.W. 660C
|
|
gptkbp:landingGear
|
tricycle gear
|
|
gptkbp:length
|
15.24 m
|
|
gptkbp:manufacturer
|
gptkb:Armstrong_Whitworth
|
|
gptkbp:maxSpeed
|
400 km/h
|
|
gptkbp:maxTakeoffWeight
|
6,000 kg
|
|
gptkbp:notableFeature
|
high payload capacity
|
|
gptkbp:numberOfEpisodes
|
2
|
|
gptkbp:operationalRange
|
1,200 km
|
|
gptkbp:passengerCapacity
|
20
1,500 kg
|
|
gptkbp:primaryUser
|
gptkb:Royal_Air_Force
|
|
gptkbp:productionLocation
|
gptkb:United_Kingdom
|
|
gptkbp:productionYears
|
1960-1965
|
|
gptkbp:propulsion
|
variable-pitch
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:retirementYear
|
1970
|
|
gptkbp:role
|
transport aircraft
|
|
gptkbp:serviceHistory
|
used by military and civilian operators.
|
|
gptkbp:services
|
7,620 m
|
|
gptkbp:speed
|
90 km/h
|
|
gptkbp:takeoffDistance
|
700 m
800 m
|
|
gptkbp:totalGoals
|
50
|
|
gptkbp:variant
|
A.W. 660C-1
|
|
gptkbp:wingArea
|
40 m²
|
|
gptkbp:wingspan
|
15.85 m
|