gptkbp:instanceOf
|
gptkb:helicopter
|
gptkbp:armament
|
none
|
gptkbp:avionics
|
analog
|
gptkbp:basedOn
|
14.63 m
3.76 m
|
gptkbp:communicationEquipment
|
UHF/VHF
|
gptkbp:constructionMaterial
|
aluminum
|
gptkbp:countryOfOrigin
|
gptkb:United_Kingdom
|
gptkbp:crew
|
2
|
gptkbp:design
|
multi-role
|
gptkbp:engine
|
gptkb:Gemini_1000
|
gptkbp:engineConfiguration
|
gptkb:Rolls-Royce
|
gptkbp:enginePower
|
1,000 shp
|
gptkbp:engineType
|
turboshaft
|
gptkbp:firstFlight
|
1970
|
gptkbp:headlights
|
gptkb:fenestron
|
gptkbp:height
|
4.57 m
|
gptkbp:historicalSignificance
|
first British helicopter with a fully articulated rotor system.
|
https://www.w3.org/2000/01/rdf-schema#label
|
Westland 414A
|
gptkbp:landingGear
|
skid
|
gptkbp:length
|
15.24 m
|
gptkbp:manufacturer
|
Westland_Aircraft
|
gptkbp:maximumDepth
|
2,000 kg
|
gptkbp:maxSpeed
|
250 km/h
|
gptkbp:maxTakeoffWeight
|
4,500 kg
|
gptkbp:navigationEquipment
|
gptkb:VOR/DME
|
gptkbp:notableFeature
|
1971
high payload capacity
|
gptkbp:numberOfEpisodes
|
5
|
gptkbp:passengerCapacity
|
6
1,500 kg
|
gptkbp:primaryUser
|
gptkb:British_Army
|
gptkbp:productionLocation
|
Yeovil,_Somerset
|
gptkbp:productionYears
|
1970-1980
|
gptkbp:products
|
gptkb:UK_CAA
|
gptkbp:range
|
800 km
|
gptkbp:relatedModel
|
gptkb:Westland_30
|
gptkbp:retirementYear
|
1980s
|
gptkbp:role
|
utility helicopter
|
gptkbp:services
|
4,500 m
|
gptkbp:successor
|
Westland_414A-1
|
gptkbp:usedIn
|
military operations
civilian operations
|
gptkbp:variant
|
Westland_414A-1
|
gptkbp:weight
|
2,500 kg
|
gptkbp:wingArea
|
none
|