Statements (56)
Predicate | Object |
---|---|
gptkbp:instanceOf |
gptkb:helicopter
|
gptkbp:armament |
none
|
gptkbp:crew |
2
|
gptkbp:engineType |
turbine engine
|
gptkbp:firstFlight |
1983
|
gptkbp:fuelCapacity |
600 L
|
https://www.w3.org/2000/01/rdf-schema#label |
Westland 109SP
|
gptkbp:introduced |
1984
|
gptkbp:length |
12.8 m
|
gptkbp:manufacturer |
Westland_Aircraft
|
gptkbp:maxSpeed |
250 km/h
|
gptkbp:maxTakeoffWeight |
3,175 kg
|
gptkbp:notableFeature |
advanced avionics
advanced safety features high reliability quiet operation customizable configurations easy maintenance low vibration levels multi-role capabilities capable of night operations retractable landing gear high payload capacity versatile mission capabilities good fuel efficiency high speed performance dual-engine design used in law enforcement missions used in search and rescue missions used in military operations used in training missions suitable for various missions used in VIP transport missions used in surveillance missions good visibility from cockpit used in medical evacuation missions used in offshore operations used in transport missions capable of all-weather operations used in fire-fighting missions |
gptkbp:numberOfEpisodes |
2
|
gptkbp:passengerCapacity |
6
|
gptkbp:primaryUser |
gptkb:British_Army
|
gptkbp:range |
600 km
|
gptkbp:retired |
2000
|
gptkbp:role |
utility helicopter
|
gptkbp:rotorDiameter |
11.0 m
|
gptkbp:services |
4,500 m
|
gptkbp:successor |
AgustaWestland AW109
|
gptkbp:variant |
gptkb:Westland_109K
gptkb:Westland_109A gptkb:Westland_109C gptkb:Westland_109E gptkb:Westland_109D gptkb:Westland_109S |
gptkbp:weight |
1,800 kg
|