Statements (54)
Predicate | Object |
---|---|
gptkbp:instanceOf |
gptkb:helicopter
|
gptkbp:armament |
none
|
gptkbp:crew |
2
|
gptkbp:design |
B._A._C._and_Agusta
|
gptkbp:engineType |
turbine engine
|
gptkbp:firstFlight |
1971
|
gptkbp:fuelCapacity |
600 L
|
gptkbp:height |
3.4 m
|
https://www.w3.org/2000/01/rdf-schema#label |
Westland 109S Mk II
|
gptkbp:introduced |
1971
|
gptkbp:length |
12.8 m
|
gptkbp:manufacturer |
Westland_Aircraft
|
gptkbp:maxSpeed |
250 km/h
|
gptkbp:maxTakeoffWeight |
3,175 kg
|
gptkbp:notableFeature |
high endurance
high speed safety features advanced avionics modern design high reliability good stability high maneuverability low noise levels advanced safety systems reliable performance easy maintenance good visibility twin-engine design retractable landing gear multi-role capability excellent climb rate adaptable configurations dual control system user-friendly cockpit versatile operations cost-effective operation good payload capacity |
gptkbp:numberOfEpisodes |
2
|
gptkbp:passengerCapacity |
6
|
gptkbp:primaryUser |
gptkb:British_Army
|
gptkbp:produces |
1971-2000
|
gptkbp:propulsion |
twin_rotor_system
|
gptkbp:range |
600 km
|
gptkbp:retired |
2000s
|
gptkbp:role |
utility helicopter
medical evacuation search and rescue VIP transport |
gptkbp:services |
4,500 m
|
gptkbp:successor |
AgustaWestland AW109
|
gptkbp:usedBy |
military
|
gptkbp:variant |
Agusta A109
|
gptkbp:weight |
1,500 kg
|
gptkbp:wingspan |
11.0 m
|