|
gptkbp:instanceOf
|
gptkb:helicopter
|
|
gptkbp:armament
|
none
|
|
gptkbp:avionics
|
modern avionics suite
|
|
gptkbp:climbRate
|
1,500 ft/min
|
|
gptkbp:cockpit
|
glass cockpit
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
twin-engine
|
|
gptkbp:engine
|
gptkb:Lycoming_T53
|
|
gptkbp:firstFlight
|
1980
|
|
gptkbp:fuelCapacity
|
1,200 liters
|
|
gptkbp:headlights
|
gptkb:Fenestron
|
|
gptkbp:height
|
4.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Bell 214ST
|
|
gptkbp:landingGear
|
skids
|
|
gptkbp:length
|
15.5 m
|
|
gptkbp:manufacturer
|
gptkb:Bell_Helicopter
|
|
gptkbp:maxSpeed
|
130 knots
|
|
gptkbp:maxTakeoffWeight
|
5,400 kg
|
|
gptkbp:notableUsers
|
gptkb:Iranian_Air_Force
gptkb:Philippine_Air_Force
gptkb:Colombian_Air_Force
gptkb:Royal_Canadian_Air_Force
gptkb:United_States_Army
|
|
gptkbp:operationalRange
|
300 nautical miles
|
|
gptkbp:passengerCapacity
|
15
|
|
gptkbp:productionCompany
|
1990
|
|
gptkbp:productionStartYear
|
1980
|
|
gptkbp:range
|
400 nautical miles
|
|
gptkbp:role
|
utility helicopter
|
|
gptkbp:rotorDiameter
|
14.6 m
|
|
gptkbp:safetyFeatures
|
fire detection system
crashworthy design
dual hydraulic systems
emergency flotation system
automatic flight control system
|
|
gptkbp:secondaryRole
|
transport
medical evacuation
search and rescue
firefighting
VIP transport
|
|
gptkbp:services
|
15,000 ft
|
|
gptkbp:setting
|
single rotor
|
|
gptkbp:speed
|
120 knots
|
|
gptkbp:successor
|
gptkb:Bell_412
|
|
gptkbp:totalGoals
|
200
|
|
gptkbp:usedBy
|
military
civilian
|
|
gptkbp:variant
|
gptkb:Bell_214ST-1
gptkb:Bell_214ST-2
Bell 214B
|
|
gptkbp:weight
|
2,800 kg
|