gptkbp:instanceOf
|
gptkb:helicopter
|
gptkbp:armament
|
none
|
gptkbp:avionics
|
modernized in some variants
|
gptkbp:constructionMaterial
|
aluminum alloy
|
gptkbp:crew
|
2
|
gptkbp:design
|
twin-engine
|
gptkbp:engine
|
gptkb:Lycoming_T53
|
gptkbp:engineType
|
turboshaft
|
gptkbp:firstFlight
|
1962
|
gptkbp:fuelCapacity
|
1,200 L
|
gptkbp:headlights
|
two-blade
|
gptkbp:height
|
4.5 m
|
https://www.w3.org/2000/01/rdf-schema#label
|
Bell 205
|
gptkbp:landingGear
|
skids
|
gptkbp:length
|
15.8 m
|
gptkbp:manufacturer
|
gptkb:Bell_Helicopter
|
gptkbp:maxSpeed
|
130 knots
|
gptkbp:maxTakeoffWeight
|
4,536 kg
|
gptkbp:notableUsers
|
gptkb:United_Nations
gptkb:United_States_Army
gptkb:Los_Angeles_Fire_Department
gptkb:Californian_Highway_Patrol
gptkb:Canadian_Forces
|
gptkbp:numberBuilt
|
over 7,000
|
gptkbp:operationalRange
|
300 miles
|
gptkbp:participatesIn
|
law enforcement
medical evacuation
search and rescue
firefighting
transport and utility
|
gptkbp:passengerCapacity
|
14
2,700 kg
|
gptkbp:performance
|
highly versatile
|
gptkbp:productionStartYear
|
1962
|
gptkbp:productionYears
|
1980
|
gptkbp:propulsion
|
single main rotor
|
gptkbp:range
|
600 km
|
gptkbp:role
|
utility helicopter
|
gptkbp:rotorDiameter
|
14.6 m
|
gptkbp:services
|
5,000 m
|
gptkbp:successor
|
gptkb:Bell_412
|
gptkbp:usedBy
|
military
civilian
|
gptkbp:variant
|
gptkb:Bell_212
gptkb:Bell_204
|
gptkbp:weight
|
2,268 kg
|
gptkbp:wingArea
|
none
|