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gptkbp:instance_of
|
gptkb:helicopter
|
|
gptkbp:aircraft_operated
|
gptkb:helicopter
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:avionics
|
modernized options available
|
|
gptkbp:capacity
|
15 passengers
|
|
gptkbp:cargo_capacity
|
2,500 lbs
|
|
gptkbp:configuration
|
gptkb:helicopter
single rotor
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
twin-turbine
|
|
gptkbp:engine
|
PT6 T-3 B
|
|
gptkbp:engine_type
|
turboshaft
|
|
gptkbp:first_flight
|
gptkb:1971
|
|
gptkbp:fuel_capacity
|
1,200 liters
|
|
gptkbp:height
|
4.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Bell 212 G
|
|
gptkbp:introduced
|
gptkb:1971
|
|
gptkbp:length
|
15.5 m
|
|
gptkbp:manufacturer
|
gptkb:Bell_Helicopter
|
|
gptkbp:max_speed
|
130 knots
|
|
gptkbp:notable_features
|
twin-engine
wide cabin
versatile design
|
|
gptkbp:operational_range
|
500 km
|
|
gptkbp:primary_user
|
gptkb:United_Nations
gptkb:United_States_Army
gptkb:Canadian_Forces
search and rescue operations
medical evacuation services
firefighting services
various law enforcement agencies
|
|
gptkbp:produces
|
over 1000
|
|
gptkbp:production_years
|
gptkb:1971
gptkb:1985
|
|
gptkbp:propulsion
|
twin-engine
|
|
gptkbp:range
|
400 nautical miles
|
|
gptkbp:role
|
gptkb:helicopter
transport helicopter
reconnaissance helicopter
|
|
gptkbp:safety_features
|
crashworthy design
dual controls
emergency flotation system
|
|
gptkbp:service_ceiling
|
15,000 ft
|
|
gptkbp:successor
|
gptkb:Bell_412
|
|
gptkbp:used_by
|
gptkb:military
civilian
|
|
gptkbp:variant
|
gptkb:Bell_212
|
|
gptkbp:weight
|
3,175 kg
|
|
gptkbp:wingspan
|
14.6 m
|
|
gptkbp:bfsParent
|
gptkb:Bell_212
|
|
gptkbp:bfsLayer
|
6
|