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gptkbp:instance_of
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gptkb:helicopter
|
|
gptkbp:armament
|
optional machine guns
|
|
gptkbp:avionics
|
modernized systems available
|
|
gptkbp:country_of_origin
|
gptkb:United_States
|
|
gptkbp:crew
|
1 pilot
1 pilot, 1 co-pilot
|
|
gptkbp:customer_support
|
gptkb:Canadian_Forces
|
|
gptkbp:design
|
gptkb:Bell_Aircraft_Corporation
|
|
gptkbp:diameter
|
gptkb:1
2
10.7 m
|
|
gptkbp:engine_type
|
turboshaft
|
|
gptkbp:first_flight
|
gptkb:1980
|
|
gptkbp:fuel_capacity
|
120 gallons
|
|
gptkbp:height
|
3.6 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Bell 210
|
|
gptkbp:introduced
|
gptkb:1980
|
|
gptkbp:landing_gear
|
skid
|
|
gptkbp:legacy
|
widely used in various countries
|
|
gptkbp:length
|
12.8 m
|
|
gptkbp:maintenance
|
easy access for servicing
|
|
gptkbp:manufacturer
|
gptkb:Bell_Helicopter
|
|
gptkbp:market
|
commercial and military sectors
|
|
gptkbp:max_speed
|
130 knots
|
|
gptkbp:max_takeoff_weight
|
5,500 lb
|
|
gptkbp:military_technology
|
gptkb:Bell_210_C
|
|
gptkbp:mission
|
transport, reconnaissance
|
|
gptkbp:modifications
|
various mission-specific configurations
|
|
gptkbp:notable_features
|
twin-engine design
|
|
gptkbp:operational_range
|
300 nautical miles
|
|
gptkbp:passenger_capacity
|
6 passengers
|
|
gptkbp:power_output
|
420 shp
|
|
gptkbp:primary_user
|
military, law enforcement
|
|
gptkbp:produces
|
over 1,000 units
|
|
gptkbp:production_years
|
1980-1995
|
|
gptkbp:range
|
400 nautical miles
|
|
gptkbp:related_aircraft
|
gptkb:Bell_206
|
|
gptkbp:role
|
gptkb:helicopter
|
|
gptkbp:safety_features
|
dual hydraulic systems
|
|
gptkbp:service_ceiling
|
15,000 ft
|
|
gptkbp:status
|
in production
|
|
gptkbp:training
|
gptkb:Bell_210_B
|
|
gptkbp:variant
|
gptkb:Bell_212
|
|
gptkbp:weight
|
2,500 lb
|
|
gptkbp:weight_limit
|
5,000 lb
|
|
gptkbp:bfsParent
|
gptkb:Bell_412
|
|
gptkbp:bfsLayer
|
5
|