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gptkbp:instance_of
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gptkb:aircraft
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|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:capacity
|
up to 13 passengers
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|
gptkbp:cargo_types
|
up to 1,500 kg of cargo
|
|
gptkbp:climb_rate
|
5.5 m/s
|
|
gptkbp:crew
|
2
2 pilots
|
|
gptkbp:cruise_speed
|
400 km/h
|
|
gptkbp:design
|
low-wing monoplane
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|
gptkbp:engine_power
|
1,100 hp
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|
gptkbp:engine_type
|
turboprop
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|
gptkbp:first_delivery
|
gptkb:1981
|
|
gptkbp:first_flight
|
gptkb:1980
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|
gptkbp:fuel_capacity
|
1,500 L
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|
gptkbp:height
|
4.8 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
C-12 J
|
|
gptkbp:introduced
|
gptkb:1980
|
|
gptkbp:landing_distance
|
900 m
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
15.8 m
|
|
gptkbp:manufacturer
|
gptkb:Beechcraft
|
|
gptkbp:max_speed
|
500 km/h
|
|
gptkbp:max_takeoff_weight
|
5,670 kg
|
|
gptkbp:military_service
|
gptkb:C-12_J_Huron
|
|
gptkbp:military_technology
|
gptkb:Beechcraft_Super_King_Air_200
|
|
gptkbp:number_built
|
over 200
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:operational_range
|
2,500 km
|
|
gptkbp:passenger_capacity
|
up to 11 seats
|
|
gptkbp:payload_capacity
|
1,500 kg
|
|
gptkbp:primary_user
|
gptkb:United_States_Army
gptkb:United_States_Navy
|
|
gptkbp:propeller
|
variable-pitch propellers
|
|
gptkbp:range
|
2,500 km
|
|
gptkbp:retired
|
still in service
|
|
gptkbp:role
|
gptkb:military_logistics
|
|
gptkbp:service_ceiling
|
7,620 m
|
|
gptkbp:service_entry
|
gptkb:1981
|
|
gptkbp:stall_speed
|
100 km/h
|
|
gptkbp:successor
|
gptkb:none
|
|
gptkbp:takeoff_distance
|
1,200 m
|
|
gptkbp:used_by
|
gptkb:United_States_military
|
|
gptkbp:variant
|
gptkb:Beechcraft_Super_King_Air
|
|
gptkbp:wing_area
|
37.2 m²
|
|
gptkbp:wingspan
|
17.4 m
|
|
gptkbp:bfsParent
|
gptkb:C-12_Huron
|
|
gptkbp:bfsLayer
|
4
|