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gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
4
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|
gptkbp:bfsParent
|
gptkb:C-12_Huron
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
gptkb:C-130_Hercules
high-wing
light transport aircraft
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:avionics
|
modernized systems
|
|
gptkbp:cockpit
|
pressurized
|
|
gptkbp:combat_role
|
transport and utility missions
|
|
gptkbp:crew
|
2
2 pilots
required for pilots
|
|
gptkbp:current_use
|
gptkb:aircraft
|
|
gptkbp:decommissioned
|
not applicable
|
|
gptkbp:design
|
gptkb:Beech_Aircraft_Corporation
|
|
gptkbp:engine
|
850 hp
|
|
gptkbp:engine_type
|
turboprop
|
|
gptkbp:features
|
high-wing configuration
|
|
gptkbp:first_flight
|
gptkb:1982
|
|
gptkbp:fuel_capacity
|
1,200 liters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
C-12 A
|
|
gptkbp:is_used_by
|
gptkb:military_unit
|
|
gptkbp:landing_gear
|
tricycle type
|
|
gptkbp:length
|
14.63 m
|
|
gptkbp:manufacturer
|
gptkb:Beechcraft
|
|
gptkbp:material
|
aluminum alloy
|
|
gptkbp:max_speed
|
500 km/h
|
|
gptkbp:max_takeoff_weight
|
900 m
1,200 m
5,670 kg
|
|
gptkbp:modifications
|
various military configurations
|
|
gptkbp:notable_users
|
gptkb:battle
|
|
gptkbp:number_built
|
over 300
|
|
gptkbp:operational_history
|
used in various conflicts
|
|
gptkbp:operational_range
|
1,500 nautical miles
|
|
gptkbp:origin
|
gptkb:United_States
|
|
gptkbp:performance
|
highly versatile
|
|
gptkbp:power_output
|
2 × Pratt & Whitney Canada P T6 A-42
|
|
gptkbp:production_years
|
1982-1992
|
|
gptkbp:range
|
2,500 km
|
|
gptkbp:retirement_year
|
still in service
|
|
gptkbp:role
|
gptkb:Company
|
|
gptkbp:seating_capacity
|
8
1,200 kg
1,500 kg
flexible seating arrangements
|
|
gptkbp:service_ceiling
|
7,620 m
|
|
gptkbp:services
|
gptkb:1984
|
|
gptkbp:successor
|
C-12 G
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:variant
|
gptkb:Beechcraft_Super_King_Air
|
|
gptkbp:wing_area
|
30.5 m²
|
|
gptkbp:wingspan
|
15.85 m
|