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gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:bfsLayer
|
7
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gptkbp:bfsParent
|
gptkb:An-12_A
|
|
gptkbp:aircraft_operated
|
gptkb:Antonov
gptkb:aircraft
gptkb:Soviet_Air_Force
freight transport
750 km/h
40,000 kg
30.3 m
high-wing
9.8 m
|
|
gptkbp:aspect_ratio
|
8.5
|
|
gptkbp:crew
|
gptkb:5
|
|
gptkbp:design
|
gptkb:Company
|
|
gptkbp:elevation
|
7,500 m
|
|
gptkbp:engine
|
gptkb:4
4,100 hp
|
|
gptkbp:engine_type
|
turboprop
AI-20
|
|
gptkbp:first_flight
|
gptkb:1957
2000s
1957-12-16
|
|
gptkbp:fuel_capacity
|
14,000 L
|
|
gptkbp:height
|
9.8 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
An-12 A-100
|
|
gptkbp:is_used_by
|
gptkb:Soviet_Air_Force
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
30.3 m
|
|
gptkbp:manufacturer
|
gptkb:Antonov
|
|
gptkbp:max_speed
|
750 km/h
|
|
gptkbp:max_takeoff_weight
|
1,200 m
800 m
60,000 kg
|
|
gptkbp:notable_users
|
Air Forces of various countries
|
|
gptkbp:number_built
|
over 1,200
|
|
gptkbp:operational_range
|
4,000 km
|
|
gptkbp:production_years
|
1957-1973
|
|
gptkbp:propulsion
|
variable-pitch
|
|
gptkbp:range
|
5,000 km
|
|
gptkbp:retirement_year
|
1990s
|
|
gptkbp:role
|
gptkb:aircraft
gptkb:Company
|
|
gptkbp:seating_capacity
|
30,000 kg
20,000 kg
120 m³
rear ramp
|
|
gptkbp:service_ceiling
|
8,000 m
|
|
gptkbp:services
|
gptkb:1958
|
|
gptkbp:speed
|
650 km/h
|
|
gptkbp:successor
|
gptkb:An-70
|
|
gptkbp:variant
|
gptkb:Antonov_An-12
|
|
gptkbp:wing_area
|
200 m²
|
|
gptkbp:wingspan
|
38.0 m
|