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gptkbp:instance_of
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gptkb:aircraft
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|
gptkbp:aircraft_configuration
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passenger and cargo
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|
gptkbp:aircraft_operated
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gptkb:light_aircraft
4.8 m
15.75 m
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gptkbp:aircraft_role
|
utility aircraft
|
|
gptkbp:aircraft_type
|
twin-engine aircraft
|
|
gptkbp:cargo_capacity
|
1,500 kg
|
|
gptkbp:crew
|
2
2 pilots
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|
gptkbp:crew_capacity
|
2
|
|
gptkbp:cruise_speed
|
300 km/h
|
|
gptkbp:design
|
gptkb:Antonov_Design_Bureau
high-wing monoplane
|
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gptkbp:engine_configuration
|
twin-engine turboprop
|
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gptkbp:engine_power
|
2 x 1,000 hp
|
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gptkbp:engine_type
|
turboprop
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gptkbp:first_flight
|
gptkb:1970
|
|
gptkbp:first_introduced
|
1970s
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gptkbp:fuel_capacity
|
1,800 L
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|
gptkbp:height
|
4.8 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
An-28 B-100
|
|
gptkbp:landing_distance
|
600 m
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
15.75 m
|
|
gptkbp:manufacturer
|
gptkb:Antonov
|
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gptkbp:max_speed
|
400 km/h
|
|
gptkbp:max_takeoff_weight
|
5,700 kg
|
|
gptkbp:notable_features
|
short takeoff and landing capabilities
|
|
gptkbp:number_built
|
over 100
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|
gptkbp:number_of_engines
|
2
|
|
gptkbp:operational_range
|
1,200 km
|
|
gptkbp:passenger_capacity
|
gptkb:14
|
|
gptkbp:payload_capacity
|
1,500 kg
|
|
gptkbp:primary_use
|
passenger and cargo transport
|
|
gptkbp:production_location
|
gptkb:Ukraine
|
|
gptkbp:production_years
|
1970s to 1990s
|
|
gptkbp:propeller
|
variable-pitch propellers
|
|
gptkbp:range
|
1,200 km
|
|
gptkbp:role
|
regional transport
|
|
gptkbp:service_ceiling
|
7,500 m
|
|
gptkbp:successor
|
An-38
|
|
gptkbp:takeoff_distance
|
800 m
|
|
gptkbp:used_by
|
various operators
|
|
gptkbp:variant
|
An-28
|
|
gptkbp:wingspan
|
17.5 m
|
|
gptkbp:bfsParent
|
gptkb:Antonov_An-28
|
|
gptkbp:bfsLayer
|
7
|