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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:aircraft_configuration
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high-wing
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gptkbp:aircraft_operated
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gptkb:transport_aircraft
8.4 m
various military operations
26.2 m
short takeoff and landing capabilities
550 km/h
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|
gptkbp:cargo_capacity
|
6,000 kg
|
|
gptkbp:cargo_types
|
rear ramp
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|
gptkbp:climb_rate
|
6 m/s
|
|
gptkbp:crew
|
2
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gptkbp:cruise_speed
|
400 km/h
|
|
gptkbp:design
|
gptkb:military_logistics
gptkb:Oleg_Antonov
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gptkbp:developed_by
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gptkb:Antonov_An-26
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gptkbp:engine
|
turboprop
|
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gptkbp:engine_type
|
turboprop
Ivchenko AI-20 D
|
|
gptkbp:first_flight
|
gptkb:1976
|
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gptkbp:fuel_capacity
|
6,000 L
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gptkbp:height
|
8.4 m
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|
https://www.w3.org/2000/01/rdf-schema#label
|
An-32 A
|
|
gptkbp:landing_distance
|
600 m
|
|
gptkbp:landing_gear
|
tricycle gear
|
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gptkbp:length
|
26.2 m
|
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gptkbp:manufacturer
|
gptkb:Antonov
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gptkbp:max_speed
|
550 km/h
|
|
gptkbp:max_takeoff_weight
|
27,000 kg
|
|
gptkbp:notable_features
|
short takeoff and landing capabilities
|
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gptkbp:number_built
|
over 300
|
|
gptkbp:number_of_engines
|
2
|
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gptkbp:operational_range
|
1,500 km with max payload
|
|
gptkbp:operational_use
|
gptkb:1977
|
|
gptkbp:passenger_capacity
|
gptkb:30
|
|
gptkbp:payload_capacity
|
7,500 kg
|
|
gptkbp:primary_user
|
gptkb:Indian_Air_Force
|
|
gptkbp:production_years
|
gptkb:1976
present
|
|
gptkbp:range
|
2,500 km
|
|
gptkbp:role
|
gptkb:transport_aircraft
|
|
gptkbp:service_ceiling
|
7,500 m
|
|
gptkbp:service_history
|
used by multiple countries
|
|
gptkbp:takeoff_distance
|
600 m
|
|
gptkbp:used_in
|
various military operations
|
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gptkbp:variant
|
gptkb:Antonov_An-26
|
|
gptkbp:wing_area
|
75 m²
|
|
gptkbp:wingspan
|
29.0 m
|
|
gptkbp:bfsParent
|
gptkb:Antonov_An-32
|
|
gptkbp:bfsLayer
|
6
|