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gptkbp:instanceOf
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aircraft
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gptkbp:aircraft
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military transport aircraft
twin-engine turboprop
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gptkbp:armament
|
can be equipped with bombs or rockets
|
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gptkbp:capacity
|
up to 38 passengers
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gptkbp:crew
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2
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gptkbp:design
|
high-wing monoplane
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gptkbp:engine
|
2 × Ivchenko AI-24V turboprop engines
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gptkbp:enginePower
|
2,400 hp
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gptkbp:firstFlight
|
1969-12-21
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gptkbp:fuelCapacity
|
5,000 liters
|
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gptkbp:height
|
8.10 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Antonov An-26
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gptkbp:introduced
|
1970
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gptkbp:landingGear
|
tricycle landing gear
|
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gptkbp:length
|
24.76 m
|
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gptkbp:manufacturer
|
gptkb:Antonov
|
|
gptkbp:maxSpeed
|
400 km/h
|
|
gptkbp:maxTakeoffWeight
|
22,000 kg
|
|
gptkbp:notableUsers
|
gptkb:Soviet_Air_Force
gptkb:Russian_Air_Force
gptkb:Ukrainian_Air_Force
gptkb:Air_Force_of_the_Republic_of_Korea
Various cargo airlines
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|
gptkbp:operationalRange
|
1,200 km with maximum payload
|
|
gptkbp:passengerCapacity
|
5,000 kg
30 m³
|
|
gptkbp:primaryUser
|
military forces
|
|
gptkbp:produces
|
over 1,400 units
|
|
gptkbp:propulsion
|
four-blade propellers
|
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gptkbp:range
|
1,500 km
|
|
gptkbp:retired
|
varies by operator
|
|
gptkbp:role
|
transport aircraft
|
|
gptkbp:services
|
7,500 m
|
|
gptkbp:status
|
in service
|
|
gptkbp:successor
|
gptkb:Antonov_An-32
|
|
gptkbp:takeoffDistance
|
600 m
|
|
gptkbp:usedBy
|
military and civilian operators
|
|
gptkbp:variant
|
gptkb:An-26-100
An-26A
An-26B
An-26-200
An-26M
|
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gptkbp:wingArea
|
75 m²
|
|
gptkbp:wingspan
|
29.00 m
|