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gptkbp:instance_of
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gptkb:helicopter
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gptkbp:bfsLayer
|
5
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gptkbp:bfsParent
|
gptkb:Moscow_Helicopter_Plant
gptkb:Mil_Mi-26
gptkb:Mi-26_Halo
gptkb:Mi-26
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gptkbp:aircraft_operated
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gptkb:helicopter
Mi-6
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gptkbp:armament
|
gptkb:none
|
|
gptkbp:avionics
|
modern navigation systems
|
|
gptkbp:crew
|
gptkb:5
|
|
gptkbp:design
|
cargo transport
|
|
gptkbp:diameter
|
fenestron type
|
|
gptkbp:engine
|
11,400 shp
|
|
gptkbp:engine_type
|
turbo-shaft
|
|
gptkbp:features
|
large cargo hold
|
|
gptkbp:first_flight
|
gptkb:1980
glass cockpit
|
|
gptkbp:fuel_capacity
|
3,000 L
|
|
gptkbp:global_presence
|
used worldwide
|
|
gptkbp:height
|
8.13 m
|
|
gptkbp:historical_significance
|
largest helicopter in the world.
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mi-26 T
|
|
gptkbp:introduced
|
gptkb:1983
|
|
gptkbp:landing_gear
|
tricycle type
|
|
gptkbp:length
|
40 m
|
|
gptkbp:maintenance
|
gptkb:launch_complex
|
|
gptkbp:manufacturer
|
gptkb:Mil_Moscow_Helicopter_Plant
|
|
gptkbp:material
|
aluminum alloy
|
|
gptkbp:max_speed
|
295 km/h
|
|
gptkbp:max_takeoff_weight
|
56,000 kg
|
|
gptkbp:military_technology
|
gptkb:Mi-26
Mi-26 T2
|
|
gptkbp:mission
|
disaster relief operations
|
|
gptkbp:notable_users
|
gptkb:Russian_Air_Force
|
|
gptkbp:operational_area
|
high
|
|
gptkbp:operational_history
|
used in various military and civilian operations
|
|
gptkbp:operational_range
|
1,000 km
|
|
gptkbp:produced_by
|
ongoing
|
|
gptkbp:production_location
|
gptkb:Russia
|
|
gptkbp:production_years
|
1983-present
|
|
gptkbp:propulsion
|
2 engines
|
|
gptkbp:range
|
800 km
|
|
gptkbp:role
|
transport helicopter
|
|
gptkbp:safety_record
|
generally safe
|
|
gptkbp:seating_capacity
|
gptkb:television_series
20,000 kg
external load capability
side door
|
|
gptkbp:service_ceiling
|
4,600 m
|
|
gptkbp:successor
|
gptkb:none
|
|
gptkbp:training
|
extensive
|
|
gptkbp:type
|
heavy-lift helicopter
|
|
gptkbp:variant
|
gptkb:Mi-26
|
|
gptkbp:weight
|
28,000 kg
|
|
gptkbp:wing_area
|
200 m²
|
|
gptkbp:wingspan
|
32 m
|