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gptkbp:instance_of
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gptkb:helicopter
|
|
gptkbp:bfsLayer
|
5
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gptkbp:bfsParent
|
gptkb:Mil_Mi-26
gptkb:Mi-26
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:avionics
|
modernized cockpit
|
|
gptkbp:country
|
gptkb:Ukraine
|
|
gptkbp:crew
|
gptkb:5
2 pilots
|
|
gptkbp:design
|
interchangeable cargo modules
|
|
gptkbp:diameter
|
fenestron
32.0 m
|
|
gptkbp:emergency_services
|
dual hydraulic systems
|
|
gptkbp:engine_type
|
gptkb:engine
|
|
gptkbp:environmental_impact
|
low noise levels
|
|
gptkbp:features
|
large cargo hold
|
|
gptkbp:first_flight
|
gptkb:1980
|
|
gptkbp:global_presence
|
used worldwide
|
|
gptkbp:height
|
8.1 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mi-26 TP
|
|
gptkbp:introduced
|
gptkb:1983
|
|
gptkbp:is_used_by
|
gptkb:Russian_Air_Force
|
|
gptkbp:length
|
40.0 m
|
|
gptkbp:manufacturer
|
gptkb:Mil_Moscow_Helicopter_Plant
|
|
gptkbp:material
|
aluminum alloy
twin-engine
|
|
gptkbp:max_speed
|
295 km/h
|
|
gptkbp:max_takeoff_weight
|
600 m
1,200 m
56,000 kg
|
|
gptkbp:military_technology
|
gptkb:Mi-26_T
gptkb:Mi-26_TP
|
|
gptkbp:mission
|
disaster relief operations
|
|
gptkbp:modifications
|
firefighting version
|
|
gptkbp:notable_users
|
gptkb:Indian_Air_Force
|
|
gptkbp:number_built
|
over 300
|
|
gptkbp:operational_history
|
used in various conflicts
|
|
gptkbp:operational_range
|
1,000 km
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:origin
|
gptkb:Monarch
|
|
gptkbp:power_output
|
2 × D-136 engines
|
|
gptkbp:production_years
|
gptkb:1980
present
|
|
gptkbp:range
|
800 km
|
|
gptkbp:role
|
cargo transport
transport helicopter
|
|
gptkbp:safety_features
|
crashworthy seats
|
|
gptkbp:seating_capacity
|
30,000 kg
20,000 kg
up to 80
|
|
gptkbp:service_ceiling
|
4,500 m
|
|
gptkbp:training
|
pilot training
|
|
gptkbp:transportation
|
heavy lift operations
|
|
gptkbp:upgrades
|
avionics modernization
|
|
gptkbp:variant
|
gptkb:Mi-26
|
|
gptkbp:wingspan
|
32.0 m
|