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Object «MIL Mi-26» has attributes

Attribute Value
General
Manufacturer MIL Helicopters
Model MIL Mi-26
Country Russia
Manufactured from 1981 year
Manufactured to Add
Type Large Helicopters
Icao MI26
Performance
Engine 2x 2 × Lotarev D-136 turboshafts
Power, hp 11,400 hp
Power, lbf Add
Avionics Groza 7A813 weather radar, Integrated PKV-26-1 flight/nav system
Max cruise speed 294 km/h
Approach speed Add
Travel range 1,952 km
Fuel economy 0.186 km/l
Service ceiling 4,602 m
Rate of climb 7.73 m/sec
Take off distance Add
Landing distance Add
Weights
Max take off weight 56,000 kg
Max landing weight Add
Max payload 20,000 kg
Fuel tank capacity 12,000 l
Baggage volume 6.16 m³
Dimensions
Seats 9
Seats - business class 9
Seats - first class 65
Cabin height 3.2 m
Cabin width 3.1 m
Cabin length 12.1 m
Exterior length 40.03 m
Tail height 7.95 m
Fuselage diameter Add
Wing span 32 m
Wing tips No Winglets

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There was one edit, no edits waiting approval. Last edited by qjast(1747), Oct 26, 2021 (43 fields were changed)
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