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name: MI-26
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Country of Origin Russia 
Builder MIL 
Date of Introduction 1983 
Role Heavy cargo-transport 
Similar Aircraft Mi-6 Hook, HH-3E Jolly Green Giant 
Blades Main rotor - 8
Tail rotor - 5 
Rotor diameter 105 ft (32 m) 
Length 111 ft (33.8 m) 
Length (rotors turning) 40 meters 
Length (fuselage) 33.5 meters 
Width 8.2 meters 
Height 26 ft., 5 in. / 8.1 meters 
Tail Rotor Diameter 7.6 meters 
Cargo Compartment Dimensions  12 meters - Floor Length
3.3 meters - Width
Height variable from 2.9 to 3.2 meters 
Weight 49500 kg - Normal takeoff weight
56000 kg - Maximum takeoff weight
28200 kg - empty weight
20000 kg - Load-lifting capacity
(100+ equipped troops, armored vehicles) 
Engine 2 x 11,400 shp Lotarev D-136 turbines 
Maximum speed 295 km/h 
Cruising speed 183 mph / 255 km/h 
Range 1200 km with Aux Fuel
800 km with maximum fuel reserve
475-800 km with maximum loading 
Service Ceiling 4600 m
1,800 m Hover (out of ground effect)
4,500 m Hover (in ground effect) 
Fuel  11,900 liters Internal 
Standard Payload 20,000 kg Internal or external load
over 80 troops, 60 litters, or
2x BRDM-2 scout cars, or 2x BMDs, or
1x BMP or,
1x BTR-60/70/80 or,
1x MT-LB
Armament Usually none 
Survivability/Countermeasures Main and tail rotor blades electrically deiced.
Infrared signature suppressors on engines.
Infrared jammers and decoys; flares.
Self-sealing fuel tanks. 
AVIONICS The avionics and navigational package, a Doppler weather radar, and a fully functioning autopilot allow for day/night all-weather operation. 
Crew 5 (2x pilots, 1x navigator, 1x flight engineer, 1x loadmaster)


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