The multi-purpose wide-fuselage Mi-26T transport helicopter. It is intended for carrying of techniques and large-size cargoes up to 20 tons either inside the cargo compartment or on an external sling.

A combined internal and external load up to 20 tons is also possible.

THE Mi-26 CAN BE SUCCESSFULLY USED:

   • For construction works (mounting derricks, bridges, electrical power line masts and other complex engineering operations) Extreme accuracy can be achieved due to the sensitive and accurate hovering system operated from an auxiliary under-fuselage pilot-operator cabin
   • For extinguishing or localizing forest and industrial fires
   • For providing medical assistance and evacuation of victims from disaster areas, located in remote and difficult of access regions.
   • For delivery and distribution of fuel to the consumers (kerosene and diesel fuels) and lubricants.

   The cargo compartment is equipped with a 6 tons hoisting device and two electric winches. A clearance control system is available for handling large-size cargo.

   The helicopter is equipped with avionics allowing operation on international routes, day or night flights, flying in extreme weather conditions.

   The cockpit is comfortable, armored, pressurized, with on air conditioning system and excellent visibility.

   The equipment and structure of the helicopter allows autonomous operation where ground facilities are not available.
The helicopter has been certified in Russia in conformity with the airworthiness regulations (NLGV-2), in accordance with the FAR-29 USA regulations

PERFORMANCE

Engine D-136..................................... 2x11.400 hp

Teke-off weight:
    normal.................................................. 49.6 t
    maximum ............................................. 56.0 t
    empty weight........................................ 28.6 t

Load-carrying capacity:
    in cargo compartment and
    on an external sling ............................... 20.0 t
    dimensions of cargo cabin 12.1x3.29x3.17 m 
    cruising speed per hour..................... 255 km

Ceiling under ISA conditions (at normal take-off weight):
    hovering OGE (minimum)................. 1.520 mf
    service (minimum)........................... 4.600 m
    
Range:
    standard tanks................................... 800 km
    four extra tanks .............................. 1.920 km
    Diameter of main rotor............................... 32.0 m
    Number of blades ................................................ 8
    Crew................................................................... 5