MI-8

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    The Mi-8T

    Multipurpose Mi-8T helicopters belongs to the middle class. This model is the most common in the world, as the reliability, low maintenance and easy to operate. On the basis of the Mi-8T, which is the original purpose of the transport and landing of the helicopter for the Air Force, more than one hundred modifications.

    The basic assembly of the helicopter Mi-8 is designed to transport people and cargo weighing up to 4 tons. The design includes an electrothermal de-icing system for frost protection of main rotor, tail rotor and a glass cockpit. This allows you to use the helicopter at low temperatures, which is especially important in the Northern regions of Russia, Scandinavia and even the Arctic.

    Additional equipment of the helicopter external sling system can be used for transportation of oversized and bulky loads weighing up to 3 tons. Construction and equipment of the helicopter allow to maintain it at independent basing on unequipped sites.

    Mi-8AMT

    E 8AMT repeats construction of the Mi-8MTs. In a modification of the Mi-171A (export name) belongs to a class of average utility. Model Mi-8AMT has a wide scope: transport, passenger, VIP, fire, ambulance and rescue.

    Components of the Mi-171A is equipped to carry up to 26 passengers in a comfortable environment. The helicopter is equipped with a toilet, wardrobe, auxiliary input on the rear fuselage, a compartment for luggage and hand luggage. Low vibration and noise, comfortable seats, wide windows, air conditioning, presence information and emergency lighting panels, fluorescent lighting provide a comfortable environment for passengers.

    Mi-8 helicopters VIP (171 VIP)

    Have a comfortable cabin for 10 to 13 passengers, the examples of VIP salons represented on the photo.

     

    Mi-8T

    Mi-8MT
    (MI-17)

    MI-8MTB-1
    (MI-17-1B)

    MI-8AMT
    (MI-171)

    MI-172

    Crew

    3 people

    3 people

    3 people

    3 people

    3 people

    Number of passengers (paratroopers)

    24 people

    24 people

    24 people

    27 people

    26 people

    Length (with rotations screws)

    25,31 m

    25,31 m

    25,31 m

    25,31 m

    25,31 m

    Height (with rotations tail rotor)

    5,54 m

    5,54 m

    5,54 m

    5,54 m

    5,54 m

    Rotor diameter

    21,3 m

    21,3 m

    21,3 m

    21,3 m

    21,3 m

    Empty weight

    6934 kg

    7200 kg

    7381 kg

    6913 kg

    7514 kg

    Normal take-off weight

    11 100 kg

    11 100 kg

    11 100 kg

    11 100 kg

    11 878 kg

    Maximum takeoff weight

    12 000 kg

    13 000 kg

    13 000 kg

    13 000 kg

    n/d

    Engines

    2 × TB2-117

    2 × TB3-117MT

    2 × TB3-117BM

    2 × TB3-117BM

    2 × TB3-117BM

    Engine power (at takeoff)

    2 × 1500 h.p.

    2 × 1900 h.p.

    2 × 2000 h.p.

    2 × 2000 h.p.

    2 × 2000 h.p.

    Maximum speed

    260 km/h

    250 km/h

    250 km/h

    250 km/h

    250 km/h

    Cruising speed

    225 km/h

    220 km/h

    240 km/h

    230 km/h

    230 km/h

    Dynamic ceiling

    4500 m

    5000 m

    6000 m

    6000 m

    6000 m

    Practical range

    480 km

    520 km

    590 km

    570 km

    715 km

    • Range, km:
    •         
      • at the maximum stock of aviation fuel 800
      •         
      • with a maximum load of 550
          
    • Consumption of aviation fuel, t / h 0.72
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