1965 MIL MI 1


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    Aircraft Summary


    General

    Year
    1965
    Manufacturer
    MIL
    Model
    MI-1
    Condition
    Used
    FlightRules
    VFR
    Description
    Helicopter in working condition. Good condition. Exchange for a Robinson R-44 in the Russian Federation

    Airframe

    Total Time
    1000.0
    Airframe Notes
    The fuselage has a truss with a shell of aluminum alloy tail boom semi-monocoque construction with the reject end up beam and controlled stabilizer. The cabin located in the front seat pilot and two passengers in the back, in a training version with dual controls - student in the front seat and the instructor behind him

    Rotor

    Rotor Notes
    Rotor - three-bladed, with hinged blades and friction dampers. The blades are mixed with the tubular spar construction made of steel, wood stringers and ribs and a covering made of fabric and plywood. Blades trapezoidal planform and profile 230 NACA variable relative thickness. Recent versions of the Mi-1 were equipped with rectangular, all-metal blades with extruded spar made from aluminum alloy with attachments thereto sections with aluminum, honeycomb. Tail rotor - three-bladed, with a diameter of 2.5 m pushing, with wooden blades trapezoidal shape. [4]

    Engine

    Engine Notes
    The power plant includes one star semitsilindrovy piston engine AI-26B design Ivchenko capacity of 423 kW. It is installed in a horizontal position and is equipped with the bevel gear and a fan for forced cooling. [4] The engine is started with compressed air, the stock of which was small. To avoid falling into a difficult situation, when the air was over, and the engine can not start somewhere in the middle of the taiga, the pilots carried a spare can of compressed air

    Modifications/Conversions

    Modifications/Conversions
    Helicopter in working condition. Raise the 1 per year into the air to keep working. Also there is a lot of spare parts (by almost 2 helicopter, except the fuselage)

    Avionics

    Avionics/Radios
    standard devices

    Additional Equipment

    Additional Equipment
    Special equipment allows the helicopter to fly at any time, even in adverse weather conditions. Main rotor and tail rotor, as well as the windshield of the cockpit equipped with anti-icing systems alcohol.

    Exterior

    Year Painted
    2012
    Exterior Notes
    The fuselage has a truss with a shell of aluminum alloy tail boom semi-monocoque construction with the reject end up beam and controlled stabilizer

    Interior

    Year Interior
    1965
    Number of Seats
    3


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