The Open Joint Stock Company «Ilyushin Aviation Complex»
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IL-76MD
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  • Technical Data


  • IL-76MD
    The IL-76MD military transport aircraft was developed based on a mass manufactured IL-76M military transport aircraft. By virtue of strengthening the airplane main structural elements (e.g. frame, landing gear) the maximum take-off weight and commercial payload were increased.

    The aircraft is designed for the following tasks:
    • air-mission landing (transportation) of personnel, weapons and military equipment, cargo, fuel and containers;
    • air drop of personnel, weapons and military equipment and cargo.
    In order to provide for the INTERNATIONAL CIVIL AVIATION ORGANIZATION newly issued requirements for the noise and harmful substances emission levels the D 30KP engines are now being replaced with the more powerful and fuel-efficient PS-90A-76 engines. All these measures will increase the airplane economical efficiency.





    Dimensions (external)
    wing span (m)50,5
    length (overall) (m)46,6
    height (overall) (m)14,76
    wing area (m2)300
    sweepback angle at 1/4-chord line (degree)25
    fuselage diameter (m)4,8

    Engines
    engine typeD30-KP ser.2 by-pass turbojet engine
    number of engines (pcs)4
    max take-off thrust (International Standard Atmosphere, Í=0) (kg)4 õ 12000
    ICAO standards complianceApp.16, Ch.2

    Weights and Volumes
    max take-off weight (t)190
    max payload (t)48
    max fuel tanks capacity (liter)109500

    Performance
    cruise speed (km/h)750-770
    range with max payload (km) 3800
    range with max fuel  (km)8700
    flight altitude (m)9000-12000
    take-off run (m)1700
    landing run (m)930

    Seats
    flight crew7


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