The Open Joint Stock Company «Ilyushin Aviation Complex»
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IL-76TD-90
  • General
  • Technical Data


  • IL-76TD
    The IL-76TD-90 aircraft equipped with the PS-90A-76 engines is a further development of the IL-76TD aircraft.

    The new engines allow substantial improvement of the aircraft effectiveness due to the following achievements:
    • 12% reduction of the specific fuel consumption;
    • 18% flight range increase;
    • direct operational costs reduction;
    • possibility to operate the aircraft from high-elevation aerodromes and in high-temperature environment;
    • noise and emission levels compliance with the latest International Civil Aviation Organization standards.






    Dimensions (external)
    wing span (m)50,5
    length (overall) (m)46,6
    height (overall) (m)14,76
    wing area (m2)300
    fuselage diameter (m)4,8

    Engines
    engine typePS-90A-76 by-pass turbojet engine
    number of engines (pcs)4
    max take-off thrust (International Standard Atmosphere, Í=0) (kg)4 õ 16000
    bypass ratio4,4
    ICAO standards complianceApp.16, Ch.3

    Weights and Volumes
    max take-off weight (t)195
    max payload (t)50
    max fuel tanks capacity (liter)109500

    Performance
    cruise speed (km/h)800-830
    range with payload (km)of 50t – 4300
    flight altitude (m)9000-12000
    take-off run (m)1300
    landing run (m)930

    Seats
    flight crew5

    Dimensions (cargo compartment)
    length including the ramp (m)24,54
    width (m)3,45
    height (m)3,4
    volume (m3)321

    Service Life
    calendar20 years
    flights10000
    flight hours30000


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