The Open Joint Stock Company «Ilyushin Aviation Complex»
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IL-96-400
  • General
  • Technical Data


  • IL-96-400
    The IL-96-400 airplane is a modified well-reputed IL-96-300. The airplane was developed taking into account the air carriers' needs, and now it meets the national and international requirements.

    The up-to-date aerodynamics of the IL-96-400 airplane, its PS-90A low fuel consumption engines, impressive commercial load capacity, improved frame design, updated onboard avionics complex and highly reliable functional aircraft systems allow the airplane to operate with maximum effectiveness that is not inferior to the best foreign analogues.

    The IL-96-400 airplane advantages are the following:
    • high technical and economical characteristics;
    • availability of the complete infrastructure within the aircraft and engine maintenance support, flight and technical personnel trained for this type of aircraft;
    • competitive prices for the airplane and its engines in comparison with the foreign analogues.





    Dimensions (external)
    wing span (m)60,105
    length (overall) (m)63,939
    height (overall) (m)15,717
    wing area (m2)350
    sweepback angle at 1/4-chord line (degree)30
    fuselage diameter (m)6,08

    Engines
    engine typePS-90A 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)265
    max payload (t)58
    max fuel tanks capacity (liter)152620

    Performance
    cruise speed (km/h)870
    range with max passenger capacity (km)10000
    flight altitude (m)9000-12000
    take-off run distance (m)2700
    landing run distance (m)1650

    Seats
    flight crew3
    passengers in  single class version – 436
      two classes version – 386
      three classes version – 315

    Service Life
    calendar20 years
    flights20000
    flight hours60000


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