Il-76MD-90A

  • Performance

    General Data

    Il-76MD-90A is created on the basis of mass production Il-76MD aircraftfor the purposes of further improvement of this type of aircraft and extension of its transportation capacity by way of modernizing the wingand installing more powerful, economical and quiet PS-90A-76engines, instead of D-30KP-2 engines.

    Il-76MD-90A is meant for parachuting and landing of military personnel, military equipment, cargoes, fuel and containers.

    Modified Il-76MD-90A aircraft complies with standards for noise level determined by requirements of Appendix 16 Chapter 4 of ICAO standards, and for emission of harmful substances into the atmosphere. All this, along with the opportunities for aircraft navigation by RNP-1 requirements allowed for expanding the flight geography of Il-76MD-90A both in local and international airlines.

    The cockpit and flying equipment have been completely modernized.The aircraft makes use of the modern digital flying and navigation instruments. The pilots’ dashboard includes six multifunctional digital displays representing all information required to fly the plane. The flight navigator’s workplace is equipped with a multifunctional indicator that enables presentation of navigation data. Thus, the aircraft design implements the so-called glass cockpit, which allows reducing the stress on the crew and improves flight safety.

    All works in modernization of the aircraft, from early designing to manufacturing a flight model, have been conducted in a digital form with the use of modern computer systems. All design technology documents for the aircraft has been digitalized completely and launched into mass production using modern digital technologies.

    First flight took place on October 12, 2012. Test pilot was N.D. Kuimov.

    Developer: S.V. Iliushin Aviation Complex OJSC.

    Manufacturer: Aviastar-SP CJSC.

    • Top thrust (SI system, H=0)
      4х16000kgf
    • Maximum takeoff weight
      210tons
    • Flight altitude
      12 100m
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    Main technical characteristics

    Dimensional characteristics
    Length, m 46,6
    Height, m 14,76
    Wingspan, m 50,5
    Wing area, sq. m. 300
    Fuselage diameter, m 4,8
    Power plant parameters
    Number x engine type 4 x turbojet engine
    Engine
    		PS-90A-76
    Top thrust (SI system, H=0), kgf 16 000
    Weight parameters
    Maximum takeoff weight, tons 210
    Maximum payload, tons 52 (with extension to 60)
    Fuel tank capacity, l 109 500

    Aircraft performance
    Cruising speed, km/h 750–800
    Flight altitude, m 9 100–12 100
    Flight range with payload of 52 tons, km 5 000
    Takeoff distance, m 1 540
    Landing distance, m 1050
    Number of seats
    Crew, persons 6
    Passengers, persons single-deck version:
    126 paratroopers
    145 military personnel
    114 wounded
    Double-deck version:
    225 military personnel
    Freight compartment parameters
    Length x Width x Height, m 24,54x3,45x3,4
    Volume, cubic meters 321
    Specified life
    Calendar operating life, years30
    Number of flights8 000
    Number of flight hours, hr.10 000

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