• Performance

    General Data

    Il-76MD-90 military transport aircraftis based on the Il-76MD series productionmilitary transport aircraftand is designed for landing and parachuting of military personnel, equipment and various cargos.

    The aircraft has more powerful and economic PS-90A-76 engines, which meet ICAO requirements for noise and harmful emissions. Installation of new engines allowed for increasing cost efficiency of the aircraft significantly, due to reduced average fuel consumption in cruise flight, increasingflying range and commercial load, and reducing direct operational costs.

    • Top thrust (SI system, H=0)
    • Maximum takeoff weight
    • Maximum flight altitude
      12 100m
    Another figure

    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
    Top thrust (SI system, H=0), kgf 16 000
    Weight parameters
    Maximum takeoff weight, tons 195
    Maximum payload, tons 50
    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 40 tons, km 5 400
    Takeoff distance, m 1 300
    Landing distance, m 930
    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, years 30
    Number of flights 4 000
    Number of flight hours, hr. 6 000
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