• Performance

    General Data

    The Il-96-400M is a wide-body long-range airliner which is created on the basis of the production Il-96 aircraft for the purpose of further development of this type of aircraft and increasing their transport capabilities due to the longer fuselage and more powerful PS-90A1 engines instead of PS-90A.

    The Il-96-400M can carry up to 370 passengers. Large diameter of the fuselage provides modern day level of comfort for passengers during long flights. In terms of reliability, safety and effectiveness the Il-96-400M is on the level with world analogues.

    Due to the usage of modern systems and “glass cockpit” the flight crew of the aircraft will consist of 3 people.

    The aerodynamic configuration, design and aircraft systems employ state-of-the-art engineering solutions, which ensure high level of safety and effectiveness of aircraft operation. Modern materials used in the structure allow for decrease of aircraft weight, at the same time providing necessary integrity and stiffness. Wing aerodynamic ensures reliable and safe flight within the whole operational speed range.

    • Top thrust (SI system, H=0)
      4х17 400kgf
    • Maximum takeoff weight
    • Flight altitude
      13 100m
    Another figure

    Estimated  technical characteristics

    Dimensional characteristics
    Length, m 63,939
    Height, m 15,717
    Wingspan, m 60,105
    Wing area, sq. m. 350
    Fuselage diameter, m 6,08
    Power plant parameters
    Number x engine type 4 x turbojet engine
    Engine model PS-90A1
    Top thrust (SI system, H=0), kgf 17 400
    Compliance with ICAO standards Appendix 16, Chapter 4
    Weight parameters
    Maximum takeoff weight, tons 270
    Maximum payload, tons 58
    Fuel tank capacity, l 150 000
    Aircraft performance
    Cruising speed, km/h 830-850
    Flight altitude, m 9 100–13 100
    Flight range with passengers, km 8 750
    Takeoff distance, m 2 020
    Landing distance, m 1 200
    Number of seats
    Crew, persons 3
    Passengers, persons single-class configuration 370
    Specified life
    Calendar operating life, years 20
    Number of flights 20 000
    Number of flight hours, hr. 60 000

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