The Open Joint Stock Company «Ilyushin Aviation Complex»
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IL-86
  • General
  • Technical Data


  • IL-86
    In September 1969, the Experimental Design Bureau n/a S.V.Ilyushin was commissioned to start the works on the development of an airplane of a greater passenger capacity. The order stipulated the aircraft operation based on the existing and available ground technical bases, runways and airports. The requirements included the luggage transportation based on the "luggage with the passenger plus containers" principle, installation of three entrance doors equipped with the built-in boarding ramps thus excluding the necessity to use the airdrome facilities to ensure passengers boarding and debarkation. A new wide-body IL-86 airplane became the airplane that met all these requirements.

    From December 1980, the IL-86 aircraft are operated on domestic and international routes with the most heavy passenger traffic flows. The IL-86 aircraft operation proved that the airplane ensures the substantial reduction of the operational costs and significant fuel economy. The aircraft design features allowed to start its regular operations without expensive reconstruction of the existing airports.

    In October 1981, IL-86 set 18 world records.

    On December 22, 1976, the experimental IL-86 made its maiden flight.

    A test pilot of the airplane was E.I.Kuznetsov.

    On October 25, 1977 was a maiden flight of the first mass manufactured IL-86.

    The IL-86 is the first home certificated airplane. The GOSAVIAREGISTR of the USSR issued a Certificate of Airworthiness No.10-86.





    Dimensions (external)
    wing span (m)48,06
    length (overall) (m)59,54
    height (overall) (m)15,5
    wing area (m2)361
    sweepback angle at 1/4-chord line (degree)35
    fuselage diameter (m)6,08

    Engines
    engine typeNK-86 by-pass turbojet engine
    number of engines (pcs)4
    max take-off thrust (International Standard Atmosphere, Í=0) (kg)4 õ 13000
    bypass ratio1,15
    ICAO standards complianceApp.16, Ch.2

    Weights and Volumes
    max take-off weight (t)206
    max payload (t)42
    max fuel tanks capacity (liter)83676

    Performance
    cruise speed (km/h)850-900
    range with max passenger capacity (km)3800
    flight altitude (m)10000-12000
    take-off run distance (m)2700
    landing run distance (m)1980

    Seats
    flight crew3
    passengers350

    Service Life
    calendar20 years
    flights20000
    flight hours30000


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