The Open Joint Stock Company «Ilyushin Aviation Complex»
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IL-114
  • General
  • Technical Data


  • IL-114
    The IL-114 airplane is a passenger airplane designed for local routes.

    The airplane can be operated day and night in good and adverse weather conditions, from small airfields with concrete or unpaved runways.

    All flight information and air alert warning display facilities and controls for the onboard systems were unified into the multifunctional display system. The system outputs the data to color displays at the pilot's console.

    The IL-114 has a built-in passenger-boarding ramp and is equipped with an auxiliary power plant in order to ensure its operation autonomy in poorly organized airports.

    The airplane salon is provided with a buffet table, wardrobe and toilet facility.

    The first flight was carried out on March 29, 1990.

    Test-pilot was – V.S.Belousov.

    The AR MAK type certificate No.130-114 was obtained in April 1997.





    Dimensions (external)
    wing span (m)30
    length (overall) (m)26,877
    height (overall) (m)9,324
    wing area (m2)81,9
    sweepback angle at 1/4-chord line (degree)3,1
    fuselage diameter (m)2,86

    Engines
    engine typeÒV7-117S turboprop engine
    number of engines (pcs)2
    propeller shaft power (International Normal Atmosphere, Í=0) (h.p.)2 õ 2500
    propeller diameter (ì)3,6
    ICAO standards complianceApp.16, Ch.3

    Weights and Volumes
    max take-off weight (t)23,5
    max payload (t)6,5
    max fuel tanks capacity (liter)8360

    Performance
    cruise speed (km/h)500
    range with max passenger capacity (km)1000
    flight altitude (m)7600
    take-off run distance (m)1100
    landing run distance (m)900

    Seats
    flight crew2
    passengers64

    Service Life
    calendar30 years
    flights30000
    flight hours30000


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