The Open Joint Stock Company «Ilyushin Aviation Complex»
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IL-114-100

  • General
  • Technical Data


  • IL-114-100
    The IL-114-100 airplane version was made on the basis of the IL-114 airplane. A new version of the airplane unlike the previous version is equipped with the PW-127H engines manufactured by «PRATT&WHITNEY» (Canada). The new power plant permits to increase the flight range. It also improves the take-off and landing characteristics including those under mountainous terrain and high temperature conditions.

    Besides, like the basic aircraft the IL-114-100 is designed for operation on local routes in order to provide passengers with services close by its comfort level to those at long-haul routes.

    The airplane first flight was carried out on January 26, 1999.

    The test pilot was – I.I.Gudkov.

    The AR MAK type certificate No.ST 178-IL-114-100 was obtained in December 1999.





    Dimensions (external)
    wing span (m)30
    length (overall) (m)26,877
    height (overall) (m)9,324
    wing area (m2)81,9
    fuselage diameter (m)2,86

    Engines
    engine typeÐW-127Í turboprop engine
    number of engines (pcs)2
    propeller shaft power (International Standard Atmosphere, Í=0) (h.p.)2 õ 2645
    propeller diameter (ì)3,72
    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) up to 500
    range with 52 passenger capacity (km) 2000
    flight altitude (m) up to 7600
    take-off run (m)750
    landing run (m)550

    Seats
    flight crew2
    max passengers64

    Service Life
    calendar30 years
    flights30000
    flight hours30000


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