Il-114-100

  • Performance

    General Data

    The Il-114-100 is a passenger aircraft for local airlines and is based on Il-114 aircraft.The aircraft is equipped with high-efficiency PW-127Нengines by Pratt & Whitney (Canada) with the capacity of 2 750 hp. Fuel consumption for a standard Il-114-100 aircraft is 500-550 kg per flight hour. The aircraftuses a modernized digital flight navigation complex, the TsPNK-114 Collins, jointly developed by NII AO Federal State Unitary Enterpriseand Rockwell Collins (USA), which complies with ICAO and Eurocontrol navigation requirements for aircraft of this class.

    A modern passenger cabin ensures comfortable flight in any weather conditions.

    For this aircraft, the system of operation on technical conditionand without capital repairs has been accepted, which ensures maintaining the required level of airworthiness.

    Aircraft is operated by Uzbek AirlinesNational Air Line (Republic of Uzbekistan).

    First flight took place on January 26, 1999. Test pilot was I.I. Gudkov.

    Type Certificate No. ST178 Il-114-100 AR by IAC was granted in December 1999.

    • Maximum shaft power (МСА, H=0)
      2х2750kgf
    • Maximum takeoff weight
      23,5tons
    • Maximum flight altitude
      7 600m
    Another figure

    Main technical characteristics

    Dimensional characteristics
    Length, m 26,877
    Height, m 9,324
    Wingspan, m 30
    Wing area, sq. m. 81,9
    Fuselage midsection, m 2,86
    Power plant parameters
    Number x engine type 2 x turbo-propeller engine
    Engine 
    		PW127H
    Maximum shaft power (МСА, H=0), kgf. 2 750
    Propeller diameter, m 3,93
    Compliance with ICAO standards Appendix 16, Chapter 3
    Weight parameters
    Maximum takeoff weight, tons 23,5
    Maximum payload, tons 6,5
    Fuel tank capacity, l 8 780
    Aircraft performance
    Cruising speed, km/h up to 500
    Flight altitude, m up to 7 600
    Flying range with maximum number of passengers, km 1 500
    Flying range with maximum fuel reserve, km 4 730
    Takeoff distance, m 750
    Landing distance, m 550
    Number of seats
    Crew, persons 2
    Passengers, persons 64
    Specified life
    Calendar operating life, years 30
    Number of flights 12 000
    Number of flight hours, hr. 18 000