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  • Antonov An-140

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    Description

    The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips.

    General Information

    First flown on 17 September 1997, the 52 passenger An-140 is manufactured at the main production line in Kharkiv by KHDABP, in Samara by Aviakor, and assembled under license by Iran Aircraft Manufacturing Industrial Company (HESA) in Iran as the IrAn-140. Assembly in Kazakhstan has also been discussed in tri-partite discussions between the Kazakh government, Ukraine and Russia.[5]

     

    An identical-in-appearance airplane with the same name is also manufactured by Aviakor in Samara, Russia. Since Ukraine is no longer cooperating with Russia in aircraft production, the Aviakor version of the An-140 is manufactured entirely with Russian components. The P&W Canada engine option is not offered.

     

    For further information on variants, click here.

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    an140UR-NTP.jpg_thumb.64ca56ac6403a9533f0134667260ee94.jpg

    Specifications

    Seats:
    Crew: 2 Capacity: 52 pax / 6,000 kg (13,228 lb) max payload
    Length:
    22.605 m (74 ft 2 in)
    Wingspan:
    24.505 m (80 ft 5 in)
    Height:
    8.225 m (27 ft 0 in)
    Wing Area:
    51 m2 (550 sq ft)
    Empty Weight:
    12,810 kg (28,241 lb)
    MTOW:
    19,150 kg (42,219 lb)
    Fuel Capacity:
    4,370 kg (9,634 lb)
    Powerplant:
    2 × Motor-Sich AI-30 series 1 turboprop engines, 1,838 kW (2,465 hp) each (licence-built Klimov TV3-117VMA-SBM1)
    Cruise Speed:
    Cruise speed: 575 km/h (357 mph, 310 kn) at 7,200–7,500 m (23,622–24,606 ft) max
    Range:
    900 km (560 mi, 490 nmi) with 6,000 kg (13,228 lb) payload at econ. cruise; 3,700 km (2,300 mi; 2,000 nmi) with 33 pax
    Rate of Climb:
    6.83 m/s (1,344 ft/min)
    Service Ceiling:
    7,600 m (24,900 ft)

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