Military Users- Law Enforcement Force of the Islamic Republic of Iran, Russian Naval Aviation, Ministry of Defence (Russia), Ministry of Defence (Ukraine)
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.
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.
An identical-in-appearance airplane with the same name is also manufactured by Aviakor in Samara, Russia.
Since the Ukraine is no longer cooperating with Russia in aircraft production, the Aviakor version of the An-140 is manufactured entirely with Russian components.
Capacity: 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)
Max takeoff weight: 19,150 kg (42,219 lb)
Maximum zero fuel weight: 17,800 kg (39,242 lb)
Maximum landing weight: 19,100 kg (42,108 lb)
Fuel capacity: 4,370 kg (9,634 lb)
Power plant: 2 × Motor-Sich AI-30 series 1 turboprop engines, 1,838 kW (2,465 hp) each (license-built Klimov TV3-117VMA-SBM1)