Илюшин Ил-76
Il-76MD. Monino aviation museum
The Ilyushin Il-76 (NATO reporting name: Candid) is a multi-purpose, fixed-wing, four-engine turbofan strategic airlifter designed by the Soviet Union’s Ilyushin design bureau as a commercial freighter in 1967, to replace the Antonov An-12. It was developed to deliver heavy machinery to remote, poorly served areas. Military versions of the Il-76 have been widely used in Europe, Asia and Africa, including use as an aerial refueling tanker or command center.
The Il-76 has seen extensive service as a commercial freighter for ramp-delivered cargo, especially for outsized or heavy items unable to be otherwise carried. It has also been used as an emergency response transport for civilian evacuations as well as for humanitarian aid and disaster relief around the world. Due to its ability to operate from unpaved runways, it has been useful in undeveloped areas. Specialized models have also been produced for aerial firefighting and zero-G training.
Il-76TD-90VD “Volga-Dnepr” (RA-76950). Vnukovo airport (Moscow, Russia)
The aircraft was conceived by Ilyushin in 1967 to meet a requirement for a freighter able to carry a payload of 40 tonnes (88,000 lb) over a range of 5,000 kilometres (2,700 nmi; 3,100 mi) in less than six hours, able to operate from short and unprepared airstrips, and capable of coping with the worst weather conditions likely to be experienced in Siberia and the Soviet Union’s Arctic regions. It was intended to replace the Antonov An-12. Another design was a double-decked 250-passenger airliner but that project was cancelled. The Il-76 first flew in March 1971.
Production of Il-76s was allocated to the Tashkent Aviation Production Association in Tashkent, Uzbekistan, then a republic of the Soviet Union. Some 860 of the basic transport variants were manufactured. In the 1990s, modernized variants also equipped with Soloviev D-30 turbofan engines were developed (MF, TF), with a cargo compartment 20 m (66 ft) long by 3.4 m (11 ft) wide by 3.4 m (11 ft) tall; these larger variants were not produced in significant quantity due to the financial difficulties being experienced by the Russian Air Force, which was the primary operator of the type. The prototype of the Il-76MF conducted its first flight on 1 August 1995.
Development: OKB Ilyushin (USSR)
Assembly: Aviastar-SP (Ulianovsk, USSR/Russia)
First flight: 1971
Production: 957
Crew: 5
Engine: 4 × PS-90A
Max speed: 850 km/h
Flight range: 9,400 km
Ceiling: 12,000 m
Weight: 88,5 t
Max load capacity: 60 t
