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The Mil Mi-54 was a projected twin-turbine civil utility helicopter, first announced in 1992, intended to replace the Mi-2 and the Mi-8 helicopters. It was planned to use two 574 kW Saturn/Lyulka AL-32 turboshaft engines, four-bladed main and tail rotors, and fixed tricycle-type landing gear with one nosewheel and two rear wheels on sponsons.
Specifications
Data from
General characteristics
Crew: 2
Capacity: 10-12 passengers
Length: 13.113 m (43 ft 0 in)
Height: 4.8 m (15 ft 9 in)
Empty weight: 3,000 kg (6,614 lb)
Max takeoff weight: 4,700 kg (10,362 lb) with external cargo on the sling, 4,500 kg (9920,802 lb) with internal cargo
