title description price download
Mi-171 2007 release year The modification of the Mi-8AMT (MI-171), rotor diameter, m - 21.29, diameter tail rotor, m 3.91, Length, m - 18.17, Height, m ​​- 5.65, Weight, kg:.... Empty - 6800.. normal takeoff - 11100., maximum take-off - 12,000, engine Type - 2 TBG Klimov TV2-117VM (VC-2500) Power, kW -. 2 x 1641 (2014), maximum speed, km / h -. 250. , Cruising speed, km / h - 225, Practical range, km: normal - 610, with two fuel tanks - 1065., ceiling, m - 5000, Static ceiling, m - 3900, crew - 3 ., Payload: up to 26 passengers or 37 paratroopers or 12 stretchers with accompanying or 4000 kg of cargo in the cab or 4000 kg per hanger. 8 800 000 $
Mi-171E 2016 release year Maximum takeoff mass of (category A): 12000 kg., Maximum takeoff weight (category B): 13000 kg. Normal takeoff weight: 11,100 kg., Dimensions of cargo cabin: - Length: 5.34 M, - width: 2 . 34 m - height: 1,8 m., - effective area: 12.5 sq. . M, - the useful volume of 23 cubic meters. m Practical flight ceiling (Category A). 5000m Practical flight ceiling (Category B): 6000 m Flight range at the maximum take-off weight (with emergency reserve of fuel for 30 minutes) to the main fuel tanks: 610 km with two additional fuel tanks : 1,065 km maximum flight speed: 250 km / h, the speed of climb: -. at normal takeoff weight:.. 10.4 m / s, - with a maximum take-off weight: 7.2 m / s, helicopter is equipped with two engines TV3 117VM takeoff power 2200 h Available: 4 num. 11 900 000 $