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Mil Mi-38 is powered by two Pratt & Whitney Canada / Russia PW127TS turboshafts, with 2,500 hp (1,864 kW), equipped with FADEC (full authority digital engine control). Twin engines are installed above the main cabin.
The Mil Mi-38 is a helicopter designed by Mil. Originally intended as a replacement for the Mil Mi-8 and the Mi-17, it is being marketed in both military and civil versions. It flew for the first time on 22 December 2003.
MIL engine arrangement reduces cabin noise and improves survivability during emergency landings. Each PW127 is rated at approximately 2,500-shp at takeoff. The internal fuel tanks (3,055 kg) provide a maximum range of 885 kilometers or 1,300 kilometers with auxiliary fuel tanks.
4 cze 2024 · The Mi-38 is also fitted with modified main rotor blades and a new Tranzas "glass cockpit" avionics system. The Mi-38 will be fitted out with up-to-date integrated avionics. Five multifunctional color displays will screen flight data.
The Mil Mi-38 is a transport helicopter designed by Mil Moscow Helicopter Plant and being developed by Kazan Helicopters. Originally intended as a replacement for the Mil Mi-8 and the Mi-17, it is being marketed in both military and civil versions. [6] It flew for the first time on 22 December 2003 and was certified on 30 December 2015. [7]
Engines. The Mi-38 is powered by two Pratt & Whitney Canada / Russia PW127TS turboshaft engines, rated at 2,500hp (1,864kW), fitted with FADEC (full authority digital engine control). The twin engines are installed above the main cabin. The bladder fuel tanks are installed under the main cabin floor.
