0 - 1000hp turboshaft MS-500V

for general aviation

The engines are intended for installation in civil purpose helicopters with takeoff mass of 3.5 to 6 t and permit to attain high economic standards in the course of commercial use. Main advantages of the engine: simple and effective design; high reliability; low specific fuel consumption; high stability of characteristics in service; compliance with current and future environmental requirements; extended service life and durable calendar life; ease and convenience of maintenance and repair; low cost of life cycle.