Designed for the use on light helicopters and aircraft in the take-off weight class of 1500-4000 kg. Usable as part of aircraft twin-engine and single-engine power plants.
|Takeoff (H=0 m; M=0; ISA )|
|Specific fuel consumption, kg/h/hp||0.260|
|Air flow, kg/sec||1.72|
|Specific fuel consumption, kg/h/hp||0.297|
|Weight, dry (without propfan), kg||103|
|Dimensions, mm||1,085 х 536 х 515|
|Specified service life, h||3,000|