Designed for the use on multipurpose general aviation aircraft and unmanned aerial vehicles. Planned to be installed on the EV-55 (Czech Republic).
|Takeoff (SLS, ISA+30°C)|
|Specific fuel consumption, kg/hp/h||0.259|
|Maximum cruise ( H=3,000 m, V=407 km/h )|
|Specific fuel consumption, kg/hp/h||0.246|
|Dimensions, мм||1,120 х 578 х 700|
|Weight, dry, kg||140|