Basic technical information: | |
---|---|
Construction | 2 cylinder V2/90° |
Continuous power | 52 hp at 4 370 rpm |
Dry weight | 52.8 kg |
Cooling | air |
Reduction gear unit | 1:1.65 |
TBO | 1500 h |
Propeller RPM | 2 650 1/min |
Fuel supply | electronic multipoint fuel injection |
VAXELL Aircraft engines
Basic technical information: | |
---|---|
Construction | 2 cylinder V2/90° |
Continuous power | 52 hp at 4 370 rpm |
Dry weight | 52.8 kg |
Cooling | air |
Reduction gear unit | 1:1.65 |
TBO | 1500 h |
Propeller RPM | 2 650 1/min |
Fuel supply | electronic multipoint fuel injection |