Basic technical information: | |
---|---|
Construction | 2 cylinder V2/90° |
Continuous power | 35 hp at 4 640 rpm |
Dry weight | 34,6 kg |
Cooling | air |
Reduction gear unit | 1:1.77 |
TBO | 1500 h |
Propeller RPM | 2 620 1/min |
Fuel supply | electronic multipoint fuel injection |
VAXELL Aircraft engines
Basic technical information: | |
---|---|
Construction | 2 cylinder V2/90° |
Continuous power | 35 hp at 4 640 rpm |
Dry weight | 34,6 kg |
Cooling | air |
Reduction gear unit | 1:1.77 |
TBO | 1500 h |
Propeller RPM | 2 620 1/min |
Fuel supply | electronic multipoint fuel injection |