| 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 |