| Aircraft Engine Manufacturer |
Rotax |
| Aircraft Engine Type |
Piston |
| Dry Weight (kg) |
60 |
| Length (mm) |
56.1 |
| Width (mm) |
57.6 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Rotax_912 |
| Fuel |
Unleaded: 87 octane AKI (Canada/USA) / 90 octane RON (European) or higher. Leaded fuel and AVGAS 100 LL can be used but… |
| Oil System |
Dry sump with trochoid pump, camshaft driven |
| Cylinders |
4 |
| Cylinders Disposition |
opposed |
| Bore (mm) |
79.5 |
| Stroke (mm) |
61 |
| Compression Ratio |
9 |
| Valvetrain |
OHV, hydraulic lifters, pushrods, rocker arms |
| Cooling |
Liquid-cooled cylinder heads, air-cooled cylinders |
| Maximum Takeoff Power (kW) |
59.6 |
| Specific Fuel Consumption (g/(kW·h)) |
285 |