| Rotax 532 ✕ | |
|---|---|
| Aircraft Engine Manufacturer | Rotax |
| Aircraft Engine Type | Piston |
| Dry Weight (kg) | 46.8 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Rotax_532 |
| Fuel | premium unleaded: RON 90 octane or higher leaded or unleaded or AVGAS 100 LL |
| Oil System | oil-in-fuel (pre-mix) at 50:1 |
| Cylinders | 2 |
| Cylinders Disposition | rotary |
| Bore (mm) | 72 |
| Stroke (mm) | 64 |
| Displacement (L) | 0.5213 |
| Valvetrain | rotary inlet valve, piston ported exhaust |
| Cooling | liquid cooled |
| Maximum Takeoff Power (kW) | 48 |
| Power To Weight (kW/kg) | 1.019 |