| Continental IO-360 ✕ | |
|---|---|
| Aircraft Engine Manufacturer | Continental |
| Aircraft Engine Type | Piston |
| Dry Weight (kg) | 133.3562 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Continental_IO-360 |
| Fuel | minimum 100LL Avgas |
| Cylinders | 6 |
| Cylinders Disposition | horizontally opposed |
| Bore (mm) | 112 |
| Stroke (mm) | 98 |
| Displacement (L) | 5.9 |
| Compression Ratio | 8.5 |
| Maximum Takeoff Power (kW) | 145.4115 |
| Power To Weight (kW/kg) | 1.167 |