| Lycoming O-540 ✕ | |
|---|---|
| Aircraft Engine Manufacturer | Lycoming |
| Aircraft Engine Type | Piston |
| Dry Weight (kg) | 198.6735 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Lycoming_O-540 |
| Fuel | 100 octane rating gasoline |
| Fuel System | Fuel injection |
| Cylinders | 6 |
| Cylinders Disposition | horizontally opposed |
| Bore (mm) | 130.175 |
| Stroke (mm) | 111 |
| Displacement (L) | 8.9 |
| Compression Ratio | 8.7 |
| Valvetrain | Two overhead valves per cylinder |
| Cooling | Air-cooled |
| Maximum Takeoff Power (kW) | 223.71 |
| Specific Power (kW/L) | 0.4101 |
| Power To Weight (kW/kg) | 0.68 |