| SPA 6A ✕ | |
|---|---|
| Aircraft Engine Type | Piston |
| Dry Weight (kg) | 255 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/SPA_6A |
| Fuel System | Twin Zenith carburettors or one Duplex Zenith type 55-DC carburettor |
| Oil System | Dry-sump |
| Cylinders | 6 |
| Cylinders Disposition | Inline |
| Bore (mm) | 135 |
| Stroke (mm) | 170 |
| Displacement (L) | 14.5665 |
| Compression Ratio | 5.2 |
| Valvetrain | SOHC, two valves per cylinder |
| Cooling | Water-cooled |
| Maximum Takeoff Power (kW) | 111.855 |
| Power To Weight (kW/kg) | 0.439 |
| Specific Fuel Consumption (g/(kW·h)) | 0.288 |