| Aircraft Engine Manufacturer |
Warner |
| Aircraft Engine Type |
Piston |
| Dry Weight (kg) |
132.449 |
| Diameter (mm) |
92.8688 |
| Length (mm) |
73.66 |
| Height (mm) |
92.71 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Warner_Scarab |
| Fuel |
67 octane Avgas |
| Fuel System |
Stromberg NA-5SA carburetor or Holley equivalent |
| Oil System |
Dry sump |
| Cylinders |
7 |
| Cylinders Disposition |
radial |
| Bore (mm) |
107.95 |
| Stroke (mm) |
108 |
| Displacement (L) |
6.9153 |
| Compression Ratio |
5.15 |
| Valvetrain |
1 inlet and 1 exhaust valve per cylinder |
| Cooling |
Air-cooled |
| Maximum Takeoff Power (kW) |
93.2125 |
| Power To Weight (kW/kg) |
0.707 |
| Specific Fuel Consumption (g/(kW·h)) |
334.6 |