| Aircraft Engine Manufacturer |
Ranger |
| Aircraft Engine Type |
Piston |
| Dry Weight (kg) |
331.1224 |
| Length (mm) |
157.48 |
| Height (mm) |
81.788 |
| Width (mm) |
71.12 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Ranger_V-770 |
| Fuel |
87 octane gasoline |
| Fuel System |
Holley non-icing carburetor |
| Oil System |
Full pressure type |
| Cylinders |
12 |
| Bore (mm) |
101.6 |
| Stroke (mm) |
130 |
| Displacement (L) |
12.6672 |
| Supercharger |
Single-speed, single-stage, produced 45 inches of mercury (1.5 bar, 22 psi) at take-off |
| Compression Ratio |
6.5 |
| Valvetrain |
Single overhead camshaft (SOHC) (1 shaft per bank), gear driven |
| Cooling |
Air-cooled |
| Maximum Takeoff Power (kW) |
387.7639 |
| Specific Power (kW/L) |
0.5071 |
| Power To Weight (kW/kg) |
1.167 |