Do you have a question about the Textron Lycoming O-235-C and is the answer not in the manual?
Bore | 4.375 in (111.1 mm) |
---|---|
Stroke | 3.875 in (98.4 mm) |
Compression Ratio | 8.5:1 |
Fuel Type | Avgas 100LL |
Fuel system | Carburetor |
Cooling system | Air-cooled |
Type | Four-cylinder, horizontally opposed |
Displacement | 3.85 L (235 cu in) |