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Lycoming IO-360-C1C6 Engine Information
First run in 1955, the Lycoming O-360 Series is a family of four-cylinder, direct drive, horizontally opposed, air-cooled, piston aircraft engines. Different variants of the O-360 produce between 145 and 225 hp. The IO-360 is a fuel injected version. The Lycoming IO-360-C1C6 produces 200 hp at 2700 rpm. The compression ratio is 8.70:1.
Variant models of the Lycoming IO-360 Series include the IO-360-A1A, IO-360-A1B, IO-360-A1B6, IO-360-A1B6D, IO-360-A1C, IO-360-A1D, IO-360-A1D6, IO-360-A1D6D, IO-360-A2A, IO-360-A2B, IO-360-A2C, IO-360-A3B6, IO-360-A3B6D, IO-360-A3D6D, IO-360-B1A, IO-360-B1B, IO-360-B1C, IO-360-B1D, IO-360-B1E, IO-360-B1F, IO-360-B1F6, IO-360-B1G6, IO-360-B2E, IO-360-B2F, IO-360-B2F6, IO-360-B4A, IO-360-C1A, IO-360-C1B, IO-360-C1C, IO-360-C1C6, IO-360-C1D6, IO-360-C1E6, IO-360-C1E6D, IO-360-C1F, IO-360-C1G6, IO-360-D1A, IO-360-E1A, IO-360-F1A, IO-360-J1AD, IO-360-J1A6D, IO-360-K2A, IO-360-L2A, IO-360-M1A, and IO-360-M1B.
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