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The Lycoming O-360 is a family of four-cylinder, direct-drive, horizontally opposed, air-cooled, piston aircraft engines. Engines in the O-360 series produce between 145 and 225 hp (110 and 170 kW), with the basic O-360 producing 180 hp (130 kW).
O-360-A1A 180 hp (134 kW) at 2700 rpm, Minimum fuel grade 91/96 avgas, compression ratio 8.50:1.The base model. A four-cylinder, horizontally opposed, air-cooled, direct-drive engine which includes provisions for supplying oil through the propeller shaft for installation of a single-acting controllable-pitch propeller.
The company manufactures replacement parts for Lycoming and Continental aircraft engines. The cylinder assemblies use newer cylinder head alloys and fully hardened cylinder liners. [1] Most of the company's production is outsourced, with Superior ensuring that the parts meet their engineering and testing standards. [2]
By 1961, Lycoming produced 600 to 700 engines per month. [17] Its most successful post-war products were a series of air-cooled flat-4 and flat-6 general aviation engines. Most famous among these are the O-320 and O-360 four-cylinder engines, and the O-540 six-cylinder engine.
O-360-A4A2 Carburetor-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 1 style dynafocal engine mount for a front propeller governor, that produces 180 hp (134 kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 291 lb (132 kg). [2] O-360-A5A2
The recommended engine is the 180 hp (134 kW) Lycoming O-360, but a variety of powerplants from 160 to 220 hp (119 to 164 kW) have been used. One installation uses two Suzuki 1600 automobile engines driving two concentric contrarotating propellers.