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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-G1A6 180 hp (134 kW) at 2700 rpm, Minimum fuel grade 91/96 avgas, compression ratio 8.50:1. Same as the F1A6 except that it has a machined pad on the right front of the crankcase for installation equipment. [1] [2] Robinson R22 Beta II with Lycoming O-360-J2A engine. O-360-J2A
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.
Standard engines available are the 180 hp (134 kW) Lycoming O-360-C4P or O-360-C1G and the 180 hp (134 kW) Superior O-360-A3A2 four-stroke powerplants. [1] [3] The aircraft can be flown on wheels, tundra tires, skis or amphibious floats. Belly pods are available to increase cargo and fuel capacity. [1]
Lycoming O-360 powered production variant. SB7L-360A-2 Lycoming IO-390 210 hp variant [7] SB7L-360A-3 ROAMES Short for Remote Observation Automated Modelling Economic Simulation. Two Lycoming IO-390-A1B6 powered variants built for Ergon Energy featuring upgraded avionics, Garmin G500 EFIS cockpit. The aircraft is capable of fully automated ...
The 200 was quickly replaced by the Lancair 235, equipped with the slightly more powerful Lycoming O-235. Re-engined versions quickly followed; the Lancair 320 with the 150 hp Lycoming O-320, and the Lancair 360 with the 180 hp Lycoming O-360. A new tail was introduced for the later models in order to address stability problems at low speeds ...
The base engine is a Lycoming O-360 180 hp (134 kW) engine, but alternative examples have been built using the Lycoming IO-540, Ranger, Ford V-8 and V-6, Continental, Jacobs, and even Pratt & Whitney R-985 engines. [2]
The Aiglon is an all-metal low-wing monoplane with a fixed tricycle landing gear and powered by a nose-mounted 180 hp (134 kW) Lycoming O-360-A3AD or a Lycoming O-360-A3A engine. It was based on the early HR100 but had a lighter airframe and new fin and rudder.