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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).
The Beechcraft Duchess uses one 180 hp (130 kW) O-360-A1G6D on the left wing and one LO-360-A1G6D on the right wing. O-360-A1G6D 180 hp (134 kW) at 2700 rpm, Minimum fuel grade 91/96 avgas, compression ratio 8.50:1. Same as the A1G6 except that it is equipped with a Bendix D4LN-2021 magneto in place of two single magnetos. [1] [2] O-360-A1H
In March 2014 Seeker Aircraft (US), a subsidiary of the global aviation company CSI Aviation, acquired Seabird Aviation, the Australian manufacturer of the Seabird Seeker, with plans to eventually move Australia-based manufacturing operations to the United States [2] In March 2016 Seeker Aircraft (US) announced that Erickson Inc. of Portland, Oregon, would begin manufacturing the Seeker ...
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 ...
Download as PDF; Printable version; In other projects Wikidata item; Appearance. move to sidebar hide. ... List of Lycoming O-360 variants; Lycoming GSO-580; Lycoming ...
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.
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]
Replacing the prototype's truss tailboom with a simple aluminum tube as the tailboom, the 269A came with the option for several models of Lycoming O-360 engines: the carbureted O-360-C2D, restricted to 165 hp (123 kW) in the 269A, or the carbureted HO-360-B1A/B1B or fuel-injected HIO-360-B1A/B1B, all rated for 180 hp (134 kW) in the 269A.