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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).
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 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
The RV-4 is a new design based upon the concepts proven in the RV-3 and is not merely a stretched RV-3. The RV-4 airframe will accept a range of engines up to 180 hp (134 kW), including the Lycoming O-360. The RV-4 has a new wing, with increased wingspan and wing area over the RV-3. The RV-4 is designed for sport aerobatics.
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 ...
Data from Aviat website General characteristics Crew: one Capacity: one passenger Length: 22 ft 7 in (6.88 m) Wingspan: 35 ft 6 in (10.82 m) Wing area: 183 sq ft (17.0 m 2) Empty weight: 1,275 lb (578 kg) on wheels Gross weight: 2,200 lb (998 kg) on wheels and floats Fuel capacity: 50 US gallons (190 litres) Powerplant: 1 × Lycoming O-360-A1P four cylinder, four stroke piston aircraft engine ...
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.