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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-A1G6 180 hp (134 kW) at 2700 rpm, Minimum fuel grade 91/96 avgas, compression ratio 8.50:1. Same as the A1G except has a crankshaft that is equipped with counterweights. [1] [2] 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
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.
Production version with a Lycoming O-360 A1A 180 hp (134 kW), type certified 26 July 1960. This differed from the Colonial C-2 in having four foot greater span, revised nose, doors, higher gross weight and reinforcement of the wing and wing-to-fuselage carry-through structure. [2] [3] LA-4A Shorter bow from the Colonial C-2, only two built.
The R22 HP was fitted with a 160 bhp Lycoming O-320-B2C engine, an increase of 10 bhp (7.5 kW) over the original R22. The steel-tube frame on the R22 Alpha was modified by extending the aft landing-gear mounting points, giving it a slightly nose-down attitude on the ground and better matching of the skids to the ground in a low-altitude hover ...
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.
The earlier J-5s had been powered by either a 100 hp (75 kW) Lycoming O-235 or a 75 hp (56 kW) Lycoming O-145. The newer PA-12 model was initially powered by a 108 hp (81 kW) Lycoming O-235-C engine, was fully cowled, and had a metal spar wing with two 19 gallon fuel tanks.
Prototype, first flew 29 April 1959 with two 180 hp (130 kW) Lycoming O-360-A1A engines and fixed pitch two-blade propellers ; one built. Do 28A-1 Designation of production aircraft with 250 hp (190 kW) Lycoming O-540-A1A engines and a 7 ft increase in wingspan, 60 built. First flown on 20 March 1960 at Oberpfaffenhofen.