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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 Cessna 177B Cardinal uses a Lycoming O-360-A1F6D of 180 hp (130 kW). O-360-A1F6D 180 hp (134 kW) at 2700 rpm, Minimum fuel grade 91/96 avgas, compression ratio 8.50:1. Same as the A1F6 except that it is equipped with one Bendix D4LN-2021 impulse coupling dual magneto instead of incorporating two single magneto. [1] [2] O-360-A1G
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.
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 standard engine available is the 180 hp (134 kW) Lycoming O-360-C1 (CC363i) four-stroke powerplant, driving a Hartzell Trailblazer composite, constant speed propeller. In July 2019 a 215 hp (160 kW) version powered by a Lycoming IO-390 (CC393i) engine and a Hartzell Pathfinder three-bladed propeller was introduced as the CC19-215. [7]
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.
Later production Seminoles were built with Lycoming O-360-A1H6 engines. [5] The PA-44-180T Turbo Seminole version was certified on November 29, 1979. It features two turbocharged 180 hp (135 kW) Lycoming TO-360-E1A6D engines, which offer a significant improvement in performance at high density altitude. The Turbo Seminole had its takeoff gross ...
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.