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The Lycoming O-290 is a dual-ignition, four-cylinder, air-cooled, horizontally opposed aircraft engine.It was first run in 1939, and entered production three years later. A common variant of the type is the O-290-G, a single-ignition model which was designed to drive a generator as part of a ground power unit.
Lycoming Engines is a major American manufacturer of aircraft engines.With a factory in Williamsport, Pennsylvania, Lycoming produces a line of horizontally opposed, air-cooled, four, six and eight-cylinder engines including the only FAA-certified aerobatic and helicopter piston engines on the market.
The Lycoming O-320 is a large family of naturally aspirated, 320 cu in (5.2 L) air-cooled, horizontally-opposed four-cylinder, direct-drive engines produced by Lycoming Engines. Introduced in 1953, it is commonly used on light aircraft such as the Cessna 172 and Piper Cherokee , and remains in production as of 2024.
Variant to replace the PA-18-95 with flaps and horn-balanced elevators and a 125 hp Lycoming O-290-D piston engine and either wood or metal controllable-pitch propeller. [5] PA-18-135 Super Cub Variant with a 135 hp Lycoming O-290-D piston engine and fitted with two wing tanks as standard. [5] PA-18-150 PA-18-150 Super Cub
The Rocket 125 was a low-wing cabin monoplane powered by a Lycoming O-290 engine. [2] He developed the design into the Rocket 185 with a 185 hp (138 kW) Lycoming O-435-A engine and retractable landing gear. [3] It was a high performance aircraft for the late 1940s with a top speed of 180 mph (290 km/h).
HL-6B Cauré - Similar to HL-6A but with more powerful engine 216 kW (290 hp) Lycoming O-290C, and optional enclosed cabin. 39 units were constructed in 1944. 39 units were constructed in 1944. Specifications (HL-6B Cauré trainer)
The Lycoming O-540 is a family of air-cooled six-cylinder, horizontally opposed fixed-wing aircraft and helicopter engines of 541.5 cubic inches (8.9 L) displacement, manufactured by Lycoming Engines. The engine is a six-cylinder version of the four-cylinder Lycoming O-360.
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.