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  2. List of Lycoming O-360 variants - Wikipedia

    en.wikipedia.org/wiki/List_of_Lycoming_O-360...

    Same as the IO-360-A1B6 but it is equipped with an inverted oil system kit for aerobatic flight. [4] AEIO-360-A1C 200 hp (149 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.70:1. Same as the IO-360-A1C but it is equipped with an inverted oil system kit for aerobatic flight. [4] AEIO-360-A1D

  3. Lycoming O-360 - Wikipedia

    en.wikipedia.org/wiki/Lycoming_O-360

    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).

  4. Aircraft engine controls - Wikipedia

    en.wikipedia.org/wiki/Aircraft_engine_controls

    In adjustable-pitch propeller control system, the pilot has to adjust the propeller pitch angle and thus angle of attack of the propeller blades (typically with a lever) to achieve the desired propeller rotational speed. The increased pitch (blade angle of attack) increases the load on the engine and therefore slows it down, and vice versa.

  5. Velocity SE - Wikipedia

    en.wikipedia.org/wiki/Velocity_SE

    Powerplant: 1 × Lycoming IO-360 4-cyl. horizontally-opposed air-cooled piston engine, 200 hp (150 kW) Performance Cruise speed: 187 kn (215 mph, 346 km/h) at 75% power

  6. Lycoming IO-360-M1A - Wikipedia

    en.wikipedia.org/?title=Lycoming_IO-360-M1A&...

    This page was last edited on 6 December 2019, at 14:34 (UTC).; Text is available under the Creative Commons Attribution-ShareAlike 4.0 License; additional terms may apply.

  7. Piper PA-28 Cherokee - Wikipedia

    en.wikipedia.org/wiki/Piper_PA-28_Cherokee

    This aircraft featured a constant-speed propeller and retractable landing gear and was powered by a 180 hp (130 kW) Lycoming IO-360-B1E engine. A 200 hp (150 kW) version powered by a Lycoming IO-360-C1C was offered as an option beginning in 1969 and designated the PA-28R-200; the 180 hp (130 kW) model was dropped after 1971. [17]

  8. Continental IO-360 - Wikipedia

    en.wikipedia.org/wiki/Continental_IO-360

    Same as IO-360-A except for reduced compression ratio and rated power. The crankshaft has two 6th order dampers. [4] IO-360-C 210 hp (157 kW) at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-D except for accessory drive provisions. The crankshaft has two 6th order ...

  9. Lycoming Engines - Wikipedia

    en.wikipedia.org/wiki/Lycoming_Engines

    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.