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  2. Time between overhauls - Wikipedia

    en.wikipedia.org/wiki/Time_between_overhauls

    Time between overhauls (abbreviated as TBO or TBOH) is the manufacturer's recommended number of running hours or calendar time before an aircraft engine or other component requires overhaul. [ 1 ] On rotorcraft , many components have recommended or mandatory TBOs, including main rotor blades , tail rotor blades and gearboxes .

  3. Lycoming O-320 - Wikipedia

    en.wikipedia.org/wiki/Lycoming_O-320

    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.

  4. Lycoming TIO-541 - Wikipedia

    en.wikipedia.org/wiki/Lycoming_TIO-541

    The Lycoming TIO-541 engine is a turbocharged, fuel-injected, horizontally opposed, six-cylinder aircraft engine featuring three cylinders per side, manufactured by Lycoming Engines. [ 1 ] [ 2 ] The TIO-541 family of engines includes the TIGO-541 turbocharged, fuel-injected, geared, horizontally opposed engine.

  5. 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.

  6. 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).

  7. Engineered Propulsion Systems Graflight V-8 - Wikipedia

    en.wikipedia.org/wiki/Engineered_Propulsion...

    The design is a 320–450 hp (240–340 kW), 4.3-liter engine with steel pistons, connecting rods, and crankcase to improve reliability. At 650 lb (290 kg), it weighs 40 to 50 lb (18 to 23 kg) more than a conventional aircraft engine, not including the 30 lb (14 kg) radiator for cooling.

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