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The 110-horsepower (82 kW) IOL-200, also referred to as the Voyager 200, was the rear engine and—unlike the forward engine, another modified engine, a Continental O-240 —ran throughout the entire nine-day flight save for a four-minute shutdown due to a fuel problem.
In the 1930s, Lycoming made a number of attempts to develop successful high-power aircraft engines. The 1 200 hp (895 kW) O-1230 was Lycoming's attempt to produce an engine based on the United States Army Air Corps hyper engine concept, and used a variety of features to produce nearly 1 hp/in 3 (46 kW/L) of engine displacement.
200 hp (149 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.70:1. Same as the A1A but with impulse coupling magnetos. [4] IO-360-A1B6 200 hp (149 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.70:1. Same as the A1B but with a crankshaft that has one 6.3 order and one 8th order counterweights.
The aircraft's recommended engine power is 100 to 180 hp (75 to 134 kW) and standard engines used include the 100 hp (75 kW) Continental O-200, the 180 hp (134 kW) Lycoming O-360 and the 180 hp (134 kW) ECi CC340 four-stroke powerplant. Construction time from the supplied kit ranges from 700 to 1100 hours (Depending on builder experience).
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.
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).
Lancair 200 Model first flown in 1984, powered by a 100 hp (75 kW) Continental O-200 engine. Overall length is 19.75 ft (6.02 m). [3] Lancair 235 Model introduced in 1985, powered by a 100 to 115 hp (75 to 86 kW) Lycoming O-235 engine. Overall length is 20.00 ft (6.10 m), slightly longer than the 200, due to the engine and mount dimensions. [3] [2]
In the late 1950s Piper began designing a two-seated (side-by-side) low-wing monoplane trainer built of fiberglass reinforced plastic construction. [1] Originally intended to be powered by a 100 hp (75 kW) Continental O-200 piston engine, the prototype instead used a 108 hp (81 kW) Lycoming O-235-CIB piston engine. [1]