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The Continental IO-360 is a family of fuel-injected air-cooled, horizontally opposed six-cylinder aircraft engines manufactured by Continental Motors in the United States of America, now part of AVIC International since 2010.
Same as the IO-360-A1B but it is equipped with an inverted oil system kit for aerobatic flight. [4] AEIO-360-A1B6 200 hp (149 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.70:1. Same as the IO-360-A1B6 but it is equipped with an inverted oil system kit for aerobatic flight. [4] AEIO-360-A1C
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).
Continental IO-346; Continental IO-360; Continental IO-370; Continental IO-550; J. Teledyne CAE J69; Teledyne CAE J402; Teledyne CAE J700; O. Continental O-170 ...
[citation needed] Other variants were introduced including the Rocket which is powered by a 210 hp (157 kW) Continental IO-360-A engine, a deluxe Franklin-powered M-4 Astro-Rocket and a Franklin-powered Rocket which is known as the M-4 Strata-Rocket. A STOL variant of the Strata Rocket was developed as the Maule M-5 Lunar Rocket.
180C with a 210-horsepower (157 kW) Continental IO-360-D engine in a revised cowling, 206 built. M-5-210TC Lunar Rocket 210C fitted with a turbocharged 210-horsepower (157 kW) Lycoming TO-360 engine, 10 built. M-5-220C Lunar Rocket 210C fitted with a 220-horsepower (164 kW) Franklin 6A-350-C1 engine, 57 built. M-5-235C Lunar Rocket
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Engines available as kits from the manufacturer for all models are the Lycoming IO-360 of 180 to 200 hp (134 to 149 kW), Lycoming IO-540 of 260 to 300 hp (194 to 224 kW), Continental IO-550 of 310 to 350 hp (231 to 261 kW) and the Franklin 6A350C1 of 205 to 235 hp (153 to 175 kW).