Search results
Results from the WOW.Com Content Network
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
Lycoming IO-720 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).
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 ...
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 design is officially designated the Superior Air Parts O-360 and IO-360. Vantage is a marketing name. [1] [2] The company is owned by the Chinese company Superior Aviation Beijing, which is 60% owned by Chairman Cheng Shenzong and 40% owned by Beijing E-Town, an economic development agency of the municipal government of Beijing.
The IO-390 was developed from the similar IO-360 engine, by using cylinders from the IO-580 [citation needed] to increase the O-360's cylinder bore. (Although the IO-390 cylinder assembly [4] is not the same part number as the IO-580, [5] the cylinder barrels of both have a 5.318 bore and 4.375 stroke dimension.)
The type certification for the P.68 Victor, a twin piston engine, high wing monoplane with fixed tricycle landing gear was applied for on 22 January 1969. [2] The Partenavia P.68 was designed as a six-seat light transport and trainer powered by two 200 hp (149 kW) Lycoming IO-360 engines, it made its first flight on 25 May 1970 at Naples. [1]
Lycoming IO-390; Lycoming IO-580; Lycoming IO-720; L. Lycoming LTS101; ... List of Lycoming O-360 variants; Lycoming O-435; Lycoming O-480; Lycoming O-540; Lycoming O ...