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IO-360-M1A 180 hp (134 kW) at 2700 rpm, Minimum fuel grade 91/96 avgas, compression ratio 8.50:1. Same as the B1E but with a front inlet fuel injector, propeller governor on front of the crankcase and a retard magneto. [2] [4] IO-360-M1B 180 hp (134 kW) at 2700 rpm, Minimum fuel grade 91/96 avgas, compression ratio 8.50:1.
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 ...
S.205 F/R-18: Avco Lycoming O-360 S.205 F/R-20: Avco Lycoming IO-360-A1A S.205 F/R-22: Franklin 6A-350C1 S.206 6-seat version, never realized S.208 5-seat version with a 260 hp engine and a retractable undercarriage S.208M military version for the Italian Air Force S.208AG agricultural version, also used as an aviation-ambulance. S.210 twin ...
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 Tango 2 is a side-by-side two-seat composite aircraft that can be flying in as little as 1000 hours of build time. Current aircraft have been built with engines ranging from the 150 HP O-320 Lycoming to the Geared Drives 205 hp EcoTech 2.2 liter supercharged Cobalt SS power package, with the most popular the 180 hp IO-360 Lycoming.
The Lycoming O-540 is a family of air-cooled six-cylinder, horizontally opposed fixed-wing aircraft and helicopter engines of 541.5 cubic inches (8.9 L) displacement, manufactured by Lycoming Engines. The engine is a six-cylinder version of the four-cylinder Lycoming O-360.
The P2010 is powered by a 135 kW (180 hp) Lycoming IO-360-M1A horizontally opposed four cylinder piston engine, with a 215 hp Lycoming IO-390 option available. [3] The cabin seats the pilot and three passengers in two side-by-side rows, accessed by three doors. Its fixed tricycle undercarriage has spring cantilever main legs and a castoring ...
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