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The Superior Air Parts Vantage is a type certified piston aircraft engine developed by Superior Air Parts of Coppell, Texas, United States and based upon the non-certified Superior Air Parts XP-360. The design is officially designated the Superior Air Parts O-360 and IO-360 .
The Superior Air Parts XP-360 is an aircraft engine, designed and produced by Superior Air Parts of Coppell, Texas, United States for use in homebuilt aircraft. [1]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.
A line of diesel engines is under development, including the 100 hp (75 kW) Gemini Diesel 100 and 125 hp (93 kW) Gemini Diesel 125. [13] The XP-360 was developed into a certified engine design, the Superior O-360, marketed as the Vantage and certified in 2004. [14] [15]
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).
In January 2009 the base price of the IO-390-EXP version was USD$32,650.00. [7] In November 2009 Lycoming announced that it had obtained an FAA Supplemental Type Certificate to replace the originally fitted Lycoming O-360 engines in the Mooney M20E, M20F and M20J with a new or remanufactured IO-390-A3A6 engine. [8]
Standard engines available are the 180 hp (134 kW) Lycoming O-360-C4P or O-360-C1G and the 180 hp (134 kW) Superior O-360-A3A2 four-stroke powerplants. [1] [3] The aircraft can be flown on wheels, tundra tires, skis or amphibious floats. Belly pods are available to increase cargo and fuel capacity. [1]
O-360-A1P 180 hp (134 kW) at 2700 rpm, Minimum fuel grade 91/96 avgas, compression ratio 8.50:1. Same as the C1G except that it has dynafocal engine mounts. [1] [2] O-360-A2A 180 hp (134 kW) at 2700 rpm, Minimum fuel grade 91/96 avgas, compression ratio 8.50:1. Same as the A1A except that it has no provisions for a controllable-pitch propeller ...
The engine is available in both naturally aspirated, fuel injected IO-360 models and turbocharged TSIO-360 versions. It is also available in both left and right hand rotation versions for use on twin-engined aircraft. [3] There was no carbureted version of this engine, which would have been designation O-360, therefore the base model is the IO ...
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