The Superior Air Parts Vantage is a

type certified A type certificate signifies the airworthiness of a particular category of aircraft, according to its manufacturing design (''type design''). It confirms that the aircraft of a new type intended for serial production, is in compliance with applica ...

piston aircraft engine developed by

Superior Air Parts Superior Air Parts, Inc. is a Chinese-owned manufacturer of aviation piston engine replacement parts, headquartered in Coppell, Texas, United States. The company has been owned by Superior Aviation Beijing since 2010. History Superior Air Pa ...

of Coppell, Texas,

United States The United States of America (U.S.A. or USA), commonly known as the United States (U.S. or US) or America, is a country primarily located in North America. It consists of 50 states, a federal district, five major unincorporated territori ...

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. Vantage is a marketing name. 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 Beijing E-Town is an economic development agency of the Beijing municipal government that traces its origins to 1994 when the Beijing government chartered an entity to help foster high tech manufacturing in Beijing. E-Town supports high-tech ...

, an economic development agency of the municipal government of

Beijing } Beijing ( ; ; ), alternatively romanized as Peking ( ), is the capital of the People's Republic of China. It is the center of power and development of the country. Beijing is the world's most populous national capital city, with over 21 ...

Development

The Vantage engine is a development of the XP-360 experimental engine that was put through the US

Federal Aviation Administration The Federal Aviation Administration (FAA) is the largest transportation agency of the U.S. government and regulates all aspects of civil aviation in the country as well as over surrounding international waters. Its powers include air traffic ...

engine

type certification A type certificate signifies the airworthiness of a particular category of aircraft, according to its manufacturing design (''type design''). It confirms that the aircraft of a new type intended for serial production, is in compliance with applic ...

process starting in 1996. Certification was based on FAR 33 through amendment 20, effective 13 December 2000, application 17 July 2001 and certification was achieved on 31 March 2004. The initial

time between overhaul Time between overhauls (abbreviated as TBO or TBOH) is the manufacturer's recommended number of running hours or calendar time before an aircraft engine or other component requires overhaul. On rotorcraft, many components have recommended or ma ...

s was set at 1,000 hours, with an aim of expanding that to 2,000 hours.

Design

The engine is a four-cylinder, horizontally opposed, four-stroke, displacement, air-cooled, direct-drive, gasoline engine design. It produces , depending on the model. It is available in carburetor-equipped and

fuel injected Fuel injection is the introduction of fuel in an internal combustion engine, most commonly automotive engines, by the means of an injector. This article focuses on fuel injection in reciprocating piston and Wankel rotary engines. All comp ...

versions.

Variants

O-360

180 hp models

;O-360-A1A2 :Carburetor-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 1 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and a basic dry weight of . ;O-360-A2A2 :Carburetor-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 2 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and a basic dry weight of . ;O-360-A3A2 :Carburetor-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a conical style engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;O-360-A4A2 :Carburetor-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 1 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;O-360-A5A2 :Carburetor-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 2 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;O-360-A6A2 :Carburetor-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a conical engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;O-360-B1A2 :Carburetor-equipped model with a thin wall front main bearing journal crankshaft, for a constant speed propeller, and a number 1 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;O-360-B2A2 :Carburetor-equipped model with a thin wall front main bearing journal crankshaft, for a constant speed propeller, and a number 2 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;O-360-B3A2 :Carburetor-equipped model with a thin wall front main bearing journal crankshaft, for a constant speedh propeller, and a conical style engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;O-360-B4A2 :Carburetor-equipped model with a thin wall front main bearing journal crankshaft, for a constant speed propeller, and a number 1 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;O-360-B5A2 :Carburetor-equipped model with a thin wall front main bearing journal crankshaft, for a constant speed propeller, and a number 2 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;O-360-B6A2 :Carburetor-equipped model with a thin wall front main bearing journal crankshaft, for a constant speed propeller, and a conical engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;O-360-C1A2 :Carburetor-equipped model with a heavy wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 1 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;O-360-C2A2 :Carburetor-equipped model with a heavy wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 2 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;O-360-C3A2 :Carburetor-equipped model with a heavy wall front main bearing journal crankshaft, for a fixed pitch propeller, and a conical style engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;O-360-C4A2 :Carburetor-equipped model with a heavy wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 1 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;O-360-C5A2 :Carburetor-equipped model with a heavy wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 2 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;O-360-C6A2 :Carburetor-equipped model with a heavy wall front main bearing journal crankshaft, for a fixed pitch propeller, and a conical engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;O-360-D1A2 :Carburetor-equipped model with a heavy wall front main bearing journal crankshaft, for a constant speed propeller, and a number 1 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;O-360-D2A2 :Carburetor-equipped model with a heavy wall front main bearing journal crankshaft, for a constant speed propeller, and a number 2 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;O-360-D3A2 :Carburetor-equipped model with a heavy wall front main bearing journal crankshaft, for a constant speed propeller, and a conical style engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;O-360-D4A2 :Carburetor-equipped model with a heavy wall front main bearing journal crankshaft, for a constant speed propeller, and a number 1 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;O-360-D5A2 :Carburetor-equipped model with a heavy wall front main bearing journal crankshaft, for a constant speed propeller, and a number 2 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;O-360-D6A2 :Carburetor-equipped model with a heavy wall front main bearing journal crankshaft, for a constant speed propeller, and a conical engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;O-360-E1A2 :Carburetor-equipped model with a solid front main bearing journal crankshaft, for a fixed pitch propeller, and a number 1 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;O-360-E2A2 :Carburetor-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 2 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;O-360-E3A2 :Carburetor-equipped model with a solid front main bearing journal crankshaft, for a fixed pitch propeller, and a conical style engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;O-360-E4A2 :Carburetor-equipped model with a solid front main bearing journal crankshaft, for a fixed pitch propeller, and a number 1 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;O-360-E5A2 :Carburetor-equipped model with a solid front main bearing journal crankshaft, for a fixed pitch propeller, and a number 2 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;O-360-E6A2 :Carburetor-equipped model with a solid front main bearing journal crankshaft, for a fixed pitch propeller, and a conical engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of .

168 hp models

;O-360-A1A1 :Carburetor-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 1 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and a basic dry weight of . ;O-360-A2A1 :Carburetor-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 2 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and a basic dry weight of . ;O-360-A3A1 :Carburetor-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a conical style engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;O-360-A4A1 :Carburetor-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 1 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;O-360-A5A1 :Carburetor-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 2 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;O-360-B1A1 :Carburetor-equipped model with a thin wall front main bearing journal crankshaft, for a constant speed propeller, and a number 1 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;O-360-B2A1 :Carburetor-equipped model with a thin wall front main bearing journal crankshaft, for a constant speed propeller, and a number 2 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;O-360-B3A1 :Carburetor-equipped model with a thin wall front main bearing journal crankshaft, for a constant speedh propeller, and a conical style engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;O-360-B4A1 :Carburetor-equipped model with a thin wall front main bearing journal crankshaft, for a constant speed propeller, and a number 1 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;O-360-B5A1 :Carburetor-equipped model with a thin wall front main bearing journal crankshaft, for a constant speed propeller, and a number 2 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;O-360-B6A1 :Carburetor-equipped model with a thin wall front main bearing journal crankshaft, for a constant speed propeller, and a conical engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;O-360-C1A1 :Carburetor-equipped model with a heavy wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 1 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;O-360-C2A1 :Carburetor-equipped model with a heavy wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 2 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;O-360-C3A1 :Carburetor-equipped model with a heavy wall front main bearing journal crankshaft, for a fixed pitch propeller, and a conical style engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;O-360-C4A1 :Carburetor-equipped model with a heavy wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 1 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;O-360-C5A1 :Carburetor-equipped model with a heavy wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 2 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;O-360-C6A1 :Carburetor-equipped model with a heavy wall front main bearing journal crankshaft, for a fixed pitch propeller, and a conical engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;O-360-D1A1 :Carburetor-equipped model with a heavy wall front main bearing journal crankshaft, for a constant speed propeller, and a number 1 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;O-360-D2A1 :Carburetor-equipped model with a heavy wall front main bearing journal crankshaft, for a constant speed propeller, and a number 2 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;O-360-D3A1 :Carburetor-equipped model with a heavy wall front main bearing journal crankshaft, for a constant speed propeller, and a conical style engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;O-360-D4A1 :Carburetor-equipped model with a heavy wall front main bearing journal crankshaft, for a constant speed propeller, and a number 1 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;O-360-D5A1 :Carburetor-equipped model with a heavy wall front main bearing journal crankshaft, for a constant speed propeller, and a number 2 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;O-360-D6A1 :Carburetor-equipped model with a heavy wall front main bearing journal crankshaft, for a constant speed propeller, and a conical engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;O-360-E1A1 :Carburetor-equipped model with a solid front main bearing journal crankshaft, for a fixed pitch propeller, and a number 1 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;O-360-E2A1 :Carburetor-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 2 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;O-360-E3A1 :Carburetor-equipped model with a solid front main bearing journal crankshaft, for a fixed pitch propeller, and a conical style engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;O-360-E4A1 :Carburetor-equipped model with a solid front main bearing journal crankshaft, for a fixed pitch propeller, and a number 1 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;O-360-E5A1 :Carburetor-equipped model with a solid front main bearing journal crankshaft, for a fixed pitch propeller, and a number 2 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;O-360-E6A1 :Carburetor-equipped model with a solid front main bearing journal crankshaft, for a fixed pitch propeller, and a conical engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of .

IO-360

180 hp models

;IO-360-A1A2 :Fuel injection-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 1 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and a basic dry weight of . ;IO-360-A2A2 :Fuel injection-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 2 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and a basic dry weight of . ;IO-360-A3A2 :Fuel injection-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a conical style engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;IO-360-A4A2 :Fuel injection-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 1 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;IO-360-A5A2 :Fuel injection-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 2 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;IO-360-A6A2 :Fuel injection-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a conical engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;IO-360-B1A2 :Fuel injection-equipped model with a thin wall front main bearing journal crankshaft, for a constant speed propeller, and a number 1 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;IO-360-B2A2 :Fuel injection-equipped model with a thin wall front main bearing journal crankshaft, for a constant speed propeller, and a number 2 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;IO-360-B3A2 :Fuel injection-equipped model with a thin wall front main bearing journal crankshaft, for a constant speedh propeller, and a conical style engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;IO-360-B4A2 :Fuel injection-equipped model with a thin wall front main bearing journal crankshaft, for a constant speed propeller, and a number 1 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;IO-360-B5A2 :Fuel injection-equipped model with a thin wall front main bearing journal crankshaft, for a constant speed propeller, and a number 2 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;IO-360-B6A2 :Fuel injection-equipped model with a thin wall front main bearing journal crankshaft, for a constant speed propeller, and a conical engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;IO-360-C1A2 :Fuel injection-equipped model with a heavy wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 1 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;IO-360-C2A2 :Fuel injection-equipped model with a heavy wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 2 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;IO-360-C3A2 :Fuel injection-equipped model with a heavy wall front main bearing journal crankshaft, for a fixed pitch propeller, and a conical style engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;IO-360-C4A2 :Fuel injection-equipped model with a heavy wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 1 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;IO-360-C5A2 :Fuel injection-equipped model with a heavy wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 2 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;IO-360-C6A2 :Fuel injection-equipped model with a heavy wall front main bearing journal crankshaft, for a fixed pitch propeller, and a conical engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;IO-360-D1A2 :Fuel injection-equipped model with a heavy wall front main bearing journal crankshaft, for a constant speed propeller, and a number 1 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;IO-360-D2A2 :Fuel injection-equipped model with a heavy wall front main bearing journal crankshaft, for a constant speed propeller, and a number 2 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;IO-360-D3A2 :Fuel injection-equipped model with a heavy wall front main bearing journal crankshaft, for a constant speed propeller, and a conical style engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;IO-360-D4A2 :Fuel injection-equipped model with a heavy wall front main bearing journal crankshaft, for a constant speed propeller, and a number 1 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;IO-360-D5A2 :Fuel injection-equipped model with a heavy wall front main bearing journal crankshaft, for a constant speed propeller, and a number 2 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;IO-360-D6A2 :Fuel injection-equipped model with a heavy wall front main bearing journal crankshaft, for a constant speed propeller, and a conical engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;IO-360-E1A2 :Fuel injection-equipped model with a solid front main bearing journal crankshaft, for a fixed pitch propeller, and a number 1 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;IO-360-E2A2 :Fuel injection-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 2 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;IO-360-E3A2 :Fuel injection-equipped model with a solid front main bearing journal crankshaft, for a fixed pitch propeller, and a conical style engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;IO-360-E4A2 :Fuel injection-equipped model with a solid front main bearing journal crankshaft, for a fixed pitch propeller, and a number 1 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;IO-360-E5A2 :Fuel injection-equipped model with a solid front main bearing journal crankshaft, for a fixed pitch propeller, and a number 2 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of . ;IO-360-E6A2 :Fuel injection-equipped model with a solid front main bearing journal crankshaft, for a fixed pitch propeller, and a conical engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of .

168 hp models

;IO-360-A1A1 :Fuel injection-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 1 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and a basic dry weight of . ;IO-360-A2A1 :Fuel injection-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 2 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and a basic dry weight of . ;IO-360-A3A1 :Fuel injection-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a conical style engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;IO-360-A4A1 :Fuel injection-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 1 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;IO-360-A5A1 :Fuel injection-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 2 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;IO-360-A6A1 :Fuel injection-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a conical engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;IO-360-B1A1 :Fuel injection-equipped model with a thin wall front main bearing journal crankshaft, for a constant speed propeller, and a number 1 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;IO-360-B2A1 :Fuel injection-equipped model with a thin wall front main bearing journal crankshaft, for a constant speed propeller, and a number 2 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;IO-360-B3A1 :Fuel injection-equipped model with a thin wall front main bearing journal crankshaft, for a constant speedh propeller, and a conical style engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;IO-360-B4A1 :Fuel injection-equipped model with a thin wall front main bearing journal crankshaft, for a constant speed propeller, and a number 1 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;IO-360-B5A1 :Fuel injection-equipped model with a thin wall front main bearing journal crankshaft, for a constant speed propeller, and a number 2 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;IO-360-B6A1 :Fuel injection-equipped model with a thin wall front main bearing journal crankshaft, for a constant speed propeller, and a conical engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;IO-360-C1A1 :Fuel injection-equipped model with a heavy wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 1 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;IO-360-C2A1 :Fuel injection-equipped model with a heavy wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 2 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;IO-360-C3A1 :Fuel injection-equipped model with a heavy wall front main bearing journal crankshaft, for a fixed pitch propeller, and a conical style engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;IO-360-C4A1 :Fuel injection-equipped model with a heavy wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 1 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;IO-360-C5A1 :Fuel injection-equipped model with a heavy wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 2 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;IO-360-C6A1 :Fuel injection-equipped model with a heavy wall front main bearing journal crankshaft, for a fixed pitch propeller, and a conical engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;IO-360-D1A1 :Fuel injection-equipped model with a heavy wall front main bearing journal crankshaft, for a constant speed propeller, and a number 1 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;IO-360-D2A1 :Fuel injection-equipped model with a heavy wall front main bearing journal crankshaft, for a constant speed propeller, and a number 2 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;IO-360-D3A1 :Fuel injection-equipped model with a heavy wall front main bearing journal crankshaft, for a constant speed propeller, and a conical style engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;IO-360-D4A1 :Fuel injection-equipped model with a heavy wall front main bearing journal crankshaft, for a constant speed propeller, and a number 1 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;IO-360-D5A1 :Fuel injection-equipped model with a heavy wall front main bearing journal crankshaft, for a constant speed propeller, and a number 2 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;IO-360-D6A1 :Fuel injection-equipped model with a heavy wall front main bearing journal crankshaft, for a constant speed propeller, and a conical engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;IO-360-E1A1 :Fuel injection-equipped model with a solid front main bearing journal crankshaft, for a fixed pitch propeller, and a number 1 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;IO-360-E2A1 :Fuel injection-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a number 2 style dynafocal engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;IO-360-E3A1 :Fuel injection-equipped model with a solid front main bearing journal crankshaft, for a fixed pitch propeller, and a conical style engine mount for a rear propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;IO-360-E4A1 :Fuel injection-equipped model with a solid front main bearing journal crankshaft, for a fixed pitch propeller, and a number 1 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;IO-360-E5A1 :Fuel injection-equipped model with a solid front main bearing journal crankshaft, for a fixed pitch propeller, and a number 2 style dynafocal engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of . ;IO-360-E6A1 :Fuel injection-equipped model with a solid front main bearing journal crankshaft, for a fixed pitch propeller, and a conical engine mount for a front propeller governor, that produces at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of .

Applications

Cessna 172 The Cessna 172 Skyhawk is an American four-seat, single-engine, high wing, fixed-wing aircraft made by the Cessna Aircraft Company.Boxer engines 2000s aircraft piston engines Air-cooled aircraft piston engines Superior Air Parts engines