[{"@context":"http:\/\/schema.org\/","@type":"BlogPosting","@id":"https:\/\/wiki.edu.vn\/en\/wiki40\/superior-air-parts-vantage-wikipedia\/#BlogPosting","mainEntityOfPage":"https:\/\/wiki.edu.vn\/en\/wiki40\/superior-air-parts-vantage-wikipedia\/","headline":"Superior Air Parts Vantage – Wikipedia","name":"Superior Air Parts Vantage – Wikipedia","description":"before-content-x4 From Wikipedia, the free encyclopedia after-content-x4 American\/Chinese aircraft engine The Superior Air Parts Vantage is a type certified piston","datePublished":"2015-11-05","dateModified":"2015-11-05","author":{"@type":"Person","@id":"https:\/\/wiki.edu.vn\/en\/wiki40\/author\/lordneo\/#Person","name":"lordneo","url":"https:\/\/wiki.edu.vn\/en\/wiki40\/author\/lordneo\/","image":{"@type":"ImageObject","@id":"https:\/\/secure.gravatar.com\/avatar\/c9645c498c9701c88b89b8537773dd7c?s=96&d=mm&r=g","url":"https:\/\/secure.gravatar.com\/avatar\/c9645c498c9701c88b89b8537773dd7c?s=96&d=mm&r=g","height":96,"width":96}},"publisher":{"@type":"Organization","name":"Enzyklop\u00e4die","logo":{"@type":"ImageObject","@id":"https:\/\/wiki.edu.vn\/wiki4\/wp-content\/uploads\/2023\/08\/download.jpg","url":"https:\/\/wiki.edu.vn\/wiki4\/wp-content\/uploads\/2023\/08\/download.jpg","width":600,"height":60}},"image":{"@type":"ImageObject","@id":"https:\/\/en.wikipedia.org\/wiki\/Special:CentralAutoLogin\/start?type=1x1","url":"https:\/\/en.wikipedia.org\/wiki\/Special:CentralAutoLogin\/start?type=1x1","height":"1","width":"1"},"url":"https:\/\/wiki.edu.vn\/en\/wiki40\/superior-air-parts-vantage-wikipedia\/","about":["Wiki"],"wordCount":8454,"articleBody":"     (adsbygoogle = window.adsbygoogle || []).push({});before-content-x4From Wikipedia, the free encyclopedia       (adsbygoogle = window.adsbygoogle || []).push({});after-content-x4American\/Chinese aircraft engineThe 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. Vantage is a marketing name.[1][2]       (adsbygoogle = window.adsbygoogle || []).push({});after-content-x4The 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.Table of ContentsDevelopment[edit]Variants[edit]O-360[edit]180 hp models[edit]168 hp models[edit]IO-360[edit]180 hp models[edit]168 hp models[edit]Applications[edit]Specifications (O-360-A1A2)[edit]General characteristicsComponentsPerformanceSee also[edit]References[edit]External links[edit]Development[edit]The Vantage engine is a development of the XP-360 experimental engine that was put through the US Federal Aviation Administration engine type certification 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 overhauls was set at 1,000 hours, with an aim of expanding that to 2,000 hours.[1][3][4]       (adsbygoogle = window.adsbygoogle || []).push({});after-content-x4The engine is a four-cylinder, horizontally opposed, four-stroke, 361\u00a0cu\u00a0in (5,916\u00a0cc) displacement, air-cooled, direct-drive, gasoline engine design. It produces 165 to 180\u00a0hp (123 to 134\u00a0kW), depending on the model. It is available in carburetor-equipped and fuel injected versions.[2]Variants[edit]O-360[edit]180 hp models[edit]O-360-A1A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and a basic dry weight of 288\u00a0lb (131\u00a0kg).[2]O-360-A2A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and a basic dry weight of 288\u00a0lb (131\u00a0kg).[2]O-360-A3A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 288\u00a0lb (131\u00a0kg).[2]O-360-A4A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 291\u00a0lb (132\u00a0kg).[2]O-360-A5A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 291\u00a0lb (132\u00a0kg).[2]O-360-A6A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 291\u00a0lb (132\u00a0kg).[2]O-360-B1A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 291\u00a0lb (132\u00a0kg).[2]O-360-B2A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 291\u00a0lb (132\u00a0kg).[2]O-360-B3A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 291\u00a0lb (132\u00a0kg).[2]O-360-B4A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 291\u00a0lb (132\u00a0kg).[2]O-360-B5A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 291\u00a0lb (132\u00a0kg).[2]O-360-B6A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 291\u00a0lb (132\u00a0kg).[2]O-360-C1A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 291\u00a0lb (132\u00a0kg).[2]O-360-C2A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 291\u00a0lb (132\u00a0kg).[2]O-360-C3A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 291\u00a0lb (132\u00a0kg).[2]O-360-C4A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 294\u00a0lb (133\u00a0kg).[2]O-360-C5A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 294\u00a0lb (133\u00a0kg).[2]O-360-C6A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 294\u00a0lb (133\u00a0kg).[2]O-360-D1A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 294\u00a0lb (133\u00a0kg).[2]O-360-D2A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 294\u00a0lb (133\u00a0kg).[2]O-360-D3A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 294\u00a0lb (133\u00a0kg).[2]O-360-D4A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 294\u00a0lb (133\u00a0kg).[2]O-360-D5A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 294\u00a0lb (133\u00a0kg).[2]O-360-D6A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 294\u00a0lb (133\u00a0kg).[2]O-360-E1A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 295\u00a0lb (134\u00a0kg).[2]O-360-E2A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 295\u00a0lb (134\u00a0kg).[2]O-360-E3A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 295\u00a0lb (134\u00a0kg).[2]O-360-E4A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 298\u00a0lb (135\u00a0kg).[2]O-360-E5A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 298\u00a0lb (135\u00a0kg).[2]O-360-E6A2Carburetor-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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 298\u00a0lb (135\u00a0kg).[2]168 hp models[edit]O-360-A1A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and a basic dry weight of 288\u00a0lb (131\u00a0kg).[2]O-360-A2A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and a basic dry weight of 288\u00a0lb (131\u00a0kg).[2]O-360-A3A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 288\u00a0lb (131\u00a0kg).[2]O-360-A4A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 291\u00a0lb (132\u00a0kg).[2]O-360-A5A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 291\u00a0lb (132\u00a0kg).[2]O-360-B1A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 291\u00a0lb (132\u00a0kg).[2]O-360-B2A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 291\u00a0lb (132\u00a0kg).[2]O-360-B3A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 291\u00a0lb (132\u00a0kg).[2]O-360-B4A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 291\u00a0lb (132\u00a0kg).[2]O-360-B5A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 291\u00a0lb (132\u00a0kg).[2]O-360-B6A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 291\u00a0lb (132\u00a0kg).[2]O-360-C1A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 291\u00a0lb (132\u00a0kg).[2]O-360-C2A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 291\u00a0lb (132\u00a0kg).[2]O-360-C3A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 291\u00a0lb (132\u00a0kg).[2]O-360-C4A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 294\u00a0lb (133\u00a0kg).[2]O-360-C5A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 294\u00a0lb (133\u00a0kg).[2]O-360-C6A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 294\u00a0lb (133\u00a0kg).[2]O-360-D1A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 294\u00a0lb (133\u00a0kg).[2]O-360-D2A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 294\u00a0lb (133\u00a0kg).[2]O-360-D3A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 294\u00a0lb (133\u00a0kg).[2]O-360-D4A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 294\u00a0lb (133\u00a0kg).[2]O-360-D5A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 294\u00a0lb (133\u00a0kg).[2]O-360-D6A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 294\u00a0lb (133\u00a0kg).[2]O-360-E1A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 295\u00a0lb (134\u00a0kg).[2]O-360-E2A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 295\u00a0lb (134\u00a0kg).[2]O-360-E3A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 295\u00a0lb (134\u00a0kg).[2]O-360-E4A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 298\u00a0lb (135\u00a0kg).[2]O-360-E5A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 298\u00a0lb (135\u00a0kg).[2]O-360-E6A1Carburetor-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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 298\u00a0lb (135\u00a0kg).[2]IO-360[edit]180 hp models[edit]IO-360-A1A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and a basic dry weight of 290\u00a0lb (132\u00a0kg).[2]IO-360-A2A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and a basic dry weight of 290\u00a0lb (132\u00a0kg).[2]IO-360-A3A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 290\u00a0lb (132\u00a0kg).[2]IO-360-A4A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 293\u00a0lb (133\u00a0kg).[2]IO-360-A5A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 293\u00a0lb (133\u00a0kg).[2]IO-360-A6A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 293\u00a0lb (133\u00a0kg).[2]IO-360-B1A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 293\u00a0lb (133\u00a0kg).[2]IO-360-B2A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 293\u00a0lb (133\u00a0kg).[2]IO-360-B3A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 293\u00a0lb (133\u00a0kg).[2]IO-360-B4A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 293\u00a0lb (133\u00a0kg).[2]IO-360-B5A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 293\u00a0lb (133\u00a0kg).[2]IO-360-B6A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 293\u00a0lb (133\u00a0kg).[2]IO-360-C1A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 293\u00a0lb (133\u00a0kg).[2]IO-360-C2A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 293\u00a0lb (133\u00a0kg).[2]IO-360-C3A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 293\u00a0lb (133\u00a0kg).[2]IO-360-C4A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 296\u00a0lb (134\u00a0kg).[2]IO-360-C5A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 296\u00a0lb (134\u00a0kg).[2]IO-360-C6A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 296\u00a0lb (134\u00a0kg).[2]IO-360-D1A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 296\u00a0lb (134\u00a0kg).[2]IO-360-D2A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 296\u00a0lb (134\u00a0kg).[2]IO-360-D3A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 296\u00a0lb (134\u00a0kg).[2]IO-360-D4A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 296\u00a0lb (134\u00a0kg).[2]IO-360-D5A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 296\u00a0lb (134\u00a0kg).[2]IO-360-D6A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 296\u00a0lb (134\u00a0kg).[2]IO-360-E1A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 297\u00a0lb (135\u00a0kg).[2]IO-360-E2A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 297\u00a0lb (135\u00a0kg).[2]IO-360-E3A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 297\u00a0lb (135\u00a0kg).[2]IO-360-E4A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 300\u00a0lb (140\u00a0kg).[2]IO-360-E5A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 300\u00a0lb (140\u00a0kg).[2]IO-360-E6A2Fuel 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 180\u00a0hp (134\u00a0kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 300\u00a0lb (140\u00a0kg).[2]168 hp models[edit]IO-360-A1A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and a basic dry weight of 290\u00a0lb (132\u00a0kg).[2]IO-360-A2A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and a basic dry weight of 290\u00a0lb (132\u00a0kg).[2]IO-360-A3A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 290\u00a0lb (132\u00a0kg).[2]IO-360-A4A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 293\u00a0lb (133\u00a0kg).[2]IO-360-A5A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 293\u00a0lb (133\u00a0kg).[2]IO-360-A6A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 293\u00a0lb (133\u00a0kg).[2]IO-360-B1A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 293\u00a0lb (133\u00a0kg).[2]IO-360-B2A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 293\u00a0lb (133\u00a0kg).[2]IO-360-B3A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 293\u00a0lb (133\u00a0kg).[2]IO-360-B4A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 293\u00a0lb (133\u00a0kg).[2]IO-360-B5A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 293\u00a0lb (133\u00a0kg).[2]IO-360-B6A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 293\u00a0lb (133\u00a0kg).[2]IO-360-C1A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 293\u00a0lb (133\u00a0kg).[2]IO-360-C2A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 293\u00a0lb (133\u00a0kg).[2]IO-360-C3A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 293\u00a0lb (133\u00a0kg).[2]IO-360-C4A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 296\u00a0lb (134\u00a0kg).[2]IO-360-C5A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 296\u00a0lb (134\u00a0kg).[2]IO-360-C6A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 296\u00a0lb (134\u00a0kg).[2]IO-360-D1A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 296\u00a0lb (134\u00a0kg).[2]IO-360-D2A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 296\u00a0lb (134\u00a0kg).[2]IO-360-D3A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 296\u00a0lb (134\u00a0kg).[2]IO-360-D4A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 296\u00a0lb (134\u00a0kg).[2]IO-360-D5A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 296\u00a0lb (134\u00a0kg).[2]IO-360-D6A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 296\u00a0lb (134\u00a0kg).[2]IO-360-E1A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 297\u00a0lb (135\u00a0kg).[2]IO-360-E2A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 297\u00a0lb (135\u00a0kg).[2]IO-360-E3A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 297\u00a0lb (135\u00a0kg).[2]IO-360-E4A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 300\u00a0lb (140\u00a0kg).[2]IO-360-E5A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 300\u00a0lb (140\u00a0kg).[2]IO-360-E6A1Fuel 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 168\u00a0hp (125\u00a0kW) at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 300\u00a0lb (140\u00a0kg).[2]Applications[edit]Specifications (O-360-A1A2)[edit]Data from TCDS[2]General characteristicsComponentsFuel system: Precision Airmotive MA-4-5 carburetorFuel type: 100LL or 100VLL avgas or 91 octane automotive gasoline with no alcoholOil system: 8\u00a0US\u00a0qt (8\u00a0L) dry sumpCooling system: airReduction gear: nonePerformanceSee also[edit]Related listsReferences[edit]External links[edit]     (adsbygoogle = window.adsbygoogle || []).push({});after-content-x4"},{"@context":"http:\/\/schema.org\/","@type":"BreadcrumbList","itemListElement":[{"@type":"ListItem","position":1,"item":{"@id":"https:\/\/wiki.edu.vn\/en\/wiki40\/#breadcrumbitem","name":"Enzyklop\u00e4die"}},{"@type":"ListItem","position":2,"item":{"@id":"https:\/\/wiki.edu.vn\/en\/wiki40\/superior-air-parts-vantage-wikipedia\/#breadcrumbitem","name":"Superior Air Parts Vantage – Wikipedia"}}]}]