Superior Air Parts Vantage Explained

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. 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.

Development

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]

Design

The engine is a four-cylinder, horizontally opposed, four-stroke, 3610NaN0 displacement, air-cooled, direct-drive, gasoline engine design. It produces 165to, depending on the model. It is available in carburetor-equipped and fuel injected versions.[2]

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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and a basic dry weight of 2880NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and a basic dry weight of 288lb.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 288lb.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 291lb.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 291lb.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 291lb.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2910NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 291lb.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 291lb.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 291lb.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 291lb.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 291lb.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2910NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 291lb.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 291lb.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 294lb.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 294lb.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 294lb.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2940NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 294lb.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 294lb.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 294lb.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 294lb.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 294lb.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2950NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 295lb.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 295lb.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 298lb.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 298lb.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 298lb.[2]

    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and a basic dry weight of 2880NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and a basic dry weight of 288lb.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 288lb.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 291lb.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 291lb.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2910NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 291lb.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 291lb.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 291lb.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 291lb.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 291lb.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2910NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 291lb.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 291lb.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 294lb.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 294lb.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 294lb.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2940NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 294lb.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 294lb.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 294lb.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 294lb.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 294lb.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2950NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 295lb.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 295lb.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 298lb.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 298lb.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 298lb.[2]

    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and a basic dry weight of 2900NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and a basic dry weight of 2900NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2900NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2930NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2930NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2930NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2930NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2930NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2930NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2930NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2930NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2930NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2930NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2930NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2930NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2960NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2960NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2960NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2960NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2960NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2960NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2960NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2960NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2960NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2970NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 2970NaN0.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 297lb.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 300lb.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 300lb.[2]
    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 1800NaN0 at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 300lb.[2]

    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and a basic dry weight of 2900NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and a basic dry weight of 2900NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2900NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2930NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2930NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2930NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2930NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2930NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2930NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2930NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2930NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2930NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2930NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2930NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2930NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2960NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2960NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2960NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2960NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2960NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2960NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2960NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2960NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2960NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2970NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 2970NaN0.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 297lb.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 300lb.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 300lb.[2]
    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 1680NaN0 at 2700 rpm, with a compression ratio of 7.2:1 and with a basic dry weight of 300lb.[2]

    Applications

    Notes and References

    1. Web site: New Kid on Block. 22 August 2014. Escobar. Joe. 1 May 2004. aviationpros.com.
    2. Web site: Type Certificate Data Sheet No. E00001SC . 17 April 2018. Federal Aviation Administration. 20 July 2016.
    3. Web site: Vantage Engine. Superior Air Parts. superiorairparts.com. 22 August 2014.
    4. Web site: Type certificate E00001SC. 17 April 2018. . 31 March 2004 .
    5. Web site: Superior Skyhawk SV. Superior Air Parts. superiorairparts.com. 17 April 2018.

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