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O-360 R22 Beta II Engine

General characteristics

Type: Four-cylinder, dual magneto, horizontally opposed, four-stroke aircraft engine
Bore: 5.125 in (130 mm)
Stroke: 4.375 in (111 mm)
Displacement: 361 cu in (5,916 cc)
Dry weight: 258 lb (117 kg)
Components
Fuel type: 91/96 avgas minimum grade[12]
Oil system: 8 US qt (8 l) dry sump
Cooling system: air-cooled
Performance
Power output: 180 hp (134 kW) at 2700 rpm

General characteristics Type: Four-cylinder, dual magneto, horizontally opposed, four-stroke aircraft engine Bore: 5.125 in (130 mm) Stroke: 4.375 in (111 mm) Displacement: 361 cu in (5,916 cc) Dry weight: 258 lb (117 kg) Components Fuel type: 91/96 avgas minimum grade[12] Oil system: 8 US qt (8 l) dry sump Cooling system: air-cooled Performance Power output: 180 hp (134 kW) at 2700 rpm

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