The Agusta GA.140 was a 4-cylinder, air-cooled, horizontally-opposed engine developed in Italy for helicopter use. It was produced from 1962 to 69.

General characteristics

• Type: 4-cylinder air-cooled horizontally opposed helicopter piston engine
• Bore: 114 mm (4.5 in)
• Stroke: 89 mm (3.5 in)
• Displacement: 3.6 L (223 in³)
• Dry weight: 256 lb (116 kg)

Components

• Cooling system: Air-cooled

Performance

• Power output: 103 kW (138 hp) at 3,200 rpm

[edit] Applications

• Agusta A.104

[edit] References

• Erickson, Jack. Horizontally-Opposed Piston Aero Engines

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