The Agusta GA.70 was a 4-cylinder, air-cooled, horizontally-opposed engine developed in Italy for light aircraft and helicopter use. It was produced in the 1950s and 60s.

General characteristics

• Type: 4-cylinder air-cooled horizontally opposed aircraft piston engine
• Bore: 92 mm (3.6 in)
• Stroke: 86.5 mm (3.4 in)
• Displacement: 2.3 L (140 in³)
• Dry weight: 176 lb (80 kg)

Components

• Cooling system: Air-cooled

Performance

• Power output: 54 kW (72 hp) at 3,100 rpm

[edit] Applications

• Agusta A.103
• Bölkow Bo 103
• de Bernardi Aeroscooter
• Phoenix Minor
• Phoenix Major

[edit] References

• Erickson, Jack. Horizontally-Opposed Piston Aero Engines

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