Agusta GA.70
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| Agusta GA.70 |
| Type |
4-cylinder, air-cooled, horizontally opposed engine |
| National origin |
Italy |
| Manufacturer |
Agusta |
| Designed by |
M. Ginnini |
| First run |
1955 |
| Unit cost |
$1010 for the GA.70/O, $1340 for the GA.70/V in 1958 [1] |
The Agusta GA.70 was a 4-cylinder, air-cooled, horizontally opposed engine developed in Italy for light aircraft and helicopter use. The GA.70/V featured a bottom sump for vertical applications and was rated at 158hp. It was produced in the 1950s and 60s.[2]
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
[edit] References
- ^ Sport Aviation. July 1958.
- ^ Flight. July 1957.
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