Agusta GA.70

__NOTOC__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.

pistonspecs

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)
length=
diameter=
width=
height=
weight=176 lb (80 kg)
valvetrain=
supercharger=
turbocharger=
fuelsystem=
fueltype=
oilsystem=
coolingsystem=Air-cooled
power=54 kW (72 hp) at 3,100 rpm
specpower=
compression=
fuelcon=
specfuelcon=
oilcon=
power/weight=

Applications

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

References

* Erickson, Jack. " [http://home.comcast.net/~aeroengine/ Horizontally-Opposed Piston Aero Engines] "