Agusta GA.140

Agusta GA.140

__NOTOC__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.pistonspecs

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)
length=
diameter=
width=
height=
weight=256 lb (116 kg)
valvetrain=
supercharger=
turbocharger=
fuelsystem=
fueltype=
oilsystem=
coolingsystem=Air-cooled
power=103 kW (138 hp) at 3,200 rpm
specpower=
compression=
fuelcon=
specfuelcon=
oilcon=
power/weight=

Applications

* Agusta A.104

References

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


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