Agusta GA.40
The Agusta GA.40 was a 2-cylinder, air-cooled, horizontally opposed engine developed in Italy by Agusta for light aircraft use. It was intended for use in motorgliders. The engine was produced in the 1950s and 1960s.
primaryTopic
Agusta GA.40
The Agusta GA.40 was a 2-cylinder, air-cooled, horizontally opposed engine developed in Italy by Agusta for light aircraft use. It was intended for use in motorgliders. The engine was produced in the 1950s and 1960s.
has abstract
The Agusta GA.40 was a 2-cylin ...... oduced in the 1950s and 1960s.
@en
Wikipage page ID
31,732,111
Wikipage revision ID
716,328,304
coolingsystem
designer
first run
fuelsystem
fueltype
national origin
oilsystem
Pressure lubrication with a gear driven pump
power
power/weight
ref
Jane's All the World's Aircraft 1962-63
specpower
unit cost
valvetrain
pushrod operated overhead valve, 1x inlet + 1x exhaust per cylinder
hypernym
comment
The Agusta GA.40 was a 2-cylin ...... oduced in the 1950s and 1960s.
@en
label
Agusta GA.40
@en