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  TM
55-1730-229-34
AG
320A0-MME-000
TO
35C2-3-473-2
TM
1730-34/1
gearcase pad, and is driven by the en-
cooler (heat exchanger), a manifold,
gine.
The hydraulic pump output pres-
filters (2), and hydraulic lines, fit-
sure is controlled by a switch on the
tings, and valves.
hydraulic control panel. The hydraulic
module controls the application of hy-
f. Propulsion System. The propul-
draulic fluid to an aircraft for power,
sion system, figure 1-6, provides sus-
filling, or flushing requirements. The
pension, steering, brakes, and drive
hydraulic module contains a control
power for the AGPU.
A speed/direction
panel, a reservoir, an accumulator, a
control assembly mounted on a tow bar
Figure 1-6. Propulsion System
1-8
Change 2
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