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Page Title:
ATTACH HOSES BETWEEN TEST STAND AND AIRCRAFT |
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 TM 55-4920-426-13&P
2-4
2-4
HYDRAULIC SYSTEM OPERATION Continued
Return the flow control valve to the by-pass
g.
position.
h.
With the volume control, adjust to the required fluid
flow on the flowmeter for test.
i.
Turn throttle to the left and push fully in, let engine
idle for a minute or two.
Put ignition switch in the stop position. Engine
j.
stopped.
k.
The test stand is now ready for attaching to the
aircraft.
Do not attach hoses to aircraft when
test stand is operating.
2-5
ATTACH HOSES BETWEEN TEST STAND AND AIRCRAFT
2-5
Remove dust cap from the supply port coupling on
a.
the test stand.
(Remove dust plug from the supply hose union
nut.)
(Connect the supply hose union nut to the supply
port coupling.)
Remove dust cap from the return port coupling on
b.
the test stand.
(Remove dust plug from the return hose union nut.)
(Connect the return hose union nut to the return
port coupling.)
Connect the supply hose and return hose to corr-
c.
esponding ports on the aircraft.
2-17
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