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Section VII. ENGINE CONTROLS AND INSTRUMENTS
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TM-55-4920-226-15 Test Stand Aircraft Hydraulic AHT-5A-1 Type D-5A Manual
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Chapter 6. HYDRAULIC SYSTEM MAINTENANCE INSTRUCTIONS
in the panel and secure with the
(b) Remove the hex nut and lockwasher
that secure the fuse holder in the
bracket, lockwashers, and nuts.
panel and remove the fuse holder.
(b) Connect the oil line tubing to the oil
pressure gage.
(2) Installation.
(a) Position a new fuse holder (3) in
138. Engine Controls
the panel and secure with the lock-
a. Ignition Switch.
washer and hex nut.
(b) Connect the electrical leads to the
(1) Testing. Tag and disconnect the elec-
fuse holder.
trical leads from the ignition switch
and test the switch for continuity with
d. Throttle.
a suitable test lamp circuit.
(1) Removal.
(2) Ignition Switch Replacement.
(a) Disconnect the throttle control (6,
(a) Tag and disconnect all electrical
fig. 11) from the governor control
leads from the ignition switch (1,
assembly.
fig. 10).
(b) Remove the hex nut (4) that se-
(b) Remove the hex nut and lockwasher
cures the throttle in the engine con-
that secure the ignition switch to
t r o l panel (2) and remove the
the panel and remove the switch.
throttle.
(c) Position a new ignition switch (1)
(2) Installation.
in the panel and secure with the
(a) Insert the throttle control (6) in the
lockwasher and hex nut.
engine control panel (2) and secure
(d) Connect the electrical leads to the
with the hex nut (4).
ignition switch in accordance with
(b) Connect the throttle to the governor
tags attached during removal.
control assembly.
b. Starter Switch. Test the starter switch
e. Choke Control. Remove and install the
for serviceability and replace the starter switch
choke control (5, fig. 11) in a manner similar
in a manner similar to that described in a above.
to that described in d above.
c. Fuse Holder.
(1) Removal.
(a) Disconnect the electrical leads from
the fuse holder (3, fig. 10).
AGO 5742A

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