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Section II. 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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Oil Pressure Gage
Figure 9. Controls and instruments, removal points.
the hourmeter, armature relay, and the reser-
voir level indicator.
20. Starter Switch
The starter switch (2, fig. 10), mounted on
the engine control panel, is a spring loaded,
push-type switch. When pressed inward, it
energizes the armature relay which in turn com-
pletes the electrical circuit between the battery
and the starter.
21. Tachometer
The tachometer (9, fig. 9), mounted on the
4 Throttle control
Ignition switch
test stand control panel, is a needle-indicating,
5 Choke control
Starter switch
Fuse holder
direct-reading instrument graduated from 0 to
3500 rpm in increments of 100 rpm. The tacho-
Figure 10. Engine control panel.
AGO 5742A

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