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Figure 8-27.-Hydraulic booster block diagram.
Stability Augmentation Mode

Aviation Electrician's Mate 3&2
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Figure 8-28.--Automatic pitch trim block diagram.
NOTE: The AFCS channel shown in figure
and the aircraft flight control system provide the final
8-29 represents the basic design of the channel and
amplifying link to move the flight control surfaces.
is for instructional use only. For further study of
Look at figure 8-29. Each AFCS control
the AFCS, you should refer to the MIM for your
channel is basically the same; however, its design
particular aircraft.
depends on the type and mission of the aircraft.
Figure 8-29.-Basic AFCS control channel.
8-25


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