BEECHCRAFT
Duchess
76
section
VII
Systems
Description
An
emergency release button, incorporated
in
the system, is
located on the left handle grip of the pilot's control wheel.
This button can
be
qUickly depressed
to
deactivate the sys-
tem in case
of
a malfunction
in
the system. The system will
remain deactivated
only
while the button
is
being held
in
the
depressed position.
AILERON TRIM
The aileron trim control, located
on
the lower center console,
is provided
to
displace the ailerons for trimming purposes.
Displacement is maintained by cable loads imposed
by
the
trimmer.
INSTRUMENT
PANEL
The standard instrument panel consists of flight, navigation,
and engine instruments on the left, and
an
avionics section
on the right.
The lower left subpanel contains the switches for control of
the battery and alternators, magneto/start and prime, lights,
environmental, and optional equipment. Also contained on
the
left sUbpanel are the auxiliary fuel pump switches, instru-
ment air gage, landing gear control switch and gear indicator
lights.
Located
on
the
lower
right
subpanel
are
the
rheostat
switches for the instrument flood and post lights, parking
brake control knob, flap switch,
and
flap position indicator. All
of
the circuit breakers, that are associated with the various
placarded systems, are also located on the lower right sub-
panel.
January
1978
7-7
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