Pitch angle (climb or dive) can
be
controlled
within
limits
by
rotation of Pitch Control Knob. (Command
limits
are approximately 10°
down,
15° up).
Controlled
tums
left
or
right,
up
to
26°
bank angles,
can be made by rotating Turn Control Knob oft center.
Operation
of the
Turr;i
Knob off center disconnects
the
"Heading Lock".
When
the Turn Knob is
set
at center for level flight,
the
"Heading Lock"
button
can
be
pushed in
to
provide
heading reference to
the
Directional Gyro. Heading
can
b!'f
selected by setting
the
upper card of
the
Direc·
tional Gyro
with
the
''Course"
Selector Knob.
Auto·
pilot
will
bring airplane
to
desired heading
if
within
800 of either side of desired heading. Past
80°,
the
Heading Lock
will
turn
the airplane to
the
reciprocal of
th~
heading requested. All corrections using
the
Course Selector Knob have a turn rate of approxi-
mately 1° per sscond. The tab beneath
the
Turn Knob
can
be
moved left or right to
shift
the roll zero point up
to
two
degrees in the corrosponding direction.
When
desired altitude is attained, engage
Altitude
Hold
(if
installed) by
pulling
out
Altitude
Hold Knob on right
side of Command Control Unit.
Disengage
Altitude
Hold
by
pushing
in
Altitude
Hold
Knob whenever a change
to
another altitude is
desired.
PERFORMANCE
• No change
Approved:
-;'
),<
;/
fi
~
/ff
//
011~.u-"'~
FAA
Approved
Revised:
September
1977
P;N
33-690013-3
Chester
A.
Rembleske
IBeech
Aircraft
Corporation
DOA
CE-2
3
of
3
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