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CESSNA
MODEL
182S
SECTION 9 - SUPPLEMENTS
SUPPLEMENT
15
-
FAA APPROVED
14.
OMNI
BEARING
SELECT (OBS)
KNOB
-- Selects the
desired
course to
be tracked by the
autopilot. (Note: The
HDG
bug
must also be positioned
to the
proper course
to
capture
and
track the selected radial or desired track).
15. HEADING
SELECT KNOB
(HDG)
--
Positions
the heading
bug
on the compass
card.
Note that
the
position
of the
heading
bug also
provides
course
datum
to the
autopilot
when
tracking
in
NAV, APR,
or
REV (BC)
modes. This is in
addition
to
its
more intuitive use
in
the
HDG mode.
16.
PITCH TRIM (PT) Annunciator
--
lndicates
the
direction
of
required pitch
trim.
The
annunciation
will flash if auto trim
has
not satisfied
the
request
for trim for a
period
of
10
seconds.
A
solid
I
without an arrowhead is an
indication
of
a
pitch trim
fault.
Refer
to the
EMERGENCY PROCEDURES
for
proper
response to a pitch trim fault.
17.
PITCH TRIM Annunciation
--
llluminates whenever
the
automated preflight self
test
detects
a
pitch trim fault or
the
continuous monitoring system detects
a
pitch
trim fault
in
flight.
Refer
to the
EMERGENCY
PROCEDURES
for
proper
response to a pitch trim fault.
Figure
1.
Bendix/King 2-Axis
KAP
140
Autopilot, Operating
Controls and lndicators (Sheet
5 of
5)
Dec
1/97
s15-11
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