Cessna 182S Pilot Operating Handbook page 403

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CESSNA
MODEL 182S
SECTION
9 - SUPPLEMENTS
SUPPLEMENT 11
-
FAA
APPROVED
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
-- Indicates
the
direction of
required
pitch
trim.
With
electric
trim
installed,
the
annunciation
simply
provides
status as
to the autopilot's
request
for autotrim. A
solid
indication represents the lowest
demand level for
trim; whereas a
flashing
annunciator
implies
a greater
demand. A
solid
~
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
--
Illuminates
whenever
the
automated
preflight
self test detects
a
pitch
trim
fault or a
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 Indicators (Sheet 5 of 5)
C
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/0"7
C 1
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