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CESSNA
MODEL
182S
SECTION
9 -
SUPPLEMENTS
SUPPLEMENT
11
- FAAAPPROVED
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.
W¡th
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
í
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
Annuncíation
--
llluminates 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 lndicators (Sheet
5 of
5)
Feb 3/97
s11-11
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