Cessna 182S Pilot Operating Handbook page 344

CESSNA
MODEL 182S
SECTION 9 - SUPPLEMENTS
SUPPLEMENT 15 - FAA APPROVED
14.0MNI 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 -- Indicates the direction of
required pitch trim. The annunciation will flash if autotrim
has not satisfied the request for trim for a period of 10
seconds. A solid
~
without an arrowhead is an indication
of a pitch trim fault. Refer to EMERGENCY PROCEDURES.
for proper response to a pitch trim fault.
17. PITCH TRIM Annunciation (located on instrument panel or
glareshield) -- Illuminates 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.
**18. AUTOPILOT ENGAGE
I
AP
I
Annunciation -- Illuminates
whenever the autopilot is engaged. Flashes during pilot
initiated or automatic disengagement.
** Airplane serials 18280165 · thru 18280944 Incorporating.
Honeywell Service Bulletin KC140-M1 .
Figure 2. Bendix/King KAP 140 2-Axis Autopilot Operating Controls
I
and Indicators (Sheet 4)
Revision 3 S15-11