Cessna 182S Pilot Operating Handbook page 402

SECTION 9 - SUPPLEMENTS
SUPPLEMENT 11 - FAA APPROVED
CESSNA
MODEL 182S
If AL T mode is active, pressing the UPIDN buttons will modify
the captured altitude by 20 feet per cycle, or if held
continuously will command the airplane up or down at the rate
of 500 FPM , synchronizing the AL T reference to the actual
airplane altitude upon button release.
10. AUTOPILOT CIRCUIT BREAKER -- A 5-amp circuit breaker
supplying 28 VDC to the KAP 140 system.
11. WARN CIB -- Power to the autopilot disconnect horn and the
annunciator panel.
12. AUTOPILOT DISCONNECT (NP DISC TRIM INT) SWITCH --
When depressed wi ll disengage the autopilot and interrupt
electric trim power. An autopilot disconnect will be
annunciated by a continuous 2 second tone accompanied by a
flashing "AP" displayed on the autopilot computer.
13. MANUAL ELECTRIC TRIM SWITCHES (MET) -- When both
switches are pressed in the same direction, will activate pitch
trim in the selected direction. If only one switch is moved, the
trim system will not operate. If only the right half of the MET
switch assembly is held for 3 seconds, the trim monitoring
system will detect a switch failure resulting in a
t
annunciation on the autopilot display and the disabling of the
electric trim system. Autopilot power will have to be cycled to
clear the fault. Use of manual electric trim during autopilot
operation will disengage the autopilot.
14. 0MNI BEARING SELECT KNOB (OBS) -- Selects the desired
course to be tracked by the autopilot. (Note: The HOG bug
must also be positioned to the proper course to capture and
track the selected radial or desired track).
Figure 1. Bendix/King 2-Axis KAP 140 Autopilot, Operating
Controls and Indicators (Sheet 4 of 5)
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