Cessna 182S Pilot Operating Handbook page 343

SECTION 9 - SUPPLEMENTS
SUPPLEMENT 15 - FAA APPROVED
CESSNA
MODEL 182S
9. VERTICAL SPEED (UP/ON) MODE BUTTONS -- The action
of these buttons depends on the vertical mode present when
pressed. If VS mode is active (AP plus any lateral mode) and
the UP button is pressed, the autopilot will modify the
displayed VS command (FPM) in the up direction. Single
momentary cycles on either the UP or ON button will
increment the VS command by 100 FPM per cycle. When
either button is continuously held in, it will mOdify the vertical
speed command by 300 FPM per second.
If
AL T mode is active, pressing the UP/ON 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. AUTO PILOT CIRCUIT BREAKER -- A 5-amp pull-off circuit
breaker supplying 28 VDC to the KAP 140 system.
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11. WARN CIRCUIT BREAKER -- Power to the autopilot
disconnect horn and the ship's annunciator panel (PITCH
TRIM).
12. AUTOPILOT DISCONNECT (NP DISCITRIM INT) SWITCH --
When" depressed, will disengage the autopilot and interrupt
manual electric trim (MET) power. An autopilot disconnect
will be annunciated by a continuous 2 second tone
accompanied by flashing "AP" annunciations on the autopilot
computer.
13. MANUAL ELECTRIC TRIM (MET) SWITCHES -- When both
switches are pressed in the same direction the trim system
will provide pitch trim in the selected direction. Use of manual
electric trim during autopilot ope ration will disengage the
autopilot.
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Figure 2. Bendix/King KAP 140 2-Axis Autopilot Operating Controls
and Indicators (Sheet 3)
S15-10
Revision 3