Cessna 182S Pilot Operating Handbook page 339

SECTION 9 - SUPPLEMENTS
SUPPLEMENT 15 - FAA APPROVED
CESSNA
MODEL 182S
I
C. Pitch accelerations in excess of + 1.4g or less than +0.6g
only when produced by a failure causing seNO runaway. The
pilot cannot maneuver the airplane and trip the monitor.
D. Turn Coordinator failure (small square red flag visible on
instrument).
E. Computer autopilot monitor that detects either the R (ROLL)
or P (PITCH) axis annunciator.
Activation of AlP DISCfTRIM INT control wheel switch will also
disconnect the autopilot.
The AVIONICS MASTER switch supplies power to the aviohics bus
bar of the radio circuit breakers and the autopilot circuit breaker.
The AVIONICS MASTER switch also seNes as an emergency
AP/MET shutoff.
The following circuit breakers are used to protect the
KAP
140
2-Axis Autopilot:
LABEL
AUTO PILOT
WARN
S15-6
FUNCTIONS '
Pull-off circuit breaker supplies power to
the KC 140 Computer and the autopilot
pitch, roll and pitch trim seNOS.
Supplies separate power for autopilot
alerting (PITCH TRIM) on the ship's
annunciator panel.
Revision
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