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SECTION
9 -
SUPPLEMENTS
SUPPLEMENT
15
- FAA APPROVED
CESSNA
MODEL
182S
C.
Pitch accelerations
in
excess
of
+1.49
or
less than
+0.69
I
only when
produced
by a failure causing servo
runaway.
The
I
pilot cannot maneuver the
aircraft
and
trip
the
monitor.
D.
Turn coordinator failure (flagged
gyro).
E.
Computer autopilot monitor
that
detects either
the R
(ROLL)
or
P
(PITCH) axis annunciator.
Activation
of A/P
DISC/TRIM INT control wheel switch
will
also
disconnect the autopilot.
The AVIONICS MASTER switch supplies power to the
avionics
bus bar
of the
radio circuit breakers and
the
autopilot
circuit
breaker.
The
AVIONICS MASTER switch
also serves
as
an
emergency AP/MET
shutoff
.
The following circuit breakers are used
to
protect
the KAP
140
2-Axis Autopilot:
LABEL
FUNCTIONS
AUTO
Pull-off circuit breaker supplies power to
the
KG
PILOT
140 Computer and the autopilot pitch, roll
and
pitch trim servos.
WARN
Supplies separate power
for
autopilot
alerting
(PITCH TRIM)
on
the ship's annunciator panel.
s15-6
Dec 31/99
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