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SECTION
9
- SUPPLEMENTS
SUPPLEMENT
11
- FAAAPPROVED
CESSNA
MODEL
182S
C.
Pitch accelerations
in
excess
of +1.49 or
less
than
0.69
will
cause the autopilot to disengage.
D.
Flagged
turn
and bank
gyro.
E.
Computer autopilot monitor that detects either
the R
(ROLL)
or
P
(PITCH) axis annunciator.
Activation
of AP
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 airplane MASTER switch function
is
unchanged and can
be
used
in an
emergency
to shut off electrical
power
to
all flight
control
systems while
the
problem is
isolated.
The following circuit breakers are used
to
protect
the KAP
140
2-Axis Autopilot:
LABEL
FUNCTIONS
I AUTO
Supplies power
to
the
KC
140
Computer
and
I
PILOT
the
autopilot pitch, roll and pitch trim
seruos.
WARN
Supplies separate power
for
autopilot
alefting
on
the
ship's annunciator
Panel'
s1 1-6
Dec
1197
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