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SECTION
9.
SUPPLEMENTS
SUPPLEMENT
11
- FAAAPPROVED
CESSNA
MODEL
182S
lf ALT mode
¡s active, pressing
the UP/DN
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 ALT
reference
to the
actual
airplane altitude
upon
button release.
10.
AUTOPILOT CIRCUIT BREAKER
-- A
S-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. AUTOPTLOT
DTSCONNECT
(A/P DISC TRIM INT)
SWITCH
--
When
depressed
will
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. lf only one switch is
moved, the
trim system will not operate. lf 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 !
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.
OMNI
BEARING
SELECT KNOB (OBS) --
Selects
the
desired
course to
be tracked by the
autopilot. (Note: The
HDG
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 lndicators (Sheet
4
of 5)
s1
1-10
Feb
3/97
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