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SECTION
9
- SUPPLEMENTS
SUPPLEMENT
15
- FAA APPROVED
CESSNA
MODEL 182S
9.
VERTICAL SPEED
(UP/DN)
MODE BUTTONS --
The action
of
these buttons
depends
on the
vertical mode present
when
pressed. lf 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
DN
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.
lf ALT mode is 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.
AUTO PILOT CIRCUIT BREAKER
-- A
5-amp pull-off
circuit
breaker supplying 28 VDC
to
the
KAP
140
system.
11.
WARN CIB
--
Power
to the autopilot disconnect horn and
the
ship's annunciator panel (PITCH TRIM).
12. AUTOPTLOT DTSCONNECT
(A/p D|SC/TR|M ¡NT)
SWTTCH --
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
a
flashing "AP" displayed
on
the autopilot computer.
13.
MANUAL ELECTRIC TRIM (MET) SWITCHES
--
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, simulating
a
stuck switch,
for
3
seconds,
the trjm
monitoríng system
will
detect
a switch
failure
resulting
in
a
i
annunciation
on the autopilot dísplay and
the
disabling
of the
electric trim system.
lf
the
stuck switch
is
corrected,
the fault will
clear,
Use
of
manual electric
trim
during autopilot operation will disengage the autopilot.
Figure
1.
Bendix/King 2-Axis KAP
140
Autopilot, Operating
Controls and lndicators (Sheet 4
of 5)
s15-10
Dec
1/97
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