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SECTION 9
-
SUPPLEMENTS
SUPPLEMENT
15
-
FAA
APPROVED
1. PITCH
AXIS
(P)
ANNUNCIATOR When
illuminated,
indicates failure
of
pitch axis and
will
either disengage the
autopilot
or
not
allow engagement
of the
pitch
axis.
ln
turbulent
air, will
illuminate
during
abnormal
ve
rtical/acce
I
e
rations.
2.
AUTOPILOT ENGAGE/DISENGAGE (AP) BUTTON
--
When
pushed, engages autopilot
if
all
preflight self-test
conditions
are
met.
The
autopilot
will engage in the
basic
roll
(ROL)
mode which functions
as
a
wing leveler and the pitch
axis
vertical speed (VS)
mode.
The commanded vertical
speed will
be
displayed
in the
upper right corner
of
autopilot
display
area.
The captured VS will be the vertical speed present
at
the
moment the
AP
button
is pressed. The
button may
also
be
used to disengage the autopilot.
3.
ROLL
AXIS
(R) ANNUNCIATOR
-- When
illuminated, indicates
failure
of
the roll axis
and
disengages the autopilot.
Figure
1.
Bendix/King
2-Axis KAP
140
Autopilot, Operating
Controls and lndicators (Sheet
2
of
5)
CESSNA
MODEL 182S
HÞ
E
frLT
P
T
]5ün
FPM
s15-8
Dec
1/97
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