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CESSNA
MODEL
182S
SECTION
9
- SUPPLEMENTS
SUPPLEMENT
15
-
FAA APPROVED
4. HEADING (HDG) MODE SELECTOR
BUTTON
When
pushed,
will
select
the
Heading mode, which commands
the
airplane
to turn to and
maintain
the
heading selected by
the
heading bug
o
e
selected
at
an
o
the new
head
e
between
HDG
d
to engage the autopilot
in
HDG mode.
5.
NAVIGATION (NAV) MODE SELECTOR BUTTON
--
When
pushed, will
select
the Navigation mode. This mode
provides
automatic beam capture and tracking
of VOR,
LOC,
or
GPS
signals
as
selected
for
presentation
on the #1
CDl.
NAV
mode is recommended for enroute navigation tracking.
6. APPROACH (APR) MODE SELECTOR BUTTON
--
When
pushed, will select the Approach
mode.
This mode
provides
automatic beam
capture and tracking of VOR, GPS, LOC
and
Glideslope (GS)
on an lLS, as selected for
presentation
on
#1
CDl.
APR
mode tracking sensitivity
is
recommended for
instrument approaches.
7.
BACK COURSE APPROACH (REV) MODE BUTTON
--
This
button
is
active only when the coupled navigation receiver
is
tuned
to
a
LOC/ILS
frequency. When
pushed will select
the
Back Course
approach
mode. This
mode
functions
identically
to the
approach mode except that
the
autopilot response
to
LOC signals
is reversed.
Glideslope
is
locked out with
REV
mode.
8.
ALTITUDE HOLD (ALT) MODE SELECT BUTTON
--
When
pushed,
will
select
the
altitude
hold
mode.
This
mode
provides capture and tracking
of the
selected
altitude.
The
selected altitude
is
the
airplane
altitude
at
the
moment
the
ALT
button
is
pressed.
lf
the ALT
button
is
pressed
with
an
established
VS
rate present,
there will be about
a
10"/"
(of
VS
rate) overshoot. The airplane
will
return positively
to
the
selected
altitude. This
button may
be
used
to
engage
the
autopilot
in
the ALT
mode.
Figure
1.
Bendix/King 2-Axis
KAP
140
Autopilot, Operating
Controls and lndicators (Sheet
3 of
5)
Dec
1/97
s15-9
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