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CESSNA
MODEL
182S
SECTION
9 -
SUPPLEMENTS
SUPPLEMENT
11
- FAAAPPROVED
5.
NAVIGATION (NAV) MODE SELECTOR BUTTON
--
When
pushed,
The mode
provides
automat
VOR, LOC,
or
GPS
signals
the #1
CDl.
NAV
mode
is
ion
tracking.
6. APPROACH (APR) MODE SELECTOR BUTTON
--
When
7.
BAOK COURSE APPROACH (REV) MODE BUTTON
--
This
button
is
active only when the couled navigation receiver
ís
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
approximately
a
10%
(of VS
rate)
overshoot,
with
the
airplane
returned
positively
to the selected altitude. This button may be
used
to
engage the autopilot.
9.
VERTICAL SPEED (UP/DN) MODE BUTTONS --
The
action
of
these buttons are dependent upon the veftical 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.
Figure
1.
Bendix/King 2-Axis KAP
140
Autopilot, Operating
Controls and lndicators (Sheet
3 of 5)
Feb
3/97
s11-9
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