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CESSNA
MODEL
182S
SECTION
9.
SUPPLEMENTS
SUPPLEMENT
11
-
FAA
APPROVED
SUPPLEMENT
BENDDUKING
KAP
140
2 AXIS
AUTOPILOT
SECTION
1
GENERAL
The KAP
140
2
Axis
Autopilot provides the
pilot with
the
following
features:
Vertical Speed
mode
(VS);
Altitude
hold
(ALT);Wing
Level
(ROL); Heading select (HDG); Approach (APR); ILS coupling
to
Localizer (LOC) and Glideslope
(GS); and
backcourse (REV) modes
of
operation.
The KAP
140
2 Axis Autopilot has an
electric
trim system
which
provides autotrim during autopilot
operation and
manual
electric
trim
(MET)
for the pilot when the autopilot
is
not engaged. The
electric
trim
system
is
designed
to fail
safe for any single
inflight
trim
malfunction.
Trim
faults
are
visually and aurally annunciated.
A
lockout device prevents
autopilot or
MET engagement
until
the
system
has
successfully passed preflight
self
test.
Automatic
preflight self-test begins
with initial
power
application
to
the
autopilot.
The
following conditions
will cause the
Autopilot
to
automaticattyl
disengage:
A.
Power
failure.
B.
lnternal Flight Control System failure.
Ðec
1197
s11-5
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