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CESSNA
MODEL 182S
SECTION 9
-
SUPPLEMENTS
SUPPLEMENT 15 - FAA APPROVED
3.
Flashing GS
--
Indication
of a flagged
glideslope.
(GS will
re-arm
automatically
if a
valid
GS signal is received.)
NOTE
To
continue
tracking
the
localizer,
observe
the
appropriate
minimums for a non-precision
approach.
(Press AL
T
twice
in
rapid
succession
to terminate the flashing
.
Control
the
pitch
axis
in the default VS
mode.)
.
NOTE
At the
onset of
mode annunciator flashing, the
autopilot
has
already
reverted
to a default mode of
operation,
i.e., ROL
and or VS
mode.
An immediate
attempt to
re-engage to lost
mode may be made
.
if the offending navigation, glideslope
or
compass flag
has
cleared.
EXCEPTION
The HOG
annunciation will
flash for
5
seconds upon
selection of
NAV, APR,
or REV modes to remind
the
pilot
to
set
the HOG bug for use as course
datum.
Effects
of
instrument losses upon
autopilot operation:
1.
Loss
of
the
ArtifiCial
Horizon
--
no
effect
on the
autopilot.
2. Loss
of
the Turn Coordinator --
autopilot
inoperative.
3.
Loss of
the
Directional Gyro (DG)-- The directional gyro does
not provide
any
system
valid
flag.
If the DG fails to function
properly the autopilot heading
and
navigation mode
will not
function
correctly.
Under these
conditions,
the
only
useable
lateral mode is ROL.
.
4.
Loss of
Horizontal
Situation
Indicator (HSI) (if
installed) -- If the
HSI
fails
.
to function properly, the autopilot heading
and
navigation mode
will
not
function correctly.
Under these
conditions, the
only
usable
lateral mode is ROL.
5. Loss
of
Blind Altitude Encoder
-- Altitude Alerter and Altitude
Preselect function
inoperative.
Revision 1
S15-19
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