Cessna 182S Skylane Information Manual page 404

CESSNA
MODEL 182S
SECTION 9
- SUPPLEMENTS
SUPPLEMENT 15
-
FAA APPROVED
3. Note that the emergency
procedure
for any
malfunction
is
essentially
the
same:
immediately grasp
the
control
wheel
and
regain
airplane control while
pressing and
holding
the
A/P
DISCÆR|M
INT switch down, and retrim
the
airplane
as
needed.
After these steps have been accomplished
secure
the
autopilot electric
trim
system
by
pulling
the
autopilot
(AUTO PILOT) circuit breaker. As with any other
airplane
emergency procedure,
it is
important that
the
4
steps of
the
emergency procedure located'on Page 15 be committed
tol
memory.
4. The AVIONICS MASTER switch may be used
to
remove
all
electric power from the
Autopilot
and
Electric
Trim
systems
while
the
circuit breaker
is
located
and
oulled.
Return
the
AVIONICS MASTER switch
to the
ON position
as
soon
as
possible. With the AVIONICS
MASTER switch
off, all
avionics
and autopilot equipment
will
be inoperable.
5. lt
is
important
that all portions of the
autopilot
and electric
trim
system are preflight tested prior to
each flight
in
accordance
with
the procedures published herein in
order
to
assure
their
integrity and continued safe operation during
flight.
¡[, wnnurc
DO NOT
RESET AUTOPILOT CIRCUIT
BREAKER
FOLLOWING
AN
AUTOPILOT/AUTOTRIM
OR
MANUAL ELECTRIC TRIM MALFUNCTION
UNTIL
THE CAUSE
FOR
THE
MALFUNCTION HAS BEEN
CORRECTED.
A flashing
ç
auto trim annunciation on the face of
the
autopilot
indicates
a
failure
of the
auto trim function
to
relieve pitch
seruo
loading
in a timely
manner.
This condition should
be
temporary.
D
1. FLASHING
i
ANNUNCIATION
--
OBSERVE aircraft
pitch
behavior.
lf
pitch behavior is
satisfactory, wait 5-10
seconds
for
the annunciation
to
stop.
Dec 31/99 s15-17