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SECTION
9
- SUPPLEMENTS
SUPPLEMENT
11
- FAAAPPROVED
CESSNA
MODEL
182S
I l.
ln
case of Autopilot, Autopilot Trim,
or
Manual Electric
Trim
I
malfunction (accomplish ltems A
and
B
simultaneously):
A. Airplane Control
Wheel
--
GRASP FIRMLY
and
regain
aircraft control.
B.
A/P
DISC/TRIM
INT
Switch
PRESS
and
HOLD
throughout recovery.
C. AIRCRAFT -- RETRIM Manually
as
Needed.
D.
AUTOPILOT Circuit Breaker -- PULL.
NOTE
The Avionics Master Switch may be used as an
alternate
means
of
removing
all
power
from the
autopilot
and
electric
trim systems.
lf
necessary perform sÌeps 1A through
1C
above, then turn
the Avionics Master
Switch OFF
before
locating
and
pulling
the Autopilot Circuit Breaker. Turn
the
Avionics Master
Switch on as soon as possible
to
restore
power
to all
other avionics equipment. Primary
attitude,
airspeed, direclional compass, and altitude instruments
will
remain operational at
alltimes.
¡[,
mnrurruc
DO
NOT
ATTEMPT
TO
RE.ENGAGE
THE
AUTOPILOT FOLLOWING
AN
AUTOPILOT,
AUTOTRIM,
OR
MANUAL ELECTRIC
TRIM
MALFUNCTION UNTIL
THE
CAUSE FOR
THE
MALFUNCTION
HAS
BEEN CORRECTED.
Maximum Altitude losses due to autopilot malfunction:
CONFIGURATION
ALT.
LOSS
Cruise, Climb,
Descent
250
ft.
Maneuvering
100
ft.
APPR
50ft.
AMPLIFIED
EMERGENCY PROCEDURES
are
presented
to
supply
additional
inf
of
providing
the
pilot with
a
more
co
e
recommended course
of
action for
an emergency situation.
s1 1-14
July 18/97
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