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SECTION
9
- SUPPLEMENTS
SUPPLEMENT
15
-
FAA
APPROVED
CESSNA
MODEL 182S
AMPLIFIED EMERGENCY PROCEDURES
are
presented
to
supply
additional
of
providing
the pilot with
a
more
e
recommended course
of
action for
an emergency situation.
1.
An
autopilot
or
autotrim malfunction
occurS
when there
is
an
uncommanded deviation
in the
airplane flight path
or
when
there
is abnormal control
wheel or trim wheel motion. ln
some
cases, and especially for autopilot trim, there may be little to
no
airplane motion,
yet the red
PITGH TRIM
annunciator
(ship's annunciator panel) may illuminate and
an
alert tone
may
sound.
The
primary concern
in
reacting
to
an
autopilot
or
autopilot
trim
malfunction,
or to an
automatic disconnect
of
the
autopilot,
is in
maintaining
control of the aírplane.
lmmediately
grasp the control wheel and press and hold down
the
A/P
DISC/TRIM INT switch throughout
the recovery.
Manipulate
the
controls
as
required
to
safely maintain operation
of
the
airplane within
all
of
its
operating limitations. Elevator
trim
should be used manually as needed
to
relieve
control
forces.
Locate and
pull the
AUTO PILOT
circuit
breaker on
the
right hand circuit
breaker panel
to
completely disable the
autopilot system.
2.
A
manual electric
trim
malfunction may
be
recognized
by
illumination
of the red
PITCH
TRIM
annunciator, accompanied
by an
alert tone,
or by
unusual trim wheel motions with the
autopilot OFF, without
pilot
actuation
of the
manual
electric
trim switches. As with an
autopilot malfunction,
the
first
concern following
a
manual electric
trim
malfunction
is
maintaining control
of the airplane.
Grasp the control
wheel
firmly and press and hold down the
A/P
DISC/TRIM
INT
switch.
Locate and pull
the AUTO
PILOT circuit breaker
on
the
right hand breaker panel.
l.
,u-
,u
Dec
31/99
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