AFMS
N"D07
FOR
GARMIN
GFC700
AUTOPILOT
AND
VARIABLE
PITCH
PROPELLER
EQUIPPED
AEROPLANES
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age
APV3-3 I
12.
AUTOPILOT
EMERGENCY
PROCEDURES
In
the
event
of
autopilot ma
lf
unctwn. or
wh
en
th
e syst
em
is not per-
forming as expected or commanded, take immediately
th
e aircraft
control disconnecting
the
autopilot which must
be
set moperauve
unul the failure has been identifi
ed
and corrected.
12.1
AUTOPILOT
HARDOVER
OR
FAILURE
TO
HOLD
THE
SELECTED
HEADING
In
case
of
A/P hardover or failure
to
ho
ld
selected h
ea
din
g,
ap-
ply
following procedure:
Arromplisb items I a
gd
2 5jmultancgusly·
I.
2.
3.
4.
Airplane control wheel GRASP FIRMLY and OVER-
POWER
if
necessary
to
regam
aircraft control
AP
DIS
Cff
RIM
INTR
switch
PRESS
AP
MASTER SWITCH OFF
AP
Circuit Breaker PU
LL
Following an AIP or MET system malfunctton,
do
not engage
the autopilot until the cause
of
the ma/functton has been cor-
rected.
When
Autopilot
1s
disconnected,
ii
may
be
necessary operate the
pitch trim through either the Manual Electric Tnm Switch or the
Trim
Wheel.
Ed.
2.
Rev.O
Section
3 -
Emergency
procedures
AUTOPILOT
EMERGENCY
PROCEDURES
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