Textron Cessna 172R - Page 440

SECTION
9
-
SUPPLEMENTS
SUPPLEMENT
15
-
FAA
APPROVED
CESSNA
MODEL
172R
SECTION
2
LIMITATIONS
The
following
autopilot
limitations
must
be
adhered
to:
1.
The entire
preflight
test
procedure
outlined under
Section
4,
paragraph
A
of
this
supplement,
including
steps
1
through
7,
must
be
successfully
completed prior
to
each
flight.
Use
of
the
autopilot
or
manual electric
trim
system
is
prohibited
prior
to
completion
of
these
tests.
2.
During
autopilot operation,
a
pilot
with
seat
belt
fastened
must
be
seated
at
the
left
pilot position.
3.
The
autopilot
must
be
OFF
during
takeoff
and
landing.
4.
KMA
28
audio
amplifier
PUSH
OFF/EMG
operation
is
prohibited
during
normal
operations.
NOTE
During
emergency
operation
of
the audio
amplifier,
the
PUSH
OFF/EMG
state
of
the
KMA
28
will
prevent
flight
control
system
alerts
from
being
heard.
5.
The
system
is
approved
for
Category
I
operation
(Approach
mode
selected).
6.
Autopilot
maximum
airspeed
limitation
--
140
KIAS.
Autopilot
minimum
airspeed
limitation
--
70
KIAS.
Autopilot
minimum
approach
speed
--
80
KIAS.
7.
Maximum
flap
extension
-
10°.
8.
The
autopilot
must
be
disengaged
below
200
feet AGL
during
approach operations
and below
800
feet AGL
for
all
other
/%
phases
of
flight.
1
9.
Overriding
the
autopilot
to
change
pitch
or
roll attitude is
prohibited.
(Disengage
with
A/P
DISC/TRIM
INT
or
AP
select
button.)
10.
The
AUTO PILOT
circuit
breaker
must
be
pulled
following
any
inflight
illumination
of
the red
"PITCH
TRIM"
warning light,
but
only
after
first
completing
the
Emergency
Procedures
(Section
,
3,
paragraph
1.).
The manual electric trim
and
autopilot
autotrim
systems
will
be disabled with the
AUTO
PILOT
circuit
breaker
pulled.
S15-14
Original
Issue
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