SECTION 9
-
SUPPLEMENTS
SUPPLEMENT 15
-
FAA APPROVED
CESSNA
MODEL
172R
NOTE
The
following
procedures
apply to
airplane serials
I
17280831
thru
17281118
incorporating Honeywell
Service
Bulletin
KC140-M1,
and serials 17281119
and on.
The
following
voice
messages
will be annunciated as
conditions
warrant:
1.
"TRIM IN
MOTION"
-
Elevator trim
running for
more
than
5
seconds,
message
repeats every 5
seconds.
2.
"CHECK PITCH TRIM"
-
An
out
of
trim condition has existed
for approximately
20
seconds,
take
immediate
corrective
action.
a.
Airplane
Control
Wheel
--
GRASP
FIRMLY
and
regain
aircraft
control.
b.
A/P
DISC/TRIM INT
Switch
-
PRESS and
throughout
recovery.
c.
AIRCRAFT
--
RE-TRIM
Manually
as
Needed.
HOLD
d.
AUTO PILOT
Circuit
Breaker
--
PULL.
SECTION
4
NORMAL PROCEDURES
A.
PREFLIGHT
(PERFORM PRIOR TO
EACH
FLIGHT):
1.
AVIONICS MASTER
-
ON.
POWER APPLICATION AND SELF TEST
--
A self
test
is
performed
upon power
application
to
the
computer.
This
test
is a
sequence
of
internal checks that validate proper
system
operation
prior
to
allowing
normal
system
operation.
The
sequence
is indicated
by
"PFT"
with an
increasing
number
for
the sequence
steps.
Successful completion
of
self
test
is
identified by
all
display
segments
being
illuminated
(Display
Test),
external
"Pitch Trim"
(A/C
System Annunciator Panel)
being
illuminated, and the disconnect
tone
sounding.
S15-20
Revision
2
Summary of Contents for 172R
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