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SECTION
9
- SUPPLEMENTS
SUPPLEMENT
15
- FAA APPROVED
CESSNA
MODEL
182S
SECTION
4
NORMAL PROCEDURES
A.
PREFLTGHT
(PERFORM pRtOR
TO
EACH
FLTGHT):
1.
AVIONICS MASTER
-.
ON.
2.
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 ís indicated by
"p5¡"
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"
(4,/C
System Annunciator
Panel)
being illuminated, and the disconnect tone sounding.
NOTE
Upon applying power
to the
autopilot,
the red P warning
on
the face of the autopilot may illuminate indicating that the
pitch axis cannot
be engaged. This
condition
should
be
temporary, lasting approximately
30 seconds. The P
will
extinguish and normal operation will
be
available.
¡l,
wnnnnc
IF
PITCH TRIM LIGHT STAYS ON, THEN THE
AUTOTRIM
DID NOT PASS
PREFLIGHT
TEST.
THE AUTOPILOT CIRCUIT BREAKEB MUST BE
PULLED.
MANUAL
ELECTRIC
TRIM AND AUTO.
PILOT
ARE
INOPERATIVE.
3. MANUAL
ELECTRIC TRIM
-
TEST as
follows:
Press
both
halves
of the split Manual
Electric
Trim
(MET)
switches
to
the
nose down position, verify that the trim wheel and the trim
tab
position indicator
are
moving
in the down direction.
Repeat
test for
the
nose up direction.
l'u-ro
Dec 31/99
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