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clocK
/ o.A.T.
|ND|CATOR
I
An
integrated clock
/
O.A.T.
is
installed in
the
upper left side
of
the
instrument panel
as
standard equipment.
For
a
complete
$::i,rjf[:
and operating instructions, refer
to the
Supptements,l
STALL WARNING
SYSTEM
control panel, protects the stall warning
system.
The vane in
the
wing senses the change in airflow over the wing, and operates the
warning horn at airspeeds between
5
and 10 knots above the
stall
in
allconfigurations.
The
airplane has
a
heated stall warning system,
the vane
and
sensor unit
in the wing
leading
edge
is
element. The
heated part of the
system
HEAT switch, and
is
protected
by
the
PITO
.
The.stall warning system should be checked during the
pre-flight
inspectíon
by
momentarify
turning
on the
mastei switch
an¿
actuating
the vane in the
wing.
The system is
operational
if
the
warning horn sounds
as
the
vane
is
pushed upward.
CESSNA
MODEL
182S
SECTION 7
AIRPLANE
&
SYSTEMS DESCRIPTION
Nov
15/00
7-47
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