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Glareshield lighting
is
accomplished using
a
fluorescent
light
ç.cegsed into the
glareshield.
This light is controlled by rotating
the
GLARESHIELD
LT
dimmer, located below
the nav
indicãtors.
Rotating
the dimmer clockwise increases light
intensity,
and
rotating
the dimmer counterclockwise decreases light intensity.
Panel lighting is accomplished using individual lights mounted
in
each instrument and gauge. These lights are wired in parallel
and
are
controlled
by the PANEL LT dimmer, located below the
nav
Pilot control wheel lighting
is
accomplished by use of
a
rheostat
and light
assembly,
located
underneath
the pilot
control
wheel
yoke.
The light
provides downward illumination
from the bottom
of
the
Regardless
of the
light system
in
question,
the
most
probable
cause of
a
light failure is
a
burned out bulb.
However,
in the
event
any of the lighting systems fail to
illuminate
when turned on,
check
the
appropriate circuit breaker.
lf the
circuit breaker has
opened,
and there is no obvious
indication
of a shoft circuit
(smoke
or
odor),
turn off the light switch of the affected lights,
reset
the breaker,
and
turn the switch on again.
lf
the
breaker opens again, do not reset
it
CESSNA
MODEL
182S
SECTION 7
AIRPLANE
&
SYSTEMS DESCRIPTION
Nov
15/00
7-39
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