CESSNA
MODEL R182
SECTION
7
AIIIPLANE
&
SYSTEMS DESCR,IPTIONS
If no
avionics
eguipment is to
be used
or
worked
on, the
avionics
power
switch should
be turned off.
If
maintenance
is required on
the avionics
equipment,
it is advisable
to
utilize
a battery cart external
power
source
to
prevent
damage
to the avionics equipment
by transient voltage.
Do
not
crank or start
the engine with
the
avionics
power
switch turned on.
Just before connecting
an
external
power
source
(generator
tSrpe
or
battery cart), the avionics
power
switch should
be turned
off, and the
master switch turned on.
.
The
ground
service
plug
receptacle
circuit incorporates
a
polarily
reversal
protection.
Power
from the
extemel
power
source will
flow only.if
the
ground
senjrice
plug
is correctly connicted to the
airplane.
If the
plug
is
accidentally connected
backwards,
no
power'will
flow
to
the
electrical
system,
thereby
preventing
any damage to
eleetrical
equipment.
-'('
The battery
and exter:nal
power
circuits have
been designed
to com-
\
pletely
eliminate
the need'to
"jumper"
across
the battery
contactor to close
it for charging
a completely
"dead"
batt€ry. A
special
fused
circuit in
the
external
power
system
supplies
tJre needed "jumper"
across
the contacts
so that with a
"dead"
battery
and an
external
power
source applled,
turnirrg
on
the master switch
will
close the battery contactor.
LIGHTING SYSTEMS
EXTERIOR LIGHTING
Conventional
navigation
lights
are located
on the wing
tips
and tail
stinger, and dual
landing
lights are installed
in the
cowl
nose cap.
Additional
lighting is available
and includes
a
strobe
light
on each wing
tip,
a flashing
beacon
on top of the vertical
stabilizer, and
two
courtesy
lights,
one
under each
wing,
just
outboard
of the cabin door.
The
courtesy
lights
are operated"by
a switch
located'bn
the left rear
door
post.
All
exterior lights, except
the courtesy lights,
are
controlled
by
rocker
type
"
switches
on
the left switch
and control
panel.
The
switches are
ON in the up
(
nsition and off
in the down
position.
The flashing
beacon should not be used when
flying through
clouds
or
system. The roceptacle is located
behind a door
on the left
side of the
fuselage
near the aft edge of
the
cowling.
NOTE
7-33