Cessna R182 - Page 143

CESSNA
MODEL R182
SECTION
7
AIRPLANE & SYSTEMS
DESCRIPTIONS
m&nual
prirner.
The
primer
is actually a small
pump
which
draws
fuel
from the
frlel
strainer
when the
pluuger
is
pulled
out, and
injects it
into the
engine
intake
ports
when the
plunger
is
pushed
back in.
Ttre
plunger
is
equipped
with a lock and, after being
pushed
full in, mustbe rotated either
1
left or
right until the
knob cannot be
pulled
out.
COOLING
SYSTEM
Ram
air for engine
cooling
enters through
two intake openings
in the
front
of
the
eugine
cowling.
The cooling air is directed
through the
remote
oil
cooler
(behind
the left
intake opening), and
around the cylinders
and
other
areas of
the engine
by baffling,
and is then exhausted
through
powl
'
right
to clear
a detent,
then moving
the lever up
to the
OPEN
position.
Anytime
the lever
is repositioned,
it
must first be
moved to the
right.'Uhttg
should
usted
to keep
t4g
eyliqeslhegd
of ther
r_$bgql4.
be-som:
he CLOSED
A
winterization
kit
is available and'consists
of
two clips
and two
bafflep,which,attach
to
the air intakes
in the
cowling
nose cap,
and a
placard
to be
installed on
the instrument
panel.
This
equipment
should be
installed
for
operations
in temperatures
consistently
below
-7"C
(20'F).
PROPELLER
The
airplane
has an
all-metal,
two-bladed, gonstant-speed;
governor-
regulated
propeller.
A setting
introduced
into the
governor with the
propeller
control
establishes
the
propeller
speed,
and thus
the engine
speed
to
be .maintained.
The
governor
tben controls
flow of engine
oil'
boosted
to
high
by
the
governing;itrmp,
to or
ffgm a
piston
in
the
propeller hub.
on the
piston
twists
the
blades toward
-EETAL
A
control
knob
on the
lower
center
portion
of
the instrument
panel
is
used
to
set the
propeller
and control
engine
RPM
as desired
for various
towa
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