Cessna R182 - Page 141

CE!SSNA
MODEL
R182
SECTION
7
AII1PLANE
& SYSTEMS
DESCRIFTIONS
aviation
glade
straight
mineral
oil confolrring
to specification
No-
MIL-
L-6082.
'*.T
ENGINE
OIL
SYSTEM
oil
for engino
lubrication
and
propeller
governor
operation
is
supp-
lied
from
" ",rip
on
the
bottom
of the
engine.
The
capaciry
of the
sump.is.8
quarts
lone
aaditional
quart
is c_ontained
in
tbe engine
oil
filter).
oil
is
dirawn
fiom
the
sump
thiough
a
fitter screen
on
the end
of a
pickup tube
to
the
engine_driven
oir
pump.
oil
from the
pump
pas-ses
through
an_
oil
\,-
.
pressure
screen,
full
flow
oit
filter,
a
pressure
relief
valve
at ttre rear
of
the
iignt
oit
g"llery, and
a
thermostatically
controlled
remote
oil cooler.
Oil
from
the
iemoti
cooler
is tben
circulated
to the
left
gallery
and
propeller
govemor. The
engine
parts
are
then
lubricated
by
oil
from the
galleries.
After
lubricating
the
engiue,
the
oil returns
to
the sump
by
gravity. The
filter
adapter
iDl-the
full
flow
oil
filter
is
equipped
with a bypass
v-alve
wbich
will cause
lubricating
oil to bypass
tJre filter
in
the
event
the'filter
becomes
plugged, or
the
oil temperature
is
extremely
cold'
Section
8 of
this
bandbook.
remove
the
drain
hose.
/
I
IGN
ITION-STARTE
R
SYSTE
M
"
"f
the
fuel-air
mixture
with
dual
ignition'
Ignition
and
starter
operation
is controlled
by
a
rotary
type
switch
7-2L