Cessna R182 - Page 144

SECTION
7
AIR,PLANE
& SYSTEMS
DESCIiPTIONS
CESSNA
MODEL
R182
knob clockwise
to
increase
RPM,
and counterclockwise
to
decrease
it.
To
make
rapid
or
large
adjustments,
depress
the
button
on
the
end of the
control
knob and
repositioD
the
control
as desired.
FUEL
SYSTEM
Fugl
flows
by
gravity from the two
w'ing tanks to
a four-position
selector
ve,lve,
labeled
BoTH,
RIGHT,
LEFT, and oFF.
With
tbe
selector
valve
in
either
the
BOTH,
RIGHT,
or
LEFT
position,
fuel
flows through
a
strainer
to
the
engine-driven
fuel
pumP'
and
from the
purnp
to
the
,
carburetor.
Wben
tbe
auxiliary
fuel
pump
is operating,
it
draws
fuel
from
a
(
tee
located
between
tbe
strainer
and tJre
engine-driven
fuel
pump,
and
'
delivers
it
to
the carburetor.
From
the carburetor,
mixed
fuel and air
flows
to'the
cylinders
through.:ibtake
manifold
tubes. Tbe
manual
prirner
draws
its
fuel,from
the
fuel
strainer
616
iniects
itr into the engine
intake
ports.
Fuel
system
venting
is essential
to system
operation.-
Complete
blockage
of
the venting
system
will
result
in collapsiag
of
tJre
bladder
FUEL OUANTITY
DATA
(U.
S.
GALLONS}
TANKS
TOTAL
USABLE
FUEL
ALL FLIGHT
CONDITIONS
TOTAL
UNUSABLE
FUEL
TOTAL
FUEL
VOLUME
STANDARD
(30.5
Gal.
Each)
56
5
61
LONG
RANGE
(40
Gal.
Each)
75
5
80
7-24
Figure
7-5. Fuel
Quantit5r
Data