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CESSNA
MODEL
182S
SECTION
7
AIRPLANE &
SYSTEMS
DESCRIPTION
AIR
INDUCTION SYSTEM
lower cowl area.
An
open alternate
air
door
will
result
in
an
approximate
107o
power loss
at full throtile. After
passing
through
the air box,
induction air enters
a
fuel/air control unit ùnder
tñe
engine, and
is then
ducted
to the
engine cylinders through
intake
manifold tubes.
EXHAUST SYSTEM
Exhaust gas from each cylinder
passes
through riser
assemblies
to a
muffler and tailpipe. Outside
air is
pulled
ln
around
shrouds
which are constructed around the outsidè
of the
mufflers
to
form
heating chambers which supply
heat to
the cabin.
COOLING SYSTEM
Feb
3/97
7-23
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