Cessna T182 Series User Manual

MODEL
182
&
T182
SERIES
SERVICE
MANUAL
Turn
adjusting
screw
OUT
(counterclockwise)
for a
box. Inspect
gaskets
and install
new gaskets,
if dam-
richer
mixture.
aged.
Check manually-operated
air door
for
ease of
f. If
mixture
is set
too RICH,
engine
speed
will
operation
and
proper
rigging.
increase
above
25
RPM.
thus
requiring
a
leaner
mixture.
Turn
adjusting
screw IN
(clockwise)
for
11-65A.
INSTALLATION
OF INLET
DUCTS.
When
a leaner mixture. cutting duct assembly to length, the support wire
should
be out
back far enough
to bend
back (mini-
NOTE
mum bend radius
1.8 inch) under
the clamp and pro-
trude
1/4 inch.
Do
not break
the
bond between
wire
After each adjustment
to the
idle mixture,
and fabric.
Before tightening
clamps,
make sure there
run engine up to approximately
2000 RPM
is no twist
or torque on hose.
If hose is wrapped
to
clear engine of
excess fuel to
obtain a
with
MIL-Y-1140 cord
in place of wire
support, the
correct idle speed.
same
installation
procedure applies
except; MIL.Y-
1140 has no minumum
bend radius requirement.
11-61.
INDUCTION
AIR
SYSTEM.
The minimum
installed
bend
radius
for wire
11-62.
DESCRIPTION.
Ram air enters
the
induc-
supported
hose in
the plane
of bend is
as
tion air system through a filter at the front of the follows:
lower cowling and is ducted to the airbox
at the car- 1. Neoprene, one-ply hose
-1/4 diameter of the
buretor. From
the induction airbox
the filtered
air maximum
hose dimension.
is directed
to the inlet
of the carburetor,
mounted
2.
Neoprene, two-ply
hose and silicone,
one-ply
on the
lower side
of the engine,
through
the carbure-
hose
-1/3 diameter
of the maximum
hose
dimension.
tor, where
fuel is mixed
with the
air, to the
intake
4. Silicone,
two-ply
hose -
1/2 diameter
of the
manifold.
From
the intake
manifold,
the fuel-air
maximum
hose
dimension.
mixture
is distributed
to
each
cylinder
by
separate
intake
pipes.
The
intake
pipes
are attached
to the
11-66.
INDUCTION
AIR
FILTER.
manifold
with
hoses
and
clamps
and
to
the cylinder
with
a four
bolt
flange
sealed
with
a gasket.
A butter-
11-67.
DESCRIPTION.
An
induction
air
filter,
fly
valve,
located
in the
airbox,
may
be operated
mounted
at the
induction
air
inlet
on the
front
of the
manually
from
the
cabin
to permit
the
selection
of
lower
cowling,
removes
dust
particles
from
the
ram
either
cold
or heated
air.
When
the
induction
air
door
air
entering
the
engine.
is closed,
heated air
is drawn from
a shroud
on the
left
exhaust
stack
assembly.
11-68.
REMOVAL
AND
INSTALLATION.
a.
Remove
screws
securing
filter
cover,
release
11-63.
AIRBOX.
the
quick-release
fasteners
securing
the
filter
assem-
bly and lift filter
out of nose
cap.
11-64.
REMOVAL
AND
INSTALLATION.
b.
Reverse
the
preceding
steps
for
reinstallation.
a. Remove
engine
cowling
in accordance
with
para-
graph 11-3.
b.
Disconnect
flexible
duct
from
left
side
of airbox.
inspect
filter
in accordance
with
instructions
in
c.
Disconnect
boot
from
forward
end
of
airbox.
Section
2.
d.
Disconnect
carburetor
heat
control
at arm
on
NOTE
right
side
of airbox
and
remove
clamp
securing
con-
e. Remove
mounting
bolt safety
wire,
remove bolts
filter gasket
becomes
loose,
and
gasket
and
carefully
remove
airbox.
bond
with
EC-1300L
or
equivalent.
f.
Reverse
the
preceding
steps
for
reinstallation.
Rig
carburetor
heat
control
in
accordance
with
para-
11-70.
IGNITION
SYSTEM.
graph
11-86.
11-71.
DESCRIPTION.
The
ignition
system
is com-
11-65.
CLEANING
AND
INSPECTION.
Clean
metal
prised
of two
magnetos,
two
spark
plugs
in
each
cyl-
parts
of
the
induction
air
box
with
Stoddard
solvent
inder,
an
ignition
wiring
harness,
an
ignition
switch
or
equivalent.
Inspect
for
cracks,
dents,
loose
mounted
on
the
instrument
panel
and
required
wiring
rivets,
etc.
Minor
cracks
may
be stop-drilled.
In
between
the
ignition
switch
and
magnetos.
case
of continued
or severe
cracking,
replace
air
SHOP
NOTES:
Revision 1 11-23

Cessna T182 Series Specifications

General

Engine Type	Lycoming IO-540-AB1A5
Horsepower	230 hp
Seating Capacity	4
Service Ceiling	18, 100 feet
Takeoff Distance	1, 600 feet
Landing Distance	1, 350 ft
Type	Single-engine
Max Takeoff Weight	3, 100 lb
Wingspan	36 ft
Length	29 ft
Height	9 feet 3 inches
Fuel Capacity	92 US gal (348 L)