Cessna T182 Series User Manual

MODEL 182
& T182 SERIES SERVICE
MANUAL
NOTE
6. Exhaust
gas temperature
wire at quick-
disconnect.
During the following procedures. remove any 7. Remove all clamps and lacings attaching
clamps or lacings
which secure controls. wires
or cables to engine, and pull wires and cables
wires,
hoses or lines to the engine.
engine aft to clear
engine.
mount or attached
brackets. so they will not
p. Disconnect lines and hoses as follows:
interfere with
engine removal.
Some of the
1. Vacuum
hose at vacuum
pump.
items listed can be disconnected
at more 2. Oil breather
vent lines where secured to the
than one place. It may be desirable to dis- engine.
connect some
of these items at other than
WARNING
the places
indicated. The reason
for engine
removal
should
be
the
governing
factor
in
removal should be the governing factor in Residual fuel and oil draining from discon-
deciding at which point to disconnect
them.Residual fuel
and hoses
Omitany of the items which are not presentes
on a particular engine installation.
of such
fuel and oil when
lines or hoses are
g. Drain the engine oil sump and oil cooler. disconnected.
h. Disconnect
magneto
primary
lead wires
at
6.
Oil pressure line
at engine fitting.
The magnetos
are in a SWITCH ON condition
7. Manifold pressure line at engine.
when the switch wires
are disconnected.
q. Carefully
check the engine again
to ensure ALL
Ground the magneto
points or remove the hoses,
lines, wires, cables, clamps and lacings
high tension
wires from
the magnetos
or
which would
interfere with
the engine removal
are
spark plugs
to prevent
accidental
firing,
disconnected
or
removed.
Ensure
all wires.
cables
and
engine controls have
been pulled aft to clear
the
i.
Remove the spinner and propeller
in accordance
engine.
with Section
13. Cover exposed end of crankshaft
flange
and propeller flange to
prevent entry of foreign
material.
Place
suitable stand
under tail tie-down
ring
j. Disconnect
throttle
and mixture
controls at car-
before
removing
engine. The loss
of engine
buretor. Remove
clamps attaching
controls to engine
weight will cause
the aircraft to be tail
heavy.
and pull controls
aft clear of engine.
Use care to
avoid
bending
controls
too sharply.
Note
EXACT
r.
Attach
a hoist
to
the lifting
lug
at the
top center
position, size
and number
of attaching washers
and
of the engine
crankcase. Lift
engine just enough
to
spacers
for reference on
reinstallation.
relieve the
weight from the engine
mount pads.
k. Disconnect propeller
governor control
at gover- s.
Remove bolts attaching
engine to engine mount
nor.
Note
EXACT
position,
size
and
number
of
pads
and
slowly
hoist
engine
and pull
it
forward.
attaching
washers
for reference
on reinstallation.
Check
for any items
which would interfere
with the
Remove clamps
attaching control to
engine and pull
engine removal Balance
the engine by hand
and
control
aft
clear
of engine.
carefully
guide
the disconnected
parts out
as
the
1. Disconnect
all
hot and
cold
air
flexible
ducts
and
engine
is removed.
remove.
t. Remove
engine
shock-mount
pads
and bonding
m.
Remove exhaust system in
accordance with para-
straps.
graph 11A-69.
n. Disconnect
carburetor
heat control
from arm on
11A-18.
CLEANING.
Refer to Section
2.
airbox.
Remove clamps and
pull control clear
of
engine.
11A-19.
ACCESSORIES
REMOVAL.
Removal of
o. Disconnect
wires and cables
as follows:
engine
accessories
for overhaul
or for engine
re-
1.
Tachometer
drive shaft
at adapter.
placement
involves stripping
parts,
accessories
and components
from the engine
to reduce it to the
removed should be tagged for repair or replacement
When
disconnecting
starter cable
do not
as
required.
permit starter terminal bolt to rotate.
Rotation
of the bolt could
break the con-
NOTE
ductor between bolt and field coils causing
the starter
to be
inoperative.
Items easily
confused
with similar
items
should be tagged to provide a means of
2.
Starter
electrical
cable at starter.
identification
when being
installed
on a
3.
Cylinder
head temperature
wire
at probe.
new
engine.
All openings
exposed
by
the
4. Carburetor
air temperature wires at quick-
removal of an item should be
closed by
disconnects.
installing
a suitable cover, cap or tape
5.
Electrical
wires and
wire shielding
ground
at
over the
opening.
This will
prevent
entry
alternator. of foreign material.
11A-10

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)