Cessna T182 Series User Manual

MODEL
182 & T182 SERIES
SERVICE MANUAL
*3 \
*
2. Engine
Mount
' I
2 ^ 1 1
3. Washer
6
/ I
4. Firewall
/
1
>"
'
l /
I ,5.
Nut/
3\ "/ 3
6.
Shock
Mount
Pad
7. Barrel Nut
8.
Roll
Pin
12
3
9. Spacer
MOUNT-TO-FIREWALL
10. Ground Strap *10
11.
Lockwasher
6
TORQUE
MOUNT-TO-FIREWALL
12. Washer
11
BOLTS TO 160-190 LB-IN. *10
· Washer (3) is
installed on
NGINE-TO-MOUNT
the lower mounts only.
* THRU
18268106
TORQUE
ENGINE-TO-MOUNT
18268107
& ON
BOLTS
TO
450-500
LB-IN
* 18268107 & ON
Figure 11-2. Engine Mount Details
11-29. REMOVAL AND INSTALLATION. Removal 11-35. PAINTING. Refer to Section 19 of this man-
and installation of the various
baffle segments is pos- ual
for painting procedures.
sible with the cowling removed. Be sure that any re-
placed baffles and seals are installed correctly and 11-36. ENGINE SHOCK-MOUNT PADS. (See
that they seal
to direct the airflow
in the correct di-
figure 11-2.) The bonded
rubber and metal
shock-
rection. Various lines, hoses, wires and
controls mounts are designed to reduce
transmission of en-
are
routed through some
baffles. Make sure that
gine vibrations
to the airframe. The
rubber pads
these
parts are reinstalled correctly after installa-
should be wiped clean with a clean
dry cloth.
tion of baffles.
NOTE
11-30. REPAIR. Repair of an individual segment of
engine baffle
is generally impractical,
since,
due to
Do not clean
the rubber
pads and dampener
the small size
and formed
shape of the part,
replace-
assembly
with any type
of cleaning solvent.
ment is usually more economical. However, small
cracks
may be stop-drilled
and a
reinforcing doubler
Inspect
the metal parts
for cracks and
excessive wear
installed.
Other repairs may
be made as long as
due to aging and
deterioration. Inspect
the rubber
strength
and cooling requirements
are met. Replace
pads for separation
between the pad and
metal backing,
sealing
strips if they
do not seal properly.
swelling,
cracking or
a pronounced set
of the pad.
Install
new parts
for all
parts that
show evidence
of
11-31.
ENGINE
MOUNT.
(See figure
11-2.)
wear
or damage.
11-32.
DESCRIPTION.
The
engine mount
is com-
11-37.
ENGINE
OIL SYSTEM.
posed of sections
of steel tubing welded
together and
reinforced
with
gussets.
The
mount is
fastened
to
11-38.
DESCRIPTION.
A wet-sump,
pressure-
the fuselage
at four
points.
The engine
is
attached
lubricating
oil
system
is employed
in the engine.
to the
engine
mount
with
shock-mount
assemblies
Refer
to applicable
engine
manual
for
specific
de-
which
absorb
engine
vibrations.
Each
engine
mount
tails
regarding
engine
oil system.
pad has a small
hole for a locating
pin which serves
as a locating
dowel
for the
engine shock-mounts.
WARNING
11-33.
REMOVAL
AND INSTALLATION.
The
U.S. Environmental
Protection
Agency
a.
Remove
engine
in accordance
with paragraph
advises
that mechanics
and other
workers
11-17.
who handle
engine
oil
are advised
to
b. Remove
bolts from
upper and lower
mount-to-
miniTnmz
skin contact
with used
oil and
fuselage
structure and
carefully
remove engine
mount.
promptly
remove
used oil
from the
skin. In a
c. Reverse
the preceding
steps
for reinstallation.
laboratory
study. mice
developed
skin cancer
Torque
bolts
to 160-190
Ib-in.
Reinstall
engine
in
after skin
was
exposed
to used
engine
oil
accordance with paragraph
11-22.
twice
a week without being
washed off, for
most of
their life
span. Substance
found to
11-34.
REPAIR. Refer to Section
18 of this manual
cause cancer
in laboratory animals
may also
for
repair procedures.
cause cancer in
humans.
11-14

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)