Cessna T188C - Removal and Installation; Repair; Engine Mount; 11-30. Description

MODEL 188 & T188 SERIES SERVICE MANUAL
Inspect
baffles
for
cracks
in
the
metal
and for
loose
11-26.
REPAIR.
Refer
to Section
17.
and/or torn seals. Repair or replace any defective
parts.
11-27.
PAINTING.
Refer
to Section
18.
11-22. REMOVAL
AND INSTALLATION.
Removal 11-28.
ENGINE SHOCK-MOUNT PADS.
(See
and installation
of the
various
baffle segments
is
figure
11-1.)
The
bonded
rubber
and metal
shock-
possible
with
the cowling
removed.
Be sure
that any
mounts
are designed
to reduce
transmission
of
engine
replaced
baffles and
seals are
installed
correctly
vibrations
to
the airframe.
The
rubber pads
should
and
that they seal
to direct the
airflow in
the correct
be wiped
clean with a clean
dry cloth.
direction.
NOTE
11-23. REPAIR. Baffles ordinarily should be re-
placed if damaged or cracked. However, small plate Do not clean the rubber pads and dampener
reinforcements riveted
to the baffle will often prove
assembly with any
type of cleaning solvent.
satisfactory both
to the strength
and cooling
require-
ments of the unit.
Inspect the metal parts for
cracks and excessive
wear due to aging and deterioration. Inspect the
11-24. ENGINE MOUNT. (See figure 11-1.) rubber pads for separation between the pad and
The engine
mount is
comprised of sections
of tubing
metal backing,
swelling,
cracking or
a pronounced
welded
together
and reinforced
with welded
gussets.
set
of the pad.
Install
new parts
for all parts
that
The purpose
of the
mount
is to support
the
engine and
show
evidence
of wear
or damage.
attach it to the
airframe. Each
engine mount
pad has
a small
hole
for a locating
pin
which
serves as
a
11-29.
ENGINE
OIL
SYSTEM.
locating dowel for the engine shock-mounts.
11-30. DESCRIPTION. A wet-sump, pressure-
11-25. REMOVAL AND INSTALLATION. lubricating oil system is employed on this engine.
a. Remove engine in accordance with paragraph Refer to applicable engine, manufacturer's overhaul
11-11.
..
manual
for
specific
details
and
descriptions.
b. Remove bolts
from upper
and lower
mount-to-
fuselage structure and carefully remove engine mount.
c. Reverse the
preceding
steps for reinstallation.
Torque bolts to 160-190 lb-in. Reinstall engine in
accordance
with paragraph
11-16.
SHOP NOTES:
11-11