Cessna 182 1978 - Cabin Headliners; Seat Repair; Soundproofing; Cabin Upholstery

MODEL
182
& T182 SERIES
SERVICE
MANUAL
3-54. REMOVAL AND INSTALLATION. soundproofing panel is placed in the gaps between
a. Remove bolts securing seat to cabin structure. wings and the fuselage, and is held in place by wing
b. Lift seat out.
root fairings.
c. Reverse preceding
steps for installation.
3-62. CABIN HEADLINERS.
(See figure
3-11.)
3-55.
AUXILIARY
SEAT.
(See figure
3-7, Sheet
5.)
-
3-63. REMOVAL
AND INSTALLATION.
3-56. DESCRIPTION.
The auxiliary seat consists
a. Remove sunvisors, all inside finish strips
and
of a
fixed, one-piece seat bottom and a fixed, one-
plates, overhead console, upper doorpost
shields
piece, seat back. The seat is secured to
brackets and any other visible retainers
securing the head-
mounted
in the floorboard.
liner.
b. Remove moulding
from fixed
windows.
3-57. REMOVAL AND INSTALLATION. c. Remove screws securing headliner and carefully
a.
Remove bolts securing seat to brackets
mounted take down the
headliner.
in floorboard. d. Remove spun glass soundproofing panels above
b. Lift seat out. the headliner.
c. Reverse
preceding steps
for installation.
NOTE
3-58. SEAT
REPAIR. Replacement
of defective
parts is
recommended in seat
repair. However,
a The lightweight
soundproofing
panels are
cracked framework may be welded,
provided the held in place
with industrial rubber cement.
crack
is
not located
in
an area
of stress
concentra-
e. Reverse
preceding
steps for
reinstallation.
tion (close to a
hinge or bearing point).
The square
tube
framework
is 6061
aluminum,
heat-treated
to
NOTE
a T-6 condition.
Heliarc welding should
be per-
formed
on
this tubing,
since torch
welding
will
Before
installation,
check
all items
concealed
destroy
the
heat-treatment
of the
aluminum
seat
by
headliner
for
security.
Use
wide cloth
tape
frame
structure.
Instructions
for
replacing
defec-
to
secure
loose
wires to
fuselage
skin
and to
tive cams
on
reclining
seat frames
are outlined
in
seal
openings
in wing
roots.
figure 3-8.
3-64. UPHOLSTERY
SIDE PANELS.
Removal
of
3-59.
CABIN
UPHOLSTERY.
Due to
the wide
selec-
upholstery
side panels
may be accomplished
by
tion
of fabrics,
styles and
colors,
it is
impractical
removing
seats
for access,
then
removing
parts
to describe
each
particular
type
of upholstery.
The
attaching
side panels.
Remove
screws,
retaining
paragraphs
which
follow,
describe
general
proce-
strips,
arm
rests and
ash trays
as
required
to free
dures
which
may be
used
as a guide
in
removal
and
upholstery
side panels.
Automotive-type
spring
installation
of
cabin
upholstery.
Major
work,
if
clips attach
most
door
panels.
A dull
putty
knife
possible,
should
be performed
by a
mechanic
experi-
makes
an excellent
tool for
prying clips
loose.
enced
in upholstery
replacement.
However,
if the
When
installing
side panels,
do not
over-tighten
work
must be
performed
by a mechanic
unfamiliar
screws.
Larger
screws
may be
used
in enlarged
with
upholstery
practices,
the
mechanic
should
make
holes
as
long as
area
behind
hole is
checked
for
carefully
detailed
notes
during
removal
of
each
item
electrical
wiring,
fuel
lines
and other
components
to
facilitate
reinstallation
or
replacement.
which
might
be
damaged
by
using
a longer
screw.
NOTE
Repair
kits
are available
for
the repair
of
partment
carpeting
is
held in
place by
Velcro
fas-
cracks
in ABS,
PBC,
PVCP,
graphite
and
teners
for quick
removal
and inspection.
When
fiberglass
material.
(Cessna
Supply
Division,
fitting
a new
carpet,
use
the old
carpet for
a pattern
P.O. Box
949,
Wichita,
KS 67201,
316/685-
for trimming
the carpet
and
for marking
screw
holes.
9111, Telex 417-489.)
3-66.
SAFETY
PROVISIONS.
3-60. MATERIALS
AND
TOOLS. Materials
and
3-66 SAFETY
PROVISIONS.
tools
will vary
with the
job to be
performed.
Scis-
3-67. CARGO
TIE-DOWNS.
(See
figure 3-12.)
sors
for trimming upholstery and a dull-bladed knife
Cargo tie-downs are utilized to ensure
that baggage
for wedging
material beneath retainer strips are the
cannot enter the seating area during flight.
Methods
only tools required for
most trim and upholstery
work. of attaching
the seating area during
flight. Methods
soundproofing
mats and fabric
edges in place. For
in the baggage area.
Sliding tie-down lugs
also uti-
repair
of glass-fiber constructed
components, refer
lize eyebolts
and attach to the seat rails.
A baggage
to Section 18 of this manual.
net
can be secured
to the
aft cabin wall
and floor
for
3-61. SOUNDPROOFING. The aircraft is insulated baggage security.
with
spun
glass,
mat-type
insulation
and a
sound-
3-68.
SEAT
BELTS.
(See figure
9.) Seat
belts
deadener compound applied to the inner surfaces
of used with the pilot and copilot
seats, or auxiliary
skin in most areas of
the cabin and baggage
compart- seat,
if installed, are attached
to fittings in the
ment. All soundproofing
material should be replaced floorboard.
The buckle half is inboard of each seat,
in its original position any
time it is removed. A
and the link half is outboard of each
seat. Seat belts
3-24 Revision 1