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Cessna 150M - Rear View Mirror Installation; Upholstery Side Panels; Carpeting; Baggage Compartment Upholstery

Cessna 150M
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1.
Cover
2.
Mirror
3.
Grommet
4. Nut
5.
Washer
6.
Deck
Skin
7.
Glare
Shield
2
3
THRU 15073658, A1500342,
F15000864 AND FA1500166
2
6
BEGINNING WITH 15073659,
A1500343,
F15000864 AND
FA1500167
Figure
3-9.
Rear
View
Mirror
Installation
3-41.
UPHOLSTERY SIDE PANELS.
Removal
of
upholstery
side
panels
is
accomplished
by
removing
seats
for
access,
then
removing
parts
attaching
panels.
Remove
screws,
retaining
strips,
arm
rests
and
ash
trays
as
required
to
free
the
various
panels.
Automotive
type
spring
clips
attach
most
door
panels.
A dull
putty
knife
makes
an
excellent
tool
for
prying
the
clips
loose.
When
installing
up-
holstery
side
panels,
do not
over-tighten
sheet
metal
screws.
Larger
screws
may
be
used
in
enlarged
holes
as
long
as
the
area
behind
the hole
is
checked
for
electrical
wiring,
fuel
lines
and
other
compon-
ents
which
might
be
damaged
by
using
a
longer
screw.
3-42.
CARPETING.
Cabin
area
and
baggage
com-
partment
carpeting
is
held
in
place
by
rubber
cement,
sheet
metal
screws
or
retaining
strips.
When
fitting
a new
carpet,
use
old
one
as
a
pattern
for
trimming
and
marking
screw
holes.
3-43.
BAGGAGE COMPARTMENT UPHOLSTERY.
A
washable
plastic
held
in
place
by
screws
and
retain-
ers
is
used
in
the
baggage
compartment.
Cargo
tie-
down
and/or
seat
belt
brackets
must
be
removed
as
necessary
to
facilitate
upholstery
removal.
3
-44.
SAFETY
PROVISIONS.
3-45.
CARGO TIE-DOWNS.
Cargo
tie-downs
are
SHOP
NOTES:
used
to
ensure
baggage
cannot
enter
seating
area
during
flight.
A
baggage
net
can
be
secured
to
aft
cabin
wall
and
cabin
floor
for
baggage
security.
3
-46.
SAFETY
BELTS.
Safety
belts,
bolted
to
the
cabin
structure
are
provided
for
each
seat.
Belts
should
be
replaced
if
frayed
or
cut,
latches
are
de-
fective
or
stitching
is
broken.
Attaching
parts
should
be
replaced
if
excessively
worn
or
defective.
Refer
to
figure
3
-8.
I
3-47.
SHOULDER HARNESS.
Shoulder
harnesses
may
be
installed
in
the
aircraft.
The
latches
re-
quire
no
lubrication.
Component
parts
should
be
re-
placed
as
outlined
in
preceding
paragraph.
Refer
to
figure
3-8.
I
3-48.
INERTIA
REEL
SHOULDER HARNESS.
Beginning
with 15075782
and
F15001134
Inertia
reel
shoulder
harnesses
may
be
installed.
The
in-
ertia
reel
allows
free
movement
for
the
seat
occu-
pant
but
will
lock
when
subjected
to
a
sudden
load.
Proper
operation
of
the
reel
can
be
checked
by
ap-
plying
a
quick
jerk
to
the
belt,
inertia
reel
should
lock
and hold.
Figure
3 -8
sheet
2
may
be
used
as
a I
guide
for
removal
and
imtallation.
3-48.
REAR VIEW MIRROR. A
rear
view
mirror
may
be
installed
on
the
cowl
deck
above the
instru-
ment
panel.
Figure
3 -9
illustrates
details
and
may
be
used
as
a guide
for
removal
and
installation.
Change
3 3
-15/(3
-16 blank)

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