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Cessna 150M - Cracks

Cessna 150M
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WOOD
REINFORCEMENT
B
ALWAYS DRILL END
OF
CRACK CUSHION
OF
RUBBER
TO
RELIEVE
STRAIN OR FABRIC
SOFT
WIRE
LACING
TEMPORARY
REPAIR
OF
CRACKS
CEMENTED
FABRIC PATCH
SANDING
REPAIR
Figure
3-1.
Repair
of
Windows
and
Windshield
pressure
and
cover
an
area
large
enough
to
prevent
formation
of
"bull's-eyes"
or
other
optical
distor-
tions.
ICAUTION\
Do not
use
a
coarse
grade
of
abrasive.
No.
320
is
of
maximum
coarseness.
b.
Continue
sanding
operation,
using
progressively
finer
grade
abrasives
until
scratches
disappear.
c.
When
scratches
have
been
removed,
wash
area
thoroughly
with
clean
water
to
remove
all
gritty
par-
ticles.
The
entire
sanded
area
will
be
clouded
with
minute
scratches
which
must
be
removed
to
restore
transparency.
d. Apply
fresh
tallow
or
buffing
compound
to
a
motor-driven
buffing
wheel.
Hold
wheel
against
plas-
tic
surface,
moving
it
constantly
over
damaged
area
until
cloudy
appearance
disappears.
A
2000-foot-per-
minute
surface
speed
is
recommended
to
prevent
overheating
and
distortion.
(Example:
750
rpm
polishing
machine
with
a 10
inch
buffing
bonnet.
)
NOTE
Polishing
can
be
accomplished
by
hand
but
will
require
a
considerably
longer
period
of
time
to
attain
the
same
result
as
pro-
duced
by a buffing
wheel.
e.
When
buffing
is
finished,
wash
area
thoroughly
and
dry
with
a
soft
flannel
cloth.
Allow
surface
to
cool
and
inspect
area
to
determine
if
full
transpar-
ency
has
been
restored.
Apply a
thin
coat
of
hard
wax
and
polish
surface
lightly
with
a
clean
flannel
3-2
cloth.
NOTE
Rubbing
plastic
surface
with
a
dry
cloth
will
build
up
an
electrostatic
charge
which
attracts
dirt
particles
and
may
eventually
cause
scratching
of
surface.
After
wax
has
hardened,
dissipate
this
charge
by
rub-
bing
surface
with
a
slightly
damp
chamois.
This
will
also
remove
dust
particles
which
have
collected
while
wax
is
hardening.
f. Minute
hairline
scratches
can
often
be
removed
by
rubbing
with
commercial
automobile
body
clean-
er
or
fine-grade
rubbing
compound.
Apply
with
a
soft,
clean,
dry
cloth
or
imitation
chamois.
3-8.
CRACKS.
(Refer
to
figure
3-1.)
a.
When
a
crack
appears,
drill
a hole
at
end of
crack
to
prevent
further
spreading.
Hole
should
be
approximately
1/8
inch
in
diameter,
depending
on
length
of
crack
and
thickness
of
material.
b.
Temporary
repairs
to
flat
surfaces
can
be
ac-
complished
by
placing
a
thin
strip
of wood
over
each
side
of
surface
and
inserting
small
bolts
through
wood
and
plastic.
A
cushion
of
sheet
rubber
or
air-
craft
fabric
should
be
placed
between
wood
and
plas-
tic
on
both
sides.
c.
A
temporary
repair
can
be
made
on
a
curved
surface
by
placing
fabric
patches
over
affected
areas.
Secure
patches
with
aircraft
dope,
Specification
No.
MIL-D-5549;
or
lacquer,
Specification
No.
MIL-L-
7178.
Lacquer
thinner,
Specification
No.
MIL-T-
6094
can
also
be
used
to
secure
patch.

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