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Cessna 150M - Nose Gear Shock Strut; Nose Gear Shimmy Dampener; Hydraulic Brake Systems; Cleaning

Cessna 150M
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NOTE
Recommended
tire
pressures
should
be
main-
tained.
Especially
in
cold
weather,
remember
that
any
drop
in
temperature
of
the
air
inside
a
tire
causes
a
corresponding
drop
in
air
pres-
sure.
2-26.
NOSE GEAR SHOCK
STRUT.
The
nose
gear
shock
strut
requires
periodic
checking
to
ascertain
that
the
strut
is
filled
with
hydraulic
fluid
and
is
in-
flated
to
the
correct
air
pressure.
To
fill
the
nose
gear
strut
with
hydraulic
fluid
and
inflate
with
air,
proceed
as
follows:
'
a.
Remove
filler
valve
cap
and
depress
valve
core
to
completely
deflate
nose
strut.
b.
Remove
filler
valve
from
strut.
c.
With
nose
gear
strut
compressed
to
its
shortest
length,
fill
strut
with
hydraulic
fluid
to
the
bottom
of
the
filler
hole.
d.
Raise
nose
of
aircraft,
extend
and
compress
strut
several
times
to
expel
any
entrapped
air,
then
lower
nose
of
aircraft
and
repeat
step
"c".
e.
With
strut
compressed
to
its
shortest
length,
install
filler
valve
assembly.
f.
With
nose
wheel
off
ground,
inflate
strut.
Shock
strut
pressure
is
listed
in
figure
1-1.
NOTE
The
nose
landing
gear
shock
strut
will
nor-
mally
require
only
a
minimum
amount
of
service.
Maintain
the
strut
extension
pres-
sure,
as
shown
in
figure
1-1.
Lubricate
landing
gear
as
shown
in
figure
2-5.
Check
the
landing
gear
daily
for
general
cleanli-
ness,
security
of
mounting,
and
for
hydrau-
lic
fluid
leakage.
Keep
machined
surfaces
wiped
free
of
dirt
and
dust,
using
a
clean
lint-free
cloth
saturated
with
MIL-H-5606
hydraulic
fluid
or
kerosene.
All
surfaces
should
be
wiped
free
of
excessive
hydraulic
fluid.
2-27.
NOSE GEAR SHIMMY
DAMPENER.
The
shimmy
dampener
should
be
serviced
at
least
every
1
5
0
hours.
The
shimmy
dampener
must
be
filled
completely
with
flUid,
free
of
entrapped
air,
to
serve
its
purpose.
To
service
the
shimmy
damp-
ener,
proceed
as
follows:
a.
Remove
shimmy
dampener
from
aircraft.
b.
While
holding
the
dampener
in
a
vertical
posi-
tion
with
fitting
end
pointed
downward,
pull
fitting
end
of
the
dampener
shaft
to
its
limit
of
travel.
c.
While
holding
dampener
in
this
position,
fill
dampener
through
open
end
of
cylinder.
d.
Push
the
shaft
upward
slowly
to
seal
off
the
fil-
ler
hole.
e.
Clean
dampener
with
solvent.
Be
sure
to
keep
the
shaft
protruding
through
the
filler
hole
until
dampener
is
installed
on
the
aircraft.
£.
Install
dampener
on
aircraft.
NOTE
Keep
shimmy
dampener,
especially
the
ex-
posed
portions
of
the
dampener
piston
shaft,
clean
to
prevent
collection
of
dust
and
grit
which
could
cut
the
seals
in
the
dampener
barrel.
Keep
machined
surfaces
wiped
free
of
dirt
and
dust,
using
a
clean
lint-free
cloth
saturated
with
MIL-H-5606
hydraulic
fluid
or
kerosene.
All
surfaces
should
be
wiped
free
of
excessive
hydraulic
fluid.
2-28.
HYDRAULIC BRAKE SYSTEMS.
Check
brake
master
cylinders
and
refill
with
hydraulic
fluid
as
specified
in
the
inspection
charts.
Bleed
the
brake
system
of
entrapped
air
whenever
there
is
a spongy
response
to
the
brake
pedals.
Refer
to
paragraph
5-58
for
filling
and
bleeding
the
brake
system.
2-29.
CLEANING.
2-30.
Keeping
the
aircraft
clean
is
important.
Be-
sides
maintaining
the
trim
appearance
of the
aircraft,
cleaning
lessens
the
possibility
of
corrosion
and
makes
inspection
and
maintenance
easier.
2-31.
WINDSHIELD AND WINDOWS
should
be
cleaned
carefully
with
plenty
of
fresh
water
and
a
mild
detergent,
using
the
palm
of the
hand
to
feel
and
dislodge
any
caked
dirt
or
mud.
A
sponge,
soft
cloth,
or
chamois
may
be
used,
but
only
as
a
means
of
carrying
water
to
the
plastic.
Rinse
thoroughly,
then
dry
with
a
clean
moist
chamois.
Do
not
rub
the
plastiC
with
a
dry
cloth
as
this
builds
up
an
electro-
static
charge
which
attracts
dust.
Oil
and
grease
may
be
removed
by
rubbing
lightly
with
a
soft
cloth
moistened
with
Stoddard
solvent.
I~AUTION\
Do not
use
gasoline,
alcohol,
benzene,
acetone,
carbon
tetrachloride,
fire
extinguisher
flUid,
de-icer
flUid,
lacquer
thinner,
or
glass
window
cleaning
spray.
These
solvents
will
soften
and
craze
the
plastic.
After
washing,
the
plastic
windshield
and
windows
should
be
cleaned
with
an
aircraft
windshield
cleaner.
Apply
the
cleaner
with
soft
cloths
and
rub
with
mod-
erate
pressure.
Allow the
cleaner
to
dry,
then
wipe
it
off
with
soft
flannel
cloths.
A thin,
even
coat
of
wax,
polished
out
by
hand
with
soft
flannel
cloths,
will
fill
in
minor
scratches
and
help
prevent
further
scratching.
Do not
use
a
canvas
cover
on
the
wind-
shield
or
windows
unless
freezing
rain
or
sleet
is
anticipated
since
the
cover
may
scratch
the
plastic
surface.
2-32.
PLASTIC TRIM.
The
instrument
panel,
plas-
tic
trim,
and
control
knobs
need
only
be
wiped
with
a
damp
cloth.
Oil
and
grease
on
the
control
wheel
and
control
knobs
can
be
removed
with
a
cloth
moist-
ened
with
Stoddard
solvent.
Volatile
solvents,
such
as
mentioned
in
paragraph
2-31,
must
never
be
used
since
they
soften
and
craze
the
plastic.
2-33.
PAINTED SURFACES. The
painted
exterior
surfaces
of the
aircraft,
under
normal
conditions,
require
a
minimum
of
polishing
and
buffing.
Approxi-
mately
15
days
are
required
for
acrylic
or
lacquer
paint
to
cure
completely;
in
most
cases,
the
curing
Change
3
2-9

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