Raytheon Beech Baron E55 - Page 300

Raytheon
AiKraft
Company
BARON
55
AND
58
SHOP
MANUAL
13
11 12
2
o
o
4
O
y
I.
CYLINDER
2.
PISTON
8
5
3.
FRICTTON
RING
3
4.
INSULATOR
11
10
5.
PRESSURE
PLATE RSSEMBLV
6.
BACK
PLATE
ASSEMBIV
O
Q
O
16
7.
"0"
RING
’llhl
17
LININGSHIM-BACK
PCAiE
10. ANCHOR
BOLT
15’
-‘1
4
Il.
NUT
m
12. BOLT
O
13. WASHER
14.
CAP,
BLEEDER
9
15. SCREW.
BLEEDER
16. "0"
RING
6
17.
SEAT,
BLEEDER
18.
TORC3UE
PLATE
ASSEMBLY
O
18
ss-21a-13
Cleveland
Heavy
Duty
Brake
Assembiy (Optional)
Figure
3
WHEEL
AND
TIRE
REPAIR
Smooth
wheel
abrasions,
nicks and burrs
with
a
fine
file
and
retouch with
zinc chromate
primer
and
aluminum
lacquer
to
prevent
corrosion.
Replace
any
damaged
wheel
parts.
Replace
tire
casings
showing
breaks,
blisters,
or
excessive
wear.
In
service,
tire
carcasses
grow
slightly
due
to
shock loads
in
landing. Normally,
this
growth
is
balanced
by
tread
wear
so
there is
no
increase
in tire
diameter.
Raytheon
Aircraft
Company
cannot
recommend the
use
of
recapped
tires
on
the Baron
models. The
tires
may pass
the
retraction
test
when
first
installed; however,
recapped
tires
have
a
tendency
to
swell after
use
and
may
cause
malfunction of
the
retract
system
or
damage
the
landing
gear
doors.
REMOVING
AND
INSTALLING
THE
BRAKE
MASTER
CYLINDERS
a.
Close
parking
brake
valve
by pulling
parking
brake
handle.
b.
Unsnap
the floor
mat
and
remove
the floorboard
section
below
the
brake
pedals.
c.
Disconnect the
two
brake
hydraulic
lines
at
each
master
cylinder
and
mark the lines
to
assure
correct
installation.
d. Remove the
master
cylinder
attaching
bolts and
nuts
and
remove
the
master
cylinders.
e.
If
new
master
cylinders
are
to
be
installed,
note
the
positions
of
the
master
cylinder
45-degree
elbow
fittings.
f. Install the
master
cylinders
by reversing
the
removal
procedure.
g.
Replenish
and bleed
the brake
hydraulic
system.
Jun
30/04Page
6
SECTION
5
522