Raytheon Beech Baron E55 - Page 333

Raytheon
AiKraft
Company
BARON
55
AND
58
SHOP
MANUAL
Chant
2
Main
Landing
Gear
Wear
Tolerances
And
Inspection
Procedures
(TC-251,
TC-344,
TC-355
and
After;
TE-1
and
After;
TH-1 and
After)
(Continued)
ITEM
I,D.
O.D.
WEAR
TOLERANCES
AND
INSPECTION
PROCEDURES
Lower
(19)
1.8695
Visually
inspect
for
wear,
damage
and
1.8650
corrosion.
Replace
bearing
if
wear
tolerances
are
exceeded.
If
replacement
is
required,
remove
the
bearing
from
the
cylinder assembly
(9)
and
measure
the
O.D.
Select from
the
O.D.
dimensions
below
to
determine
the
correct
replacement bearing:
2.0035/2.0010
in.
(PM
35-815246-9
Standard
Bearing)
2.0185/2.0170
in.
(P/N
35-815246-27,
Oversize
Bearing)
If
the O.D. dimension
of
the
bearing
is
greater
than
the
replacement
dimensions
above,
replace
the
cylinder
assembly
(9).
If
additional
information
is
required,
contact the
Technical
Support
Department
of
Raytheon
Aircraft
Company,
P.O.
Box
85,
Wichita,
KS
67201.
If
replacement
of
bearing
is
required,
coat
bore
with
locquic
primer
(72,
Consumable
Materials
Chart,
Section
2)
and install
new
bearing
using
an
adhesive
(71,
Consumable
Materials
Chart,
Section
2).
Upper
Torque
Knee Attachment
0.5010
Visually
inspect
for
wear,
damage
and
Hole
0.4995
corrosion.
Replace
if
wear
tolerances
ate
exceeded.
Instruction
Placards
Do
not
remove
from
cylinder
assembly except
for
inspection
purposes
or
replacement.
Brace
Assembly
(11)
Visually
inspect
for
wear,
damage
and
corrosion.
Conduct
a
fluorescent
or
dye
penetrant
inspection
per
MIL-STD-6866.
Any
sign
of
cracks,
scratches
or worn
areas
which
can
not
be
repaired
is
cause
for
rejection.
Hinge
Bushings
Outer
Hinge
(12)
0.7192
Replace
bearings
when
main
landing
gear
is
0.7184
overhauled.
E22
SECTION
5
39