Raytheon Beech Baron E55 - Page 345

RByfheOR
AiKraft
Company
BARON
55
AND
58
SHOP
MANUAL
Chart
3
Nose
Gear Wear
Tolerances
and
Inspection
Procedures
(TC1
and
After;
TE-1 thru
TE-300)
(Continued)
ITEM
I.D.
O.D.
WEAR
TOLERANCES
AND
INSPECTION
PROCEDURES
Axle
(52)
1.249
Visually
inspect
for
wear,
damage
and
corrosion.
Any
sign
of
1.248
scratches and
worn
areas
which
can
not
be
repaired
is
cause
for
rejection.
Conduct
a
magnetic
particle
inspection
per
Mlt-
STD-1949.
Any
sign
of
cracking
is
cause
for
rejection.
Strip
and
cadmium
plate
axle
as
necessary,
per
Fed
OQ-P-416,
Type
II,
Class
2
on
scratched
or
wom
areas.
Brace
Assembly
(15)
Visually
inspect
for
wear,
damage
and
corrosion.
Any
scratches
or
worn
areas
which
can
not
be
repaired
is
cause
for
rejection.
Remove
all
bearings
and
inspect
for corrosion.
Conduct
fluorescent
or
dye
penetrant
inspection
per
MIL-STD-6866.
Any
crack
is
cause
for
rejection.
Coat
interior
of
brace
and
hinge
bearing
holes with corrosion
preventative
compound
per
MIL-
C-16173,
Grade
1
or
2.
Replace
all
bearings
when
nose
gear
is
overhauled.
Hinge
Bushings
(12)
0.4692
Replace bearings
when
nose
gear
is
overhauled.
Alignment
0.4682
ream new
bearings
to
specified
wear
tolerances.
Drill
out
lubricator
holes
through
bearings
and
install
lubricators.
Internal
Bearings
Upper
and Lower
2.252
Replace bearings
when
nose
gear
is
overhauled.
Alignment
(8
and
22)
2.250
ream
new
bearings
to
specified
wear
tolerances.
Drill
out
lubricator
holes
through bearings
and
install lubricators.
Instruction Placards
Do
not
remove
from
brace
assembly
except
for
inspection
purposes
or
replacement.
E22
SECTION 5
Jun
30/04Page
51