Raytheon Beech Baron E55 - Page 331

RaytheMI
AiKraft
Company
BARON
55
AND
58
SHOP
MANUAL
Chart
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
Knee
Pins
(21
and
31)
0.4990
Visually
inspect
for
wear,
damage
and
0.4980
corrosion.
Any
sign
of
scratches
or worn
areas
which
can
not
be
repaired
is
cause
for
rejection.
If
no
visible
wear
is
evident,
conduct
magnetic
particle
inspection
per
MIL-STD-1949.
Any sign
of cracks
is
cause
for
rejection.
Replace
if
wear
tolerances
are
exceeded.
Torque
Knee
Center
Hinge
Joint
Bore
(Upper) (25)
0.4420
Inspect
for
wear,
damage
and
corrosion.
0.4370
Replace
if
wear
tolerances
are
exceeded.
Bushing
(24)
0.3150
0.4360
Visually
inspect
for
wear,
damage
and
0.3120
0.4330
corrosion.
Replace
if
wear
tolerances are
exceeded.
Bore
(Lower)
(33)
0.3175
Visually
inspect
for
wear,
damage
and
0.3125
corrosion.
Replace
if
wear
tolerances
are
exceeded.
Orifice
Assembly
(6)
1.560
Visually
inspect
for
wear,
damage
and
1.557
corrosion.
Any
sign
of
scratches or
wom
areas
which
can
not
be
repaired
is
cause
for
rejection.
Check
the
orifice
O.D.
does
not
exceed
wear
tolerances.
Check
that
orifice
hole does
not
exceed
0.192/0.187
in..
Cadmium
plate
as
necessary
except
for
ring
groove
in
orifice
head,
per
Fed
QQ-P-416,
Type
I,
Class
2.
Cylinder
Assembly
(9)
Visually
inspect
for
wear,
damage
and
corrosion.
Any
sign
of
cracks,
scratches
or
wom
areas
which
can
not
be
repaired
is
cause
for
rejection.
If
no
visible
wear
is
evident,
conduct
fluorescent
or
dye
penetrant
inspection
per
MIL-
STD-6866.
Corrosion
proof
per
MIL-C-5541
and
touch
up
paint
as
required.
E22
SECTION
5
Jun
30/04Pege
37