Raytheon Beech Baron E55 - Page 344

RalkheMI
Aircraft
Company
BARON
55
AND
58
SHOP
MANUAL
Chart
3
Nose
Gear
Wear
Tolerances
and
Inspection
Procedures
(TC-I
and
After;
TE-1 thru
TE-300)
(Continued)
ITEM
I.D.
O.D.
WEAR
TOLERANCES
AND INSPECTION
PROCEDURES
Knee
Pin
(42)
0.374
Visually
inspect
for
wear,
damage
and
corrosion.
Any
scratches
0.373
or
worn
areas
which
can
not
be
repaired
is
cause
for
rejection.
If
no
visible
wear
is
evident,
conduct
a
magnetic
particle
inspection
per
MIL-STD-1949.
Any
crack
is
cause
for
rejection.
Replace
if
wear
tolerances
are
exceeded.
Orifice
Assembly
(6)
1.449
Visually
inspect
for
wear,
damage
and
corrosion.
Any sign
of
P/N
35-825195
1.436
scratches
or
worn
areas
which
can
not
be
repaired
is
cause
for
I
(TC-1
thru.TC-2433,
TE-I
rejection.
Conduct
a
magnetic
particle inspection
per
MIL-STD-
thru
TE-300)
1949.
Any
sign
of
cracking
is
cause
for
rejection.
Check
the
orifice
O.D.
does
not
exceed
wear
tolerances.
Check
that
orifice
I
hole
does
not
exceed
0.185/0,180
in..
Cadmium
plate
as
necessary
per
Fed
QQ-P-416,
Type
I,
Class
2.
NOTE:
If
the
orifice
assembly
P/N 35-825195
exceeds
wear
tolerances,
use
Orifice
Assembly
P/N
36-820021
as
a
replacement spare.
Orifice
Assembly
(6)
1.449
Visually
inspect
for
wear,
damage
and
corrosion.
Any
sign
of
P/N36-820021
1.436
scratches
or
worn areas
which
can
not
be
repaired
is
cause
for
(TC-2434
and
After)
rejection.
Conduct
a
magnetic
particle
inspection
per
MIL-STD-
1949.
Any
sign
of
cracking
is
cause
for
rejection.
Check
the
orifice
O.D.
does
not
exceed
wear
tolerances.
Check
that
orifice
hole
does
not
exceed
0.142/0.140
in..
Cadmium
plate
as
necessary per
Fed
QQ-P-416,
Type
I,
Class
2.
Barrel
Assembly
(23)
Visually
inspect
for
wear,
damage
and
corrosion.
Any sign
of
scratches
or
worn
areas
which
can
not
be
repaired
is
cause
for
rejection.
Conduct
a
magnetic
particle
inspection
per
MIL-STD-
1949.
Any sign
of
cracking
is
cause
for
rejection.
Bearings
-Upper
1.755
Visually
inspect
for
wear,
damage
and
corrosion.
Replace
1.751
barrel
assembly
if
wear
tolerances
are
exceeded.
-Lower
1.755
Visually inspect
for
wear,
damage
and
corrosion.
Replace
1.751
barrel
assembly
if
wear
tolerances
are
exceeded.
Upper
Torque
Knee
0.3755
Visually
inspect
for
wear,
damage
and
corrosion.
Replace
if
Attachment
Hole
0.3745
wear
tolerances
are
exceeded.
Piston
and
Fork
Assembly
(48)
Chrome
Portion
(top)
1.490
Visually
inspect
for
wear,
damage
and corrosion.
Any sign
of
1.482
scratches
and
worn
areas
which
can
not
be
repaired
is
cause
for
rejection.
Conduct
a
magnetic
particle
inspection
per
MIL-
STD-1949.
Any
sign
of
cracking
is
cause
for
rejection.
Replace
if
wear
tolerances
are
exceeded.
Jun
30/04Page
50
SECTION
5