Raytheon Beech Baron E55 - Page 334

Raytheon
Aircraft
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
Inner
Hinge (13)
0.6240
Replace
bearings
when
main
landing
gear
is
0.6230
overhauled.
Brace
Bores
Forward
Bolt
(14)
Bore
0.4425
Visually
inspect
for
wear,
damage
and
0.4370 corrosion.
Replace
if
wear
tolerances
are
exceeded.
Center
Bolt
(10)
Bore
0.2520
Visually
inspect
for
wear,
damage
and
0.2495
corrosion.
Replace
if
wear
tolerances
are
exceeded.
Aft
Bolt
(14)
Bore
0.4425
Visually
inspect
for
wear,
damage
and
0.4370 corrosion.
Replace
if
wear
tolerances
are
exceeded.
Forward
and
Att
Columns
(15)
Upper
and
Lower
Attachment
Forward
Bolt
(14)
Bores
0.4425
Visually
inspect
for
wear,
damage
and
0.4370 corrosion.
Replace
if
wear
tolerances
are
exceeded.
Aft Bolt
(14)
Bores
0.4425
Visually
inspect
for
wear,
damage
and
0.4370 corrosion.
Replace
if
wear
tolerances
are
exceeded.
Safety
Switch
Components
Ensure
there is
electrical
continuity
when switch
is
activated.
Replace wiring
and
components
on
condition
Jun
30/04SECTION
5
E22