Raytheon Beech Baron E55 - Page 324

Rll~hCOn
Aircraft
Company
BARON
55
AND
58
SHOP
MANUAL
Chart
1
Main
Landing
Gear Wear Tolerances
and
Inspection
Procedures
(TC-1
thru
TC-354,
except
TC-251
and
TC-344)
(Continued)
WEAR
TOLERANCES
AND
INSPECTION
ITEM
I,D
O,D, PROCEDURES
Instruction Placards
Do
not
remove
from
cylinder assembly except
for
inspection
purposes
or
replacement.
Welded Brace
(9)
Hinge
Bore
(7)
0.6275
Visually
inspect
for
wear,
damage
and
0.6245 corrosion.
If
wear
tolerances
are
exceeded,
contact
the Technical
Support
Department
of
Raytheon
Aircraft
Company,
P.O.
Box
85,
Wichita,
KS
67201.
Hinge Bushings
(8)
0.5005 0.6235
Replace
bearings
when
main
landing
gear
is
0.4995
0.6220
overhauled.
Safety
Switch
Components
Ensure there
is
electrical
continuity
when switch
is activated.
Replace
wiring
and
components
on
cond ition.
Jun
30/04Page
30
SECTION
5
E22