Raytheon Beech Baron E55 - Vertical Stabilizer

Raytheon
Aircraft
BEECH
BARON
55
AND
58
SHOP
MANUAL
CHART
4-3
RUDDER
TAB
FREE
PLAY
LIMITS
1.5-POUND
3-POUND
READING
READING
28
-A
=X
20 -C
=Y
X
+Y
=E
E
0.090 inch
maximum
VERTICAL STABILIZER
VERTICAL
STABILIZER
REMOVAL
Remove
the
tail
section
access
doors
on
the left hand side
of
the
fuselage.
I.
Remove
the
rudder.
See
RUDDER REMOVAL.
m.
Remove
the
screws
securing
the
fairings
to
the
vertical
stabilizer.
n.
Remove
the
attaching
bolts
at the
forward and
rear
spare
and
remove
the
center
hinge
bracket
from
the lower
center
spar
and
remove
the
stabilizer.
VERTICAL
STABILIZER
INSTALLATION
a.
Position
the vertical
stabilizer
and
install
the
bolts
as
follows:
1.
On
airplanes
TO-1
through
TC-2456,
TE-1
through
TE-1201
and TH-1
through
TH-1483,
torque
the bolts
at
the
forward
spar
and
upper
rear
spar
to
160
to
190
inch-pounds.
Install
the
elevator
center
hinge
bracket
on
the
bottom
of
the
rear
spar
and
torque
the
bolts
to50
to
70
inch-pounds.
2.
On
TC-2457 and
after,
TE-1202 and
after
and
TH-1484
and
after,
torque
the bolts
at
the
forward
spar
and
upper
rear
spar
to
330
to
360
inch-pounds.
Install
the
elevator
center
hinge
bracket
on
the bottom
ofthe
rear
spar
and
torque
the
bolts
to
85
to
100
inch-pounds.
b.
Installthevertical
stabilizerfairings.
c.
Install
the
rudder.
See
RUDDER
INSTALLATION
in
this section.
d.
Install
the
access
doors.
E16
4-59