Raytheon Beech Baron E55 - Page 217

Ray~heon
Aircraft
BEECH BARON 55
AND
58
SHOP MANUAL
CONTROL COLUMN CHAIN RIGGING
FIGURE
4-4
a.
Rig
neutral
on
the control wheels
by securing
a
straightedge
across
the
tops
of
both control
wheels.
The
grips
must
be
aligned
within
0.06
inch.
b.
The ends of the control
column chain
around
the
right
sprocket
must
be
equidistant,
within
one
link,
from
the
centerline
of
the
sprocket.
c.
The link
assembly
must
be
centered
within
0.20
inch with
respect
to
the
stop.
d.
Adjust
the turnbuckles
to
obtain
0.19
to
0.31
inch
of
deflection
with
a
vertical
pressure
of
1.50
to
2.50
pounds
on
the
upper
control
column
chain
near
the
airplane
centerline.
e.
Rig
the aileron
control
system
as
described
in
RIGGING
THE AILERON
CONTROL
SYSTEM.
CONTROL COL UMN
ROLLER ADJUSTMENT
FORWARD
OUTER-TUBE ROLLERS
(ROLL
ON
THE SQUARE
INNER
SHAFT)
FIGURE
4-5
There
are
four
rollers
on
the
forward endof each
control
column which transmit
torque
to
the
square
inner
shaft.
Two
of
the rollers
for each control column
are
installed
with eccentric bolts which
allow for
adjustment
of
roller clear-
ance.
These
two
bolts
may
be
identified
by
their 10-32
threads.
Adjust
the
rollers
as
follows:
TURNBUCKLE
STOP
TORQUE
GUARD
PIN
SHAFT
LINK
ASSEMBLY
CHAIN
ASSEMBLY
CONNECTOR
SPROCKET
LINK
ASSEMBLY
AILERON
CABLE
ASSEMBLY
AIRCRAR-
36-~55-6
Dual
Control
Column
Chain
Rigging
(TH-1389,
TH-1396
and
After)
Figure
4-4
E16
4-9