Raytheon Beech Baron E55 - Page 210

Raytheon
Aircraft
BEECH
BARON
55
AND
58
SHOP MANUAL
EFFECT
OF
TEMPERA
TURE
UPON
CABLE TENSION
Graphs
specifying
the
correct
maximum
and minimum cable tension
for
the
various controls
appear
on
the
individual
control
system
rigging
illustrations.
The
graphs
provide
tension
limits
at
temperatures
from
30"
to
110"
Fahrenheit.
The horizontal
scales
on
the
graphs
designate
the
temperature
at
which the
control
cables
can
be
rigged,
and
the vertical scales
designate
the
correct
tension
in
pounds
for
each
temperature
reading.
I
CAVTION
I
CAUTION
A control cable
must
be
replaced
if
it is determined
to
have
more
than three
broken strands
along
any
three
foot
segment.
NOTE
I
When
inspecting
control
cables,
it
is
important
to
operate
the controls
through
their full
range
so
that
the cables
move
away
from
the
pulleys
and all
portions
of the
cables
are
exposed
for
inspection.
TAPER
PINS
When
installing
taper
pins,
use
a
lightweight
rawhide
or
nylon
mallet
to
set
the
pin.
The small
end
of the
tapered
shank
must
be
flush
with,
or
extend
no more
than
0.06
inch above the surface.
I
cnunon
I
CAUTION
The
taper
pin
can
crack the
torque
tube
if it is
driven
too
far.
SINGLE
THROW-OVER
CONTROL
COLUMN
(OPTIONAL
ON
TC-1
AND
AFTER;
TE-1
AND
AFTER;
TH-1
THRU
TH-1388,
TH-1390
THRU
TH-1395)
FIGURE
4-1
CONTROL
COLUMN
ARM REMOVAL
a.
Remove
the four
screws
that
secure
the
retainer collar
assembly
to
the control
column
housing.
b.
Disconnect
any
electrical
wiring.
I
c.
Pull the T
handle located
on
the
forward side
of the control
arm.
d.
Rotate
the control
column
arm
to
the
nearly
vertical
position
and slide
the control
column
arm
off the
housing.
CONTROL
COLUMN
ARM
INSTALLA
TION
a.
Position
the control
arm
in
a
vertical
position.
Refer
to
Figure
4-1.
Ensure that
the slot in
the lower
sprocket
is
approximately
parallel
to
the sides of
the
arm
and
the turnbuckles
between
the
long
and short chains
are
opposite
each
other
near
the
access
opening.
b.
The
ailerons
MUST be
in
the
neutral
position.
I
c.
Pull
the
T handle
located
on
the
forward
side of
the control
arm.
4-2
E16