Raytheon Beech Baron E55 - Page 243

Ray~heon
Aircraft
BEECH
BARON
55
AND
58
SHOP MANUAL
g.
Wrap
the cable
counterclockwise
las
viewed from
the
left)
around
the
shaft
toward the
hole
three
full
turns.
Insert
the cable
through
the holes and
wrap
the
excess
cable
clockwise around
the shaft.
h. Take
the
cable
coming
off the
bottom of
the indicator
drum
(wrapped
clockwise)
down
to
the
aft side
of
the
con-
trol
wheel
shaft
to
the
right
of
the hole.
Wrap
the
cable
clockwise
las
viewed
from
the
left)
around
the
shaft
toward the
hole three
full
turns. Insert
the
cable
through
the
holes
and
wrap
the
excess
cable
counterclockwise
around the
shaft.
j.
Twist
the
two
cable
ends
together
and
solder with
rosin
core
solder.
k.
Check
the
tab
control
and
dial
to
be
sure
that
it
moves
freely
from
one
stop
to
the other.
i.
Check
the
tab
travel
and
direction of
movement to
be
sure
that
it
corresponds
to
the
movement
of
the
control
and indicator.
ELEVA TOR
TRIM
TAB A CTUA
TOR REMOVAL
a.
Remove the
access
panel
near
the
trailing
edge
of the horizontal stabilizer
to
gain
access
to
the elevator
trim
tab
actuator.
b.
Detach the tail
cone,
disconnect
the
tail
navigation light
wire
and
remove
the tail
cone.
c.
Remove the
access
panel
on
the
left
hand side of
the
fuselage
just
forward of the
horizontal
stabilizer.
d.
Remove the
access
panel
near
the
leading
edge
of the horizontal
stabilizer to
gain
access
to
the elevator
trim
tab
actuator
sprocket.
e.
Remove the
elevator
as
outlined
in
Section
4
of
this
Shop
Manual
under the
heading
ELEVATOR
REMOVAL.
f.
Disconnect
the elevator
trim
tab
cables
at
the
turnbuckles
in the
aft
fuselage.
Secure the
forward
elevator
trim
tab cables
to
prevent
them
from
unwinding
at
the
universal.
I
CAUTION
I
CAUTION
Do
not
damage
the
cables.
Use
a
material
such
as
phenolic
to
protect
the cables.
g.
Remove the chain and cable
assembly
from
the elevator
trim
tab
actuator
sprocket.
h.
Remove
the hardware
attaching
the
elevator trim tab
actuator to
the
horizontal stabilizer.
Remove
the
actuator
from
the
airplane.
NOTE
If the
actuator
is
to
be
reinstalled,
identify
with
a
tag
to
ensure
proper
movement
of
the
elevator
tabs
upon
reinstallation
of
the
actuators.
E16
4-35