Raytheon Beech Baron E55 - Page 235

Raytheon
Aircraft
BEECH
BARON
55
AND
58
SHOP
MANUAL
b.
Adjust
the
length
of the
elevator
push-pull
rods to
obtain
14"
to
16"
of
down travel.
c.
Adjust
the
lower
stop
bolt
in
the
elevator
bellcrank
to
obtain
29"
to
31"
of
up
travel.
d.
Rig
the
cable
tension
as
shown in
Figure
4-1 1.
Adjust
the
cable
so
that the elevator
bellcrank
contacts
its
down-
stop
before
the
control column
is
in the
full
forward
position.
NOTE
Tensiometer
readings
must be
taken
on
the
top
and
bottom
cables with
the elevator
in the
down
position against
the
stop
and the
downsprings
connected.
e.
With
the elevator
bellcrank
against
its
upstep,
adjust
the
control
column
stop
to
obtain
a
clearance
of
0.06
to
0.12
inch.
f. Check elevator
travel.
I
WARNING)
WARNING
Check the elevators
for
correct
direction
of
movement.
When the
control
wheel
is
moved
forward,
the elevators
must
move
down.
When
the
control
wheel
is moved
aft,
the
elevators
must
move
up.
g.
Check the elevator
downspring
loads
as
described
in
the
following procedure.
ELEVATOR
DOWNSPRING
LOADS
With
the
downsprings
connected,
the
loads in the
elevator
control
system
must
be
within
the
limits
given
below.
Mea-
sure
the
loads in
a
draft-free
area
using
a
push-pull
scale
on
the control
wheel.
For
TC-1 and After:
24
to
28
pounds
breakout
(down
elevator),
23
to
25
pounds
breakout
at
O"
elevator
(neutral),
10
to
12
pounds
at
30"
up
elevator
(0.06
inch
off
stop).
For
TE-1
and After:
21
to
24
pounds
breakout
(down
elevator),
22
to
24
pounds
breakout
at
O"
elevator
(neutral),
20
to
21
pounds
at
30"
up
elevator
(0.06
inch
off
stop).
For TH-1
thru
TH-1388,
TH-1390
thru TH-1395:
32
to
35
pounds
moving
the
control
wheel
aft
through
neutral
from full
down
elevator,
19
to
33
pounds
moving
the
control
wheel
forward
through
neutral
from full
up
elevator,
0
to
14
pounds
difference
between
readings.
E16
4-27