Raytheon Beech Baron E55 - Elevator System

Ray~heon
Aircraft
BEECH
BARON
55
AND
58
SHOP
MANUAL
d.
Apply
another
piece
of
masking
tape
in
the
corresponding
location
on
the bottom
surface of the
tab.
e.
Set
the
dial
indicator
at
zero.
Do not
reset
the
dial indicator
during
the
checking
procedure.
f.
With
the
push-pull
scale
on
the
masking
tape,
apply
a
3.0
pound
downward
load. Record
the
dial
reading
as
A.
g.
Release
half
of
the
load
to
obtain
a
1.5
pound
downward
load. Record
the
dial
reading
as
B.
h.
On
the
masking
tape
on
the
bottom
surface,
apply
a
3.0
pound
upward
load. Record the dial
reading
as
C.
i.
Release
half ofthe load
to
obtain
a
1.5
pound upward
load.
Record the
reading
as
D.
j.
Enter
the recorded
readings
on
a
copy
of Chart
4-1 and
proceed
as
follows.
1.
Multiply
B
by
2
and
record
as
2B.
2.
Subtract
A
from 28
and
record
as
X.
3.
Multiply
D
by
2
and
record
as
2D.
4.
Subtract C
from 2D
and record
as
Y.
NOTE
X and
Y
can
be
negative
numbers.
Add X
and
Y
and record
as
E.
CHART 4-1
AILERON TAB FREE PLAY
LIMITS
1.5-POUND 8-POUND
READING
READING
28
-A
=X
2D
-C
=Y
X
+Y
=E
E
0.094
inch
maximum
k.
If the
free
play
is
over
the
maximum
specified
in Chart
4-1,
inspect
all
components
of the tab
actuator
system
to
determine
the
cause.
All
worn
parts
must
be
replaced.
ELEVATOR
SYSTEM
ELEVA
TOR
REMO VAL
NOTE
Refer
to
Beech Service
Instructions
No.
0636-133
for
inspection
of
the elevator
hinges
and
torque
fittings
on
airplane
serials TC-1
through
TC-1414,
TE-1
through
TE-848
and TH-1
through
TH-184.
4-22
E16