Raytheon Beech Baron E55 - Page 251

Raytheon
Aircraft
BEECH
BARON
55
AND
58
SHOP MANUAL
k. If
the
free
play
is
over
the
maximum
specified
in Chart
4-2,
inspect
all
components
of
the
tab
actuator
system
to determine
the
cause.
All
worn
parts
must
be
replaced.
i.
Repeat
steps
b
through
k
on
the other
elevator
trim
tab.
CHART
4-2
ELEVATOR
TAB FREE PLAY LIMITS
1.&POUND
8-POUND
READING
READING
2B
-A
=X
2D
-C
=Y
X
-I-Y =E
E
0.084
inch
maximum
(TE-1
and
After;
TH-1
and
After)
E
0.069
inch
maximum
(TC-1
and
After)
ELEVATOR
TRIM
TAB
HORN
REPAIR
NOTE
Elevators
must
be removed
from
the
airplane
and checked for
static
balance
after
the
repair
procedures
described
below
are
performed.
FOR TAB
HORNS
WITH BRAZED IN
BUSHINGS
a.
Carefully
grind
or
spot
face
the
brazed-in
bushing
flush with the sides
of
the
tab
horn.
NOTE
Maintain
the
bushing
centerline
as
nearly
perpendicular
as
possible
to
trim
tab
tube
centerline.
b.
Drill
and
ream
the
existing
hole
to
an
inside
diameter
of
0.4995/0.5010-inch.
c.
Using
a
clean
rag
dampened
with
solvent
(19,
Consumable Materials
Chart,
Section
2), thoroughly
clean
the
hole in
the tab
horn,
the
area
around
the hole
and
a
new
P/N
96-610026-1
bushing.
d.
Scuff
sand
the
contact
surfaces
of
the
bushing
and
the tab
horn
and clean
the
area
thoroughly
as
specified
in
step
c.
e.
Wipe
off
the
parts
with
a
clean
rag
before
the solvent
evaporates.
f.
Apply
a
thin
coat of adhesive
(37,
Consumable
Materials
Chart,
Section
2)
to
the
contact
surfaces
of
both
the
bushing
and
the
tab horn.
E16
4-43