Raytheon Beech Baron E55 - Page 248

Ray~heon
Aircraft
BEECH
BARON
55
AND
58
SHOP
MANUAL
ELEVA
TOR
TRIM
TAB
ACTUA
TOR
CLEANING
AND
L
UBRICA
TION
(TC-
1144
AND
AFTER;
TE-618
AND
AFTER;
TH- I
AND
AFTER)
NOTE
Refer
to Beech Service
Instructions
No.
0610-152,
Revision
II,
for
modification
of
the
elevator
trim
tab
installation.
a.
Clean
all
parts
with
solvent
(15,
Consumable
Materials
Chart,
Section
2)
and
inspect
for
cracks,
corrosion
and
distortion.
b.
Replace
any
parts
showing
evidence
of
wear.
c.
Lubricate
all
parts
with
lubricating
grease
(11,
Consumable
Materials
Chart,
Section
2).
ELEVA
TOR
TRIM TAB
ACTUA
TOR
ASSEMBL
Y
(TC-
1144
AND
AFTER;
TE-618
AND
AFTER;
TH-
1
AND
AFTER)
FIGURE
4-16
a,
install
the
actuator
screw
(4)
into
the
nut
assembly (6).
IWARNINO
WARNING
The trim
tab
actuator to
be
installed
on
the
left-hand
horizontal
stabilizer,
shall have
threads
on
its
actuator
screw
(4)
that
rotate
clockwise when
screwed
into the
nut
assembly
(6),
The
trim
tab
actuator to
be
installed
on
the
right-hand
horizontal
stabilizer,
shall
have threads
on
the
actuator
screw
(4)
that
rotate
counterclockwise
when
screwed
into
the
nut
assembly
(6).
SHOULDER
1.
Snap
Ring
e/PIN
1
2.
Nut
AssemMy
RIVET
3.
Bearing
Airplane
serials
TC-1071,
~20435F
-8
4.
Actuator
Screw
TC-1073
through
TC-1143,
5.
Spacer
TE-521,
TE´•528
through
7.
Bearing
6.
Actuator Rod
End
TE-538
and
TE-543
throughWASHER
9.
Check
Nut
TE-617
8.
Bushing
~e
NUT
10.
Adjusting
Bushing
14
11.
Housing
12.
Rivet
(AN470AD-3)
2
4
13.
Rivet
(AN470AD3)
14.
O-ring
!2
13
9
10
3
11
8
7
1
5
6
55-16410
Elevator
Trim
Tab
Actuator
(TC-1
thru
TC-1143;
TE-1
thru
TE-617)
Figure
4-15
4-40
616