Raytheon Beech Baron E55 - Page 234

Ray~heon
Aircraft
BEECH
BARON
55
AND
58
SHOP
MANUAL
u.
Use
a
clamping
device to
clamp
the
bonding
area
of the
elevator.
Refer
to
Figure
4-10.
NOTE
The
clamping
device
must
be
tightened
just
enough
to
hold
the bonded
area
together.
v.
Use
a
suitable
clamping
device
to
hold
the
trailing
edge
of
the skins
together
for
drilling
and
riveting.
w.
Drill rivet holes in
the
trailing
edge
using
the
same
spacing
as
was
used
on
the old skin.
Use
a
No.
40
drill bit.
x.
Rivet
the
trailing
edge.
y.
Install
all
screws
and
attaching
hardware
removed
during
disassembly.
z.
Paint
the
elevator.
aa.
Balance
the
elevator.
(See
BALANCING
THE
ELEVATOR)
ab.
Install the
elevator
on
the
airplane.
RIGGING
THE
ELEVA TOR
CONTROL
SYSTEM
(TC-I
AND
AFTER;
TE-I AND
AFTER;
TH-1
THRU
TH-1388,
TH-1390 THRU
TH-1395)
FIGURE
4-11
NOTE
Beech recommends the
use
of
the elevator travel
gage
shown
in the GENERAL
INFORMATION
section of this
manual. Locate
the travel
gage
at
station 35.75.
a.
Adjust
the
upper
elevator
stop
bolt
so
that the centerline
of
the
bottom cable attachment hole
in the
elevator
bellcrank
is
0.70
to
0.80
inch
from the aft
bulkhead.
C-CLAMP
OR
.EOUIVALENT
TOOL
CENTER
LINE
HINGE
POINT
BOND
AREA
UPPER
SKIN
EXTRUSION OR SOME
OTHER
RIGID MATERIAL
TO
CLAMP BONDED
AREA
TRAILING
EDGE
LOWER SKIN
51-131-3
Elevator
Skin
Replacement
(TC-547
and
After;
TE-1 and
After;
TH-1
and
After)
Figure
4-10
4-26
E16