Raytheon Beech Baron E55 - Aileron System

Raytheon
Aircraft
BEECH
BARON
55
AND 58 SHOP
MANUAL
e.
Tighten
the
nuts.
f.
Recheck
for
proper
clearance
(step
b).
g.
Repeatforthe
othercontrol column.
AILERON SYSTEM
AILERON REMOVAL
a.
Disconnect
the lower
aileron
tab
push-pull
rod
(left
aileron
only).
NOTE
Lowering
the
flaps
will
aid in
disconnecting
the aileron tab
push-pull
rod.
b.
Support
the aileron
and
remove
the
two
attaching
screws
from
the
top
and
bottom
of each
hinge
bracket.
c.
Pull the
aileron
straight
away
from the
wing
to
avoid
damage
to
the
attaching
areas
and
gain
access
to
the bond-
ing
cable
screws.
d.
Remove
the
screws
attaching
the
bonding
cable to
the aileron.
AILERON
INS
TA LLA
TION
NOTE
If
the
aileron tab
has
been
removed
and
reinstalled,
or
a new
tab
installed,
lubricate
the
tab
hinge
with
VV-L-800A
(preferred)
or
CRC
3-36,
LPS-1
or
WD-40
(50,
Consumable
Materials
Chart,
Section
2).
a.
Attach the
bonding
cable
to
the
aileron.
b.
Place
the
aileron in
position
on
the
hinge
brackets.
The
hinge
brackets must
be in the
correct
place
between
the
aileron skin and the
reinforcing
structure.
c.
Install the
upper
and
lower
hinge
bracket
screws.
d.
Pull
on
the
aileron in
a
direction
straight
away
from
the
wing
to
make
sure
that the
hinge
brackets
are
positioned
correctly.
If
there
is
any
movement
of
the
aileron,
recheck
the
position
of
all
hinge
brackets.
e.
Connect
the aileron
tab
push-pull
rod
and install
the
cotter
pin
(left
aileron
only).
NOTE
Lowering
the
flaps
will
aid in
connecting
the aileron
tab
push-pull
rod.
RIGGING
THE AILERON CONTROL
SYSTEM
(TC-
I
AND
AFTER;
TE-
1
AND
AFTER;
TH-
I
THRU TH-
1388
TH-
1390
THRU
TH-
1395)
FIGURE
4-6
NOTE
Beech
recommends
the
use
of
the
aileron
travel
gage
shown
in
the GENERAL
INFORMATION
section
of
this manual.
Locate
the
travel
gage
at
wing
station
122.75.
616
4-11