Raytheon Beech Baron E55 - Page 160

Rayn~on
Aircraft
Company
BARON
55
AND 58
SHOP
MANUAL
f.
Torque
the
wing
nuts
in
the
following
order:
Upper
forward,
upper
aft,
lower
forward
and lower
aft. When
a
torque
wrench
adapter
is
used,
the
length
of
the
adapter
must
be
added
to
the
length
of
the
torque
wrench and the
proper
torque
value
computed
as
detailed
in
Section
1.
Coat
the bolt
threads
that
protrude
through
the
nut
with
corrosion
preventive compound (49,
Consumable
Materials
Chart,
Section
2).
CAUTION:
When
torquing
the
wing
bolts,
assure
that
the
wing
bolt
wrenches do
not
bottom
out
on
the
wing
fittings.
Such
an occurrence
could
cause
false
torque
readings
and
damage
the
fittings.
After
torquing
the
upper
forward
wing
attach
bolt,
remove
the
holding
force from the
wing
cradle
prior
to
torquing
the
remaining
three bolts.
g.
Install the
engine
and
connect
the
engine
controls.
Install the
clamps
that
secure
the
engine
controls
to
the
leading edge.
h.
Connect
the
plumbing
between
the
wing
root
rib and
the
fuselage.
i.
Connect
the
plumbing
and
wiring
in
the wheel well.
Connect
the
aileron cables
and
install
the roll
pins
in the
inboard
aileron cable
pulley
brackets.
Connect
the aileron tab cables and aileron
tab
stops
(LH
only).
j.
Connect
the
landing
gear
actuator
rod
to
the V-brace in the wheel
well and
install
the inboard door
actuating
rod
on
the
inboard door control horn.
k.
Connect
the
wiring
to
the
electrical
components
located
in
each side of the
upper
nacelle. Install
the
clam
securing
the
wire bundles
to
the
leading edge
and
connect
the
wiring
to
the
terminals
on
the
aft
side
of
the
firewall.
i.
Install the
leading edge
cover
between
the
fuselage
and nacelle. Install the
lower
aft
naceile
fairing
assembly.
m.
Connect
the
flap
drive
shafts
at
the
motor
and install the
clamps
that attach the
shafts
to
the
fuselage.
n.
Connect
the
uplock
cable
at
the
inboard floor idler
arm
in the
cabin.
o.
Fill
the
brake
reservoir with
hydraulic
fluid
and bleed the brake
system.
p.
Remove
the stands
from under
the
wing
and tail
and
take
the
airplane
off the
jack.
q.
Installthewing
boltcovers.
r.
Install the
rear
seat
panel,
side
panels
and
front
seats.
s.
Test
fly
the
airplane
to
assure
proper
wing
and stall
warning
vane
adjustment.
page
12Dec
31/04
SECTION
3
E29