Raytheon Beech Baron E55 - Page 157

R~ytheon
Aireraft
Company
BARON
55
AND
58
SHOP
MANUAL
WING
REMOVAL
a.
Drain
all
fuel from
the
airplane.
b.
Remove the
front
seats
and
side
panels.
c.
Remove
the
rear
seat
panel.
d.
Remove
the
wing
bolt
access
covers
from the
wing.
e.
Place
the
airplane
on a
three
point
jack
and
raise
until the wheels
are
clear of
the
ground.
Refer
to
Section
2
for
jacking
instructions.
A
three
point
jack
should
be
used
because
of
the unbalanced
condition
of
the
airplane
after
the
wing
is removed.
f.
Place
a
suitable
cradle
under
the
wing
being
removed and
a
wing
stand under the
opposite
wing.
A tail
stand
will
also
be
required
to
assure
stability.
g.
Disconnect
and
cap
off brake lines
at
root
rib.
h.
Retract
the
landing
gear
until
the
inboard
landing
gear
doors
are
fully
open.
i.
Disconnect the
inboard door
actuating
rod
from
the
control horn.
j.
Disconnect the
landing
gear
uplock
cable
at
the
idler
arm
in
cabin.
k.
Disconnect
the
landing
gear
actuator
rod
from
the
V
brace
in the wheel
well.
i.
Disconnect the aileron cables
at
the
turnbuckle
in
the wheel
well
and
remove
the
roll
pins
from
inboard aileron
cable
pulley
brackets. Disconnect aileron
tab
cables and
aileron
tab
stops
in
left wheel well.
m.
Disconnect
fuel
lines
between
wing
root
rib
and the
fuselage.
n.
Disconnect
the
flap
drive
shaft at
the
motor
and
remove
the
clamps
attaching
the shaft
to
the
fuselage.
o.
Remove
the
lower
aft
nacelle
fairing
assembly.
p.
Remove
the
leading
edge
cover
of
the
wing
located
between
the
fuselage
and
nacelle.
q.
Remove
the
clamps securing
the
wiring
bundles
to
the
wing
inboard
leading
edge.
Disconnect
wiring
bundles
at
terminals
located
on
aft side
of
nacelle firewall.
r.
Disconnect
wiring
to
the
electrical
components
located
in each
side
of
the
upper
nacelle.
s.
Disconnect
the
plumbing
between
the
wing
root
rib
and
the
fuselage.
t.
Disconnect
flap
wire bundle
and
safety
switch
wiring
in
left
wheelwell.
Disconnect
plumbing
and electrical
wiring
(booster
pump
and
fuel
quantity
transmitter)
in
each wheel
well.
u.
Remove the
clamps securing
engine
controls
to
leading
edge.
v.
Disconnect
the
pitot
line
between the
wing
root
rib
and the
fuselage
(left
wing
only).
w.
Using
a
grease
pencil,
outline
the
position
of
the
wing
on
the
fuselage.
CAUTION:
There should be
no
bolt
binding during
removal.
Should
binding
occur,
adjust
the
wing
position
until the
bolt
disengages
freely.
Do
not
screw
or
drive
a
bolt
in
or
out
of
the
fittings.
E23
SECTION
3
Dec
31/04Pags
9