Raytheon Beech Baron E55 - Page 159

Ray~heon
Aircraft
Company
BARON
55
AND
58
SHOP
MANUAL
e.
Install
the
machine
screws
that
attach
the
root
nose
rib
to
the
front
spar.
f.
Install
screws
attaching
the
nose
skin
to
the
front
spar.
g.
Install
the
screws
attaching
the
forward
section
of
the
outboard
rib
to
the
spar.
h.
Connect
the
navigation light
wire
and
install the
wing
tip.
i.
Install the
screws
that attach the
wing
tip
to
the
wing.
j.
Connect
the
electrical
wiring
to
the
landing
light.
k.
install
the
nacelle.
i.
Cement
the
rubber
fillet
to
the
root
of
the
wing, using
cement
155,
Consumable
Materials
Chart,
Section
2)
or
an
equivalent
fuel
resistant
rubber
cement.
m.
Install
the
fuel cell
and
connect
the fuel lines.
n.
Install
the
access
doors.
WING INSTALLATION
NOTE:
When
replacing
wing
bolts make
sure
that the
replacement
bolts have
been
properly
inspected
using
the
magnetic
particle
process.
Bolts
must
be
magnetically
inspected
before installation
as
wing
botts.
Bolts
may
be
acquired
through
Raytheon
Aircraft Parts
Inventory
and Distribution
(RAPID).
The
individual
placing
the
order
must
stipulate
the need
to
have
the
bolts
inspected
before
shipment.
a.
Using
a
nonmetallic brush
and
solvent
(18
or
19,
Consumable
Materials
Chart,
Section
2),
clean the
wing
attach
fittings
and hardware
(bolts,
washers
and
nuts). Inspect
the
wing
attach
fittings
and
hardware
as
instructed
under
WING
BOLT,
NUT,
AND
FITTING
INSPECTION.
WARNING:
Wing
bolts that
have reached their
life
limit
(10
years
after
the
initial
inspection),
must not
he
reused
(Ref, Figure
12).
The
mounting
nuts
must
be
replaced
at
each
inspection
interval.
I
b.
Coat
the
fitting
bolt
bores
and
bearing
faces, bolts,
washers,
and
nuts
with corrosion
preventive compound (49,
Consumable
Materials
Chart,
Section
2).
CAUTION:
Each
bolt
must
be inserted
by
hand without
binding.
If
a
bolt
cannot
be
easily
inserted,
reposition
the
wing
until
the
bolt
moves
freely
in the
fittings,
Do
not
screw
or
drive
the
bolt
into
the
fittings.
c.
Move
the
wing
into
position
and
align
the
wing
fittings
with
the
carry-through fittings.
Insert
the bolts into the
fittings.
CAUTION:
Bolts,
washers
and
nuts must
be
oriented
as
shown
in
the
applicable figure
for
each
location
I
(Pef
Figures
8,
9
10,
and
1
I).
d.
Start
the
nuts
on
the
upper
forward and aft bolts.
Rotate
the
wing trailing edge
until
alignment
with
the
outline
drawn
on
the
fuselage
is
realized. After
rotation
is
established,
verity
that
the lower
forward
bolt
is
not
binding
in
the bolt bore.
If
bolt
binding
is
encountered,
adjust
the
wing
until
the
bolt
moves
freely.
e.
Tighten
the
upper
forward
and
aft
nuts.
CAUTION:
Prior
to
the lower
ah
nut,
a
slight
gap may
be
evident
between
the
fittings.
This
gap
should
naf
exceed 0.060
in
width.
No
gap
should
remain
after
torquing
the lower aft
nut.
E23
SECTION
3
Dec
31/WPage
11