Raytheon Beech Baron E55 - Page 205

~ytheon
Aircraft
Company
BARON
55
AND 58
SHOP
MANUAL
d.
To
facilitate
installation,
mark the location
of the
trim
strip
clips.
e.
Remove
the rivets
around the
window.
f.
Remove the
window.
CABIN
DOOR
WINDOW INSTALLA
TION
a.
Clean
the sealer
from
the
door where the
old
window
was
removed
using
toluol
(20,
Consumable
Matenals
Chart,
Section
2).
b.
Place the
window
in
position
and
mark the
areas
where
material
must
be
removed
to
obtain
a
proper
fit.
c.
Remove
the
window
and
trim
off
excess
material
as
determined
in
Step
b..
I
d.
Place
the
window
in
position
and
cleco
in
place
using
the
two
pilot
holes
on
the aft
side
of
the
window
frame~
NOTE:
To
eliminate
the
possibility
of
the
door
being
warped,
the door
must
be
closed
and latched when
drilling
the
attaching
holes and
riveting
the
window
in
place.
e.
Back drill
the
window frame
using
the
existing
holes
in
the
door
as
a
guide.
f.
Remove
the
window,
clean
and
deburr
all
holes and
apply
sealer
~4,
Sealing
Chart,
Section
2)
to
an
area
approximately
1/2-inch
wide
on
the
door
where
the
old
sealer
was
removed.
g.
Place
the
window
in
position
and
cleco in
place.
h.
Using
AN470AD4
rivets,
secure
the
window
to
the
door.
NOTE:
When
riveting
the
window
in
place,
install the
trim
strip clips
in
the
same
locations
as
marked
in
Step
d.
of
I
the
window
removal
procedure.
i.
Install
the
trim
strip.
j.
Clean
and
paint
as
necessary.
k.
Install
the
center
upholstery
pane.
i.
Install
the
inboard
door
handle,
ash
tray
and
arm
rest.
CENTER
WINDOW
REMOVAL
AND
INSTALLATION
a.
Remove
the
emergency
release
pin.
b.
Remove
the
hinge
pin.
c.
Installation
is
accomplished by
reversing
the
above
procedure.
NOTE:
Some
hand
forming
may
be
required
to
obtain
a
proper
fit.
Ena
SECTION
3Page
57