Raytheon Beech Baron E55 - Page 206

Raytheon
Aircraft
Company
BARON
55
AND
58
SHOP MANUAL
AFT
WINDOW
REMOVAL
a.
Remove the
upholstery
panel
along
bottom
of
the
window.
b. Remove the
royalite
molding
around
the window.
c.
Remove
the
top,
bottom and
forward
retaining angles
by removing
the
attaching
screws.
d.
Remove
the window.
AFT
WINDOW
INSTALLA TION
a.
Clean the sealer
from
the
canopy
section
where the old window
was
removed
using
toluol
(20,
Consumable
Materials
Chart,
Section
2).
I
b.
Apply
sealer
(4, Sealing
Chart,
Section
2)
to
an area
approximately
1/2-inch
wide
on
the
canopy
section
where
the old sealer
was
removed.
c.
Position
the window and
secure
in
place
with
the retainer
angles
and
retainer
attaching
screws.
d.
Install
the
royalite
molding
and
the
upholstery
panel.
THIRD
OR
FOURTH WINDOW REMOVAL
(TE-766
AND
AFTER;
TH-
I
AND
AFTER)
a.
Remove
the
upholstery panels
as
required
to
gain
access
to
the window frame.
b. Remove the trim
strip
from
around
the
inside of the
window.
c.
To facilitate
installation,
mark the
location of the trim
strip clips.
d.
Removetherivetsfrom
aroundthewindow.
e.
Remove the window.
THIRD
OR FOURTH
WINDOW
INSTALLATION
(TE-766
AND
AFTER;
TH-
I
AND
AFTER)
a.
Clean
the sealer
from
the cabin
section
where
the old window
was
removed
using
toluol
(20,
Consumable
Materials
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 the
excess
material
as
determined
in
Step
b..
d. Place the window
in
position
and cleco
in
place
using
the
pilot
holes
provided.
e.
Back drill the
window
frame
using
the
existing
holes in the back
section
as
a
guide.
f.
Remove
the
window,
clean and
deburr
all
holes and
apply
sealer
(4, Sealing
Chart,
Section
2)
to
an area
I
approximately
1/2-inch
wide
on
the
canopy
section
where
the old
sealer
was
removed.
g.
Using
AN470AD4
rivets,
secure
the window
to
the
cabin section.
Page
58Dec
31/04
SECTION
3
Eza