Raytheon Beech Baron E55 - Fuselage

Raytheon
nircraft
Company
BARON
55
AND
58
SHOP
MANUAL
FUSELAGE
FORWARD
CARRY-
THROUGH SPAR COVER REMOVAL
a.
Removethe
pilotandcopilotseats.
b.
Remove
emergency
landing
gear
crank
cover
from
spar
cover.
c.
On
aft side of
spar
cover,
pull
back
carpet
and
remove screws
from
spar
cover.
d. On forward side
of
spar
cover,
pull
back
carpet
and
remove screws
from
spar
cover.
e.
Remove
RH
access
cover.
f.
From
inside of RH
access
cover,
loosen
clamp
and
remove
air
duct
from
plenum
and
grill assembly.
g.
Lift
spar
cover
and
remove
from
forward
spar.
FORWARD
CARRY-THROUGH
SPAR
COVER INSTALLA
TION
CAUTION:
Improper
installation of
the
forward
carry-through
spar
cover
may
interfere
with the
landing
gear
emergency
hand crank
operation.
Ensure
the
landing
gear
hand crank will
engage
and
rotate
without
interference
with
the
spar
cover.
a.
Centersparcoveron
thefomardspar.
b. From
inside of
RH
access
cover,
install
air
duct
on
plenum
and
grill
assembly
and
tighten
clamp.
c.
Install
RH
access
cover
assembly.
d. On forward
side
of
spar
cover,
install
screws
to
secure
forward
end
of
spar
cover
and
install
carpet.
e.
On
aft
side
of
soar
cover,
install
screws
to
secure
aft end
of
spar
cover
and install
carpet.
f.
Check
the
emergency
landing
gear
hand
crank
to
ensure
handle
will
engage
and
rotate
without
interference
with
the
forward
carry-through
spar
cover.
g.
Install
emergency
landing
gear
crank
cover
to
spar
cover.
h.
Install
the
pilot
and
copilot
seats.
WING
FORWARD
SPAR CARRY-THROUGH
STRUCTURE
INSPECTION
WITHOUT REPAIR
KIT
This
procedure
provides
inspection
and
repair
information
relating
to
the forward
wing
spar
structure
at
the forward
and aft frames.
I
NOTE:
The
areas
identified
in
Figure
16
should
be
inspected
for
cracking
at
the
intervals
specified
for
non
repaired
structures
by
Chart
4
using
the
following
inspection procedure:
a.
Remove
the
pilot’s
and
copilot’s
seats
and
the
carry-through
cover
to
obtain
access
to
the front
spar
carry-through
structure.
b.
Thoroughly
clean
the
forward
and
aft
frames
(webs)
of the
front
spar
carry-through
structure
in
the
areas
shown
I
in
Figure
16 with
solvent
(16,
Consumable
Materials
Chart,
Section
2).
Dec
31/04Page
26
SECTION 3
E23