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Raytheon Beech Baron E55 - Page 172

Raytheon Beech Baron E55
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RBylheOn
Aircraft
Company
BARON
55
AND
58
SHOP
MANUAL
WING
MAIN
SPAR
CAP
VISUAL
INSPECTION
The
wing
spar
cap
must
be
inspected
for
corrosion
annually.
WARNING:
All
areas
of
the
wing
main
spar
caps,
from
the
wing
attach
fitting
to
the
outboard
end
of
the
spar
cap,
must
be
inspected.
Kit
58-4002-1
contains
the
parts
and
instructions
necessary
to
install
a
new
LH
and
RH
spar
on
the
model
55
and
58
series
wing
panels.
The
kit
does
not
contain
the
spars
which
must
be
ordered
separately.
NOTE:
Special
emphasis
should
be
placed
on
airplanes
that
have
been
operated
or
stored
for
extended
periods
(5
years
or
longer)
in
geographical
locations
where
atmospheric
conditions
are
highly
conducive
to
corrosion.
Inspection
of
the
upper
and
lower
spar
caps
should
be
accomplished
in
the
following
manner:
a.
Examine
the
forward
and
aft
sides
of
the
spar
cap
where
it
meets
the
skin.
If
a
whitish,
saltlike,
nonmetallic
substance
is
noted,
a
thorough
inspection
must
be
performed
to
determine
if
corrosion
has
occurred.
Wax
or
paint
trapped
between
the
edge
of
the
skin
and
the
exposed
section
of
the
spar
cap
should
not
be
misinterpreted
I
as
corrosion
(Ref.
Figure
14).
NOTE:
To
gain
access
to
the
upper
spar
cap
in
the
nacelle
area,
remove
the
shaded
panels
shown
in
Figure
15.
b.
Wash
all
exposed
areas
of
the
upper
and
lower
spar
caps.
c.
Visually
inspect
all
exposed
areas
of
the
upper
and
lower
spar
caps
for
irregularities,
such
as
paint
blisters,
raisdd
or
uneven
areas,
and
cracks.
The
exposed
areas
of
the
spar
caps
are
extruded
flat
and
irregularities
could
be
an
indication
of
corrosion.
Thoroughly
investigate
all
irregular
areas
to
determine
if
any
damage
has
occurred.
NOTE:
Uneven
or
raised
areas
on
the
spar
caps
may
be
detected
by
sliding
the
fingers
over
the
surface,
by
moving
I
a
straight
edge
over
the
surface,
or
by
sighting
down
the
length
of
the
spar
cap
surface.
If
unusual
conditions
are
encountered
that
cannot
be
resolved
locally,
contact
the
Technical
Support
Department
at
Raytheon
Aircraft
Company
for
evaluation
and
determination
of
corrective
action
that
may
be
required.
Page
24SECTION
3
ana

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