Raytheon Beech Baron E55 - Page 900

Ray)heon
Aireraft
Company
BARON
55
AND
58
SHOP
MANUAL
ITEM
INSPECTION REQUIREMENT INSPECTION
INTERVAL
INSPECTION
AFTER
ENCOUNTERING
TURBULENT
AIR
(Continued)
Wings
a.
Inspect
the
top
and
bottom
wing
surface for
cracks,
wrinkles
and
loose
or
missing
rivets.
b.
Inspect wing
attachment
fittings
for cracks.
c.
Inspect
aileron,
aileron
tab
and
flaps
for
wrinkles
or
cracks.
d.
Inspect
internal
structure
and
fuel
cells
through
access
panels.
e.
Inspect
plumbing
and
wiring
for
security
of
attachment.
Fuselage,
Nose
a.
Check
external skin surface for
cracks,
wrinkles and loose
or
missing
rivets.
b.
Inspect
area
forward
of
windshield
for
evidence
of structural deformation
or
failure.
c.
Inspect
avionics,
antenna
and
components
for
security
of attachment.
Fuselage,
Center Section
Inspect
external skin
surface for
cracks,
abnormal
wrinkles
and loose
or
missing
rivets.
Fuselage,
Aft
a.
Inspect
the entire
length
of
the external skin
surface
for
cracks,
stress
wrinkles and loose
or
missing
rivets.
b.
Check
the
empennage
surfaces for
damage
and
free
movement.
c.
Inspect
for
skin wrinkles
at
the
juncture
of
the
fuselage
and
empennage.
SECOND
LEVEL INSPECTION
As
required
NOTE:
Because
G
loading
may
be
transmitted
along
one
structural member
to
another,
carefully
inspect
the
surrounding
and
supporting
structure
in
any
damaged
area
found
in
the first
level
inspection.
Wing
Center
Section
a.
Dye
check
wing
attachment
fittings,
examine
(magnaflux
or
replace)
attachment
bolts
and check bolt holes for
alignment
and
correct
dimension.
b. Remove
floorboards
and
access
plates
and
inspect
the front and
rear
spar
and keel
structure
for
evidence
of
deformation
or
structural failure.
c.
Operational
test
plumbing,
wiring,
flaps,
control
cables,
pulley
mounts
and
any
other
system
found
in this
area.
Page
262~,
SECTION
16
E23