Raytheon Beech Baron E55 - Page 899

RBYthColl
AiKraft
Company
BARON
55
AND
58
SHOP
MANUAL
ITEM
INSPECTION
REQUIREMENT
INSPECTION
INTERVAL
INSPECTION
AFTER
HARD
LANDING
(Continued)
LOG
BOOK
ENTRY
Following
a
hard
landing
inspection,
an
entry
covering
the
extent
of
inspection,
the
damage
and the
repair
(if
applicable)
must
be
noted
in the
airplane
permanent
records.
INSPECTION
AFTER
ENCOUNTERING
TURBULENT
AIR
Perform the
following:
As
applicable
NOTE:
This
inspection
should
be carried
out
after the
airplane
has
been
subjected
to
high
G
loading
while
flying
through
turbulent
air and
before the
airplane
is retumed
to
sen/ice.
The
inspection
is conducted
on
two
levels.
The
first
level
consists
of
determining
if
any
external
damage
has occurred and
looking
for
evidence
of
internal
structural
failure.
The second level
is
concerned
with
a more
detailed
inspection
of
damaged
areas
which
were
indicated
in
the
findings
of the
first
level
inspection.
if
it
is
determined
by
the
first
inspection
that there
is
no
damage
to
the
airplane,
it is
not
necessary
to
proceed
to
the
second
level
inspection
F\RST
LEVEL
INSPECTION
Prior
to next
flight
WARNING:
Even
though
wrinkles in
the
wing
or
fuselage
skin surface
may
be
alight
enough
to
be
considered
as
negligible,
a
close
inspection
of the
internal
supporting
structure
may
reveal
serious
damage.
General
Appearance
Determine
that
the
airframe
components
(nacelles, wings,
fuselage
and
empennage)
are
in
their normal
configuration.
Wing
Center
Section
a.
Inspect
the
external skin
surface
(upper
and
lower)
for
cracks,
abnormal stress
wrinkles
and
Loose
or
missing
rivets.
b.
Check
wing
attachment
fittings
for
cracks.
c.
Inspect
plumbing
and
wiring
for
damage
and
security
of
attachment.
d.
Check the
keel
and
the
front
and
rear
spar
on
the
lower side
of
the
fuselage
for
damage
and
alignment.
Nacelles
a.
Inspect
the external
skin
surfaces
for
wrinkles
and
loose
or
missing
rivets.
b.
Check
cowling
attachment
fittings
for
alignment
or
damage.
c.
Inspect
the
engine
support
mounts
for
cracks
or
deformation
or
structural failure.
d.
Inspect
engine
control
cables
for
smooth
operation
and
check
plumbing
and
wiring
for
security
and
attachment.
e.
Inspect
structure
in
wheel well
for
damage
or
cracks.
E23
SECTION
16Page
25