Raytheon Beech Baron E55 - Page 898

Raytheon
Aircraft
Company
BARON
55
AND
58
SHOP
MANUAL
ITEM
INSPECTION
REQUIREMENT
INSPECTION
INTERVAL
INSPECTION
AFTER HARD
LANDING
(Continued)
Wing
Center Section
a.
Dye
check
wing
attachment
fittings;
examine
(magnaflux
or
replace)
attachment
bolts
and check bolt
holes for
alignment
and
correct
dimensions
b.
Remove
floorboards
and
access
plates
and
inspect
the
front
and
rear
spar,
and keel
structure
for
evidence of
deformation
or
structural failure.
c.
Test
plumbing,
wiring,
flaps,
control
cables,
pulley
mounts,
and
any
other
system
found
in
this
area
for
proper
operation.
Wings
a.
Dye
check
wing
attachment
fittings;
examine
(magnaflux
or
replace)
attachment
bolts
and check
bolt holes for
alignment
and
correct
dimensions
b.
Test
plumbing
and
wiring
for
proper
operation.
Fuselage,
Nose
Section
a.
Remove
baggage compartment
floor
boards
and
inspect
the keel
structure
and
supporting
members for
damage.
b.
Inspect
wheel
well
structure
and
surrounding
areas
for
signs
of
structural
failure.
c.
Test
avionics,
radar
antenna,
plumbing
and
wiring
for
proper
operation.
Fuselage,
Center
and Aft
a.
Examine
stringers,
frames
and
sidewalls
for
Section
deformation
structural
failure.
b.
Test
plumbing
and
wiring
for
proper
operation.
c.
Inspect
heating
and
air-conditioning
ducts
for
damage.
d. Examine
the
control
cables
and
pulley
mountings
and
check
for
clearance from
structure
at
pass-through
locations. Ensure
a
smooth
operation.
REPAIR
OF DAMAGE
Due
to
the
variety
and
degree
of
structural
damage
which
may
be
involved,
the
best
repair
of
replacement
procedure
must
be based
on
the
findings
of the
individual
airplane.
If
the hard
landing
inspection
indicates
that
serious structural
damage
has
occurred,
contact
Raytheon
Technical
Support,
Raytheon
Aircraft
Company,
Wichita,
Kansas,
67201
for
assistance.
Page
24Dec
31/04
SECTION
16
E23