Raytheon Beech Baron E55 - Page 896

Raycheon
nircraft
Company
BARON
55
AND
58
SHOP
MANUAL
ITEM
INSPECTION
REQUIREMENT
INSPECTION
INTERVAL
INSPECTION
AFTER
HARD
LANDING
(Continued)
g.
Inspect
area
around
landing
gear
attach
points.
Nacelles
I
a.
Inspect
external skin
surfaces for
distortion,
loose
or
missing
rivets.
b.
Check
cowling
attachment
fittings
for
alignment
or
damage.
c.
Inspect engine
control cables for
smooth
operation
and check
plumbing
and
siring
for
security
and
attachment.
d.
Inspect engine
support
mounts
for
cracks
or
structural
failure.
e.
Check
tips
of
propellers
for
damage.
f.
Check
propeller
spinner
and
backplate
for
evidence
of
interference
with
cowling.
g.
Inspect
wheel
well
structure
for
damage
or
cracks. Check
area
surrounding
the
landing
gear
attachment
points.
Wing
Center
Section
a.
Check
wing
attachment
fittings
for
cracks.
Perform
a
Dye
Penetrant
inspection.
b.
Inspect
plumbing, wiring
and
actuator
for
damage
and
security
of
attachment.
c.
Check
keel,
front and
rear
spar
on
the
lower
side of
fuselage
for
damage
and
alignment.
Wings
a.
Inspect
external
wing
surface
skin for
cracks,
abnormal wrinkles and loose
or
missing
rivets.
b.
Check
wing
attachment
fittings
for
cracks
Perform
a
Dye
Penetrant
inspection.
c.
Inspect
internal
structure.
d.
Inspect
plumbing
and
wiring
for
security
of
attachment.
Fuselage,
Nose
a.
Check
external skin surface for
cracks,
abnormal wrinkles and
loose
or
missing
rivets.
b.
Check
wheel well
structure
and
area
surrounding
gear
attach
point
for
damage.
c.
Inspect
avionics,
radar
antenna,
wiring
and
plumbing
for
security
and attachment.
Page
22Dec
31/04
SECTION
16
E23