Raytheon Beech Baron E55 - Page 897

Raytheon
Aircraft
Company
BARON
55
AND
58
SHOP
MANUAL
ITEM
INSPECTION
REQUIREMENT
INSPECTION
INTERVAL
INSPECTION
AFTER
HARD
LANDING
(Continued)
Fuselage
Center
Section
a.
Inspect
external skin surface
for
cracks,
abnormal
wrinkles
and
loose
or
missing
rivets.
b.
Inspect
around
cabin
windows
for
structural
cracks
Fuselage,
Aft
a.
Check
external
skin
surface the entire
length
for
cracks,
abnormal wrinkles
and
loose
or
missing
rivets.
b.
Inspect
empennage
and control surfaces
for
freedom
of
movement.
SECOND
LEVEL
INSPECTION
I
As
required
NOTE:
Because
shock
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.
Landing
Gear
a.
Place
airplane
on
jacks
and check shock
strut
for
free
up
and
down
movement.
b.
Remove
tires
and
inspect
internally
for
cuts
or
broken
areas.
c.
Disassemble
and examine
wheels
trims)
for
cracks
or
distortion.
d.
Visually
inspect
axle
with
1
O-power
glass.
If
suspect,
dye
check
or
magnaflux.
e.
Remove and
replace
or
magnafiux
the
landing
gear
attach
bolts,
check
bolt holes
for cracks
or
elongation.
f.
Remove and
replace
or
magnaflux
drag
link
bolts
and
supports.
g.
Perform
landing
gear
retraction
test.
Nacelles
a.
If
tips
of
propeller
have been
damaged,
refer
to
the
applicable
Engine
Maintenance
Manual
for
engine
inspection procedure.
b.
Inspect
areas
surrounding
the
engine
mounts.
c.
Check
the internal
structure
of
the
wheel
well
for
cracks
or
damage.
d.
Test
plumbing
and
wiring
for
proper
operation
E23
SECTION
16
23