Raytheon Beech Baron E55 - Page 901

Raytheon
AiKraft
Company
BARON
55
AND
58
SHOP
MANUAL
ITEM
INSPECTION REQUIREMENT
INSPECTION INTERVAL
INSPECTION
AFTER
ENCOUNTERING
TURBULENT
AIR
(Continued)
Nacelles
a.
Inspect
areas
surrounding
the
engine
mounts.
b.
Inspect
internal
structure
for cracks
or
damage.
c.
Operational
test
plumbing
and
wiring.
Wings
a.
Dye
check
wing
attachment
fittings,
examine
(magnaflux
or
replace)
attachment
bolts.
b.
If
there is
evidence
of
damage
to
the
fuel
cells
or
fuel
lines,
remove
the cells
and
inspect
the
fuel
cell
liners
and liner
support
structure.
c.
Operational
test
the
plumbing
and
wiring,
flap
actuator,
aileron and tab control cables
and
pulley
mounting.
Fuselage
Nose
a.
Remove floorboards and
inspect
the
keel
structure
and
supporting
members
for
damage.
b.
Examine
any
fixed
equipment
for
loose,
broken
or
cracked
mountings.
c.
Operational
test
avionics,
radar
antenna,
plumbing
and
wiring.
Fuselage
Center Section
a.
Examine
stringers,
frames
and
sidewalls for
deformation
or
structural
failure.
b.
Examine
heating
and
air-conditioning
ducts
for
damage.
c.
Operational
test
plumbing
and
wiring.
d.
Examine
the
control
cables,
pulley
mountings
and the
cable
clearance
at
areas
the
cables
pass
through
the
structure.
Ensure
a
smooth,
normal
operation.
Empennage
a.
Inspect
elevator
pushrods,
torque
tubes
and
bellcrank for
damage.
b.
inspect
the
attachment
of
the vertical
stabilizer
spars
to
the
top
of
the
fuselage
for
evidence
of
damage.
c.
Inspect
skin surfaces for condition
and
loose
or
missing
rivets.
E23
SECTION
16
27