Raytheon Beech Baron E55 - Page 883

RBYthdOll
Aircraft
Company
BARON
55
AND
58
SHOP
MANUAL
100-HOUR
INSPECTION
(Continued)
D.
WINGS
AND
CARRY-THROUGH
STRUCTURE
(Cantinued)
MECH INSP
tH RH
9.
FLAP LIMIT
SWITCHES
Check
for the
condition,
security
and
freedom
of
flap
operation.
10.
FLAPS
AND
ACTUATORS Check
for
condition,
security,
binding
or
chafing
of
actuator
cables
or
actuator
drive
shaft. Check
flap
skin
and
structure
for
cracks,
I I
loose
or
missing
rivets.
Check
roller
bearings
and
tracks
for
condition.
Check
stop
area
for condition
and
damage.
11.
FLAP
POSITION
TRANSMITTER
Check
for
security
and
operation.
12.
DRAIN
HOLES
Check
the drain
holes in the
left
and
right
upper
wing
attach
fittings
to
ensure
that
they
are
open
and
free of
obstruction.
13.
WING
SPAR
CAP
Inspect
the
wing
spar
cap
for
corrosion
as
outlined
in
Section
3.
1 I I I
14.
WING BOLTS Check
wing
bolts
for
proper
torque
at
the
first
1
GO-hour
inspection
and
at
the first
1
GO-hour
inspection
after
each
installation
of
the
wing
attach bolts.
Refer
to Section
3
for
wing
bolt,
nut
and
fitting
inspection
criterion
and
frequency.
15.
WING
BOLT
NUTS
Check
wing
bolt
nuts
for
proper
torque
at
the
first 100-hour
inspection
and
at
the
first
100-hour
inspection
after
each
installation
of
the
wing
attach
bolts.
Refer
to
Section
3
for
wing
bolt,
nut
and
fitting
inspection
criterion
and
frequency.
16.
PITOT
TUBE
(TC-1
thru
TC-16G7;
TE-1
thru
TE-941,
except
TE-938)
Check
for
I I I I
condition and
obstructions.
17.
STALL
WARNING
VANE Check for condition and
obstructions.
I I I I
18.
AILERON TRIM
TAB
Check
for attachment
and
freedom
of
movement.
i i 1 I
19.
FUEL
QUANTITY
TRANSMITTER
Check for attachment
and
electrical
I I 1 I
connection
20.
NAVIGATION
LIGHTS Check
for
cracked
or
broken
lenses
and
replace
bulbs
I I I
as
necessary.
21.
LANDING
LIGHTS
Check for
security
and
operation.
Replace
lens
and
bulbs
as
I I I I
necessary.
22.
AUXILIARY
FUEL
PUMP AND FUEL
LINES
Check
for
condition,
security
and
I I i I
1
leaks.
Check
lines
for
signs
of
chafing
or
cracks.
23.
FUEL
SELECTOR
VALVE
(TC-1970,
TC-2003 and
After; TE-1O81,
TE-1O84 and
I 1 I
1
After;
TH-1
and
After)
Check
for
security,
operation
and
leakage.
24.
FUEL
STRAINER
(Located
in
the main
gear
wheel
well)
Inspect,
clean
and
I
check
for
leaks.
Refer
to
Section
8.
25.
FUEL
STAINS Check
the
under side of
the
wings
for fuel
stains.
See
S.
i.
0632.
I
0632).
26.
Perform the
INSPECTION
OF
THE
BAFFLE
MAIN FUEL
CELL
FLAPPER
I I I I
I
VALVE
OR
RESERVOIR
FLAPPER VALVE
procedure
in
Section
8.
E23
SECTION
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