Raytheon Beech Baron E55 - Page 881

Raytheon
Aircraft
Company
BARON
55
AND
58
SHOP
MANUAL
100-HOUR
INSPECTION
(Continued)
B.
POWER
PLANT
(Continued)
MECH
IFISP
LH
RH
29.
OIL SEPARATOR
(Vacuum
System)
Clean
the
screen
by
back
flushing
or
submerge
in
solvent
and blow
dry
with
shop
air.
Check
for
condition,
mounting
and
proper
operation.
Install the
screen
and
check for
security.
Inspect
for
cracks.
30.
A\R
CONDITIONER
COMPRESSOR
Check
for
security
and attachment.
Check
refrigerant
level and for
oil
leaks.
(See
Section
2).
Check
belt
for
tension and
wom
I i’ 1
or
frayed
condition.
31.
INDUCTION
AIR
FILTER
Check
for
condition,
cleanliness and
security.
32.
INDUCTION SYSTEM
AND
ALTERNATE
AIR Check
flexible
air ducts
for
delamination
of
the inner
lining.
Check
the alternate
air valve
for
blockage,
security,
cracks,
operation
and
wear.
33.
FUEL
INJECTION
CONTROL
VALVE
Clean the
screen
and
check
for
damage.
Install
screen
and
check
for leaks.
34.
FUEL
INJECTION SYSTEM
Inspect
all
fuel
injection
components,
lines
and
fittings
for
evidence
of fuel
leaks,
fraying
and
cracking.
35.
VACUUM
RELIEF
VALVE
Clean
and
inspect
filter,
check for
the
security
of
attachment.
36.
ELECTRIC PROPELLER
DEICER Check
for
service
damage
to
the
deicer
heaters,
brush
rods,
springs
and
brushes.
Check
the lead
strap
and
all
other
clamps,
connectors
and
wiring
for
electrical
soundness.
Check
the
slip
rings
for
roughness,
cracks,
burned
or
discolored
areas
and
for
deposits
of
oil,
grease
or
dirt.
Check
for
security
and
attachment
of
all
components.
Check
deicer boots
for
wrinkles,
loose
or
torn
areas.
37.
ENGINE
BAFFLE
SEALS
Inspect
for
security
and condition
at
each
100-hour
or
annual
inspection.
Replace
as
necessary
or
refer
to
Section
15
for additional
information.
38.
PRESSURE
PUMP
(Airborne)- Inspect
as
required by
Parker
Hannifin
Service
Letter
43A
or
subsequent.
Refer
to Section
15
for additional
information.
PRESSURE
PUMP
(Aero
Accessories
Pump
Part
Number
AA216CW)
Initially
inspect
at
600 hours
time-in-service
in
accordance
with
Aero
Accessories
Service
Letter No. 004
and thereafter
as
directed
by
the
Service
Letter. Refer
to Section
15
for
additional information.
39.
PROPELLER
DOME PRESSURE
Check
pressure
in
accordance
with
manufacturers
instructions.
40.
PROPELLER
UNFEATHERING
ACCUMULATOR
Check
pressure.
Refer
to
the
PROPELLER
UNFEATHERING
ACCUMULATOR
data
in
Section
2.
EZ3
SECTION
16
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