Raytheon Beech Baron E55 - Page 885

Ray~heon
Aircraft
Company
BARON
55
AND
58
SHOP
MANUAL
100-HOUR
INSPECTION
(Continued)
E.
CABIN
AND
BAGGAGE
COMPARTMENT
(Continued)
MECH
INSP
11.
PLUMBING Check
all
plumbing
and
connections
for
security,
leakage
and
general
condition.
Inspect
the
area
of
the
fuel selector valve
to
ensure
clearance
between
the
fuel
plumbing
and
the
arm
rest
post
with
the
arm
rest
fully
retracted
to
its
down
stop.
If
contact
is
found,
inspect
the
fuel line
for
wear
and
damage.
If
the
fuel
line is
serviceable,
reposition
it,
otherwise
replace
it.
Check
the
armrest
post,
mount
bracket,
and
stops
for
proper
security
and
excess
wear.
Replace
any
components
that
are
worn
excessively.
12.
WINDOWS AND
DOORS
Inspect
windows
for
scratches,
crazing
and
general
condition.
Inspect
doors
for
security
of attachment.
Check
latching
mechanism for
proper
engagement
and
ease
of
operation.
Check
that
rotation
of
the
interior
door
handle
without
depressing
the handle
lock release
button,
does
not
unlatch
the
door.
13.
INSTRUMENTS
AND
INSTRUMENT
PANEL
Inspect
instrument
panel,
sub
panels, placards
and instruments
for
condition
and attachment.
Check
all
knobs
for
security.
Inspect
shock
mounts,
ground
straps
for
cracks
and
security.
14.
SEATS,
SEAT BELTS
AND
SHOULDER
HARNESSES
Inspect
cabin
seats,
seat
belts
and
shoulder harnesses
for
proper
operation,
condition and
security
of
attachment.
Inspect
floorboards
for
condition
and
seat
attachment.
Check
for
operation
of
the
seat
stops.
15. OXYGEN SYSTEM
Check condition
of
the
oxygen
system
and check
the
oxygen
masks
for cleanliness and
stowage.
16.
VENTILATING
SYSTEM Check
all fresh
air
and
heat
outlet
vents
for
proper
movement
and
operation.
17.
FUEL
SELECTOR
VALVE
(TC-I
thru
TC-2002,
except
TC-1970;
TE-1
thru
TE-1082,
except
TE-1081)
Inspect
for
leakage, security,
freedom of
movement,
proper
detent
feel
and
condition.
Check
for
proper
placarding.
18.
VACUUM SYSTEM
Replace
individual
instrument
air filters
and/or
time
change
master
filter
on vacuum
system
airplanes
in
accordance with Sections
11
and
15.
i i
19.
VACUUM SYSTEM
AIR
FILTER
(Located
behind instrument
panel)
Check
for
security
of
attachment. Refer to
Section
15
for
additional
information.
20.
EMERGENCY
EXIT
HATCH
Check
emergency
release handle and latch
assembly
for
proper
operation.
Check
that
the
hatch
moves
out
freely.
Check
the
complete
latch
assembly
for
condition and all
moving
parts
for
proper
operation.
With
the
hatch
installed,
check
for
proper
latching
and seal.
Safety
the
emergency
exit
with
0.020
inch
diameter
copper
wire after
opening.
21.
STATIC
SYSTEM Check
and
drain
water
from
the
static
lines.
22.
CONTROL COLUMN
(TH-1389,
TH-1396 and
After)
Inspect
the
control
column
U-joint
roll
pins
and
ensure
they
are
not
backing
out.
E23
SECTION
16
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