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Raytheon Beech Baron E55 - Page 97

Raytheon Beech Baron E55
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Raydheon
nircraft
Company
BARON
55
AND
58
SHOP
MANUAL
Landing
Lights
a.
Cover
with
barrier
material
and
secure
with
tape.
Stall
Warning
Unit
a.
Remove
and
store
according
to
standard
practices.
b.
Tape
connections.
Loose
Tools
and
Equipment
a.
Remove
the
loose
tools
and
equipment
and
store
in
a
dry
room.
Airframe
a.
Cover
static
ports
and
all
openings
with
barrier
material
and
secure
with
tape
to
exclude
rain,
sun
and
foreign
material.
I
u~taduaorm.
aullaadls*esnrsan
ansi
prr~au.n.
~canmnd.d
by
manufacturer
of
such
equipment.
I
Hydraulic
System
a.
Fill
the
hydraulic
reservoir
to
the
operational
level
and
inspect
the
system
for
leaks,
then
repair
as
necessary
prior
to
storage.
CONTROL
LOCK
(TC-1
THRU
TC-1436;
TE-1
THRU
TE-859;
AND
TW-1
THRU
TH-222)
NOTE:
The
rudder
pedals
must
be
in
the
aft
position
before
the
rudder
lock
can
be
installed.
The
control
lock
holds
the
throttles
closed
and
all
primary
flight
controls
in
the
neutral
position.
The
elevator
and
aileron
controls
are
locked
by
a
locking
pin
which
slides
into
matching
holes
in
the
elevator
shaft,
aileron
torque
tube,
and
control
column
hanger.
Another
part
of
the
lock
slips
over
the
throttles,
preventing
them
from
opening
while
the
elevator
and
aileron
controls
are
locked.
To
insert
the
locking
pin,
place
the
elevator
and
aileron
controls
in
an
approximately
neutral
position.
A
rudder
control
locking
pin,
which
joins
and
locks
the
pilot’s
rudder
pedals,
is
attached
to
the
control
column
lock
by
a
chain
or
cable.
The
pin
is
inserted
in
the
holes
at
the
top
of
the
pilot’s
rudder
pedal
arms,
where
it
is
retained
by
spring
tension.
Install
the
rudder
lock
after
first
attaching
the
control
column
lock.
Insert
the
spring
end
of
the
rudder
lock
into
the
left-hand
pilot’s
rudder
pedal
arm,
neutralize
the
pedals,
and
insert
the
opposite
end
of
the
locking
pin
in
the
other
pedal
arm
by
compressing
the
spring.
To
lessen
the
possibility
of
taxiing
or
takeoff
with
the
control
lock
installed,
remove
the
locking
components
in
the
following
order:
rudder,
elevator-aileron
and
throttle.
Dec
31/04Page
12
SECTION
2
E23

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