Raytheon Beech Baron E55 - Page 98

Ray~heon
AiKraft
Company
BARON
55
AND
58
SHOP
MANUAL
CONTROL LOCK
(TC-
1437
AND
AFTER;
TE-860
AND
AFTER;
TH-223 AND
AFTER)
The
control lock holds the throttles
closed,
the elevator
11"
down,
and the aileron
control wheel 12"
nght
of
the
neutral
position.
The
throttle,
elevator and aileron
controls
are
locked
by
a
locking
pin
that
is
inserted between the
throttle
levers
through
the control column
hanger,
the
elevator
shaft and
matching
holes in
the aileron
torque
tube.
The
portion
of the
lock
that is inserted between
the
throttle
levers and
through
the
control column
hangar
prevents
the
throttles
from
being opened.
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.
The
throttle
control locks
are
to
be
installed
in
the
following
sequence:
Close
the
throttles,
install
the
control
rocking
pin
between the throttles
through
the control
column
hanger, through
the
elevator control
and the
aileron
torque
tube.
Route the
cable and
rudder lock around
the
right
side
of
the
control
column,
position
the rudder
pedals
in
the
aft
position
and install the rudder
lock
by
inserting
the
spring
end
of
the 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.
RETURN
TO
SERVICE
FROM
STORAGE
I
RETURN TO
SERVICE FROM
FLYABLE
STORAGE
a.
Remove
all
covers,
tape
and control
locks.
Clean
the
airplane
and
give
it
a
thorough
inspection,
particularly
wheel
wells,
flaps
and control
openings.
b. Drain
the
corrosion
preventive compound
(3,
Chart
3)
after
ground
warm-up.
Fill
with
engine
oil
(2.
Chart
3)
1
before
flight.
c.
Preflight
the
airplane.
RETURN
TO SERVICE
FROM TEMPORARY STORAGE
a.
Remove all
covers,
tape
and
control locks.
Clean
the
airplane
and
give
it
a
thorough
inspection,
particularly
wheel
wells,
flaps
and control
openings.
b. With
the
bottom
spark
plugs
removed,
hand-turn the
propeller
several revolutions
to
clear
excess
preservatrve
oil,
then
reinstall the
spark plugs.
c.
Drain
the corrosion
preventive
compound
(3,
Chart
3)
after
ground
warm-up.
Fill
with
engine
oil
(2,
Chart
3)
before
flight.
d.
Preflight
the
airplane
and
flight
test.
RETURN
TO SERVICE FROM INDEFINITE STORAGE
a.
Remove all
covers,
tape
and
tags
from the
airplane.
b.
Remove the
cylinder
protex
plugs,
all
paper
tape
and
dehydrating
agent
used
to
preserve
the
engines.
,2,
SECTION
2Pags
13