Raytheon Beech Baron E55 - Page 367

Aircraft
Company
BARON
55
AND
58
SHOP
MANUAL
REMOVING
AND
INSTALLING
THE
LANDING
GEAR
MOTOR
a.
Remove the
right
front
seat.
b.
Remove the
access
plate
over
the
motor.
c.
Disconnect
the
electrical
wiring
at
the
landing
gear
dynamic
brake
relay.
d. Remove
the three
landing
gear
motor
attaching
bolts and
remove
the
landing
gear
motor.
e.
Install
the
landing
gear
motor
by
reversing
the above
removal
procedure
and
safety
the
three
attaching
bolts.
REMOVING
AND
INSTALLING
THE
LANDING GEAR
DYNAMIC
BRAKE RELA
Y
a.
Removethe
rightfrontseat.
b.
Remove the
access covers
on
top
and
directly
behind
the front
carry
through
structure.
c.
Disconnect
the
electrical
wiring
at
the
dynamic
brake
relay.
d.
Remove the
two
dynamic
brake
relay
attaching
screws
and
remove
the
dynamic
brake
relay.
e.
Reinstall
the
dynamic
brake
relay by
reversing
the above
removal
procedure
and
check
rigging.
NOSE
WHEEL
STEERING
MECHANISM
The
nose
wheel
should
be
parallel
to
the
fore
and the
aft
center
line
of
the
airplane
with
the rudder
pedals
in
the
neutral
position.
Take
the
nose
gear
steering
actuator
arm
loose
at
the back end
and
screw
the
end
fitting
either
in
or
out
to
make the
adjustment.
NOSE
WHEEL TRA VEL
STOP ADJUSTMENT
The travel
stop
must
be
adjusted
so
the
nose
wheel
travel
is
stopped
when the
shimmy
damper
is
1/32
in. from
its
maximum travel. If
adjustment
is
required
the
following
procedure
is recommended:
a.
Loosen
the
lock
nuts
on
the
adjustment
bolts until
they
clear
the
stops
on
the
nose
wheel
straightener.
b.
Turn
the
nose
wheel
to
the
extreme
left
turn
position.
The
adjustment
bolts
must
clear
the
stops
with
the
nose
wheel
in
this
position.
c.
Place
tape
around
the aft
end
of
the
shimmy
damper piston
rod
1/32
in.
from
the
scraper
ring.
I
d. Turn
the
lock
nuts
on
the
adjustment
bolts
so
the
nose
wheel is turned
and
the
tape
on
the
piston
rod
just
contacts
the
scraper
ring.
Tighten
the
lock
nuts
securely.
e.
Turn the
nose
wheel
to
the
extreme
right, place
the
tape
on
the forward
end of
the
piston
rod and
repeat
Step
d..
LANDING GEAR
POSITION
LIGHT
ADJUSTMENT
(TC-1608
AND
AFTER; TE-938,
TE-943 AND
AFTER;
TH-385
AND
AFTER)
The
landing
gear
position lights
on
the
instrument
panel
are
controlled
by
the
UP
indicator
switches
and
DOWN
indicator
switches
on
each
gear.
With the
airplane
on
jacks, adjustment
of
these switches
may
be made
as
follows:
E22
SECTION
5
73