Raytheon Beech Baron E55 - Page 368

Ray~heon
Aircraft
Cc~mpany
BARON
55
AND
58
SHOP
MANUAL
MAIN
GEAR
a.
With
the
gear
down and
locked,
adjust
the
DOWN
switch
(located
on
the
forward
side
of
the
main
gear
V
brace)
so
that
the overtravel
of
the
switch
plunger
is 0.050
in.
after
the
switch is
actuated
to
the
ON
position.
With the
gear
in
the
full
up
position,
adjust
the UP
switch
(located
inboard of the
forward
side
of
the
main
gear
V
brace)
so
that
the
overtravel
of the
switch
plunger
is
0.050
in. after
the switch
is
actuated
to
the
ON
position.
NOSE
GEAR
a.
With the
gear
down
and
locked,
adjust
the
DOWN switch
(located
on
the
right
side
of
the
wheel
well)
so
that the
overtravel
of
the switch
plunger
is 0.050
in, after the
switch
is
actuated
to
the
ON
position.
With
the
gear
in
full
up
position,
adjust
the
UP switch
(located
on
the
right
side
of the
wheel
well)
so
that
the
overtravel
of
the
plunger
is
0.050
in. after the
switch is
actuated
to
the
ON
position.
Check
the instrument
panel
to
be
sure
the indicator
lights
correspond
to
the
gear
position.
b.
Recheck
the
switch
adjustment,
then
remove
the
airplane
from the
jacks.
THROTTLE
WARNING HORN
SWITCH
ADJUSTMENT
(TC-
I
AND
AFTER)
Adjustment
of the
throttle
warning
horn
may
be
accomplished
as
follows:
a.
With the
airplane
in
flight, place
the
propeller
controls
in
the
low
pitch position
and
slowly
retard
the
throttle
controls until
12
to
14
in. of
manifold
pressure
is
indicated.
b. Mark
the
position
of
the
throttle controls.
c.
After
the
airplane
has landed and with
the
engines
shut
off,
position
the
throttle
controls
at
the
mark
made
in
Step
b..
d.
Adjust
the
phenolic
blocks
on
the threaded
linkage
behind the instrument
panel
until the switches
actuate
closed
as
indicated
by
an
audible
click.
e.
Securetheblocks
inthisposition.
THROTTLE
WARNING HORN
SWITCH ADJUSTMENT
(TE-
f
AND
AFTER;
TH-
I
THRU
TH-1544,
EXCEPTTH-1543)
Adjustment
of
the throttle
warning
horn
may
be
accomplished
as
follows:
a.
With
the
airplane
in
flight, place
the
propeller
controls
in
the low
pitch position
and
slowly
retard
the
throttle
controls
until
12
to
14
in,
of manifold
pressure
is
indicated.
b. Mark
the
position
of
the
throttle
controls.
c.
After
the
airplane
has
landed and
with
the
engines
shut
off,
position
the
throttle controls at
the mark made
in
Step
b..
d.
Adjust
the
microswitch
in
each
engine
compartment
until
the
switch is
actuated
closed
as
indicated
by
an
audible
click.
e.
Secure
the
switch
in this
position.
Jun
30/04Page
74
SECTION
5