Raytheon Beech Baron E55 - Page 380

~eechcraft
BARON
55
AND
58
SHOP
MANUAL
d. Loosen
the locknut
(upper)
on
the control
assem-
c.
Reinstall
the
102933892T1680
spacer
on
the
act-
bly
adjusting
mechanism,
uatar
shaft.
e.
Hold
the rod end
to
prevent
its
turning,
then
pull
d. The extended
position
of the
cawl
Rep
should
be
upward
on
the rod end
with a firm
pressure.
3.6+.1
inch
as measured from the
trailing
edge
of
the
NOTE
cowl
flap
to
the nacelle.
Do
not
use
any
tool
as an
aid when
NOTE
exerting upward
pressure
on
the rod
end:
applying
a
strong
pressure
will
If the
openining
is
not
3.6
r
.1
inch,
relo-
have
a
tendency
to
stretch the cable
in
cate
the
attaching
bracket
to
obtain this
the
control
assembly.
setting.
f. Turn
the lower
retaining
nut
down
against
the
COWL FL4P ACTUATOR
RIGGING
(TE-I
I
sleeve
on
the
adjusting
mechanism,
THRU TE-942 U(CEPT
TE-9381
NOTE
a.
Retract the
cowl
flap
electrically
Never
overtighten
the
retaining
nut
against
the sleeve
as
this will increase
b.
Disconnect the
actuator shaft from the
attaching
the
effort
required
to
operate
the control.
bracket.
g.
Turn the
locknut down
against
the lower
retaining
c.
Adjust
the rod
end
on
the
actuator
shaft
to
obtain
nut.
Do
not
let the
rod
end
turn
when
tightening
the
1 .1 inch of
clearance between
the
trailing
edge
of
locknut.
the cowl
flap
and
the nacelle.
h. Connect
the control lever
to
the rod end.
d.
Connect the
actuator
shaft
to
the
attaching
i.
Install
the
two
screws
securing
the instrument
bracket.
panel
and
replace
the
glareshield.
THROTTLE
AND MIXTVRE
yrC-9s
AND
AFTER,
TE-1
AND
AFTER,
TH-I AND
AFTER)
The
engine
throttle and
mixture
centrals
may
be
adjusted
by loosening
the
jam
nut,
removing
the rod
end
pin,
and
turning
the
rod end
ehher in
or
out to
obtain
an
adjustment
which
provides
smooth
opera-
tion of the
controls. Refer
to
Figure
6-5.
COWL FLAP ACTUATOR
RIGGING
(TC-I
THRU
TC-1607)
This
rigging procedure
is
applicable
to
both
right
and
ten
mwl
flaps.
7 a
a.
Retract
the cowl
flap electrically,
b.
To
adjust
the
actuator to
obtain
1 .1 inch of
clearance between the
trailing edge
of the cowl
flap
and the
nacelle,
disconnect the
actuator
shaft
at
the
attaching
bracket,
remove
the 102933592T1680
spacer
and
install 100951S032XD
and
100951S063XD
washers
on
the
actuator
shaft
as
nec
essary.
NOTE
Normally,
one
of each of the washers
on
the
actuator
shaft
will be
sufficient
to
maintain the
clearance
required
for the
closed
flap position. Figure
6-5
Engine
Controls
515
57