Raytheon Beech Baron E55 - Page 381

~eechcraft
BARON
55
AND
58
SHOP MANUAL
e.
The extended
position
of the cowl
flap
should
be
3.
For
TH1389
and
TH-1396
and after the
clear-
3.6
~.1
inch
as
measured
from
the
trailing
edge
of
the
ance
between
the
cowl
flap
and
the
cowling
is
.5
to
cowl
flap
to
the
nacelle.
1.0 inch in the
closed
position
and
4.4
to
4.6
inches
in
the
open
position.
NOTE
f.
Attach
the
pushrod
to
the cowl
flap
and
check
for
If
the
opening
is
not
3.6
.1
inch,
relo-
the
desired
clearance,
making
sure
that
the
cow)
flap
cate
the
attaching
bracket to
obtain this
dimension,
control
crank
assembly
contacts
the
crank
stop
in
both
the
open
and
closed
position.
I
COWL
FLAP
ACTUATOR
RIGGING
g.
Loosen
the
jam
nut
on
the
control
cable.
(Effectivi~L:
TH-I thru
TH-384)
NOTE
a.
Retractthecowlflap electrically.
To reduce
the
tendency
for
the
cowl
flap
b.
Disconnect
the
actuator
shaft
from the
attaching
to
creep
away
from
the
fully
closed
posi-
bracket.
tion,
rig
the
cowl
flap
bellcrank
to
an
c.
Adjust
the
rod
end
on
the
actuator
shaft
to
obtain
on-center
position
or
slightly beyond.
a
flush
fitting
between the
trailing edge
of the cowl
flap
h.
Loosen
or
tighten
the rod
end
to
obtain
a
slight
and the nacelle.
cushion effect
on
the
cowl
flap
controls in
both
the
d.
Connect
the
actuator
shaft
to
the
attaching
open
and
closed
positions.
bracket.
i.
Attach
the control cable
to
the
bellcrank
assembly.
e.
The
extended
position
of
the
cowl
flap
should
be
2.6
~.1
inch
as
measured
from
the
trailing edge
of the
j.
Operate
the
cowl
flap
controls
to
both
the
open
cowl
flap
to
the
nacelle.
and closed
positions, making
sure
that
the clearance
for
the
cowl
flap
is
correct,
that
the
bellcrank
assem-
NOTE
bly
is
contacting
the crank
stop
in
both
positions
and
If
the
opening
is
not
2.6
.1
inch,
relo-
that there
is
a
slight
cushion
effect
on
the
cowl
flap
cate
the
attaching
bracket to
obtain this
controls
in each
position.
dinension.
FUEL INJECTOR
PUMP REMOVAL
MECHANICAL COWL
FLAP
RIGGING
(Effectivity:
TC-1608 and
after;
TE-938,
a.
Remove
the air
box.
(See
REMOVAL OF
THE
AIR BOX
(TC-1
and
after.)
TE-1
and after
and
TH-1
TE-943
and
after;
TH-385
and
after)
and
after do
not
require
removal
of
the
air
box.
a.
Open
the
cowl
flap.
b.
Disconnect
fuel
the
lines,
loosen the
clamps,
and
b.
Remove
the
attach
bolt
connecting
the
control
remove
the
intake
tube
assembly
between the
air
cable
to
the
crank
assembly,
metering
valve
assembly
and
the No.
2
intake.
c.
Remove the attach bolt
connecting
the
pushrod
to
c.
Remove
the lower
fitting
from
the
left
side and the
the
cowl
flap.
upper
fitting
from
the
right
side
of
the
fuel
injection
d.
Loosen
the
jam
nuts at
each
end
of
the
pushrod.
pUmp´•
e.
Loosen
or
tighten
equally
the
rod ends
on
the
d.
Remove the
four
screws
from
the
injector
pump
pushrod
to
obtain
the
desired
clearance
for the
cowl
shroud,
disconnect the
flexible
duct,
and
remove
the
flap
as
follows:
shroud.
1.
For
TC-1608
and
after and for
TE-938,
e.
Remove the
pump
retaining
nuts
and
remove
the
TE-943 and
after,
the
clearance
for the
cowl
flap
is 1.0
pump.
in
the closed
position
and
3.5
inches
in
the
open
posi-
tion.
FUEL INJECTOR
PUMP INSTALLATION
2.
For
TH-385 thru TH-1395
(except
TH-1389),
a.
Place
a new
gasket
on
the
pump
pad.
the,cowl
flap
should
be
flush
with
the
skin of
the
cowl-
ing
in
he closed
position
and
2.5 inches
from
the skin b.
Place the
pump
in
position
on
the
engine
and
in
the
open
position,
install
the
retaining
nuts.
6-8
515