Raytheon Beech Baron E55 - Page 375

Baeechc~aft
BARON
55
AND
58
SHOP
MANUAL
To avoid
bottoming
out
of the
nut
and
to
g.
Connect the
plumbing
at
the firewall.
I
assure
proper
tightening
of
the
nut,
a
h.
Install the
propeller
(see
Section
7).
maximum of
three
AN960-616
washers
may
be
installed
for each
bolt installa-
I~
tion,
using
one
washer under
the
bolt
CAUTION
head and
two
washers
under
the
nut.
NOTE
Because the
cowling
is
an
integral
part
of
the
cooling
system,
the
engine
will
If
the
engine
is
disconnected
at
the
eng-
overheat
if
operated
with the
cowling
ine
shock
mounts
(vibration
isolators),
removed for
more
than
a
very
brief
test
rather
than
at
the
firewall,
on
reinstalla-
period.
tion
torque
these
engine
mount
bolts
to
323
~25
inch-pounds
on
TC-1
and after
FUEL INJECTOR
LINE
NUTS
and
torque
to
475
~t25
inch-pounds
on
TE-1 and
after
and TH-1
and after.
Be If
the fuel
injector
line
nuts
at
the
nonle
are
removed
careful
to
align
the holes
in
the rubber
from the 10-470
or
the 10-520
engine,
they
should
be
mount
bushings
(plates)
with
the
index
retorqued
to
40
45
in. Ibs. The
injector
line
nuts
at
pin
which
protrudes equidistantly
on
the
manifold
valve should also be
retorqued
to
40
45
both sides of
the
steel
bushing.
in. Ibs.
d. Remove the hoist hook from
the
engine lifting ring
and
move
the hoist
away
from
the
airplane.
CYLINDER
HEAD
-TEMPERATURE BULB
e.
Connect
the electrical
wiring
at
the firewall
or
at
The
cylinder
head
temperature
bulb
may
be
located
in
the
accessory
as
necessary.
one
of
two
locations,
depending
on
the
engine
model.
f.
Connect
the
engine
controls
to
the
engine.
On
the
IO-470-L
engines
the
temperature
bulb
is
2
4
i.
ENGINE
2.
PLATES
(5
EACH)
3. ENGINE MOUNT
r
TTT n
4.
PLATES
(3
EACH)
I
I I I
I
I I I II
5. AN960-716L
WASHER
"luull
6. BOLT
C95TH7180227
C
Figure
6-1.
Lower
Engine
Vibration Isolator
Mount
6-2
515