Raytheon Beech Baron E55 - Page 423

3.
Disconnect
the
heater fuel line
(LH
cell
c.
Connect the
vent
lines.
only).
J.
Airplane
serials
TH-I
thru
TH-iX~.
TH-’hh.
I‘H
773
and
after.
TC-1970,
TC-2003
and
aftrr,lnd
TE-I()XI.
i.
Airplane
serials
TC-1608
thru
TC-~003,.
except
TE-1084
and
after:
TC-1970:
TE-938,
TE-943
thru
TE-1083,
except
TE-IOSI;
TH-385
thru
TH-772,
except
TH-76h:
I.
Position
the
fuel cell
in
place
and
the’
I.
Remove
fuel
cell reservoir
and
fuel
connec- velcro
pile
and hook
together
pressing
vutw:trd
in
the
arr;~
~,i
tor
as
described
in RESERVOIR REMOVAL
in
this
section.
the velcro
tape.
Inspect
flappzr
valvr
Li~
In
IS-
j.
Disconnect the
vent
lines
at
the outboard
end
of
SPECTION
OF
MAIN
FU
EL
CELI.
FLAPPER
V.~
L.~’
E
in
the cell,
this
section.
k.
Snap
out
the cell
and
pull
it
through
the
top
of the
3.
Install
hose,
sump
assembly
and
fuel outlet
outboard
access
opening.
4.
Install
heater
fuel
line
tLH
onlyi.
e.
Airplane
serials
TC-lhl)X thru
TC´•2002.
s\ic´•pl
NOTE
TC-
1()70:
TE-93H,
TE-933
thru
TE-IOHj,
siit~pl
TE-lctXI.
TH-385
ihru TH-772.
except
TH-7hh:
Wrap
the
edges
of
the
access
hole
and the
liner
I.
Install
the
fuel
cell
rc~rrvoir
and
fuel
ii,nnt´•e
with
masking
tape
to
prevent
snagging
the
fuel
tor
as
described in
this
Sectjun
under
the
hcaJlngg
KES~-.H´•
cell
during
its
removal.
VOIR
INSTALL.ATION.
INSTALLING INBOARD
LEADING EDGE
FUEL
CELL
CA
UTION
(76-1608
and
after,
TE-938,
TE-943
and
after and
~H-
1
and
after)
Thi
caution
doe!,
not
LLpP()
TH-I
thru
TH-3X4.
To
prevent
push~ng
the
Inlc~r
connect
tube~
out
of
place
when
In4i~iling
:he
NOTE
inboard
leuding
edge
fuel
~eil. ii
ma)
nc´•
ncis´•
to
hold
rube~
throu~h
This
note
does
not
apply
to
airplane
serials
TH-
i
in
the
box
thru TH-j84. Prior
to
installing
a
new
inboard
leading
edge
fuel
cell,
particular
attention
should
be
paid
to
the removable
yellow
tag
which
is
f.
Connect
the
fuel
outlet.
~orque
~O
ri,
7()
In~h-
attached
to
the
cell
near
the
nipple
and
which
pounds
and
safety
wire.
reads
as
follows: g.
Install
the
clamps
on
the
inrerconnrcl
Tor-
que
the
nipple
clamps
to
I
I
r
I
inch-pounds
on
Uniro~al
THIS
CELL CONTAINS AN INTERNAL
cells
and
It;
5
inch-pounds
on
crll~.
NIPPLE
WHICH
IS
COVERED
BY
A
WEB
INTEGRAL WITH
THE
CELL.
WHEN
THIS
CELL IS BEING INSTALLED
IN
MODELS
NOTE
ES5 AND
58
EQUIPPED
WITH
THE
OUT-
BOARD LEADING EDGE
CELL.
THE
NIP-
On
airplane
serials
prior
re,
TC-
IhiJ.
PLE
MUST
BE
LOCATED
AND
THE
WEB
TH-J37,
which
were
originally t~quipprj
with
In-
CAREFULLY
CUT-OUT.
THIS
NIPPLE
IS
board
interconnect
flapper
valves,
there
Is
no
LOCATED ON
THE
OUTBOARD
END.
’.87
need
to
replace
a
flapper
valve should either
one
INCHES
FORWARD
OF
THE
LOWER
AFT
or
both
be
removed.
CORNER.
h. Install
the
fuel
cell
access
plates
and
\aCet)
H´•ire
NOTE
i. Install
the
transmitters
a´•i
descrlb~d under
the
heading
FUEL
CELL
TRANSMITTER
INSTXLL.I\TIO~
For
ease
of
installation,
place
the
fuel
cell
in
an
in this
section.
area
where
the
temperature
is
at
least
600F,
and
j.
Install
the
access
covers.
allow
a
sufficient
heat
soak
period
to ensure
flexibility
of
the cell.
REMCl/ING
BOX
SECTION CELL
(TC-1608
and
al-
ter,
TE-9~8,
TE-943
and
alter
and TH-
I
and
after)
a.
Install
the ceil
through
the
top
outboard
access
opening.
a.
With
the
selector valves
in the
OFF
?usition.
drain
b.
Align
the
snap
hangers
that
secure
the
cell
to
the
all
wing
cells.
upper
wing
and
fasten
it
iq
place,
b.
Remove
the
screws
securing
the
fuel
cell filler
cap
8-13