Raytheon Beech Baron E55 - Page 413

wing
box
section fuel
cell
sump:
wet
wing tip
(flush-type
NOTE
drain).
Fuel
crossfeed
operations
are
used
in
these
~y\
tems
during
emergency
conditions
in
level
flight
only.
7%-
19i"0,
TC-Z003
AND
AFTER
6
snap-type
drains (3
drains
per
wing)
Lire
provided.
One
drain
in
each
wing
is
provided
for
the
inboarcl
wing
leading
Airplane
serials
TC-1970,
TC-’~W)3 and
after
are
equipped
edge
fuel
cell
sump:
fuel strainer:
wing
box
section
fuel
cell
with
an
interconnected
fuel
system.
The
cells which
are
sump.
interconnected
within
each
wing,
provide
the
airplane
with
a
total
fuel
capacity
of
1’42
gallons
1136
gallons
usable).
Thc166,
~H-773
AND
AFTER
This
system
has
an
inboard
wing
leading
edge,
baffled
fuel
cell
with
sump
strainer
and
fuel
outlet
nipple
through
the
Airplane
serials
TH-7hh.
TH-773
and
after,
are
equipped
inboard
end
of
the
wing
main
spar;
7’his
cell is intercon-
with
an
OFF-ON-CROSSFEED
interconnected
142.
a
172
or
nected
to
a
wing
box
section
fuel
cell
for
hs
gallons
usable
in
a
300
gallon
total
capacity
fuel
system
each
wing
system
or
a
total
of
136
gallons
usable
with
left
and
right
wing
systems
full. One
flush,type
filler
cap
is
Airplane
serials
TH-7hf~,
TH-773
and
after,
the 142
and 172
located
in the
outboard
end
of
the
wing
box
section
cell.
A
gallon
total
capacity
systems
are
the
same
as
the 14? and
17
fuel
selector
panel,
located
on
the cabin
fuselage
floorboard
gallon
systems
described
for
airplane
serials
TH-I
thru
TH-
forward
of
the front
spar
cover,
is
placarded
OFF-ON-
384
except,
the
fuel
sensor
in
the inboard
end
of
the
uut-
CROSSFEEDfor
fuel
management,
Remote
fuel controls in
board
wing leading
edge
fuel
cell
is
bottom
mounted
in~tead
this
panel
are
attached
to
fuel selector
valves
in the
wheel
of
top
mounted.
wells
for
each
engine.
During
normal
operation,
fuel
is
con-
sumed from
each
wing
system
as
indicated
by
the
remote
The 200
gallon
total
capacity
fuel
system
uIiliz~4
the
c´•ell4
fuel
selector handles
in
the
cabin
fuselage.
Two fuel
quantity
described
in the
172
gallon
fuel
,ystem
and
an
addiri~nal
Ht´•l
indicators
on
the
instrument
panel
indicates
the
amount
of
wing tip
fuel
tank.
This
system
i~
interconnected
to
provjcle
fuel
in each
wing
system.
97
gallons
usable
in each
wing
system.
or
a
total
of
IYJ
gallons
usable
with
left
and
ri~ht
systems
full. One
flu~h
6
snap-type
drains
(3
drains
per
wing)
are
provided.
One
type
filler
cap
is in
each
wet
wing
tip
rank
in
addition
:o
rh~
drain
in
each
wing
is
provided
fur:
inboard
wing
leading
edge
flush
type
filler
cap
in
the
outboard
end
~f uutboarll
fuel
cell
sump:
Fuel
strainer;
wing
box
section
fuel
cell
sump.
leading
edge
cell for
the 172
gallon
system.
The
fuel
panel.
remote
fuel
controls,
fuel
valves
and
fuel
quantity
indicators
for
the
above
\ys(ems
are
TE-
1081,
~E-
108~
AND
AFTER
in
the
same
location
as
described for
TH-
I
through
TH-772.
except
TH-76h.
fuel
systems.
The
function
for
fuel
manage
ment
is
also
the
same.
Airplane
serials TE-1081.
TE-1084
and
after
are
equipped
with
an
OFF-ON-CROSSFEED
142
or
a
172
gallon
total
capacity
fuel
system.
Except
for
engine
lines
forward
of the
NOTE
firewal\s.
the
142
gallon
total
capacity
system
is
the
same as
the
142
.gallon
total
capacity system
described
under
the
Fuel
L´•rossfeed
operation!,
are
used
in
these
sv~-
heading
TC-1970.
TC-?003
AND
AFTER
in this
section,
tems
during
emergency
conditions in level
flight
only.
The
172
gallon
total
capacity system
utilizes
the
fuel
cells
described
in the 142
gallon
fuel
system
and
an
additional
Airplane
serials
TH-766.
TH-77?
and
after,
with
tither
the
outboard
wing
leading
edge
fuel
cell
on
each
wing.
This
132
or
172
gallon
total
capacity
fuel
system
are
equipyxd
system
is
interconnected
to
provide
83
gallons
usable
in each
with
a
total
of
6
snap-type
drains
(3
drains
per
wing).
Each
wing
system,
or a
total
of
166
gallons
usable
with
left
and wing
is
provided
with
L
drain
for
the
inboard
wing
teilding
right wing
system
full.
One
flush
type
filler
cap
is in the
edge
fuel
sump:
fuel
strainer:
wing
box
section
fuel
cell
outboard
end
of each outboard
wing
leading
edge
cell,
sump.
Airplane
~eriRls
~TH-76h.
TH-777
and
after.
t´•quippetl
Kith
The
function
for
fuel
management
is
the
same
and
the
fuel
wet
wing
tips
(200
gallon
total
capacity
s~stem);lre
provided
selector
panel,
remote
fuel
controls,
fuel
selector
valves
aiid
with
a
total of
6
snap-type
and
2
flush-type
drains
(4
drains
fuel
quantity
indicators
are
in
the
same
location as
described
per
wing).
Each
wing
is
provided
with
I drain
fur the
inboard
for the
142
gallon
total
capacity
system
under
the
heading
wing
leading
edge
fuel
cell
sump;
fuel strainer:
wing
hoa
TC-1970,
TC-ZOOj
AND
AFTER,
section
fuel
cell
sump:
wet
wing
tip
(flush-type
drain).
8-3