Raytheon Beech Baron E55 - Page 412

wing
box
section
fuel cell
for
68
gallons
usable in
each
wing
controls
in
this
panel
are
attached
to
fuel
selector
valves
in
system
or
a
total
of
136
gallons
usable with
left
and
right
the
wheel
wells
for
each
engine.
During
normal
operation,
wing
systems
full. One
flush-type
filler
cap
is
located in
the
fuel
is
consumed from each
wing
system
as
indicated
by
the
outboard end of the
wing
box
section
cell.
A
fuel
selector
remote
fuel
selector handles
in
the
cabin
fuselage.
Two
fuel
panel,
located
on
the cabin
fuselage
floorboard
forward
of
quantity
indicators
on
the
instrument
panel
indicate
the
the
front
spar
cover,
is
placarded
OFF-ON-CROSSFEED
amount of fuel
in each
system.
for
fuel
management.
Remote
fuel controls
in
this
panel
are
attached
to
fuel
selector
valves
in
the wheel
wells
for
each
The
172
gallon
total
capacity
system
utilizes
the
fuel
cells
engine.
During
normal
operation,
fuel
is
consumed
from
described
in
the 142
gallon
fuel
system
and
an
additional
fuel
each
wing
system
as
indicated
by
the
remote
fuel
selector
cell
in
each
outboard
wing
leading
edge.
This
celt
has
a
handles
in
the
cabin
fuselage.
Two
fuel
quantity
indicators
bottom
mounted
fuel
level
transmitter located
in
the
jnbuarJ
on
the instrument
panel
indicate
the
amount
of
fuel in
each
end of
the
cell.
The cells
are
interconnected
to
provide
X7
wing
system.
gallons
usable
in each
wing
system
or a
total
of I~f,
gallons
usable
with left
and
right
wing
systems
full.
One
flush-type
The 172
gallon
total
capacity
system
utilizes
the cells
de-
filler
cap
is
in
the
outboard
end
of
each
uutboard
wing
scribed in
the
142
gallon
system
and
an
additional
fuel
cell
in
leading
edge
cell.
each
outboard
wing leading edge.
The
cells
are
intercon-
nected
to
provide
83
gallons
of
usable
fuel in each
wing
The
200
gallon
total
capacity
system
(TH-h69
thru
TH-771!
system
or
a
total
of
166
gallons
usable
with
left
and
right
except
TH-766)
utilizes
the
fuel
cells
described
in
the
172
wing
systems
full.
One
flush-type
filler
sap
is in
the
outboard
gallon
fuel~system
and
an
additional
wet
wing
tip
fuel
tank
on
end
of
each outboard
wing
leading
edge.
A
fuel
level
trans-
each
wing.
The
system
is
interconnected
to
provide
91
gal
mitter is
mounted
in
the
top
of
the
outboard
wing leading
ions
of
usable fuel
in
each
wing
system
or
a
total
of
I~j
edge
fuel cell.
gallons
usable
with left
and
right
wing
systrms
full.
()ne
flush-type
filler
cap
is in
each
wet
wing tip
tank
in
addition
to
The function
for
fuel
management
and
the
fuel
selector
the
flush-type
filler
cap
in
the
outboard
end
of
each
outboard
panel,
remote
fuel
controls,
fuel
selector valves and
fuel
wing
leading
edge
ceil
for the
172
gallon
capacity
system.
quantity
indicators
are
in
the
same
location
as
described
for
the
142
gallon
total
capacity
system.
CAU~ION
NOTE
When
servicing
this
system.
remove
the
~ur-
board
cap
first
to
prevent
loss of
fuel
If
It
is
Fuel
crossfeed
operations
are
used
in
these
sys-
above
the level
of
the
inboard
cap.
tems
during
emergency
conditions
in level
flight
only.
The
function
for
fuel
management
and
the
fuel
srlector
panel,
remote
fuel
controls,
fuel
selector
valves
and fuel
6
snap-type
drains
(3
per
wing)
are
provided.
Each
wing
is
quantity
indicators
are
in the
same
location
fur
the
17’
or
)(W)
provided
with
I
drain
for: inboard
wing leading edge
fuel
cell
gallon
total
capacity
system
as
described
for
the
14?
gallon
sump;
fuel strainer:
wing
box
section
fuel
cell
sump.
total
capacity
system.
TH-385
THRU
7H-772,
EXCEPT
~H-766
NOTE
Airplane
serials
TH-385 thru
TH-772.
except
TH-766
are
Fuel
crossfeed
operations
are
used
in
these
´•iys-
equipped
with
an
interconnected
Cuel
system.
The cells
are
tems
during
emergency
conditions
in
level
flight
interconnected within
each
wing
and
provide
the
airplane
only.
with
a
total
fuel
capacity
of
142
gallons
(136
gallons
usable),
172
gallons
(166
gallons
usable),
or
~00
gallons
(194
gallons
usable),
Airplane
serials
TH-3R5
thru
-TH-772.
except
TH-7hfi.
with
either the
142
or
172
gallon
total
capacity
fuel
system,
are
The 142
gallon
total
capacity
system
has
an
inboard
wing
equipped
with
a
total
of
6
snap-type
drains
1!
drains
per
leading
edge
unbaffled fuel cell
with
a
fuel
reservoir,
finger
wing).
Each
wing
is
prov~ded
with
I
drain
for
the
inboitrd
strainer
and
fuel outlet
nipple
through
the
wing
root
rib.
This
wing
leading
edge
fuel
cell
sump;
fuel
strainer;
wing
box
cell
is
interconnected
to
a
wing
box
section
fuel
cell
for
68
section fuel cell
sump.
gallons
usable
in each
wing
system
or a
total of
136
gallons
usable
with
left
and
right
wing
systems
full, One
flush-type
Airplane
serials
TH-6h9
thru
TH-771_.
except
TH-7hh
rquip
filler
cap
is
located
in
the
outboard
end
of
the
wing
box
ped
with
wet
wing
tips
(ZM)
gallon
total
capucity
~yslrmlarc‘
section cell,
A
fuel
selector
panel,
located
on
the cabin
provided
with
a
total
of
6
snap-type
and
flush-type
drain
fuselage
floor forward
of the front
spar
cover,
is
placarded
(4
drains
per
wing).
Each
wing
is
provided
with
I
drain for
OFF-ON-CROSSFEED
for
fuel
management.
Remote
fuel
the inboard
wing
leading
edge
fuel
cell
sump;
fuel
strainer:
8-2