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Compensators
Densitometer
Temperature
Hi/Lo Level
Pump Pressure Switches
SOVs Position Feedback
Cockpit Control
Panel
Cockpit Fuel
Fire Handles
Panel
APU On
L Engine On
R Engine On
Fuel System
Components
Refuel
Defuel
Panel
Displays Data:
Total Fuel Quantity
Individual Tank Quantities
Preselect Quantity
Alert Messages
Boost Pumps INHIB
Wing Transfer Mode
Aft Transfer Mode
XFEED Mode
Input and output
Input or output
LEGEND
Engine Start
GF1210_030
FUEL
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
12−10−32
EICAS MESSAGES
GF1210_031
WING TO CTR LEAK
Indicates that the fuel
level in the centre tank
has increased by 600
lbs or more.
L−R PRI FUEL PUMPS
Indicates that the forward
and aft primary AC pumps
on the affected side have
failed to operate when
requested.
FUEL COMPUTR FAIL
Indicates that both
channels of the fuel
system computer have
failed.
AFT XFER OFF
SCHED
Indicates that fuel
transfer from the aft
tanks to the wings is
unable to keep pace
with the optimum aft
transfer schedule.
−> FUEL XFER FAIL
Transfer from the left
wing to the right wing
has been requested and
failed.
FUEL UNIT MISMATCH
The refuel/defuel panel
and EICAS indications
are correct but in different
units of measurements.
FUEL IMBALANCE
Indicates that a fuel quantity imbalance
exists between the left and right wing
tanks of:
More than 1100 lbs (499 KG) in flight.
Between 600 lbs (272 KG) and
1100 lbs (499 KG) on ground or in
Takeoff
/ Approach configuration.
FUEL LO QTY
Indicates fuel in the left
or right wing tank is less
than 600 lbs (272 KG).
<− FUEL XFER FAIL
Transfer from right wing
to left wing has been
requested and failed. −> FUEL XFER ON
Indicates that fuel is
being transferred from
the left wing tank to the
<− FUEL XFER ON right wing unrequested.
Indicates that fuel is
being transferred from
the right wing tank to the
left wing unrequested.
FUEL TEMP SENSOR
On ground, indicates that a
fuel temperature sensor is
failed. With flaps deployed,
will be posted only if the failure
requires corrective action.
L−R FUEL RECIRC FAIL
Indicates that the FRTT
valve is not in the
commanded or allowed
position.
On airplanes with
SB 70028036
incorporated:
Indicates that the FRTT
valve is not in the
commanded position.
FUEL IMBALANCE
FUEL COMPUTR FAIL
L−R PRI FUEL PUMPS
FUEL UNIT MISMATCH
WING TO CTR LEAK
AFT XFER OFF SCHED
FUEL TEMP SENSOR
L−R FUEL RECIRC FAIL
FUEL LO QTY
−> FUEL XFER FAIL
−> FUEL XFER ON
<− FUEL XFER FAIL
<− FUEL XFER ON
FUEL
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
12−10−33
EICAS MESSAGES (CONT'D)
AFT XFER FAIL
Both left and right aft transfer
components have failed to
operate when requested. Aft
tank fuel is no longer
available.
CTR FUEL XFER FAIL
Indicates that both left
and right centre tank
pumps have failed to
operate when
requested.
L−R WING FULL
Indicates that fuel quantity
in the affected wing tank
has exceeded its
maximum allowable value.
WING FUEL HI TEMP
Indicates that the left or
right wing fuel bulk
temperature is greater
than 42°C.
On airplanes with
SB 70028034
incorporated:
If Fuel ReCirculation
system is On:
Indicates that the left or
right wing fuel bulk
temperature is greater
than 0°C.
If Fuel ReCirculation
system is Off:
Indicates that the left or
right wing fuel bulk
temperature is greater
than 42°C.
WING FUEL LO TEMP
Indicates that either the
left or right wing fuel
bulk temperature is at
or below −35°C.
L−R ENG FUEL SOV
Indicates that the
engine fuel shutoff
valve on the affected
side is not in its
commanded state.
APU FUEL SOV
Indicates that the APU fuel
shutoff
valve has failed.
AFT XFER FAIL
APU FUEL SOV
L−R ENG FUEL SOV
　
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