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Differences in Later Refuel/Defuel Panel are as follows:
• The MODE SELECTOR switch is now rotary
• The START/STOP switch now includes the SOV test function
• The master ON/OFF switch is part of the mode selector switch
P I LOT T R A I N I N G GU I D E
GLOBAL 5000 DIFFERENCES
APPENDIX 1
Appx-50 For Training Purposes Only
Sept 04
EICAS MESSAGES
GX_appx_025
CTR TANK FULL
FUEL COMPUTR FAIL
FUEL LO QTY
L (R) FUEL RECIRC FAIL
L (R) PRI FUEL PUMPS
WING TO CTR LEAK
FUEL IMBALANCE
FUEL UNIT MISMATCH
FUEL XFER FAIL
FUEL XFER ON
FUEL XFER FAIL
FUEL XFER ON
FUEL TEMP SENSOR
FUEL UNIT MISMATCH
The refuel/defuel panel and
EICAS indications are correct
but in different units of
measurements.
CTR TANK FULL
Center tank has reached or
exceeded its computer
controlled maximum capacity
of 6100 lbs.
FUEL XFER ON
Indicates that fuel is being
transferred from the left wing
tank to the right wing
unrequested.
FUEL XFER ON
Indicates that fuel is being
transferred from the right wing
tank to the left wing
unrequested.
FUEL COMPUTR FAIL
Indicates that both channels of
the fuel system computer have
failed.
L (R) PRI FUEL PUMPS
Indicates both left or both right
forward and aft primary AC
pumps have failed to operate
when requested.
WING TO CTR LEAK
Indicates that the fuel level in
the center tank has increased by
600 lbs or more.
FUEL XFER FAIL
Transfer from the left wing to the
right wing has been requested
and failed.
FUEL XFER FAIL
Transfer from right wing to left
wing has been requested and
failed.
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.
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
L (R) FUEL RECIRC FAIL (272 kg).
Indicates that the FRTT valve is
not in the commanded or
allowed position.
For Training Purposes Only
Sept 04
Appx-51
P I LOT T R A I N I N G G U I D E
GLOBAL 5000 DIFFERENCES
APPENDIX 1
EICAS MESSAGES (Cont)
APU FUEL SOV
L (R) ENG FUEL SOV
CTR FUEL XFER FAIL
WING FUEL HI TEMP
WING FUEL LO TEMP
L (R) WING FULL
L (R) PRI FUEL PUMP
L (R) AUX FUEL PUMP
CTR XFER FAULT
XFER VALVE OPEN
FUEL XFER ON
XFEED VALVE FAIL
APU FUEL SOV
Indicates that the APU fuel
shutoff valve has failed.
GX_appx_026
L (R) WING FULL
Indicates that fuel quantity in
the left or right wing tank has
exceeded its maximum
allowable value.
L (R) AUX FUEL PUMP
Indicates that the auxiliary fuel
pump on the affected side has
failed to operate when
requested.
WING FUEL HI TEMP
Indicates that the left or right
wing fuel bulk temperature is
above the high temperature
limit.
L (R) ENG FUEL SOV
Indicates that the engine fuel
shutoff valve on the affected
side is not in its commanded
state.
XFER VALVE OPEN
Indicates that the wing transfer
valve has failed to close at the
completion of wing transfer
operation.
CTR FUEL XFER FAIL
Indicates that both left and right
center tank pumps have failed
to operate when requested.
WING FUEL LO TEMP
Indicates that either the left or
right wing fuel bulk temperature
is below -35°C.
L (R) PRI FUEL PUMP
Indicates that a single primary
fuel pump on the affected side
has failed to operate when
requested.
CTR XFER FAULT
Indicates a center fuel transfer
fault exists (either the left or
right fuel transfer is not
working).
FUEL XFER ON
Indicates that the left to right
transfer system is in the AUTO
mode of operation.
XFEED VALVE FAIL
Indicates that the crossfeed valve
is not in its commanded position.
P I LOT T R A I N I N G GU I D E
GLOBAL 5000 DIFFERENCES
APPENDIX 1
Appx-52 For Training Purposes Only
Sept 04
EICAS MESSAGES (Cont)
FUEL XFER ON
XFER VALVE OPEN
FUEL COMPUTR FAULT
　
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