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CSP A-
013
Vol. 1
13-
60-
2
FUEL SYSTEM
REV56,Jan 31/03
Fuel Quantity Gauging
<0039> <0006>
Primary Page
<0039>
FUEL CH 1, 2 FAIL
status (white) Comes ontoindicate that the respectivechannelof the fuel system computer has failed.
<0039>
Status Page
Refuel/Defuel ---EICAS Messages <MST> Figure 13---60---1
Flight Crew Operating Manual
MASTER
CSP A-
013
Vol. 1
13-
60-
3
FUEL SYSTEM Fuel Quantity Gauging
REV56,Jan 31/03
FUEL USED Quantity Readout
Indicates the amount of fuel used, i.e. , in lbor in kg<0001>. Five amber dashes are displayedif input data is invalid.
P
Fuel PageFUEL CH 1/2 FAIL status (white)
Comes on to indicate that the respective channelof the fuelsystem computer has failed.
FUEL CH 1/2 FAIL caution (amber)
Comes on to indicate that both channels of the fuelsystem computer has failed.
FUEL CH (1,2) FAIL status (white)
Comes on to indicate that the respective channelof the fuelsystem computer has failed.
Refuel/Defuel System ---Fuel Synoptic Page Indications <MST>
Figure 13---60---2
Flight Crew Operating Manual
MASTER
CSP A-
013
FUEL SYSTEM Fuel Quantity Gauging Vol. 1 13-
60-
4
REV 56, Jan 31/03
Flight Crew Operating Manual MASTER
CSP A-
013
FUEL SYSTEM Vol. 1 13-
60-
5
Fuel Quantity Gauging REV 56, Jan 31/03
A. Magnetic Level Indicators
Two magnetic levelindicators (MLI’s)are installedin each wingtankand oneis installed in thecentertank. TheMLIs are locatedunderthe wingand are usedto manually checkthefuellevelin eachtank.
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