(2)  
Putting the FUEL QTY test switch in the FUEL QTY position will cause the subsequent:

 (a)  
The left, center, and right fuel quantity indicators on the overhead panel, P5, will show 88.8.

 (b)  
The total fuel quantity indicator on the P5 panel will show

 188.8.
 (c)  
The fuel temperature indicator on the P5 panel will show -185 |2.

 (d)  
The FUEL CONFIG light on the P5 panel will come on.

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DENSITOMETER FUEL
RETENTION SYSTEM

SEE A
DENSITOMETER (REF) 
RIGHT WING SHOWN 
REAR SPAR 
DENSITOMETER 
ELECTRONICS  FROM THE 
UNIT  FUELING 
MANIFOLD 
RETENTION 
CANISTER 

FLOAT VALVE
DENSITOMETER FUEL RETENTION SYSTEM
A
Center Tank Densitometer Fuel Retention System

Figure 6A

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FUEL QUANTITY

FLIGHT COMPARTMENT

TEST
AIR DATA CONFIG L CMPTR R T/O GND PROX

L STALL R LDG INOP
WING DUCT YAW DMPR EQUIP COOL ANTI ICE LEAK L FWD

FUEL QUANTITY
FUEL QUANTITY INDICATOR, M10054 TEST SWITCH, S6

MISCELLANEOUS TEST PANEL, M10398 (REF) (EXAMPLE PANEL SHOWN)

THE UNITS ARE IN LBS OR KGS.
Fuel Quantity Indicator
Figure 7

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 (e)  
The EICAS caution message, LOW FUEL, will show on the top display.

 (f)  
The EICAS status message, FUEL QTY IND, will show on the bottom display.
　
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