(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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本文链接地址：757 AMM 飞机维护手册 燃油 CHAPTER 28 - FUEL 4(94)
