SV Fuel Flashcards

1
Q

The expanded fuel quantity display appears when: [8.120.20]

A

A. One or more fuel quantity indicators are inoperative. B. The FUEL QTY LOW message is displayed.
C. The EICAS message FUEL IMBALANCE is displayed. D. All the above

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2
Q

Actual fuel temperature is displayed on . [8.120.10, 8.120.20]

A

A. EICAS
B. FUEL synoptic
D. Both A and B

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3
Q

T or F
The DC powered fuel pump is located in the left main tank. [8.70.30]

A

A. True

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4
Q

The DC fuel pump operates automatically when: [8.70.30]

A

C. The APU is started without AC power available

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5
Q

The CDU message INSUFFICIENT FUEL indicates: [8.120.30]

A

B. Predicted fuel at destination will be less than entered reserves

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6
Q

When all available fuel has been jettisoned, there will be: [8.120.10]

A

D. 8700 pounds remaining in each main fuel tank

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7
Q

On the ground, the fuel jettison system: [8.120.10]

A

A. Is inhibited

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8
Q

A DC powered fuel pump located in the tank provides fuel for APU start if AC power is not available. [8.70.30, 8.120.10]

A

C. Left main

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9
Q

The fuel balance system is inhibited: [8.120.10]

A

A. During defueling, refueling or ground transfer of fuel. B. With the fuel jettison system armed.
C. On the ground and one or both engines are running. D. All the above

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10
Q

Placing the left fuel jettison NOZZLE switch to ON in-flight with the jettison system ARMED will: [8.120.10]

A

A. Open both main tank jettison isolation valves.
B. Open both center tank jettison isolation valves.
D. A and B.

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11
Q

Placing the fuel jettison ARM switch to the ARMED position causes the Fuel To Remain indication to be displayed: [8.120.10]

A

C. On both the EICAS fuel display and FUEL synoptic

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12
Q

Fuel jettison time is displayed: [8.120.10]

A

D. On the FUEL synoptic only

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13
Q

The center tank scavenge system will begin to transfer fuel from the center tank when: [8.120.10]

A

A. Either main tank quantity is below 35,000 pounds and both center tank pumps are off

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14
Q

When balancing fuel, what indication(s) appear when the main tank fuel is balanced? [8.120.20]

A

A. A flashing FUEL BALANCED indication replaces the Fuel Quantity title on the expanded quantity display.

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15
Q

The minimum fuel temperature is displayed on the: [8.110.20, 8.120.10]

A

C. CDU PERF INIT page and the FUEL synoptic

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16
Q

On the ground or in flight, certain fuel pumps may load shed when: [8.120.10]

A

A. Less than all engines or generators are operating.

17
Q

If a center tank pump has low output pressure with low center tank quantity, the ______ EICAS message is displayed. [8.120.20]

A

C. FUEL LOW CENTER

18
Q

The minimum fuel temperature is entered on the: [8.110.20]

A

D. CDU PERF INIT page

19
Q

The minimum fuel temperature should be set to fuel freeze temperature. [8.110.20]

A

A. 3° above

20
Q

A FUEL CROSSFEED advisory message displayed on EICAS indicates: [8.120.10]

A

B. The crossfeed valve position disagrees with the switch position

21
Q

When the fuel jettison system is ARMED, the fuel to remain is automatically set to a quantity that will when jettison is complete. [8.120.10]

A

D. Have the airplane weight at the maximum landing weight

22
Q

The center fuel tank pump pressure lights illuminate: [8.120.20]

A

A. When pump pressure is low with the pump switch selected ON

23
Q

An EICAS message FUEL JETTISON MAIN indicates: [8.120.30]

A

D. Fuel jettison from the main tanks is inoperative

24
Q

During normal operations, the APU receives fuel from the: [8.120.10]

A

A. Left fuel manifold

25
Q

Where does the APU get its fuel? [8.120.10]

A

D. Any fuel tank that has an operating fuel pump

26
Q

An amber fuel temperature on the EICAS indicates: [8.120.10]

A

A. The fuel temperature is approaching the maximum allowable temperature
C. The fuel temperature is approaching the fuel freeze temperature that was entered in the CDU
D. Both A and C