Fuel System Flashcards

(33 cards)

1
Q

What are the fuel quantities for pressure refueling?

A

700, 900, 900EP:
Total: 19,594 lbs
Mains: 7,492 lbs
Center: 4,610 lbs

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2
Q

What are the fuel quantities for gravity refueling (900 and 900EP)?

A

Total: 14,810 lbs
Mains: 7,405 lbs
Center: N/A

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3
Q

What are the fuel quantities for gravity refueling (700)?

A

Total: 14,580 lbs
Mains: 7,290 lbs
Center: N/A

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4
Q

How is the fuel moved from the main tanks to the collector tanks?

A

Scavenge ejectors

Gravity line used as a backup

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5
Q

How is the fuel moved from the center tank to the main tanks?

A

Transfer ejectors

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6
Q

How is fuel moved from the collector tanks to the engine driven high pressure fuel pump?

A

Main ejectors

Backed up by boost pumps

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7
Q

What is the function of the electric boost pumps?

A

To provide initial fuel for engine start and to back-up the main ejectors

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8
Q

What is the flight deck indication of a high pressure fuel pump failure?

A

Engine flameout

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9
Q

When will the fuel system automatically begin transferring fuel?

A

200 lb fuel imbalance

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10
Q

What is the maximum fuel imbalance?

A

300 lb for takeoff

800 lbs for all other phases

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11
Q

When are the boost pump automatically energized?

A

Low pressure from the main ejectors (as long as the boost pumps are armed)

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12
Q

Where is the high pressure fuel pump located?

A

N2 accessory gearbox

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13
Q

Where is the bulk fuel temperature taken?

A

Right Main Tank

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14
Q

What is the Minimum Bulk Fuel Temperature for take-off (Jet A)?

A

-30º C

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15
Q

What is the minimum bulk fuel temperature during flight (Jet A)?

A

above -40º C

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16
Q

How is engine fuel heated?

A

Fuel/oil heat exchanger

17
Q

What is the minimum engine fuel temperature for takeoff?

18
Q

What is the takeoff limitation if the center tank has more than 500 lbs of fuel?

A

Each main tank must have at least 4400 lbs of fuel

19
Q

Which Bus powers the refuel/defuel panel and refuel/defuel SOVs?

A

APU direct battery bus

20
Q

Where is the refuel/defuel panel located?

A

The fuselage forward of the right wing

21
Q

Where is the singe point adapter located?

A

Right Wing Root

22
Q

How are the fuel system faults annunciated?

A

The switch lights on the overhead panel and on EICAS in the form of messages

23
Q

What is used to provide the fuel computer with fuel quantity information?

A

6 fuel quantity probes with compensator units in each of the main tanks and 3 in the center

24
Q

What maintains fuel symmetry between the main tanks?

A

Automatically or manually controlled by the XFLOW pump

25
How are the collector tanks kept full?
Gravity feed lines and scavenge ejectors
26
What is used to back up the main ejectors?
2 electric boost pumps
27
The electric fuel boost pumps...
1) are energized during engine start 2) can feed fuel to either engine from 1 collector tank 3) back up the main ejector pumps
28
From what source is APU fuel feed supplied?
From the left collector tank via APU fuel pump
29
Where is the bulk fuel temp taken?
Right main tank
30
How is pressure refueling and suction defueling accomplished and how is it controlled?
Accomplished through the single point refuel/defuel adapter. Controlled from the refuel/defuel control panel
31
If a fuel asymmetry condition exists between main tanks, what visual amber CAUTION message is presented on EICAS?
FUEL IMBALANCE
32
What fuel system information is displayed on the EICAS Primary page?
Individual tank quantities, total fuel quantity, fuel flow per engine
33
For automatic pressure refueling, what does the refuel/defuel control panel permit?
Preselection of the fuel quantity Built in test feature (BITE) Refuel/defuel SOV's to close automatically if the maximum fuel level is reached