Trans GK Fuels Flashcards

1
Q

What temperature range is the fuel system designed for?

A

Between -40C - 50C

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2
Q

During normal operation, fuel feed to each engine is provided by:

A

The primary jet pump

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3
Q

Motive flow for the primary jet pump is supplied by:

A

The engine-driven fuel pump through the motive flow valve

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4
Q

The boost pump is used during:

A

Engine starting
Fuel crossfeed
Wing tank to feed tank fuel transfer
As a backup for the primary jet pump

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5
Q

Does the boost pump energize automatically during engine start and automatically stop after the engine is started?

A

Yuh (on Gawd)

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6
Q

If a fuel filter becomes clogged, what happens?

A

A filter pressure switch actuates and the filter is bypassed (L F FLTR BYPASS and/or R F FLTR BYPASS annunciator illuminates )

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7
Q

When does the filter bypass valve open, supplying fuel to the engine? (Fuel is unfiltered)

A

When the pressure differential exceeds 2.3 psi

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8
Q

In the automatic mode, the boost pump will operate when:

A

Fuel feed line pressure drops below 5 PSI
Fuel feed chamber volume falls below approximately 11 gallons
Engine starting is selected
Crossfeed is selected

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9
Q

The fuel system has 4 electric pumps, what are they?

A

2 boost pumps
2 transfer pumps

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10
Q
A
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11
Q

One electric boost pump is located where?

A

In each fuel feed chamber

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12
Q

Transfer pumps are used to transfer fuel where?

A

2 transfer pumps are used to transfer fuel from the mid fuselage tanks into the wing tanks

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13
Q

When does the fuel transfer pump automatically shut off (when in AUTO position)

A

When the fuel level within the tank reaches a level slightly above empty and the line pressure drops to 5.0 +/-0.5 PSI

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14
Q

What do you do if the fuel transfer pump operation light remains illuminated with either L or R XFER PRESS LO annunciator illuminated, and the switch is in AUTO?

A

Pull the LH or RH TRANS PUMP C/B to avoid fuel transfer pump damage

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15
Q

What is a jet pump?

A

A low pressure device that transfers energy from a high velocity, low mass, fluid stream to induce a low velocity, high mass fluid stream (motive flow)

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16
Q

Transfer jet pumps are used to:

A

Maintain fuel quantity in each fuel feed chamber (one installed on the aft and forward side of the fuel feed chamber; 2 each wing)