SYS107 Flashcards

1
Q

The motive flow system is normally driven by the electric boost pump. (T/F)?

A

False, it is driven by the primary and transfer jet pumps.

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2
Q

When using the primary refueling method, the total amount of usable fuel in the tanks is approximately
__________ pounds.

A

1100

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3
Q

The collector tank holds a maximum of approximately __________ pounds of fuel

A

40

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4
Q

What is the primary method of refueling the T-6A?

A

Single point pressure refueling

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5
Q

Using the single point pressure refueling method, approximately how long does it take to refuel the aircraft?

A

3-5 minutes

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6
Q

The secondary or backup method for refueling the T-6A is called __________ refueling.

A

over the wing gravity

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7
Q

The engine-driven high-pressure fuel pump is fed from the

A

engine-driven low pressure fuel pump

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8
Q

The motive flow line routes fuel to which of the following pumps?

A

primary jet pump and transfer jet pump

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9
Q

The collector tank is equipped with two fuel pumps for engine feed operations. Which one is used after
engine start?

A

primary jet pump

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10
Q

During negative-G flight, the flip-flop valve activates, providing the engine access to fuel located in the

A

collector tank

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11
Q

Once the engine is running and motive flow has been activated, the boost pump is automatically turned off by the low pressure switch. (T/F)?

A

True. If the lines drop below 10 psi the boost pump will activate.

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12
Q

The wing tanks are internally vented to each other by ___________

A

a cross-vent line

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13
Q

The fuel system incorporates an auto balance system which maintains the fuel load in each wing tank to within __________ pounds of the other wing

A

20

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14
Q

Using the primary refueling method, the maximum fuel quantity for one wing tank is __________ pounds.

A

530

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15
Q

The flip-flop valve in the collector tank provides a minimum of __________ seconds of fuel regardless of aircraft orientation

A

60

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16
Q

Which method of refueling fills the wing tanks simultaneously?

A

single point pressure refueling

17
Q

Which of the following maintains fuel balance by shutting off fuel flow to the light wing tank?

A

transfer (solenoid) valve

18
Q

The primary and transfer jet pumps are operated by

A

Venturi flow

19
Q

How long does it take to defuel the T-6A through the over the wing gravity refueling ports?

A

The T-6A cannot be defueled through the over the wing gravity refueling ports.

20
Q

Fuel is routed from the engine-driven fuel pump to the primary jet pump through which line?

A

motive flow line

21
Q

The left and right fuel quantity arrows on the AEDD turn yellow when indicated fuel quantity in the respective tank is below __________ pounds.

A

150