Fuel Flashcards

1
Q

When must the FUEL X-FEED knob be set to OFF?

A

For takeoff, landing and go-around

AOM 9-10-30 and AOM 2-36

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2
Q

Which MFD page provides a visual representation of the fuel system operation and parameters?

A

The FUEL synaptic page

AOM 9-10-30

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3
Q

What color does the total and individual tank quantities and fuel temperature indications indicate when in the normal operating range?

A

Green

AOM 9-10-30

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4
Q

When the total fuel quantity is displayed in red, which aural warning is played twice?

A

FUEL

AOM 9-10-50

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5
Q

Can fuel be transferred from one wing to another?

A

No

AOM 9-10-50

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6
Q

How does the crossfeed valve allow corrections in the event of a fuel load imbalance?

A

It allows both engines and/ or the APU to be fed by one tank

AOM 9-10-50

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7
Q

Which CAS message is displayed on the EICAS when the difference between current and expected fuel quantities is higher than 880lbs for 5 mins

A

FUEL LEAK SUSPECTED

AOM 9-10-50

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8
Q

How many fuel pumps does each fuel tank have?

A

Two DC fuel pumps (Main A and Backup B) and 2 scavenge pumps

AOM 9-10-50

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9
Q

What controls the backup (B) pump when the fuel pump is in the AUTO position

A

The FCU

AOM 9-10-50

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10
Q

List the four times when the backup (B) pump will be automatically commanded on when the fuel pump is in the AUTO position

A

1) During Engine Start
2) APU start on the run
3) fuel low pressure detetection
2) When the main (A) pump fails

AOM 9-10-50

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11
Q

When will the Amber FUEL WING IMBALANCE CAS message be displayed on the EICAS

A

When the fuel imbalance between the tanks is higher than 510 lbs

AOM 9-10-500

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12
Q

Where is the pressure refueling point and the REFUELING/DEFUELING control panel located at

A

Forward portion of the right wing fuselage

AOM 9-10-50

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13
Q

How long does the system pre-check on the REFUELING/ DEFUELING panel take to verify fuel system operation

A

Approximately 10 seconds

AOM 9-10-50

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14
Q

Which switch located on the REFUELING/DEFUELING panel pressurized refueling to be performed with the airplane energized by either the APU/GPU or battery power

A

The power selection switch

AOM 9-10-50

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15
Q

What should happen if the STOP REFUEL is displayed on the REFUELING/ DEFUELING control panel during the refueling process?

A

The process shall be halted manually by the operator by moving the refueling switch to the off position

AOM 9-10-50

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16
Q

May the tanks be refueled using gravity refuel port on the top of each wing

A

Yes

AOM 9-10-50

17
Q

What are the two different methods that the airplane can be de-fueled

A

Suction and pressure

AOM 9-10-50

18
Q

Can the forward or ventral tanks in the Praetor 600 be refueled via gravity

A

No, only via pressure

AOM 9-10-50

19
Q

How is the fuel transferred from the FWD or VTRL tanks and where

A

Automatically to both wings simultaneously

AOM 9-10-50

20
Q

Can fuel be transferred from the FWD/VTRL tanks to each other?

A

No, only to the wings

AOM 9-10-50

21
Q

If the AUTO function of the fuel panel for the FWD/VTRL tanks fail, how do we access the remaining fuel

A

By selecting either the FWD or VTRL on the FUEL TRANSFER panel

AOM 9-10-30

22
Q

When is transfer operations from FWD or VTRL tanks not allowed

A

During X Feed, takeoff, landing and go around

AOM 9-10-35