FUEL SYSTEM (CSG) Flashcards

1
Q

Fuel System

Each wing has a useable fuel capacity of ________ gallons.

A

201

AOH Vol 2, Section 18

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2
Q

Fuel System

How many fuel drains are on the aircraft and where are they located?

A

6; Fuel filter, fuel/air sep, wing main (2) and coll tank (2)

AOH Vol 2, Section 18

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3
Q

Fuel System

(T/F) A check valve is installed in the motive flow line at each collector tank to prevent fuel flow between the left and right wing tanks.

A

True

AOH Vol 2, Section 18

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4
Q

Fuel System

(T/F) Inward and Outward fuel vents are used under each wing to ensure safe pressure inside the fuel tanks.

A

True

AOH Vol 2, Section 18

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5
Q

Fuel System

During normal operations, what process moves fuel from the main tanks to the collector tanks and on to the engine?

A

Motive Flow distribution system

AOH Vol 2, Section 18

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6
Q

Fuel System

Can the low pressure engine driven fuel pump be bypassed if the pump fails?

A

Yes

AOH Vol 2, Section 18

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7
Q

Fuel System

The fuel low pressure switch closes and turns on the boost pumps when fuel pressure decreases below _____ psi. The switch opens again when pressure increases above _____ psi.

A

2, 3.5

AOH Vol 2, Section 18

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8
Q

Fuel System

What should you do if you find the red button on the fuel filter is popped during the walk-around inspection?

A

Notify Maintenance; do not fly until corrected

AOH Vol 1, Normal Procedures

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9
Q

Fuel System

What does the Firewall Shutoff Valve do and when would you activate it?

A

stops fuel flow to the engine at the fire wall shutoff valve; emergency procedure for confirmed engine fire or emergency landing after engine failure

AOH Vol 2, Section 18

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10
Q

Fuel System

What does the Oil to Fuel Heat Exchanger do?

A

Uses warm oil to heat up fuel prior to entering FCU

AOH Vol 2, Section 27

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11
Q

Fuel System

What will happen if the High Pressure Engine-Driven Fuel Pump fails?

A

Engine rollback and likely flameout

AOH Vol 2, Section 27

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12
Q

Fuel System

The fuel balancing system keeps fuel balanced to within ______ % (____ gal) of full
wing tank amount or approximately ________ segments on the analog fuel gauge.

A

5, 10.5, 2

AOH Vol 2, Section 18

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13
Q

Fuel System

How is the digital FUEL QTY gauge updated after refueling?

A

Press FUEL RESET switch on EIS

AOH Vol 2, Section 18

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14
Q

Fuel System

When checking for fuel availability in the Chart Supplement or DOD IFR Supp, what
does a “+” indicate after a listed fuel type? Why should you care?

A

FSII (PRIST) added to the fuel; must have FSII in contract fuel, and always needed to fly in temperatures below freezing

AOH Vol 1, Chapter 5

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15
Q

Fuel System

What is PRIST?

A

Type of fuel additive that lowers freezing point of water in fuel; prevents ice crystals from forming

AOH Vol 1, Chapter 5; in-class discussion

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16
Q

Fuel System

When do the L FUEL LOW and R FUEL LOW CAWS lights illuminate?

A

20 gal remaining in respective collector tank

AOH Vol 2, Section 18

17
Q

Fuel System

What are some possible causes for a FUEL PRESS CAWS light?

A

Ice crystals in fuel, failure of low press engine driven fuel pump, other contamination

AOH Vol 1, Chapter 3; in-class discussion

18
Q

Fuel System

If there are _____ or more segments difference between the left and right analog
fuel gauges prior to takeoff, do not take off.

A

4

AOH Vol 1, Chapter 3

19
Q

Fuel System

If there are ______ segments or more difference between left and right, possible
aileron deflection required for wings level flight, especially at low speed.

A

3

AOH Vol 1, Chapter 3

20
Q

Fuel System

For a suspected fuel leak situation, consider burning off fuel until the fuel imbalance
is not greater than _____ segments for landing. Use flaps up to keep approach
speed high.

A

5

AOH Vol 1, Chapter 3