Section 05 - Fuel Flashcards

1
Q

What might cause the illumination of a red “FUEL PRESS LOW” CAS message?

A
  1. Both fuel boost pumps for that engine switched OFF with the cross flow closed
  2. fuel pressure at the inlet side of the high pressure fuel pump less than 15 PSI
  3. Fuel leak
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2
Q

How is a fuel imbalance corrected using the cross flow valve?

A

By opening the cross flow valve and turning off the fuel pumps on the light wing

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3
Q

What are the correct indications during the fuel quantity indicator test?

A

L - 7,000 R - 7,000 Total - 14,000

Amber L-R FUEL LEVEL LOW CAS message

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4
Q

Where is the fuel hopper located?

A

In the inboard portion of each wing tank

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5
Q

Fuel low-level warning is provided by low-level sensors, which are installed where in the wing?

A

In the fuel hopper tank

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6
Q

Where are the electric fuel boost pumps located?

A

In the main wheel well

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7
Q

What is the function of the pressure fueling static port located under each wing?

A

It provides a reference pressure to prevent over-pressurization of the wing during fueling operations

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8
Q

How are the main fuel shutoff valves checked during the preflight walk-around?

A

Verify that the valves are open by physically checking that the red valve position indicator is in approximately the seven o’clock position

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9
Q

When and how is a fuel quantity update performed?

A

Hourly, using data from the FQMS. On FMS PERF INIT page 5/5, perform a “DELETE” to line select key 2L

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10
Q

What are the electrical power sources of the fuel boost pump?

A

L & R MAIN: ESS DC bus

L & R ALT: R MAIN DC

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11
Q

How much fuel is remaining in the hopper when an amber left or right “FUEL LEVEL LOW” CAS message appears?

A

Approximately 650 lbs

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12
Q

What is the capacity of each fuel hopper tank?

A

190 gallons

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13
Q

What is the maximum standard fuel load?

A

29,500 lbs, more can be added provided max ramp and max takeoff weights are not exceeded, and the loaded airplane center of gravity is within limits

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14
Q

What is the maximum fuel imbalance?

A

Varies with aircraft weight, reference chart in QRH, Section EF

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15
Q

If a main fuel boost pump should fail, will the alternate fuel boost pump automatically turn on, if selected OFF?

A

Yes, there is a boost pump auto-change feature.

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16
Q

If you are powering the aircraft with the HMG only, what components of the fuel system will be available?

A

L & R MAIN BOOST pumps

Crossflow & Intertank Valve

17
Q

If an engine fire handle is pulled, where is the fuel shut off?

A

At the boost pumps in the main wheel well

18
Q

The engine should run without boost pump pressure up to what maximum altitude?

A

20,000ft

19
Q

If two boost pumps fail on the same side, how would you keep the fuel balanced?

A

By opening the intertank valve and using sideslip (nose of the aircraft toward the heavy wing)

20
Q

How are the hopper tanks kept full?

A

Flapper valves and ejector pumps

21
Q

Where can fuel quantity indications be read?

A
  1. On DU #3, engine instruments display
  2. Standby fuel quantity indicator
  3. On the FUEL synoptic page
22
Q

What is the difference between “fuel temperature” and “engine fuel temperature“?

A

Fuel temperature (found on the FUEL synoptic page) is the temperature of the fuel in the left hopper. Engine fuel temperature is the temperature of the fuel as it exits the engine oil cooler.

23
Q

What does the “CB” light in each boost pump control switch indicate?

A

The respective circuit breaker on the PDB is tripped.

24
Q

What is the maximum fuel imbalance at 55,000 lbs airplane gross weight?

A

2,000lbs

25
Q

What is the maximum fuel imbalance at 61,000 lbs airplane gross weight?

A

400 lbs

26
Q

What is the maximum engine fuel temperature?

A

90ºC (fuel temperature up to 120ºC for a maximum of 15 minutes is permissible)

27
Q

What is the minimum engine fuel temperature?

A

-40ºC