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Fuel System PART 1

Authored by Abhishek Verma

Engineering

Vocational training

Used 1+ times

Fuel System PART 1
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15 questions

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1.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

Which subsystem ensures fuel is supplied from tanks to the engines during normal operation?

Pressure refueling subsystem

Fuel storage subsystem

Engine fuel feed subsystem

Fuel quantity indicating subsystem

2.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

In maintenance documentation, what does FQIS stand for?

Fuel quantity indicating system

Fuel quality inspection system

Fuel quick-installation system

Fuel quantity isolation System

3.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

Media Image

A maintenance team encounters light frost on the upper wing surface while fuel in the main tanks is at or below 32°F (0°C). Which action aligns with CSFF procedures when any AMM conditions are not met?

Walk the wing to visually confirm frost thickness

Allow frost if limited to lower wing surfaces

Apply deicing or anti-icing fluids to remove frost

Proceed without deicing and continue preflight checks

4.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

Which statement best describes the surge tank function in this aircraft’s fuel system?

Houses boost pumps for crossfeed operation

Balances wing weight during asymmetric loading

Stores additional usable fuel for engine feed

Collects overflow and vents excess fuel safely

5.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

Media Image

In the wing diagram, which pair of ribs bounds the surge tanks for the main tanks, determining where surge tank access doors are located?

Ribs 1 and 5 near side-of-body

Ribs 5 and 22 mid-wing area

Ribs 22 and 25 near the tip

Ribs 8 and 12 outboard ribs

6.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

At the right-wing refueling station, which power source will allow refueling when the airplane is connected to external power but the battery switch is OFF?

Switched hot battery bus available power

APU supplying DC bus 2

BPCU internal transformer rectifier

Ground service bus

7.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

Refueling valves are actuated by which control during normal operations?

Pneumatic actuator with bleed air

Hydraulic ram driven by engine pump

Mechanical linkage from cockpit lever

Solenoid controlled by fuel pressure

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