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A380

Total questions: 52

Worksheet time: 26mins

Name
Class
Date
1.

What are the two main types of fuel tanks on the A380?

a)

Inner and Outer Tanks

b)

Main and Standby Tanks

c)

Fuel Storage and Transfer Tanks

d)

Auxiliary and Primary Tanks

2.

Which of the following is NOT a part of the Main Tank?

a)

Feed Tank

b)

Inner Tank

c)

Mid Tank

d)

Trim Tank

3.

What is the function of the Feed Tank?

a)

Stores extra fuel for backup

b)

Directly supplies fuel to the engine

c)

Balances the aircraft’s center of gravity

d)

Removes contaminants from the fuel

4.

Why is the Trim Tank important?

a)

It helps with aircraft stability by adjusting center of gravity

b)

It serves as a backup fuel source

c)

It filters impurities from the fuel

d)

It prevents excess fuel evaporation

5.

What is the most common type of fuel contamination?

a)

Water

b)

Oil

c)

Carbon deposits

d)

Dirt

6.

How is water contamination in fuel prevented?

a)

Heating the fuel

b)

Using fuel additives

c)

Filtering the fuel before use

d)

Mixing fuel with engine oil

7.

Which fuel system component is most affected by fuel contamination?

a)

Fuel Pump

b)

Fuel Valve

c)

Fuel Filter

d)

Fuel Injector

8.

Why is fuel system maintenance important in the A380?

a)

Prevents fuel leaks and contamination

b)

Reduces passenger weight

c)

Improves in-flight entertainment

d)

Reduces engine noise

9.

Why is a Fuel Filter important?

a)

It separates fuel and air

b)

It removes contaminants from the fuel

c)

It transfers fuel between tanks

d)

It regulates fuel pressure

10.

What is the primary function of the APU?

a)

Powering the landing gear

b)

Providing electrical power when engines are off

c)

Storing excess fuel

d)

Cooling the cockpit

11.

What happens if the Check Valve fails?

a)

Fuel leaks into the cabin

b)

Fuel may flow backward, causing pressure loss

c)

The fuel filter stops working

d)

The engine overheats

12.

Which of the following is NOT a reason to declare a fuel emergency?

a)

Fuel contamination

b)

Unexpected fuel loss

c)

Fuel imbalance

d)

Fuel temperature above normal

13.

Which of the following is NOT a part of the main tank?

a)

Feed Tank

b)

Inner Tank

c)

Mid Tank

d)

Trim Tank

14.

What is the function of the Feed Tank?

a)

Stores extra fuel for backup

b)

Directly supplies fuel to the engine

c)

Balances the aircraft's center of gravity

d)

Removes contaminants from the fuel

15.

Why is the trim tank important?

a)

It helps with aircraft stability by adjusting center of gravity

b)

It serves as a backup fuel source

c)

It filters impurities from the fuel

d)

It prevents excess fuel evaporation

16.

Which tank is responsible for handling excess fuel and pressure?

a)

Inner Tank

b)

Surge Tank

c)

Outer Tank

d)

Feed Tank

17.

What happens if a fuel pump fails during flight?

a)

The engine automatically shuts down

b)

The aircraft uses gravity feed to supply fuel

c)

The pilot performs an emergency landing

d)

The APU takes over fuel supply

18.

How is fuel pressure maintained in the A380?

a)

By using multiple fuel pumps

b)

By heating the fuel

c)

By mixing fuel with oil

d)

By reducing aircraft speed

19.

Why is fuel pressurization important?

a)

Prevents cavitation and fuel starvation

b)

Reduces fuel temperature

c)

Prevents excessive fuel storage

d)

Increases aircraft weight

20.

What safety feature prevents overpressure in the fuel system?

a)

Pressure relief valve

b)

Fuel jettison valve

c)

Gravity feed line

d)

Check valve

21.

What is the primary reason for using multiple fuel pumps in the Airbus A380?

a)

To increase fuel efficiency

b)

To ensure continuous fuel supply in case of pump failure

c)

To reduce aircraft weight

d)

To prevent fuel contamination

22.

How does the Airbus A380 prevent excessive fuel loss during an engine failure?

a)

By automatically shutting off the affected engine’s fuel supply

b)

By redirecting fuel to the APU

c)

By jettisoning excess fuel

d)

By mixing fuel with air to reduce consumption

23.

What is the function of the Fuel Jettison System in the Airbus A380?

a)

To transfer fuel between tanks for balance

b)

To remove excess fuel in case of an emergency landing

c)

To store reserve fuel for extended flights

d)

To cool down the aircraft’s hydraulic systems

24.

Why does the Airbus A380 have a fuel recirculation system?

a)

To prevent fuel freezing at high altitudes

b)

To increase fuel tank capacity

c)

To distribute fuel evenly across all tanks

d)

To transfer excess fuel to the APU

25.

Which of the following is NOT a type of tank in the Airbus A380 fuel system?

a)

Feed Tank

b)

Inner Tank

c)

Gravity Tank

d)

Trim Tank

26.

What is the function of the Trim Tank in the Airbus A380?

a)

Directly supplies fuel to the engines

b)

Stores reserve fuel to be transferred later

c)

Helps balance the center of gravity for efficiency

d)

Filters fuel before it reaches the engines

27.

How much contingency fuel (5%) is required for a trip fuel of 180,000 kg?

a)

7,500 kg

b)

9,000 kg

c)

10,000 kg

d)

12,000 kg

28.

What is the purpose of the fuel refueling valve in the Airbus A380?

a)

Moves fuel from auxiliary tanks to main tanks

b)

Helps prevent fuel from flowing back through the fuel inlet

c)

Regulates fuel flow into the aircraft during refueling

d)

Removes sediment and water from fuel

29.

What is the function of the crossfeed valves in the A380 fuel system?

a)

They prevent fuel contamination.

b)

They allow fuel to be transferred between tanks for balance and efficiency.

c)

They increase the pressure in the fuel system.

d)

They regulate fuel temperature.

30.

How does the flow meter assist in monitoring and managing fuel consumption in an aircraft?

a)

It calculates the total fuel capacity.

b)

It measures the fuel temperature.

c)

It measures real-time fuel consumption and detects irregularities.

d)

It controls the fuel pumps.

31.

What is the purpose of the trim tank in the A380, and where is it located?

a)

It stores extra fuel for long-haul flights and is located in the wings.

b)

It balances the aircraft’s center of gravity and is located in the tail section.

c)

It filters impurities in the fuel system and is located near the engines.

d)

It prevents fuel overheating and is located in the fuselage.

32.

Based on the refueling process, how much time is required for dispenser positioning, connection, disconnection, and removal?

a)

10 minutes

b)

16 minutes

c)

20 minutes

d)

25 minutes

33.

What is the role of the High-Pressure (HP) Fuel Pump in the aircraft fuel system?

a)

To store reserve fuel

b)

To maintain CG balance

c)

To increase fuel pressure before combustion

d)

To heat the fuel before transfer

34.

Which component prevents fuel from flowing backward?

a)

Heat Exchanger

b)

LP Fuel Pump

c)

Check Valve

d)

Surge Tank

35.

What is the function of the Heat Exchanger?

a)

Heats fuel to melt ice

b)

Cools the engine

c)

Increases fuel pressure

d)

Transfers fuel between tanks

36.

How many types of fuel tanks does the Airbus A380 have?

a)

1

b)

2

c)

3

d)

4

37.

What is the primary function of the trim tank in the Airbus A380 fuel system?

a)

To store additional fuel for long-haul flights

b)

To balance the aircraft's center of gravity for efficiency

c)

To filter impurities from the fuel before it reaches the engine

d)

To act as a backup fuel tank in case of engine failure

38.

What component prevents fuel from flowing backward in the fuel system?

a)

Heat Exchanger

b)

HP Fuel Pump

c)

Transfer/Check Valve

d)

Flow Meter

39.

What is the function of the heat exchanger in the Airbus A380 fuel system?

a)

To transfer fuel between tanks

b)

To regulate fuel pressure in the engine

c)

To heat the fuel and melt any ice formed

d)

To monitor the amount of fuel consumed

40.

Which of the following components is responsible for ensuring a steady and reliable fuel flow to the engine-driven high-pressure fuel pump?

a)

APU

b)

LP/Transfer Fuel Pump

c)

Surge Tank

d)

Refueling Valve

41.

How does fuel load affect the Airbus A380’s takeoff performance?

a)

A heavier fuel load increases takeoff distance

b)

A heavier fuel load decreases takeoff distance

c)

Fuel load has no effect on takeoff

d)

The A380 is designed to take off with a fuel load without issue

42.

What is the fuel tank capacity of the Airbus A380’s wings alone (excluding the horizontal stabilizer)?

a)

100,000 liters

b)

200,000 liters

c)

300,000 liters

d)

320,000 liters

43.

Which airline tested biofuel on an Airbus A380 for a more sustainable future?

a)

Emirates

b)

Lufthansa

c)

Qantas

d)

British Airways

44.

How does the A380 manage fuel distribution during a flight?

a)

Uses all tanks equally

b)

Burns fuel from the wings first

c)

Uses tail fuel first for balance

d)

Transfer fuel between tanks for stability

45.

Which of the following is NOT a type of standby tank in the Airbus A380?

a)

Outer Tank

b)

Trim Tank

c)

Inner Tank

d)

Surge Tank & Vent Surge Tank

46.

Which of the following is types of fuel tank that connected with Engine Number 1 in the Airbus A380?

a)

Outer tank

b)

Inner Tank Left Wing

c)

Feed Tank 1 Left Wing

d)

Surge Tank Left Wing

47.

How many Jettison Nozzle Valve in an Airbus A380?

a)

2

b)

6

c)

3

d)

4

48.

What is the largest fuel tank in an Airbus A380?

a)

Mid Tank

b)

Inner Tank

c)

Surge Tank

d)

Trim Tank

49.

Which of the following tanks is responsible for fuel distribution across the Airbus A380’s wings?

a)

Feed Tank

b)

Trim Tank

c)

Surge Tank

d)

Inner Tank

50.

What is the primary purpose of the Surge Tank in the Airbus A380?

a)

To store emergency fuel

b)

To handle excess fuel and pressure

c)

To regulate fuel temperature

d)

To filter contaminants from the fuel

51.

What happens to fuel when it passes through the Fuel Filter in the Airbus A380 system?

a)

It is mixed with engine oil for lubrication

b)

It is filtered to remove water and other contaminants

c)

It is stored for future use

d)

It is sent to the outer wing tanks for storage

52.

Why is fuel jettison important in the Airbus A380?

a)

To reduce the weight of the aircraft in the event of an emergency landing

b)

To increase fuel efficiency during long-haul flights

c)

To prevent fuel contamination

d)

To maintain proper fuel balance during flight