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A310

Total questions: 58

Worksheet time: 29mins

Name
Class
Date
1.

What is the primary function of the refuel manifold in the A310?

a)

Control the aircraft's center of gravity

b)

Distribute fuel evenly between tanks

c)

Provide fuel directly to the engines

d)

Remove water contamination from fuel

2.

Which component allows fuel to be drained from the system?

a)

Refuel couplings

b)

Transfer valve

c)

Drain valve

d)

Refuel manifold

3.

What is the purpose of the transfer valve in the fuel system?

a)

Transfer fuel between tanks

b)

Allow refueling from external sources

c)

Vent excess pressure from the tanks

d)

Remove impurities from the fuel

4.

Where are the refuel/defuel valves located in the A310?

a)

In the engine feed system

b)

Near the wingtips

c)

Inside the fuel tanks

d)

Along the refuel manifold

5.

How does the fuel system ensure proper engine fuel supply?

a)

Through refuel couplings

b)

Using the transfer valve to feed the engine system

c)

By draining excess fuel through the drain valve

d)

Manually operated by the pilot during flight

6.

What does the green color indication on the ECAM Fuel System Display signify for a fuel pump?

a)

Pump off

b)

Pump on with low fuel pressure

c)

Pump on with normal fuel pressure

d)

Pump in manual mode

7.

What happens if the vent surge tank becomes full?

a)

It automatically drains back to the main tank

b)

It releases excess fuel overboard

c)

It redirects fuel to an auxiliary tank

d)

It triggers an alarm in the cockpit

8.

What is the function of the Low Pressure (LP) Valve in the Airbus 310-300 fuel system?

a)

Regulate the pressure inside the fuel tanks

b)

Act as a fire shutoff valve

c)

Control the amount of fuel delivered to the engine

d)

Prevent fuel contamination

9.

What is the purpose of the isolation valves in the fuel system?

a)

Prevent fuel from flowing back into the tanks

b)

Separate different fuel compartments and regulate fuel transfer

c)

Increase fuel pressure before it reaches the engines

d)

Mix different fuel types for better combustion

10.

How many electrical fuel booster pumps (TK Pumps) are installed in each main fuel tank?

a)

One

b)

Two

c)

Three

d)

Four

11.

What is the purpose of the trim tank in the Airbus A310-300?

a)

Store emergency fuel

b)

Balance the aircraft's center of gravity

c)

Act as a backup fuel supply

d)

Reduce engine fuel consumption

12.

Which component is responsible for preventing fuel contamination in the system?

a)

Crossfeed valve

b)

Low-pressure valve

c)

Fuel filters

d)

Isolation valves

13.

How does the Airbus A310-300 prevent fuel overpressure during refueling?

a)

By using pressure relief valves

b)

By using a manual fuel dump system

c)

By limiting the refueling rate

d)

By redistributing fuel between tanks

14.

What is the main function of the fuel quantity indicating system?

a)

Regulate fuel pressure

b)

Measure and display fuel levels

c)

Control fuel flow to the engines

d)

Prevent fuel leaks

15.

What is the primary purpose of the vent tanks in the fuel system?

a)

Supply additional fuel during takeoff

b)

Provide additional thermal expansion space and prevent overpressure during refueling

c)

Measure the fuel quantity in the main tanks

d)

Isolate the fuel from the engine

16.

How much is the volume of each wing vent tank?

a)

120 liters

b)

150 liters

c)

190 liters

d)

200 liters

17.

Which method is used to pressurize the vent tanks during flight?

a)

Hydraulic pressure from the fuel pumps

b)

Ram air through flush NACA intake scoops

c)

Compressed air from the cockpit

d)

Electrical actuators

18.

What function do the non-return valves serve in the fuel feed system?

a)

Prevent fuel from reverse flow back into the tanks

b)

Regulate the fuel pressure in the lines

c)

Measure fuel consumption

d)

Increase fuel temperature

19.

Which component is described as a spherical-plug type valve, electrically actuated with two electric motors and a gearbox for 90° plug travel?

a)

Isolation Valve

b)

Crossfeed Valve

c)

Low Pressure (LP) Valve

d)

Check Valve

20.

Where is the vent/surge tank located on the Airbus A310?

a)

Only at the tip of each wing

b)

At the tip of each wing and at the RH tip of the horizontal stabilizer

c)

Only at the RH tip of the horizontal stabilizer

d)

At the bottom of the fuselage

21.

What is the volume of each wing vent tank?

a)

120 liters

b)

190 liters

c)

220 liters

d)

50 liters

22.

What is the function of the vent system?

a)

Store additional fuel for longer flights

b)

Prevent tank overpressure during refueling

c)

Control the aircraft's altitude

d)

Assist in engine cooling

23.

How are the aircraft's tanks pressurized in flight?

a)

By the engine exhaust gases

b)

By a fuel pump system

c)

By ram air through flush NACA intakes

d)

By hydraulic pressure

24.

What happens if the vent tank becomes full?

a)

It overflows overboard

b)

It transfers fuel back to the center tank

c)

It triggers an emergency alarm

d)

It increases fuel pressure

25.

What is the function of the check valve in the fuel system?

a)

Regulate fuel pressure

b)

Block air entry when pumps are off

c)

Increase fuel flow

d)

Store excess fuel

26.

How many electrical fuel booster pumps (TK PUMPs) are fitted in each main fuel tank?

a)

One

b)

Two

c)

Three

d)

Four

27.

What prevents the reverse flow of fuel from the fuel feed line to the tanks?

a)

Isolation valves

b)

Fuel booster pumps

c)

Non-return valves

d)

Check valves

28.

What is the usual sequence of fuel feed from the tanks?

a)

OUTR TK → INR TK → CTR TK

b)

CTR TK → INR TK → OUTR TK

c)

INR TK → OUTR TK → CTR TK

d)

OUTR TK → CTR TK → INR TK

29.

What is the primary function of a fuel pump in the fuel system?

a)

Store excess fuel

b)

Deliver fuel from the tanks to engines and other systems

c)

Control air intake in the fuel line

d)

Filter impurities from the fuel

30.

How many main fuel tanks does the Airbus A310 have?

a)

2

b)

3

c)

4

d)

5

31.

What is the primary purpose of the center fuel tank?

a)

Store fuel for emergency use only

b)

Provide additional fuel capacity and ensure proper weight distribution

c)

Supply fuel only to the APU

d)

Act as a backup in case the wing tanks fail

32.

How is fuel primarily transferred between tanks in the Airbus A310?

a)

Electric and engine-driven pumps

b)

Manual fuel transfer by the flight crew

c)

Gravity only

d)

Hydraulically powered pumps

33.

What is the function of the trim tank in some Airbus A310 models?

a)

Optimize the aircraft's center of gravity and improve the efficiency

b)

Provide backup fuel in case of system failure

c)

Supply fuel only during takeoff

d)

Act as a separate emergency fuel tank

34.

What happens if a fuel pump fails in the Airbus A310?

a)

The aircraft must immediately land

b)

Redundant pumps take over, and fuel can also be gravity-fed if necessary

c)

The engines shut down immediately

d)

The pilots must manually transfer fuel using backup valves

35.

What is the primary purpose of the vent/surge tanks on the Airbus A310-300?

a)

Store extra fuel for emergencies

b)

Prevent tank overpressure during refueling and provide thermal expansion space

c)

Supply ram air to the engines

d)

Act as auxiliary fuel tanks during long-haul flights

36.

How is positive differential air pressure maintained in the vent/surge tanks during flight?

a)

By engine bleed air

b)

By electric booster pumps

c)

By ram air through flush NACA intake scoops

d)

By pressure relief valves

37.

What component prevents reverse fuel flow from the fuel feed line back into the tanks?

a)

Isolation valves

b)

Crossfeed valves

c)

Non-return valves

d)

Low-pressure valves

38.

Which valve on the Airbus A310-300 serves as the Fire Shutoff Valve?

a)

Isolation valve

b)

Low Pressure Valve (LP Valve)

c)

Crossfeed Valve

d)

Booster Pump Valve

39.

What is the primary function of the fuel tank vent system in the Airbus A310-300?

a)

Increase fuel pressure during takeoff

b)

Prevent tank overpressure and provide thermal expansion space

c)

Regulate temperature within the fuel tanks

d)

Remove water from the fuel

40.

Which tanks are connected to the wing vent tanks in the A310-300?

a)

Only the center tank

b)

Inner and outer tanks only

c)

Inner, outer, and center tanks

d)

Outer and tail tanks only

41.

What happens when a vent surge tank becomes full?

a)

It shuts down the fuel system

b)

It siphons the excess fuel back to the center tank

c)

It overflows overboard

d)

It activates the isolation valve

42.

What is the purpose of the check valve in the fuel pump system?

a)

Regulate fuel temperature

b)

Allow air into the tank

c)

Block air entry when pumps are off

d)

Pressurize the fuel lines

43.

Which valve type in the A310-300 is known as the Fire Shutoff Valve?

a)

IsolaƟon Valve

b)

Crossfeed Valve

c)

Low Pressure Valve (LP Valve)

d)

Non-return Valve

44.

What is the primary function of the vent/surge tanks in the Airbus A310-300?

a)

Store excess fuel for long-haul flights

b)

Prevent tank overpressure during refueling

c)

Act as emergency fuel tanks

d)

Supply additional power to the engines

45.

What is the usual fuel feed sequence in the Airbus A310-300?

a)

OUTR TK → INR TK → CTR TK

b)

INR TK → OUTR TK → CTR TK

c)

CTR TK → INR TK → OUTR TK

d)

OUTR TK → CTR TK → INR TK

46.

What happens if the vent surge tank becomes full?

a)

It transfers fuel back to the main tanks

b)

It overflows overboard

c)

It shuts off fuel flow automaƟcally

d)

It acƟvates an emergency alarm

47.

What provides additional overpressure protection for the fuel tanks?

a)

Pressure regulators

b)

Relief valves

c)

Carbon safety discs

d)

Emergency dump valves

48.

What is the function of the crossfeed valve in the Airbus A310-300?

a)

Allows fuel transfer between engines

b)

Blocks reverse fuel flow

c)

Prevents fuel leakage during flight

d)

Automatically shuts off fuel flow during an emergency

49.

How does the Airbus A310 prevent fuel leaks?

a)

Fuel monitoring system

b)

Isolation valves

c)

Manual inspections

d)

Redundant fuel lines

50.

How are fuel levels displayed to the pilots?

a)

Analog dials

b)

Digital fuel quantity indicators

c)

Pressure gauges

d)

Mechanical levers

51.

What system manages fuel transfer?

a)

Hydraulic system

b)

Fuel management system

c)

Crossfeed valves

d)

Vent surge system

52.

How does the crossfeed system operate?

a)

Manually controlled

b)

Electrically actuated

c)

Hydraulic-powered

d)

Air pressure driven

53.

What happens if a fuel pump overheats?

a)

It shuts down

b)

The system switches tanks

c)

Fuel is dumped

d)

The cockpit alerts the pilots

54.

What is the total volume of the tail vent tank in the Airbus A310-300?

a)

120 litres

b)

100 litres

c)

150 litres

d)

200 litres

55.

How is the LP valve controlled in the Airbus A310-300?

a)

By manual switches

b)

By electric motors and a gearbox

c)

By hydraulic pressure

d)

By pneumatic system

56.

What prevents overpressurization and underpressurization in the vent surge tank?

a)

Carbon safety disk

b)

Electrical switches

c)

Hydraulic relief valve

d)

Pressure regulator

57.

What is the fuel feed sequence in the Airbus A310-300?

a)

Center tank, inner tank, outer tank

b)

Outer tank, inner tank, center tank

c)

Inner tank, outer tank, center tank

d)

Center tank, outer tank, inner tank

58.

What happens if the vent tank becomes full in the Airbus A310-300?

a)

It overflows into the center tank

b)

It overflows overboard

c)

It activates a safety valve

d)

It triggers a warning signal