Airbus A330 - Pneumatic

When the APU Bleed is ON and the X-Bleed Valve is in AUTO:

Both Engine Bleed Valves are automatically closed.

Only ENG 2 Bleed Valve is automatically closed.

Only ENG 1 Bleed Valve is automatically closed.

Correct! Wrong!

In flight, with Wing anti-ice On, if there is a wing leak detection:

The X-Bleed Valve opens automatically to allow normal de-icing.

Only one wing will be de-iced.

The Wing anti-ice is automatically stopped.

Correct! Wrong!

On ground when using an Air Supply Unit (ASU) to have pneumatic pressure on both sides:

The X-Bleed selector must be OPEN and both packs will go On.

The X-Bleed selector must be OPEN and both packs will go Off.

The X-Bleed selector must be AUTO and both packs will go On.

Correct! Wrong!

Air is supplied to the aircraft’s pneumatic system via one HP ground connector only. The crossbleed valve has to be opened manually to provide air for both sides.

True.

False.

Correct! Wrong!

Air is supplied to the aircraft’s pneumatic system via two HP ground connectors. The crossbleed valve has to be opened manually to provide air for both sides.

Bleed air supply from the APU:

Is controlled by the APU Bleed Valve and is available on ground and in flight.

Is not available in flight.

Is not available for air conditioning.

Correct! Wrong!

The temperature regulation of bleed air is achieved by a precooler, that is mounted downstream of the bleed valve. The precooler is an air-to-air heat exchanger, which uses cooling air that is bled from the engine fan, to regulate the temperature to 200 deg.C.

False.

True.

Correct! Wrong!

Which of the following statements is true?

Each engine bleed system is controlled and monitored by one Bleed Monitoring Computer (BMC).

APU bleed is controlled and monitored either by BMC 1 or BMC 2.

Each engine bleed is pneumatically controlled and electrically operated.

Correct! Wrong!

If an engine bleed pylon leak is detected, the bleed valve on the same side closes, the X-Bleed valve receives a closure signal, and:

Wing anti-ice may be selected.

OFF light appears in the ENG BLEED pb associated with the closed Engine Bleed Valve.

A FAULT light appears only in the ENG BLEED pb associated with the pylon leak and wing anti-ice must not be selected.

Correct! Wrong!

The pneumatic system supplies high pressure air:

Only for air conditioning, engine starting, and wing anti-ice.

Only for the hydraulic and water reservoir pressurization.

For air conditioning, engine starting, wing anti-ice, as well as for hydraulic and water reservoir pressurization.

Correct! Wrong!

It also supplies air to Pack bay ventilation turbofan actuation, Cargo heating and Fuel Tank Inerting System (FTIS).

Each BMC (Bleed Monitoring Computer) is provided with bleed pressure, temperature and valve position information, and is interconnected to other systems involved with the bleed system and the other BMC.

True.

False.

Correct! Wrong!

In flight, when APU Bleed Valve is opened, if a wing leak is detected, Engine Bleed Valve and HP Valve on related side close and:

Wing anti-ice must not be used.

APU Bleed Valve closes automatically if the wing leak concern the left wing.

APU Bleed Valve closes automatically if the wing leak concern the right wing.

Correct! Wrong!

When AIR ENG 1 BLEED FAULT appears on ECAM:

Amber FAULT light and white OFF light appear in ENG BLEED pb.

FAULT light in ENG BLEED pb remains on as long as the failure is present.

FAULT light goes out if ENG BLEED pb is pushed off with failure still present.

Correct! Wrong!

The X-Bleed Valve is AUTO. It will open automatically when the air is coming from:

APU.

Engines.

ASU.

Correct! Wrong!

The Engine Bleed system is controlled and monitored by:

Two EBS computers, one primary and one stand-by.

One dedicated Bleed Monitoring Computer (BMC) for each engine.

An Engine Bleed System (EBS) computer.

Correct! Wrong!

The opening of the APU Bleed Valve when X-Bleed is set on AUTO, causes:

All statements are true.

The closing of the ENG Bleed Valves.

The opening of the X-Bleed Valve.

Correct! Wrong!

The APU Bleed Valve has the priority on the ENG Bleed Valves:

False.

True.

Only for engines start up.

Correct! Wrong!

X-BLEED is actuated by 2 electric motors:

One for the automatic mode, the other for the manual mode.

One is supplied by AC generation, the other is supplied by DC generation.

One is MAIN, the other one is STBY.

Correct! Wrong!

On ECAM BLEED page the 'GND' message is displayed in white. What does it mean?

External air may be connected, turns amber if pressure is out of limit.

The aircraft is on ground. It is not displayed in flight.

It is on stand by, turns green when external air is connected.

Correct! Wrong!

In case of APU leak signal:

The APU Bleed Valve closes automatically.

The X-Bleed Valve must be closed manually as soon as possible.

The APU Bleed Valve must be closed manually as soon as possible.

Correct! Wrong!

Airbus A330 – Pneumatic

Quiz

Airbus A330 - Pneumatic

When the APU Bleed is ON and the X-Bleed Valve is in AUTO:

In flight, with Wing anti-ice On, if there is a wing leak detection:

On ground when using an Air Supply Unit (ASU) to have pneumatic pressure on both sides:

Air is supplied to the aircraft’s pneumatic system via one HP ground connector only. The crossbleed valve has to be opened manually to provide air for both sides.

Bleed air supply from the APU:

The temperature regulation of bleed air is achieved by a precooler, that is mounted downstream of the bleed valve. The precooler is an air-to-air heat exchanger, which uses cooling air that is bled from the engine fan, to regulate the temperature to 200 deg.C.

Which of the following statements is true?

If an engine bleed pylon leak is detected, the bleed valve on the same side closes, the X-Bleed valve receives a closure signal, and:

The pneumatic system supplies high pressure air:

Each BMC (Bleed Monitoring Computer) is provided with bleed pressure, temperature and valve position information, and is interconnected to other systems involved with the bleed system and the other BMC.

In flight, when APU Bleed Valve is opened, if a wing leak is detected, Engine Bleed Valve and HP Valve on related side close and:

When AIR ENG 1 BLEED FAULT appears on ECAM:

The X-Bleed Valve is AUTO. It will open automatically when the air is coming from:

The Engine Bleed system is controlled and monitored by:

The opening of the APU Bleed Valve when X-Bleed is set on AUTO, causes:

The APU Bleed Valve has the priority on the ENG Bleed Valves:

X-BLEED is actuated by 2 electric motors:

On ECAM BLEED page the 'GND' message is displayed in white. What does it mean?

In case of APU leak signal: