Airbus A330 - Hydraulics

If the GREEN hydraulic system is lost:

The NWS operates in alternate.

The NWS (Nose Wheel Steering) is lost.

The NWS remains operative.

Correct! Wrong!

What indicates the amber zone on the HYD page?

The maximum reservoir filling level.

The temperature of the hydraulic fluid.

The reservoir quantity warning level.

Correct! Wrong!

The hydraulic system monitoring unit (HSMU) processes:

Fluid transfer between the three hydraulic systems.

Engine 1 and 2 hydraulic fire shut off valves closure.

Control of electric pumps, Ram Air Turbine (RAT) extension.

Correct! Wrong!

An accumulator in each system helps maintain constant pressure by covering transient demands during:

Normal operations.

Abnormal operations.

Any engine failure.

Correct! Wrong!

During landing gear retraction, the engine 1 fails and the GREEN ELEC pump is automatically activated. How will it stop?

The GREEN ELEC pump spring loaded switch must be pressed.

The ENG 1 pump pb must be selected Off to stop both pumps.

The GREEN ELEC pump will stop automatically after 25 seconds.

Correct! Wrong!

After Takeoff, one engine fails prior to the Landing Gear retraction. When the Gear handle is selected 'UP':

Only the GREEN engine driven pumps are used to retract the gear.

RAT will extend to assist gear retraction.

The GREEN ELEC pump comes on automatically to assist gear retraction.

Correct! Wrong!

Leak measurement valves pb on the Maintenance panel:

Are for maintenance purpose and ground operation only.

May be used to isolate heavy users.

May be used by the crew to isolate flight controls during flight.

Correct! Wrong!

Leak measurement valves are positioned upstream of the primary flight controls. They are used for the leak measurement of each system and may only be closed on ground, by using the LEAK MEASUREMENT VALVES pb on the maintenance panel.

In flight and during approach the FLAP handle is at 2. If an engine 2 failure occurs:

The YELLOW system is lost.

The HSMU will automatically operate the YELLOW ELEC pump.

The YELLOW ELEC pump must be manually operated.

Correct! Wrong!

The corresponding hydraulic systems can be pressurized by:

Two engine driven pumps for the YELLOW system.

Two engine driven pumps for the BLUE system.

Two engine driven pumps, an electric pump and a Ram Air Turbine (RAT) for the GREEN system.

Correct! Wrong!

In case of GREEN reservoir LO LEVEL the HSMU (Hydraulic System Monitoring Unit) will:

Extend the RAT automatically.

Start the GREEN ELEC pump automatically.

Close automatically the engine 1 and 2 fire shut off valves.

Correct! Wrong!

With a single hydraulic system failure the flight control law is:

Direct.

Alternate.

Normal.

Correct! Wrong!

When the RAT pressurizes the green system, the aileron, elevator, and spoiler servo control operating speeds are reduced.

False.

True.

Correct! Wrong!

A pump, driven by Engine 2 pressurizes the yellow system. Flight crew can also use a hand pump to pressurize the yellow system, in order to operate the cargo doors when no electrical power is available.

True.

False.

Correct! Wrong!

There is a BLUE LO AIR PRESS alarm and there is a 'FAULT' indication on BLUE ENG 1 pump pb. Which one of the following statements is true?

The BLUE ELEC pump must be set to on to recover the system.

The BLUE system cannot be restored for approach.

The BLUE ENG pump may be restored for approach.

Correct! Wrong!

In the event of hydraulic green low pressure, heavy load users are isolated to give priority to:

Ram Air Turbine (RAT).

Flight controls and normal braking.

Landing gear and nose wheel steering.

Correct! Wrong!

In the event of low hydraulic pressure, a priority valve cuts off hydraulic power to heavy load users (emergency generator, nosewheel steering, landing gear) in order to keep the pressure for normal braking and flight controls.

The BLUE hydraulic system includes operation of:

The slats.

The slats and flaps.

Outboard ailerons.

Correct! Wrong!

The Airbus A330 hydraulic system has:

Three hydraulic systems sharing the same hydraulic fluid.

Three hydraulic systems sharing the same pressure source.

Three fully independent systems working simultaneously.

Correct! Wrong!

There is no possibility to transfer hydraulic fluid from one system to another.

False.

True.

Correct! Wrong!

The hydraulic reservoirs are pressurized:

From engine one or the crossbleed duct.

From the pneumatic system.

From the packs 1 and 2.

Correct! Wrong!

The Ram Air Turbine (RAT) deployment is automatically controlled by the HSMU (Hydraulic System Monitoring Unit) when:

Both statements are correct.

Low level in GREEN and BLUE hydraulic reservoirs is detected.

Low level in GREEN and YELLOW hydraulic reservoirs is detected.

Correct! Wrong!

With the GREEN hydraulic system lost, the antiskid system is:

Lost.

Operative via the blue hydraulic system.

Limited to 2000 psi brake pressure.

Correct! Wrong!

The GREEN ELEC pump starts automatically:

After engine 1 or 2 failure .

After engine 1 failure

After engine 1 or 2 failure and Landing Gear Selector UP.

Correct! Wrong!

What is the correct statement about the RAT?

The RAT will be automatically deployed in the event of low pressure in the GREEN system.

The RAT can be manually deployed by pressing the RAT MAN ON pb.

The RAT is able to pressurize the GREEN or the YELLOW systems.

Correct! Wrong!

What is the difference between the BLUE ELEC pump and the GREEN or YELLOW ELEC pump?

The BLUE ELEC pump has a higher pressure.

The BLUE ELEC pump has a higher flow.

The BLUE ELEC pump has no automatic operation.

Correct! Wrong!

The RAT deploys automatically in the event of an engine failure or a low level in the green and yellow or green and blue reservoirs.

False.

True.

Correct! Wrong!

The RAT deploys automatically in the event of both engine failure or a low level in the green and yellow or green and blue reservoirs.

Airbus A330 – Hydraulics

Quiz

Airbus A330 - Hydraulics

If the GREEN hydraulic system is lost:

What indicates the amber zone on the HYD page?

The hydraulic system monitoring unit (HSMU) processes:

An accumulator in each system helps maintain constant pressure by covering transient demands during:

During landing gear retraction, the engine 1 fails and the GREEN ELEC pump is automatically activated. How will it stop?

After Takeoff, one engine fails prior to the Landing Gear retraction. When the Gear handle is selected 'UP':

Leak measurement valves pb on the Maintenance panel:

In flight and during approach the FLAP handle is at 2. If an engine 2 failure occurs:

The corresponding hydraulic systems can be pressurized by:

In case of GREEN reservoir LO LEVEL the HSMU (Hydraulic System Monitoring Unit) will:

With a single hydraulic system failure the flight control law is:

When the RAT pressurizes the green system, the aileron, elevator, and spoiler servo control operating speeds are reduced.

A pump, driven by Engine 2 pressurizes the yellow system. Flight crew can also use a hand pump to pressurize the yellow system, in order to operate the cargo doors when no electrical power is available.

There is a BLUE LO AIR PRESS alarm and there is a 'FAULT' indication on BLUE ENG 1 pump pb. Which one of the following statements is true?

In the event of hydraulic green low pressure, heavy load users are isolated to give priority to:

The BLUE hydraulic system includes operation of:

The Airbus A330 hydraulic system has:

There is no possibility to transfer hydraulic fluid from one system to another.

The hydraulic reservoirs are pressurized:

The Ram Air Turbine (RAT) deployment is automatically controlled by the HSMU (Hydraulic System Monitoring Unit) when:

With the GREEN hydraulic system lost, the antiskid system is:

The GREEN ELEC pump starts automatically:

What is the correct statement about the RAT?

What is the difference between the BLUE ELEC pump and the GREEN or YELLOW ELEC pump?

The RAT deploys automatically in the event of an engine failure or a low level in the green and yellow or green and blue reservoirs.