In case of one LGCIU failure, is the landing gear system affected?

Correct!
Wrong!
During landing, Nose Wheel Steering (NWS) is available:

Correct!
Wrong!
Nosewheel steering control authority depends on aircraft speed. Rudder pedals provide nosewheel steering control when the speed is below 100 kt at landing, or up to 150 kt for takeoff.
Which hydraulic system powers the landing gear normal operation?

Correct!
Wrong!
In case of GREEN hydraulic system loss, what is the correct statement?
Correct!
Wrong!
The flight crew may arm the autobrake system provided all following conditions are:
Correct!
Wrong!
Anti-skid is available:

Correct!
Wrong!
The parking brake accumulator maintains the parking pressure for at least:
Correct!
Wrong!
The two-wheel nose gear comprises an oleopneumatic shock strut and a nosewheel steering system. It retracts rearward into the fuselage.
Correct!
Wrong!
It retracts forward into the fuselage.
When depressing the pedal disconnect pb on a steering handwheel:
Correct!
Wrong!
Parking brake requires:
Correct!
Wrong!
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The IAS is 300 kt - Landing gear selector is set to DOWN:
Correct!
Wrong!
All gears and doors are hydraulically-actuated by the green hydraulic system. Hydraulic supply is automatically isolated by closing a safety valve above 280 kt. It is maintained closed until the landing gear lever is moved to the DOWN position and the aircraft speed decreases below 280 kt.
Autobrake system is disarmed by:

Correct!
Wrong!
If both pilots turn their steering handwheels at the same time:
Correct!
Wrong!
Input orders to the Nose Wheel Steering are available from:

Correct!
Wrong!
In the event of an aborted takeoff with autobrake armed, automatic braking is initiated:
Correct!
Wrong!
Information on main landing gear panel are provided by:
Correct!
Wrong!
Alternate Braking mode with Antiskid is available:
Correct!
Wrong!
Initial pedal force or displacement produces more braking action in alternate mode than in normal mode.
Correct!
Wrong!
In case of landing gear gravity extension, the nose wheel steering is lost.

Correct!
Wrong!
GEARS AND DOORS - CONTROLS AND INDICATORS - The red arrow, and associated ECAM warnings come on red in approach at _____, if the landing gear is not downlocked in landing configuration.
Correct!
Wrong!
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The ECAM memo N/W STRG DISC is displayed. What does it mean?
Correct!
Wrong!
The steering handwheels control the nosewheel steering angle up to plus or minus _____ in either direction.
Correct!
Wrong!
A visual red warning on the overhead panel indicates to the crew that an oversteer (plus or minus 93 degrees) has occurred.
A green arc overhead wheel temperature on ECAM WHEEL page indicates:
Correct!
Wrong!
The purpose of the Antiskid is to:
Correct!
Wrong!
The Brake and Steering Control Unit (BSCU) enables:
Correct!
Wrong!
After a free fall extension, it is possible to restore normal operation, provided green hydraulic pressure is available.
Correct!
Wrong!
ALTERNATE BRAKING WITHOUT ANTISKID - Accumulators are designed to supply at least _____ full brake applications.
Correct!
Wrong!
If Brake and Steering Control Unit (BSCU) channels 1 and 2 are inoperative:
Correct!
Wrong!
When the A/SKID N/W STRG switch is set to OFF:

Correct!
Wrong!
If one UNLK indication remains on at gear extension, the landing gear position can be confirmed using the WHEEL SD page (information from LGCIU 1 and 2): only one green triangle on each landing gear is sufficient to confirm that the landing gear is downlocked.

Correct!
Wrong!
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If GREEN hydraulic pressure is not available:
Correct!
Wrong!
The red arrow on the landing gear indicator panel illuminates:
Correct!
Wrong!
There are two braking systems available, the normal and the alternate system:
Correct!
Wrong!
The purpose of the RESET position on the LDG GEAR GRVTY EXTN panel is to:
Correct!
Wrong!
Airbus A330 – Landing Gear