Is the APU bleed air supply maintained when the APU FIRE pushbutton is released out ?

A. By setting the landing gear lever to the "UP" position.

B. By shock absorber extension.

C. By auto brake deactivation.

A. To interconnect the two chambers of the steering actuator.

B. To apply hydraulic pressure to the servovalve.

C. To bypass the servovalve in case of BSCU failure.

A. The autothrust disengages.

B. The autopilot engages.

C. The autothrust automatically engages with full thrust

A. Air (vent), water, hydraulic and fuel.

B. Water and fuel.

C. Hydraulic and fuel.

A. The whole electrical network is still operational.

B. AC BUS 1 is lost.

C. AC BUS 2 is lost.

A. None.

B. SYSTEM REPORT/TEST for main systems.

C. LAST LEG REPORT and LAST LEG ECAM REPORT.

A. Immediately because it has operational consequences.

B. Before next flight.

C. Class 3 failures can be left uncorrected.

A. Only by yellow high pressure.

B. Only by the brake zccumulator.

C. Either by yellow high pressure or by the brake zccumulator.

A. Autopilot, Flight Director, autothrust.

B. Autopilot modes.

C. Guidance along a flight plan.

A. The guidance part of the FMGCs.

B. The management part of the FMGCs

C. The FCU.