AP1 is engaged, FDs are engaged, A/THR1 is engaged. How do the FMGCs work in normal conditions?

A. The Vacuum System Controller

B. The vacuum generator

C. The associated Flush Control Unit BITE

A. One of the two directional valves.

B. The enable solenoid valve.

C. The Linear Variable Differential Transducer.

A. The pilot interface with the Flight Management function of the FMGC.

B. The aircraft interface between the Flight Management and Flight Guidance funtions of the FMGC.

C. An independent means of controlling the aircraft in marual flight.

A. Switch over to0 the other channel.

B. Control goes to a fail-safe position.

C. The channel in control supplies the winding of the other channel.

A. An ECAM message is displayed and a buzzer sounds.

B. The MECH light flashes on the captain ACP and a buzzer on the captain ACP and a buzzer sounds.

C. The MECH light flashes on all ACPs and a buzzer sounds

A. None.

B. SYSTEM REPORT/TEST for main systems.

C. LAST LEG REPORT and LAST LEG ECAM REPORT.

A. It is impossible to engage the autopilot.

B. Engines running, it is impossible to engage the autopilot.

C. Engines shut down, it is impossible to engage the autopilot

A. In flight with two IDG supply.

B. ON ground with APU supply only.

C. ON ground with EXT PWR only.

A. On the TAKE OFF page.

B. Only by re-aligning the Inertial Reference Systems to the new runway coordinates.

C. By making a lateral revision from the currently displayed runway on the flight plan page.

A. When all the engines are not running, and the parking brake is applied and the cabin residual pressure exceeds 2.5mbars.

B. When engines are not running, the slide is disarmed and the cabin residual pressure exceeds 2.5mbars.

C. When engines are not running, the parking brake is applied,the slide is disarmed and the cabin residual pressure exceeds 2.5mbars.