What happens if an electric trim motor fails ?

A. controller number 1

B. The AIR COND panel

C. The CABIN PRESS panel

A. By 26 V AC.

B. By 28 V DC.

C. By 115 V AC.

A. One main frame computer for all engines.

B. The ECU and its peripherals, per engine.

C. A signle ECU and its peripherals, for both engines.

A. When the LOCALIZER receiver is faulty.

B. When the deviation is excessive.

C. When the aircraft is out of range.

A. Recording of the mandatory flight data requested by the airworthiness authority.

B. Trouble shooting of avionics computers only.

C. Engine condition, APU condition and aircraft performance monitoring.

A. Reception of a ground message.

B. Reception of a voice communication demand with the ground.

C. Loss of communication with the ground.

A. The ailerons and the spoilers.

B. The ailerons and the spoilers.

C. The spoiler and the rudder.

A. IR data, pure GPS data and hybrid GPIR data.

B. VOR/DME data.

C. Only GPS data.

A. The OBSV index.

B. The IDENTIFIERS item.

C. Page block 201.

A. On the ECAM upper display.

B. On the ECAM lower display.

C. On both ECAM displays.