Which warning lights are triggerd in case of an avionics smoke detection ?

A. A red flag.

B. Dashes in place of identification.

C. The ground station characteristics and pointer disappear.

A. Its consequences on other systems.

B. Its absence of consequences on other systems.

C. Associated attention getters not activated.

A. When is the locking shaft proximity switch target is NEAR and when the manual selector valve is operated.

B. When is the locking shaft proximity switch target is FAR and when the manual selector valve is operated.

C. When is the locking shaft proximity switch target is NEAR.

A. Automatically when the selector valve is de-energized.

B. Automatically through the automatic selector.

C. As soon as the brake pedals are pressed in.

A. A warning is triggered :too much fuel.

B. All the refuelling operations are stopped.

C. The corresponding REFUEL Valve coloses.

A. To record radio communications during take off and landing.

B. To record crew conversations as soon as an incident occurs.

C. To record crew conversations and communications.

A. To inhibit DME operation.

B. To prevent simultaneous transmission and to interrupt reception of the other systems

C. To prevent simultaneous transmission and to inhibit the transmission of the other systems.

A. GPS2.

B. GPS1.

C. GPS1 and 2.

A. BMC2 ensures the complete leak detection.

B. BMC2 ensures its wing leak detection.

C. The leak detection is completely lost.

A. The speed brake function is inhibited.

B. ALL spoilers receive an additional deployment order until one reaches its maximum possible deflection.

C. The symmetrical surface is retracted until the difference between the two surfaces is equal to the roll order.