What happens if a High level is detected ?

A. In flight, if Blue hydraulic power is lost.

B. As soon as two hydraulic power systems are lost.

C. In flight, if both AC electrical power sources are lost.

A. The funtion that integrates the routes the aircraft must follow and the constraints to construct a flight plan.

B. The function that provides the aircraft position and the follow-up the flight plan.

C. The ratio of cost of time to the cost of fuel.

A. In flight automatically.

B. In flight above 200kt automatically.

C. On ground manually.

A. By pressing in the FAC pushbutton.

B. By pressing in the FAC internal monitoring(including power up test time) is healthy and engagement condition is requested.

C. A and B

A. A brake release order is given to the wheels of the same gear.

B. A brake release order is given to the related wheel.

C. A brake release order is given to all wheels.

A. Yes,from the opposite FMGC.

B. Yes,from the opposite FMGC, but after switching.

C. No,the VOR 2 cannot be tuned.

A. To control mask oxygen inlet.

B. To prevent oxygen inlet to mask.

C. To control oxygen supply during tests and mask operation.

A. During main engine start.

B. During APU start, or above 23000ft.

C. If EGT is too high.

A. Manually opened and secured by a hold open rod.

B. Hydraulically opened and secured by a hold open rod.

C. Electrically opened by a motor and secured by a hold open rod.

A. There is no hazard area.

B. There is a hazard area.

C. There is a hazard area but only if the power is set above idle.