What is the maximum normal cabin altitude for maximum cruise level(39000Ft)

A. Can be de-activated by pressing the LOCp/b.

B. Can be de-activated by a GO-AROUND engagement.

C. Can be de-activated if the APPR pushbutton is pressed.

A. GEN 1 LINE SMOKE light.

B. BLOWER FAULT.

C. GEN 1 LINE SMOKE and BLOWER and EXTRACT FAULT lights.

A. FWC2 has to be manually selected.

B. DMCs lose half of the warnings.

C. FWC2 automatically takes over.

A. To close GLC 1 and supply the fuel pumps from the AC NORMAL BUS.

B. To open GLC 1 and supply the fuel pumps from GEN 1.

C. To close the BTC and supply the fuel pumps from the AC NORMAL BUS.

A. Directly from the master lever.

B. From the MASTER lever via the ECU.

C. From tne master lever via the EIU and the ECU.

A. To reduce the rate of flap travel.

B. To increase fluid flow to the motor.

C. To lock flaps until next position demand.

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. It sends a signal to the ECU.

B. It provides a warning to the ECAM system.

C. It operates a visual indicator for ground inspection.

A. The ram air inlet flaps of the air conditioning packs open

B. The ram air outlet flaps of the air conditioning packs open

C. The emergency ram air inlet flap opens

A. When hydraulic pressure is lost.

B. When ELAC 1 signal is lost.

C. When FAC 2 and 3 signal is lost.