The cargo doors hydraulic system is pressurized by the :

A. By the FDU.

B. By the ECAM.

C. By the red disc indicator.

A. Blower fan

B. Aft cargo door

C. Pressure Regulating Valve

A. No concequence. the movement of the flap surfaces is not affected.

B. The system is locked and flap movement is no longer possible.

C. The flap surfaces extend (retract) at half speed.

A. On a tire and brake indicator.

B. On ECAM.

C. No indication.

A. In ROSE-VOR mode.

B. In ROSE-NAV mode.

C. In any mode.

A. FCU

B. MCDU TAKE OFF page

C. MCDU flight plan page

A. Each FMGC drives its own FD symbols, FMGC1 supplies both FMAs and controls the flight controls and engines.

B. FMGC1 drives FD symbols on both PFDs,supplies both FMAs and controls the flight controls and engines.

C. FMGC1 drives FD sybols on the Captain PFD, supplies FMA on Captain PFD and controls the flight controls. FMGC2 controls the engines.

A. On the right side fan cowl door.

B. On the left side fan cowl door.

C. On the left side thrust reverser "C" duct door.

A. LAST LEG REPORT and LAST LEG ECAM REPORT

B. AVIONICS STATUS, LAST LEG REPORT, SYSTEM REPORT/TEST

C. CURRENT LEG REPORT, CURRENT LEG ECAM REPORT

A. In case of FCA1(2) failure.

B. In case of FAC1(2) pushbutton is pressed in and FAC1(2) is not energized.

C. When the FAC1(2) pushbutton is released out.