What happens if FWC1 FAILS?

A. ENGINE REPORT ON REQUEST <05> and ENGINE RUN UP REPORT <11>.

B. ENGINE REPORT ON REQUEST <05> and LOAD REPORT <15>.

C. All.

A. By a momentary action on the take over pushbutton of any side stick.

B. By pulling on the deactivated stick harder than the other pilot.

C. By a simultaneous action on both take over pushbuttons.

A. From cabin distribution ducts

B. From pack 1

C. From pack 2

A. To open or close the HP fuel Shut-off Valve.

B. To command and reset the FADEC functions.

C. Both to open or close the HP fuel Shut-off Valve and to command and reset the FADEC functions.

A. ELACs and SECs

B. ELACs,SECs and FACs

C. FACs

A. To the top line data bus.

B. To the mid line data bus.

C. To an ARINC 429 data link.

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. The GCR relay and the GLC stay closed.

B. The GCR relay stays closed and the GLC opens.

C. The GCR relay and the GLC are opened.

A. When the LOCALIZER receiver is faulty.

B. When the deviation is excessive.

C. When the aircraft is out of range.

A. The system test.

B. The failure report.

C. The battery test.