Refuel valves may be actuated :

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. One

B. Two

C. Three

A. On the center pedestal in the cockpit.

B. On the forward attendant station.

C. On the aft attendant station.

A. They cut off electrical supply after 30 seconds.

B. They supply the system for 3 seconds.

C. They supply the system after 30 seconds.

A. To restore ECU power.

B. To restore EIU power.

C. To cut off ECU power.

A. On ground only.

B. On ground and in flight.

C. In flight only.

A. Armed modes.

B. Active modes

C. Engagement status.

A. In open circuit configuration

B. In intermediate circuit configuration, or in closed circuit configuration with airflow higher than the requested value

C. When the ambient Avionics bay temperature is above 34＇C(93.2＇F)

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. The autothrust disengages.

B. The autopilot engages.

C. The autothrust automatically engages with full thrust