A、The A/THR system controls the engines and the A/THR pushbutton light is ON.
B、The thrust levers control the engines and the A/THR pushbutton light is OFF.
C、The thrust levers control the engines and the A/THR pushbutton light is ON.
答案：C
A、The A/THR system controls the engines and the A/THR pushbutton light is ON.
B、The thrust levers control the engines and the A/THR pushbutton light is OFF.
C、The thrust levers control the engines and the A/THR pushbutton light is ON.
答案：C
A. ADIRU 1 or 2.
B. ADIRU 2 or 3.
C. ADIRU 1 or 3.
A. On the ECAM
B. On the ELEC PWR control panel
C. There is no indication
A. The AFT galley has been shed.
B. ALL the galleys have been shed.
C. An overload on any generator (APU or IDG).
A. By a greeg dot.
B. By a yellow arrow corresponding to the speed in 15 seconds.
C. By a yellow arrow corresponding to the speed in 10 seconds.
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. To reduce the air flow to the compressor stage
B. To modulate the pack discharge temperature
C. To increase the air flow to the turbine stage
A. Yes
B. No
A. Yes.
B. No.
A. The speed brake function is inhibited.
B. ALL spoilers receive an additional deployment order until one reaches its maximum possible deflection.
C. The symmetrical surface is retracted until the difference between the two surfaces is equal to the roll order.
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.
