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.
答案：B
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.
答案：B
A. Center and wing tank pumps.
B. Center tank pumps only.
C. Wing tank pumps only.
A. Specific for each report.
B. Similar for all the reports.
C. Similar only for the engine reports.
A. As soon as the GEN 1 LINE pushbutton is released out.
B. When any GEN 1 parameter is not correct.
C. When any GEN 1 parameter is not correct and the GEN 1 pushbutton is released out.
A. By visual warning on one ACP.
B. By visual warning on all the ACPS and an aural buzzer.
C. By visual warning on all the ACPS.
A. To limit the pressure from the hand pump
B. To protect the system against overpressure
C. To limit thermal expansion of the hydraulic fluid
A. Motor 3
B. Motor 2 and Motor 1
C. Motor 1
A. Management functions and flight envelope protection
B. Rudder control and flight envelope protection
C. Guidance functions and rudder control
A. CAPT dome light and RH CENTER lighting instrument panel.
B. F/O dome light and LH CENTER lighting instrument panel.
C. F/O dome light and F/O and RH CENTER lighting instrument panel.
A. A cabin altitude of 8000Ft
B. A cabin altitude of 9550Ft
C. A cabin altitude of 11300Ft
A. Yes
B. No
