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.
答案：C
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.
答案：C
A. MAX mode.
B. MED mode.
C. LO mode.
A. GEN 1 supplies AC BUS 1 and GEN 2 supplies AC BUS 2.
B. APU GEN or EXT PWR or one GEN supplies AC BUS 1 and AC BUS 2.
C. APU GEN supplies AC BUS 1 and EXT PWR supplies AC BUS 2.
A. The N1 limit.
B. The N1 command.
C. The N1 target.
A. Not electrically supplied.
B. Reduced.
C. Increased.
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. Flight plan data, A/C present position and wind characteristics.
B. Flight plan data, A/C present position and autotuned radio navaids.
C. Flight plan data, Decision Height and crosstrack deviation.
A. Bank angle and stall protections.
B. Bank angle and and high speed protections.
C. Stall protection only.
A. By 26 V AC.
B. By 28 V DC.
C. By 115 V AC.
A. It alerts the crew that the MCDU has failed.
B. A system, linked to the MCDU, requeats the display.
C. It alerts the crew that the MCDU MENU page is not available.
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)
