A、A cabin altitude of 8000Ft
B、A cabin altitude of 9550Ft
C、A cabin altitude of 11300Ft
答案:A
A、A cabin altitude of 8000Ft
B、A cabin altitude of 9550Ft
C、A cabin altitude of 11300Ft
答案:A
A. In the green GO band.
B. In the red band.
C. At zero.
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.
A. By a white flashing light.
B. By a red flashing light.
C. By an amber flashing light.
A. The pilot interface with the Flight Management function of the FMGC.
B. The aircraft interface between the Flight Management and Flight Guidance funtions of the FMGC.
C. An independent means of controlling the aircraft in marual flight.
A. Within five minutes of NAV mode selection when present position has bot been entered.
B. During the alignement phase in case of IRS alignment error.
C. When alignment has been completed.
A. AC BUS 1.
B. AC BUS 2.
C. Emergency Generator.
A. The air intake flap actuator cannot be overidden.
B. The air intake flap actuator can be hydraulically overidden.
C. The air intake flap actuator can be overidden by a Manual Override Device.
A. The GPCU is supplied and the EPC is open.
B. The GPCU is not supplied and the EPC is open.
C. The GPCU is supplied and the EPC is closed.
A. With avionics bay ambient air
B. With air coming directly from the pack outlet
C. With cabin ambient air
A. Ground power Control Unit.
B. Generator Control Unit.
C. Battery charge limiter.