A、SYSTEM display.
B、ENGINE/WARNING display.
C、STATUS display.
答案:B
A、SYSTEM display.
B、ENGINE/WARNING display.
C、STATUS display.
答案:B
A. Critical parameter feedback signnals
B. Acknowledgment signals and DU failure information
C. A and B
A. The valve opens when the engine is stopped.
B. The valve opens when the engine is running.
C. The valve closes when the engine is running.
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. 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. The LH and RH Wing ducts, packs and mid fuselage APU duct.
B. The pylon.
C. A and B.
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. On the center pedestal in the cockpit.
B. On the forward attendant station.
C. On the aft attendant station.
A. ELACs and SECs
B. ELACs,SECs and FACs
C. FACs
A. Yes.
B. No.
A. A brake release order is given to the wheels of the same gear.
B. A brake release order is given to the related wheel.
C. A brake release order is given to all wheels.