A、The hydromechanical unit.
B、The hydraulic pump of each engine.
C、The hydraulic power supply of the aircraft.
答案：A
A、The hydromechanical unit.
B、The hydraulic pump of each engine.
C、The hydraulic power supply of the aircraft.
答案：A
A. FMGC 1
B. FMGC 2
C. Either FMGC 1 or FMGC 2, independently of AP, FD, and A/THR engagement status.
A. Motor 3
B. Motor 2 and Motor 1
C. Motor 1
A. The emergency lighting battery only.
B. The emergency lighting system only.
C. The emergency lighting battery and the emergency lighting system.
A. Yes, because altitude data is automatically received from ADIRU 3.
B. Yes, because altitude data will be recovered after manual switching of the AIR DATA selection to ADIRU 3.
C. No, ATC 2 will be definitely lost.
A. When the ILS pushbutton is selected.
B. When G/S and LOC beams are received.
C. A and B
A. DC BUS 1 or batteries.
B. DC BUS 1, DC BUS 2 or batteries.
C. DC BUS 2 or batteries.
A. When the VOR is tuned from the MCDU.
B. When the VOR is tuned from the RMP.
C. When a failure occurs.
A. By the FDU.
B. By the ECAM.
C. By the red disc indicator.
A. Ram air for both compartments.
B. Fan air for both compartments.
C. Ram air for the fan compartments and fan air for the core compartments.
A. All.
B. Only ATC mode S equipped A/C.
C. ATC equipped A/C.
