A、An ECAM message is displayed and a buzzer sounds.
B、The MECH light flashes on the captain ACP and a buzzer on the captain ACP and a buzzer sounds.
C、The MECH light flashes on all ACPs and a buzzer sounds
答案：C
A、An ECAM message is displayed and a buzzer sounds.
B、The MECH light flashes on the captain ACP and a buzzer on the captain ACP and a buzzer sounds.
C、The MECH light flashes on all ACPs and a buzzer sounds
答案：C
A. A locking pin on the sliding window frame
B. The sliding window operating handle
C. None
A. Individual reservoir depressurization.
B. Depressurization of related hydraulic circuit.
C. Hydraulic system depressurization.
A. If an ignition fault occurs.
B. If an EGT overlimit or a stall fault occurs.
C. If an ignition fault, or EGT overlimit or a stall fault occurs.
A. The stops stay in high speed configuration
B. The stops stay where they were at the moment of the failure
C. The stops return to the low speed configuration when the slats are extended
A. The Electronic Control Box.
B. The Fuel Control Unit.
C. The IGV Control Unit.
A. The prinary parameters.
B. The secondary parameters.
C. Both the primary and the secondary parameters.
A. No concequence. the movement of the flap surfaces is not affected.
B. The system is locked and flap movement is no longer possible.
C. The flap surfaces extend (retract) at half speed.
A. Fuel crossfeed valve.
B. LP fuel and hydraulic fire shut off valves.
C. HP fuel shut off valve.
A. Refuel/defuel panel, external control panel and cockpit.
B. External power control panel.
C. The APU cannot be shut down from outside the aircraft.
A. In mode 2A, with flaps down or in the glide slope beam.
B. In mode 2B, with flaps down and in the glide slope beam.
C. In mode 2A, with flaps not down and not in the glide slope beam.
