A、When the APU is shut down.
B、When the fault is detected.
C、Both.
答案：B
A、When the APU is shut down.
B、When the fault is detected.
C、Both.
答案：B
A. The GCR relay and the GLC stay closed.
B. The GCR relay stays closed and the GLC opens.
C. The GCR relay and the GLC are opened.
A. By 26 V AC.
B. By 28 V DC.
C. By 115 V AC.
A. When the aircraft speed is above 200kts.
B. When the aircraft is stopped on the ramp.
C. When the aircraft altitude is above 2000feet.
A. The Electronic Control Box.
B. The Fuel Control Unit.
C. The IGV Control Unit.
A. WHEEL page.
B. CRUISE page.
C. FTL/CTL page.
A. All mode are inhibited.
B. Mode 4 is inhibited.
C. Mode 5 is inhibited.
A. None.
B. SYSTEM REPORT/TEST for main systems.
C. LAST LEG REPORT and LAST LEG ECAM REPORT.
A. At the rear part of the pylon.
B. At the bottom of the engine.
C. Both at the rear part of the pylon and at the bottom of the engine.
A. HP Fuel valve not open.
B. Ignition fault.
C. EGT Overlimit detected.
A. The autopilot is engaged.
B. LAND mode is armed or active.
C. An ILS frequency is autotuned.
