A、The Engine panel.
B、The ECAM control panel.
C、The ECU.
答案:C
A、The Engine panel.
B、The ECAM control panel.
C、The ECU.
答案:C
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. By pressing the central HDG-V/S / TRK-FPA pushbutton on the FCU.
B. By disengaging the HDG or V/S modes.
C. By pressing a FD pushbutton.
A. The HP compressor inlet.
B. The HP compressor discharge.
C. The combustion chamber discharge.
A. A red V/S flag comes on.
B. A degraded V/S data provided by ADR.
C. Nothing.
A. The three other door are deployed.
B. The other latches are hyd. relocked.
C. Thrust reverse is unavailable.
A. Only on the ECAM STATUS page .
B. In the LAST LEG REPORT, the AVIONICS STATUS and the ECAM STATUS page .
C. Class 2 failures are only displayed in flight.
A. ELACs and SECs
B. ELACs,SECs and FACs
C. FACs
A. By a white flashing light.
B. By a red flashing light.
C. By an amber flashing light.
A. Yes.
B. No.
A. To the locking shaft.
B. To the safety shaft.
C. To the spring unit.