A、To open or close the HP fuel Shut-off Valve.
B、To command and reset the FADEC functions.
C、Both to open or close the HP fuel Shut-off Valve and to command and reset the FADEC functions.
答案：C
A、To open or close the HP fuel Shut-off Valve.
B、To command and reset the FADEC functions.
C、Both to open or close the HP fuel Shut-off Valve and to command and reset the FADEC functions.
答案：C
A. The Vacuum System Controller
B. The vacuum generator
C. The associated Flush Control Unit BITE
A. The Electronic Control Box.
B. The Fuel Control Unit.
C. The IGV Control Unit.
A. At aircraft power up.
B. As soon as the engine is shut down.
C. 5 mn after engine shut down.
A. DMC 3 automatically replaces DMC 1
B. DMC 3 must be manully transferred
C. Nothing
A. Moves the stops to restore the maximum rudder deflection upon slat extension.
B. Maintains the last position.
C. Move the stops to the maximum rudder deflection at any time.
A. The exciter field is no longer supplied and the GCR trips.
B. The exciter field is still supplied and the GCR stays closed.
C. The exciter field is increased and the GCR trips
A. The directors directly.
B. The type A DEUs
C. The type B DEUs
A. ENGINE REPORT ON REQUEST <05> and ENGINE RUN UP REPORT <11>.
B. ENGINE REPORT ON REQUEST <05> and LOAD REPORT <15>.
C. All.
A. In flight automatically.
B. In flight above 200kt automatically.
C. On ground manually.
A. P.F.D
B. N.D
C. E/W
