A、To the locking shaft.
B、To the safety shaft.
C、To the spring unit.
答案:B
A、To the locking shaft.
B、To the safety shaft.
C、To the spring unit.
答案:B
A. Door open, gear up, door close, cancel gear up signal.
B. Door open, gear up, door close, maintain gear up signal.
C. Door open, gear up, door close, cancel door close signal.
A. Yes, if hydraulic power is available.
B. Yes,in manual mode.
C. No, it does not move the rudder pedals.
A. The guide arms.
B. The support arms.
C. The upper and lower connection links.
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. The emergency lighting battery only.
B. The emergency lighting system only.
C. The emergency lighting battery and the emergency lighting system.
A. GPS2.
B. GPS1.
C. GPS1 and 2.
A. The GCR and PR relays stay energized.
B. The GCR and PR relays are de-energized.
C. The GCR relay stays energized and PR relay is de-energized.
A. When N2 is above 12%.
B. When an engine is started.
C. Only if the Aircraft Electrical Power fails.
A. Warning are inhibited.
B. The status page is displayed.
C. The warning are recalled.
A. A cabin altitude of 8000Ft
B. A cabin altitude of 9550Ft
C. A cabin altitude of 11300Ft