A、To the top line data bus.
B、To the mid line data bus.
C、To an ARINC 429 data link.
答案：A
A、To the top line data bus.
B、To the mid line data bus.
C、To an ARINC 429 data link.
答案：A
A. The emergency lighting battery only.
B. The emergency lighting system only.
C. The emergency lighting battery and the emergency lighting system.
A. In the green GO band.
B. In the red band.
C. At zero.
A. The system continues to operate automatically
B. The outflow valve can be menully controlled to adjust the cabin altitude
C. The safety valves open
A. Automatic start and manual start.
B. Automatic start only.
C. Wet motoring.
A. Management functions and flight envelope protection
B. Rudder control and flight envelope protection
C. Guidance functions and rudder control
A. The Power Transfer Unit.
B. An engine driven pump.
C. An electric pump.
A. The TLA
B. The ground logic
C. The N2
A. To pressurize the reservoir.
B. To check the flignt controls.
C. To operate the cargo doors.
A. The failed WHC connects to the other.
B. Both systems are lost.
C. The heating of the related side is lost.
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.
