A、Only the ELACs.
B、The ELACs and the SECs.
C、The FCDCs
答案:C
A、Only the ELACs.
B、The ELACs and the SECs.
C、The FCDCs
答案:C
A. The fuel booster pumps pressure decreases.
B. The Engine is shut down or the ENG FIRE pushbutton is released out.
C. The Engine fire detection system senses an engine fire.
A. The two wing tank pumps are in operation.
B. Only one wing tank pump supplies its associated engine.
C. Both pumps are stopped.
A. On the ECAM
B. On the ELEC PWR control panel
C. There is no indication
A. controller number 1
B. The AIR COND panel
C. The CABIN PRESS panel
A. Dutch roll damping and yaw guidance order execution.
B. Turn coordination and engine failure compensation.
C. A and B
A. A.1 Ignitor Box,1Leads ,2 Ign Plugs
B. B.1 Ignitor Box,2 Leads ,2 Ign Plugs
C. C.2 Ignitor Box,2 Leads ,2 Ign Plugs
A. Management functions and flight envelope protection
B. Rudder control and flight envelope protection
C. Guidance functions and rudder control
A. Within five minutes of NAV mode selection when present position has bot been entered.
B. During the alignement phase in case of IRS alignment error.
C. When alignment has been completed.
A. During main engine start.
B. During APU start, or above 23000ft.
C. If EGT is too high.
A. - Elevator and THS
B. - Aileron and THS
C. -Rudder and THS