A、In open circuit configuration
B、In intermediate circuit configuration, or in closed circuit configuration with airflow higher than the requested value
C、When the ambient Avionics bay temperature is above 34＇C(93.2＇F)
答案：B
A、In open circuit configuration
B、In intermediate circuit configuration, or in closed circuit configuration with airflow higher than the requested value
C、When the ambient Avionics bay temperature is above 34＇C(93.2＇F)
答案：B
A. The oil flows through the bypass valve and the backup filter.
B. The IDG oil temperature increases.
C. The engine oil temperature incresases.
A. To inhibit DME operation.
B. To prevent simultaneous transmission and to interrupt reception of the other systems
C. To prevent simultaneous transmission and to inhibit the transmission of the other systems.
A. Two.
B. Three.
C. Seven.
A. At 100ft.
B. At 200ft.
C. At 400ft.
A. On Capt ND and F/O PFD.
B. On Capt PFD and F/O ND.
C. On F/O PFD and F/O ND .
A. The other stick remains deactivated after the take over pushbutton is released.
B. The other stick remains activated after the take over pushbutton is released.
C. Both stick are deactivated.
A. They compute and generate displays.
B. They generate audio warnings.
C. They generate amber warnings.
A. The control handle gearbox.
B. The safety pin
C. The liting mechanism.
A. On ground during take-off.
B. On ground during landing.
C. On ground during take-off and landing.
A. Recording of the mandatory flight data requested by the airworthiness authority.
B. Trouble shooting of avionics computers only.
C. Engine condition, APU condition and aircraft performance monitoring.
