A、The predictive windshear function is not activated.
B、The predictive windshear function is active until the WINDSHEAR/AUTO/OFF is in the AUTO position.
C、The predictive winshear function is always available.
答案:B
A、The predictive windshear function is not activated.
B、The predictive windshear function is active until the WINDSHEAR/AUTO/OFF is in the AUTO position.
C、The predictive winshear function is always available.
答案:B
A. Directly by the reverser lever.
B. By the reverser lever through the ECU.
C. By the reverser lever through the EIU.
A. Bank angle and stall protections.
B. Bank angle and and high speed protections.
C. Stall protection only.
A. At aircraft power up.
B. As soon as the engine is shut down.
C. 5 mn after engine shut down.
A. On the TAKE OFF page.
B. Only by re-aligning the Inertial Reference Systems to the new runway coordinates.
C. By making a lateral revision from the currently displayed runway on the flight plan page.
A. CAPT dome light and RH CENTER lighting instrument panel.
B. F/O dome light and LH CENTER lighting instrument panel.
C. F/O dome light and F/O and RH CENTER lighting instrument panel.
A. Is automatic.
B. Must be performed by the crew for the climb phase only.
C. Must be performed by the crew both for the clim and the descent phases.
A. By the Engine fire pushbutton.
B. Automatically when a fire is detected.
C. By the MASTER lever or by the Engine fire Pushbutton.
A. The igniter plug,six fuel nozzles.
B. Two igniter plugs,six fuel nozzles.
C. The deswirl vane assembly, two igniter plugs, two fuel nozzles.
A. In the Passenger Service Unit.
B. In the seat arm rest.
C. In the overheat stowage compartment.
A. Engine Control Unit.
B. Hydraulic Control Unit.
C. Thrust Control Unit.