A、By setting the landing gear lever to the "UP" position.
B、By shock absorber extension.
C、By auto brake deactivation.
答案:A
A、By setting the landing gear lever to the "UP" position.
B、By shock absorber extension.
C、By auto brake deactivation.
答案:A
A. Side1 and side2 Flight Guidance functions are independent.
B. Side1 and side2 Flight Management functions are independent.
C. One side is inoperative and the remaining FMGC controls both sides.
A. A brake release order is given to the wheels of the same gear.
B. A brake release order is given to the related wheel.
C. A brake release order is given to all wheels.
A. When "DOWN" is selected.
B. When "UP" is selected.
C. When the first engine starts.
A. The First Officer's ND and PFD are not in normal configuration.
B. The Captain cannot display the ND on either display unit.
C. The Captain's PFD Display Unit is inoperative.
A. Nothing happens.
B. The windshield heating is cut off.
C. The windshield and windows are heated.
A. During ECS Operation.
B. During Main Engine Start.
C. On ground.
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. To the top line data bus.
B. To the mid line data bus.
C. To an ARINC 429 data link.
A. On ARINC 429 and ARINC 453 buses
B. On Master DSEL and ARINC 453 buses
C. On ARINC 453 and Digital buses
A. The LH and RH Wing ducts, packs and mid fuselage APU duct.
B. The pylon.
C. A and B.