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. Passenger reading and work attendant lighting.
B. Cabin lighting,entrance lighting and lavatory lighting.
C. Lavatory lighted signs.
A. The flap system is locked by the WTB.
B. The flap system is not affected.
C. The flap system operates at half speed.
A. The NAVigation mode remains active and the FPA mode engages.
B. The track and FPA mode engage.
C. There is no effect.
A. Heat shield drain.
B. Flow divider drain.
C. Turbine plenum drain.
A. Two stage centrifugal compressor design.
B. Signle stage centrifugal compressor design.
C. Three stage axial compressor design.
A. The control handle gearbox.
B. The safety pin
C. The liting mechanism.
A. The Ground Power Control Unit has tripped the external ground cart.
B. The external ground cart is connected to the aircraft network.
C. The external ground cart can be connected to the aircraft network.
A. ECAM-FADEC
B. ECAM-CFDS
C. CFDS-ACARS
A. The pilot interface with the Flight Management function of the FMGC.
B. The aircraft interface between the Flight Management and Flight Guidance funtions of the FMGC.
C. An independent means of controlling the aircraft in marual flight.