C. Flight Mode Annunciator (FMA).
52. WHERE IS GROUND SPEED INFORMATION
DISPLAYED?
A. Navigation Displays (NDs).
B. Primary Flight Displays (PFDs).
C. Flight Mode Annunciator (FMA).
53. WHAT IS ACTIVATED ON THE ATTENTION
GETTERS WHEN A PROBLEM OCCURS DURING
FINAL APPROACH IN AUTOMATIC LANDING?
A. The MASTER CAUTION.
B. The MASTER WARNING.
C. The AUTOLAND warning.
54. THE FAC COMPUTES RUDDER TRAVEL LIMITING
LAW USING THE CALIBRATED AIRSPEED (VC)
PROVIDED BY THE:
A. ADIRUs.
B. FMGCs.
C. SFCCs.
55. IF ONE OR SEVERAL YAW AXIS CONTROL
FUNCTIONS FAIL:
A. The FAC is disengaged.
B. Only the amber message appears on the ECAM.
C. The FAULT light in FAC pushbutton is ON.
56. THE RESET PUSHBUTTON ENABLES TO:
A. Return the rudder to the neutral position.
B. Moves the rudder to the previous position.