A320 EFIS / FMA Guide
Started by ipuneet.
Posted
9 months ago.
NOTE: DRAFT ,not yet fully Completed
By PALS
B - Bank Angle protection
max achievable bank angle +/
Y - Yaw function change & not protection. turn coordination is lost in Abnormal law, but reactive yaw damping remains available
P - Pitch Protection +30/-15
Too high nose up - Very rapid Enegery loss
Too Low nose-down - very rapid enegery Gain
A - AOA angle of attach (Aerodynamic Protection)
enables PF to pull sidestick FULL aft in dangerous situation giving best possible Lift, protection minimizes risk of stall or control loss
L - G Load
CFIT - Load protection enables immediate PF reaction without risk of overstressing aircraft , if sidestick continued to maintained Full Aft Stick, then AOA protecion takes over
S - Speed