Previous thread on this
here.
High lift flight controls consist of:
1 inboard & 1 outboard surface + 1 flaperon & aileron droop
1 inboard & 6 outboard slats + 1 Krueger flap by the pylon.
Primary actuation is hydraulic. Secondary and Alternate actuation is electric.
Automatic load relief protects flaps from excessive airloads at high airspeeds by auto retraction and then re-extension when airspeed is back within safe range.
Automatic slat deployment will autoextend slats when impending stall is sensed.
False Capture, no one is supposed to know about iii.
