Hi terrain noted,
AoA sensors/pitot static feed the 2 ADIRUs via ADMs.
The ADIRUs feed the stall management yaw dampers(2).
The SMYDs also get info from FMc(weight),IRs(adirus) for roll rate and acceleration and yaw rate ,trailing edge flaps position.
With this info the SmYD compute a Vspeed you will see on your speed tape(top of red/black stripe).
The aircraft has a few tricks to delay the stall,which includes LE flaps going from mid to full extent in te flaps are between 1 and 5.
The PLI(pitch limit indicator) was designed to help during windshear recovery but mostly used now for pilot to identify their pitch margin to shaker in specific configuration.
The elevator shift will increase hydraulic pressure to give you heavier feel to reduce you pulling some more...
The speed trim system will trim the stabilizer down.
The Rudder travel is limited to 2 1/2 degrees with flaps down.(not 100 perc sure bout nr,may be 2 degrees).
The stall strips will help for a root stall rather than a tip stall.
The stick shaker will come i think 5 kts or 5 perc before the actual stall .(certification thing,im not sure about those nrs,will have to check).
Last edited by de facto; 12th June 2012 at 03:32.