PuraVidaTransport
So can someone explain why it takes so long to get control surfaces to give the actions requested by the pilot. As I see it, the pilot wanted the nose down for 17 seconds and got nothing more than 15 degree nose up then the other wanted FULL nose down for 7 seconds and the computers once again only gave him nose up elevator. Does this have something to do with the cumulative inputs? Can a set of bad inputs cause the airplane to not respond quickly as was needed in this case??
That question was asked before, and i hoped the final report would answer this quetion. Bottom line is, that you have to ask the automation logic, because the SS only orders a change of g. How much change was ordered with full ND SS? I dont know, there are tables with g values corresponding to respective SS deflection, but i dont know wether there are speed gains involved or wether the load factor protection could have played a role in this.
Load factor protection was the only protection left, and again, i dont know wether it has some speed dependent gains as well.
Maybe an overlay of the graph you mentioned with actual normal acceleration values would shed some light.