Ive heard the term "Rudder Reversal" in connection with the Boeing 737 Rudder hard over issue in that the acuator would in fact create a rudder reversal whereby the rudder pedal inputs were reversed. This was a possible explanation as why pilot input was ineffective in recovery from full hard over.
I take it this is not the same thing. Is this the correct terminology for the AA587 issue? Just curious if there might be a connection?
Any thoughts or clarifications?
CattlePax/KATLPax