Most folks don't realize the highly sensitive nature of this airplane's rudder system. I think 3 inches and not very much force is all that is required for full deflection of the rudder pedals. Here's a snippit from an email I wrote to a friend this morning after hearing the released findings.
Hope all is well in the land of CT today. Im a little disappointed because they blamed the Co-Pilot of AAL 587. (just saw the headline, but I've been following the crash investigation).
The Airbus A-300 only requires about 3 inches of pedal movement for full deflection, and there is very little resistance. If you get into turbulence (wake turbulence from a 747 variety) you get a bit of pucker factor. I know that my legs tense up at the first sign of an emergency (only for a moment while my brain starts to process again) and if that happened or he was just knocked around, kicking full rudder in that airplane is no chore. I hope Airbus gets *****-slapped with a lawsuit that puts them under because I don't think its AAL's fault in the least. Especailly the co-pilot. They followed a training program approved by Airbus and there were some rudder things specifically brought up during the course of the investigation that Airbus had signed off on.
Yet another reason "if it ain't Boeing, I ain't going."
Have a good'n