fdr, thanks. I could not make out what the rudder was doing, I was trying to understand the right roll, and hadn't considered roll rate limitations. (DOH!) Thanks also on the incipient spin and inertial coupling points.
Insofar as the wings being more or less level at impact, do you think (once the nose fell through) that sufficient control authority was restored to roll level using ailerons (roll rate limits considered)?
