Looking at the posted faults i'm curious...
I know (from 411 here) that the 330 has various safeguards built in to protect the airframe in normal law. Not fully understanding the complexities or variation when switched to alternate law I have 2 questions.
1) Can you tell if its abnormal alternate law (unusual attitude) or ALTLAW:PROT Lost (computer issues if my understanding is correct). From what I gather the flight control modifications are a bit different in each. It would also seem to indicate if an upset was the trigger for the AP disconnect or came later....
2) the last fault is the CTL RUD TRV LMT FAULT, is this an indicator that the control limit has faulted out or an indication of excessive rudder travel. I know that rudder use at high speeds is a very delicate undertaking and that the software normally dampens inputs. From what I read on the locked post under abnormal alt yaw is mechanical and controlled by direct law...is that correct?