RWA
You are now the one making things up.
A lot of backstick' was not applied, leave alone 'maintained' - even the BEA states that the PF did exactly what he should have done, applied forward stick, controlled any tendencies to roll, and levelled the aeroplane out:-
Your previous quote from post 1994
"From 2 h 10 min 05 , the autopilot then auto-thrust disengaged and the PF said "I have the controls". The airplane began to roll to the right and the PF made a left nose-up input. The stall warning sounded twice in a row.
My bolding and colour change.
Pray tell why if the aircraft was in Alpha Prot it would increase the AOA by pitching UP!! Plus in ALT LAW 1/2 Alpha Prot is not available. Roll is direct which is why there could have been slight over-controlling in roll. High AOA and High speed protections could also have been lost. Once the AOA had been sensed greater than 30 degrees Abnormal Attitude Law would have been in place to allow recovery of the A/C. (Pitch control alternate law with no protections as mentioned before and Roll would now be direct - NO auto-trim from that point on and Manual Pitch trim required. This would be displayed on the PFD.)
You are like a dog with a bone and need to just relax and wait for further information to be given out by the BEA. With your continued misinformation and lack of understanding you seem to be trying to prove your own conspiracy theory.