Thanks a lot for the document
mm43.
In paralele to the outer ailerons inaction, another point of interest :
in low speed, the auto pitch trim stops at Vc prot (below VLS) and natural longitudinal static stability is restored, with STALL WARNING at 1.03 VS 1g
This is in page 126 and relates to Alternate Law.
If I get it right, the THS should NOT have moved ... but it did !?
What was happening in that aircraft ?
This reminds me the WRG fault message ... only
Svarin was interested to discuss.