DJ77,
I never mentionned lateral control
That's a pity because I can't see how you could derive anything on your flight controls state if you did not know the initial *triggers* of the degradation to ALT.
But of course, just mentioning the pitch control allows you to criticize in a very sleazy manner this architecture. So, when you wrote
... / ALT LAW 2 / Pitch control
Identical to ALT 1 law" Note the ambiguity: nothing is said if Alt law 2 is due ADR faults or disagree conditions.
,
you very conveniently forgot to mention that the conditions for ALT2 are, among others :
DOUBLE ADR FAULT ...ADR DISAGREE...
Thank you, the doubt I had is lifted.