I've noticed that the flight control fault logic when failing PRIM's and SEC's don't follow the correct aircraft logic. For instance, failing Prim 3 and Sec 1 doesn't cause any impact to the LH outboard ailerons.

I'll pass this along to the team, in the meantime are you able to assist with providing documentation an FCOM or some sort of material reference for the team to look at as well, thank you :)