Airbus ECAM msg: Pitch ELAC 2 fault.

[Atoll]

Hi all,

I had the other day after take off the msg as follows: ELAC 2 Pitch Fault as an advisory.
As far I understood the syst it means Pitch fonction of ELAC 2 is INOP and ELAC 1 has taken over the pitch function.
In QRH section 2.38 RESET of SYST, it refers to FCOM etc....., therefore a reset inflight should not be recommended and actually I did not agree as no ECAM called for it....
My question is with this msg, the pitch function is transferred to ELAC 1, what about the ailerons?. What about the reset inflight did somebody tried?

Thanks.