Just trying to get some greater understanding of this system, hopefully someone with more than my basic knowledge can help
In the event that probe/ sensor blockages cause a dual ADR fault, the ECAM instructs us to turn off the affected ADRs, and the aircraft reverts to ALTN LAW.
Hypothetically, if the blockage/s were cleared, could the ADR's be turned back on, and would the affected systems recover? Any references would be appreciated
