Hi guys i have a question that i dont find on fcom1:
During dc bus 2 fault on a-32o between the inop systems appear the elac2 (with a note at the bottom of the fcom) say that we will recover the elac2 at gear extension

i dont find any related explanation on fcom1 anybody can tell me the reason???

Thank u in advance...

Hi luron,

Please see post #14 http://www.pprune.org/tech-log/486651-airbus-dual-eng-fail-procedure-question.html by KBPsen.

thank u... now is clear