I am learning about the ECAM in the airbus.
I was hoping some one could tell me how the following faults would affect the automation or any systems in the aircraft.
or the considerations if one was to encounter these faults.
'Gen 1 or Gen 2 fault'
DC Bus-1 or the Bus 2 fault
AC Bus-1 or the Bus 2 fault
When the ecam presents the fault it will tell you how to correct it or at least what actions are to be taken.
Once the actions have been taken and the ecam page has been cleared as you proceed.....you will be left with the status page which will give you the information you are requesting!
I think this is what you are asking......if not those exact faults are in the manual and show on the page as it appears on the ecam ....Hope this helps!