AC Bus 2 fault

[ptithomme]

Hi,

Small question about AC2 failure and the associated electrical reconfiguration:

Is DC ESS supplied by DC1 via DC BAT ? (no change compared to the normal configuration)

Or, is DC ESS supplied by AC ESS via ESS TR ? (similar to the AC BUS 1 Fault)

I would say it's the second option, but I can't find the answer in my documentation...

Any idea ?

[FE Hoppy]

You may need to supply a little more info. i.e. aircraft type

[ptithomme]

you're probably right

It's on A320...

[Fly3]

DC ESS is supplied as normal and DC2 by TR1 via DC1 and DC Bat.