![]() |
AC Bus 2 fault
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 ? |
You may need to supply a little more info. i.e. aircraft type:ugh:
|
you're probably right :O
It's on A320... |
DC ESS is supplied as normal and DC2 by TR1 via DC1 and DC Bat.
|
| All times are GMT. The time now is 08:04. |
Copyright © 2026 MH Sub I, LLC dba Internet Brands. All rights reserved. Use of this site indicates your consent to the Terms of Use.