Airbus 320 Interconnectivity Thread
 

I propose a Airbus 320 Interconnectivity Thread here, where we can learn more about how stuff is Interconnected and the implications.
Questions and Answers. Also general explanations imparting knowledge related to Interconnective items

It is interesting that there is not more info on it.
It is fascinating and surprising in the MEL how stuff is interconnected.

Like

1) If a SFCC flap channel why do all ADIRS need to be operative ?

2) When ADR 2 is OFF aircraft is Conf 1+F the SFCS no 2 Flap channel unable to crsscheck, uncommanded flap retraction possible

3) ELAC 1 inop both TR 1 and TR 2 must be operative why? Is that right that there are implications to the DC BUS tie Why ?

4) ADIRS and Nosewheel steering

5) Etc.


Thanks for your input.