Just want to clarify something for some comments made on this thread. Regulator A (and also Stator A) in normal conditions power both ECU A and ECU B and all the components fed by them, that is Injectors (all ), iginition coils (all), and both fuel pumps. Regulator B (and stator B) in normal conditions feed the aircraft loads (charges the battery, feed lights, avionics, etc.). This is stated on the user manual, and installation manual.
For better understanding, I think that Regulators A and B should be named for example X and Y, so nobody confuses the letters of the regulators with the letters of both ECUs.
regards,