Last week, I found my right engine alternator belt shredded in the bottom of the engine cowling (due to a frozen idler pulley .. another matter). During the just ended flight, I had no idea I had lost an alternator.
According to the PA30 Maint Manual, Figure 11-68a, the outputs of the Left and Right alternators connect to a common buss bar after passing through their respective 90 amp breakers.
My question is this: does anyone have a way of connecting some sort of indicator (lights?) to the respective alternators such that they will indicate an INDIVIDUAL alternator is outputting current (or not outputting current .. either way will do)?
Unfortunately, our L/R push button ammeter doesn't have a built-in indicator like our vacuum gauge does. I have a voltage monitor on my JPI Engine Monitor, but it only indicates buss voltage.