On a recent flight I elected to validate my Monkworkz MZ-30L standby alternator by running it for a few minutes with the primary alternator off for ~10min. During this, I kept an eye on the MZ-30 current output, as reported by the MZ-30 voltage regulator proportional current output (pin 5) wired into my Dynon EMS/EFIS. The results were odd, with the system reporting a peak to trough current measurement delta of ~7.5A. For the first ~5min I didn't change anything electrical with the aircraft (strobes on, beacon on, everything else off). I switched both the strobes and beacon off at ~7min into the test and observed no change.
The MZ-30 is wired into the secondary 60A ANL fuse, plus has an inline fuse itself. The primary fuse has the B&C alternator tied to it, and the current shunt on the Dynon is connected between this and the main contactor. If I understand this correctly, it is really a battery meter, and doesn't show actual load on the avionics bus in flight.


Any and all thoughts are much appreciated!
The MZ-30 is wired into the secondary 60A ANL fuse, plus has an inline fuse itself. The primary fuse has the B&C alternator tied to it, and the current shunt on the Dynon is connected between this and the main contactor. If I understand this correctly, it is really a battery meter, and doesn't show actual load on the avionics bus in flight.


Any and all thoughts are much appreciated!