[snip]
I began working on the 767 electrical power systems shortly after this incident. There were a number of systems that were discovered to have been left off the standby power system (the barry power).
We also ran into a problem in that the system incorporated a static inverter with a 1 kVA rated output. The original design had only utilized about 50% of its capacity. Unfortunately, its rating had been specified assuming linear loads. While the Boeing specs limited the current THD any load was allowed to draw, loads of less that 200 VA were exempt. And most of the loads supplied by the inverter were small and of the non linear variety (power supplies mostly) with up to 30% current THD.
After the Gimli incident, the missing bits were moved on to the inverter bus, whereupon the inverter refused to produce an output voltage within spec. The loads were taken back off. Since my responsibility only extended to the power system, when I asked where the loads were put, I was told to shut up and mind my own business.