This has probably been answered before, though I don't have it written
down anywhere. I am laying out my current load for the aircraft on my
spreadsheet. I need to know what the steady state amp draw is for the
fuel pumps on the 914 installation. Also are the electronic ignitions
supplied from their own independent coils on the alternator/flywheel or
are they drawing off the miserly output of the PM alternator? If so what
is the current required of these guys?--- Steve HagarA143 Mesa, AZ---
hagargs@earthlink.net
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