Allow 2.5 Amps per pump.
The ignitions are supplied by their own coils and are thus independent
of the alternator.
The Rotax specified currents are...
Fuel pump main 3A max
Fuel pump standby 3A max
Turbo Control Unit 0.3A
Servo motor 1A max
Warning lamp c. 0.25A
Caution lamp c. 0.25A
Tony
-----Original Message-----
From: Steve Hagar
Sent: Wed 20/11/2002 6:25 p.m.
Cc:=09
Subject: Amp Draw
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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