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I used an Aeroelectic Connection resource to help design the electrical system below. It has no standby battery to power the Surefly Ignition Module. Power is always supplied via the battery. The master switch can be turned off with the battery powering the ignition for a longer duration than the aircraft has fuel with full tanks. The direct battery connection to the L ignition complies with the Surefly Ignition Module installation instructions. The R side was moved to the Relay to avoid a single point of failure.
I don't like a host of extra backup batteries. But the main battery needs to be fully charged and maybe even replaced annually because its so critical to system integrity. Trying to keep it simple.
What are your thoughts?
I used an Aeroelectic Connection resource to help design the electrical system below. It has no standby battery to power the Surefly Ignition Module. Power is always supplied via the battery. The master switch can be turned off with the battery powering the ignition for a longer duration than the aircraft has fuel with full tanks. The direct battery connection to the L ignition complies with the Surefly Ignition Module installation instructions. The R side was moved to the Relay to avoid a single point of failure.
I don't like a host of extra backup batteries. But the main battery needs to be fully charged and maybe even replaced annually because its so critical to system integrity. Trying to keep it simple.
What are your thoughts?
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