A thread was started by Scott Balmos earlier to encourage members of this forum to review his electrical diagram for his aircraft. I am at the same point in my build and it inspired me to get my drawings done.
The aircraft will be using the EFII’s fuel injection and dual ignition systems integrated with the VPX system. The review of Scott’s diagram made me think differently of my original designed system. My diagram is at a point that I want to encourage others to review my diagrams and give me feedback.
I have elected to have an electrical dependent aircraft with dual fuel pumps, ignition systems and alternators. I have three busses; main through the VPX, Essential for the engine and a Battery Buss for an alternate power for mission critical components in the event of a VPX failure.
in the event of a software failure, I plan to carry a Stratus and iPad along with a portable radio for additional redundancy.
https://www.dropbox.com/s/huean6xr27g2jjm/N219PB Wiring Rev2.pdf?dl=0
This is my latest drawing
N219PB rev4
The aircraft will be using the EFII’s fuel injection and dual ignition systems integrated with the VPX system. The review of Scott’s diagram made me think differently of my original designed system. My diagram is at a point that I want to encourage others to review my diagrams and give me feedback.
I have elected to have an electrical dependent aircraft with dual fuel pumps, ignition systems and alternators. I have three busses; main through the VPX, Essential for the engine and a Battery Buss for an alternate power for mission critical components in the event of a VPX failure.
in the event of a software failure, I plan to carry a Stratus and iPad along with a portable radio for additional redundancy.
https://www.dropbox.com/s/huean6xr27g2jjm/N219PB Wiring Rev2.pdf?dl=0
This is my latest drawing
N219PB rev4
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