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I am ready to build my panel on my RV6 project. I had read posts where others had submitted their designs for review and they had good feedback.
I based my electrical system on Bob Knuckolls Z-14 Dual Battery, Dual Alternator, Split bus design.
My thinking is run all primary equipment on the main bus, and the backups on the secondary bus and not have a cross-over switch and relay.
The EFIS equipment has input for both power sources and I am selecting the power to the autopilot.
40A Main alternator (BUS A)
Odyssey PC680 on the engine side of the firewall
MFD-1 Horizon HX 6.5"
MFD-2 Horizon HX 8.4"
MFD-3 Horizon HX 6.5"
AHRS-1
AHRS-2
SL30 NAV/COM
GNX330 Transponder
Trutrak ADI
Trutrak Digflight IIVSGV (Switch bus A or bus B)
Everything else except what is on bus B
20A Secondary on the vacuum pad (BUS B)
Odyssey PC680 on the engine side of the firewall
MFD-1 Horizon HX 6.5"
MFD-2 Horizon HX 8.4"
MFD-3 Horizon HX 6.5"
AHRS-1
AHRS-2
Supplies GNC300XL GPS/COM
Garmin 340 Audio Panel
Trutrak Digflight IIVSGV (Switch bus A or bus B)
The 4 breakers MFD-1, MFD-2, AHRS-1 and AHRS-2 are just in case I want to do a power off reset. I would turn off BUS B and pull the breaker. It is unlikely I would need this but I do testing of the EFIS equipment also.
The other 2 breakers I used for the alternator fields are just for over-voltage indicators.
The 3 switches between the 8.4" MFD and the radio stack would normally be set to EFIS for A/P source, A?P power from BUS A, and the TRIM PWR ON. They would only be changed for testing or a problem.
For the attitude redundancy I have 2 AHRS that are cross checked and only a composite is displayed. If they disagree then they split and I use the Trutrak ADI to pick the good AHRS. After that everything is the same as before, just my backup has changed to the A/P and ADI.
For air speed and altitude I have three sources, the 2 AHRS and the EIS, easy to fail one source. I will have a second pitot also.
Todd Stehouwer
RV6