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  #11  
Old 09-20-2019, 10:00 PM
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johnbright johnbright is offline
 
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Location: Newport News, Va
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Originally Posted by MCA View Post
I haven't seen the Z-14 in common use for a while. It was used for IFR panels in exp aircraft a while back (like 20 years ago), but these days we have ways to provide backup and redundancy using a simpler single main bus architecture.

That can be accomplished using a combination of EFIS with built-in battery, essential bus architecture, and/or battery backup modules (Like the IBBS).

You haven't mentioned if your RV-10 is for IFR or VFR use.

My suggestion would be to look at a simpler architecture then design in the needed level of backup for your mission.
What if one is using EFI with no mechanical fuel pump?
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O-360, 8.5:1, vert sump, dual SDSEFI EM-5-F
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  #12  
Old 09-20-2019, 10:48 PM
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MCA MCA is offline
 
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Originally Posted by johnbright View Post
What if one is using EFI with no mechanical fuel pump?
A single main bus works for most conventional aircraft, both VFR and IFR, with varying levels of backup and redundancy depending on your mission.

If you are running an electrically-dependent engine or some other alternate configuration, the manufacturer of those systems typically specifies the needed electrical system and you should follow that.
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