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It looks I found it:

https://store.vansaircraft.com/oil-pressure-switch-ie-spdt-pres-15-sw.html

Which Oil Press Switch model P/N is used in this scheme?

http://www.aeroelectric.com/PPS/Engine/Gaging/Oil_P_Warn.pdf

Thank you Doc, I'll have a look on that.. anyway, pls post pics when you'll be at your airplane.

Would you have pictures of lowering or raising the aileron with the help of washers..?

thank you

Hi David,

here is a 3 way, lockable, double pole switch from APEM. I'm selling these, feel free to send me a PM..

https://www.ebay.com/itm/164244841780

Thank you all!

I'll remove the long neg. wire and ground the battery locally.

After reading this article: https://www.kitplanes.com/positively-negative/

I ran a positive and a negative 2awg conductor from the back (battery) of my RV10 to the front. I missed the point where I ...

One more question regarding the AVIONX relay/switch combo.

Some builders suggested to use a NC relay, so that in case the relay or switch fails - power to the avionics bus would still be available ...

Thank you for taking the time to review my diagram and sorry for my late answer!

I hope my answers or questions do no sound ignorant. I'm trying to better understand my options (pros/cons) and that ...

>
> I'm talking about the 20A cb on the bus feeder?
>
>
>
> Bob . . .

Yes, it's a Circuit Breaker.

Could you give me that link to your current ...

>
> > When I sum up the Total BUS Peak Draw (9.04A) + Top Delta Peak of the GTN COM connection (assume this connection is shorted): TOTAL PEAK with fault on the GTN COM side equals 15.02 ...

At 07:16 AM 7/4/2020, you wrote:
--> AeroElectric-List message posted by: "supik" <bionicad>

Here is my calculation to avoid a situation when the AVIONICS ESS CB trips before ...

Here is my calculation to avoid a situation when the AVIONICS ESS CB trips before the equipment on this bus does. Taking care about the AVIONX ESS BUS CB in series:

The total PEAK DRAW on the AVION ...

There's a thread running now that claims
roots in Z101. ALL of the z-figures
were crafted with a particular airframe/mission
in mind. Occasionally I run a across a builder's
asser ...

I would rethink what you are trying to accomplish.

With all the monkey motion going on, it would seem you would be better served going with a Z-14 rather than a gummed up Z-101.

Why an avionic ...

Joe, thank you for your comments.

The schematic diagram is overly complicated.
The utility bus can be eliminated and those loads can be powered directly from the Main power bus.
Both avio ...

Version 35

-UTIL BUS eliminated / rebranded to MAIN BUS fuse block (non essential stuff)
-AutoPilot head unit + servos moved to ESS BUS

https://i.ibb.co/Z67GnDy/Diagram-OM-ELA-Igor-v-035.jpg
...

I think I am somehow close to the Z101. As the batt in the RV10 is located in the tailcone -with the ALT-2 connected to the ESS bus I tried to avoid the long always hot wire between the BATT and ALT-2 ...

At 10:00 AM 6/13/2020, you wrote:
--> AeroElectric-List message posted by: "supik" <bionicad>

I have the ACS 502 key switch and was wondering how to wire the center ground.
...

I have the ACS 502 key switch and was wondering how to wire the center ground.

B&C instructions for the GERDES key switch say DO NOT connect the center GND to any structural member in the cabin ...