I've been flying with a single D10A with remote mag compass and OAT probe, and I'm adding a second one with its own remote sensors. The manual explains that the secondary sensors will only ever be operational if the primary D10A fails, bringing down the network. It's a bit unclear what I'm meant...
Ok, I'm still looking and I'll buy it immediately if you will accept paypal goods and services... I still haven't decided for sure whether or not you're trying to scam.
There is a setting for when the audio alert begins, with options like "top of yellow", "bottom of yellow", etc. I find them a bit unclear. Which setting has the audio alert start sooner when approaching a stall and which has it start later?
I see that the HS34 allows the D-10A to understand vertical guidance from the GNS 430W. Does this mean the D-10A autopilot will follow an approach if we add an HS34? It seems like a reasonable thing to infer, but I haven't been able to find any documentation that specifically explains anything...
I see in the manual that the wires need to be shielded, but I am I correct that they do not need to be twisted? Would the 22 ga 4 conductor cable here be suitable? https://www.aircraftspruce.com/catalog/elpages/edmotefzel.php
I'm using the harness from Dynon, which includes 20 ga. wires for power which should be plenty based on the ampacity charts that I found. I think the easiest and cleanest way to split would be to daisy chain the connectors. That is, to put two wire ends into the same pin. Is there any reason not...
What is the preferred method of splitting the Dynon bus, power, etc. wires to go to the separate roll and pitch servos? I can think of any number of ways to do it, but what is the "right way"?
I (and I suspect many others) don't really care much about ADSB-out integration and will happily use the echoUAT with my existing GPS and transponder. However, I have not seen any technical reason for the lack of ADSB-in support. This is especially confusing given that the supported ADSB-in...