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<If you are a bit technical, you can use our document to make up the sender yourself for the specific sender you have. > Where and in what document is this defined?

Thanks for the link, but these seem like separate questions. The VP-X is a version of the VP system with no display that uses the EFIS for display, control and software updates. It does not involve sharing EIS or EFIS data at all as far as I can see.

Ditto

I am also interested in this option, since I am building a Sportsman which has a steel cage within the fuselage.  Results with magnetometers of other systems in the vicinity of the cage have been mixed.  Most folks end up putting them in the wings. If you have a beta tester for this aircraft I...

Thanks, so going into the ADAHRS we have: Pitot Static AOA OAT what else? power? DSAB?

Will AOA and OAT also be connected to the ADAHRS?

Is Dynon working on supporting this device in the nextGen and/or current product line? Dynon is conspicuously absent from the list of supported EFIS systems listed on the Navworx site.

That was my thread, but I am just puting it in the suggestion box for the record and interested to see if anyone else concurs. Displaying units as you suggest and allowing the setting of other graphical limits would also be welcome enhancements that would make this system more competitive...

Since critical AOA varies with flap position, and you already have the means to read flap position, it would be helpful to allow for several different critical AOAs in the calibration procedure, corresponding to different flap positions.  This is a feature in several of the competing AOA systems.

Thnaks much. Of course for wiring, fusing and primary alternator sizing I would use the 100 watts, but since my aircraft has a Vne of 165 knots and will not be in the flight levels, it would be useful to know what the probable current draw would be under less extreme conditions, to consider...

I am trying to size battery and bus power requirements. The heated AOA installation manual indicates a 100 watt power usage at 13.8 volts, from which I calculate a current of 7.25 Amps. Is this a short term surge value during start up or a possible steady state requirement? If there is a...

It is not clear from the AOA calibration procedure whether separate stall AOAs are being recorded for different flap positions (if flap settings are being read by the EFIS) but it looks doubtful. Is this correct? If so, is there any likelyhood that the AOA calibration will be expanded to...

I am planning for a Dynon EFIS installation on my Sportsman (Glastar).  Since there is a steel cage, the good choices for the remote magnetometer location away from the steel seem to be in the wings somewhere or in the tail section of the fuselage.  It looks like the OAT sensor should be in the...

Although the Dynon EFIS and EMS products seem to be set up to run on 12V or 28V, it appears that the heated pitot is 12V only and I have been unable to determine what the situation is with the AP servos. If I want to incorporate the heated pitot and AP, am I pretty much locked into a 12V...