On Saturday, October 12, 2019 at 10:18:14 PM UTC-4, wrote:
Regarding the problems arising from sharing pitot, static, and TE across mechanical and transducer-based instruments:

I can see why the flow generated by anything using a capacity would be large enough to cause trouble. My gut feeling is that flow into or out of an altimeter or a mechanical ASI would be too small to matter.

If these instruments are impactful, what’s a workaround for a situation where finding truly separate pitot and static sources for the mechanical instruments is impractical? I’ve seen experimental gliders with digital altimeters, but I suspect a TSO’d option would be hard to come by, and I don’t think I’ve ever seen a (modern) sailplane without a mechanical ASI.

Would T’ing off static and pitot lines somewhat further than the traditional 6 inches from the instruments do enough to mitigate the effects?

Genuinely curious about this.

Neiman

If you want good instrumentation, it starts with good sources. Fin mount triple probe is the reliable standard for vario sources. Use the nose pitot and side statics for basic instruments (as usually specified by the manufacturer).

T8