BM,
By all means, let us know what you think. My contention remains that on a single engine airplane, these things will NEVER be able to be very precise, or reliable in avoiding stall/spin accidents, since the AOA at any moment can easily vary span-wise, and THAT is precisely where most folks get into that kind of trouble. Due to propeller blast effect, the only place to mount the "sensors" for these things is out on the wing, far away from the prop blast. And, the problem there is that the wing itself dramatically influences the flow of air around it....just like it does for an airspeed pitot mast.
Look at the "sensor" for the one the guy in Minnesota makes.....it looks remarkably like the PITOT mast from a Cherokee or Warrior. It's comparing pressure differential between to ports on the same mast, just like the Piper pitot mast does. So, how is this thing going to be so much more accurate than a pitot mast, pray tell?
REAL AOA information is great. The problem is, it's really hard to derive ACCURATE AOA information in a single engine airplane for the reasons noted above. And, frankly, if the thing isn't that precise, it's no better than an airspeed instrument. And, if you're working a small airplane in close quarters, your BUTT is going to be MUCH more reliable, assuming it's properly trained.
Let us know which model you're installing, how it goes with the FSDO (have you verified with the FSDO that THEY think it's a minor?) and what your experience with it is.
MTV
