#1 The pitot tube is integral with a static source which is the larger outer tube. The assembly is two tubes, one inside the other. The two mounting tabs are simply drilled to the assembly's diameter then bent and riveted to the root tube with stainless steel rivets. The bend angle is such that it "springs back" some after the pitot assembly is inserted thru them. This holds the pitot assembly in place while permitting easy removal should one desire. Twelve holes were drilled in the front of the static tube but I now think that's way too many. Probably half that would work just as well. I wanted the static port as close to the pitot tube's inlet as possible so as to sense the same air.

Here's a side view of the assembly. I made it long enough to protrude into (what I thought would be) undisturbed air coming off the windshield. The inside tube goes to the pitot port on the ASI. For the outside tube (static port), I drilled then filed an enlongated hole so a smaller tube could be inserted and aluminum soldered to it. The ends of the large tube were V-notched all around such that I could bend the ends down and aluminum solder them to seal off the ends to the inside tube. The angle is for relative "levelness" in flight.

You can see the vinyl tubing coming off the pitot and static ports in this shot. It also shows the mounting tabs better. They have worked very well and keep the tube assembly in place quite well.

There are two short vinyl tubes, one for the pitot pressure and one for the static pressure. Each goes to one of the down tubes for the back of the seat. This photo shows one of the vinyl tubes routed back to its down tube, attached to a 90° piece of plastic tubing. Longer lengths of vinyl tubing run from those 90° pieces, down inside each of the seat back tubes, secured under the seat and over along the fuselage side then up to the instrument panel and the ASI. The bottom edge of the down tubes were notched out so the vinyl tubing could exit without being pinched.