Hehe - drilling more holes in my plane is not an option!
The error is not large, even at very high altitude. Worst case - I'll just live with it.
Keep in mind that if the source of your airspeed error is static source position error that this affects your altimeter too. You said in an earlier post that you think your IAS is reading 30 - 40 mph too high. If it is reading 30 mph too high at 8500 ft, your altimeter will be reading about 500 ft too high. This is too big an error to ignore, even if you only fly VFR.
Good point, but then that doesn't track with the fact that my altitude tracked within 300' of GPS altitude all the way up to 17,500'.
At this point I think we're drifting back into a discussion we've had before. I'll try the dams and see if I can get it perfect; flying VFR these days until I build more confidence in the install, so I have a while to tweak it.
GPS altitude is a very different thing than barometric altitude, so there is little to be learned by comparing the two. For example, if you sit on top of a 17,500 ft mountain, staring at a GPS, the GPS altitude should be relatively constant. But, if you also have a barometric altimeter, with the altimeter setting from a low altitude airport, the barometric altitude displayed on the altimeter will vary as the temperature of the air between you and the airport varies. This variation can easily be several hundred feet at the altitude of your mountain.
For a bit more info, see
Lies Your Barometric Altimeter Tells You.
Assuming you have no static system leaks and insignificant ASI instrument error, the source of your high ASI readings must be in the static system position error. Just to be sure you are hunting the right thing, it is worthwhile doing one last quick static system leak check, and an ASI instrument error check at a single airspeed in the cruise airspeed range.
The static system leak check should take less than five minutes. Block off one static port with a piece of tape, and push a piece of rubber tubing against the fuselage over the other static port. Gently suck on the end of the tubing until the altimeter has climbed 1000 ft. Put your tongue over the end of the tube to hold the suction constant, and watch the altimeter. It should descend less than 100 ft in one minute. When you are done, release the suction slowly to avoid damaging the ASI or altimeter.
Do an ASI instrument error check at a single cruise speed as described in this old
Kitplanes article by Jim Weir. Note that his recent Kitplanes article has huge errors in the table of ASI readings vs water manometer height. More info
here.
Happy hunting.