If you want close tolerance
There has been really good advice concerning AN3 bolts on this thread.
Great for those with less experience. I love this forum, this is how we learn without having to make all the mistakes ourselves.
If actually have the application requiring it, and you want close tolerance
Don't use AN3 bolts, they are not close tolerance by any means.
The AN173 is the close tolerance version, but....
They are getting less available as time goes on and the industry is using NAS bolts such as the NAS1103, NAS1303, NAS6203, or the one that would be the most likely close tolerance sub for the AN3, the NAS6603.
If you are not looking for the structural shear strength, go with the AN bolt and any of the 3 size drills all the others have recommended, 10,11, or 12.
They should be perfectly fine for almost everywhere on an RV.
If you're installing for an actual structural application, use an NAS bolt as above or similar, in this example AN173-??.
Prep the hole by first drilling the hole just big enough to allow the pilot of the reamer to go in the pilot hole. Ream the hole using a reamer that will make a clean hole with an interference of .0005 to .0015. The best reamers will produce a hole that will require a light to medium drive fit using a small (4 to 6 oz) hammer struck several times per inch. The fastener should not be able to be pushed in by hand. Possibly if you pushed it in with a hammer handle and about 10 pounds of force it should go in the hole, but a tight fit is not an easy fit.
A loose hole and fastener combination in a sing shear situation, stressed to the point of structural shift will normally stretch the fastener or pop the head off.
Pop the head off, but it was in shear???? The structure shift allowed by the lose holes allows the fastener to rock in the hole changing the load on the fastener to a combination load of both shear and tension. The tension part comes from the edge of the head being relieved on one side and pressured on the other, while the same thing is happening to the nut end also.
That is why so many thing in aircraft are designed in double shear, thing may get strained, but the strength is greater and the fasteners are not as easily subject to combination loads.
You will notice that the spar splice plates ar all in at least double shear, and they call for close tolerance fasteners and close tolerance holes.
If as time goes on and you do your inspections, you find bolts loose on your plane that used to be tight, something has moved.
![Eek! :eek: :eek:](data:image/gif;base64,R0lGODlhAQABAIAAAAAAAP///yH5BAEAAAAALAAAAAABAAEAAAIBRAA7)
Just tightening them may not be the best solution.