Is #3 a good location for the return fuel line (for an electronic fuel injection system)?
I think I saw all three variants (marked #1, #2 and #3) used by different builders, and looking at the plans there doesn't seem to be much difference to me. In terms of plumbing, it will be routed aft to enter the fuselage somewhere around the fuel supply line. In the fuel tank, it will terminate at the second bay from the last (the outboard one).
I was thinking straight union fitting AN832. An anti-rotation bracket inside the fuel tank, then AN 6D spacer and AN924 nut outside. Seems like there should be enough space between the wing and the fuselage for a 90° tubing bend (though it's going to be more like an S-shaped bend).
Alternatively, I can use an AN833 elbow, but I my (zero-experienced) thinking is that it will be 1) might be a bit harder to torque the coupling nut due to the orientation 2) nothing other than sealant prevents fitting from loosening (but shouldn't be an issue due to the coupling nut torque orientation).
Thoughts?

I think I saw all three variants (marked #1, #2 and #3) used by different builders, and looking at the plans there doesn't seem to be much difference to me. In terms of plumbing, it will be routed aft to enter the fuselage somewhere around the fuel supply line. In the fuel tank, it will terminate at the second bay from the last (the outboard one).
I was thinking straight union fitting AN832. An anti-rotation bracket inside the fuel tank, then AN 6D spacer and AN924 nut outside. Seems like there should be enough space between the wing and the fuselage for a 90° tubing bend (though it's going to be more like an S-shaped bend).
Alternatively, I can use an AN833 elbow, but I my (zero-experienced) thinking is that it will be 1) might be a bit harder to torque the coupling nut due to the orientation 2) nothing other than sealant prevents fitting from loosening (but shouldn't be an issue due to the coupling nut torque orientation).
Thoughts?








