That structure is designed for *mostly* vertical loads. I would not pull it horizontally on a routine basis, especially pulling against the tie-down ring, which increases the bending moment.
If I was going to pull the airplane using the tail tie down hardpoint, I'd fabricate a piece of steel with a pair of holes in it. One the diameter of the tail tie-down and the other sized for whatever hook you're using to pull the airplane. I'd bolt the piece of steel to the airplane using the tie-down ring and attach the winch to the other hole. That will greatly reduce the bending moment on the assembly. The loads may still be too high for the underlying structure over the long term.
With a little ingenuity, you could probably attach a Y shaped harness to the main gear and pull it that way. No structural issues with that approach.
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Kyle Boatright
Marietta, GA
2001 RV-6 N46KB
2019(?) RV-10
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