RTW - that sucks. Wonder if Sig should update the build manual then? Given those LT-40s had good proper surface to surface CA bonds, use of CA should not be an option if the wings folded. Every thread I've read regarding the LT-40 advised to "follow the manual and you should do great" with regards to the build...

Guess I can go back and run some beads of epoxy around the MADB joint to the spars in addition to the fiberglass being epoxied to the wing joint seam.

somegeek