I remember reading some time ago about the possibility of exposing parts of a microlight wing to sustained -ve G loadings under reasonably normal flying conditions. From memory, here's the scenario:
As we all know, a microlight flexwing has washout built in to the wingtips. The purpose of washout is to ensure the nose tips forward as you approach a stall. Let's say you're flying straight and level and begin to push the bar out. The AoA of the wing root (main centre section) increases above 16 degrees and in begins to stall, however the wingtips have washout (lower AoA) therefore they keep on flying. Because the wingtips are behind the CofG, as the root of the wing stalls, the wing will naturally pitch forward, increase speed and begin to fly again - all good.
Now consider the opposite situation. You are flying straight and level, apply engine power and begin to pull the bar in to speed up. The AoA on the root of the wing decreases and your speed increases. If you have a powerful 912 on the back you can pull the bar right in to your gut and really speed things up. You might even decide to do this in a shallow dive to give you that bit of extra speed. In this situation the AoA of the root will be very small but the built in washout of the wingtips may have put the wingtips into continuous -ve G as they are now pushing down!
Now consider the scenario where you fly into turbulance. A natural reaction might be to pull the bar in to speed up so you can 'punch through' the turbulance and reduce your exposure to it. This may place the wingtips close to (or maybe into) sustained -ve G's with turbulance added on top. Suddently we might end up with wingtip failure due to -ve Gs without ever attempting loops.
Anyway, I remember reading that explanation somewhere and it sounds like it might be possible. I'm no expert so I'll open it up for comment ...