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Date: 9 Jan 2006 02:42 (UTC)I think the problem wasn't the structure per se. It's that nobody made the connection that in a pressurized fuselage, even a minor crack at a window corner can "run," propelled by the interior pressure, and then the whole fuselage ruptures like a punctured balloon. Unless they incorporate rip stoppers into the structure, which I understand they now do.
Composite fatigue.. hrm. The worst I've heard of so far is that some of the composites in light aircraft have a short lifespan because they take damage from ultraviolet light. One would hope that's something Boeing has considered. I think it's probably only a problem with the more basic composites like fiberglass, but... (shrugs)