Belgian1979 wrote:I remember some engineering saying that fatique can be calculated...
Yep, that's reassuring.
Engineers can calculate all they want. The FAA or EASA WILL NOT certify any PSE (primary structural element) until it has been tested to the point of breakage. The automobile industry does something very similar with any new car that is designed and marketed to the public. They have to build "x" amount of the cars AS DELIVERED and crash them in a variety of different manners to prove to the DOT that they meet certain safety standards. When Ford re-released the GT back in 2005 my older brother was one of the chassis engineers on that project (it was a small group of guys that Bill Ford Jr jr jr... whatever wanted hand picked). I think it was around 2003 or 2004 when he took me to the building where they were assembling them and it was the first time I had ever seen one. It was badass! At the end of the very short production line there were two or three completed GT's just loaded with telemetry sensors all over and inside of the car. These were cars that were complete with engines, stereos, etc. I asked him what the deal was with them. He just told me, "These are the ones we're going to crash". That floored me.
Anyway, I got way off base there. If you want to see some interesting video footage, go on YouTube and look up "Boeing 777 wing test". It's about three minutes long and basically a bunch of engineers who had worked long and hard to develop the wing for the then-new Boeing 777. They're standing in a room watching a 777 wing be bent by hydraulic rams until the main spar breaks. There's a calculated point at which they "think" it'll break. Where it actually breaks is what the FAA cares about... and they don't do it just once. It's pretty amazing how far they can bend a wing before it fails.
Years back I worked for Gulfstream corporate jets in Savannah, GA. Whenever they would design a new aircraft (G450, G550, G650) they would take one into the "stress hangar" and bend the living hell out of it in every direction imaginable. That hangar had no windows and only one door in. They didn't want anyone seeing what was going on in there I guess. Anyway, Gulfstream aircraft are certified to 20,000 cycles (basically 20,000 times of pressurizing and depressurizing the cabin). In the stress hangar they would blow up the fuselage to simulate pressurization and then dump the pressure. While doing this, the entire aircraft is mounted to hydraulic rams all over the place that bend it like a circus performer throughout the entire testing phase. I don't know the exact number they pressurize and dump the cabin, but I know it's substantially higher than 20,000. It's a pretty insane thing to witness, and uncomfortable, because you know what's going on, and you see the aircraft, and your brain just tells you, "metal shouldn't bend like that", but it does.
Never half ass two things... Whole ass one thing!