"this was another typical DC10/MD11 rollover. Touchdown of >2.0G with a slight angle of bank, which causes the rear spar of the low wing to shear as the MLG is apparently bolted directly to the wing box. Because the aircraft is still traveling at high forward speed, the wing on this side is just folded over by its own lift while releasing the contents of the onside main fuel tank, and the rest of the aircraft is then rolled upside down by lift generated the other wing."
Bravo, A-FLOOR. Excellent description of the mechanics of the structural failure. Most interesting.