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For me this looks like a fully inverted nose down impact. Fuselage completely disintegrates, wings (being the most heavy part) slide forward and come to rest at end of debris field (inverted in direction of flight). Due to fuselage desintegration, the tail section flips over 180° and lands VTP up agains flight direction destroying most of the lower forward part but keeping the HTP attached.
Again, and how would the main gear strut come off that early in the szenario above? It is designed to withstand heavy loads. The strut located in the vicinity of the tailsection
http://www.pprune.org/rumours-news/4...ml#post5699903 is not only seperated from the structure, the lower crossbone supporting the four wheels is separated as well and shows in onother picture bent and broken
http://www.pprune.org/rumours-news/4...ml#post5701898 . That kind of damage is most probably asociated with excessive loads on the whole wheel assembly while still attached to the aircraft. The inverted impact does not fit for this kind of damage.
franzl