Originally Posted by PJ2
In Neofit's linked image of the aft fuselage, the fixtures at the mid-point of the two cross-frames are the forward fastening mounts/pivot points for the THS.
That rear frame is an interesting structure. Trying to understand the thinking behind it, I guess the need to 'mount' the THS within the fuselage structure dictates it, i.e. the need to disassemble the double links at both sides when 'inserting' or removing the THS. Just curious how these links look like after the event.