Its not just CASA that is highlighting problems with this model, its happening all over the world with other CAA's.
A few that have crashed in AU have had chutes if i remember correctly so the comments about weight and balance are really not valid. Anyway, the aircraft should NOT be registered that it is that far out of balance that it can affect the flying performance and characteristics.
The piper sport (sport cruiser or whatever name they go by now) has just ceased manufacture and gone into bankruptcy again, I think it is the third time this has happened. There seems to be something generically wrong with this design and all of the clones that are having these problems.
The real issue here is that (in my opinion, from the outside) is not that the aircraft is or, is not dangerous to fly, the real issue here from what I see is that the manufacturer is refusing to properly validate their compliance. They claim that the aircraft has been tested thousands of times for spin characteristics but they can't produce the documentation or proof according to CASA and they tried to get the Tail-wheel aircraft through the spin approvals by using data from the nosewheel so the Tail-wheel aircraft was never tested but they stated that it did comply when in fact it was never tested.
I think this is the real problem for CASA, they (the manufacturer) are just declaring things as being safe or in compliance with the regulations that they have nothing to back it up and the manufacturer is just giving them the bird.
I was speaking with a guy at the airport yesterday and he was telling me about Cirrus how they couldn't meet the requirements for spin recovery so they added a parachute and managed to sneak through the certification. He said that no aircraft would ever be allowed to do this again and if the FAA had their time again they would not approve the aircraft until modifications were made so that it would recover from a spin.
The problem does not just exist with LSA, the problem also exists with certified aircraft. Another thing that just came to memory that he mentioned to me was that icon got a whole heap of dispensations which allowed a heavier takeoff weight than approved in LSA. This was apparently because they needed the extra weight to make their design completely spin proof but if I remember correctly more than a few have crashed very shortly after takeoff as a result of a stall/spin.
Just my two cents worth, none is expert opinion just information gained from around the traps