I agree.For example, from one of the forums I attended at Oshkosh this year:
Aft cg limit is commonly determined from compliance with spin recovery requirements.
Another point is that there are some aeroplanes around where, at aft cg, the stick position to hold a steady airspeed does not vary much so the term "stall stick position" is of little use as a cue.
As a comparison, the Decathlon spin doesn't vary much in behaviour between the forward and aft limits although at fwd cg it may tend to enter a spiral dive. Misuse of of aileron and/or power will flatten it regardless of cg; forward stick prior to rudder on recovery will steepen the nose down attitude (an accelerated spin) which can significantly delay the recovery.