It's not the autotrim that you can't fight. The plane can be trimmed (elevator surface) in such a way that pilot yoke input (stabilizer surface) cannot fight against. That is common to all 737's, and all pilots know about it. It is not that the autotrim feature can't be fought.
What's new in the MAX is the autotrim doesn't terminate when the pilot gives back pressure on the yoke if MCAS senses high angle of attack, it will do an uncommanded nose down (every I think 10s). This is to compensate for the MAX engine nacelle which provides a meaningful amount of lift to cause a pitch up moment in high angles of attack, unlike previous 737's.
I wonder whether the stall behavior between 737's is slightly dissimilar or very dissimilar without MCAS, between 737NG and 737 MAX? And then quantifying that difference. I also seriously wonder if it's even slightly more likely for a pilot to induce a stall as a result of not knowing about the natural uncorrected stall behavior of the new design compared to previous designs. MCAS is not my concern, it's how the plane flies without it that I wonder about.
Also, WSJ is reporting that the MCAS software update mandated by the FAA in an airworthiness directive was delayed due to the nearly five week government shutdown. I'm already imagining the tweets...