Earlier quoted context omitted.
But the normal way of stopping it (the yoke) doesn't necessarily work, and the pilots wouldn't necessarily think to physically stop the wheel with their hands. Well, no. Pulling on the yoke traditionally moves the elevator. MCAS adjusts the horizontal stabilizer. You can adjust the stabilizer with switches on the yoke or with the trim wheels by your knee. MCAS will pause for five seconds if the pilot hits one of the…
I believe you may have misunderstood the comment you were replying to. They were saying you cannot counteract MCAS's control inputs with the elevator alone. Which is a somewhat unconventional design, in a lot of aircraft the elevator can overpower the horizontal stabilizer, whereas with a bad sensor MCAS will continue to move the stabilizer until you cannot overcome it. To use a bad analogy, in a car the break is str…
Pulling on the yoke is not how you counteract a runaway stabilizer on the 737. I've pasted the relevant part of the QRH in a few previous comments. Yes, the stabilizer ultimately has more pitch authority under some circumstances. That may be what happened here, but if I'm interpreting the graphs on the preliminary report correctly I wonder about mechanical failure of some sort.
This gets a bit more complex with the 737 because moving the yoke WILL actually stop one of the stabilizer trim algorithms, but not MCAS.