is it not true that this MCAS failure mode is just a special case of runaway trim?
That is true and it is why the failure risk analysis, performed during initial MAX certification, rated the risk from an unscheduled MCAS activation low and didn't required the added complexity of combining AoA inputs from both the left and right ADIRUs and FCCs. The risk assessment was based on the assumption that the pilots would respond to a runaway stabilizer by applying the runaway stabilizer non-normal procedure. The complexity of adding that comparison, without introducing new, unanticipated failure modes, is a big part of why re-certification took so long. After three flight where the crews did not (initially) respond as expected, the risk analysis was revised to a higher level that required the upgrade.
The part that is news to me is that the Ethiopian pilots *did* actually disable the electronic trim system, but still crashed (?). Is this accurate?
That is accurate, to a point. They did eventually take the STAB CUTOUT switches to CUTOUT but they didn't do it until the stabilizer trim had already been run to nearly full nose-down trim.
What they needed to do was follow the procedure which would have included disengaging auto-throttle and auto-pilot (instead of repeatedly trying to engage it), flying the airplane manual with pitch and power settings, limiting airspeed to something reasonable, all while using the primary electric trim (thumb switches) to keep the airplane in-trim by stopping and removing all of the MCAS nose-down trim input.
People seem to interpret my comments as me saying that it is easy. It isn't easy. V1 cuts aren't easy. Unexpected failures are not easy. It requires discipline, training, and experience to ignore the distractions and to fly the airplane first. That isn't easy, but it is necessary if you are going to transport hundreds of paying passengers at this level. Both of the accident airplanes were very flyable. This was proven by the second-to-last crew to fly the Lion Air accident airplane. Not only did they, after prompting from the jumpseater, successfully stop the MCAS activations but they continued to fly the airplane to its intended destination in it's system degraded condition. (Something that never would be accepted at a western airline). (The airplane was degraded as it had lost its stall warning system, autopilot system, half of it's primary flight data, electric trim, speed-trim system, and its high-AoA pitch-feel protection)