Furthermore, the signature feature of the MCAS failure that downed the Lion Air flight was runaway trim, and there is no indication in this report that the crew had to take any action to stop it by disabling MCAS (setting STAB TRIM CUTOUT to CUTOUT, the documented procedure for doing so), or to restore the correct trim manually (as far as I know, it would not revert to the correct setting simply because MCAS was disabled.)
As far as I am aware (totally a layperson), there have been potentially only 3 potential 737-MAX MCAS trim issue occurrences:
1. The Lion Air flight prior to the fatal lion air flight
2. The Lion air flight which crashed
3. The Ethiopian flight which crashed
Of course I don't think any of those 3 are absolutely confirmed, but I do think it seems likely the three had MCAS trim related issues. If the success rate for pilots dealing with this issue just 1 in 3, does that say anything regarding the MCAS issue difficulty/complexity or the skill/training of pilots?
The latest crash certainly looks suspicious, but we don't really know yet, and the Lion Air crash occurred before the details about how MCAS could behave on sensor failure had been revealed. One would certainly hope that after this was revealed, all Max-8 pilots would be well prepared to recognize the situation and handle it, which might suggest that there is something more (or different) about this case (which could be worse news for Boeing).
Far from certain, becaus Boeing is selling and the companies indeed treat it as "the same plane like old" even if it obviously isn't:
For obvious reasons, pilots tend to take a keen interest in matters of aviation safety, so I wonder if this was not simply a repeat of the Lion Air crash (which, as I said elsewhere, might be even worse news for Boeing.)
[1] https://rgl.faa.gov/Regulatory_and_Guidance_Library/rgad.nsf...
Day 3 of 3 departing in a MAX 8 after a long overnight. I was well rested and had discussed the recent MAX 8 MCAS guidance with the Captain. On departure, we had strong crosswinds (gusts > 30 knots) directly off the right wing, however, no LLWS or Micro-burst activity was reported at the field. After verifying LNAV, selecting gear and flaps up, I set "UP" speed. The aircraft accelerated normally and the Captain engaged the "A" autopilot after reaching set speed. Within two to three seconds the aircraft pitched nose down bringing the VSI to approximately 1,200 to 1,500 FPM. I called "descending" just prior to the GPWS sounding "don't sink, don't sink." The Captain immediately disconnected the autopilot and pitched into a climb. The remainder of the flight was uneventful. We discussed the departure at length and I reviewed in my mind our automation setup and flight profile but can't think of any reason the aircraft would pitch nose down so aggressively.
This sounds very similar to the MCAS problems on the other flights, and these pilots were aware of MCAS (this is post Lion Air).
I have not read in detail yet about the proposed update to MCAS they are working on