What did they fix? Basically they played with the software. They’ve limited the ability to continually reactivate, as well as reducing the amount (i.e. power) of the possible movement. It also now requires agreement between the two AoA systems. There were fixes to unrelated wiring systems.
What would I want?
1. Triple AoA system with agreement required from all three.
2. Reactivation of the stab trim cutout if the control column is moved in the opposite direction. This exists in virtually every other (non FBW) Boeing aircraft, but was removed from the Max.
3. Backup ELECTRIC trim. The days of a manual trim wheel, that does not have enough mechanical authority to move at all, at high speed, should have ended decades ago.
4. MCAS OFF switch on the coaming, right next to the master caution!
I’d probably like to hear an admission that the issue is not one of ‘stall prevention’. The aircraft obviously has an unacceptable pitch couple at high AoA and high power settings, so MCAS isn’t about making it stall proof, but all about gaining certification.