Apologies if this has been mentioned before (I can't find a direct post...). On an
737NG Ground School Slide Show I see the following:
45. Control column actuated stabilizer trim cut out switches stop operation of the main electric and autopilot trim when the control column movement opposes trim direction. i.e. If the pilot is pulling nose up nose down trim is inhibited. When the STAB TRIM override switch is positioned to OVERRIDE, electric trim can be used regardless of control column position. The control column activated cut out switches are bypassed. [my emphasis]
Anyone know whether the Max is more-or-less the same? I.e., you can have tripped the cut-out switches, but their cut-out effect can be overridden?