When extreme yoke movement cuts out stab trim on a 737-NG, does it stay off after yoke returns from limits?
From the Boeing 737 NG FCOM v2 (9.20.8 Flight Controls - System Description):


  Control column actuated stabilizer trim cutout switches stop operation of the main
  electric and autopilot trim when the control column movement opposes trim
  direction. When the STAB TRIM override switch is positioned to OVERRIDE,
  electric trim can be used regardless of control column position.


So any opposite movement of the yoke will stop the stab trim. There is nothing mentioned in the FCOM about staying off, so I would assume stab trim would continue immediately after the yoke is released.