As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE SENSOR IS ATTACHED TO THE SPOILER AT THE HINGE POINT AND ROTATES WITH THE SPOILER WHEN IT IS DEPLOYED. THE SENSOR SHAFT IS CONNECTED AND INDEXED TO THE WING AND REMAINS STATIONARY DURING DEPLOYMENT. THE 3 WIRES THAT CONNECT THE SENSOR MUST TWIST WITH THE SENSOR ON EACH DEPLOY CYCLE, CAUSING STRESS ON THE WIRE HARNESS. THE WIRE WORK HARDEN AND BREAK. ALL 4 SPOILER WIRE HARNESS HAVE BROKEN.