As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
IN SERVICE FLEXING OF WIRE BUNDLE CAUSED THE SHIELDING AND A WIRE TO BREAK AT THE AIRFRAME-TO-WIRE BUNDLE CLAMP. SERVICE LOOP DID NOT APPEAR TO BE OF SUFFICIENT SIZE TO ALLOW THE NEEDED FLEXING OF THE WIRE BUNDLE. FORCE SENSOR DID NOT FUNCTION.