From the Materials report in the docket of the subject accident: "
The cable segments had separated in two locations, mid‐length through the wires and at an attaching clasp. The fracture surfaces were examined using a 5x to 50x stereo‐zoom microscope.
The features on all of the fracture surfaces were consistent with overstress." [emphasis added] They attributed the overstress to crash dynamics, not something that happened in flight.
They did not report any sign of prior degradation. It's not exactly a thorough report but the highlights don't support the speculation.
Probable cause: "A loss of aircraft control for reasons that could not be determined because postaccident examination did not reveal any evidence of preimpact mechanical malfunctions or failures of the flight controls that would have precluded normal operation."
Final report (NTSB).
Nauga,
and his weekly reader