As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING THE HARNESS REPAIR PROCESS, THE FINAL ELECTRICAL CONTINUITY TEST FOR SHIELDING BETWEEN CONNECTORS WAS NOT PERFORMED. AS A RESULT, SUBSEQUENT TESTING ON SITE REVEALED THE ENGINE OVERSPEED HARNESS WAS FOUND TO BE NON-COMPLIANT WITH SAFRAN CONTAINMENT LETTER REQUES NO. 218065-26-CNT-005_V1.