As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) ON AIRCRAFT 6125, THE CABLE 1EA17D22WHT/1EA18D22GRN OF HARNESS WAS FOUND DAMAGED APPROXIMATELY 4 INCHES FROM CONNECTOR J259. THE CABLE BEND RADIUS WAS NOT RESPECTED WHICH CAUSED AN AOG. THE SAME ISSUE WAS FOUND ON OTHER AIRCRAFT. PRODUCTION DID NOT FOLLOW THE BAPS 145-003 DURING INSTALLATION OF HARNESS. S/N: 6121, 6122, 6123 & 6124 ALSO AFFECTED. CAW PROJECT CL6-CA-77-0001.