As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EGT HARNESS CRUSHED (REF IPC 71-52-45 ITEM 83 OR 84) 6 INCHES FWD OF JUNCTION BOX IN CORE AREA. ON ENGINE NR 1, INSTALLED NEW EGT CORE HARNESS. HARNESS CLAMPS FROM JUNCTION BOX TO HALF WAY POINT ON HARNESS NEED TO BE INSTALLED AND HARNESS NEEDS TESTING PER MM. SECURED REMAINING CLAMPS OF EGT HARNESS AND ACP TEST PER MM, OPS CHECK NORMAL.