As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ON NR 2 ENG CJ9 CORE HARNESS THERE ARE TWO LEADS ON WHICH THE STEEL BRAID IS WORN THROUGH. REPLACED NR 2 ENGINE CJ9 CORE HARNESS THROUGH STEP F(1) OF MM 73 21 06. FADEC SYS TEST TASK 73 21 00 840 801 F00 73 21 00 700 804 F00 73 21 00 700 808 F00 AND 73 21 00 700 809 F00 OPS NORMAL. PERFORMED ACTUATORS TEST. REF MM 71 00 00 700 807 F00. ACTUATORS TEST PASSED. NO ACTUATORS TEST FAULTS NOTED.