As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 ENGINE RIGHT SIDE CORE AREA F10 HARNESS AT 1 O`CLOCK POSITION HAS DAMAGE TO OUTER CLOTH SHEATH MEASURING 1 INCH LONG, 2.5 INCHES FROM T3 SENSOR CONNECTOR DP1005. NO DAMAGE TO METALLIC SHEATH NOTED. ACFT GROUNDED. REPAIRED AFFECTED AREA IAW AMM 70-70-01-350-801-F00. . TESTED GOOD IAW EEC, TEST IAW AMM 73-21-00-700-804-F00.