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 MW0325 HARNESS AT 3:00 POSITION SIX INCHES FORWARD OF RIGHT CORE DETECTOR LOOP HAS 5 INCHES OF HARNESS SHIELD SHEATH MISSING BEHIND PNEUMATIC DUCT. ACFT GROUNDED. REMOVED & REPLACED FIRE DETECTION HARNESS IAW AMM 26-11-02. ENGINE FIRE DETECTION OPS TESTED GOOD IAW AMM 26-11-00.