As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT ENGINE THRUST REVERSER INBOARD HALF INNER FAN DUCT WALL AFT SKIN HAS SURFACE CORROSION. REMOVED CORROSION AT RIGHT ENG THRUST REVERSER INBOARD HALF INNER FAN DUCT WALL AFT SKIN IN REF SRM 51-10-02-0G-0. ORIGINAL THICKNESS 0.071" MIN THICKNESS NOTED: 0.053, REMOVED MATERIAL: 0.018" FOUND OUT OF LIMITS IAW SRM 54-30-01-1A-4. COMPLIED REPAIR WITH THE REQUIREMENTS OF ESR-WI 15-15326 AND ECRA5430-02428.