As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 ENGINE INLET AND FAN BLADES DETAILED INSPECTION, FOUND ONE FASTENER COUNTERSINK ON 1 & 3 STRUT PANELS DAMAGED BY LOOSE FASTENERS. FOUND NR 2 ENG NR 3 STRUT PANEL AFT UPPER SCREW NUT CUP ON BEARING WORN. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 ENG NR 1 STRUT PANEL IAW AMM 72-23-07. REMOVED THE NR 2 ENG NR 3 STRUT PANEL. ACCOMPLISHED ALT DEACTIVATION. ACFT CONFIG TO NORMAL.