As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 1 ENGINE INLET AND FAN BLADE DETAILED INSPECTION FOUND STRUT PANEL NR 5 AT 5 O'CLOCK POSITION HAS ONE AFT INBD INSERT DELAMINATED FROM PANEL. ACFT GROUNDED. REMOVED AND INSTALLED A NEW STRUT PANEL NR 5 AT 5 O'CLOCK POSITION IAW AMM 72-23-07.