As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
REF T/C 78472000, NR 1 ENGINE INLET AND FAN BLADES. DETAILED INSPECTION FOUND NR 5 FAN STRUT PANEL 5 O'CLOCK POSITION HAS 1 FASTENER INSERT DELAMINATED FROM PANEL, AFT OTBD FASTENER. ACFT GROUNDED. REPLACED NR 5 FAN STRUT PANEL AT 5 O'CLOCK POSITION, REF AMM 72-23-02.