As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT I/B MAIN FLAP DELAMINATED AT OB WEDGE PANEL. REMOVED LH IB MAIN FLAP OB WEDGE PANEL IAW CMM 57-53-05. RE-INSTALLED LT MAIN FLAP OUTBOARD WEDGE PANEL PER CMM 57-53-05 AND COMPLIED WITH TEMPORARY REPAIR OF DELAMINATED DAMAGE PER EA 21-157-01555 (REF TTG8Q00TTKP9).