As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L/H WING O/B T/E AFT FLAP I/B END LOWER T/E WEDGE SKIN DELAMINATED 1' FROM T/E AND 1' FROM I/B END. DELAMP MEASURES 9' X 8' / COMPLIED WITH REPAIR-57EA-04560 REFERENCE INSP-57EA-04562 AND REPAIR-57EA-04563 FOR REPEAT AND PERMANENT REPAIR