As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THREE SEPARATE ITEMS OF DAMAGE TO LT IB AFT FLAP AND MID FLAP: A) TEAR IN LT IB MID FLAP AFT PANEL 0.800" LONG BY 0.500 HIGH. ALLOWABLE DAMAGE PER SRM 51-70-02. TEAR IN ALUM SKIN UPPER SURFACE RUB STRIP LT IB AFT FLAP 0.600 INCH TEAR WITH CRACKS EMANATING FROM EITHER END 0.200" OB END AND 0.150" IB END. IMPACT DAMAGE TO T/E OF LT IB AFT FLAP 0.650" LONG BY 0.200" HIGH.