As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C-CK, FORWARD CARGO PIT AT BODY STA 800 AND BETWEEN STR 22R AND 23R , FUSELAGE FRAME INBD FLANGE HAS DENT. REMOVED DAMAGE AND REPAIRED STA 800 FRAME BETWEEN STR 22R AND 23R IAW SRM 53-00-07-2R5 FABRICATED -1 REPAIR ANGLE FROM 7075-0 .071 AND HEAT TREATED TO T6 IAW SRM 53-00-07-2R5 DETAIL I. ORIGINAL FRAME THICKNESS .063"