As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C-CHECK, FORWARD CARGO PIT AT BODY STA 680 FRAME AND BETWEEN STRINGER 25R A ND 24R, FUSELAGE FRAME INBD FLANGE HAS DENT. REMOVED DAMAGE AND REPAIRED STA 680 FRAME BETWEEN STR 25R AND 24R IAW SRM 53-00-07-2R5. FABRICATED-3 REPAIR ANGLE FROM 7075-0 .063 AND HEAT TREATED TO T6 IAW SRM 53-00-07-2R5 DETAIL III. ORIGINAL FRAME THICKNESS .056".