As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE: C, FORWARD CARGO BAY AT BODY STA 820 AND BETWEEN STR 23L AND 24L, FUSELAGE FRAME INBD FLANGE HAS DENT. REMOVED DAMAGE AND REPAIRED IAW SRM 53-00-07-2R5. FABRICATED REPAIR ANGLE AND HEAT TREATED TO T6 IAW SRM 53-00-07-2R5 DETAIL II. ORIGINAL FRAME THICKNESS .063".