As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FUSELAGE FRAME AT STA 1580 AT S25L HAS DENT IN FREE FLANGE. REMOVED DAMAGE FABRICATED REPAIR ANGLE FROM 7075-0.080 HEAT TREATED TO T6 DRILLED UP AND INSTALLED REPAIR IAW SRM 53-00-07-2R5 FASTENER INSTALLED THROUGH STRINGER CLIP AND STRINGER INSTALLED IAW EA 111102 IR/UPS EO B757-5310-44170-A.