As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BS 333 FRAME CORRODED AT LOWER SIDE NEAR STRINGER 26L. REMOVED CORROSION IAW SRM 51-21-06-00. PERFORMED UT THICKINESS INSPECTION IAW MAC NDT PROCEDURES UT-3. MIN MATERIAL REMAINING IS .045" ORIGINAL IS .050" MATERIAL REMOVED IS.005". ALODINED AREA, WET SHOT RIVETS, PRIMED, PAINTED AREA IAW REO 601R-53-21-2264, ECTC 601R-53-21-2264.