As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STRINGER 25 RIGHT IS CORRODED BETWEEN FS 319-333. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT-3. MIN MATERIAL REMAINING IS .042", ORIGINAL IS .063:, MATERIAL REMOVED IS .021". REPAIRED IAW REO 670-53-21-865.