As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STRINGER 25L IS CORRODED BETWEEN FS 319.00-333.00. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PROCEDURES UT-3, MIN MATERIAL REMAINING IS .038", ORIGINAL IS .063:, MATERIAL REMOVED IS .025". REPAIRED IAW REO 670-53-21-865.