As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STRINGER 26L IS CORRODED BETWEEN FS 319.00-333. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURES UT-3, MIN MATERIAL REMAINING IS .052", ORIGINAL IS .063:, MATERIAL REMOVED IS .011". REPAIRED IAW REO 670-53-21-865.