As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STRINGER 26 RT BETWEEN FRAMES 333 AND 349 HAS CORROSION AROUND SEVERAL RIVET SHANKS. REMOVED CORROSION IAW SRM 51-42-06-001-001-A01 AND 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PROCEDURE UT-3. MINIMUM MATERIAL REMAINING IS .050 FROM ORIGINAL .063. MATERIAL REMOVED IS .013. REPAIRED IAW REO 670-53-21-744.