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 295.00 AND 310.00 HAS CORROSION AROUND SEVERAL RIVET SHANKS. REMOVED CORROSION IAW 51-42-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PROCEDURE UT-3. MINIMUM MATERIAL REMAINING OS .042. DAMAGE IS OUT OF LIMITS IAW SRM CH 53-21-03-101-002. R & R STRINGER IAW SRM CH 51-42-06-001-001.