As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CIRCUMFERENTIAL JOINT STRAP HAS CORRODED AT BS 280 STRINGER 26L-26R. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION IAW NDT INSPECTION PROCEEDURE 4.3. PERFORMED EDDY CURRENT INSPECTION IAW NDTM PT 1 51-20-006-250-A01. COMPLIED WITH EC/TC EA 30-2016-371.