As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INITIAL INSPECTION: CORROSION STR 26L BTW FS=280.00 / FS=333.00 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (E/E) (SM). IN REFERENCE NRC 00084 TASK 900-53-140-300 APPENDIX A ]. NEW STRINGER 26L BTW FS=280 AND FS=333 ATINTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT WAS INSTALLED PER SRM 51-42-06-001-001-A01 AND 51-42-20-001-001-A01. LEVEL CORROSION 2.