As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INITIAL INSPECTION: CORROSION ON STRINGER SPLICE 25R AND 26R IN STA. FS= 327 TO FS= 337 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (E/E) (SM). IN REFERENCE NRC 00084 TASK 900-53-140-300 APPENDIX A ]. (TCI:100-09) STRINGER SPLICE 25R AND 26R IN FS327 TO FS337 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT WERE REMOVED AND NEW STRINGER SPLICE 25R AND 26R IN FS327 TO FS337 WERE INSTALLED PER SRM 51-42-06-001-001-A01. LEVEL CORROSION 2.