As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-7 CHECK, INSPECTION NOTED CORROSION IN STRINGER CLIP AT STA 787, STR 26 R. MAINTENANCE FABRICATED STRINGER CLIP IN ACCORDANCE WITH BOEING DRAWING 69.35352. THE PART WAS THEN TREATED, PRIMED, PAINTED AND INSTALLED IN ACCORDANCE WITH THE REQUIREMENTS OF SOPM 20.41.02 AND SRM 51.40.02.