As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
REPAIR OF CORROSION WAS FOUND AT SEVERAL LOCATIONS ALONG STRINGER 38R AND 39R AF FS 434. THE DAMAGE TO THE BUTT SPLICE STRIP WAS BLENDED AND HFEC INSPECTED. SKIN DAMAGE WAS REPAIRED PER THE SRM 53-00-01 FIG 201. INFORMATION WAS PROVIDED TO BOEING AND BOEING APPROVED THE REPAIR VIA 8100-9 FORM.