As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A ROUTINE INSPECTION, FUSELAGE STRINGER NR 17 R WAS FOUND TO BE CORRODED BEYOND LIMITS. DAMAGED PORTION OF STRINGER WAS LOCATED BETWEEN FRAMES NR 35-40. MAINTENANCE REMOVED AND REPLACED THE DAMAGED PORTION OF STRINGER AND THE AIRCRAFT WAS LATER APPROVED FOR RETURN TO SERVICE. (M)