As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE CPCP INSPECTION, FOUND STRINGER END FITTINGS CRACKED S-34R AND S-34L STA1530 AFT SIDE. REMOVED END FITTINGS IAW DC8 SRM 51-1-20. INSTALLED NEW END FITTINGS IAW DC8 SRM 51-1-21. CORROSION TASK CARD NUMBER C5600-0551. NON-ROUTINE TASK CARD NUMBER 11285.