As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING CURRENT C-CHECK AT SIAEC INSPECTION OF BS 2484 UPPER BULKHEAD STRUCTURE DISCOVERED THE WEB CRACKED AT STRINGER 15L LBL 45 WL 287.03. REMOVED STIFFENER 65B02571-153. TRIMMED OUT CRACK IN WEB AREA. DYE CHECKED AREA. NO FINDINGS. FABRICATED REPAIR DOUBLER, FILLERS AND REPLACEMENT STIFFENER (65B02571-153) FROM DRAWING 65B02571. INSTALLED PER STANDARD SRM 51-30 PRACTICES. (M)