As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C LH SIDE NWW INTERNAL BTN BS 260 AND 280 CRACK FOUND AT WL150, WL160 OF THE STIFFENER RADIUS RESPECTIVITY, CRACK LENGTH 1/4". NWW BS 260-280 WL150 AND WL160 INTERNAL STIFFENER REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.