As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C2 CRACK ON FWD STRINGER END FITTING AT XRS 204 FROM STRINGER S-62 - S-63. REMOVED END FITTING AT STA XRS 204 S-62 - S-63 IAW SRM 51-03-02, FABRICATED AND INSTALLED END FITTING AT STA XRS 204 STRINGER S-62 TO STRINGER S-63 IAW DWG 5615767 AND SRM 51-1-20D.