As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TWO CRACK INDICATIONS APPROXIMATELY 1 INCH, EACH LENGTH FOUND DURING X-RAY INSPECTION AT STA 5-123, LONGERON 1L SPLICE AFT AND FWD CTR SECTION. THE LONGERON SPLICE REMOVED IAW SRM 51-33-01-0G. A NEW LONGERON SPLICE WAS FABRICATED IAW DWG #A5A7111 REV C AND INSTALLED IAW SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.