As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK FOUND APPROX .7500" LENGTH DURING X-RAY INSPECTION AT STA 6-100, LONGERON 6R CENTER SECTION OF THE SPLICE. CRACKED LONGERON REMOVED. NEW LONGERON FABRICATED IAW DWG A6A7112 REV 'A'. FPI CARRIED OUT ON NEW FABRICATED LONGERON SPLICE FOUND NO CRACK. FABRICATED LONGERON SPLICE REWORKED IAW DWG A6A7112 REV 'A'. REPAIR CLASSIFIED AS MAJOR IAW GMM6-2-100 REV 112.