As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING AN X-RAY INSPECTION ON THE TRANSVERSE SKIN SPLICE AT STA 5-0, FOUND ONE CRACK APPROXIMATELY 3 INCHES ON THE LONGERON SPLICE 2L. A NEW LONGERON SPLICE WAS FABRICATED IAW DRAWING AEA7634 REVISION B. REMOVED AND REPLACED IAW SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.