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 TRANSVERSE SKIN SPLICE AT STA 5-0, FOUND ONE CRACK APPROX 5 INCHES ON SPLICE LONGERON 7L AT EDGE OF 3 - 7 FASTENERS. REPAIRED IAW SRM 53-00-05 REPAIR 1 AND EA 1-5310-T0334128 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.