As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK INDICATION FOUND DURING X-RAY INSPECTION AT BS 5-0, LONGERON SPLICE 1R FROM TWO EACH FASTENER HOLE. CRACK LENGTH APPROX 0.3 INCHES. AREA REMOVED IAW SRM 51-33- 01. NEW LONGERON SPLICE FABRICATED IAW DRAWING AEA7634 REVISION B. NEW LONGERON SPLICE INSTALLED IAW SRM 51-33-01. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.