As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK INDICATION FOUND APPROXIMATELY 0.3 INCHES IN LENGTH ON FUSELAGE SKIN DURING HIGH FREQUENCY EDDY CURRENT INSPECTION AT BS 695 LONGERON 50L. REPAIRED IAW SRM 53-00-01 FIGURE 201 REPAIR 1 REVISION 53 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 119