As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE FRAME 47 SPLICE FITTING FOUND CRACK DURING NDT INSPECTION. COMPLIED WITH EA 6-5310-T0326855 P1. FUSELAGE, MAINFRAME AD 2006-01-10. SB A300-53-6123. HOLE CRACKS ON FRAME 47 AND SPLICE FITTING LT & RT. THIS IS A MAJOR REPAIR IAW GMM 6-2-100.