As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
IN THE PROCESS OF SSIP, NDT INSPECTION DISCOVERED RT SKIN CRACKED IS BETWEEN LAP JOINT AND LARGE EXISTING REPAIR. CRACK LOCATED AT BS 927 +13 BETWEEN STRINGER 20R AND 21R. CRACK APPROXIMATELY 3.5 INCHES LONG. 11/11/07 - CRACK WAS REPAIRED IN ACCORDANCE WITH ECO 3685.