As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE SCHEDULED MAINTENANCE THE FUSELAGE SKIN WAS FOUND CRACKED AT F.S. 447 BETWEEN STRINGERS 6R AND 7R. CRACK LOCATED AT UPPER FORWARD CORNER OF A PREVIOUS REPAIR. CRACK IS APPROXIMATELY .5" IN LENGTH. MAINTENANCE REPAIRED THE SKIN AND PERFORMED THE REQUIRED II INSPECTIONS AT F.S. 447 BETWEEN STRINGERS 6R & 7R I.A.W. E.O. 09-1900-53-029. MATERIALS UTILIZED ARE LISTED ON THE ENGINEERING ORDER.