As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAJOR REPAIR - SKIN CRACKS ON TOP OF FUSELAGE AT F.S. 150.6 AT STRINGER 1 WERE FOUND DURING SCHEDULED STRUCTURAL CHECK. RIVET HEAD WAS SHEARED WITH CRACKS STARTING AT SAID RIVET AND ANOTHER CRACK AT A RIVET SAME LOCATION OTHER SIDE OF STRINGER 1. MAINTENANCE REPAIRED THE AFFECTED AREA IAW EO-09-1900-53-001. RII INSPECTION COMPLIED WITH PER TASKCARD 4.3.7.