As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT FUSELAGE, TO WING FILLET PANEL 152GT HAS A CHUNK OUT OF THE LOWER EDGE. REMOVED DAMAGED, CLEANED & PREPPED REPAIR. APPLIED REPAIR PLYS & VAC BAGGED. CURED & SANDED. APPLIED FIBERGLASS SEALER, CURED & SANDED SMOOTH IAW SRM 51-43-01 VOL II PARA 16-A (4) & 16-A (10). APPLIED REFINISH IAW SRM 51-21-02; VOL II. MINOR REPAIR