As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
HOLE IN FUSELAGE ON THE RT SIDE FORWARD OF FS 423.25 AND 2 INCHES ABOVE STRINGER 12R. APPROXIMATELY 1 INCH V SHAPE HOLE/CUT. MAINTENANCE REPAIRED AFFECTED AREA WITH A FLUSH REPAIR IAW MFG SRM 51-70. RII COMPLIED WITH IAW TASKCARD 8.2.1. HOLE CUTOUT SIZE 1.3 INCH X 1.3 INCH.