As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
A 2 INCH LONG CRACK WAS FOUND IN THE FUSELAGE SKIN 3 INCH FWD OF FS 756 AND JUST ABOVE STRINGER 20R. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 380723-14.