As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DAMAGE FOUND ON CROWN AREA OF FUSELAGE ON RT SIDE AT STA 641 AND ONE INCH RT OF STRINGER S3R. REMOVED DAMAGE AREA THAT WAS OUT OF LIMITS. EDDY CURRENT ACP NO CRACKS NOTED. REPAIRED WITH SOLID FASTENER PER SRM 53-00-01 REPAIR 6 115824 THIS IS A PERMANENT REPAIR. DEEPEST PART OF DENT WAS REMOVED WITH REMOVAL OF GOUGE. NEW DENT MEASUREMENTS WITHIN LIMITS.