As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
GSO - INSPECTION FOUND A 4 INCH BY 2 INCH HOLE AND SEVERAL CRACKS TOTALING 12 INCHES IN LENGTH IN SKIN PANEL ABOVE RUDDER ON RIGHT SIDE OF VERTICAL STABILIZER. THE DAMAGED SKIN WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-01 AND SRM 51-30-8. (X)