As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE/ATTACH FITTING, VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE: REPAIR FOR CRACK. THE VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE ON THE LT SIDE OF THE AIRCRAFT WAS FOUND WITH A .90 CRACK AT FS 937. THE CRACKED FLANGE WAS TRIMMED OUT AND A .080 THICK A-286 STEEL REPAIR ANGLE WAS INSTALLED PER ER/A 364553-14.