As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FW/AFT DRAG ANGLE BTW 55.625% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. (ET) HFEC INSPECTION WAS PERFORMED 01 CRACK WAS FOUND ON AFT DRAG ANGLE AND FWD DRAG ANGLE NO CRACKS WERE FOUND. IAW NDT MANUAL. PART 1. 51-20-06-250-A01 AND CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER SRM 55-31-00-201-001-A01