As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACKED LEFT VERTICAL STAB TO AFT FUSELAGE ATTACHMENT DRAG ANGLE BTW 55.625% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. 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 IAW SRM 55-31-00-201-001-A01.