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 FWD/AFT DRAG ANGLES BTW 55.625 % STRG DATUM TO 67.5 % REAR SPAR DATUM (TRACE AT BL 0). CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLES BTW 55.625 % STRG DATUM TO 67.5 % REAR SPAR DATUM (TRACE AT BL 0) WERE REPAIRED PER SRM 55-31-00-201-001-A01