As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON VERTICAL STAB LH FACE TO FUSELAGE FWD. AFT DRAG ANGLE BTW STRG DATUM 37.81 & RS 23.11 (TRACE AT BL 0.00) VERTICAL STAB LH FACE TO FUSELAGE FWD. AFT DRAG ANGLE BTW STRG DATUM 37.81 & RS 23.11 (TRACE AT BL 0.00) WAS REPAIRED PER SRM 55-31-00-201-001-A01