As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON VERTICAL STAB RH FACE TO FUSELAGE FWD/AFT DRAG ANGLE BTW STRG DATUM 37.81 & RS 23.11 (TRACE AT BL 0.00) VERTICAL STAB RH 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