What was found
RIGHT VERTICAL STAB TO FUSELAGE AFT ANGLE HAS EVIDENCE OF A CRACK ON THE FWD END APPROX 3/4 INCHES LONG. REPAIRED IAW ERS-CR-55MR-229.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT VERTICAL STAB TO FUSELAGE AFT ANGLE HAS EVIDENCE OF A CRACK ON THE FWD END APPROX 3/4 INCHES LONG. REPAIRED IAW ERS-CR-55MR-229.