What was found
LEFT VERTICAL STAB TO FUSELAGE FWD ANGLE HAS EVIDENCE OF A CRACK ON THE AFT END. APPROX 1 INCH LONG. REPAIRED IAW EO CR-55MR-038.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT VERTICAL STAB TO FUSELAGE FWD ANGLE HAS EVIDENCE OF A CRACK ON THE AFT END. APPROX 1 INCH LONG. REPAIRED IAW EO CR-55MR-038.