What was found
RIGHT VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE APPEARS TO BE CRACKED APPROX. ONE INCH IN LENGTH. REPAIRED IAW EO-CR-55MR-038.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE APPEARS TO BE CRACKED APPROX. ONE INCH IN LENGTH. REPAIRED IAW EO-CR-55MR-038.