What was found
LEFT VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE APPEARS TO BE CRACKED, 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.
LEFT VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE APPEARS TO BE CRACKED, ONE INCH IN LENGTH. REPAIRED IAW EO-CR-55MR-038.