What was found
LT VERT STAB AND FUSELAGE ATTACHMENT ANGLE CRACKED ON T/E, ABOVE THE FWD OF TAIL CONE. REMOVED AND REPLACED LT VERT STAB DRAG ANGLE IAW REO 670-55-31-018
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT VERT STAB AND FUSELAGE ATTACHMENT ANGLE CRACKED ON T/E, ABOVE THE FWD OF TAIL CONE. REMOVED AND REPLACED LT VERT STAB DRAG ANGLE IAW REO 670-55-31-018