As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
IAH - DURING A-CHECK INSPECTION, THE RIGHT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPERSS ENGINEERING CHANGE REPAIR AUTHORIZATION EC5530-01013, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)