As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING 3A INSPECTION THE LT FWD VERTICLE STABILIZER TO FUSELAGE DRAG ANGLE (SHAPE L ATACHMENT) WAS FOUND TO BE CRACKED APPROX 1.75" FROM THE AFT END. MX R & R THE AFFECTED DRAG ANGLE, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 07/12/13.