As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A SCHEDULED INSPECTION TO COMPLY WITH AD 2013-24-03, A CRACK WAS IDENTIFIED ON PN 101-6400 11-4. THIS PART IS LOCATED ON THE HORIZONTAL ATTACH POINT OF THE VERTICAL STABILIZER. A REPAIR WAS DEVELOPED BY THE MANUFACTURER TO CORRECT THIS IAW DWG FR-CO-102291 REV 1. ADDITIONAL PHOTOS & ILLUSTRATIONS RELATED TO THIS DISCOVERY WILL BE SUPPLIED TO SUPPORT THIS SDR.