As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING THE DND STRUCTURAL INSPECTION AND REPAIR PROGRAM (SIRP), THE STABILIZER WAS REMOVED AND STRIPPED OF ITS FABRIC AND PAINT. AT THAT POINT A CRACK WAS DISCOVERED PROCEEDING FROM THE END OF THE FWD. ATTACHMENT TUBE TOWARDS THE ATTACHMENT BOLT HOLE. JUST PRIOR TO THE BOLT HOLE THE CRACK SPLIT INTO A SHAPE AND ONE END WENT INTO THE BOLT HOLE AND THE OTHER END BEGAN TO WRAP AROUND THE TUBE.