As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING AAIP A1040 300 HOUR, 12 MONTH INSPECTION, STEP A1040 2.4, A CRACK WAS FOUND IN THE LT UPPER STABILIZER MOUNT DURING THE VISUAL INSPECTION. THE CRACK RAN FROM THE FWD EDGE OF THE MOUNT THROUGH THE FWD OTBD BOLT HOLE & TO THE MIDLINE OF THE MOUNT.