As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PART CRACKED AT 90 DEGREES BEND RADIUS FROM APPROX 5 O`CLOCK POS. TO THE 10 O`CLOCK POS. BEFORE IT CRACKED TO THE OUTER SURFACE WHERE IT WAS NOTICED DURING A DAILY INSPECTION. PROBABLE CAUSE MAY HAVE BEEN AN EARLIER GROUND BUMPING INCIDENT THAT CAUSED OTHER DAMAGE TO THE AIRCRAFT. RECOMMENDATIONS TO PREVENT RECURRANCE WOULD BE TO CHOSEY INSPECTION. THIS AREA AFTER ANY TAIL BUMPING INCIDENT.