As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(AUS) REAR FUSELAGE SKIN CRACKED IN FIVE PLACES AROUND TWO RIVETS AT STN 210 BULKHEAD AND NEAR STRINGER PNO HSJ 5893 - CRACK LENGTHSAPPROXIMATELY 10MM (0.393IN) - SUSPECT CAUSED BY OIL CANNING OF THE SKIN - STRINGER IS NOT ATTACHED TO THE BULKHEAD AT THIS POINT