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 SIX PLACES IN AREA AROUND TWO RIVETS AT STN 210 BULKHEAD AND NEAR STRINGER PNO 105-440000-11 - CRACK LENGTHS 6MM (0.236IN) - SUSPECT CAUSED BY OIL CANNING OF THE SKIN - STRINGER IS NOT CONNECTED TO THE BULKHEAD AT THIS POINT