As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(AUS) FUSELAGE SKIN BULGING AT L25 BETWEEN STN 1070 AND STN 1081 - WHENTHE SKIN WAS LIFTED BACK THE FOLLOWING CORROSION WAS FOUND:1. FILIFORM CORROSION ON FACE OF 'T' SECTION BETWEEN STN 1070 AND STN 10762. EXFOLIATION CORROSION ON ONE SIDE OF THE BACK FACE OF THE 'T'BETWEEN STN 1076 AND STN 1081