As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(AUS) FUSELAGE REAR BULKHEAD CORRODED IN AREA OF STABILATOR ATTACHMENT BRACKETS - RIVETS POPPED AT FRAME OF FORWARD FIN ATTACHMENT AREA- FOLLOWING REMOVAL OF TOP AFT FUSELAGE SKIN AND SKIN ON FIN AND STABILISER. WIDE SPREAD SURFACE CORROSION WAS FOUND WHERE FRAMES AND STRINGERS ATTACH - SUSPECT DUE TO LACK OF CORROSION PROTECTION DURING MANUFACTURE