As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING TH ESTRUCTURE INSPECTION WAS AT UPPER FUSELAGE AFT PAX CABIN AT FR 68+80MM Y160.5 LONGITUDINAL BEAM WITH CORROSION. DUE TO THIS FACT LONGITUDINAL BEAM FROM FR 68 TO FR 70 Y160.5 WAS REPLACED IAW A319 SRM 51-72-11-911-001. THE REPLACE WAS HANDLED UNDER COOPESA JOB: A1M116 ITEM 2-21