What was found
AFT CABIN FLOOR PANEL SUPPORT AT Y-765 LT FR 66 TO FR68 SCEW HOLES CORRODED. REMOVED CORROSION, MATERIAL REMOVED .035 INCH (BEYOND LIMITS AS PER A320 SRM 53-41-14). REPLACED BEAM AS PER A320 SRM 51-42-11 PG 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT CABIN FLOOR PANEL SUPPORT AT Y-765 LT FR 66 TO FR68 SCEW HOLES CORRODED. REMOVED CORROSION, MATERIAL REMOVED .035 INCH (BEYOND LIMITS AS PER A320 SRM 53-41-14). REPLACED BEAM AS PER A320 SRM 51-42-11 PG 1.