What was found
CORROSION ON FLOOR SUPPORT AT FWD CABIN BS294+13 LBL11 WL208.<[01] NO ENTRIES FOUND ON SRM DAMAGE REMOVED I.A.W ORIGINAL MATERIAL THICKNESS IS 0.080' REMAINING MATERIAL THICKNESS IS 0.040 PART TO BE REMOVE AND REPLACE I.A.W SRM 51-10-02-0G-0 PAR 9.A(1);C;[02] VERIFIED CORRECTIVE ACTION 1.;[03] REMOVED DAMAGE LAV FLOOR SUPPORT BS294-312 LBL11 WL208 LOCATED AND DRILLED NEW ALL I.A.W SRM 51-10-02-0G-0;SRM 51-40-05-0G-0 AND BOEING DWG 141A5600 OK TO INSTALL;[04] VERIFIED CORRECTION ACTION ITEM 3 AND OK TO INSTALL GIVEN.;[05] CORRECTION ON CORRECTIVE ACTION 3 SHOULD READ<BR>INSTALLED NEW LAV FLOOR SUPPORT BS294-312 LBL11 WL208 LOCATED AND DRILLED NEW ALL I.A.W SRM 51-40-02-0G-0;SRM 51-40-05-0G-0 AND BOEING DWG 141A5600 OK TO INSTALL;[06] CORRECTION ON CORRECTIVE ACTION 5 SHOULD READ<BR>REMOVED DAMAGE LAV FLOOR SUPPORT BS294-312 LBL11 WL208 LOCATED AND DRILLED NEW ALL I.A.W SRM 51-40-02-0G-0;SRM 51-40-05-0G-0 AND BOEING DWG 141A5600 OK TO INSTALL;[07] INSTALLED NEW LAV FLOOR SUPPORT BS294-312 LBL11 WL208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A5600;[08] VERIFIED CORRECTION ACTION ITEM 7.;[09] COMPLETED REMOVED AND REPLACED LAV FLOOR SUPPORT BS294-312 LBL11 WL208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A5600 TASK COMPLETED;[10] VERIFIED CORRECTIVE ACTION 9;[11] VERIFIED MEASUREMENT TABLE