What was found
CORROSION ON FSD MOP SILL BS294+7 RBL54 WL208.<[01] VERIFIED APLICABILITTY OF SRM 53-10-15-1A-2;[02] EVALUATED CORROSION ON FSD MOP SILL BS294+7 RBL54 WL208 1'X1' ORIGINAL MATERIAL THICKNESS IS 0.080' REMAINING MATERIAL THICKNESS IS 0.020' DAMAGE FOUND TO BE OUT LIMITS I.A.W SRM 53-10-15-1A-2 PAR 4.A(2)(A) FIGURE 103 DETAIL D PART TO BE REMOVE AND REPLACE I.A.W SRM 51-10-02-0G-0 PAR 9.A(1);[03] TOOLS USED CORRECTIVE ACTION 2<BR>TOOL USED<BR>ATS 1225 DUE DATE<BR>08/2023 AND<BR>ATS2883<BR>DUE DATE 04/2024.;[04] VERIFIED CORRECTIVE ACTIONS 1;2 AND 3.;[05] REMOVED FSD MOPSILL I.A.W SRM 51-40-02-0G-0;[06] LOCATED AND DRILLED FSD MOPSILL I.A.W SRM 51-40-05-0G-0 AND BOEING DWG 141A8310 OK TO INSTALL;[07] VERIFIED CORRECTIVE ACTION #6;[08] INSTALLED FSD MOPSILL I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A8310 EXCEPT FOR FASTENER COMMON TO FWD ATTACH ANGLE TO COCKPIT FLOOR COSTUMER CARD TTG8Q00M8TPR;[09] VERIFIED CORRECTIVE ACTION 8;[10] VERIFIED MEASUREMENT TABLE