What was found
CORROSION ON FSD MOP SILL BS294+7; BS326 - BS346 RBL56 WL208.<[01] VERIFIED APPLICABILITY OF SRM 53-10-15-1A-2;[02] REMOVED CORROSION ALONG FSD MOP SILL <BR>AT RBL56; WL208 BS 291.5 + 11' - BS312 + 10' L:20' X W:1'; REMOVED CORROSION ALONG FSD MOP SILL AT RBL56; WL208; BS328 + 2'; L: 2 X W:1' D: 0.002' FROM ORIGINAL THICKNESS IS 0.080' FOUND WITHIN LIMITS PER SRM 53-10-15-1A-1 FIG. 103 DETAIL D.;[08] REMOVED CORROSION ALONG FSD MOP SILL AT RBL56; WL208; BS 291.5 + 11' - BS312 + 10' L:20' X W:1'; D: 0.005' FROM ORIGINAL THICKNESS IS 0.080' REMOVED MATERIAL AROUND THAN MORE THREE FASTENERS IN ALL GROUPS OF TEN; FOUND WITHOUT LIMITS PER SRM 53-10-15-1A-1 FIG. 103 DETAIL G. DAMAGE IS BEYOND LIMITS DUE TO REMOVED MATERIAL AROUND THAN MORE THREE FASTENERS IN ALL GROUPS OF TEN; FOUND WITHOUT LIMITS PER SRM 53-10-15-1A-1 FIG. 103 DETAIL G. DAMAGE IS BEYOND LIMITS DUE TO REMOVED MATERIAL AROUND THAN MORE THREE FASTENERS IN ALL GROUPS OF TEN; FOUND WITHOUT LIMITS PER SRM 53-10-15-1A-2 FIG. 103 DETAIL G.;[11] HFEC ROTARY INSPECTED OPEN HOLES IN BLENDED AREA PER 737NDT PART 6 51-00-00 PROCEDURE 16. NO CRACKS FOUND. TOOL N500 IS000681 DUE 04/2024.;[12] UT INSPECTED BLENDED AREA IAW 737 NDTM PART 4; 51-00-00 PROCEDURE 2.<BR>REMAINING MATERIAL THICKNESS IS 0.074' ADJACENT TO 0.080'. <BR>SEE ATTACHED GRID.<BR>EQUIP USED: <BR>-EPOCH 650 ID: ATS2342 CAL DUE: 07/23;[13] COMPLETE;[14] VERIFIED MEASUREMENT TABLE AND CORRECTIVE ACTION 13