What was found
CORROSION ON LATERAL BEAM AT FWD CABIN BS270 LBL10 WL208.<[01] REMOVED 1 EA HILOK AT LBL 10 BS 270WL 208.1 IAW SRM 51-40-02;[02] REMOVED CORROSION ON LATEAL BEAM AT FWD CABIN BS 270 LBL 10 WL 208 IN 1.1'LX 0.8'W AREA IAW SRM 51-10-02;[03] VERIFIED CORRECTIVE ACTIONS 1 AND 2;[04] REQUESTED HFEC UT REMAINING THICHNESS ON THE BLENDED AREA AND OPEN HOLE;[05] ACCOMPLISHED HFEC SURFACE SCAN IAW 737 NDTM PART 6 CHAPTER 51-00-00 PROCEDURE 23. NO CRACKS NOTED.<BR><BR>ACCOMPLISHED HFEC OPEN HOLE INSPECTION IAW 737 NDTM PART 6 CHAPTER 51-00-00 PROCEDURE 16. NO CRACKS NOTED.<BR><BR>ACCOMPLISHED HFEC COUNTERSINK INSPECTION IAW 737 NDTM PART 6 CHAPTER 53-30-00 PROCEDURE 3. NO CRACKS NOTED.<BR><BR>ACCOMPLISHED UT THICKNESS MEASUREMENT IAW 737 NDTM PART 4 CHAPTER 51-00-00 PROCEDURE 2.<BR>MINIMUM REMAINING MATERIAL THICKNESS FOUND 0.077' ADJACENT TO 0.100'<BR><BR>EQUIPMENT USED: <BR>-NORTEC 600 ID: ATS2353 CAL DUE: 01/2024<BR>-EPOCH 600 ID: ATS843 CAL DUE: 06/2023;[06] AFTER REMOVED CORROSION ON LATEAL BEAM AT FWD CABIN BS 270 LBL 10 WL 208; EVALUATED DAMAGE ON REWORKED AREA ORIGINAL THICKNESS .100' MATERIAL REMOVED 0.023' REMAINING MATERIAL; 0.077' ALLOWABLE DAMAGE ONLY 10% OF MATERIAL LOSS; FOUND TO BE OU OF LIMIT IAW SRM 53-10-51-1A-1;[07] VERIFIED CORRECTIVE ACTION ITEM 6.;[08] FABRICATED REPAIR PARTS; [1] STRAP FROM MAT 7075-T6#0.063 LOT# 1498631-1 [2] 3(EA) TAPERED FILLERS FROM MAT 7075-T6#0.063 LOT# 1498631-1; LOCATED AND DRILLED ALL PARTS IAW EA NO: 23-153-00883;