What was found
CORROSION ON ANGLE AT MID CABIN BS663+29 RBL66 WL203.<[01] NO ALLOWABLE LIMITS FOUND DAMAGE TO BE REMOVED I.A.W SRM 51-10-02-0G-0 AND SUBMITTED ENGINEERING FOR FURTHER INSTRUCTION.;[02] REMOVED CORROSION ON ANGLE SURFACE AT MID CABIN BS692 RBL64-RBL65 WL203 1'X0.500' AREA I.A.W SRM 51-10-02-0G-0;[03] REQUEST HFEC TO VERIFY CRACK FREE CONDITION AND UT TO VERIFY REMAINING MATERIAL THICKNESS;[04] UPDATED P/N;[05] VERIFIED CORRECTIVE ACTION 1 AND 2;[06] ACCOMPLISHED HFEC SURFACE SCAN IAW 737 NDTM PART 6 CHAPTER 51-00-00 PROCEDURE 23. NO CRACKS NOTED.<BR><BR>ACCOMPLISHED UT THICKNESS MEASUREMENT IAW 737 NDTM PART 4 CHAPTER 51-00-00 PROCEDURE 2.<BR><BR>MINIMUM REMAINING MATERIAL THICKNESS FOUND 0.070' ADJACENT TO 0.071'<BR><BR>EQUIPMENT USED:<BR>-NORTEC 600 ID: ATS1465 CAL DUE: 09/2023<BR>-EPOCH 650 ID: ATS2342 CAL DUE: 07/2023;[07] AS PER EA 23-153-01206; THE REWORK IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITHOUT REPETITIVE INSPECTIONS AND NO TERMINATING ACTION REQUIREMENTS.;[08] VERIFIED CORRECTIVE ACTION 7.