What was found
RT WING SLAT #6 T/E WEDGE TOP SURFACE I/B CORNER HAS CORROSION. ; / [01] REMOVED CORROSION AT R/WING #6 SLAT UPPER SURFACE I/B CORNER AS REFERENCE B737-700 SRM 51-10-02-0G-0; [02] CERTIFIED; [03] VERIFIED CORROSION REMOVAL; [04] PERFORMED UT THICKNESS INSP ON REWORKED AREA. IAW B 737 NDT PART 4 51-00-00 PROCE 3. TOOL 27MG. BC 172139. CALIB DUE 4-1-22. MINNI THICK 0.018'.; [05] AFTER UT THICKNESS INSP. FOUND REWORKED AREA WIHING LIMITS AS REFERENCE B737-700 SRM 57-42-01-1A-1 STEP 4.B.2 FIGURE 105 ORIGINAL MAT.020' MATERIAL REMOVED.002' MATERIAL REMAINING .018'; [06] VERIFIED LIMITS; [07] OK TO ALODINE AND PRIME & TOP COAT; [08] TREATED; PRIMED AND TOP COATED REWORKED AREA AS REFERENCE B737-700 SRM 51-20-01-0G-0; AMM 51-21-72-370-804 AND AMM 51-21-73-370-803; [09] VERIFIED STEP # 8