What was found
R/H WING # 5 SLAT LOWER CENTER WEDGE HAS CRACK ON EDGE OF WEDGE. REMOVED R/H WING # 5 SLAT LOWER CENTER WEDGE IAW SRM 51-40-02-0G-0. UT IAW B737 NDT PART 4; 51-00-01. NO ADDITIONAL DEFECTS NOTED. TOOL#31896; DUE 29APR25. EVALUATED AND FOUND SMALL CRACK AT CENTER OF FLEX SKIN AS MARKED. FOUND TO BE REPAIRABLE FOR 250 DEGREE PRE-PREG LAY UP IAW SRM 57-42-01-2R-13 AND SRM 51-70-05-2R-0 REPAIR GENERAL.REMOVED DAMAGE & TAPER SANDED IAW SRM 57-42-01-2R-13 STEP 4 E-H. VERIFIED MATERIAL IAW SRM 57-42-01-2R-13 STEP 4 I-J. BONDED REPAIR IAW SRM 57-42-01-2R-13 STEP 4 J-U AND SRM 51-70-05-2R-0 REPAIR GENERAL LWR AND UPPER SURFACE AT 250 DEGREES FOR 90 MINUTES EACH SIDE (OVEN B0-06 EXP 4-25-25). UT IAW B737 NDT PART 4; 51-00-01. NO DEFECTS NOTED. SEALED TOOL SIDE AROUND REPAIR IAW SRM 57-42-01-2R-13 STEP 4 (X)(1-2). EC3501 (B108904). APPLIED ANTI-STATIC IAW SRM 57-42-01-2R-13 STEP 4(X)(3) AND SOPM 20-10-06. APPLIED PRIMER BMS 10-103 (A275086) IAW SRM 57-42-01-2R-13 STEP 4 (X)(4). APPLIED DECORATIVE FINISH IAW SRM 57-42-01-2R-13 STEP 4 (X)(5). PAINT. APPLIED TOPCOAT PAINT IAW SRM 57-42-01-2R-13 AND AMM 51-21-99-701.