What was found
REMOVED DAMAGED UPPER SKIN @ S-24-R AND APROX STA 216 TO 226 PER AVO11125 STEP 3. C/W AVO11125 REV A. VERIFIED REMOVED DAMAGED UPPER SKIN S-24-R AND APROX STA 216 TO PERFORMED 737 NDT PART 6, 51-00-00 TO VERIFY CRACK FREE AREA OF 226 PER AVO11125 STEP 3 IAW AV011125, AND REMOVED EXISTING DMG CUT OUT IAW AVO 11141 SREP 2, NO CRACKS FOUND. ON UPPER SKIN AT APROX STA 216-229 S-24-R PER AVO11141 STEP 2. REMOVED EXISTING DMG ON UPPER SKIN AT APROX STA 216-229 @ S-24-R NEED TO PERFORM NDT OF DMG REMOVAL PER AVO 11141 STEP 2. PER AVO11141 STEP 2 MATERIAL ID FOR UPPER SKIN REPAIR REF AVO11141 PAGE 3 SUB STEP C1 IS AS FOLLOWS: 2024-T3 .040 / PO# 9006951 FOR -1 DOUBLER AND -4 FILLER 2024-T3 .063 / PO# 2407996 FOR -2 TRIPLER AND -3 FILLER 2024-T3 .032 / PO# 2677856 FOR -5 FILLER VERIFIED MATERIAL ID FOR UPPER SKIN REPAIR REF AVO11141 PAGE 3 SUB STEP C1 IS AS FOLLOWS: 2024-T3 .040 / PO# 9006951 FOR -1 DOUBLER AND -4 FILLER 2024-T3 .063 / PO# 2407996 FOR -2 TRIPLER AND -3 FILLER 2024-T3 .032 / PO# 2677856 FOR -5 FILLER . PER AVO11141 REV.A NEED TO COMPLY WITH STEPS B.4 AND B.5 HFEC HOLE PROBE AND COUNTERSINK INSPECTION OF EXHISTING FASTENER HOLES COMMON TO REPAIR. ACP. RII INSPECTION IAW GMM 09-25-05 & AVO11141 REV A. ACP. OPEN HOLE HFEC IAW 737NG NTM PART6 51-00-00 PROCEDURE 16, & COUNTERSINKS IAW NTM PART 6 53-30-00 PROCEDURE 3. OF ALL EXISTING FASTENER HOLES COMMON TO POWER- EDIT TO PREVIOUS UPDATE... PER AVO11141 REV.B NEED TO COMPLY UPDATE TO PREVIOUS EDIT.