What was found
PANEL 661AB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED) / STARTED DAMAGE REMOVAL PER SRM 51-70-04-2R-9 PARA 4 STEPS A & B CHOPPED FIBERS FILLED THE DEFECTIVE FASTENER HOLES & SET TO CURE IAW SRM 51-70-04-2R-9 PARA 4 STEPS D & E .;[07] USING BMS8-301/EA 9390 RESIN LOT JN1HAA6331 & CHOPPED FIBERS FILLED THE DEFECTIVE FASTENER HOLES & SET TO CURE IAW SRM 51-70-04-2R-9 PARA 4 STEPS D & E FABRICATED THE REPAIR PLIES ; LAID UP THE REPAIR ;VACUUM BAGGED LEAK CHECKED ;THEN SET TO CURE IAW SRM 51-70-04-2R-9 PARA 4 STEPS J-L .;[10] COMPLETED REPAIR PLY CURE PROCEDURE IAW SRM 51-70-04-2R-9 PARA 4 STEP M. PER GENERAL REPAIR SRM 51-70-04-2R-0 FIGURE 214 PAGE 39 REF CAL TOOL HOT BONDER ID ATS2802 CAL DUE 10/2023 .;[11] CORRECTIVE ACTION 7 IS A DUPLICATE ENTRY OF CORRECTIVE ACTION 6<BR><BR>VERIFIED CORRECTIVE ACTIONS 6-10;[12] REQUEST POST REPAIR EXAMINATION IAW SRM 51-70-04-2R-9 PARA 4 . O;[13] UT INSPECTED POST CURE IAW 737 NDTM PART 4 51-00-02. <BR>NO DISBONDS NOTED.<BR>EQUIP USED: <BR>-EPOCH 650 ID: ATS2031 CAL DUE: 03/23;[14] RESTORE THE CONDUCTIVE COATING : APPLIED BMS10-21 TYPE III CONDUCTIVE COATING ; CURED THEN TESTED GOOD IAW AMM 51-21-71-370-801 PARA 3. D . STEPS 1-4 & 7 (B) . REF CAL TOOL MULTIMETER ID ATS1658 CAL DUE 03/2023;