What was found
#2 ENGINE PYLON PANEL 444AL IS DELAMINATED AT AFT LOWER CORNER< PANEL TO BE OUT OF ALLOWABLE DAMAGE LIMITS ACCORDING TO SRM 54-50-70-1A-3; PARA'S 2.A.(4); AND 4.A.(4).<BR><BR>AREA OF DAMAGE IS TO BE REPAIRED ACCORDING TO SRM 51-70-05-2R-6; AS REQUIRED BY SRM 54-50-70-2R-3; PARA'S 2.C; 4.B.(2); AND TABLE 202.<BR><BR>REMOVED DELAMINATED PLIES TO A REGULAR SHAPE; TAP TESTED AREAS (NO DISBONDS NOTED); REMOVED CONTAMINANTS FROM REPAIR AREA; AND PREPARED AREA FOR APPLICATION OF REPAIR PLIES; ALL ACCORDING TO SRM 51-70-05-2R-6; PARA'S 4.A AND 4.D.;] CLEANED REPAIR AREA; FABRICATED AND APPLIED REPAIR PLIES FROM BMS 8-139; ST 1581 FIBERGLASS (LOT# 1507054-1) AND BMS 5-154; GR 05 ADHESIVE (LOT# 1515856-1); VACUUM BAGGED UNIT FOR HEAT BLANKET CURE; ACCOMPLISHED VACUUM BLEED DOWN TEST (PASS); CURED REPAIR AREA; REMOVED ALL BAGGING MATERIALS; AND LIGHTLY SANDED THE REPAIR AREAHOT BOND CONSOLE ID: NCX000526; DUE: 11/2023;[05] INSPECTED AND VERIFIED CORRECTIVE ACTION 4.;[06] REQUEST NDI FOR UT DISBOND CHECK IAW SRM 51-70-05-2R-6 PARA 4.H;[07] 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;[08] APPLIED AND CURED CONDUCTIVE COATING;REFINISHED IAW AMM 51-21-99-300-802 PARA 3.C(1)(A-E)<BR><BR>REPAIR DELAMINATION AT AFT LOWER CORNER ON #2 ENGINE PYLON PANEL 444AL IAW SRM 51-70-05-2R-6;