What was found
DURING C4/S1 CHECK, INSPECTION REPORTED RT ENGINE PYLON SUPPORT ANGLE THAT ATTACHES PYLON PANELS 423DL AND 424CR AT RIB 5 CRACKED (AREA AROUND AFT SCREW HOLE). REMOVED AND FABRICATED REPLACEMENT SUPPORT ANGLE IAW SRM'S 54-52-12, P28, 51-31-00, P44,51-44-11, 51-42-11 AND 51-72-11, AND AIRBUS DRAWING S2 D54630462. INSTALLED NEW SUPPORT ANGLE IAW SRM 51-42-11, P7.