What was found
DURING C CHECK, RT WING NR 4 LEADING EDGE FLAP INNER SKIN CRACKED 3 PLACES AROUND RIVETS AT INBOARD IND WS 150. STOP DRILLED 3 EACH CRACKED PLACES AROUND RIVETS AT INBOARD END WS 150 (DIAMETER 0.190") IAW SRM 51-10-1 AND 57-50-3 FIGURE 12. HFEC C/W AROUND STOP DRILL HOLES, NO CRACKS NOTED PER NDT PART 6 51-00-00 FIG 23. FABRICATED REPAIR DOUBLER IAW SRM 57-50-3 FIGURE 12. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR DOUBLERS IAW SRM 51-30-2 AND 57-50-3 FIGURE 12.