What was found
INSPECTION TYPE:C LEFT WING OUTBOARD FLAP-FOREFLAP LEADING EDGE SKIN CRACKED AT RIVET HEAD (NR 2 FOREFLAP CARRIAGE). PERFORMED HFEC INSP OF CRACK AT L/W O/B FOREFLAP IAW NDT MANUAL PART 6, 51-00-00, FIG 4. VERIFIED CRACK EXTENDS FROM RIVET HOLE TO SKIN EDGE. NO STOP DRILL REQUIRED. INSTALLED DOUBLER REPAIR AS PER B727 S RM 57-50-4 FIG 7. MATERIAL USED, 2024-T3, 0.063, 5 BY 8.