What was found
INSPECTION FOUND GENERATOR FEEDER CABLE CHAFED AGAINST ADJACENT CLAMP AT NR 2 ENGINE PYLON AT WING LEADING EDGE. THE CHAFING CAUSED CONTACT OF WIRE CONDUCTOR TO AIRCRAFT FRAME WITH ARCING DAMAGE TO FEEDER CABLE, CLAMP, AND ATTACH HARDWARE. THE FEEDER WIRE, CLAMP, AND HARDWARE WERE REMOVED AND REPLACED AND THE CLAMP WAS REPOSITIONED TO PROVIDE SUFFICIENT CLEARANCE.