What was found
INSPECTION FOUND TWO .5 INCH CRACKS THROUGH BOLT HOLES AT O/B LOWER ANGLE INSIDE RT WING FIXED LEADING EDGE RIB, WBL 92.0 (AFT OF NR 4 L/E FLAP I/B END). THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, PAGE 2, 51-40-3, PAGE 1, AND 51-20-2, PAGE 1.