What was found
CORROSION AND WEAR ON BORES OF LT WING SLAT PANEL NR 2, RIBS BS XOS=196, XOS=240 AND XOS=286. RIBS BORES WERE REPAIRED WITH NEXT FINAL DIMENTIONS: XOS=196, 4 HOLES: 0.938" XOS=240, 2 HOLES: 0.940" XOS=286, 2 HOLES:1.123" AND REPAIR BUSHINGS WERE FABRICATED AND INSTALLED SO THE FINAL DIMENTIONS ARE WITHIN LIMITS OF REPAIR IAW SRM 57-02, PAR 9.