What was found
DURING WALKAROUND INSPECTION, MX FOUND THE NR 9 VARIABLE CAMBER FLAP - BULL NOSE PUNCTURE AND EDGE DAMAGE REF FIG 1. THE DAMAGE EXCEEDS THE LIMITS OF SRM 57-43-02, FIG 101, ALLOWABLE DAMAGE 3 - L/E FLAP SKIN. DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS; SCHEDULE REPEAT INSPECTIONS AT EVERY 15 FC AND PERMANENT REPAIR PRIOR TO THE ACCUMULATION OF 1,000 FH (FLIGHT HOURS) AFTER PART 1.