What was found
LEFT WING LANDING GEAR - SHOCK STRUT INBOARD DOOR FAIRING - LEADING EDGE DAMAGE. (REF FIGURE 1). DAMAGE FOUND TO BE BEYOND THE LIMITS OF SRM 52-80-02, FIGURE 101 ALLOWABLE DAMAGE 4 PER SRM 51-70-02, FIGURE 101 ALLOWABLE DAMAGE GENERAL. (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 OF EO 4452A162 AND FAA 8110-3 DATED 30OCT12. SCHEDULE REPEAT INSPECTIONS AT EVERY 5 FC (FLIGHT CYCLES) AND PERMANENT REPAIR PRIOR TO THE ACCUMULATION OF 1,000 FH (FLIGHT HOURS) PER SRM 51-70-17 OR SRM 51-70-07.