What was found
11" CRACK ON WING CENTER SECTION REAR SPAR BETWEEN 45.64 AND 31.83 STIFFENERS. COMPLETED INTERIM REPAIR IAW SRM 57-10-10-2R-2 PARAGRAPH 6. ITEM WILL BE PLACED ON GMM/MTI FOR TRACKING PURPOSES FOR A DETAILED VISUAL INSPECTION EVERY 3,000 FLIGHT CYCLES. IF ADDITIONAL DAMAGE IS FOUND DURING THE DETAILED VISUAL INSPECTION THE INTERIM REPAIR MUST BE REPLACED WITH A PERMANENT REPAIR AS GIVEN IN SRM 51-70-04, REPAIR 10.