What was found
CORROSION WAS FOUND ON THE LT WING TOP NR 2 PANEL BETWEEN RIB 19 AND RIB 20, AT MANUAL REFUELING PORT CUTOUT. BLEND REPAIR WAS ACP IAW UA EVA 80263 AND EA 319-5721-13-A2032, ON N-R C6017Q. REPAIR MUST BE INSPECTED AT THRESHOLD OF 200,300 FLIGHT HOURS, OR 124,500 FLIGHT CYCLES, WHICHEVER OCCURS FIRST. INSP INTERVALS AND METHOD OF INSP HAVE NOT BEEN DETERMINED. MFG WILL ISSUE A NEW RAS WITH THE INSP INTERVALS AND METHOD BEFORE AC ACCUMULATES ABOVE FH AND FC.