What was found
UPON INSPECTING THE EXTERIOR OF THE AIRCRAFT, FOUND THE RIGHT INBOARD TRAILING EDGE MID FLAP WEDGE DELAMINATED AT THE INBOARD END. ABOUT 20 INCHES FROM THE INBOARD END HAS A DELAMINATION APPROX 6 INCHES LONG SPANWISE AND THE WIDTH OF THE WEDGE. PART REPAIRED UTILIZING BOEING STRUCTURAL REPAIR MANUAL 51-40-20. ALUMINUM HONEYCOMB REPAIR, 51-50-2 MATERIAL IDENTIFICATION, AND 51-40-21. MATERIAL USED 7075-T6 .016" PO NR 9005802. THIS IS A MAJOR REPAIR AND PERMANENT REPAIR.