What was found
REPAIRED CORRODED AREAS OF THE LT & RT WINGS UPPER SKINS LOCATED UNDER AND ADJACENT TO THE LT FORWARD, MIDDLE, AND AFT, AND RT FORWARD AND AFT FUSELAGE/WING DRAG ANGLES (WING/FUSELAGE FAIRING) BY R&R THE DRAG ANGLES FOR ACCESS, BLENDING, PERFORMING NDT, TREATING, PRIMING, AND REPLACING FASTENERS AS REQUIRED IN ACCORDANCE WITH FIELD REPAIR.