What was found
REMOVED THE LT UPPER WING DRAG MIDDLE AND AFT ANGLES (WING-TO-FUSELAGE FAIRINGS) AND BLENDED CORRODED AREAS OF THE UPPER SURFACE OF THE LT UPPER WING SKIN, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPLACED 17 CORRODED HI-LOCS IN THE REPAIR AREA. TREATED AND PRIMED, PER TEXTRON REPAIR AND REINSTALLED DRAG ANGLES. REMOVED THE RT UPPER WING MIDDLE DRAG ANGLE (WING-TO-FUSELAGE FAIRING) AND BLENDED CORRODED AREAS OF THE UPPER SURFACE OF THE RT UPPER WING SKIN, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPLACED 38 CORRODED HI-LOKS IN THE REPAIR AREA. TREATED AND PRIMED REPAIR AREAS, PER TEXTRON REPAIR AND REINSTALLED DRAG ANGLE.