What was found
RIGHT WING, OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER INBD. STUD ATTACH SURFACES FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING THICKNESS 0.420", MATERIAL REMOVED: 0.010" & MINIMUM ALLOWABLE THICKNESS 0.423". NEW REPAIR SHIM FABRICATED & INSTALLED IAW EA 1-5750-T0324430 PT 1 STEP 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57503670 FOR WORK DETAILS.