What was found
RIGHT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH SURFACE FOUND CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING THICKNESS: 0.404", MATERIAL REMOVED 0.010", REMAINING THICKNESS 0.394", MINIMUM ALLOWABLE THICKNESS 0.423". REPAIR SHIM FABRICATED & INSTALLED IAW EA 1-5750-T0324818 PART 1 STEP 1B & STEP 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57503807 FOR WORK DETAILS.