What was found
LEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH SURFACE FOUND CORROSION. REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING THICKNESS 0440 INCHES, MATERIAL REMOVED, FWD FACE, 0.016 INCHES, AFT FACE, 0.037 INCHES & REMAINING THICKNESS 0387 INCHES. MINIMUM ALLOWABLE THICKNESS 0.423 INCHES. REPAIRED SHIM, FABRICATED & INSTALLED IAW EA 1-5750-T0324816 PART 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57503810 FOR WORK DETAILS.