What was found
LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE SURFACE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.400", MATERIAL REMOVED: 0.006", FWD FACE; 0.023", AFT FACE, REMAINING THICKNESS: 0.371". MINIMUM ALLOWABLE THICKNESS: 0.408". REPAIR SHIM FABRICATED AND INSTALLED IAW EA: 1-5750-T0326401, PART 1, STEP 1, TITLE: WINGS, FLIGHT SURFACES, EO 1- 5750-7-5002, LT WING, OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI: 57504779 FOR WORK DETAILS.