What was found
RIGHT WING OTBD FLAP OTBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH SPOT FACE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.408", MATERIAL REMOVED: FWD 0.008", AFT 0.025", REMAINING THICKNESS: 0.375" AND MINIMUM ALLOWABLE THICKNESS: 0.408". NEW REPAIR SHIM FABRICATED AND INSTALLED IAW EA NR 1-5750-T0325483, PT 1, STEP 1, TITLE: WINGS FLIGHT SURFACES, EO 1-5750-7-5002, RT WING, OTBD FLAP, OTBD HINGE, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM6-2-100. REFER TO NR 57503738 FOR WORK DETAILS.