What was found
LEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM57-44-08. EXISTING HOLE DIA: 0.709", FINAL HOLE DIA: 0.727" AND MAXIMUM ALLOWABLE HOLE DIA: 0.709". NEW SHOULDER BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0325538, PT 1, STEP 1B, TITLE: WINGS, FLIGHT SURFACES, EO 1-5750-7-5002. LT WING, OTBD FLAP INBD HINGE, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM6-2-100. REFER TO NR 57503739 FOR WORK DETAILS.