What was found
LEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE FOUND CORROSION. HOLE 3 CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER 0.596", FINAL HOLE DIAMETER 0.598" & MAXIMUM ALLOWABLE HOLE DIAMETER 0.584". NEW SHOULDER BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0325482 PT 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57503736 FOR WORK DETAILS.