What was found
RIGHT WING, OTBD FLAP, INBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE, FOUND CORROSION. CORROSION REWORKED FOUND EXCEEDED LIMIT IAW CMM 57-44- 08. EXISTING HOLE DIAMETER 0.720", FINAL HOLE DIAMETER 0.737 & MAXIMUM ALLOWABLE HOLE DIAMETER 0.709". NEW SHOULDER BUSHINGS, TWO EACH FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0324430 PT 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57503670 FOR WORK DETAILS.