What was found
LT WING OTBD FLAP, INBD AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE CORROSION. CORROSION FOUND EXCEED LIMIT IAW CMM 57-52-04. EXISTING HOLE DIA 1.148", FINAL HOLE DIA 1.162", MAXIMUM ALLOWABLE DIA 1.150". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0325946, PART 1, STEP 1-A WINGS-FLIGHT SURFACES EO1-5750-7-5002. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.