What was found
LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT LOWER HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA, 0.325" FINAL HOLE DIA: 0.406" MAXIMUM ALLOWABLE DIA: 0.391". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0325889 PT1 STEP 1B WINGS-FLT SURFACES-EO 1-5750-7-5002. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.