What was found
LEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 0.704", FINAL HOLE DIAMETER 0.723", MAX ALLOWABLE HOLE DIAMETER 0.709". SHOULDER BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0319682 PART 1 STEP 1C. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.