What was found
LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER BARREL NUT HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE 0.390", FINAL HOLE 0.408", MAXIMUM ALLOWABLE HOLE 0.391". OVERSIZED BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0319681 PART 1 STEP 1D. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.