What was found
RIGHT WING OTBD FLAP VANE HORN FITTING-D, FWD HOLE CORROSION. CORROSION FOUND TO EXCEED LIMIT IAW SRM 57-50-02, REPAIR 5, FIGURE 201. EXISTING SLOT: 0.890", LENGTH, 0.625", WIDTH. FINAL SLOT: 0.965", LENGTH, 0.662", WIDTH. MAXIMUM ALLOWABLE: 0.940", LENGTH, 0.670" WIDTH. REPAIR BUSHING, SLOT, FABRICATED BY MACHINING IAW EA 1-5750-T0326035, PART 1, STEP 2A WINGS, FLIGHT SURFACES, EO1-5750-7-5002. BUSHING INSTALLED IAW AMM 27-50-32-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.