As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT WING OUTBOARD FLAP VANE FITTING 'B' BUSHING HOLE CORROSION. BUSHING HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. EXISTING HOLE SIZE 0.935" X 0.650", FINAL HOLE SIZE: 1.0325" X 0.740", MAXIMUM ALLOWABLE LIMIT: 0.940" X 0.670". OVERSIZE BUSHING FABRICATED AND INSTALLED PER EA 1-5750-T0326517 PART 1 STEP 2A. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO WRI: 57504768 FOR WORK DETAILS.