As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING OUTBOARD FLAP INBOARD AFT HINGE FORWARD FITTING INBOARD CENTER HOLE FOUND WITH CORROSION DURING ACCOMPLISHMENT OF EO 1-5750-7-5008. ORIGINAL HOLE DIAMETER = 0.580"; FINAL HOLE DIAMETER = 0.656". [SUP 05-14-07] COMPLIED WITH FEDEX EA 1-5750-109875, CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.