As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
A.A. / AD (VT) (GVI) WAS PERFORMED AND DAMAGES WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP, SECTION 05, HOLE #13 CORROSION ON FITTING AT 9 O CLOCK POSITION AND HOLE #17 CORROSION ON FITTING BTW 8 AND 9 O CLOCK POSITION. OPEN HOLES AT LT ENG DRAG FTG CLAMP-UP HOLES #13 AND #17 WERE REAMED TO FIRST OVERSIZE (0.5778") PER AMDS.