As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT SIDE FRAME FITTING HAS SEVERAL AREAS OF CORROSION ON THE FORWARD FACE ABOVE HOLE 1. CLEANED AREAS OF CORROSION IAW B767-200 SRM 53-50-08. REMOVED CORROSION WITHIN LIMITS .638 REMAINING FROM ORIGINAL THICKNESS OF .700 VERIFIED WITH NDT. PRIMED AND PAINTED SIDE FITTING IAW AMM 51-21-10, ACFT WAS GROUNDED.