As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FWD NR 2 ENGINE MOUNT MATING SURFACE FOUND WITH CORROSION. CORROSION REMOVED AT NR 2 ENGINE FORWARD MOUNT MATING SURFACE AND FOUND WITHIN LIMITS AS PER CMM 71-20-04 REPAIR 5 FIGURE 504 REV 54. MATERIAL ORIGINAL THICKNESS= 0.765", MATERIAL REMOVED= 0.003", MATERIAL REMAINING= 0.762". MPI CARRIED OUT ON REWORKED AREA. NO CRACK EVIDENT. REPAIR ARE PAINTED AS PER CMM 71-20-04 REV 54. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 111.