As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING THE RECENT C-CHECK, THE LEFT OUTER CYLINDER SPUD BOSS WAS FOUND CORRODED IN THE AREA OF CHROME LOSS. AREA CLEANED OF CORROSION, TREATED, CHECKED FOR HEAT RELATED DAMAGE. REWORK AREA IS 5MM IN DIAMETER WITH MISSING CHROME AND MATERIAL LOSS OF .4 MM AFTER CORROSION CLEAN UP. ATLAS AIR EO 4732A014 ISSUED FOR REWORK AND FOLLOW UP INSPECTION. (M)