As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C2 CHECK FOUND CORROSION IN CENTER LANDING GEAR FITTING. CLEANED UP CORROSION BY MACHINING FAYING SURFACE, ENLARGED HOLE DIAMETER OF TURNION FITTING AND INSTALLED BUSHING. THE DIMENSIONS OF REWORK AREA ARE WITHIN LIMITS PER SRM 53-40-00 VOL 1 FIG 15.