As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION WAS FOUND ON THE NOSE LANDING GEAR INBD AND OTBD TRUNNION FITTINGS. BOTH BORES WERE ENLARGED TO A DIA OF 2.813 INCHES FROM AN ORIGINAL SIZE OF 2.762 INCHES. THE INBD TRUNNION FITTING FACE WAS CORRODED REQUIRING REMOVAL WITH SPOTFACE DIA 3.440 INCHES. REMAINING THICKNESS OF 0.940 INCHES. REWORK COMPLETED PER ERA 503918-14.