As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CURING NLG INSPECTION, FOUND STEERING TRUSS BOLT HOLES ELONGATED WHERE OVERCENTER LINK BOLTS ONTO TRUSS; MFG SPECS FOR ALLOWABLE WEAR AT THIS LOCATION IS .375 INCH - .379 INCH. MEASURED WEAR WAS .392 INCH. REPLACED TRUSS WITH SERVICEABLE UNIT. SUSPECT WEAR WAS FROM THE BOLT BEING LOOSE.