As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING 300 HOUR INSPECTION (GEAR SERVICE) THE INNER STRUT CHROME WAS FOUND DAMAGED APPROXIMATELY .001 INCH DEEP. PROBABLE CAUSE: WEAR OF SEALS CAUSING THE UPPER CAM TO CONTACT THE INNER CYLINDER. INSPECTION REPACK OF THE NOSE LANDING GEAR ASSY AT 3,000 LANDING INSPECTION. (EA09200504488) (K)