As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT MAIN LANDING GEAR STRUT CYLINDER SHOWED PITTING ALONG THE INNER SURFACE AT LOWER FLANGE AT CHROME AREA. DAMAGED GLAND THREADS. RIGHT MAIN LANDING GEAR STRUT ASSEMBLY REMOVED AND REPLACED WITH SERVICABLE UNIT IAW MM 32-40-1-02, 32-42-01-4 AND 32-43-02-2. ANTI-SKID SYSTEM OPS CHECKED GOOD.