As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT BODY GEAR RETRACT ACTUATOR PISTON THREADED END WHERE ROD END ATTACHES HAS A GAP AND IS MISSING THREADS (THREADED MATERIAL FELL INSIDE ROD END). DEPRESSURIZED HYD NR 1, 4 SYSTEM. DISCONNECTED 3 LINES FROM BODY ACTUATOR. CAPPED LINES. COMPLETED REMOVAL & INSTALLED ACTUATOR PER MM. PERFORMED LEAK CHECK. NO LEAKS NOTED.