As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ON SHORT FINAL, THE HYDRAULIC FLUID QUANTITY LEVEL DROPPED TO THE STANDPIPE LEVEL AFTER GEAR AND FLAP EXTENSION. LEVEL REMAINED THERE AFTER LANDING. FOUND THE RIGHT GEAR UNLOCK BOGIE TRIM LINE RUPTURED. REMOVED AND REPLACED THE HYDRAULIC LINE IAW DC 8 MM CHAPTER 32. SYSTEM LEAK AND OPS CHECKED GOOD.