As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER LANDING IN SKCL LOSS OF HYDRAULICS PRESSURE AND QUANTITY. FOUND HYDRAULIC LEAK IN LEFT BOGIE TRIM CYLINDER. REMOVED AND REPLACED LEFT HYDRAULIC BOGIE TRIM CYLINDER AS PER ALTERNATE METHOD MM REF 32-33-1. SERVICED HYDRAULIC IAW MM 12-30-1 AND BLEED SYSTEMS IAW MM 29-00, NO LEAKS NOTED.