As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
COMBINED HYDRAULIC SYSTEM FAILURE ON SHORT FINAL TO BIKF. UPON LANDING NOTED HYDRAULIC LEAK COMING FROM RT LANDING GEAR WHEEL WELL AREA. FOUND "FLIGHT POWER SHUTOFF VALVE" LEAKING IN RT MAIN GEAR WELL. INSTALLED NEW VALVE P/N 1159SCH246-5 S/N 888. INSTALLATION AND OPERATIONAL CHECKS COMPLIED WITH IN ACCORDANCE WITH AMM 27-08-00. PERFORMED COMBINED/FLIGHT HYDRAULIC SYSTEM SERVICING AND BLEEDING IAW AMM 29-01-00.