As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAIN WHEEL LEAKING HYD FLUID. BRAKES VERY RIGID ON BOTH RUDDER PEDALS WHEN BRAKES APPLIED ON TAXI/TAKEOFF/LANDING ROLLOUT. BOTH PILOT BRAKE APPLICATIONS REQUIRED MORE BRAKE APPLICATION THEN NORMAL TO STOP. R & R THE LT OTBD WHEEL & BRAKE ASSY AND INSTALLED AN O/H UNIT IN THE LT OTBD POSITION IAW MM 32-41-10. OPS & LEAK CHECKED GOOD.