What was found
LANDING, WE NOTICED THE BRAKES WERE CATCHING AND CAUSING THE PLANE TO SHAKE. THE HARDER WE APPLIED THE BRAKES THE WORSE THE CATCHING AND SHAKING. CORRECTIVE ACTION: CARRIED OUT A GVL OF THE RH & LH MLG FOR LOOSE HYDRAULIC LINES AND LEAKS. COMPLIED WITH FLM 32-41-00-810-824-A, UNDESIRED YAW TENDENCY WITH BRAKES APPLIED. C/W GVI .OF BRAKE ASSEMBLIES, BRAKE WEAR PINS, MLG TIRES. C/W CHECK OF THE HYDRAULIC RESERVOIR FLUID LEVEL. CHECKED TIRES FOR EQUIVALENT WEAR. CHECKED GAP ON WOW SENSORS AND TARGETS. C/W NORMAL & EMERGENCY/PARKING BRAKE SYSTEMS - BLEEDING. NOTED SUBSTANTIAL AIR REMOVED FROM LH BRAKE WHEN BLEEDING NORMAL BRAKE LINES. TAXIED THE AIRCRAFT AT A SPEED OF 20 KTS AND BRAKED THE AIRCRAFT USING NORMAL AND PARKING/EMERGENCY BRAKES TO STOP THE AIRCRAFT MULTIPLE LIMES WITH NO ADVERSE BRAKING NOTED.