What was found
AFTER TOUCHDOWN WHEN REVERSE THRUST WAS APPLIED, THE NR 3 ENGINE DID NOT ACCELERATE. THE NR 2 ENGINE DEVELOPED MAXIMUM REVERSE THRUST WHILE THE NR 1 THRUST REVERSER WAS INOPERATIVE ON MEL. MAXIMUM BRAKING WAS APPLIED BUT THE AIRCRAFT DID NOT STOP UNTIL APPROXIMATELY 200 FEET INTO THE OVERRUN AREA. AIRPORT CFR WAS NOTIFIED AND PERFORMED A HOT BRAKE INSPECTION AFTER WHICH MAINTENANCE TOWED THE AIRCRAFT TO THE GATE. THE NR 3 ENGINE, ADJUSTMENT OF THE POWER LEVER SYSTEM RIGGING PER MM 76-11-00.