What was found
MRR-M04-11, ENGINE RPM ONLY WENT TO 97 PERCENT DURING TAKEOFF ROLL AND TORQUE WAS ALSO LOW, ALSO, THERE WAS LITTLE RESPONSE TO POWER LEVER MOVEMENT. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. INITIALLY SUSPECTED FCU FAILURE, BUT UPON INSPECTION FOUND FCU INPUT ARM ROD END DISCONNECTED. RECONNECTED ROD END AND SAFETIED. A FUEL LEAK WAS NOTED WHEN COWLING WAS OPENED, AND WAS FOUND TO BE COMING FROM THE SECONDARY FUEL MANIFOLD LOCATED AT THE 8:00 O’CLOCK POSITION. THE FUEL MANIFOLD LINE WAS REPLACED. MR`S WERE ISSUED TO INSPECT ALL OTHER AIRCRAFT FUEL MANIFOLD LINES, FUEL NOZZLE TASK CARD WAS ISSUED TO INCLUDE INSPECTION OF THE MANIFOLD LINES AT EACH INSPECTION.