What was found
LEFT ENGINE WOULD NOT RESPOND TO POWER LEVER INPUT. ENGINE RPM INCREASED TO 100 PERCENT WITH POWER LEVER AT IDLE. ENGINE SHUT DOWN (PRECAUTIONARY) VIA NORMAL PROCEDURE. LANDING MADE. T/S, REPLACED DEFECTIVE FUEL CONTROL AND PUMP ASSY. REMOVED P/N 5002T94G42, S/N GAT 60192 AND PUMP ASSY, P/N 37E501242P107, S/N CGW 312740, AND INSTALLED FUEL CONTROL, P/N 5002T94G42, S/N GAT 60015 FUEL PUMP, P/N 9234-AB, S/N CGW 312618. AIRCRAFT WAS GROUND RUN, LEAK CHECKED. OPS CHECKED, NO DEFECTS NOTED.