What was found
AT 1000 FEET DURING FINAL, EXPERIENCED A COMLETE LOSS OF LT HYD SYS FLUID AND PSI FOUND DOWNLOCK ACTUATOR FLEX LINE WITH HOLE, REPLACED LINE AND RAN ENGINETO VERIFY CORRECT OPERATION OF ENGINE PUMP, ADP AND PTU. ALL FUNCTIONS NORMAL, NO FURTHER ACTION REQUIRED IAW AMM 29-11-05-206-001, I TEM 2. CLEANED AREA OF RESIDUAL HYDRAULIC FLUID. AIRCRAFT RETURN ED TO SERVICE.