What was found
RIGHT ENG OIL QTY 0 QTS, OIL PRESS HOVERING AROUND 20 PSI. NR 1 ENGINE IS THE DISCREPANT ENGINE. INITIAL OIL SVC ACCOMPLISHED. ADDED NR 1 ENG 26QTS, AND NR 2 ENG-4QTS. 40 MIN IDLE RUN CARRIED OUT PER TEST NR 5 IDLE LEAK CHECK IAW AMM 71-00-00-700-805-G00. AFTER SHUTDOWN CHECKED PLASTIC BAG AROUND DRAIN MAST FOUND JUST 1 DROP OF OIL FOUND. COWL OPENED AND INSPECTED AREA, NO OBVIOUS LEAK NOTED. ONLY SLIGHTLY WET FOUND AROUND STARTER AREA IAW AMM 71-71-00-700-802-G00. RAN ENGINE AT 70% N1 FOR A PERIOD OF TIME TWICE SPECIFIED W ITH AMM 71-71-00-700-802-G00, AFTER TEST 5 IDLE LEAK CHECKS PERFORMED IAW AMM 71-00-00-700-805-G00, FOUND A FEW DROPS IN BAG AT FIRST RUN, NO DROP AT SECOND. IAW PILOT REPORT, TECH ACCOMPLISHED IN-FLT WINDMILLING INSPECTION AMM 71-00-00-200-812-G00, NO/LOW OIL PRESSURE INSPECTION IAW AMM 71-00-00-200-811-G00, HIGH POWER LEAK CHECKED AMM 71-00-00-700-8 49-G00, OIL CONSUMPTION HIGH/LOW OIL QTY FIM 71-05 TASK 805. DMS INSPECTION 79-00-00-200-806-G00 ACCOMPLISHED, NO DEBRIS FOUND AT DMS, AGB, & TGB. CAPPED AGB DRAIN LINES IAW AMM 71-71-00-700-802-G00, STEP 2.1.(3)(B). CAPPED AGB OIL DRAIN LINES FOR MAX 25 FLIGHT CYCLES. PERFORMED IDT INSPECTION FOR DMS SENSOR ON #1 ENG,INSTALATION OK REF AMM TASK 79-00-00-200-806-G00.