What was found
ENG #2 OIL CONSUMPTION IS HIGHER THAN NORMAL. GROUNDED - YES. ACOMPLISHED TSR STEPS 1 THROUGH 5 NOTED & LARGE AMOUNT OF RESIDUAL OIL ON THE ENGINE FAN CASE AND COMPONENTS. THE IDG DRIVE PAD LEAKS STATICALLY AND DYNAMICALLY. REPLACED FLO SEAL FOR FLO #2 IDG PER B737-800 AMM 72-60-00. REMOVED/REINSTALLED THE #2 IDG PER MM 24-11-11. LK AND OPS CK GOOD. THOROUGHLY CLEANED FAN CASE AND COMPONENTS. NO OTHER LEAKS NOTED, IDG DRIVE PAD DRAIN LINE BAGGED FOR PART POWER LK CK. ACCOMP STEP 6 (PPRUN) FOUND STARTER PAD WET WITH OIL AFTER. REPLACED #2 ENGINE STARTER DRIVE PAD SEAL PER ASA T/C N8472002. NO LEAKS NOTED. TSR COMPLETED.