I'm interested in what others are seeing for takeoff fuel flow at sea level in an M20J. I can't find a specification for this from Lycoming. The Operator's manual shows  94 pph (15.7 gph) at 100% power, best power mixture (not full rich). For the HIO-360 it shows a suggested high limit of 105 pph (17.5 gph) for 100% power. The test stand data that came with my rebuilt IO-360-A3B6 shows 92.83 pph at an airflow of 1000 pph. Max power generated an airflow of 1118.5 pph but fuel flow was not recorde