For the density controller to work correctly you need about 180 dF oil temp, I turn the boost pump on manually when I enter the runway just in case the throttle switch fails, line up, check cowl flaps open, push mixture rich, if enough runway slowly turn in boost, watch RPM rise to 2575, check oil pressure, check fuel flow 29-30, check boost, minimum 35, maximum 37" as a function of induction air temperature, which is typically between 90 and 150 dF, watch airspeed, rotate between 70 and 75 kt depending on weight, positive rate, no runway remaining gear up, flaps up check boost below 37 with intercooler full flow, 1000 ft reduce power 34" 2400, boost pump off, fuel flow around 23, lean for 1580 TIT, cruise climb about 120KT, keep CHTs below 400 dF. Depending on weight the Bravo will climb at around 600 fpm through 18000 ft, when altitude captured close cowl flaps, let speed build up, reduce boost to 30", reduce rpm to 2300, fuel flow about 18.5 gph, produces about 1580 TIT, 350-380 CHT and about 185 KT TAS in my TKS Bravo, others may be 5KT faster, power is about 78%, reducing power I take out 2" per minute, keep TIT between 1550 and 1580, CHT reduction not more than 15 dF per minute, Lycoming says 50 dF per minute is permississible, descent 750 fpm, don't go below 18" at that descent rate, engine starts driving propeller and rings may start fluttering, with gear down power can go below 18", don't push mixture rich for landing, just fouls plugs, keep mixture where you had it during descent