38 iQue 3600a Que Applications GuideQueE6BQueE6B calculates density altitude and windsaloft, based upon information you enter. Toopen QueE6B, press ESCAPE to displaythe Que Applications Launcher. HighlightQueE6B and press ENTER.QueE6BCalculatedFiguresUser-EnteredFiguresIndicated Altitude—required entry for densityaltitude/true airspeed calculation. Enter the aircraft’saltimeter reading.Calibrated Airspeed—required entry for densityaltitude/true airspeed calculation. Enter the aircraft’sairspeed indicator.Heading—required entry for winds aloft calculation.Use the heading from the aircraft’s heading indicatoror directional gyro.True Airspeed—(calculated or user-entered figure)required entry for winds aloft calculations.Baro Pressure—required entry for density altitude/true airspeed calculation. Use current altimeter setting(barometric pressure).Total Air Temperature—required entry fordensity altitude/true airspeed calculation. Total AirTemperature (TAT) is the temperature of the airincluding the heating effect caused by speed. Usethe temperature reading on a standard outside airtemperature gauge found on most piston aircraft.Wind From—(calculated figure) determined fromentry of heading and true airspeed.ADVANCED AVIATION OPERATION > QUE E6B
