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38 iQue 3600a Que Applications Guide
QueE6B
QueE6B calculates density altitude and winds
aloft, based upon information you enter. To
open QueE6B, press ESCAPE to display
the Que Applications Launcher. Highlight
QueE6B and press ENTER.
QueE6B
Calculated
Figures
User-Entered
Figures
Indicated Altitude—required entry for density
altitude/true airspeed calculation. Enter the aircraft’s
altimeter reading.
Calibrated Airspeed
—required entry for density
altitude/true airspeed calculation. Enter the aircraft’s
airspeed indicator.
Heading—required entry for winds aloft calculation.
Use the heading from the aircraft’s heading indicator
or 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 for
density altitude/true airspeed calculation. Total Air
Temperature (TAT) is the temperature of the air
including the heating effect caused by speed. Use
the temperature reading on a standard outside air
temperature gauge found on most piston aircraft.
Wind From—(calculated figure) determined from
entry of heading and true airspeed.
ADVANCED AVIATION OPERATION > QUEE6B