Garmin 3600a Instruccion De Instalación

  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. 

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.

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E6B