E6b Flight Computer Exercises Jun 2026
12. You are flying at a Pressure Altitude of 8,000 ft with an Outside Air Temperature (OAT) of +10°C . The Calibrated Airspeed (CAS) is 130 knots . Calculate the True Airspeed (TAS) . 13. The field elevation is 5,500 ft . The altimeter setting is standard (29.92" Hg). The temperature is 30°C . Calculate the Density Altitude .
Which you want to focus on (calculator vs. wind face)
Align 115 under the STAT arrow. Read 100 under the NAUT arrow. Answer 3.3: 59∘F59 raised to the composed with power F
Always remember to set the rate index (60) to the speed or rate before solving time-speed-distance problems. e6b flight computer exercises
Ensure all inputs are in compatible units before starting. Convert knots to mph or vice versa first.
to Fahrenheit using the temperature scale at the bottom of the calculator side. Answer Key & Steps
To drill your skills efficiently, you can practice with interactive digital versions such as the E6B Practice App . Calculate the True Airspeed (TAS)
120 knots. Align 18 on the outer scale with 9 on the inner scale. Look at the 60 index arrow to read 120 knots. 2. Fuel Consumption and Endurance
Mastering these exercises takes time, but doing them periodically will vastly improve your situational awareness and pilot-in-command decision-making. If you want to keep sharpening your skills, tell me:
The most basic, yet most frequent, calculation on any cross-country flight is the relationship between Speed , Time , and Distance (the “Big Three”). The E6B’s outer scale (distance) and inner scale (time) are designed for this. The altimeter setting is standard (29
Runway 27 is in use. The winds are from 300° at 25 knots. What is your headwind and crosswind component?
Do you prefer practicing with a or an electronic E6B app ? Which specific calculation gives you the most trouble? Share public link
This is where the E6B shines. There is no shortcut around learning the wind side of the manual computer. These assume you have a sliding window with a rotating azimuth.