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  1. You can use the calculator side of your flight computer to convert nautical miles (NM) to statute miles (SM), or knots (kt.) to miles per hour (mph). Remember, the units you use must be equivalent, i.e., nautical miles and knots or statute miles and miles per hour.

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  2. E6B, NavLog Calculator, Weather Reports, METAR, TAF, Wind Components, Instrument Simulator, Weight and Balance, Pressure Altitude, Density Altitude, True Air Speed, and a lot more.

  3. 23 mar 2024 · Knowing your aircraft’s fuel consumption rate is vital for flight planning and ensuring you have sufficient fuel reserves. The E6B flight computer simplifies fuel consumption calculations by considering the aircraft’s specific fuel flow rate. Let’s explore how to use the E6B flight computer to calculate fuel consumption: 1.

  4. Instructions for Using ASA Flight Computer. Your ASA E6-B Flight Computer has two main parts: a circular slide rule side for making quick calculations, and a wind side for computing ground speed and wind correction angle. The slide portion of the circular slide rule side also includes quick-reference material.

  5. Sporty’s E6B Flight Computer is designed to perform 24 aviation functions and 20 standard conversions, and includes timer and clock functions. We hope that you enjoy your E6B Flight Computer. Its use has been made easy through direct path menu selection and calcu - lation prompting. As you will soon learn, Sporty’s E6B is one of the

  6. www.sportys.com › media › pdfSPORTY'S E6B

    This function is used to calculate true airspeed for preflight planning. It will compute the density altitude, mach number and true airspeed in knots, given the pressure altitude, temperature, and calibrated airspeed in knots. In this example, pressure altitude is 10,000 feet, temperature is 2°C, and CAS is 200 knots. Tap PLAN TAS from the ...

  7. This document provides instructions on how to use an E6B flight computer to perform various flight calculations. It covers calculating wind correction angle and ground speed, flight time per leg, fuel burn per leg, and density altitude.

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