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  2. Flight length - Wikipedia

    en.wikipedia.org/wiki/Flight_length

    In commercial aviation, this means the time from pushing back at the departure gate to arriving at the destination gate. [2] Flight time is measured in hours and minutes as it is independent of geographic distance travelled. Flight time can be affected by many things such as wind, traffic, taxiing time, and aircraft used. [3]

  3. Flight planning - Wikipedia

    en.wikipedia.org/wiki/Flight_planning

    Commercial airlines generally wish to keep the cost of a flight as low as possible. There are three main factors that contribute to the cost: the amount of fuel needed (to complicate matters, fuel may cost different amounts at different airports), actual flying time affects depreciation charges, maintenance schedules, and the like,

  4. Top of climb - Wikipedia

    en.wikipedia.org/wiki/Top_of_climb

    The airplane's Pilot Operating Handbook has a table of fuel burned, time, and distance to reach a given altitude from sea level. To calculate the values for airport at 900 m (3,000 ft), you subtract the values for sea level to 900 m (3,000 ft) from the sea level to cruise altitude. [1]

  5. Air navigation - Wikipedia

    en.wikipedia.org/wiki/Air_navigation

    Once the pilot has calculated the actual headings required, the next step is to calculate the flight times for each leg. This is necessary to perform accurate dead reckoning. The pilot also needs to take into account the slower initial airspeed during climb to calculate the time to top of climb.

  6. Top of descent - Wikipedia

    en.wikipedia.org/wiki/Top_of_descent

    The top of descent is usually calculated by an on-board flight management system, and is designed to provide the most economical descent to approach altitude, or to meet some other objective (fastest descent, greatest range, etc.). The top of descent may be calculated manually as long as distance, air speed, and

  7. Range (aeronautics) - Wikipedia

    en.wikipedia.org/wiki/Range_(aeronautics)

    The term , where is the speed, and is the fuel consumption rate, is called the specific range (= range per unit mass of fuel; S.I. units: m/kg). The specific range can now be determined as though the airplane is in quasi-steady-state flight.

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  9. E6B - Wikipedia

    en.wikipedia.org/wiki/E6B

    The base name "E-6" was fairly arbitrary, as there were no standards for stock numbering at the time. For example, other USAAC computers of that time were the C-2, D-2, D-4, E-1 and G-1, and flight pants became E-1s as well. Most likely they chose "E" because Dalton's previously combined time and wind computer had been the E-1.

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