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Appendix G. EA50 Standard and Best Fit Departure Profiles The following two graphs show the thrust use in pounds (left axis), altitude in feet above field level (left axis as well), and speed in knots (right axis). As shown, the use of thrust is only slightly modified from standard to best fit profile. Rather, the best fit departure follows the general concept of the standard departures with a takeoff segment, then adjustments in succeeding segments of the target altitudes and climb rates to reach the measured altitude and SEL value. For the EA50, this approach results in a somewhat unusual set of speed and altitude profiles, but see Section 0. Figure 35 EA50 INM standard profile variables Figure 36 EA50 best fit profile variables G-1