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Appendix E. LJ35 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). In addition to having the thrust applied differently from the standard for the best fit, the takeoff and cruise thrust were lowered to 85% of the standard maximum thrust, and the weight was lowered to 75% of the standard maximum takeoff weight. Figure 31 LJ35 INM standard profile variables Figure 32 LJ35 best fit profile variables E-1
