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3.Refer to Figure 36 on page 38. Determine the approximate manifold pressure setting with 2,450 RPM to achieve 65 percent maximum continuous power at 6,500 feet with a temperature of 36 °F higher than standard.
4.Refer to Figure 36 on page 38. Approximately what true airspeed should a pilot expect with 65 percent maximum continuous power at 9,500 feet and a temperature of 36 °F below standard?
5.Refer to Figure 8 on page 10. What is the effect of a temperature increase from 35 to 50 °F on the density altitude if the pressure altitude remains at 3,000 feet MSL?