Using Figure 8.1, calculate the takeoff ground roll given the following information: Temperature = 10 C Pressure

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Using Figure 8.1, calculate the takeoff ground roll given the following information:

Temperature = 10 °C Pressure altitude = 8000 ft Weight = 2400 lb Tailwind component = 5 kts.

a. 2400 ft

b. 900 ft

c. 1500 ft

d. 1100 ft

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Flight Theory And Aerodynamics

ISBN: 9781119772415

4th Edition

Authors: Joseph R. Badick; Brian A. Johnson

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