Using Figure 9.1, calculate the landing ground roll given the following information: Temperature = 10 C Pressure
Question:
Using Figure 9.1, calculate the landing ground roll given the following information:
Temperature = 10 °C Pressure altitude = 8000 ft Weight = 2400 lb Tailwind component = 5 kts.
a. 1500 ft
b. 1375 ft
c. 1250 ft
d. 2100 ft
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Related Book For 
Flight Theory And Aerodynamics
ISBN: 9781119772415
4th Edition
Authors: Joseph R. Badick; Brian A. Johnson
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