42. (Refer to Figure 40.) Determine the approximate ground roll distance required for takeoff.
OAT: 32 °C. Pressure altitude: 2,000 ft. Takeoff weight: 2,500 lb. Headwind component: 20 kts

42. (Refer to Figure 40.) Determine the approximate ground roll distance required for takeoff. OAT: 32 °C. Pressure altitude: 2,000 ft. Takeoff weight: 2,500 lb. Headwind component: 20 kts

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