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3708
(Refer to figure 41.) Determine the approximate ground roll distance required for takeoff.
| OAT |
90 °F |
| Pressure altitude |
2,000 ft |
| Takeoff weight |
2,500 lb |
| Headwind component |
20 kts |
| * | A) 650 feet. |
| | B) 850 feet. |
| | C) 1,000 feet. |
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