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H317
->6.6.7.5.4.B.1
6754
(Refer to figure
26
.) Determine the ground roll required for takeoff.
Temperature
25 °C
Pressure altitude
2,000 ft
Weight
2,200 lb
Headwind
15 kts
A) 237 feet.
*
B) 261 feet.
C) 205 feet.
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