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Refer to figure. (For this question use CAP 698 Figure 4.7). Planned take-off ...
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Refer to figure. (For this question use CAP 698 Figure 4.7).Planned take-off mass is 64000 kg, pressure altitude 4000 ft, OAT +10°C, V, 151, 155, 161. Runway slope is -1% andtailwind 5 kt. What is the maximum permitted take-off mass?
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